d0 solenoid upgrade project - fermilablss.fnal.gov/archive_notes/d0-en/fermilab-d0-en-349.pdf · d0...
TRANSCRIPT
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D0 SOLENOID UPGRADE PROJECT
Thermal Contraction analysis
for the D0 Solenoid Chimney
O-ZERO ENGINEERING NOTE 3823111 EN-349
September 30 1993
Russ Rucinski ROOflJ Mechanical Group
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This engineering note documents the thermal contraction analysis that was done for the D-Zero solenoid chimney The analysis was done as support of the Design Report of the 2 Tesla Superconducting Solenoid for the Fermilab DO Detector upgrade tI
SUMMARY
The cryogenic LHE and LN2 lines were analyzed for combined pressure thermal movement and dead weight The tubing was stress analyzed per ASME code for Pressure Piping standard ANSI ASME B313 for eight combinations of thermal loading A commercial pipe stress analysis and design system by Algorreg was used for the analysis Stresses calculated were well below allowables Based on the analysis the cryogenic lines will be installed at an offset from the vacuum jacket centerline so that during steady state cold operation the cryogenic lines will be in a proper location
ANALYSIS
The chimney route as of this writing follows the path shown in Figure 1 The majority of the analysis was done almost a year earlier (1192 thru 12192) with a slightly different path The difference in the path is in the longest inclined section At the time of analysis it was thought that the chimney would be straight up the incline and then elbow at 90 degrees into the side of the control dewar The analysis was done for that configuration See Figures 2 and 3 for a sketch showing the route and the locations of the spider support guides for the cryogenic piping The slight difference in the chimney path route will not significantly change the outcome of the analysis and therefore the results from the analysis that was done is still considered valid
The analysis was done using Pipe Plus Pipe Stress Analysis and Design System software version 450 from Algorreg This DOS application was borrowed from the RDlMechanica1 support group A copy of the application and case files used in the analysis can be found on the hard drive of the mM machine in the D-Zero cryo control room The computer is a Gateway 2000 model 4DX-33V with a Fermilab property number 78384 The files ~n hard drive C directory PIPE To run the software run the file named PIPEEXE The software filetl menu will allow access to all case files See table 1 for the cases Cases 12 and 3 are saved under filename tlCASEI23 Cases 4 and 5 are saved as CASE4amp5
2 For each case run the results were from the combined effect of
Dead Weight + Pressure + Thermal contraction + Displacement
Dead Weight considered the pipe itselfplus contents with SG - 10
Pressure was always 150 psig
Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall
TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold
CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable
Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads
Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar
Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction
Case 3 Rather trivial case
3
Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage
Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm
Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5
Case 8 Trivial case not run
Allowable
The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded
The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is
Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi
The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi
4
-
Results
The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs
The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2
TABLE 2 Built in offsets to compensate for thermal movement
Location X Offset ny Offset Z Offset
TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches
HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
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PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
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~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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SUBJECT NAME
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This engineering note documents the thermal contraction analysis that was done for the D-Zero solenoid chimney The analysis was done as support of the Design Report of the 2 Tesla Superconducting Solenoid for the Fermilab DO Detector upgrade tI
SUMMARY
The cryogenic LHE and LN2 lines were analyzed for combined pressure thermal movement and dead weight The tubing was stress analyzed per ASME code for Pressure Piping standard ANSI ASME B313 for eight combinations of thermal loading A commercial pipe stress analysis and design system by Algorreg was used for the analysis Stresses calculated were well below allowables Based on the analysis the cryogenic lines will be installed at an offset from the vacuum jacket centerline so that during steady state cold operation the cryogenic lines will be in a proper location
ANALYSIS
The chimney route as of this writing follows the path shown in Figure 1 The majority of the analysis was done almost a year earlier (1192 thru 12192) with a slightly different path The difference in the path is in the longest inclined section At the time of analysis it was thought that the chimney would be straight up the incline and then elbow at 90 degrees into the side of the control dewar The analysis was done for that configuration See Figures 2 and 3 for a sketch showing the route and the locations of the spider support guides for the cryogenic piping The slight difference in the chimney path route will not significantly change the outcome of the analysis and therefore the results from the analysis that was done is still considered valid
The analysis was done using Pipe Plus Pipe Stress Analysis and Design System software version 450 from Algorreg This DOS application was borrowed from the RDlMechanica1 support group A copy of the application and case files used in the analysis can be found on the hard drive of the mM machine in the D-Zero cryo control room The computer is a Gateway 2000 model 4DX-33V with a Fermilab property number 78384 The files ~n hard drive C directory PIPE To run the software run the file named PIPEEXE The software filetl menu will allow access to all case files See table 1 for the cases Cases 12 and 3 are saved under filename tlCASEI23 Cases 4 and 5 are saved as CASE4amp5
2 For each case run the results were from the combined effect of
Dead Weight + Pressure + Thermal contraction + Displacement
Dead Weight considered the pipe itselfplus contents with SG - 10
Pressure was always 150 psig
Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall
TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold
CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable
Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads
Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar
Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction
Case 3 Rather trivial case
3
Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage
Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm
Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5
Case 8 Trivial case not run
Allowable
The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded
The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is
Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi
The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi
4
-
Results
The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs
The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2
TABLE 2 Built in offsets to compensate for thermal movement
Location X Offset ny Offset Z Offset
TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches
HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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2 For each case run the results were from the combined effect of
Dead Weight + Pressure + Thermal contraction + Displacement
Dead Weight considered the pipe itselfplus contents with SG - 10
Pressure was always 150 psig
Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall
TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold
CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable
Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads
Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar
Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction
Case 3 Rather trivial case
3
Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage
Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm
Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5
Case 8 Trivial case not run
Allowable
The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded
The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is
Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi
The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi
4
-
Results
The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs
The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2
TABLE 2 Built in offsets to compensate for thermal movement
Location X Offset ny Offset Z Offset
TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches
HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage
Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm
Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5
Case 8 Trivial case not run
Allowable
The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded
The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is
Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi
The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi
4
-
Results
The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs
The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2
TABLE 2 Built in offsets to compensate for thermal movement
Location X Offset ny Offset Z Offset
TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches
HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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SECTION
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-
Results
The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs
The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2
TABLE 2 Built in offsets to compensate for thermal movement
Location X Offset ny Offset Z Offset
TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches
HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
21 (j
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN
21 (j
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
File Name Project Department Contract Number Description Prepared by Checked by
ANSI code Input unit Output unit Output columns Base temperature F factor E factor
Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance
CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski
ANSI B313 English English 80 70 10 133
0 0 Hz 0 0 0 lb
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
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~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
I
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
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1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
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DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
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PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
-------- -------- -------- -------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf
Frm Point DX DY DZ Radius X Y l~
To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)
T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping
o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04
T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page
- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE
Point Data Description
TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
TR2
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
-------------------------------------------------
101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
lt
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr
Point Data Description
3 70 150 0000000 Anchor Rigid in all directions
Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree
HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop
Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case
1 1 1 1 2
translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0
inch degree degree degree
inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point Data Description
Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design
TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions
Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-
TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide
~- TL6c TL7 TL7al TL7a Line stop
Guide TL7b Guide TL8
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
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f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
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r IN L shy
A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
----- -------- -------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~
Point Data Description
TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch
Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree
Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch
Case 2 translational Y 0 inch Case 2 translational Z 0 inch
Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree
Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree
y Case 3 rotational 0 degree Case 3 rotational Z 0 degree
Free Y restraint during hanger design
-
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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~
SECTION
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ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE
Case number Combination
1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 HEOa Fx
Fy Fz Mx
0 -1
0 2
0 0 0 0
4 0 --gt J
44
-1 -6 -0
0
0 0 0 0
5 -1
4 46
-
r
HE3
HE4Near
HE5
HE6a
HE6d
HE7a
HE7b
HE7b
HE7c
HE9
My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz
2 1 0 1
-0 -0 -2 -0 -0
0 -0 -1
0 -2
0 1 0
-3 -4
1 -1 -0
1 -1 -0
0 -0
0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
14 2 4
17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
-6 -18
0 0
-2 -2
-13 -3
0 -0 -9 -0
0 -0
0 -0 -3 -4 -6
0 -0 -0
0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
~
17 3 4
18 1
-0 -2 -0
2 4
-0 -1
7 6 0 1 0
-3 -4
1 -1
0 1
-1 -0
0 -0
0 -0 -0 -0
PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 D-Zero Solenoid Upgrade
Fermi Natl CHIMNEY DESIGN
Accelerator Lab 101593 10S7i=lage File CASE
Support Summary Forceslb or Momentsinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1
Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1
TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0
Fz 0 0 0 0 0 0
Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204
0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256
0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379
TR7a 0000 -0000 --0000 0142 0173 -0141
TR7b -0000 -0000 -0000 -0169 -0211 0131
0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009
-0447 -0282rR9 0139 -0117 0009 -0285
HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005
HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013
0013 -0053 0000HE2Far 0009 --0002 -0027
-0056 0016 HE3 -0062 0013 -0012 0027
0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140
HE5 -0249 0061 0126 0217 -0049 0203
HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495
HE6a -0000 -0000 0216
HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164
HE6c -0029 -0224 0045 0420 -0064
HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472
HE7Near 0242 0295 -0117
0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c
-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109
-0259 -0346 -E9 -0159 -0525 -0058 -0322
0000 -0000 0000 00000000 0000ILl
0000 -0025 0006 00250001 0002
0004 -0101TL2 0000 -0000 0000 0044
TL2a 0114 0019 -0274-0004-0005 -0031TL3
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
--
--------- ---------- ---------- ---------- ---------- ---------- ----------
~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z
-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257
PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1
System Stresses (ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000
517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000
530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439
100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367
422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350
805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002
595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507
1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102
1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002
20000805 1280 1282 1760HE5 100 100 002 20000
HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805
3339 3690 20000HEba 100 100 002 805 3337
1936 2104 20000HE6b 100 100 002 805 1931
2764 2861 20000HE6c 100 100 002 805 2761
4293 5090 20000HE6d 100 100 002 805 4292
5334 5523 20000HE7Near 123 102 002 805 5334
5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002
805 782 815 1087 20000HE7b 100 100 002
200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000
HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805
343 806 453 2000019 100 100 002 805
722 751 829 20000TLl 100 100 001 517
20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001
----------~ ~~ ~~-- --- ---- -shy
1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
Point Name
TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
System Stresses (ANSI B313) In- Out
Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal
100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100
100 100
001 001
517 517
318 518 518
Code
992 610 714 641 546 428 530 512
1604 358 435 429 347
1687 1534
365 425 329
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(
middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far
Maximum Z displacement 0307 inch at point HE6Near
Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7
Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b
Maximum - force -4 Ib at point HEOa
Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far
bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274
PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257
I
--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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--------- ----- ----- ------- -------- -------- -------- -------- --------
rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses (ANSI 8313 ) In- Out
Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000
-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
---------
PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2
System
In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a
100 100
100 100
001 001
TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001
9 100 100 001
Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy
Stresses ( ANSI 8313)
Stressespsi Hoop Longitu Principal Code
------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329
Page 20 CASE123
Allow
20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca
D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum
Maximum Maximum Maximum Maximum Maximum
+ Pressure 2 + Thermal 2 + Displacement 2
System Maxima
X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near
X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7
X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa
X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3
hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131
rJR8 Near R8Far
0229 0227
-0174 -0173
0008 0009
-0281 -0282
-0433 -0438
-0294 -0292
rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1
--0000 -0000
0111 0109
-0000 -0000
0129 0149
-0014 -0016
-0067 -0091
HE2Near HE2Far HE3 HE4Near HE4Far
-0002 -0003 -0020
0020 -0017
0096 0088 0004 0004 0003
-0000 -0001 -0004 -0004 0007
0202 0226 0145 0112 0045
-0022 -0029 -0029 -0024 -0036
-0202 -0261 -0054
0047 0006
HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006
HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014
HE7a HE7b HE7c HE8Near HE8Far
~E9
L1 TL2 TL2a TL3
-0000 -0000 -0000
0193 0195 0157 0000 0001 0000
-0005
-0000 -0000 -0000 -0147 -0149 -0130 0000 0002
-0000 -0031
0000 -0000 -0000
0015 0016 0016 0000 0000 0000
-0004
-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114
0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019
-0023 0040
-0139 -0318 -0317 -0314 0000 0025
-0101 -0274
~--~~~~~~
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
--------- ---------- ---------- ---------- ----------
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead
Point Name
TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9
Weight + Pressure 3 + Thermal 3 + Displacement 3
System Deflections Displacementsinch Rotationsdegree
X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379
-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075
-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3
System StresSes ( ANSI 831 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----
TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000
m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000
517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100
2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697
2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996
1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373
100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494
20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654
20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535
100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002
20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -
813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772
805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394
-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334
100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364
20000TL2a 100 100 001 517 1493 1498 1600
N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Stresses (ANSI 8313) In- Out
Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow
TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e
PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3
System Maxima
Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar
Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7
Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near
Maximum Z force 1 lb at point HE3
=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS
F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by
ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133
Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb
~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~
C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(
o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy
F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
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H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
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101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
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SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)
T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99
~
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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SECTION
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ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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SUBJECT NAME
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
-------- -------------------------------------------------
H
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Point
TRl
TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a
Data Description
Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses
(degF) (psi) -320 8000
Load Load data identifier = LN2 Case Temperature Pressure Expansion
No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857
Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
Guide
Guide
Guide
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
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ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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SUBJECT NAME
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
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Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
-------------------------------------------------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN
Point Data Description
TR6b Guide TR7 TR7a Line stop
Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)
X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design
HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10
Material Data Identifier = AL Load Load data identifier = LHE
Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)
1 -452 150 -0003900 2 -452 150 -0003900
Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
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Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
----- --------
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~
Point Data Description
Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)
X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree
HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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SUBJECT NAME
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
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Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
----- -------- -------------------------------------------------
101493 1243 PageFile CAS[
PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN
point Data Description degree
Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid
Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =
0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0
HE6b HEbc
Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet
2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree
HE7 ~
HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
----- -------- -------------------------------------------------
------~-- ~
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
J
Point Data Description
TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )
translational X 0 inch Case 2 translational Y 0 inch Case )
lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3
rotational Y
rotational Z 0 0
degree degree
Free Y restraint during hanger design
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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~
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
Case number Combination
1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot
~
Support Summary Forceslb or Momentslinch-lb
Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1
Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0
TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0
-
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
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PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z
TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019
TR7b TR8Near
-0319 middot-0241
-0420 -0807
0000 -0080
-0198 -0666
-0286 -0210
013 -030
TR8Far -0242 -0803 -0088 -0695 -0194 -030
TR9 -0274 -0656 -0132 -0770 -0146 -029
HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007
HEl HE2Near HE2Far HE3 HE4Near HE4Far
0015 0025 0022
-0077 -0109 -0309
0109 0098 0091
-0017 -0052 -0064
-0005 -0021 -0027 -0004 -0008 0126
0132 0170 0175 0187 0202 0101
0156 0106
-0033 -0105 -0020 -0216
-010 -022 -029 -036 -032 023
HE5 HE6Near HE6Far HE6a
--03l1 -0358 -0354 -0096
-0052 0088 0097 0035
0137 0170 0155 0073
0097 0095 0123 0201
-0200 0290 0505 0601
025 035 034 o 30(
HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3
0046 0081 0110 0187 0184 0052 0264
-0356 -0481 -0479 -0437 0000
-0002 -0048 -0088
-0044 -0062
0031 0201 0205 0060
-0515 -0459 -0609 -0612 -0589 0000 0002 0010
-0013
-0012 -0096 -0181 -0270 -0280 -0124 0067 0026
-0070 -0079 -0121 0000
-0021 -0010 -0007
0163 -0090 -0393 -0327 -0230
0201 0012
-0014 -0095 -0110 -0129 -0000 -0037 0021 0099
0188 0040 0155 0120 0049
-0230 -0011 0084 0192 0207 0222
-0000 -0050 -0102 -0053
025 021 017 014 013
-024 000 026
-009 -009 -009 000 002
-010 -027
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
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eA~E-O
)
IE L He TtJeE
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1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
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CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy
TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7
0368 0411
0010 0002
-0271 -0287
0084 0140
0619 0559
040 040
TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9
-0278 -0277 -0280
-0762 -0760 -0638
-0084 -0092 -0135
-0537 -0564 -0640
-0061 -0045 -0000
-028 -027 -026
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN
L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1
System Stresses ( ANSI 8313 ) In- Out
Point Name --------shy
Plane SIF
----shy
Plane SIF
-----shy
Section Modulus ------shy
Stressespsi Hoop Longitu
---------shy ---------shyPrincipal -------shy
Code ~---- -shy
Allot ----_
TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a
100 115 115 100 100 100 100 100 100 100 100 100
100 100 100 100 100 100 100 100 100 100 100 100
001 001 001 001 001 001 001 001 001 001 001 001
517 517 517 517 517 517 517 517 517 517 517 517
918 1116 1075 1509
887 4)4 641 659
1124 1793 1752 2005
929 1123 1083 1514
900 577 672 687
1130 1796 1752 2005
1376 1233 1186 1800 1078
611 924 910
1560 1906 1919 2122
200( 200( 200 200 200( 200 200 r
200 200( 200( 200( 200(
TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(
T R 7 a TR7b
100 100
100 100
001 001
517 517
1448 1525
1452 1528
2022 1831
200 200
TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001
HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1
HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200
r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
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PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
--------- ----- ----- ------- -------- -------- -------- -------- -----
~ -
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
I
System Stresses ( ANSI B31 3) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot
TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200
001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200
981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
e E itocJ ICD
f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
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7001 -~-----
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1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far
Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a
Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
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PAGE
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t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Name X
Displacementsinch Y Z X
Rotationsdegree Y Z
TRl 0000 0000 0000 -0000 -0000 o OO(
TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT
TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~
TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191
TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0
TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~
HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl
-0437 0000
-0589 0000
-0121 0000
-0129 -0000
0222 -0000
-0) o l6(
TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
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IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
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PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
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b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1
TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027
I TL9 -0280 -0638 -0135 -0640 -0000 -026
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
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IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
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A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
Go
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4
Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313 ) In- Out
Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (
HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r
TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
e E itocJ ICD
f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
FQcM I 1 0
r IN L shy
A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot
_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Stresses ( ANSI 8313) In- Out
Point Plane Plane Section Stressespsi Name --------shy
SIF ----shy
SIF -----shy
Modulus --------shy
Hoop --------
Longitu -------shy
Principal -------shy
Code --------
Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r
TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200
-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
e E itocJ ICD
f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
FQcM I 1 0
r IN L shy
A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2
System Maxima
Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar
Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a
Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a
Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3
Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
e E itocJ ICD
f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
FQcM I 1 0
r IN L shy
A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
-------------
I
~
SECTION
IltDJ 016 AI FERMILAB
ENGINEERING NOTE PROJECT SERIAL-CATEGORY
J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )
PAGE
SUBJECT NAME
Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE
~ENOD -reP-MM MltN~--r DUl2 Q 3
4 OF
c ~ A ~ ( E~
10 80 ~ e - 11 uloJ
eA~E-O
)
IE L He TtJeE
e E itocJ ICD
f
c ~EgtjIlA(-o AT HE 1shy IoJ CASpound
A IJ 1or-1--t ~ f S AN~ a T kGR
A fIO W Ii I-~ STLe-~ ~
o O~ 41 v~ Oo3~ I
eo iVEc i 0r s2~ 26
~~igtb -E
w ~oP7raquo
FQcM I 1 0
r IN L shy
A-lA-l-1S (S
7001 -~-----
505 bull
1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe
IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc
M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE
1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E
DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5
~-~---~--~
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
(
(
PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~
t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R
rI u~S Ucl tJltS DATE IREVISION DATE
DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook
JIItk ) t) -0 i
eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M
r 0(
- I J 254 M
ALO~ 7 p)(
CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(
Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~
b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220
%d0%9c%d0%b0%d0%b3 %d0%95%d0%ba%d0%b1 %d0%91%d1%96%d0%be%d1%82%d0%b5%d1%85%d0%bd%d0%be%d0%bb%d0%be%d
%d0%9a%d0%a3%d0%a8%d0%9d%d0%86%d0%a0%d0%95%d0%9d%d0%9a%d0%9e%20%d0%9e %d0%90 %d0%9e%d0%91%d0%9b%d0%8
%d0%9f%d1%80%d0%be%d0%b3%d1%80%d0%b0%d0%bc%d0%bc%d0%b0 %d0%a1%d1%8a%d0%b5%d0%b7%d0%b4%d0%a2%d0%b5%d1
%d0%a3%d1%87%d0%b5%d0%b1%d0%bd%d0%b8%d0%ba%d0%b8%20%d0%98%d0%b7%d0%b4 %d0%b2%d0%b0%20%d0%9c%d0%98%d0
%d0%a4%d0%93%d0%9e%d0%a1%203 %20%d0%9b%d0%b5%d1%87%d0%b5%d0%b1%d0%bd%d0%be%d0%b5%20%d0%b4%d0%b5%d0%b
%d1%81%d0%b8%d1%81%d1%82%d0%b5%d0%bc%d0%b0 %d0%bd%d0%b0%d0%bf%d0%be%d0%bb%d1%8c%d0%bd%d0%be%d0%b3%d0
%d0%b5 %d0%b5%d0%ba%d1%80%d0%b0%d0%bd %d0%b4%d0%be%d1%80%d0%b0%d0%bd%d0%b8%d0%ba%d0%b8 %d0%bb%d1%8e%
1060204 %d0%bb%d0%b8%d1%81%d1%82%d0%be%d0%b2%d0%ba%d0%b0 %d0%bf%d0%be %d1%82%d0%b5%d0%bf%d0%bb%d0%be
%d0%9a%d0%b0%d1%82%d0%b0%d0%bb%d0%be%d0%b3 %d0%9c%d0%be%d0%bb %d0%a1%d0%bf%d0%b5%d1%86 %d1%83%d0%ba%
%d0%a3%d1%87%d0%b5%d0%b1%d0%bd%d1%8b%d0%b9%d0%9f%d0%bb%d0%b0%d0%bd %d0%a4%d1%83%d0%bd%d0%b4%d0%9c%d0
%d0%a1%d0%b1%d0%be%d1%80%d0%bd%d0%b8%d0%ba %d0%a1%d1%8a%d0%b5%d0%b7%d0%b4%d0%a2%d0%b5%d1%80%d0%b0%d0
%d0%9f%d0%be%d0%bb%d0%be%d0%b6%d0%b5%d0%bd%d0%b8%d0%b5 %d0%9f%d0%be%d1%81%d0%bb%d1%8b%20%d0%9f%d0%be
%d0%9c%d0%b0%d0%b3 %d0%95%d0%ba%d0%b1 %d0%a2%d0%b5%d1%85%d0%bd%d0%be%d0%bb%d0%be%d0%b3%d1%96%d1%97%2
%d0%93%d0%a3%d0%97%20%d0%93%d0%b0%d0%b7 %d0%97%d0%b0%d0%b2%d0%be%d0%b4%d1%81%d0%ba%d0%b0%d1%8f%20%d0
%d0%a8%d0%b0%d0%b1%d0%bb%d0%be%d0%bd %d0%a0%d0%9f %d0%b0%d1%81%d0%bf%d0%b8%d1%80%d0%b0%d0%bd%d1%82%d
%d0%bf%d1%80%d0%be%d0%b5%d0%ba%d1%82%d0%b8%d1%80%d0%be%d0%b2%d0%b0%d0%bd%d0%b8%d0%b5 %d0%b2%d0%bd%d1
%d0%93%d0%90%d0%a3%d0%97%20%20%d0%a0%d0%9f%d0%a6%20%d0%b3 %d0%a3%d0%bb%d0%b0%d0%bd %d0%a3%d0%b4%d1%8
%d0%9d%d0%b0%d0%b2%d1%87%d0%b0%d0%bb%d1%8c%d0%bd%d0%be %d0%bc%d0%b5%d1%82%d0%be%d0%b4%d0%b8%d1%87%d0