international nuclear information system...jul24199b engineering data transmittal 622233 2. to:...

JUL24199B ENGINEERING DATA TRANSMITTAL 622233

2. To: (Receiving Organization)

Distribution3. From: (Originating Organization)

TWRS Projects/SST Retrieval4. Related EDT No.:• n / a

W-320 TWRS/TCPN #.-G2fto1-

6. Design Authority/ Design Agent/Cog.

^ J i , NHC7. Purchase Order No.:

n/a8. Originator Remarks:For approval and release of a new supporting document. Thisdocument has been generated to ensure retrievability of the'Project W-320 "Piping Calculations, Vol. 5".

9. Equip./Component No.:

n/a10. System/Bldg./Facility:

241-C-10611. Receiver Remarks: 11A. Design Baseline Document? [X] Yes [] No 12. Major Assm. Dug. No.:

n/a13. Permit/Permit Application No.

n/a14. Required Response Date:

DATA TRANSMITTED (G). (H)

ItemNo.

(B) Document/Drawing No.

(C)Sheet

No.

ID)Rev.No.

IE) Title or Description of DataTransmitted

ApprovalDesig-nator

Reasonfor

Trans-mittal

Origi-natorDispo-sition

Dispo-sition

HNF-2475 Project W-320, 241-C-106 Sluicing, PipingCalculations, Vol. 5

NA

Approval Designator (F) Reason for Transm'rttal (G) Disposition <H) & (I)

E, S, Q, D or N/A(see WHC-CM-3-5,Sec.12.7)

1. Approval 4. Review2. Release 5. Post-Review3. information 6. Dist. (Receipt Acknow. Required)

1, Approved 4. Reviewed no/comment2, Approved w/comment 5. Reviewed w/comment3, Disapproved w/comment 6. Receipt acknowledged

17. SIGNATURE/DISTRIBUTION(See Approval Designator for required signatures)

[] Approved[] Approved w/conments[] Disapproved w/comnents

BO-7400-172-2 (05/96) GEF097

BD-7400-172-1

HNF-2475, Rev. 0

Project W-320, 241-C-106 SluicingPiping Calculations, Vol. 5

John W. BaileyNumatec Hanford Co., Richland, WA 99352U.S. Department of Energy Contract DE-AC09-96RL13200

EDT/ECN: 622233Org Code: 8C452B&R Code: EW313001O

Key Words: W-320, Sluicing, Tank 241-C-106, Tank 241-AY-102, WRSS,calculations, piping.

UC: 506Charge Code: D2991/HANA0600Total Pages:

Abstract: This supporting document has been prepared to make the FDNWcalculations for Project W-320, readily retrievable.

TRADEMARK DISCLAIMER. Reference herein to any specific commercial product, process, or service bytrade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply itsendorsement, recommendation, or favoring by the United States Government or any agency thereof orits contractors or subcontractors.

Printed in the United States of America. To obtain copies of this document, contact: DocumentControl Services, P.O. Box 950, Hailstbp H6-08, Richland UA 99352, Phone <509) 372-2420;Fax (509) 376-4989.

OATH:

STA:

H"•MM*

\ HA'ifORD 1

I R3£AG2 ^

X-—,J-

Release Stamp

8

'D: y26/

Approved for Public Release

A-6400-073 (01/97) GEF321

HNF-2475, Rev. 0

Project W-320, 241-C-106 SluicingPiping Calculations, Vol. 5

TABLE OF CONTENTS

Calc. No. Title Page

W320-27-028 Miscellaneous Pipe Stress Analysis A-i

W320-27-029 AY Farm Jumper Stress Analysis B-i

W320-27-030 W320 Tank 241-C-106 HVAC Seal Loop C-i

W320-27-031 Booster Pump Restraint Analysis D-i

HNF-2475, Rev. 0

W320-27-028

Miscellaneous Pipe Stress Analysis

A-i

ICF KAISER |HANFORD COMPANY

CALCULATION IDENTIFICATION AND INDEX Page

Date

This sheet shows the status and description of the attached Design Analysis sheets.

Discipline 27 , P i p i n g and Vesse ls WO/JobNo._ER4319 Calculation No.

Project No. & Name P r o j e c t W-320 Waste R e t r i e v a l f o r Tank 241-C-10S

Calculation Item M i s c e l l a n e o u s Pipe S t r e s s A n a l y s i s

These calculations apply to:

Dwg. No. H-2-818482 Sheets 1 , 2 , and 3 Rev. No

Dwg. No. ES-320-M07, ES-320-M08 Rev. No

Other (Study, CDR)

Rev. No

The status of these calculations is:

D Preliminary Calculations

E l Final Calculations

D Check Calculations (On Calculation Dated

D Void Calculation (Reason Voided

Incorporated in Final Drawings? tS3

This caiculation verified by independent "check" calculation? •

Original and Revised Calculation Approvals:

Originator

Checked by

Approved by

Checked AgainstApproved Vendor Data

Rev. 0Signature / Date


i <*

8 / 2 2

i i i

/S5

W320-27-028

0

0

Yes D

Yes Si

Rev. 2Signature/Date

INDEX

Design Analysis Description

Page No.

i - i i Calculation Identification and Index

i i i . Calculation Cross Index

1 - 4 "'• •• Objective, Design Criteria ,Design Inputs

5 Assumptions, Calculations and Conclusions

6 References

)

No

No

INDX-M.XLSHNF-2475, Rev. 0Page A-l

ICF KAISER JHANFORD COMPANY

CALCULATION IDENTIFICATION AND INDEX i i i

8 / 2 2 / 9 5

Discipline 27,Piping and Vessels WO/Job No._ER4319 Calculation No. W320-27-028

Rev. 0Signature /Date



Originator

Checked by

Design Analysis

Page No.

Description

INDEX

Sustained Loading Analyses

Summary of Encasement Pipe Expansions and

and Bend Stresses

10 & 1 1 Anchor Loads at Pit Wall Penetrations

Appdx A Stress Isometric andSketches derived' from project drawings

Appdx B STAB Results Filenames:SB90M8-S.mcd & SB45M8-T.mcd

Appdx C Autopipe Results Filename: M7-R0.out

Rev. 1 : A3-

...u.i.i.,)ii.u...U£»^i!

HNF-2475, Rev. 0Page A-2

INDX-M.XLS

si?s «

CALCULATION CROSS INDEX (Typical)Subject Calculation No. W320-27-028

SubjectCalculation

RevisionNo.

0

0

I

I-2475, Rev

A-3

©

Supercededt>y Calculation

No.

NA

NA

These interfacing calculation/documentsprovide input to the subject calculation,

and if revised may require revision ofthe subject calculation.

Calcualtion/Document No.

Dwg.# ES-320-M07

Dwg.# ES-320-M08

^ f t iH-Z.-818'V^i, sVr 1

A>/V lH-2-818^1 . ^ + 3

MAH-2.--2IS52-1 , sW )H-2--Si8S<K.sWt 1

•

Revision.No.

0

0

1)

o1

1

Results and conclusions of the subjectcalculation are used in these interfacing

calculations and/or documents.

Calcualtion/Document No.

NA

NA

A

Revision.No.

Does the outputinterface calculation/

documents requirerevision?

Yes 1 No

X

X

~-

Has the output interfacecalculation/ documents

been revised?

Yes No

X

X

[

Page iii of iii

Discipline manager's signature anddate indicating evaluation

complete.

Ii

1

( ̂ I

1

>

KEH 1£ 75.00 (12/88)

ICF KAISERHANFORD COMPANY

DESIGN ANALYSIS

CaioNo. W-320-27-028

Revision No. & '

• Page No. 1 of 1 1

Client WESTINGHOUSE HANFORD COMPANY wo/JobNo. ER4319 Filename TEXT-M.WPsubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 2 2 / 9 5 By D.L.STONE

PROJECT W-320 WASTE RETRIEVAL for TANK 241 -C-106 Checked^ tZ=tJcfS~ By C^>^Location C TANK FARM - 200 EAST AREA - HANFORD Revised )2_/ ] I c.-j By )/,|A

OBJECTIVE:

The objective of this calculation is:

BY: 3,2-3-

1. To perform static and dynamic stress analysis of the Drain Pipeline servicing Tanks 241 -C-106 in order tobe in compliance with the Code ASME B31.3 requirements.

2. To calculate the pipe anchor loads at building penetrations in order to transmit these loads to Civil /Structural group.

DESIGN CRITERIA:

1. ASME CODE B31.3-93 with Addenda up to 1994.2. SDC4.1, REV-11. (UoJ FOW^ AicUe * I33. PROJECT W-320 FDC: WHC-SD-W320-FDC-001, REV.^

DESIGN INPUTS:

1.2.3.4.5.6.7.8.9.10.11.12.13.

Ambient temperaturePipe WallEncasement Pipe material:Process Pipe Materials:Corrosion rate:Safety Class category:Pipe mechanical properties:Soil characteristics:Design Pressure:Design Temperature:Process FluidSpecific gravityPiping Dimensions

40°F (Ref. 11)Schedule 40 (Ref. 16)ASTM A53 Type E Grade B, Seamless (Ref: 16)ASTMSA312 TP304L Stainless Steel (Ref: 16)2 mils/yr.for 20 years (considered as 0.06) (Ref: 19)SC-2 (?- Yr ''•»' ^ jMwfot , ov. «s u ) ( R e f . 1 5 ,(See second page of "STAB", Appx. B) (Ref: 3)(See third page of "STAB", Appx. B) (Ref: 12)60 psig (Ref: 16)

1OO°F (Ref: 16)Waste Solids blown from metal filters (Ref: 20)1.25 (conservative) (Ref: 11)Drawings ES-320-M07 and ES-320-M08 (Ref: 20)(Composite sketches from these drawingshave been provided in Appendix A.)

DESIGN METHODOLOGY:

The calculation includes analysis of the encased drain line connecting the Process Air Building Seal Pot and FloorDrain with the Tank 241-C-106 Sluice Pit 241-C-06C through Nozzle U-8. (Ref: 20)

The stress analysis includes the following :

1. Analysis of the buried (outer) encasement piping for sustained, seismic and thermal loading under theimpact of soil friction in order to qualify for Code B31.3-90 requirements. The analysis is performed usingthe computer program "STAB" (Ref: 7) which is based on the principles promulgated in ASME Papers (Ref:5 & 6).

The Safety Class designation of the encasement pipe is dependent upon the designation of the Primaryprocess pipe inside the encasement pipe, and is therefore categorized as Safety Class-2 (Ref: 2) pipe.


ICF KAISER caic No. W-320-27-028HANFORD COMPANY Revision No. 0

DESIGN ANALYSIS Page No. 2 of 11

^Client WESTINGHOUSE HANFORD COMPANY wo/JobNo. ER4319 Filename TEXT-M.WPSubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 2 2 / 9 5 By D.L.STONE

PROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 C h e c k e d f / * ^ T^ By <=-~D O&-^J^ULocation C TANK FARM -200 EAST AREA-HANFORD Revised / / By

2. Analysis of the primary (inner) process piping for sustained, thermal and seismic loading isperformed using the computer program "AutoPipe" Version-4.5 by "Engineering DesignAutomation" (EDA). (Ref:8)

Seismic & thermal displacements for the encasement pipe elbows, determined by the "STAB"(Ref: 7), are checked and tabulated to ensure minimal impact on the Primary pipe.

The Primary process pipe of each line is categorized as Safety Class-2 (Ref: 1 5) pipe.

3. Pipe Loading at Building Penetration Anchors is summarized using spreadsheet program, "Excel"(Ref. 9.)

SUSTAINED LOADS:

ENCASEMENT PIPE

A The dead load for the encasement pipe is considered to include the weight of the inner primary

pipe, the weight of its contents, and the weight of the soil cover over the encasement pipe. Theweight of the encasement pipe is not a significant factor since it is supported continuously by thesurrounding soil.

The AASHTO, H20 live loads (Ref: 4) are considered to include the impact of the surface vehiclesmoving over the buried encasement pipe. (Page 7 & 8)

The encasement pipe longitudinal stress due to the sum of the dead loads and live loads iscalculated and added to the summation of pressure stress & seismic stress obtained from thecomputer program "STAB" (Ref: 7). ()

The pressure stress for the outer encasement pipe is considered similar to that of the primary pipein order to ensure operability if the primary pipe fails.

PRIMARY PIPE

The sustained stress on the inner primary pipe is the summation of longitudinal stresses resultingfrom internal pressure and the dead weight of the pipe. The pipe material is stainless steel ASMESA 312, Grade TP 304L whose Allowable stress "S" Per Code B31.3 is 1 6,700 psi. (Ref: 1)

The "AutoPipe" program checks the sustained stress in the primary pipe against Code Allowable.(Ref: 8).

HNF-2475,Rev 0Page A-5

ICF KAISER Caic No. W-320-27-028HANFORD COMPANY Revision No. 0


'client WESTINGHOUSE HANFORD COMPANY wo/Job No. ER4319 Rename TEXT-M.WPSubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 2 2 / 9 5 By D.L.STONE

PROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked <flZ--2Jc?g- ByLocation C TANK FARM - 2 0 0 EAST AREA - HANFORD Revised / / By

SEISMIC STRESSES:

ENCASEMENT PIPE

The buried, encasement pipe elbow stresses due to propagation of ground seismic waves are computedusing the computer program "STAB" (Ref: 7) which has been programmed based on the principlespromulgated in ASME Papers (Ref: 5 & 6).

The peak free field acceleration factor (ag) of "0.12g" and peak free field ground velocity of "48Xag" areconsidered as stipulated in SDC 4.1, Rev-11 (Ref: 2) for Safety Class 2 & 3 piping.

The pipe mechanical properties are obtained from "Crane Technical Paper" (Ref: 3).

The soil data for dynamic analysis is based on the report were obtained from the Shannon & Wilson Inc's"Geotechnical Engineering Studies" (Ref:12)

Since the depth of the soil cover varies at different locations and since shallower depths produces higherstresses in pipe bends, the minimum required depth for shielding (Ref: 14) three feet is used as the basis inthis analysis.

Since the seismic stresses do not occur concurrently in both pipe legs around the elbow, the elbow will besubjected to seismic stress from only one leg at a time. As such, seismic analysis is performed for thelongest straight pipe run adjacent to each pipe bend.

The sustained and seismic stresses are added together and compared to the Code B31.3 allowablerequirements for Sustained + Occasional stresses. These stresses are summarized on page 9. Themaximum seismic displacements at pipe bends are also listed on page 9.

PRIMARY PIPE

Since the Primary pipe has been classified as Safety Class 2 Pipe in the FDC (Ref: 11), Dynamic analysis isperformed using "Fig 5" seismic response spectra (5% Damping) of SDC 4 .1 , Rev-11. (Ref: 2) Thisresponse spectra has been created in "AutoPipe" as "SC2&3" and is used in dynamic analysis.

The seismic stresses from the dynamic analysis are added to the sustained stresses from the static analysisto qualify against ASME B31.3 occasional stress allowable 1.33Sh. (Ref.1)

The encasement pipe seismic movements (See page 9) are negligibly small and will not have anysignificant impact on the primary pipe stress analysis. Therefore, these movements are not considered.

HNF-2475, Rev 0Page A-6

ICF KAISER Caic No. W-320-27-028HANFORD COMPANY Revision No. 0


) Client WESTINGHOUSE HANFORD COMPANY WO/Job No. ER4319 Filename TEXT-M.WPSubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 2 2 / 9 5 By D.L.STONE

PROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked*? I~ZZJ9S~ By (L-~O OS- i - ^a^Location C TANK FARM - 200 EAST AREA - HANFORD Revised / / By

THERMAL (DISPLACEMENT) STRESS:

ENCASEMENT PIPE

The thermal analysis for the Encasement pipe is performed at the same temperature as it is for the Primarypipe (100° F) to ensure operability in case primary pipe fails. Soil static properties were obtained from the"Geotechnical Engineering Studies" report furnished by the Shannon & Wilson Inc (Ref: 12).

The computer program "STAB" is used to perform the thermal analysis and compute the stresses in eachpipe leg around each pipe bend. Since thermal stresses in each leg occur concurrently, "STAB" adds thesestresses together to compute total thermal stress at the pipe bend and qualify it for Code B31.3 Allowablethermal stress. Results are summarized on page 9 . Thermal displacements at the pipe bends are alsolisted on pages 9 . The effects of thermal displacement at guide locations were checked and sincesupport displacements of less than 0.063 inches are not considered critical, the analysis has been omittedfrom this package. (See Page 9)

The maximum design temperature for the Primary pipe is 100°F in accordance with the projectconstruction specification (Ref: 16) and has been considered in the "AutoPipe" program.

PRIMARY PIPE

Since the primary pipe is intermittently welded to the encasement pipe, the thermal movements of theencasement pipe have been taken into consideration in the primary pipe thermal analysis.

The "AutoPipe" program has been run to qualify the thermal stress to Code B31.3 allowable fordisplacement stress "Sa". (Ref: 1)

The thermal expansion of the Primary pipe at any bend obtained from Autopipe is found to be less than thegap available between the primary pipe and the encasement pipe.

SOIL CHARACTERISTICS:

The "Geotechnical Engineering Studies" report by Shannon & Wilson Inc, (Ref: 12 Tables 2 & 3) furnishescharacteristics for both Natural sand and Backfill sand. Since the "STAB" test run made using the propertiesof the Natural sand produces higher stresses in pipe bend than that of the test run using the properties ofthe Backfill sand, Natural sand properties are used conservatively for entire seismic and thermal analysis.

COMBINED LOADING AT BUILDING PENETRATION ANCHORS

The spreadsheet program, "Excel" (Ref. 9), has been used to calculate Pipe Loading at Building PenetrationAnchors. (Pages 10 & 11 .) Seismic and thermal loads on an anchor by the Encasement Pipe arecalculated by multiplying the soil friction force for the underground pipe (obtained from the corresponding"STAB" calculations) by the length of pipe attached to the anchor. For cases in which the effects ofloading by the Inner Process Pipe and Encasement Pipe are concurrent (such as pit wall penetrations),anchor loading is considered as the sum of the Inner Pipe restraint reactions at the anchor (obtained from"Autopipe" analysis) plus the calculated Encasement seismic and thermal loads. For cases in which theeffects of loading by the Inner Process Pipe and Encasement Pipe are not concurrent (such as at theProcess Air Building Floor Drain Seal Pot), anchor loads are represented in the spreadsheet, separately.(See Appx. A, Dwg.# H-2-818482)


IUh KAIHtH caic No. W-320-27-028

HANFORD COMPANY Revision No. JS^ 'DESIGN ANALYSIS Page No. 5 of 11

> Client WESTINGHOUSE HANFORD COMPANY wo/Job No. ER4319 Filename TEXT-M.WPSubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 2 2 / 9 5 By D.L.STONE

PROJECTW-320 WASTE RETRIEVAL for TANK 241 -C-106 Checked flZZltS" By C l b ' d c r v ^ a .Location C TANK FARM - 200 EAST AREA- HANFORD Revised \z[ | I^-J By (/ ,1

ASSUMPTIONS: £ M K D B V : ? L . ^ ^ 3,21*6

1. Since "Geotechnical Engineering Studies" by Shannon & Wilson Inc (Ref: 12, Sect 12.1) indicatesthat the geological hazards such as ground faulting, soil liquefaction, ground differential settle-ments, land slides, ground collapse potential and flooding either not pertinent or insignificant tothe native soil encompassing W-320 project, these hazards are not considered in the analysis.

2. The building structures are adequate to withstand the pipe loads.

3. The impact of building permanent settlements, if any, will be mitigated by designing voidsbetween the pipe and the soil, so that the pipe will move in tandem with the building and will notbe restrained by the soil.

CALCULATIONS:

Sustained load analysis . (Pages 7 & 8)

Summary of Encasement Pipe Expansions and Pipe Bend Stresses for: (Page 9)

Pipe Loads at Building Wall Penetrations for: (Pages 10 & 11)

See Appendices for seismic & thermal analysis by "STAB" program. (Appx. B )

See Appendices for AutoPipe analysis. (Appx. C )

CONCLUSION:

1. The results of the "STAB" analyses indicate that sustained, seismic and thermal stresses in theEncasement Pipe have met the Code B31.3-1990requirements.

2. The review of the "AutoPipe" summary results indicates that pipe stresses are in compliance withASME Code B31.3 requirements.

3. Building penetration anchor loads are calculated and listed on pages 10 & 1 1 .

Rev. I of " f W COIUUUTICM vei led &£. c\\Ae\f&<s <^MiT •We

COVA&\O<A.S . "fwe/t <*/£. wx'mo-c diVweisiov,^

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- f V s c cl'-ffe./t*£&5 eve. vM.^sJDt •

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ICF KAISER caic No. W-320-27-028HANFORD COMPANY Revision No. -0" I

DESIGN ANALYSIS PageNo. 6 of 11

Client WESTINGHOUSE HANFORD COMPANY wo/Job No. ER4319 Filename TEXT-M.WPSubject MISCELLANEOUS PIPING STRESS ANALYSIS Date 8 / 22 / 95 By D.L.STONE

PROJECTW-320 WASTE RETRIEVAL for TANK 241-C-106 Checked f / ZZ/<?S~ By Q.£> 3 <b^%"-.Location C TANK FARM - 200 EAST AREA- HANFORD Revised \-J [ /< ) - ] By )C,Vk- •«&-

REFERENCES: CHK& «M : <H_ Ot^-SA- 3 2 3 • ^

1. ASME Code B31.3 and B31.3a-1994 Addenda for "Chemical and Petroleum Refinery."

2. SDC 4.1 , Rev. 11, "Standard Architecture & Civil Design Criteria."(TRW) f-OMW fWt.-o. *" |3*r.ZlS.)l |7 , Oej^, UHLS C fcm'I.Vcs }

3. Crane Technical Paper No: 410, 22nd Printing-1986.

4. AISI "Modern Sewer Design" First Edition, 1980.

5. ASME PAPER on "Hand Calculation of Seismic & Thermal Stresses in Buried Pipe" by G.C.K. Yeh. PVPVolume-77, June' 1983.

6. ASME PAPER on "Flexibility analysis of Buried Pipe" By E. C. Goodling. PVP Volume-82, June, 1978

7. Computer Program "STAB" (Seismic and Thermal analysis of Buried Piping), Version-0

8. Computer application "AutoPipe" Version 4.5 by "Engineering Design Automation."

9. Computer application "Excel" Version 4.0, by Microsoft.

10. Computer application "Mathcad" Version 4.0, by Mathsoft, Inc.

11. WHC-SD-W320-FDC-001, Rev-2?. "Functional Design Criteria for Tank 241 -C-106 Waste Retrieval, ProjectW-320". /^

12. Shannon & Wilson Inc. Geotechnical and Environmental Consultants, "Final Report of GeotechnicalEngineering Studies, W-320 Waste Retrieval and Sluicing Systems", Dated April 12, 1994.

13. Data Compendium, Bruce A. Castaing

14. Calculations #W320-33-004, "Earth Cover Shielding Thickness for C-farm Piping", Dated: April 12, 1994.(DSI from G.J.Peter dated April 12,1994)

15. WHC-SD-WM-SEL-033, Rev-1. "Safety Equipment List for 241-C-106 Waste Retrieval, Project W-320"

16. Project W-320 Construction specifications W320-C1 Rev-0 for piping materials.

17. Drawing # H-2-818482

18. Calculation No: W030-034 Rev-0 for "Recirculation Building - Foundation."

19. Calculation No: W-030-011, Rev-1 for "Fouling factor and Corrosion rate."

20. Piping Stress Isometric drawings: ES-320-M07 and ES-320-M08



DESIGN ANALYSIS

Caic. No. W-320-27-028Revision No.: 0Page No. ~] of I /

Client WESTINGHOUSE HANFORD COMPANY WO/JobNo. ER4319 Filename HOOP.MCDSubject MISCELLANEOUS PIPING STRESS ANSLYSIS Date S 1111 95 By D.L. STONEPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked -f ^ 2 / 95 By cSLocation C TANK FARM - 200 EAST AREA HANFORD Revised By

TOTAL SUSTAINED LOADING ANALYSIS

for 3" in 6" drain Pipes (ES-320-M7 and ES-320-M8)

The purpose of this calculation is to determine the total sustained stress (weight of the processpipe and its contents, overlying soil column weight and impact of surface vehicular weight) on thetransfer line encasement pipe. This value will be added to the stresses computed by STAB to determinethe maximum stress on the encasement.

Unit Initialization:

PSF = — ' Unit representing weight per square foot.

SpG:= 1.25

wmo:=3.2-PSF

PROCESS PIPE AND CONTENTS

Specific Gravity of Process Fluid.

Weight of water per linear foot of 3" Schedule 40 pipe.

Weight of pipe per linear foot of 3" Schedule 40 pipe.

Ref. 3

Ref. 3

:ontents:=wH20SP° Weight of Process Fluid per Linear foot of 3" Schedule 40 pipe.

W l : = w pipe + w contents

Wj =11.58-PSFWeight of Process Pipe and Contentsper linear foot of 3" Schedule 40 pipe.

OVERLYING SOIL

H:=3ft

p:= 0.066 -M

Soil depth. (Minimum required for shielding.)

Static Specific Weight of Soil

W2:=H-p

W 2 =342.144-PSF Weight of soil overlying Encasementper linear foot of 6" Schedule 40 pipe.



DESIGN ANALYSIS

CaEc. No. W-320-27-028Revision No.: 0Page No. J" of / /

Client WESTINGHOUSE HANFORD COMPANY WO/Job No. ER4319 Filename HOOP.MCDSubject MISCELLANEOUS PIPING STRESS ANSLYSIS Date 8 /22 /95 By D.L. STONEPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked 'f K.ZJ 9S By 4Location C TANK FARM - 200 EAST AREA HANFORD Revised By

DL =353.724-PSF

LL := 600-PSF

DEAD LOAD (Weight of the process pipe and its contentsand overlying soil per linear foot of pipe).

LIVE LOAD AASHTO, H-20 Hwy Load per linear foot of pipe .

P := DL + LL

P = 953.724-PSF

P =6.623-psi

TOTAL SUSTAINED LOAD per square foot, per linear foot of pipe.

TOTAL SUSTAINED LOAD per square inch, per linear foot of pipe.

D 6 := 6.625-in

tg :=0.280inEncasement Diameter for 6" Bends.

Wall thickness of 6" Schedule 40 pipe, Bends.

Sfi:=P-2tf

S 6 =78.353 -psi Ring Compression (Hoop stress).

HNF-2475, Rev. 0PageA-11


DESIGN ANALYSIS

Client WESTINGHOUSE HANFORD CO. W O / J o b No.

Subject MISCELLANEOUS PIPING STRESS ANALYSIS Date

PROJECT W-320 WASTE RETRIEVAL for Tank 241-C-106 Checked

Location C TANK FARM 200 EAST AREA Revised

ER4319

8/22/95

Calc. No. W-320-27-28

Revision No. o

Page No. f of / /

Filename SUMRY.MCD

By D. L, STONE

By

SUMMARY OF ENCASEMENT PIPE EXPANSIONS

(Process Drain Line ES-320-M7 & ES-32O-M8 Appdx. D)

NODE

POINT

E09

E04

Nodepoint

E09

E04

SEISMIC5

(inches)0.047

THERMAL8t

(inches)

0.066

8 1(inches)

0.047

SUMMARY OF ENCASEMENT PIPE BEND STRESSES

SEISMICPR + SEIS

(psi)

(STAB)

5725

DEAD WT.

(psi)

(Page* 14 )

78

TOTAL

(psi)

5803

ALLOWABLE

(psi)

22610

THERMALACTUAL

(psi)

5797

ALLOWABLE

(psi)

49650

HNF-2475, Rev. 0Page A-12 SUMRY-M7.XLS


DESIGN ANALYSIS

Client WESTINGHOUSE HANFORD CO.Subject MISCELLANEOUS PIPING STRESS ANALYSISPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106Location C TANK FARM 200 EAST AREA

Calc. No. W.320-27-028

Revision No. n

Page No. \Q of / /

WO/Job No.DateCheckedRevised

ER431S/ 8 /22 /1995

FilenameByByBy

ANCOR.xlsD. L. STONE

ANCHOR LOADS AT PIT WALLS

Nozzle: U-S

Location: 241-C-06C

Sluice Pit

Identification: W-320

Process Air Bldg.

Floor DrainPiping

Node#: B14

Orientation:

(•6)X j

(Plan View1

SEAL POT

Location: Process Air Bldg,

Identification: W-320Process Air Bldg,Floor DrainPiping

Node*: B04

Orientation:(Elevation View)

3

Pipe Loads

Inner Pipe

(Seismic)

(adjusted Seo *6)

(Thermal)

(adjusted See *6)

(Ml

Encasement

(Seismic)(•4)

(Thermal)C5)

Absolute Sum

Pipe Loads

Inner Pipe

Encasement

(Seismic)(•4)

(Thermal)

Absolute Sum

Pipe

Length (• 2)

{in.)

L= 88

L = 88

Pipe

Length ("2)

(in.)

Friction

Force 1*3)

llb/inl

FI . 24.48

FZ. 23.18

Friction

Force («3)

lib/in)

Loads are not applicable sine

are not coincedent at the Se

l . 28.6

i = 28.6

FI . 24.48

F2. 23.18

Fx

libs) ...

114100

903

736

836

Fx

llbsl

Fy

libs)

13

-106

119

Fy

libs)

both Process and Eneas

al Pot.

0

699.15

662.02

1361

Fz

libs)

27100

138

736

2153.26

2038.91

5028

Mx

1Mb)

8 0 48 4 3

3240

3724

4573

Fz

libs)

iment Pipe a

d

Mx

lin-lbl

chors

0

My

lin-lb)

3120

21348

24468

My

(in-lb)

0

Mz

(in-lb)

396

8 4 8

2028

3724

4573

Mz

(in-lbl

0

1"1) (Ref. Appendix C, Autopipe Filename: M7-R0)l«2) L = Pipe lengths immediately preceding anchors as per DWG # ES-320-M07

and ES-320-M08 : (Ref. Appendix A)(•3) For underground pipe. (Ref. Appendix B, STAB)

(••] LOAD = F1 XL{•5) L0AD=F2xL("6) Orientation to Axis "z" is assumed for Nozzle U-8 in this tabulation.

Actual orientation of the Autopipe Mode] is as per DWG # ES-320-M07,45 degrees to the assigned axes, and adjusted for this table by the equations:

0.707 x (Fx + Fz) and 0.707 x (Mx+Mz).


ANCHOR-1.X1.S8/22/95


DESIGN ANALYSIS

Client WESTINGHOUSE HANFORD CO.Subject MISCELLANEOUS PIPING STRESS ANALYSISPROJECT W-320 WASTE RETRIEVAL for TANK 241 -C-106Location C TANK FARM 200 EAST AREA

WO/Job No. ER4319Date / 8 / 22 / 1995Checked S^Revised

Calc. No. W-320-27-028

Revision No. 0

Page No. // of Jj

Filename ANCOR.x|sBy D. L. STpNEBy ^By

Location: Process Air Bldg.Skid Floor

Identification:

Node #:

Orientation:

W-320Process Air Bldg.Metal FilterPiping

E1O

(Elevation View)

Pipe Loads

Inner Pipe(Seismic)

(Thermal)

1*1)

Encasement

(Seismic)1*4)

(Thermal)<*5)

Absolute Sum

Pipe

Length ("2)

(in.)

FrictionForce (»3)

tlb/irtl

!

L- 49

L= 49

FI . 24.48

F2. 23.18

Fx

lib!)

5

-1

6

Fy

libs)

7 4

4 4

1198.54

1134.83

2451

Fz

libs)

217

-178

395

Mx

lin-lb)

7464

5484

12948

My

frn-lb)

48

-24

7 2

Mz

lin-lb)

216

2 4

2 4 0

("1] (Ref. Appendix C, Autopipe Filename: M7-R0)1*2) L = Pipe lengths immediately preceding anchors as per DWG # ES-320-M07

and ES-320-NI08 : (Ref. Appendix A)("3) For underground pipe. {Ref. Appendix B, STAB)(•41 LOAD = F1 XLI"5I L0AD=F2xLC6] Orientation to Axis "z" is assumed for Nozzle U-8 in this tabulation.

Actual orientation of the Autopipe Model is as per DWG # ES-320-M07,45 degrees to the assigned axes, and adjusted for this table by the equations:

0.707 x IFx + Fz) and 0.707 x IMx+Mz).


APPENDIX A


I < ;

oQ_

03

in

c' CO

\k

Q

oo

r

L_

CDc

Idi

Bui

<

oce

ss8

48

2

CO

H-2

-

#

ving

roQ

Fro

m

Q_

DRAIN PIPING FROM PROCESS AIR BLDG FLOOR TO C-106 TANK

DRAIN LINE - 3" - M9ENCASEMENT LINE - 6" - M26a

ALL BENDS SHALL BE 36" RAD (UNLES OTHERWISE NOTEC)

- 14 57 (fif, ft-il)1

3" t>)?-3«l -


SEISMIC AND THERMAL STRESS ANALYSIS OF BURIED PIPE

SOURCES: 1. ASME PAPER ON 'HAND CALCULATION OF SEISMICAND THERMAL STRESSES IN BURIED PIPE' BYG.C.K.YEH, ENGINEERING SPECIALIST, BECHTELPOWER CORP. PVP VOLUME-77, JUNE'83

2. ASME PAPER ON 'FLEXIBILITY ANALYSIS OF BURIEDPIPE' BY E.C.GOODLING, SUPERVISING ENGINEER,GILBERT ASSOCIATES. PVP VOLUME-82, JUNE-78

PROGRAM VERSION: 0

PROGRAM AUTHOR: M.M.AHMED

PROGRAM VERIFIER: T.J.SCHALL.

JOB OR WORK ORDER NO: W 320 / ER 4319

FILENAME: STAB MO8.mcd - SEISMIC

INPUT BY: D.L. STONE DATE: 8 / 2 2 / 9 5

CHECKED BY: C3>^t*~th^ DATE:


STAB. VERS1ON-0PAGE-2

Filename: SB90M8-S.mcdPROGRAMMED BY: M.M.AHMED

STEP1: "DESIGN DATA."ALL UNITS IN POUNDS, INCHES, RADIANS AND DEGREE F.

A. PIPE DATA: (REF.-CRANE TECH PAPER NO:410, 22nd PKINT-1985)

PIPE MATERIAL: ASTM A53, TYPE E, GR B. SCH 40

BEND SIZE: 6" SCH 40, RADIUS=36".PIPE SIZE: 6" SCH 40.

Ds6.625in

ts0.280in

Rs36.00in

PIPE OUTSIDE DIAMETER, IN

PIPE WALL THICKNESS, IN

PIPE METAL AREA, IN*2

PIPE MOMENT OF INERTIA, IN" 4

PIPE SECTION MODULUS, IN"3

BEND METAL AREA, IN"2

BEND SECTION MODULUS, ET3

PIPE BEND RADIUS, IN (36" radius, 90 degree Bend)

056.13-10

<j>sl.57rad

TslOO-K

So=20000

hs 20000--^

Ep0.85

, t-R-4h = 1.002

(D-t

1.6S

0.9

k = 1.648

i= 0.899

MODULUS OF ELASTICITY, PSI(REF:ASME CODE B31.3-1993 ADDENDA 1994)

THERMAL EXPANSION OF ELASTICITY, IN/IN/F.(REF:ASME CODE B31.3-1993 ADDENDA 1994)

BEND ANGLE IN RADIANS (90 deg.)

DESIGN PRESSURE, PSI(REF: CONSTRUCTION SPEC W-320, PIPING CODE M-24)

DESIGN TEMPERATURE, DEG F(REF: CONSTRUCTION SPEC W-320, PIPING CODE M-24)

COLD ALLOWABLE STRESS, PSI(REF:ASME CODE B31.3-1993 ADDENDA 1994)

HOT ALLOWABLE STRESS, PSI(REF.-ASME CODE B31.3-1993 ADDENDA 1994)

WELD JOINT QUALITY FACTOR(REF:ASME CODE B31.3-1993 ADDENDA 1994)

FLEXIBILITY CHARACTER(REF:ASME CODE B31.3-1990 APPDX-D)

FLEXIBILITY FACTOR

SEF FACTOR

IF CALCULATED V IS LESS THAN 1.0, USE i=1.0 U1.00


STAB.VERSION-0 F i I e " a m e :

PAGE-3 PROGRAMMED BY: M.M.AHMED

B: SOIL CHARACTERISTICS(REF: SHANNON & WILSON, INC GEOTECH INVESTIGATION REPORT.)

Bl: SOIL DATA FOR SEISMIC ANALYSIS

C = 12000— SOIL SHEAR WAVE VELOCITY, IN/SECsec

POI = 0.3 POISSON RATIO

KdH0.32 COEF OF LATERAL STRESS

H » 0.75 COEF OF SOIL FRICTION

Eds62000-J^ DYNAMIC ELASTICITY MODULUS, PSIin

rd = 0.066-^ DYNAMIC SOIL SPECIFIC WT,LBS/IN"3in

B2: SOIL DATA FOR STATIC ANALYSIS

Ks • 0.25 COEF OF LATERAL STRESS

Es s 21000— STATIC ELASTICITY MODULUS, PSIin

Ts = 0.066- - ^ STATIC SOIL SPECIFIC WT, LBS/INA3in

H s 36 in DEPTH OF BURIED PIPE, IN

C: SEISMIC RESPONSE FOR GROUND MOTION(REF: SDC-4.1 REV-11)

ag=0.12 FREE FIELD HORIZONTAL ACCEL, FRACTION OF 'G'

Vm=48-ag•— MAX GROUND VELOCITY, IN/SECsec

Vm=5.76-—sec

COMPUTED EFFECTIVE LENGHTS:

1. SEISMIC EFFECTIVE LENGTH (Us):

Les =844.392-in


STAB. VERSION-0 Filename: SB90 M8-S.mcdPAGE-4 PROGRAMMED BY: M.M. AHMED

STAB Subroutine T-3 for Tvpe 3 Bend Analysis E04

For Calculation of Seismic Effective Length: E Lp I 0 c(> = 1.57

from Table 3, Classification of Less: F09 * E 1 °

L p = (3 + (310)+4.08)ft Lp=444.96-in

Lts(4.08)-ft Lt=48'96-in

Les= 844.392-in

Since L (<) Les , this is a case of SP Leg, therefore:

SP: L : = L p

L = 444.96-in

L = 444.96-in

ANALYSIS RESULTS :

SEISMIC ( OCCASIONAL) STRESS (Socc) :

Socc=5.725-103 •— < ALLOWABLE Sail =2.261 -104 •—in2 ia2

CONCLUSION:

PIPE OCCASIONAL STRESSES SATISFY THE CODE B31.3-1990 REQUIREMENTS.


STAB. VERSION-0 PROGRAMMED BY:PAGE 5 M.M.AHMED

STEP 2A: SEISMIC ANALYSIS OF BURIED PIPE AND COMPUTATIONOF INDEPENDENT VARIABLES.

1. SEISMIC SOIL STRAIN.( e m ) :

Vmems

2 ; C REF: 2 ON COVER SHEET

2. SUBGRADE REACTION MODULUS. (K = LBS/IN"3) :

I .< 0.0833

K - ^ U — — I Ed

" I D M E I I ,_poi2

3. SPRING CONSTANT. (S = LBS/IN"2) :

S = K-D

S=3.77-1044in

4. SYSTEM CHARACTERISTIC ( I = INM ) :

\4-E-l/

X =0.058 -in"1

5. SOIL FRICTION.

f = 24.479 •—

6. MAXIMUM SLIPPAGE LENGTH (Lm = I N ) :

ELmsem-A—

7. MAXIMUM AXIAL FORCE ( F = LBS ) :

FsfLm

F=3.93-104-lb


STAB. VERSION-0 PROGRAMMED BY:

PAGE 6 M.M.AHMED

8. MINIMUM TRANSVERSE LEG LENGTH REQUIRED (I = IN) :

JC REF: 2 ON COVER SHEET

1 = 54.048-in

NOTE: SINCE ALL PIPE RUNS WILL GENERALLY BE LONGER THAN,"1", IT IS ASSUMED THAT TRANSVERSE LEG LENGTH CRITERIA HASBEEN SATISFIED AND ALL CONSTANTS Cl THRU C6 IN SUCCEEDINGFORMULAE ARE EQUAL TO 1.0 . THEREFORE THE FOLLWINGFORMULAS ARE MODIFIED USING THE VALUES OF CONSTANTS AS 1.0

9. INDEPENDENT VARIABLE ( a21) :

X3

Jv k-R-—+ 4'E l K-D

10. INDEPENDENT VARIABLE (a31) :

2-X

a31=3.243-105 •—

11. INDEPENDENT VARIABLE (a32) :

a32»X

a32= 0.058-in1

12. INDEPENDENT VARIABLE ( a ) :

aaa31 + a21a32

a=3.496-105 •—

13. SEISMIC EFFECTIVE LENGTH (Les = IN) :

A— • 1 + 2-sm- - 1

Les =844.392-in



STEP 3B: SEISMIC ANALYSIS AND CALCULATION OF SHEAR FORCES,MOMENTS AND STRESSES IN PIPE BEND.

1. DEPENDENT VARIABLE (all) :

/ L2

all=smL- f\f

2-A-E

all =0.092-in

2. DEPENDENT VARIABLE (al2):

al2 = - iA-E

al2=-2.717-10~6 • -lb

3. DISPLACEMENT AT BEND (5 = inches):

a l lS = -

l - a l 2 a

8=0.047-in

4. SHEAR IN TRANSVERSE LEG (Qt = LBS) :

Qtsa-8

Qt = 1.649-104 -lb

5. MOMENT IN BEND ( M = IN-LBS ):

M=a21S

M = 2.052-104 -inlb

6. SHEAR IN LONGITUDINAL LEG ( Qp = LBS ) :

Qp=1.193-103-lb



7. CODE B31.3 COMPLIANCE FOR SEISMIC + SUSTAINED STRESSES.Socc < Sail

Socc=—+ i — + — Sall= 1.33-Ej-Sh*t Zb A b

Sooo = 5.725-103 - ^ < Sall=2.26M04 • —

CONCLUSION: PIPE OCCASIONAL STRESSES SATISFY CODEB31.3 REQUIREMENTS.


S T A B

SEISMIC AND THERMAL STRESS ANALYSIS OF BURIED PIPE

SOURCES: 1. ASME PAPER ON 'HAND CALCULATION OF SEISMICAND THERMAL STRESSES W BURIED PIPE' BY

G.C.K.YEH, ENGINEERING SPECIALIST, BECHTELPOWER CORP. PVP VOLUME-77, JUNE'83

2. ASME PAPER ON 'FLEXIBILITY ANALYSIS OF BURIEDPIPE' BY E.C.GOODLING, SUPERVISING ENGINEER,GILBERT ASSOCIATES. PVP VOLUME-82, JUNE-78

PROGRAM VERSION: 0

PROGRAM AUTHOR: M.M.AHMED.

PROGRAM VERIFIER: T.J.SCHALL.

JOB OR WORK ORDER NO: W 320 / ER 4319

FILE NAME: SB45M8-T.mcil

INPUT BY: D.L. STONE

CHECKED BY:

DATE: 8 / 22 / 95

DATE: ^/l

HMF-2475, Rev. 0Page A-26

STAB. VERSION-0PAGE NO: 2

Filename: SB45M8-T.mcdPROGRAMMED BY: M.M. AHMED

STEP1: " DESIGN DATA."ALL UNITS IN POUNDS, INCHES, RADIANS AND DEGREE F.

A. PIPE DATA. (REF: CRANE TECH PAPER NO. 410, 22nd PRINT-1985

PIPE MATERIAL: ASTM A53, TYPE E, GR B. SCH 40

PIPE SIZE: 6" SCH 40. BEND SIZE: 6" SCH 40, RADIUS= 36"

Ds 6.625-in

t = 0.280-in

I = 28.14-ii

Zb»8.496-in3

= 36.00in

E=29.34-106—in

a=6.13-10~6~(in-K)

<t>s2.356-rad

P.60-4in

T=100-K

lbSc.20000

in2

Sh.20000

EJ=0.85

F=1.00

t-R-4h=- h = 1.002

(D -1) '

1.65~~h~

0.9

k = 1.648

i =0.899

PIPE OUTSIDE DIAMETER, IN

PIPE WALL THICKNESS, IN

PIPE METAL AREA, IN"2

MOMENT OF INERTIA, EST4

SECTION MODULUS, D O

BEND METAL AREA, INA2

BEND SECTION MODULUS, DvT3

PIPE BEND RADIUS, IN (36" Radius, 45 degree Bend)

MODULUS OF ELASTICITY, PSI(REF:ASME CODE B31.3-1993 ADDENDA 1994)

THERMAL EXPANSION OF ELASTICITY, IN/DOT.(REF:ASME CODE B31.3-1993 ADDENDA 1994)

BEND ANGLE IN RADIANS

DESIGN PRESSURE, PSI(REF: CONSTRUCTION SPEC W-320, PIPING CODE M-24)

DESIGN TEMPERATURE, DEG F(REF: CONSTRUCTION SPEC W-320, PIPING CODE M-24)

COLD ALLOWABLE STRESS, PSI(REF:ASME CODE B31.3-1993 ADDENDA 1994)

HOT ALLOWABLE STRESS, PSI(REF:ASME CODE B31.3-1993 ADDENDA 1994)

WELD JOINT QUALITY FACTOR(RERASME CODE B31.3-1993 ADDENDA 1994)

CYCLIC FACTOR FOR 7000 C/S

FLEXIBILITY CHARACTER(REF:ASME CODE B31.3-1990 APPDX-D)

FLEXIBILITY FACTOR

SIF FACTOR

IF CALCULATED 'i' IS LESS THAN 1.0, USE i=1.0i=1.00HNF-2475, Rev. 0Page A-27

C=12000-

POI = 0.3

Kd = 0.32

Ed = 62000-

rd = 0.066-

sec

lb

lb. 3

STAB. VERSION-0 Filename: SB45M8-T.mcdPAGE-3 PROGRAMMED BY: M.M.AHMED

B: SOIL CHARACTERISTICS(REF: SHANNON & WILSON, INC GEOTECH INVESTIGATION REPORT.)

Bl: SOIL DATA FOR SEISMIC ANALYSIS

SOIL SURFACE WAVE VELOCITY, IN/SEC

POISSON RATIO

COEF OF LATERAL STRESS

COEF OF SOIL FRICTION

DYNAMIC ELASTICITY MODULUS, PSI

DYNAMIC SOIL SPECIFIC WT,LBS/BST3

B2: SOIL DATA FOR STATIC ANALYSIS

COEF OF LATERAL STRESS

STATIC ELASTICITY MODULUS, PSI

STATIC SOIL SPECIFIC WT, LBS/ENT3

H=36-in DEPTH OF BURIED PIPE, IN .

C: SEISMIC RESPONSE FOR GROUND MOTION(REF: SDC-4.1 REV-11)

ag. 0.12 FREE FIELD HORIZONTAL ACCEL, FRACTION OF 'G'

Vm=48- ag- — MAX GROUND VELOCITY, IN/SECsec

Vm=5.76-—sec

COMPUTED THERMAL EFFECTIVE LENGTH

Ks

Es

Fs

= 0.25

= 21000'

• 0.066-

lb. 2i nlb~3


STAB. VERSION-0PAGE-4

Filename: SB4SM8-T.mcdPROGRAMMED BY: M.M.AHMED

STAB Subroutine T-2 for Tvpe 2 Bend Analysis

For Calculation of Thermal Effective Length:

from Table 3, Classification of Less:

L =444.96-in

2Let=3.092-103 -in

E01Tlitl

E04 ,

Lt2(6.5 + 10 + 8.O7)-ft

L t =294.84 -in

Lp

* =2.356

E09

Lt

E10

Since L p (<) 2-Let

this is a case of SP Leg, therefore:

SP: LI := —2

LI =222.48-in

Since Lt (<) 2-Let

this is a case of SP Leg, therefore:

SP: L2 := —2

L2= 147.42-in

Ll=222.48-in L2=147.42-in

ANALYSIS RESULTS:

Set = 5.797-103 - -^ < ALLOWABLE Sa=4.965-104 - ^

CONCLUSION:

PIPE DISPLACEMENT STRESSES SATISFY THE CODE B31.3-90REQUIREMENTS.


STAB. VERSION-0 PROGRAMMED BY: M.M. AHMEDPAGE NO: 5

STEP 2B: THERMAL ANALYSIS OF BURIED PIPE AND COMPUTATION OFINDEPENDENT VARIABLES.

l.THERMAL STRAIN (st = IN/IN)

e t s a (T-40K)

8t=3.678-10"4 •—in

2. SUBGRADE REACTION MODULUS ( Kt = LBS/EST3 ) :

0.0833

3. SPRING CONSTANT ( St = LBS/IN"2 ) :

St=KtD

St = 1.167

4. SYSTEM CHARACTERISTIC ( Xt = EMM ) :

Xt= 0.043 -in"1

5. SOIL STATIC FRICTION (ft = LBS/IN):

ft =23.181--

6. MAXIMUM SLIPPAGE LENGTH ( Lt = IN) :

7. MAXIMUM AXIAL FORCE (Ft = LBS):

Ft.ftLt



8. MINIMUM LENGTH OF TRANSVERSE LEG (It = IN)

It s — REF: 2 ON COVER SHEETXt

It =72.463-in

ASSUMED THE LENGTH OF ALL TRANSVERSE LEGS WILLGENERALLYBE MORE THAN "It" . AS SUCH ALL CONSTANTS Cl THRU C6 INFOLLOWING EQUATIONS ARE CONSIDERED AS 1.0 AND FORMULAEARE MODIFIED ACCORDINGLY.

9. INDEPENDENT VARIABLE (A21) :

3k-R-* 4-Xt

HA21 s M- H

\ E-I Kt-D

10. INDEPENDENT VARIABLE (A31) :

KtDA31=

2-X.t

A31 =1.346-105 •—in

11. INDEPENDENT VARIABLE (A32 ) :

A32=Xt

A32= 0.043-in'1

12. INDEPENDENT VARIABLE ( At) :

At6A31 +A21-A32

At = 1.441-105 •—in

13. THERMAL EFFECTIVE LENGTH ( Let) :

r A-Ef/, 2stAt\ ,Lets h+ -1

At I ft /

HNF-2475, Rev. 0PageA-31


THERMAL ANALYSIS OF PIPE BEND AND COMPUTATION OF SHEAR FORCES,MOMENTS AND STRESSES IN PIPE BEND. DDE TO THERMAL STRAIN IN LONGPIPE LEG.

l.DEPENDENT VARAIBLE (All) :

All=st-Ll - ft-—\ 2-A-E

All =0.078-in

2. DEPENDENT VARIABLE (A12) :

A-E

A12=-1.359-10"6 •—lb

3. DISPLACEMENT AT BEND (6t=in) :

st_ All1 - A12-A1

St= 0.066-in

4. SHEAR IN TRANSVERSE LEG (Vt=lbs) :

VUAt-St

S. MOMENT IN BEND (Mt=in.lbs)

MUA21-5t

6. SHEAR IN LONGITUDINAL LEG (Vp=in.lbs)

Vp«X,t-Mt

Vp=624.376-lb

7. DISPLACEMENT STRESS AT BEND ( Se = Psi)

; M i v NOTE: THIS DISPLACEMENTSesi- — + STRESS AT BEND IS DUE TO

\ Z b / A b STRAIN IN ONE PIPE LEG.l b COMPUTE STRESSS DUE TO

Se=3.386-103 OTHER LEG AND ADD THESE HNF-2475, Rev. 0in2 TOGETHER. Page A-32

STAB. VERSION-0 PROGRAMMED BY: M.M.AHMEDPAGE NO: 8

B. DUE TO THERMAL STRAIN IN SHORT PIPE LEG:

1. DEPENDENT VARIABLE (BH) :

Bll=et-L2- ft—!\ 2-A-E,

Bll =0.053 -in

2. DEPENDENT VARIABLE (B12):

6 1 2 ^A-E

B12= -9.003 -10"? •—lb

3. DISPLACEMENT AT BEND (81=inches)

811 - B12At

81 =0.047-in

4. SIIEAR FORCE IN TRANSVERSE LEG (VI=Lbs):

VlsAt-Sl

5. MOMENT IN BEND (Ml=in.Ibs) :

M1=A21S1

Ml =1.025-11

6. SHEAR IN LONGITUDINAL LEG (V2=lbs) :

V2=Xt-Ml

V2 = 444.523 -lb

7. DISPLACEMENT STRESS AT BEND (Sel= Psi) :

/Ml\ VI\

Sel =2.411-103 - i


STAB. VERSION-0 PROGRAMMED BY: M.M.AHMEDPAGE NO: 9

8. CODE B31.3 COMPLIANCE FOR DISPLACEMENT STRESS.

P DSet=Se + Sel SL =

4-t

SL =354.911 - -^in

Sa = F-(1.25(So + Sh) - SL)

Sa=4.965-104 •—

CONCLUSION: PIPE DISPLACEMENT STRESSES SATISFYCODE B31.3-90 REQUIREMENTS.


APPENDIX C


M7-R0 PROJECT W-32008/22/95 DRAIN PIPING

DRAWING ES-320-M7REVISION 0

ICF KAISER HANFORD COAutoPIPE+4.60 MODEL PAGE

M7-R0 PROJECT U-32008/22/95 DRAIN PIPING

DRAWING ES-320-N7REVISION 0

ICF KAISER HANFORD COAutoPIPE+4.60 MODEL PAGE 4

P O I N T D A T A L I S T I N G

POINT OFFSETS (ft )NAME TYPE X Y Z PIPE ID DESCRIPTION



**• SEGMENT AA00 Run 0 0BOO Tee 0 -0.31A01 Bend 0 -0.75

0 PIPE 100

DOOA03

TeeRun

BOOBO1

SEGMENT BTee 0Bend -0.27

0.380.69

-0.310

0 PIPE 1-0.27

COOB02BO3B04B05

TeeReduRunRunBend

00000

-0.38-0.21-0.33-0.17-2.38

000 PIPE 200

B06B07B08B09B10

RunRunRunRunBend

00000

00000

3.8610.0010.0010.003.00

B11 Run 2.43B12 Run 7.07B13 Bend 2.07

0 2.430 7.070 2.07

Short Elbow, Radius = 2.00 inchBend angle change = 90.00 degMid point at 50.00 percentSIF - In 2.27, Out = 1.89Flex = 6.606



Long Elbow, Radius = 4.50 inchBend angle change = 90.00 degMid point at 50.00 percentSIF - In 1.78, Out = 1.48Flex = 4.577

Elbow, Radius = 36.00 inchBend angle change = 45.00 diMid point at 50.00 percentSIF - In 1.00, Out = 1.00Flex = 1.000

Elbow, Radius = 36.00 inch

E00B14

TeeRun

5.051.82

*** SEGMENT CCOO Tee -0.27C01 Dend -0.27

•** SEGMENT DDOO Tee 0.24D01 Bend 0

*** SEGMENT EE00 Tee 16.35E01 Bend -3.35

E02 Run -4.60E03 Run -7.07E04 Bend -5.71

0 00 -1.82

-0.69 -0.27 PIPE 10 0.27

-0.690

-3.780

0.24 PIPE 1-0.33

48.17 PIPE 23.35

0 -4.600 -7.070 -5.71

Bend angle change = 45.00 degMid point at 50.00 percentSIF - In 1.00, Out = 1.00Flex = 1.000

Short Elbow, Radius = 2.00 inchBend angle change = 90.00 degMid point at 50.00 percentSIF - In 2.27, out = 1.89Flex = 6.606



Long Elbow, Radius = 4.50 inchBend angle change = 90.00 degHid point at 50.00 percentSIF - In 1.78, Out = 1.48Flex = 4.577


M7-R0.OUT 8-22-95 2:27p Page 2 of 27


DRAWING ES-320-H7REVISION 0


H7-R008/22/95

PROJECT U-320DRAIN PIPING





C O M P O N E N T D A T A L I S T I N G

POINT ---COORDINATECftNAME X Y

> —Z

DATATYPE DESCRIPTION

E05E06E07E08E09

RunRunRunRunBend

00000

00000

-3.00-10.00-10.00-10.00-4.08 Long Elbow, Radius = 4.50 inch


Total weight of empty pipes : 1079 Ib

*** SEGMENT AA00 0.00

BOO

A01 NA01A01 MA01 FA02 NA02A02 MA02 FD00

A03

0.000.000.030.120.120.240.200.240.24

-0.89-1.06-1.01-1.06-1.06-1.06-1.01-0.89-0.69

I ANCHOR RigidThermal movements : None

I TEE B16.9 welding teeSIF - In = 1.19, Out = 1.25

***BOO

B01B01B01B01COO

B02B03B04B05B05B05B05B06

SEGMENT B

N

HF

N

MF

0.00

-0.15-0.27-0.23-0.27-0.27

-0.27-0.27-0.27-0.27-0.27-0.27-0.27-0.27

-0.31

-0.31-0.31-0.36-0.48-0.69

-0.89-1.23-1.39-3.40-3.78-3.67-3.78-3.78

0.00

-0.15-0.27-0.23-0.27-0.27

-0.27-0.27-0.27-0.27-0.27-0.160.113.59

TEE

TI

TEE

TI

GUIDE

-0.27 -3.78 13.60 GUIDE

-0.27 -3.78 23.60 GUIDE

TI

TEE B16.9 welding teeSIF - In = 1.19, Out = 1.25

ANCHOR RigidThermal movements : None

B16.9 welding teeSIF - In = 1.19, Out = 1.25


ID : B06 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set WeightlessID : B07 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set WeightlessID : B08 1, Connected to GroundStiffness- RIGIDGap-down = 0.00, Above = 0.06 inch

H7-R0.OUT 8-22-95 2:27p Page 3 of 27

M7-R0 PROJECT W-32008/22/95 DRAB

POINTNAME

B09

B10 NBIOB10 MB10 FB11

B12

B13 NB13B13 HB13 FEOO

B14

PIPING

C 0 M P

---COORDINATECftX

-0.27

-0.27-0.27-0.040.612.16

9.23

10.4311.3011.4012.5516.35

18.17

*** SEGMENT CCOO

C01 NC01C01 HC01 FC02 NC02C02 HC02 FC03

-0.27

-0.41-0.53-0.50-0.53-0.53-0.53-0.51-0.45-0.44

*** SEGMENT D

Y

-3.78

-3.78-3.78-3.78-3.78-3.78

-3.78

-3.78-3.78-3.78-3.78-3.78

-3.78

-0.69

-0.69-0.69-0.64-0.52-0.52-0.35-0.40-0.35-0.35

DRAWING ES-320-M7 ICF KAISER HANFORD COREVISION 0

0 N E N T

)--- DATAZ TYPE

33.60 GUIDE

35.3536.60 TI36.5037.4739.03 GUIDE

46.10 GUIDE

47.2948.17 TI47.9448.1748.17 TEE

46.35 ANCHOR

-0.27 TEE

-0.120.00 TI-0.030.000.000.00 TI0.040.140.16 ANCHOR

AutoPIPE+4.60 MODEL PAGE 7

D A T A L I S T I N G

DESCRIPTION

Gap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set WeightlessID : B09 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set Weightless

ID : B11 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set WeightlessID : B12 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set Weightless

B16.9 welding teeSIF - In = 1.22, Out = 1.30RigidThermal movements : None


RigidThermal movements : None

M7-R0 PROJECT W-32008/22/95 DRAIt

POINTNAME

D00

D01 ND01D01 MD01 FD02

PIPING

C O M

---COORDINATECftX

0.24

0.240.240.240.240.24

*•* SEGMENT EEOO

E01 NE01E01 ME01 FE02

E03

E04 NE04E04 HE04 FE05

E06

E07

16.35

13.2713.0113.0112.748.41

1.34

-4.27-4.37-4.35-4.37-4.37

-4.37

-4.37

Y

-0.69

-0.69-0.69-0.64-0.520.00

-3.78

-3.78-3.78-3.78-3.78-3.78

-3.78

-3.78-3.78-3.78-3.78-3.78

-3.78

-3.78

DRAWING ES-320-M7 ICF KAISEfREVISION 0

P O N E N T

)--- DATAZ TYPE

0.24 TEE

0.07-0.10 TI-0.05-0.10-0.10 ANCHOR

48.17 TEE

51.2551.52 TI51.3651.2546.92 GUIDE

39.85 GUIDE

34.2434.14 TI34.1233.9831.14 GUIDE

21.14 GUIDE

11.14 GUIDE

AutoPIPE+4

D A T A L I S T I N C

DESCRIPTION

B16.9 welding teeSIF - In = 1.19, Out =

Rigid

HANFORD CO.60 MODEL PAGE 8

1.25

Thermal movements : None

B16.9 welding teeSIF - In = 1.22, Out =

ID : E02 1, ConnectedStiffness = RIGIDGap-down = 0.00, AboveGap-left = 0.06, RightFriction = 0.15Gaps set WeightlessID : E03 1, ConnectedStiffness = RIGIDGap-down = 0.00, AboveGap-left = 0.06, RightFriction = 0.15Gaps set Weightless

ID : E05 1, ConnectedStiffness = RIGIDGap-down = 0.00, AboveGap-left = 0.06, RightFriction = 0.15Gaps set WeightlessID : E06 1, ConnectedStiffness = RIGIDGap-down = 0.00, AboveGap-left = 0.06, RightFriction = 0.15Gaps set WeightlessID : E07 1, ConnectedStiffness = RIGIDGap-down = 0.00, AboveGap-left = 0.06, RightFriction = 0.15

1.30

to Ground

= 0.06 inch= 0.06 inch

to Ground

= 0.06 inch= 0.06 inch

to Ground

= 0.06 inch= 0.06 inch

to Ground

= 0.06 inch= 0.06 inch

to Ground

= 0.06 inch= 0.06 inch

M7-R0.OOT 8-22-95 2:27p Page 4 o f 27

M7-R0 PROJECT W-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0

ICF KAISER KANFORD COAutoPIPE+4.60 MODEL PAGE





POINT ---COORDINATE(ft )--- DATANAME X Y Z TYPE DESCRIPTION

P I P E D A T A L I S T I N G

Pipe ID/ Norn/ O.D. ThicknessCinch) Spec Weight<lb/ft )Material Sch inch W.Th. Corr Mill Insu Ling Grav Pipe Other Total

-4.37 -3.78

E09E09E09E09E10

N

MF

-4.37-4.37-4.37-4.37-4.37

-3.78-3.78-3.67-3.400.30

-2.57-2 94-2.84-2.94-2.94

TI

ANCHOR RigidThermal movements

Gaps set WeightlessID : E08 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set Weightless

PIPE 1 2.000 2.375 0.154 0.06 0.02 0A312-TP304L STD

PIPE 2 3.000 3.500 0.216 0.06 0.03 0A312-TP304L STD

0 1.25 3.74 0 5.56

0 1.25 7.75 0 11.76

Number of points in the system : 77

> £

H7-R0.OUT 8-22-95 2:27p Page 5 of 27

H7-R0 PROJECT W-320 DRAWING ES-320-M708/22/95 DRAIN PIPING REVISION 0


M7-R0 PROJECT W-320 DRAWING ES-320-M708/22/95 DRAIN PIPING REVISION 0


M A T E R I A L D A T A L I S T I N G

Material Density Pois. Temper. Modulus Expans. Allow.Name Pipe ID Ib/cu.ft Ratio deg F E6 psi in/100ft psi

A312-TP304L PIPE 1

A312-TP304L PIPE 2

501.0 0.30 40.0 28.42 16700.0100.0 0.6457 16700.0

501.0 0.30 40.0 28.42 16700.0100.0 0.6457 16700.0

TEMPERATURE AND PRESSURE DATAC A S E 1 C A S E 2 C A S E 3

POINT PRESS. TEMPER EXPAN. PRESS. TEMPER EXPAN. PRESS. TEMPER EXPAN.NAME psi deg F in/100ft psi deg F in/100ft psi deg F in/100ft

***A00A03

***BOO814

***COOC03

D00D02

***EOOE10

SEGMENT A60.0060.00

SEGMENT 860.0060.00

SEGMENT C60.0060.00

SEGMENT 060.0060.00

SEGMENT E60.0060.00

100100

100100

100100

100100

100100

0.6460.646

0.6460.646

0.6460.646

0.6460.646

0.6460.646

H7-R0.OUT 8-22-95 2:27p Page 6 of 27



ICF KAISER HANFORD COAutoPIPE+4.60 RESULT PAGE 1

M7-R0 PROJECT W-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0


A N A L Y S I S S U M M A R Y

Current model revision number : 19

Static - Date and Time of analysis Aug 22, 1995 2:26 PMModel Revision Number 19Number of load cases 3Load cases analyzed GR T1 P1Gaps/Friction/Yielding considered NoHanger design run NoCut short included NoWeight of contents included YesPressure stiffening case 0Water elevation for buoyancy loads .... Not considered

Modal - Date and Time of analysis Aug 22, 1995 2:26 PMModel Revision Number 19Number of modes 7Cutoff frequency (Hz) 33.0Weight of contents included YesPressure stiffening case 0Water elevation for buoyancy loads .... Not considered

Response - Date and Time of analysis Aug 22, 1995 2:26 PMModel Revision Number 19Number of load cases 3Load cases analyzed R1 R2 R3Date and time of modal analysis Aug 22, 1995 2:26 PMNumber'of modes 7Cutoff frequency (Hz) 33.0Model revision of modal analysis 19Weight of contents included YesPressure stiffening case 0Water elevation for buoyancy loads Not considered

CODE COMPLIANCE COMBINATIONS

Combination Category Method Load Factor Allowable Remarks

GR + Max P Sustain1 Sum

Cold to T1 Expansion Sum

Max P Hoop

SRSS Occasion SRSS

Gravi ty 1.00 Automat i c Default

Max Long 1.00

Thermal 1 1.00 Automatic Default

Max Hoop 1.00 Automatic Default

Response 1 1.00 Automatic User

Response 2 1.00Response 3 1.00

OTHER USER COMBINATIONS

Combination Method Load Factor Remarks

GR

T1

P1

SUM

Sum

Sum

Sum

Sum

Gravity

ThermaI 1

Press 1

GravityThermal 1Press 1

1.00

1.00

1.00

1.001.001.00

Default

Default

Default

User

Abs sum Response 1 1.00 UserResponse 2 1.00Response 3 1.00

Abs sum SUMRESP

1.001.00

CODE COMPLIANCE

Y - Factor 0.40Weld efficiency factor 1.00Range reduction factor 1.00Design Pressure Factor 1.00Minimum stress ratio used in reports... 0.00Include corrosion in stress catcs YInclude torsion in code stress NInclude axial force in code stress .... NLongitudinal pressure calculation PD/4tInclude rigorous pressure Y

H7-R0.OUT 8-22-95 2:27p Page 7 of 27

M7-R0 PROJECT U-3E0 DRYING ES-320-M708/22/95 DRAIN PIPING REVISION 0

ICF KAISER HAUFORD COAutoPIPE+4.60 RESULT PAGE

M7-R0 PROJECT U-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0

ICF KAISER HANFORD COAutoPIPE+4.60 RESULT PAGE

> to4

RESPONSE SPECTRUM LOAD CASES :

Number of load cases analysed : 3

Load case 1 - R1

Missing mass : NoZPA : No

Combination method : SRSS

Load case 2

Missing mass : NoZPA : No


Y- Spectrum : SC2&3Multiplier : 1.00

X- Spectrum :Multiplier :

SC2S3

FreqeHz) Grav(

0.1000.4001.640

20.000

SC2&51 00

)

0.010.060.250.16

Freq(Hz)

0.1600.6008.00033.000

Grave >

0.020.090.250.12

FreqeBz)

0.2501.10012.000100.000

Grave )

0.040.170.200.12

FreqeHz)

0.1000.4001.640

20.000

Grave )

0.010.060.250.16

FreqeHz)

0.1600.6008.00033.000

Grave )

0.020.090.250.12

FreqeKz)

0.2501.10012.000100.000

Grave )

0.040.170.200.12

H7-R0.OUT 8-22-95 2:27p Page 8 of 27

M7-R0 PROJECT U-320 ORAUING ES-320-M708/22/95 DRAIN PIPING REVISION 0

ICF KAISER HAN FORD COAutoPIPE+4.60 RESULT PAGE

H7-R0 PROJECT U-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0

ICF KAISER KANFORD COAutoPIPE+4.60 RESULT PAGE 6

Hissing mass.: No2PA : No


Z- Spectrum : SC2S3Multiplier : 1.00

SC2S3

Freq(Hz) Gravt ) Freq(Hz) GravC ) Freq(Hz) Grav(

0.1000.4001.640

20.000

0.010.060.250.16

0.1600.6008.00033.000

0.020.090.250.12

0.2501.10012.000100.000

0.040.170.200.12

F R E Q U E N C I E S

Mode Frequency Frequency PeriodNumber (Rads/sec) (Hertz) (Sec)

Participation factorsX Y Z

1

2

3

4

5

6

7

50.1612

72.4863

73.6238

109.0702

119.4096

172.3600

183.5339

7.9834

11.5365

11.7176

17.3591

19.0046

27.4319

29.2103

0.125

0.087

0.085

0.058

0.053

0.036

0.034

-0.466

0.013

0.230

-0.616

0.014

0.319

0.355

-0.002

-0.611

0.019

0.003

-0.306

-0.042

0.022

-1.635

0.026

0.689

0.355

0.004

-0.082

0.001

M7-R0.OUT 8-22-95 2:27p Page 9 of 27




H7-R0 PROJECT W-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0


D I S P L A C E M E N T S

Point Loadname combination

TRANSLATIONS (in )X Y 2

ROTATIONS (deg )X Y Z

***

AOO

BOO

A01

A01

A01

A02

Segment A

N

M

F

II

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1 'SUMRESPTOTAL

begin •

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0020.0000.0020.0000.002

0.0000.0020.0000.0020.0000.002

0.0000.0020.0000.0020.0000.002

0.0000.0020.0000.0020.0000.002

0.0000.0000.0000.0000.0000.000

0.000-0.0020.000

-0.0020.0000.002

0.000-0.0060.000

-0.0060.0000.006

0.000-0.0060.000

-0.0060.0000.006

0.000-0.007o.ooo

-0.0070.0000.007

0.000-0.0070.000

-0.0070.0000.007

0.0000.0000.0000.0000.0000.000

0.000-0.0010.000

-0.0010.0000.001

0.000-0.0030.000

-0.0030.0000.003

0.000-0.0020.000

-0.0020.0000.003

0.000-0.0020.000

-0.0020.0000.002

0.000-0.0020.000

-0.0020.0000.002

0.0000.0000.0000.0000.0000.000

0.0000.0360.0000.0360.0030.039

0.0000.0070.0000.0070.0000.007

0.000-0.0010.000

-0.0010.0000.001

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0150.0000.0160.0030.018

0.0000.0020.0000.0020.0010.004

0.000-0.0010.000

-0.0010.0010.002

0.000-0.0060.000

-0.0060.0000.006

0.000-0.0060.000

-0.0060.0000.006

0.0000.0000.0000.0000.0000.000

0.000-0.0210.000

-0.0210.0020.023

0.000-0.0110.000

-0.0110.0010.012

0.000-0.0050.000

-0.0050.0000.005

0.000-0.0060.000

-0.0050.0010.006

0.000-0.0060.000

-0.0050.0010.006


Pointname

A02 M

A02 F

DOO

A03

Loadcombination

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

TRANSLATIONS ( i n )X

0.000-0.0010.000

-0.0010.0000.001

0.000-0.0010.000

-0.0010.0000.001

0.000-0.0010.000

-0.0010.0000.001

0.0000.0000.0000.0000.0000.000

Y

0.000-0.0070.000

-0.0070.0000.007

0.000-0.0060.000

-0.0060.0000.006

0.000-0.0050.000

-0.0050.0000.005

0.0000.0000.0000.0000.0000.000

z0.000

-0.0010.000

-0.001o.ooo0.001

0.0000.0000.0000.0000.0000.001

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

ROTATIONS (degX

0.0000.0060.0000.0060.0010.007

0.0000.0070.0000.0070.0010.008

•o .ooo0.0030.0000.0030.0010.004

0.0000.0000.0000.0000.0000.000

Y

0.000-0.0080.000

-0.0080.0000.009

0.000-0.0080.000

-0.0080.0000.008

0.000-0.0060.000

-0.0050.0000.006

0.0000.0000.0000.0000.0000.000

Jz

0.000-0.0070.000

-0.0070.0010.008

0.000-0.0070.000

-0.0070.0010.008

0.000-0.0060.000

-0.0060.0010.007

0.0000.0000.0000.0000.0000.000

*** Segment A end '

*** Segment B begin 1

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

0.0000.0000.0000.0000.0000.000

0.000-0.0020.000

-0.0020.0000.002

0.000-0 .0020.000

-0 .0020.0000.002

0.0000.0010.0000.0010.0000.002

0.000-0.0010.000

-0.0010.0000.001

0.000-0.0010.000

-0.0010.0000.001

0.0000.0360.0000.0360.0030.039

-0.0010.0800.0000.0800.0080.088

0.0000.0150.0000.0160.0030.018

0.0000.0280.0000.0280.0040.032

0.000-0.0210.000

-0.0210.0020.023

0.001-0.0330.000

-0.0320.0030.036

H7-R0.OUT 8-22-95 2:27p Page. 10 of 27

H7-R0 PROJECT W-32008/22/95 DRAIN PIPING


ICF KAISER HANFORO COAutoPIPE+4.60 RESULT PAGE





Pointname

B01 H

B01 F

COO

B02

B03

B04

Loadcombination

GRTlP1SUMRESPTOTAL

GRTlPISUMRESPTOTAL

GRTlP1SUMRESPTOTAL

GRTlPISUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRTlP1SUMRESPTOTAL

TRANSLATIONS (in )X

0.000-0.0040.000-0.0040.0000.004

0.000-0.0070.000-0.0070.0010.008

0.000-0.0110.000-0.0110.0010.012

0.000-0.0150.000-0.0150.0020.017

0.000-0.0210.000-0.0210.0020.024

0.000-0.0240.000-0.0240.0030.027

Y

0.0000.0040.0000.0040.0010.005

0.0000.0060.0000.0060.0010.007

0.0000.0040.0000.0040.0010.005

0.0000.0030.0000.003.0.0010.004

0.0000.0010.0000.0010.0010.002

0.0000.0000.0000.0000.0010.001

z0.000-0.0020.000-0.0020.0000.002

0.000-0.0060.000-0.0060.0000.007

0.000-0.0160.000-0.0160.0020.018

0.000-0.0290.000-0.0290.0030.032

0.000-0.0500.000-0.0500.0050.056

0.000-0.0610.000-0.0620.0070.068

ROTATIONS (deg

X

-0.0010.149

. 0.0010.1490.0160.165

-0.0010.2210.0010.2210.0250.246

-0.0010.2440.0010.2450.0280.273

-0.0010.2930.0010.2940.0340.328

-0.0010.3190.0020.3200.0370.356

-0.0010.3230.0020.3240.0370.361

Y

0.0000.0590.0000.0590.0070.067

0.0000.0630.0000.0630.0070.070

0.0000.0820.0000.0820.0090.091

0.0000.0820.0000.0820.0090.091

0.0000.0820.0000.0820.0090.092

0.0000.0820.0000.0820.0090.092

)z0.001-0.0880.000-0.0870.0100.097

0.000-0.0980.000-0.0990.0120.111

0.000-0.1010.000-0.1010.0120.113

0.000-0.0880.000-0.0880.0110.099

0.000-0.0790.000-0.0800.0110.091

0.000-0.0770.000-0.0780.0110.089


Pointname

B05 N

B05 M

B05 F

B06

B07

B08

Loadcombination

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

ORTlP1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

TRANSLATIONS (X

0.000-0.0530.000-0.0530.0070.060

0.000•0.0540.000-0.0540.0070.062

0.000-0.0510.000-0.0510.0070.058

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

Y

0.000-0.0130.000-0.0130.0010.014

0.000-0.0190.000-0.0190.0000.020

0.000-0.0260.000-0.0260.0000.026

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

in )z0.000-0.194-0.001-0.1950.0220.217

0.000-0.206-0.001-0.2060.0240.230

0.000-0.207-0.001-0.2070.0240.231

0.000-0.185-0.001-0.1850.0240.209

0.000-0.121-0.001-0.1210.0240.145

0.000-0.0570.000-0.0570.0240.081

ROTATIONS (deiX

-0.0010.2710.0010.2710.0320.303

-0.0010.1630.0010.1620.0210.183

-0.0020.0500.0000.0480.0090.057

0.006-0.0580.000-0.0520.0040.056

-0.0020.0150.0000.0130.0010.014

0.002-0.0030.000-0.0010.0010.002

Y

0.0000.0820.0000.0820.0100.092

0.0000.0820.0000.0820.0100.093

0.0000.0810.0000.0820.0110.092

0.0000.0500.0000.0500.0070.057

0.000-0.0170.000-0.0170.0020.019

0.0000.0170.0000.0170.0020.019

J )Z

0.000-0.0640.000-0.0640.0100.074

0.000-0.0610.000-0.0610.0100.071

0.000-0.0610.000-0.0610.0100.070

0.001-0.0560.000-0.0550.0090.065

0.002-0.0420.000-0.0400.0080.048

0.003-0.0280.000-0.0250.0080.032

! H7-R0.0OT 8-22-95 2:27p Page 11 of 27

M7-R008/22/95

Pointname

B09

B10 N

B10 M

B10 F

B11

B12

SBNF-2475, R

ev.lee A

-46

PROJECT U-320 DRAWING ES-320-H7DRAIN PIPING REVISION 0

Loadcombination

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1PISUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

D I S P L A C E M E N

TRANSLATIONS (in )X

0.0000.0000.0000.0000.0000.000

0.000-0.0200.000-0.0210.0040.024

0.000-0.0250.000-0.0250.0070.032

0.000-0.0170.000•0.0170.0100.027

0.0000.0160.0000.0160.0150.031

0.0000.0610.0000.0610.0150.076

Y

0.0000.0000.0000.0000.0000.000

0.0010.0010.0000.0010.0010.002

0.0000.0010.0000.0020.0010.003

0.0000.0010.0000.0010.0010.002

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

z0.0000.0060.0000.0070.0240.031

0.0000.0170.0000.0180.0240.042

0.0000.0260.0000.0260.0230.049

0.0000.0280.0000.0290.0210.050

0.0000.0160.0000.0160.0150.031

0.0000.0610.0000.0610.0150.076

ICF KAISER HANFORD COAutoPIPE+4.60

T S

RESULT PAGE 11

ROTATIONS (deg )X

-0.006-0.0010.000-0.0080.0020.010

0.001-0.0030.000-0.0020.0030.005

0.003-0.0040.000-0.0010.0030.004

0.004-0.0050.0000.0000.0030.004

0.009-0.0050.0000.0050.0030.008

0.024-0.0030.0000.0210.0100.031

Y

0.000-0.0520.000-0.0520.0080.059

0.000-0.0450.000-0.0450.0120.056

0.000-0.0020.000-0.0020.0150.017

0.0000.0450.0000.0460.0180.063

0.0000.0790.0000.0800.0160.096

0.000-0.143-0.001-0.1440.0180.162

Z

0.005-0.0140.000-0.0090.0070.016

0.005-0.0110.000-0.0070.0070.013

0.005-0.0100.000-0.0050.0060.011

0.006-0.0080.000-0.0030.0060.009

0.004-0.0070.000-0.0030.0070.010

0.004-0.0020.0000.0020.0020.004


Pointname

B13 N

B13 M

B13 F

E00

B14

Loadcombination

GRT1P1SUMRESPTOTAL

GRT1PISUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

*** Segment B end

*** Segment C begin

COO GRT1P1SUMRESPTOTAL

0 I S P L A C E M E N

TRANSLATIONS (in )X

0.0000.0280.0000.0290.0110.039

0.0000.0160.0000.0170.0090.025

0.0000.0200.0000.0210.0090.029

0.0000.0440.0000.0450.0080.053

0.0000.0000.0000.0000.0000.000

***

***

0.000-0.0110.000-0.0110.0010.012

Y

-0.0090.0000.000-0.0080.0030.011

-0.0160.0000.000-0.0150.0050.020

-0.0200.0000.000-0.0190.0050.025

-0.0150.0000.000-0.0150.0040.019

0.0000.0000.0000.0000.0000.000

0.0000.0040.0000.0040.0010.005

z0.0000.1080.0000.1090.0200.129

0.0000.1380.0010.1390.0230.162

0.0000.1530.0010.1540.0230.177

0.0000.0680.0000.0680.0080.076

0.0000.0000.0000.0000.0000.000

0.000-0.0160.000-0.0160.0020.018


T S

RESULT PAGE 12

ROTATIONS (deg )X

0.038-0.0030.0000.0350.0120.048

0.042-0.0020.0000.0400.0130.053

0.044-0.0020.0000.0420.0130.056

0.0490.0000.0000.0490.0150.064

0.0000.0000.0000.0000.0000.000

-0.0010.2440.0010.2450.0280.273

Y

0.000-0.153-0.001-0.1540.0170.171

0.000-0.0960.000-0.0960.0090.105

0.000-0.0130.000-0.0130.0050.017

0.0000.2090.0010.2110.0330.244

0.000O.0000.0000.0000.0000.000

0.0000.0820.0000.0820.0090.091

Z

-0.007-0.0010.000-0.0080.0000.009

-0.009-0.0010.000-0.0090.0010.010

-0.005-0.0010.000-0.0060.0000.006

0.0170.0000.0000.0170.0040.021

0.0000.0000.0000.0000.0000.000

0.000-0.1010.000-0.1010.0120.113

M7-R0.OUT 8-22-95 2:27p Page 12 of 27

M7-R0 PROJECT U-320 DRAUING ES-320-M708/22/95 DRAIN PIPING REVISION 0


M7-R0 PROJECT U-320 DRAUING ES-320-H708/22/95 DRAIN PIPING REVISION 0



Pointname

C01 N

C01 M

C01 F

C02 N

C02 M

C02 F

Loadcombination

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1PISUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL


0.000-0 .0090.000

-0 .0090.0010.010

0.000-0.0070.000

-0.0070.0010.007

0.000-0.0040.000

-0.0040.0000.004

0.000-0.0040.000

-0.0040.0000.004

0.000-0.0010.000

-0.0010.0000.001

0.0000.0000.0000.0000.0000.000

Y

0.0000.0010.0000.0010.0000.001

0.0000.0000.0000.0000.0000.000

0.0000.0010.0000.0010.0000.001

0.0000.0010.0000.0010.0000.001

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

z0.000

-0.0130.000

-0.0130.0010.014

0.000-0.0080.000

-0.0080.0010.009

0.000--0.0040.000

-0.0040.0000.004

0.000-0.0040.000

-0.0040.0000.004

0.000-0.0010.000

-0.0010.0000.001

0.0000.0000.0000.0000.0000.000

ROTATIONS <de<X

-0.0010.2220.0010.2220.0260.248

-0.0010.1840.0010.1840.0230.206

-0.0010.1330.0010.1330.0170.149

-0.0010.1330.0010.1320.0170.149

-0.0010.0650.0000.0650.0080.073

0.0000.0010.0000.0010.0000.001

Y

0.0000.0900.0000.0900.0090.100

0.0000.0720.0000.0720.0060.079

0.0000.0470.0000.0470.0030.051

0.0000.0470.0000.0470.0030.051

0.0000.0330.0000.0330.0020.035

0.0000.0010.0000.0010.0000.001

z0.000

-0.112-0.001-0.1130.0120.125

0.000-0.129-0.001-0.1300.0130.143

0.000-0.1010.000

-0.1010.0100.111

0.000-0.1010.000

-0.1010.0100.110

0.000-0.0490.000

-0.0480.0050.053

0.000-0.0010.000

-0.0010.0000.001


Pointname

C03

Loadcombination

GRT1P1SUMRESPTOTAL

TRANSLATIONS (X

0.0000.0000.0000.0000.0000.000

Y

0.0000.0000.0000.0000.0000.000

in )Z

0.0000.0000.0000.0000.0000.000

ROTATIONS (deqX

0.0000.0000.0000.0000.0000.000

Y

0.0000.0000.0000.0000.0000.000

Jz

0.0000.0000.0000.0000.0000.000

*** Segment C end '

*** Segment D begin '

D00

ooi

D01

D01

002

* * *

N

M

F

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

Segment D

Segment E

0.000-0.0010.000

-0.0010.0000.001

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

end * * *

begin * * *

0.000-0.0050.000

-0.0050.0000.005

0.000-0.0050.000

-0.0050.0000.005

0.000-0.0040.000

-0.0040.0000.004

0.000-0.0030.000

-0.0030.0000.003

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.000-0.0010.000

-0.0010.0000.001

0.000-0.0020.000

-0.0020.0000.002

0.000-0.0020.000

-0.0020.0000.002

0.0000.0000.0000.0000.0000.000

0.0000.0030.0000.0030.0010.004

0.0000.0020.0000.0020.0010.002

0.0000.0100.0000.010o.ooo0.011

0.0000.0180.0000.0180.0010.019

0.0000.0000.0000.0000.0000.000

0.000-0.0060.000

-0.0050.0000.006

0.000-0.0050.000

-0.0050.0000.006

0.000-0.0030.000

-0.0030.0000.003

0.000-0.0020.000

-0.0020.0000.002

0.0000.0000.0000.0000.0000.000

0.000-0.0060.000

-0.0060.0010.007

0.000-0.0060.000

-0.0060.0010.007

0.000-0.0040.000

-0.0040.0010.005

0.000-0.0020.000

-0.0020.0000.002

0.0000.0000.0000.0000.0000.000

M7-R0.OUT 8-22-95 2:27p Page 13 of 27


DRAUING ES-320-H7REVISION 0

ICF KAISER HANFORD COAutoPIPE*4.60 RESULT PAGE


DRAUING ES-320-H7REVISION 0




TRANSLATIONS (in )X Y Z


E00

E01 N

E01 M

E01 F

E02

E03

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1 •P1SUMRESPTOTAL

0.0000.0440.0000.0450.0080.053

0.0000.1720.0010.1730.0350.208

0.0000.1740.0010.1750.0360.211

0.0000.1710.0010.1720.0360.207

0.0000.1810.0010.1830.0376.220

0.0000.1360.0010.1370.0370.174

-0.0150.0000.000

-0.0150.0040.019

-0.0700.0000.000

-0.0700.0230.093

-0.0730.0000.000

-0.0720.0240.096

-0.0710.0000.000

-0.0710.0230.094

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0680.0000.0680.0080.076

0.0000.2350.0010.2360.0350.272

0.0000.2440.0010.2450.0370.282

0.0000.2480.0010.2490.0380.288

0.0000.1810.0010.1830.0370.220

0.0000.1360.0010.1370.0370.174

0.0490.0000.0000.0490.0150.064

0.0790.0000.0000.0780.0280.107

0.0790.0000.0000.0790.0280.107

0.0820.0000.0000.0820.0290.111

0.0630.0000.0000.0630.0220.085

0.0280.0000.0000.0280.0090.037

0.0000.2090.0010.2110.0330.244

0.0000.1850.0010.1860.0390.224

0.0000.1180.0010.1180.0270.146

0.0000.0490.0000.0490.0150.064

0.000-0.0680.000

-0.0690.0070.076

0.0000.0750.0000.0760.0100.086

0.0170.0000.0000.0170.0040.021

0.0120.0000.0000.0120.0050.017

0.0090.0000.0000.0090.0040.013

0.0040.0000.0000.0040.0030.007

0.0190.0000.0000.0190.0060.025

0.0470.0010.0000.0470.0150.062


Pointname

E04 N

E04 M

E04 F

E05

E06

E07

Loadcombination

GRT1PISUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

TRANSLATIONSX

0.000-0.0020.000

-0.0020.0220.024

0.000-0.0040.000

-0.0040.0210.025

0.000-0.0050.000

-0.0040.0200.025

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

Y

-0.0190.0000.000

-0.0200.0050.025

-0 .0190.0000.000

-0 .0200.0050.025

-0.0180.0000.000

-0.0190.0050.024

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

0.0000.0000.0000.0000.0000.000

( in )z

0.0000.2030.0010.2040.0550.259

0.0000.2020.0010.2040.0550.259

0.0000.2020.0010.2030.0550.258

0.0000.1830.0010.1850.0550.240

0.0000.1190.0010.1200.0550.175

0.0000.0550.0000.0550.0550.110

ROTATIONS (degX

0.0370.0010.0000.0370.0090.046

0.0370.0010.0000.0370.0090.047

0.0370.0010.0000.0370.0090.047

0.0170.0010.0000.0180.0060.024

-0.004-0.0020.000

-0.0060.0020.009

-0.0010.0090.0000.0080.0040.012

Y

0.0000.0450.0000.0460.0270.072

0.0000.0290.0000.0290.0300.059

0.0000.0130.0000.0130.0330.046

0.000-0.0140.000

-0.0140.0270.041

0.0000.0040.0000.0040.0070.011

0.000-0.0010.000

-0.0010.0020.003

I )z

0.0320.0010.0000.0330.0120.045

0.0320.0010.0000.0330.0120.045

0^0320.0010.0000.0330.0120.044

0.0300.0010.0000.0300.0110.041

0.0220.0010.0000.0220.0090.031

0.0130.0000.0000.0140.0060.020

M7-R0.OUT 8-22-95 2:27p Page 14 of 27

2? tEE3 §-2475, R

evA

-49

H7-R0 PROJECT U-320 DRAWING ES-320-M708/22/95 DRAIN PIPING REVISION 0

pointname

E08

E09 N

E09 H

E09 F

E10

Loadcombinat ion

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

GRT1P1SUMRESPTOTAL

* * * Segment E end

D I S P L A CE M E N


0.000O.0000.0000.0000.0000.000

0.0010.0000.0000.0010.0020.002

0.0010.0000.0000.0010.0020.002

0.0010.0000.0000.0000.0020.002

0.0000.0000.0000.0000.0000.000

* * *

M7-

Y

0.0000.0000.0000.0000.0000.000

0.000-0.0270.000

-0.0270.0030.030

0.000-0.0260.000

-0.0260.0010.028

0.000-0.0240.000

-0.0240.0000.024

0.0000.0000.0000.0000.0000.000

RO.OUT

z0.000

-0.0090.000

-0.0090.0550.064

0.000-0.0330.000

-0.0330.0540.087

0.000-0.0350.000

-0.0350.0530.088

0.000-0.0340.000

-0.0330.0500.083

0.0000.0000.0000.0000.0000.000

8-22-95

1CF KAISER HANFORD COAutoPIPE+4.60

T S

ROTATIONS (deX

0.006-0.0340.000

-0.0280.0120.040

-0.001-0.0140.000

-0.0150.0210.036

-0.0010.0170.0000.0160.0510.068

-0.0010.0460.0000.0450.0780.124

0.0000.0000.0000.0000.0000.000

2:27p

Y

-0.0010.0000.0000.0000.0020.002

-0.0010.0000.000

-0.0010.0020.003

-0.0010.0000.000

-0.0010.0020.003

-0.0010.0000.000

-0.0010.0020.002

0.0000.0000.0000.0000.0000.000

!ESULT PAGE 17

)Z

0.0050.0000.0000.0050.0040.010

0.0020.0000.0000.0020.0040.006

0.0020.0000.0000.0020.0040.006

0.0020.0000.0000.0010.0040.005

0.0000.0000.0000.0000.0000.000

H7-R008/22/95

Point/Supp. ID

806B06 1Stiff

B07B07 1stiff

PROJECT W-320DRAIN PIPING

Connect/Type

Guide:RIGID

Guide:RIGID

Load


S U P P O

Combination D i m

GR

T1

P1

SUM

RESP

TOTAL

GR

T1

P1

SUM

RESP

TOTAL

downleft

downrght

downrght

downrght

downleft

downleft

downrght

upleft

upleft

downleft

downleft

downleft

Page

R T F

L O C AForce

1000

33065

20

43165

3111

46276

1200

3420

00

8620

23

8924

15 of 27

ICF KAISERAutop"lPE+4.

O R C E S

LDeform

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

GD i m

XYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYz

HANFORD CO60 RESULT

L O B AForce

0-100

-65-330

0-2

-65-431

1131

76462

0-120

2034

00

20-86

32

2489

PAGE 18

LDeform

0.0000.0000.000

0.0000.000

-0.185

0.0000.000

-0.001

0.0000.000

-0.185

0.0000.0000.024

0.0000.0000.209

0.0000.000o.ooo

0.0000.000

-0.121

0.0000.000

-0.001

0.0000.000

-0.121

0.0000.0000.024

0.0000.0000.145

H7-R008/22/95

Point/Supp. ID

B08B08 1Stiff

B09B09 1Stiff

» a? g

-?3•

°

B11

PROJECT W-320 DRAWING ES-320-M7DRAIN PIPING REVISION 0

Connect/Type

Guide:RIGID

Guide:RIGID

S U

LoadCombination

GR

T1

P1

SUH

RESP

TOTAL

GR

T1

P1

SUH

RESP

TOTAL

GR

P P 0

Dim

downleft

downleft

downleft

downleft

downleft

downleft

downrght

uprght

uprght

downrght

downleft

downleft

down

R T F

L 0 C AForce

1200

1022

00

13122

24

13226

961

5273

01

91275

319

94294

82

ICF KAISER KANFORD COAutoPIPE+4.60

0 R C E S

LDeform

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.000

G LDim

XYZ

XYZ

XYZ

XYZ

XYZ

XYZ

XYZ

XY

XYZ

XYZ

XYZ

XYZ

X

RESULT

0 B Aorce

0-120

22-10

00

22-131

42

26132

-1-96

-2735

-10

-275-91

193

29494

-1

PAGE 19

LDeform

0.0000.0000.000

0.0000.000-0.057

0.0000.0000.000

0.0000.000-0.057

0.0000.0000.024

0.0000.0000.081

0.0000.0000.000

0.0000.0000 006

0.0000.000

•

0.0000.0000.007

0.0000.0000.024

0.0000.0000.031

0.000

H7-R008/22/95

Point/Supp. ID

B11 1Stiff

B12B12 1stiff

E02E02 1

PROJECT W-320 DRAWING ES-320-K7DRAIN PIPING REVISION 0

Connect/Type

Guide:RIGIO

Guide:RIGID

Guide

S U

LoadCombination

T1

P1

SUH

RESP

TOTAL

GR

T1

P1

SUM

RESP

TOTAL

GR

P P 0

Dim

rght

downrght

downrght

downrght

downleft

downleft

downrght

downrght

downrght

downrght

downleft

downleft

downleft

R T F

L O C AForce

1

2138

01

• 84

139

324

87163

1421

0470

02

142474

955

151529

1450


O R C E S

LDeform

0.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

G LDim

YzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXY

RESULT

O B AForce

-821

-97-297

000

-98-8498

17317

11587115

-1-142

1

-3330

333

-202

-335-142335

39939

374151374

0-145

PAGE 20

Deform

0.0000.000

0.0160.0000.016

0.0000.0000.000

0.0160.0000.016

0.0150.0000.015

0.0310.0000.031

0.0000.0000.000

0.0610.0000.061

0.0000.0000.000

0.0610.0000.061

0.0150.0000.015

0.0760.0000.076

0.0000.000

M7-R0.OOT 8-22-95 2:27p Page 16 of 27

H7-R008/22/95

Point/Supp. ID

Stiff

E03E03 1Stiff

<o

E05E05 1Stiff


Connect/Type

:RIGID

Guide:RIGID

Guide:RIGID

Load


S U P P 0

Combination Dim

T1

P1

SUM

RESP

TOTAL

GR

T1

P1

SUM

RESP

TOTAL

GR

upleft

upleft

downleft

downleft

downleft

downleft

downleft

downleft

downleft

downleft

downleft

downrght

R T F

L 0 C AForce

0102

00

145103

1419

159122

1070

057

00

10758

613

11471

1370

ICF KAISERAutoPIPE+4.

0 R C E S

LDeform

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000 -

0.0000.000

0.0000.000

0.0000.000

GDim

zXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYz

HAN FORD CO60 RESULT

L 0 B AForce

0

-72072

000

-73-14573

131413

8615986

0-107

0

-41041

000

-41-10741

969

5011450

0-137

PAGE 21

LDeform

0.000

0.1810.0000.181

0.0010.0000.001

0.1830.0000.183

0.0370.0000.037

0.2200.0000.220

0.0000.0000.000

0.1360.0000.136

0.0010.0000.001

0.1370.0000.137

0.0370.0000.037

0.1740.0000.174

0.0000.0000.000

M7-R008/22/95

Point/Supp. ID

E06E06 1Stiff

E07E07 1Stiff


Connect/Type

Guide:RIGID

Guide:RIGI0

Load


S U P P O

Combination Dim

T1

P1

SUM

RESP

TOTAL

GR

T1

P1

SUM

RESP

TOTAL

GR

T1

upleft

upleft

downleft

downleft

downleft

downrght

downrght

downrght

downrght

downleft

downleft

downleft

up

R T F

L O C AForce

1109

01

136109

1166

147175

1070

58

00

1128

516

11724

1240

19

ICF KAISER HANFORD COAutoPIPE+4.60 RESULT

O R C E

LDeform

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.000

sG

Dim

XYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYzX

L O B AForce

-1091

-10

-109-136

6611

175147

0-107

8-5

00

8-112

165

24117

0-124

-2

PAGE 22

Deform

0.0000.0000.183

0.0000.0000.001

0.0000.0000.185

0.0000.0000.055

0.0000.0000.240

0.0000.0000.000

O.OOO

o.ooo0.119

0.0000.0000.001

0.0000.0000.120

0.0000.0000.055

0.0000.0000.175

0.0000.0000.000

0.000

M7-R0.OUT 8-22-95 2:27p Page 17 o f 27


Point/ Connect/ Load


S U P P 0

Supp. ID Type Combination Dim

P1

SUM

RESP

TOTAL

E08 GRE08 1 GuideStiff :RIGID

T1

P1

• SUM

RESP

TOTAL

HN

F-2475Page A

-52,R

ev.

O

left

upleft

downleft

downleft

downleft

downrght

downrght

downrght

downrght

downleft

downleft

R T F

L 0 C AForce

2

00

1052

85

1137

981

1101

10

2092

804

2896

IGF KAISERAutoPIPE+4.

O R C E S

LDeform

0.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

GDimYzXYzXYzXYzXYzXYzXYzXYzXYzXYzXYz

HAN FORD CO60 RESULT

L O B AForce

19

00

-2-105

58

7113

1-98

1-110

0-1

2-209

480

6289

PAGE 23

LDeform

0.0000.055

0.0000.0000.000

0.0000.0000.055

0.0000.0000.055

0.0000.0000.110

0.0000.0000.000

0.0000.000-0.009

0.0000.0000.000

0.0000.000-0.009

0.0000.0000.055

0.0000.0000.064

M7-R0 PROJECT W-320 DRAWING ES-320-M708/22/95 DRAIN PIPING

Pointname

A00

A03

B06

B07

BOS

Loadcombination X

AnchorGRT1P1SUMRESPTOTAL


GuideGRT1P1SUMRESPTOTAL



REVISION 0

R E S T R A I

FORCES (Ib

-54082

40523428

1-330

-33638

0-650

-651176

020020324

022022426

Y Z

-351378

613491301480

-2-404-2

-40845453

-100-330-2

-43131462

-120340

-86289

-120-100

-1312

132

N T

j

-65092

50563569

1420431255

000000

000000

000000

R E A

Result

351524

714971471642

34072

41247458

1003362

43633468

12039089492

120240

1324

135


C T I O N S

MOMENTS (ft-lbX

-21871

18616202

-1-40-5712

000000

000000

000000

Y Z

08808815103

0-140

-14115

000000

000000

000000

Result

2-910

-9011101

1-320

-31537

000000

000000

000000

32261

22525249

135035941

000000

000000

000000

H7-R0-OUT 8-22-95 2:27p Page 18 of 27

M7-R008/22/95

Point

PROJECT W-320 DRAWINGDRAIN PIPING REVISION

Load

R E S T R

ES-320-M70

* I N T

FORCES ( I b )name combination X

B09

B11

B12

B14

C03

5»KNF

-2475, Rev. 0

ige A-53

—






-1-273

-1-275

19294

-1-97

0-98

17115

-1-333

-2-335

39374

2897

41 903

1141017

3-322

-2-321

11332

Y

-9650

-913

94

-82-20

-843

87

-14200

-1429

151

-10500

-10613

119

-15-985

-5-1005

911096

R E A

Z Resu l t

000000

197

098

• 17115

1333

2335

39374

0137

113827

165

1-727

-3-730

88818

96273

1290

19308

82138

116224

185

142470

2495

56550

105908

4920118

1037

161266

61283

1271408

ICF KAISER HANFORD CCAutoPIPE+4.60 RESULT

C T I O N S

MOMENTS ( f t - l bX

000000

000000

000000

271-10

27067

337

-3128

112621

146

Y Z

000000

000000

000000

41786

81799260

2058

-196

096

7102

j

000000

000000

000000

16900

16933

202

1-65

0-65

670

PAGE 25

Result

000000

000000

000000

3201786

81827270

2095

3173

117122

192

M7-R0 PROJECT W-32008/22/95 DRAIN

Pointname

D02

E02

E03

E05

E06

Loadcombinat


GuideGRT1PISUMRESPTOTAL




DRAWINGPIPING REVISION

R E S T R

ES-320-M70

\ I N T

FORCES ( I b )on X

1-80

-74

11

0-72

0-73

1386

0-41

0-41

950

0-109

-1-109

66175

0808

1624

Y

-8315

2309

34342

-14500

-14514

159

-10700

-1076

114

-13710

-13611

147

-107-50

-1125

117

R E

Z Resu l t

2-326

-2-325

18343

072

0731386

041

041

950

000000

000000

8453

2448

38485

145102

017824

200

10757

012214

134

137109

117567

229

10790

11217

119


A C T I O N S

MOMENTSX Y

-1164

1164

8173

000000

000000

000000

000000

RESULT

(ft-lb )

0-60

-616

000000

0000.00

000000

000000

Z

1-11

0-10

313

000O00

00000o

000000

000000

PAGE 26

Result

1165

1165

9173

000000

000000

000000

000000

M7-R0.OUT 8-22-95 2:27p Page 19 of 27

> &4^ '

C

/i

01


Point Loadname combination X

E07 GuideGRT1P1SUMRESPTOTAL

E08 GuideGRT1PISUMRESPTOTAL

E10 AnchorGRT1P1SUMRESPTOTAL

DRAWINGREVISION

R E S I t l

ES-320-M70

I N T

FORCES (Ib )

0-20-257

110246

-100-156

Y

-124190

-1058

113

-98-110-1

-20980289

-529504474118

R E A

Z Result

000000

000000

0-178-1

-178217395

124190

1059

113

981101

20981289

522021

184229413

ICF KAISER HANFORC COAutoPIPE+4.60 RESULT

C T I 0 N S

MOMENTSX Y

000000

000000

-2458 .2

4576221079

(ft-lbZ

000000

000000

-200-245

)

000000

000000

2-1021820

PAGE 27

Result

000000

000000

44582

4576221080

M7-R0 PROJECT W-320 DRAWING ES-320-M7 ICF KAISER HANFORD CO08/22/95 DRAIN PIPING REVISION C

Pointname

Loadcombi nat i on

AutoPIPE+4.60

ASME B31.3c (1992) CODE COMPLIANCE(Moments in

In-Pl.Moment

1

*** Segment A begin ***

A00

BOO -

BOO +

A01 N-

A01 N+

A01 H

A01 F-

A01 F+

Max PGR + Max PCold to T1SRSS








118713

0909

01037

0313

0413

0100

0122

0122

Out-Pl.Moment

1919

339830

217516

0272

030

0101

0111

0111

ft-lb ) (StressTorsion S.I.F Eq. LoadMoment In Out no. type

(3a) HOOP1.00 1.00 (18) SUST

88 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.19 1.25 (18) SUST

88 1.19 1.25 (17) DISP1.19 1.25 (18) OCC

(3a) HOOP1.19 1.25 (18) SUST

40 1.19 1.25 (17) DISP1.19 1.25 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

40 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

40 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

34 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

25 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

25 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

RESULT

in psiCode

Stress

9264244839511

926494

110541272

9264485440697

9263911225107

9264062173243

92638296178

926401915159

92639064775

PAGE 28

)Code

Allow.

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

H7-R0.OUT 8-22-95 2:27p Page 20 of 27


DRAWING ES-320-M7 ICFREVISION 0

KAISER HAN FORD COAutoPIPE+4.60

ASME B31.3C (1992) CODE COMPLIANCE(Moments in

Point Load In-Pl. Out-Pl.name combination Moment Moment

A02 N- Max PGR + Max PCold to T1SRSS

A02 N+ Max PGR + Max PCold to T1SRSS

A02 M Max PGR + Max PCold to T1SRSS

A02 F- Max PGR + Max PCold to T1SRSS

A02 F+ Max PGR + Max PCold to T1SRSS

DOO - Max PGR + Max PCold to T1SRSS

DOO + Max PGR + Max PCold to T1SRSS

A03 Max PGR + Max PCold to T1SRSS

*** Segment A end **

*** Seqment B beqin **

HN

F-2475. Ri

0122

0122

0112

0110

0100

0695

0251

146

*

0111

0111

061

030

060

0142

091

1324

ft-lb )Torsion S.I.FMoment In Out

1.00 1.0025 1.00 1.00

1.00 1.00

2.27 1.8925 2.27 1.89

2.27 1.89

2.27 1.8919 2.27 1.89

2.27 1.89

2.27 1.8918 2.27 1.89

2.27 1.89

1.00 1.0018 1.00 1.00

1.00 1.00

1.19 1.2518 1.19 1.25

1.19 1.25

1.19 1.2514 1.19 1.25

1.19 1.25

1.00 1.0014 1.00 1.00

1.00 1.00

(StressEq.no.

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

<3a)(18)(17)(18)

<3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

Loadtype

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

RESULT

in psiCodeStress

92639064775

926401915159

926399714139

92638268233

92638145315

9263991846215

92639474260

926419758227

PAGE 29

)Code

Allow.

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

M7-R0 PROJECT U-320 DRAWING ES-320-M708/22/95 DRAIN PIPING REVISION 0

Pointname

BOO

B01 N-

B01 N+

. B01 M

B01 F-

B01 F+

COO -

COO +

B02

Loadcombination












In-Pl.Moment

557346

130527

130527

217318

215916

123824

224722

331245

448342

Out-Pl.Moment

012815

014913

014913

0204

017718

2123

015619

552128

113912

ft-lb )Torsion S.IMoment In

1.19194 1.19

1.19

1.00194 1.00

1.00

2.27194 2.27

2.27

2.27247 2.27

2.27

2.27165 2.27

2.27

1.00165 1.00

1.00

1.19165 1.19

1.19

1.191 1.191.19

1.001 1.001.00

.FOut

1.251.251.25

1.001.001.00

1.891.891.89

1.891.891.89

1.891.891.89

1.001.001.00

1.251.251.25

1.251.251.25

1.001.001.00

(StressEq.no.

<3a)(18)(17)(18)

<3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

<3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

Loadtype

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

RESULT

in psiCodeStress

926553

145891804

9263968354970

926420

164982139

92648999641319

926535

111301606

9264436208774

92643983291145

' 926597

160492069

926525

107651425

PAGE 30

)CodeAllow.

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

H7-R0.OUT 8-22-95 2:27p Page 21 of 27





ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-lb ) (Stress in psi )

Point Load In-Pl. Out-Pl. Torsion S.I.F Eq. Load Code Codename combination Moment Moment Moment In Out no. type Stress Allow.

ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-lb' ) (Stress in psi )


B03

B04

B05

805

B05

B05

B05

B06

B07

N-

N+

M

F-

F+

Max PGR + Max Pcold to T1SRSS









331828

223221

777464

777464

887472

884971

884971

7720811

102563

112411

111710

1283

1283

173

0173

0173

017218

0344

(3a) HOOP 790 167001.00 1.00 (18) SUST 365 16700

1 1.00 1.00 (17) DISP 2374 250501.00 1.00 (18) OCC 274 22211

(3a) HOOP1.00 1.00 (18) SUST

1 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

1 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

1 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

15 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

11 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) OISP1.00 1.00 (18) OCC

790 16700358 167001810 25050211 22211

790 16700399 167005393 25050587 22211

790 16700449 167009581 250501043 22211

790 16700468 16700

10812 250501176 22211

790 16700466 16700

10501 250501147 22211

790 16700409 167005911 25050646 22211

790 167001039 167001878 25050189 22211

790 167001269 16700462 2505044 22211



• Max P

GR + Max PCold to T1SRSS

- Hax PGR + Max PCold to T1SRSS

Max PGR + Max PCold to TlSRSS


• Max PGR + Max PCold to T1SRSS

Max PGR + Max PCold to TlSRSS


10317

2

76135

2393

226327

443731

3356

19

1651

19

036

5

117921

2263

27

2393

710

1

3356

19

13324

3428

32

(3a) HOOP 790 167001.00 1.00 (18) SUST 1273 16700

11 1.00 1.00 (17) DISP 289 250501.00 1.00 (18) OCC 46 22211

(3a) HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a> HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

11 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

7 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

4 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

4 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

4 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

4 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

79010271251200

16700167002505022211

790 16700550 167001835 25050250 22211

790 16700550 167001835 25050250 22211

790 16700407 167003046 25050284 22211

790 16700392 167002478 25050177 22211

790 16700392 167002478 25050177 22211

790 16700812 16700231 25050222 22211

790 167001841 167002981 25050341 22211

H7-R0.OUT 8-22-95 2-.27p Page 22 of 27

H7-R0 PROJECT U-32008/22/95 DRAIN PIPING







Point Load In-PL. Out-Pl. Torsion S.I.F Eq. Load Code Codename combination Moment Moment Moment In Out no. type Stress Allow.

B13 N- Max PGR + Max PCold to TlSRSS

B13 N+ Max PGR + Max PCold to T1SRSS

B13 M Max PGR + Max PCold to TlSRSS

B13 F- Max PGR + Max PCold to T1SRSS

B13 F+ Max PGR + Max PCold to T1SRSS

EDO - Max PGR + Max PCold to TlSRSS

E00 * Max PGR + Max PCold to T1SRSS

B14 Max PGR + Max Pcold to T1SRSS

*** Segment B end :

•** Segment C begin •

6009

329840

567176

574482

4325

246977

19633

3111

65

329840

6009

4325

574482

50115

792

35

121786207

(3a) HOOP 790 167001.00 1.00 (18) SUST 887 16700

4 1.00 1.00 (17) DISP 2072 250501.00 1.00 (18) OCC 376 22211

(3a) HOOP1.00 1.00 (18) SUST

4 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

3 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

3 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

3 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.22 1.30 (18) SUST

3 1.22 1.30 (17) DISP1.22 1.30 (18) OCC

(3a) HOOP1.22 1.30 (18) SUST

1 1.22 1.30 (17) DISP1.22 1.30 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

1 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

790 16700887 167002072 25050376 22211

790 16700384 167004669 25050693 22211

790 16700728 16700

5175 25050753 22211

790 16700728 16700

5175 25050753 22211

790 16700901 16700

3757 25050845 22211

790 167001275 16700813 25050553 22211

790 167003186 1670012433 250501988 22211


'ol ntname

COO

C01 N-

C01 N+

C01 H

C01 F-

C01 F+

C02 N-

C02 N+

C02 M

Loadcombination










In-Pl.Moment

536525

216010

216010

0584

1436

016416

016616

119518

024022

Out-Pl.Moment

016610

0121

0121

112512

118916

11038

11038

171

0733

TorsionMoment

65

65

65

18

112

112

112

112

79

S.IIn

.19

.19

.19

.00

.00

.00

2.272.272.27

2.272.272.27

2.272.272.27

.00

.00

.00

.00

.00

.00

2.27..272.27

2.272.272.27

.FOut

1.251.251.25

1.001.001.00

1.891.891.89

1.891.891.89

1.891.891.89

1.001.001.00

1.001.001.00

1.891.891.89

1.891.891.89

Eq.no.

<3a)(18)(17)(18)

<3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

(3a)(18)(17)(18)

Loadtype

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

HOOPSUSTDISPOCC

CodeStress

9265659759995

9264323703332

9264977905752

9264355809823

92647982821098

9264324791567

9264324821571

92648097861295

926420

121311599

CodeAllow.

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

16700167002505022211

H7-R0.OUT 8-22-95 2:27p Page 23 of 27

M7-R0 PROJECT U-320 DRAWING ES-320-H708/22/95 DRAIN PIPING REVISION 0

ICF KAISER KANFORD COAutoPIPE+4.60 RESULT PAGE 35

H7-R0 PROJECT U-32008/22/95 DRAIN PIPING







In-Pl. Out-Pl. Torsion S.I.F Eq. Load Code CodeMoment Moment Moment In Out no. type Stress Allow.

C02 F- Max PGR + Max PCold to T1SRSS

C02 F+ Max PGR + Max PCold to T1SRSS

C03 Max PGR + Max PCold to T1SRSS

*** Segment C end '

*** Segment D begin '

D00 Max PGR + Max PCold to T1SRSS

001 N- Max PGR + Max PCold to T1SRSS

D01 N+ Max PGR + Max PCold to T1SRSS

D01 M Max PGR + Max PCold to TlSRSS

D01 F- Max PGR + Max PCold to TlSRSS

216317

216317

214316

1456

0291

0986

0986

0965

(3a) HOOP 926 167002.27 1.89 (18) SUST 535 16700

9 2.27 1.89 (17) DISP 8873 250502.27 1.89 (18) OCC 1290 22211

(3a) HOOP1.00 1.00 (18) SUST

I 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

I 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.19 1.25 (18) SUST

5 1.19 1.25 (17) DISP1.19 1.25 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

5 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

5 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

0 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

6 2.27 1.89 (17) DISP2.27 1.89 (18) OCC

926 16700451 167004081 25050578 22211

926 16700464 167003702 25050532 22211

926 16700397 167001074 25050229 22211

926 16700386 16700227 2505053 22211

926 16700398 16700442 25050121 22211

926 16700383 167001449 2505075 22211

926 16700389 16700418 2505071 22211

D01

D02

***

***

E00

E01

E01

E01

E01

E01

F+ Max PGR + Max PCold to T1SRSS


Segment D end

Segment E begin


N- Max PGR + Max PCold to T1SRSS

Nt Max PGR + Max PCold to T1SRSS

M Max PGR + Max PCold to T1SRSS

F- Max PGR + Max PCold to T1SRSS

F+ Max PGR + Max PCold to T1SRSS

061

01647

...

***

0373106

403

349168

353274

352674

44015

071

1113

1231

48

349168

403

35012

44015

352674

(3a) HOOP1.00 1.00 (18) SUST

6 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.22 1.30 (18) SUST

0 1.22 1.30 (17) DISP1.22 1.30 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

926 16700383 16700230 2505036 22211

(3a) HOOP 926 167001.00 1.00 (18) SUST 395 16700

6 1.00 1.00 (17) DISP 3528 250501.00 1.00 (18) OCC 235 22211

790 167001789 167003175 250501317 22211

790 16700377 167003419 25050619 22211

790 16700401 167006075 250501099 22211

790 16700805 167006580 250501215 22211

790 16700936 167006499 250501214 22211

790 16700741 16700

3658 25050687 22211

H7-R0.OUT 8-22-95 2:27p Page U of 27



M7-R0 PROJECT U-320 DRAUING ES-320-M708/22/95 DRAIN PIPING REVISION 0



Point Load In-Pl. Out-Pl. Torsion S.I.F Eq. Load Code Codename combination Moment Moment Moment In Out no. type stress Allow.

ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-lb ) (stress in psi )


E02 Max PGR + Max PCold to T1SRSS


E04 N- Max PGR + Max PCold to T1SRSS

E04 (1+ Max PGR + Max PCold to T1SRSS

E04 H Max PGR + Max PCold to T1SRSS

E04 F- Max PGR + Max PCold to T1SRSS

E04 F+ Max PGR + Max PCold to T1SRSS



1991

37

901

1115

125046

125245

124341

159121

112814

117120

125046

1115

124341

04973

01320

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

<3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a> HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

790 167002157 16700892 25050362 22211

790 167001159 167001190 25050197 22211

790 16700433 167001741 25050424 22211

790 16700480 167003094 25050752 22211

790 16700384 16700

3118 25050738 22211

790 16700403 167002999 25050677 22211

790 16700381 167001688 25050382 22211

(3a) HOOP 790 167001.00 1.00 (18) SUST 1786 16700

0 1.00 1.00 (17) DISP 342 250501.00 1.00 (18) OCC 697 22211

(3a) HOOP 790 167001.00 1.00 (18) SUST 1071 16700

0 1.00 1.00 (17) DISP 108 250501.00 1.00 (18) OCC 187 22211



E09 N- Max PGR + Max PCold to T1SRSS

E09 N+ Max PGR + Max PCold to T1SRSS

E09 M Max PGR + Max PCold to T1SRSS

E09 F- Max PGR + Max PCold to T1SRSS

E09 F+ Max PGR + Max PCold to T1SRSS


*** Segment E end

1083210

7412136

4232187

4232187

4237185

3201146

3201146

0458501

2115

(3a) HOOP 790 167001.00 1.00 (18) SUST 1328 16700

0 1.00 1.00 (17) DISP 225 250501.00 1.00 (18) OCC 101 22211

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a> HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.78 1.48 (18) SUST

0 1.78 1.48 (17) DISP1.78 1.48 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC

790 167001011 16700841 25050333 22211

790 16700377 167001613 250501713 22211

790 16700408 167002866 250503043 22211

790 16700409 167002936 250503001 22211

790 16700430 167002483 250502381 22211

790 16700397 167001397 250501340 22211

(3a) HOOP 790 167001.00 1.00 (18) SUST 359 16700

0 1.00 1.00 (17) DISP 3186 250501.00 1.00 (18) OCC 4588 22211

H7-R0.OUT 8-22-95 2:27p Page 25 of 27

M7-R0 PROJECT U-320 DRAWING ES-3Z0-M708/22/95 DRAIN PIPING REVISION 0




S Y S T E M S U M M A R Y S U M M A R Y

Maximum disptacements fin)

Maximum restraint forces(lb)

Maximum sustained stress

Maximum X :Maximum Y :Maximum Z :Max. total:

Maximum rotations Cdeg)

Maximum X :Maximum Y :Maximum z :Max. total:

0.2200.0960.2880.367

0.3610.2440.1430.383

PointPointPointPoint


E02E01E01E01

B04E00C01B04

HFF

M

LoadLoadLoadLoad

LoadLoadLoadLoad

Comb.:Comb.:Comb.:Comb.:

Comb.:Comb.:Comb.:Comb.:

TOTALTOTALTOTALTOTAL


PointStress psiAllowable psiRatioLoad combination

Maximum displacement stress


Maximum occasional stress


101714808181642

laximum restraint momentsCft-lb)


107920582022095



B14A00C03A00

E10B14814B14

LoadLoadLoadLoad

LoadLoadLoadLoad

Comb.Comb.Comb.Comb.




Maximum hoop stress



Maximum sustained stress ratio


Maximum displacement stress ratio


B14.3186167000.19GR + Max P

B01 N16498250500.66Cold to T1

E104588222110.21SRSS

A00926167000.06Max P

B143186167000.19GR + Max P

B01 N16498250500.66Cold to T1

H7-R0.OUT 8-22-95 2:27p Page 26 of 27



Maximum occasional stress ratio

Maximum hoop stress ratio

* * * The system satisfies ASME B31.3 code requirements * * *• * • for the selected options * * *

M7-R0.OUI 8-22-95 2:27p Page 27 of 27

HNF-2475, Rev. 0

W320-27-029

AY Farm Juniper Stress Analysis

B-i

ICF KAISER |

HANFORD COMPANY

CALCULATION IDENTIFICATION AND INDEX i i i

09 /01 /95


Discipline 27 , P i p i n g and Vesse l s WO/Job No._ER4319 Calculation No. W320-27-029

Project No. & Name

Calculation Item

Project W-320 Waste Retrieval for Tank 241-C-106

AY Farm Jumper Stress Analysis


Dwg. No. ECN NO: W-320-380

Dwg. No.

Other (Study, CDR)

Rev. No.

Rev. No.

Rev. No.


• Preliminary Calculations

E l Final Calculations

• Check Calculations (On Calculation Dated

D Void Calculation (Reason Voided

Incorporated in Final Drawings?

This calculation verified by independent "check" calculation?

El Yes • No

• Yes H No





Originator

M.M. AHMED 9-1-95 M.M.Ahmed 7-12-96 M.M.Ahmed 3-12-97Checked by

M.K. Pal 9/11/95 D.L. Stone 7-15-96 •P.L. stoop 3- lt-97Approved by

CD. Jones 9/11/95 C.D.Jones 7-16-96Checked AgainstApproved Vendor Data

Design Analysis

Page No.

i - ii

5 -6

9 - 1 0

INDEX

Description

Calculation Identification and Index

Calculation Cross Index

Objective, Design Criteria ,Design Inputs

Design Methodology

Assumptions

References

Calculations and Conclusions

ISB Jumper Connectors qualification

Pit wall Anchor loads

JUMPER PIPING 3D ISOMETRIC

HNF-2475, Rev. 0

PageB-1

INDX-AY.XLS

FLUOR DANIELNORTHWEST INC.

CALCULATION IDENTIFICATIONAND INDEX

Page ia of \\\


Discipline: (27) Piping and Vessels wo/job No.: ER4319

Project No. & Name: Project W-320 Waste Retrieval for Tank 241 -C-106

Calculation Item: AY Farm Jumper Stress Analysis


Dwg. No.: See Calculation Cross Index

Dwg. No.:

Other (Study. CDR):


[] Preliminary Calculations

[X] Final Calculations

[] Check Calculations (On Calculation Dated)

[] Void Calculation (Reason Voided)

Incorporated in Final Drawings? [X]

This calculation verified by independent "check" calculations? []


Calculation No.: W320-27-029

Rev. No.

Rev. No.

Rev. No.

Yes

Yes

[I

[X]

No

No




Originator

Checked by

Approved by

Checked AgainstApproved Vendor Data

INDEX

Design AnalysisPage No. Description

l - i i Calculation Identification and Index

Calculation Cross Index

Objective, Design Criteria, Design Inputs

2 - 4 Design Methodology

Assumptions

5 - 6 References

Calculations and Conclusions

ISB Jumper Connectors qualification

Pit Wall Anchor Loads

9-10 JUMPER PIPING. 3D ISOMETRIC

FDNW CALCULATION COVER SHEET

HNF-2475, Rev. 0PageB-2

.ICF KAISER |

HANFORD COMPANY

CALCULATION IDENTIFICATION AND INDEX

09 /01/95

Discipline 27, P i p i n g and V e s s e l s WO/Job No._ER4319 Calculation No. W320-27-029




Originator

M. M. AHMED 9-1-95 M. M. Ahmed 7-12-96q t o r t

MM. Ahmed 3-^-97Checked by

M.K. Pal 9/11/95 D. L. Stone 7-15-96 D.L. Stone *a/2--?7

Design Analysis

Page No.

Appdx A

Appdx B

Appdx C

INDEXDescription

AutoPipe File no: AY02A1R2 For Static Analyisand AY02A2R2 for Dynamic Analysis for Pump Pit jumper

AutoPipe File no:AY02E~R2 for Static andDynamic analysis for Sluice Pit jumper

Reference Documentation

Rev-1 Summary of Changes:

Revised:

Replaced:

Deleted

Pages 1 thru 7

Page 8

Appendix-D

Rev-2 Summary of changes

Revised

Added

and Appendices A , B & C

Pages 1 thru 5

Pages 6 thru 8

Pages 9 S 10


INDX-AY.XLS

FLUOR DANIELNORTHWEST INC.

CALCULATION IDENTIFICATIONAND INDEXContinuation Sheet

Page i ia of

| Discipline (27) Piping and Vessels wo/Job No. ER4319 Calculation No. W320-27-029




Originator

Checked by

3.

INDEX

Design AnalysisPage No.

Description

Appdx A Autopipe File no: AY02A1R2 For Static Analysis and

AY02A2R2 for Dynamic Analysis for Pump Pit jumper

Appdx B Autopipe File no: AY02E-R2 for Static and Dynamic analysis for Sluice Pit jumper

Appdx C Reference Documentation

RevisionNo.

Description

Verify As-Built conditions.

Pages ia, iia, and 6a added. Pages iii, 1, 5, and 10 revised.

FDNW CALCULATION COVER SHEET HNF-2475,Rev.OPageB-4

SubjectCalculationRevision

No.

3

CALCULATIONSubject Calculatio

Supercededby

CalculationNo.

NA

These interfacing calculation/documentsprovide input to the subject calculation,and if revised may require revision of

the subject calculation.

Calculation/Document No.

H-2-818501, Sheen

H-2-818503, Sheen

H-2-818503, Sheet 2

H-2-818544, Sheet 1

H-2-818544, Sheet 2

H-2-818545, Sheen

RevisionNo.

/s,2

1

jar J

^ 2

/ 2 .

CROSS INDEX (Typican No.: W320-27-029


calculations and/or documents


NA

A

RevisionNo.

I)

Does the outputinterface calculation/documents require

revision?

Yes No

K

X

<

<

)<

Has the outputinterfacecalculation/

documents beenrevised?

Yes No

<

X.

P a g e iii o f f j j


complete.

i\ o

'I *\\

KEH 1975.00 (12/88)


DESIGN ANALYSIS

Client WESTINGHOUSE HANFORD COMPANYSubject AY FARM - JUMPER STRESS ANALYSISPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106Location: C TANK FARM - 200 W.

CaicNo. W320-27-029

Revision No. JST^iPage No. 1 of 10

WO/Job No. ER4319 Filename:AY02E.WPDate 8/31/95 By: M.M. AhmedChecked 9/1 1/95 By: M. K. PalRevised By:

Rev-1 By: M.M. Ahmed 7/12/96Checked By: D.L. Stone 7/1 5/96 Checked By:

OBJECTIVE: , p , »>

The objectives of this calculation are:

1. Perform static and dynamic piping stress analysis of the "AY Tank Farm" Jumper Assembliesin order to be in compliance with the Code ASME B31.3 requirements.

2. Qualify the Integral Seal Block (ISB) Jumper connectors for loads exerted bypiping in accordance with document WHC-SD-W236A-DA-002, Rev-0

3. Prepare a report on piping loads exerted on pit wall at pipe penetration location.

To incorporate the design changes made by the ECN NO:W-320-380

REV-2:To incorporate the design changes made by the ECN NO:W-320-587

DESIGN CRITERIA:

1. ASME CODE B31.3-93 with Addenda up to 1994. .2. SDC 4 .1 , REV-12. (MovJ FOMvJ f i n i t e * I3*f.2-i5. \T-\~I )3. PROJECT W-320 FDC: WHC-SD-W320-FDC-001, REV. ?. ^4. WHC-SD-W236A-DA-002, Rev-0

DESIGN INPUTS:

I Rev-1

I Rev-2

GENERAL (Applicable to all Jumpers)Ambient TemperatureDesign Temperature:Design Pressure:Pipe Materials:Pipe Sizes:Pipe WallSafety Class category:Corrosion AllowanceB31.3 Code Allowable stressFlangesConnector weights

Nozzle weightsKickplate weights

40°F180°F325 psigASTM A312TP304L2 in., 3 in. and 4 in.Schedule 40SC-30.06 inches16700 psi300# ANSI rated4": 122 Ibs(Vert) 3":4": 120lbs(Horz)4": 11 lbs 3": 6.5 lbs4": 16.5 lbs 3": 12 lbs

77 lbs 2": 29 lbs

2": 2.5 lbs2": 3.5 lbs

(Ref. 3)(Ref: 3)(Ref: 10)(Ref: 19)(Ref: 19)IRef: 5)(Ref. 4)(Ref. 7)(Ref: 1)(Ref. 21)

.(Ref: 9)

(Ref: 9)(Ref: 9)



DESIGN ANALYSIS


CaicNo. W320-27-029

Revision No. 0Page No. 2 of 10

WO/Job No. ER4319 Filename:AY02E.WPDate 8/31/95 By: M.M. AhmedChecked 9/11/95 By: M. K. PalRevised By:

Rev-1 By: M.M. Ahmed 7/12/96Checked By: D.L. Stone 7/15/96

Rev-2 By: VUChecked By: J)^ -n

JUMPER U2-A, B SLUICE PIT 241-AY-02E (Autopipe Filename: AY02E-R2) I Rev-2

Process Fluid:Specific gravity:Piping Dimensions:Pressure Element WeightPumpPump Motor

241-AY-102 Supernate1.12Dwg: B503AR2, Rev-24": 27 lbs 2": 12 lbsWPumB = 1000 lbs I Rev-1WPumi, „„,,,, = 2250 lbs I Rev-1

Blank 2" Connector with Counter Weight 86.98 lbs4" -2 Way Ball Valve w/ Actuator 93 lbs

• (Ref: 20)(Ref: 8 )(Ref: 191(Ref. 18)(Ref: 1 7)(Ref: 17)(Ref. 22)(Ref: 15)

JUMPER U11 -A PUMP PIT 241-AY-02A (Autopipe Filename: AY02A1 R2 & AY02A2R2) I Rev-2

Process Fluid:Specific gravity:Piping Dimensions:Density/Flow/Temp sensor3"- 3 Way Ball Valve

DESIGN METHODOLOGY:

241-C-106 Slurry1.2H-2-818501, Rev-2153 lbs65 lbs

(Ref: 20)(Ref: 3)(Ref: 19)(Ref: 24)(Ref: 1 5)

AY Farm Jumper Piping Assemblies include Jumper U2-A that is located in Sluice Pit 241-AY-02E I Rev-1and Jumper U11-A located in Pump Pit AY-02A. I Rev-2

The jumper assembly models include connectors and nozzles. The nozzles are considered to be rigidlyanchored either to pit walls or cover plate for tanks (H-2-818545, Ref: 19). I Rev-1

The jumper connectors used on W-320 project are PUREX Connectors. However for analysis I Rev-1purpose, assumed as Integral Seal Block (ISB) connectors (Ref:9) The document WHC-SD-W236A-DA-002 (Ref:22) provides all the analytical data such as connector stiffness, acceptable pipingloads & seating forces for the ISB connectors. These connectors have been modeled in Autopipeas short radius elbows and flexible couplings with specified translation and rotational stiffness.The connector and nozzle weights are imposed at Flexible coupling.

The weights of structural steel assemblies and lifting bails used to connect jumper piping to nozzlesduring installation are calculated and imposed at appropriate points.

Stress analysis of the jumpers has been performed in accordance with ASME B31.3 for sustained,thermal and seismic loading (Ref. 1) using the computer program "Autopipe" Version-4.6 by"Engineering Design Automation" (EDA) (Ref. 11).

HNF-2475, Rev. 0Page B-7

ICF KAISERHANFOHD COMPANY

DESIGN ANALYSIS

client WESTINGHOUSE HANFORD COMPANYsubject AY FARM - JUMPER STRESS ANALYSISPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106Location: C TANK FARM - 200 W.

Rev-1 By: M.M, Ahmed 7/12/96Checked Bv: D.L. Stone 7/15/96

Calc No W320-27-029Revision No.

Page No

WO/Job No. ER4319Date 8/31/95Checked 9/1 1/95Revised

Rev-2, Bv: t_Checked Bv: T

File

By:

By:

By

03 of 10

1ame.-AY02E.WPM.M. AhmedM. K. Pal

= = = = = = = =

Clhmt^-5.1.2 . I - ;£ C S P 3 / 2 - ? 7

SUSTAINED LOADS:

The "AutoPipe" program checks the sustained stress (the summation of gravity and pressurestresses) against the B31.3 Code Allowable stress "S" for the material specified for eachjumper piping.

THERMAL (DISPLACEMENT) STRESS:

The maximum design temperature for the pipe of 180°F and the ambient temperature of 40°Fhas been used in "AutoPipe" program to qualify the thermal expansion stress to theCode B31.3 allowable for displacement stress, "Sa".

SEISMIC STRESSES:

The jumper piping has been categorized as Safety Class 3. However the pit structure isclassified as Safety Class 1 category. In order to perform Safety Class 3/1 analysis forthis investigation, dynamic response spectra analysis is performed using Safety class-1,"Fig 3" seismic response spectra (5% Damping) of SDC 4 .1 , Rev-12 (Ref.2). Thisresponse spectra is created in "AutoPipe" as "SC1" and used in this dynamic analysis.Autopipe qualifies seismic stresses as occasional stress with the code allowable 1.33S.

The Jumper Connectors are qualified in accordance with WHC-SD-236A-DA-002, Rev-0(Ref:22) Table 3.4 Acceptable piping loads. The acceptable axial force is limited toallowable seating forces for 50 ft-lb torque of Table 3.3 assuming all the actual axialloads tend to un-seat connector assembly. This results in conservative analysis. Theacceptable loads are not increased by 1/3 as permitted on page-6 of Ref:22, which isconservative. The interaction of loads for critical connector is calculated (See page-7of this calculations) as specified on page-7 of Ref:22.

HYDRO-STATIC ANALYSIS: I Rev-2

The Jumper Assembly U11-A in pump pit, as a worst case basis, has been analyzed forHydro-Test pressure. The Hydro-Test pressures is considered as 490 psi which is 1.5 times ofthe design pressure 325 psi in accordance with ASME Code B31.3. The AutoPipe programcombines pressure load with gravity load to obtain Sustained stress and compares against Codeallowable for this category.


ICF KAISER caic No. W320-27-029HANFORD COMPANY Revision No. 0


client WESTINGHOUSE HANFORD COMPANY wo/Job No. ER4319 niename.-AY02E.WPsubject AY FARM - JUMPER STRESS ANALYSIS Date 8/31/95 By: M.M. AhmedPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked 9/1 1/95 BV: M. K. PalLocation: C TANK FARM - 200 W. Revised By:

: ft--Rev-1 By.- M.M. Ahmed 7/12/96Checked By: D.L. Stone 7/15/96 Checked By:

The following describes the modelling and analysis techniques unique to individual jumpers.

JUMPER U2-A, SLUICE PIT

Jumper U2-A includes the piping extending from the Tank 102 AY Submersible Pump AssembI'nozzle (A) to the Tank 102 AY Booster Pump, and from the Booster Pump to the Transfer Linenozzle (U-2). The "Frame" feature of the "Autopipe" program has been used to assimilate theBooster Pump Assembly in order to consider the adequate stiffness of the pump in the system.The weight of the pump and motor is imposed at locations corresponding the centers of gravityof the pump and motor. The seismic stabilizer is represented in the model by Channel steelC3x4.1 that connect to the lifting frame sub-assembly and anchored to the pit wall. I Rev-1

A Gravity support (Y-stop) has been modeled directly below the pump assembly which is seatedon concrete pedestal. I Rev-1

Weight of instrumentation has been applied at the instrument center on the pipe with flangesinput as 300# ANSI rated in accordance with the 325 psig design pressure.

Because Autopipe does not provide an eccentric reducer component, the eccentric reducers aremodeled as concentric reducers.

JUMPER U11-A, PUMP PIT 1 Rev-2

The density/Flow/Temperature Sensor has been modelled as rigid section because it is relatively rigidcompared to pipe section. The weight of the Sensor is equally divided and imposed at three locationswhere it is supported by the structural steel members.

Since three way valve can not be modelled in AutoPipe, it has been modelled as three separate valveswith one third of weight of the 3" 3-Way- Ball Valve.

The jumper supporting dunnage steel is modelled as the Frame members. The Guide and Y-stop supportsare modelled at proper locations. Since AutoPipe can not perform Non-Linear dynamic analysis, Y-stopis not considered in Seismic Response Spectra analysis.

PIPING LOADS AT BUILDING PENETRATION ANCHORS I Rev-2

The Pipe Nozzle (U-2 & U-11) Loads at Building Penetrations are summarized on page no:8.


ICF KAISER Caic No. W320-27-029HANFORD COMPANY Revision No. , 0 - 3


Client WESTINGHOUSE HANFORD COMPANY wo/Job No. ER4319 Fiiename:AY02E.WPsubject AY FARM - JUMPER STRESS ANALYSIS Date 8/31/95 By: M.M. AhmedPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked 9/11/95 By: M. K. PalLocation: C TANK FARM - 200 W. Revised By:

Rev-1 By: M.M. Ahmed 7/12/96 Rev-2, By: W- . L"*"^- 3.12 .37Checked By: D.L. Stone 7/15/96 Checked Bv:~7)< <£?&> H-lt-'??

ASSUMPTIONS: I Rev-1

1. It is assumed that the lifting bail and structural steel assemblies designed to supportthe jumper piping during installation will be supported by the jumper during operation.

2. ISB jumper connectors data considered in analysis is compatible with the PUREX connectorused.

3. Building structures and tank nozzles are structurally adequate to withstand pipe loads.

REFERENCES:

1. ASME Code B31.3 and B31.3a-1994 Addenda for "Chemical and Petroleum Refinery."

2. SDC 4 .1 , Rev. 12, "Standard Architecture & Civil Design Criteria."(Vo^d fW^J PtecA.cc * 131-.2.I5. I I 1*7, Oei'j" Lt»Ai '(<•' fac\\,tj, ")

3. WHC-SD-W320-FDC-001, Rev-/. "Functional Design Criteria for Tank 241-C-106 WasteRetrieval, Project W-320". 4̂

4. WHC-SD-WM-SEL-033, Rev-1, "Safety Equipment List for 241-C-106 Waste RetrievalProject W-230"

5. Construction specifications W-320-C5, Rev-0 , Section 15493 for piping materials.

6.Construction Specification No: B-131-C1, Section 1 5415 for piping materials.

7. Calculation No: W-030-011, Rev-1 for "Fouling factor and Corrosion rate."

8. Data Compendium, Bruce A. Castaing

9. Jumper Design Fabrication Drawings: H-2-32440-2 I Rev-1

10. DSI from C.D.Jones dated March 28, 1994 "Design Pressure for Slurry and Sluice Pumps"

11. Computer program "AutoPipe" Version 4.6 by "Engineering Design Automation."

12. Computer Program "EXCEL" Version 4.0, by Microsoft.

13. Crane Technical Paper No: 410, 22nd Printing-1986.

14. Ryerson Stock List and Data Book, 1985-86 Edition, Joseph T. Ryerson & Son, Inc.


ICF KAISER Caic No. W320-27-029

HANFORD COMPANY Revision No. 0DESIGN ANALYSIS Page No. 6 of 10

Client WESTINGHOUSE HANFORD COMPANY WO/Job No. ER4319 Filename:AY02E.WPSubject AY FARM - JUMPER STRESS ANALYSIS Date 8/31/95 By: M.M. AhmedPROJECT W-320 WASTE RETRIEVAL for TANK 241-C-106 Checked 9/11/95 By: M. K. PalLocation: C TANK FARM - 200 W. Revised By:

Rev-1, Bv: M.M. Ahmed 7/12/96 Rev-2: By:Checked By: D.L. Stone 7/15/96 Checked Bv:

15. PBM Reference Book Sec. II (SP Series) and Sec. IV (MP Series), PBM, Inc.

16. Micro Motion, Inc. CMF300 Physical specifications. (Appendix-C)

17. Lawrence Pumps Inc. Vendor Dwg: 5 5 6 4 1 , Rev-2. (Appendix-C)

18. Red Valve Co. Inc., Vendor data on Series 40 Pressure Sensors. (Appendix-C)

19. Piping Arrangement and Detail drawings: H-2-818501 (2 Sheets) Rev-2, H-2-818503(3 Sheets) Rev-2 and ECN No: W-320-587. I Rev-2

20. Process Flow Diagrams: H-2-81 8558 H-2-81 8559, and H-2-818560 . •

2 1 . ASME/ANSI B16.5

22. WHC-SD-W236A-DA-002, Rev-0 "Stress Analysis of Single Port (ISB) Jumper Connectorsfor 2-, 3-, and 4-in Sizes".

23. Seismic Design White Paper Project W-320 Tank 241-C-106 Sluicing

24. Micro-Motion Inc. Product Catalog. I Rev-2

CALCULATIONS:

The calculations are documented in this package as shown below. I Rev-2

AutoPipe stress analysis results Appendices A & B

Jumper Connector load qualification Page-7

Pit Wall Anchor Loads Page-8

Jumper Piping 3D Isometric model for Autopipe Pages- 9 & 10

CONCLUSION: I Rev-2

The review of the "AutoPipe" summary results attached as Appendices to this calculationindicates that all pipe stresses are in compliance with the requirements of ASME Code B31.3requirements.

The Jumper qualification on page-7 indicates that ISB connectors are adequate for pipingloads. The Piping loads on Pit walls at piping penetrations are summarized on page 8.


FLUOR DANIEL Calc No W320-27-029NORTHWEST INC. R**\sim: 3

DESIGN A N A L Y S I S p^ NO.: £* of / OClient: Numatec WO/Job No.: ER4319/W-320

Subject: AY Farm Jumper Stress Analysis Date: n / ^ ^ / . Br- K ̂ vProjectW-320 Waste Retrieval for Tank 241-C-106 checked: 3 . , 3 .q g By: f

Location: AY Tank Farm 200 East Area Revised: By:

Rev. 3

CONCLUSION (CONTINUED)

Rev. 3 of this calculation verified the analysis against the as-built conditions (ao oM1/g1<07). The analysisincludes the weights of valves, flow meters, and pressure sensors. These weights are not critical to theresults of the analysis. Therefore, any differences between the weights used in the analysis and the approvedvendor data are negligible. There are minor dimensional differences (+ 2") between the Autopipe models andthe as-built conditions, however, these differences are also negligible.

HNF-2475, Rev. 0FONW CALCULATION SHEET P 0ftB 19 W320-OI6.WPD


DESIGN ANALYSIS


CaicNo. W320-27-029

Revision No. 0Page No. 7 of 10

WO/Job No. ER4319 Filename:AYO2E.WPDate 8/31/95 By: M.M. AhmedChecked 9/11/95 By: M. K. PalRevised By:

Rev-1. Bv: M.M. Ahmed 7/12/96Checked Bv: D.L. Stone 7/1 5/96

Rev-2, Bv:Checked By

ISB JUMPER CONNECTOR LOADS QUALIFICATION I Rev-2

CONNECTORLOCATION

SLUICE PITConnector A

Connector U-2

PUMP PITConnector U-11

Connector A

AUTO PIPEFILE NAME& NODE

AY02E-R2AOKN)

B10(F)

AY02A1R2AY02A2R2A04IN)

A19(F)

Connector Allowable loads

SIZE

4 "

4 "

4 "

4 "

4 "

CONNECTOR ACTUAL LOADSloads/ ALLOWABLE LOADS

AxialX

(Ibsl

399

1061

135

566

6310

ShearY

(lbs)

547

258

348

144

2220

ShearZ

(lbs)

3 1 0

179

2 3 4

144

2220

TorsionMx

(ft-lb)

26

22

62

35

780

1 Rev-2

BendMy

(ft-lb)

20

304

161

151

1170

BendMz

(ft-lb)

81

128

212

5 5 2

1170

REFNO:

APDX-B

APDX-B

APDX-AGR + T1+RESP

APDX-A

Ref: 22

SEATING FORCES BETWEEN CONNECTOR & NOZZLES:

The axial allowable load considered in table above are limited to seating forces for 4" Connectorsfor 50 ft-lb (pre-load) torque as specified in Table 3.3(Ref:22). Since the actual axial forces are less thanthe allowable seating forces, the connector wilf not be un-seated from the nozzle.

INTERACTION OF SHEAR. TORSION AND BENDING:

I = fyz/Fyz + [mx]/Mx + myz/Myz < 1.0 Ref:22, page-7

Review of actual loads and allowable loads in the table above indicates that the Connector-A

in the Pump Pit is more critical for interaction. I Rev-2

fyz = 204 lbs (SRSS of fy = 144 &fz = 144)

myz = 572ft-lbs (SRSS of my=151 &mz=552)

I = 204/2220 + 35/780 + 572/1170

I = 0.63 < 1.00 As such Jumper Connectors are adequate. HNF-2475, Rev. 0Page B-13


DESIGN ANALYSIS

Client WESTINGHOUSE HANFORD COMPANYSubject AY FARM - JUMPER STRESS ANALYSISPROJECT W-320 WASTE RETRIEVAL for TANK 241 -C-106Location: C TANK FARM - 200 W.

CaicNo. W320-27-029

Revision No. 0

Page No. 8 of 10

WO/Job No. ER4319 Filehame:AY02E.WPDate 8/31/95 By: M.M. AhmedChecked 9/11/95 By: M. K. PalRevised By:

PIT WALL ANCHOR LOADS I Rev-2

NOZZLE ORIENTATION LOADCASES

LOADS (FORCES IN POUNDS & MOMENTSIN FT-LBS)

Fx . Fy Fz Mx My Mz

REF:

U-11PUMPPITAY-02A

Thermal 63 390 52 183 20 35 AY02A1R2A00

Seismic 205 102 90 209 200 27 AY02A2R2A00

Total 268 492 142 392 220 62

U-2SLUICEPITAY-02E

Thermal 125 865 157 449 63 387 AY02E-R2B12

Seismic 102 86 125 94 53 68 SAME

Total 227 951 282 543 116 455

Notes:

1. Seismic Loads could be positive or negative.

2. Thermal loads specified are the algebric sum of gravity and thermal loads.

3. Total loads specified are the absolute sum of thermal and seismic loads disregarding the signs.



DESIGN ANALYSIS

Calc No. W320-27-029

Revision No. 0

Page No. 9 of 10

Client WESTINGHOUSE HANFORD C O M P A N Y wo/Job No.ER4319 Fiiename:AY02E.WP

Subject AY FARM-JUMPER STRESS ANALYSIS Date 8 / 3 1 / 9 5 By: M. M. A h m e dPROJECT W-320 WASTE RETRIEVAL FOR TANK C-106 Checked 9 / 1 1 / 9 5 By: M. K. Pal

Location C T A N K FARM - 2 0 0 W . Revised By:

Rev-2, By: L - OkS^*_,2.<j7Checked By: M-f^€^> 3'/Z'i7

JUMPER ASSEMBLY PUMP PIT: AY-02A-U11-A

DWG: H-2-818501ACAD FILE: AY02AIAPIPE FILE: AY02A1R2

& AY02A2R2PREPARED BY:MM AHMED

CHECKED BY:Dl. STONE

rNOTES: 1. THREE WAY VLAVE IS MODELLED ASTHREE VALVES EACH WEIGHING 22 Lbs.2. FLOW METER'S WEIGTH 153# IS IMPOSED ATTHREE SUPPORT LOCATIONS.3. Y-STOP AT NODE " 7 " IS NOT CONSIDEREDFOR DYNAMIC ANALYSIS.

HNF-2475, Rev 0PageB-15


DESIGN ANALYSIS

Calo No. W320-27-029

Revision No.*&-S>

Page No. 1 0 of 1 0

Client WESTINGHOUSE HANFORD COMPANY wo/Job No.ER4319 Fiiename:AY02E.WPSubject AY FARM-JUMPER STRESS ANALYSIS Date 8 /31 /95 By: M. M. Ahmed

PROJECT W-320 WASTE RETRIEVAL FOR TANK C-106 Checked 9 /11 /95 By: M. K. Pal

Location C TANK FARM - 2 0 0 W . Revised By:

^ t ^ . ^ Rev-2, By: L--

PROJECT W-320: JUMPER ASSY FOR SLUICE PIT

PREPAREDCHECKED I

Vc,We. cf

Itowavtf,-ftie-

A03 4- /107

1. M. AHMEDL. STONE

REF: ECN 1V-320-380

ECN W - 3 2 0 - 5 8 7

DWG: B503AR2 REV-2

AUTOCAD: AY02E

AUTOPIPE: AY02E-R2


AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE*4.60 MODEL PAGE 3

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoP!PE+4.60 MODEL PAGE 4





*** SEGMENT AA00 Run 0A01 Flex 0

A03 Run 0A04 Bend 0

0 0 4"PIPE0 0.25

0 0.100 0.40

A05 Bend -0.17 -1.28

A06 Redu 0A07 Run 0A08 Bend 0

0 0.870 0.33 3»PIPE0 0.38

A09A10A11A12A13

A13AA14A15

A15AA16

RunTeeTeeRunValv

RunTeeValv

RunBend

0.380.771.830.770.96

0.160.100.10

0.160.98

00000

000

00

0 RIGID000 3"PIPE0

000

00

A16 F FarA17 Bend -0.25 -0.83

Wt= 137 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID Bend= 2080.0Z-Shear= RIGID Bend= 2080.0

Short Elbow, Radius = 4.00 inchBend angle change = 90.00 degHid point at 50.00 percentSIF - In 2.56, Out = 2.13Flex = 7.908



Rating = 300, Weight = 22 IbSurface factor = 4.40, SIF = 1.00


Long Elbow, Radius = 4.50 inchBend angle change = 90.00 degHid point at 50.00 percentSIF • In 1.78, Out = 1.48Flex = 4.577

short Elbow, Radius = 4.00 inch

-0.67 -0.25 0

0 0 2.57

0 -0.40 0

A21A22

***A10801802

RunRun

SEGMENT ITeeRunBend

00

!0.98

00

-0-0

-1

.10

.25

.2800 •

220

00

.33 RIGID

.00

.71

B04A11

A14C01

C01AC02

RunTee

SEGMENTTeeValv

RunBend

00

C4.80

0

00

00

-1.280

00

-0.71-2.00

2.33 3"PIPE-0.10

-0.16-0.66

Bend angle change = 84.21 dogMid point at 50.00 percentSIF - In 2.56, Out = 2.13Flex = 7.908

short Elbow, Radius = 4.00 inchSend angle change = 90.00 degMid point at 50.00 percentSIF • In 2.56, Out = 2.13Flex = 7.908

Short Elbow, Radius = 4.00 inchBend angle change = 90.00 degHid point at 50.00 percentSIF - In 2.56, Out = 2.13Flex = 7.908

Ut= 139 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID Bend= 2080.0Z-Shear= RIGID Bend= 2080.0

Elbow, Radius = 6.00 inchBend angle change = 90.00 degSIF - In 1.00, out = 1.00Flex = 1.000

Elbow, Radius = 6.00 inchBend angle change = 90.00 degSIF - In 1.00, Out = 1.00Flex = 1.000


Long Elbow, Radius = 4.50 inchBend angle change = 90.00 deg

AY02A1R2.0UT 3-12-97 9:03a Page 2 of 23

AY02A1R2 PROJECT W-320: TANK03/12/97 AY-02A-U11-A JUMPER

POINTNAME

C03C04C05

C06

C07

TYPE

ReduRunBend

Send

Run

P O I N T

241-CHYDRO

0 A

----OFFSETS (ft )

X Y

0 0.380 0.290 0.48

-0.50 0

0 0

Total weight of empty pipes

Z

000

0

0.96

: 132

-106 SLUICINGSTATIC ANAL.

T A L I S T

FLUOR DANIELAutpPIPE+4.60

I N G

PIPE ID DESCRIPTION

Mid point at 50.00SIFFlex

2"-PIPELong

In 1.78, Out= 4.577

Elbow, RadiusBend angle change =Mid point at 50.00SIFFlex

LongBendMidSIFFlex

Ib

In 1.73, Out= 4.404

Elbow, Radiusangle change =joint at 50.00In 1.73, Out

= 4.404

NORTHWEST, INC.MODEL PAGE 5

percent= 1.48

= 3.00 inch90.00 degpercent= 1.44

= 3.00 inch90.00 degpercent= 1.44

AY02A1R203/12/97

POINT -NAM

***A00

A01A03A04A04A04A04A05A05A05A05A06A07A08A08A08A08A09

A10

A11

A12

A13

PROJECT W-320AY-02A-U11-A

C O H

--COORDINATEDX

SEGMENT

N

MFN

MF

N

MF

A13AA14

A15A15AA16A16A16A16A17A17A17A17A18A18A18

N

HFN

MFN

H

0.

0.

A00

000.000.000.-0.-0.-0.-0.-0.-0.-0.-0.-0.-0.-0.0.0.

0.

2.

3.

444

4

0001041017151717171717062121

98

81

58

547080

905.065.666566

04930404

6.04

55555

9676683746

\

t

tCCc•c•c-c----

--

---

.00

.00

.00

.00

.00

.10

.33

.78

.28

.13

.28

.28

.28

.28

.28

.28

.28,28

.28

.28

.28

.28

.28

.28

.28

.28

.28

.28

.31

.39

.44

.53

.54

.64

.66

.78-1.75

:TANKJUMPER

P O

j

Z

0

0

N E

00

250.350.42000

756575

0.75001

759025

1.621.951.952222

2

33223333

33

2.33

2

222

2222211111111

33

333333

333333332297795058505050.60

241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.HYDRO STATIC ANAL. AutoPIPE*4.60 MODEL PAGE 6

N T

DATATYPE

ANCHOR

TI

TI

TI

FLANGE

FLANGE

TEE

TEE

FLANGE

FLANGE

TEE

WEIGHT

TI

TI

TI


DESCRIPTION


Weld neck SIFRating = 300, Weight =Weld neck SIFRating = 300, Weight =B16.9 welding teeSIF - In = 1.00, Out =B16.9 welding teeSIF - In = 1.00, Out =Weld neck • SIFRating = 300, Weight =Weld neck SIFRating = 300, Weight =

B16.9 welding teeSIF - In = 1.22, Out =5 Ib , No offsets

= 1.0015 Ib= 1.0015 Ib

1.00

1.00= 1.00138 Ib= 1.00138 Ib

1.30

AY02A1R2.OUT 3-12-97 9:03a Page 3 of 23

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 MODEL PAGE 7



POINT ---COORDINATE(ft )--- DATANAME X f Z TYPE DESCRIPTION


POINT ---COORDINATECft )--- DATANAME X Y Z TYPE DESCRIPTION

A18A19A19A19A19A20A21A22

••»A10

801

FN

MF

5.375.375.375.375.375.375.375.37

SEGMENT B0.98

0.96

-1.78•1.78-1.78-1.88•2.11•2.18-2.28•2.53

-1.28

-1.28

1.833.744.073.974.074.074.074.07

2.33

4.33

C06 NC06C06 MC06 FC07

4.55 -0.134.304.374.304.30

•0.13-0.13-0.13-0.13

1.411.41 TI1.481.662.37 WEIGHT 35 1b

B02B02B02B03B03B03B04

N

FN

F

0.980.981.482.312.812.812.81

-1.28•1.28-1.28-1.28•1.28-1.28-1.28

4.545.045.045.045.044.544.33

2.81 -1.28 2.33 TEE

ANCHOR RigidThermal movements : None

TEE B16.9 welding teeSIF - In = 1.00, Out = 1.00

GUIDE ID : B01 1, Connected to 9Stiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.30Gaps set Weightless

TI

ID : B04 1, Connected to 5Stiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.30Gaps set WeightlessB16.9 welding teeSIF - In = 1.00, Out = 1.00

number of points in the system : 73

*** SEGMENT CA14

C01C01AC02 NC02C02 MC02 FC03C04C05 NC05C05 MC05 F

4.80

4.804.804.804.804.804.804.804.804.804.804.734.55

•1.28

-1.28-1.28-1.28-1.28-1.17•0.90-0.90-0.61-0.38•0.13-0.20-0.13

2.33 TEE

2.232.071.781.41 TI1.521.411.411.411.411.41 TI1.411.41


AY02A1R2.0UT 3-12-97 9:03a Page 4 of 23

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 MODEL PAGE 9

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 MODEL PAGE 10

^


Pipe ID/ Nom/ 0.0. Thickness(inch) Spec UeightClb/ft )Material Sch inch W.Th. Corr Hill Insu Ling Grav Pipe Other Total

4"P!PE 4 4.500 0.237 0.06 0.03 0 0 1.20 11.04 0 17.66A312-TP304L STD

3"PIPE 3.000 3.500 0.216 0.06 0.03 0 0 1.20 7.75 0 11.60A312-TP304L STD

2"-PIPE 2.000 2.375 0.154 0.06 0.02 0 0 1.20 3.74 0 5.48A312-TP304L STD



A312-TP304L 4"S>!PE

A312-TP304L 3"PIPE

A312-TP304L 2"-PIPE

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

AY02A1R2.OUT 3-12-97 9:03a Page 5 of 23



FRAME POINT DATA LISTING

POINT ---COOROlNATECft )--- DATANAME X Y Z TYPE DESCRIPTION

BEAM DATA LISTING

BEAMID

M1

H2

H3

M4

MS

M6

M7

M8

M9

M10

Mil

M12

M13

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

;FromTor

FromTo

FromTo

POINTNAME

A091

12

23

34

4. A12

35

56

67

78

89

910

5B05

9B01

LENGTH(ft )

0.58

0.77

1.83

0.77

0.58

2.00

1.00

0.92

0.91

1.00

2.00

0.58

0.58

SECTION 10/MATERIAL ID

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4 "A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

BETAANGLE

RIGID RELEASEEND(ft) Ax Y-Y 2-2

A091234A12567

89B0110805

0.210.210.982.813.583.582.812.811.89

0.980.980.980.982.81

-1.28-0.70-0.70-0.70-0.70-1.28-0.70-0.70-0.70

-0.70-0.70-1.28-0.70•1.28

2.332.332.332.332.332.334.335.335.33

5.334.334.332.334.33

WEIGHT

WEIGHTWEIGHT

Y-STOP

WEIGHT

51 Ib

8 Ib51 Ib

10 : 7Gap-BeloiFrictionGaps set51 Ib

, No offsets

, No offsets, No offsets

1, Connected to Groundi = 0.00, Above = 0.50 inch= 0.30Weightless, No offsets

0.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

NN

NN

NN

NN

NN

NN

AY02A1R2.0OT 3-12-97 9:03a

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE*4.60 MODEL PAGE 13

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL.

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 MODEL PAGE 14

CROSS SECTION LISTING

Section ID AreaCsq.in )ID Axial Y-Shear Z-Shear

Inertia (in"*4 )Torsion Y-Y Bend Z-Z Bend

MATERIAL ID

A36

•BEAM MATERIAL LISTING

Elastic Yield Ultimatemodulus Poissons Stress Density Expansion stressE6 psi ratio psi Ib/cu.ft E-6 /F psi

Ar02A1R2.0Ur 3-12-97 9:03a Page 7 of 23



FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60 RESULT PAGE t


POINT PRESS. TEMPER EXPAN. PRESS. TEMPER EXPAN. PRESS. TEMPER EXPAN.NAME psi deg F in/IOOft psi deg F in/WOft psi deg F in/100ft

***AOOA07A09A12A16A22

***A10A11

•*•A14C04C07

SEGMENT A490490490490

F 490490

SEGMENT B490490

SEGMENT C490490490

180180180180180180

180180

180180180

1.5441.544•0.0001.5441.5441.544

0.0000.000

1.5441.5441.544



Static - Date and Tirrte of analysis Mar 12, 1997 9:02 AMMode 1 Rev ? s i on Number 5Number of Load cases 2Load cases analyzed GR T1Gaps/Friction/Yielding considered YesToterance - Force, Displacement tOO.OO tb 0.0162 inFriction - Factor, tolerance 1.00 0.10Hanger design run NoCut short included NoOccasional load analysis type NonlinearNon-linear analysis summary file .. AY02A1R2.LOGBase load cases for nonlinear analysis

GR = NoneT1 = GR

Weight of contents included YesPressure stiffening case 0Water elevation for buoyancy loads Not considered

AY02A1R2.OUT 3-12-97 9:03a Page S of 23

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 2

AY02A1R2 PROJECT H-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 3

CO to



GR * Hax P

Cold to T1

Hax P

Sustain

Expansion

Hoop

Sum

Sum

GraMax

vityLong

Thermal 1

Max Hoop

11

1

1

.00

.00

.00

• op

Automatic

Automatic

Automatic

Default

Default

Default



GR Sum . Gravity 1.00 ' Default

T1 Sum Thermal 1 1.00 Default

GR+T1 Sum Gravity 1.00 UserThermal 1 1.00

CODE COMPLIANCE

Y - Factor 0.40Weld efficiency factor 1.00Range reduction factor 1.00Design Pressure Factor 1.00Minimum stress ratio used in reports... 0.00Include corrosion in stress calcs YInclude torsion in.code stress NInclude axial force in code stress NLongitudinal pressure calculation P0/<itInclude rigorous pressure Not analyzed



*** Segment A begin *

TRANSLATIONS (in )X Y 2

ROTATIONS (deg )X Y 2

A00

A01

A03

A04

A04

A04

A05

A05

A05

A06

A07

N

M

F

K

M

F

GRT1

HT1

GRT1GR+T1

GRT1

GRT1GR+T1

GRT1GR<

GRT1

GRT1GR-

-T1

>T1

•T1

GRT1GR+T1

GR

n

GRT1

I-T1

GRT1GR+T1

0.0000.0000.000

0.0000.0000.000

0.0000.0000.000

0.0010.0000.000

0.0000.0010.001

0.0050.0020.007

0.0160.0030.019

0.0240.0040.027

0.0250.0040.029

0.0230.0030.026

0.0210.0030.023

0.0000.0000.000

0.0000.0000.000

0.0000.0000.000

-0.0010.000-0.001

-0.002-0.002-0.004

-0.002•0.005-0.008

-0.001-0.012-0.013

-0.001-0.018-0.018

-0.001-0.020-0.021

-0.002-0.019-0.021

-0.002-0.019-0.021

0.0000.0000.000

0.0000.0040.004

0.0000.0040.004

0.0000.0050.005

-0.0010.0080.008

-0.0020.0100.008

-0.0040.0100.005

-0.0060.0120.006

-0.0060.0170.011

-0.0060.0230.017

-0.0060.0280.022

0.0000.0000.000

0.0010.0000.001

0.0340.0010.035

0.0340.0010.035

0.0340.0020.035

0.0290.0020.031

0.0280.0020.O3O

0.021-0.0010.020

0.009-0.0040.005

0.006•0.0040.002

•0.001•0.004-0.005

0.0000.0000.000

0.0010.0000.000

0.024-0.0050.019

0.024-0.0050.019

0.026-0.0040.022

0.027-0.0030.024

0.028-0.0020.025

0.0280.0010.029

0.0290.0070.036

0.0290.0090.038

0.0290.0110.040

0.0000.0000.000

0.0000.0000.000

-0.109-0.007-0.117

-0.109-0.007-0.117

-0.109-0.007-0.117

-0.112-0.005-0.117

-0.113-0.005-0.118

-0.1190.002-0.117

-0.1210.006-0.115

-0.1230.008-0.115

-0.1260.011-0.115

AY02A1B2.0UT 3-12-97 9:03a Page 9 of 23

AY02A1R2 PROJECT tf-320: TANK03/12/97 AV-02A-U11-A JUMPER

Pointname

A08 N

Loadcombinati

GRTlGR+T1

241-C-HYDRO

D I S P L A

TRANSLATIONSon X Y

-0.021-0.003-0.023

-0.002-0.019-0.021

106 SLUICINGSTATIC ANAL.

C E M E N T S

(in )

z•0.0060.0280.022

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 RESULT PAGE 4


-0.001-0.004-0.005

0.029 -0.1260.011 0.0110.041 -0.115

AY02A1R2 PROJECT U-32003/12/97 AY-02A-U11-A


: TANKJUMPER

241-C-106 SLUICINGHYDRO STATIC ANAL.



A16 N GR -0.018T1 0.037GR*T1 0.019

-0.120 -0.0470.014 -0.023•0.106 -0.070



-0.120-0.009-0.129

0.035 -0.0570.035 0.0200.070 -0.037

GR71GR+T1

GRT1GR+T1

•0.0190.000

•0.019

-0.0180.005

•0.013

•0.004-0.018-0.022

-0.009-0.017-0.026

-0.007O.O320.025

-0.009O.O310.022

-0.043-0.008-0.050

-0.064-0.011-0.075

0.0310.0300.061

0.0330.0490.082

-0.1190.017

-.0.102

-0.1110.028

-0.083

GRT1GR*T1

GRT1GR+T1

A09

A10

All

A12

A13

A13A

A14

A15

A15A

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

-0.0180.005•0.013

-0.0180.005•0.013

-0.0180.005-0.013

-0.0180.005•0.013

-0.0180.0200.002

•0.0180.0220.004

•0.0180.0240.006

•0.0180.0260.007

-0.0180.0280.010

•0.009-0.017-0.026

•0.027•0.012-0.039

-0.070-0.001-0.071

-0.0880.003-0.085

•0.1060.009-0.097

•0.1080.009-0.098

•0.1090.010-0.099

•0.1110.010-0.100

•0.1130.011-0.102

-0.0090.0310.022

-0.0140.0230.009

-0.0270.004-0.022

-O.O32-0.004-0.036

-0.039-0.013-0.052

-0.040-0.015-0.055

-0.041-0.016-0.056

-0.041-0.016-0.058

-0.042-0.018-0.060

-0.065-0.011-0.075

-0.065-0.011•0.075

-0.065-0.011•0.075

-0.045-0.011-0.075

-0.095-0.010-0.105

-0.095-0.O1O-0.105

-0.099-0.010•0.108

-0.102-0.010-0.111

•0.102•0.010-0.111

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0340.0440.078

0.0340.0440.078

0.0340.0430.077

0.0340.0420.076

0.0340.0420.076

-0.1110.028•0.083

-0.1110.028-0.083

-0.1110.028-0.083

-0.1110.028-0.083

-0.0700.025-0.045

-0.0700.025•0.045

-0.0670.025-0.042

-0.0640.024-0.040

•0.0640.024-0.040

A17

A17

A17

A18

A18

A18

A19

A19

A19

N

M

F

N

M

F

N

M

F

GRTlGR+T1

GRT1GR+T1

GRT1GR*T1

GRT1GR+T1

GRT1GR+T1

GRTlGR+T1

GR 'TlGR+T1

GRT1GR+T1

GRT1GR+T1

-0.0190.0410.022

-0.0220.0430.020

-0.0250.0430.018

-0.0280.0420.014

-0.0300.0400.009

-0.0310.0380.008

-0.0300.0340.004

-0.02S0.0300.003

0.0010.0050.006

0.0030.0020.005

0.0010.0000.002

-0.1260.014

-0.112

-0.1360.013

•0.123

-0.1420.011

•0.131

-0.1490.009

-0.140

-0.1500.007

-0.143

-0.1490.006

•0.143

-0.1410.005

-0.136

-0.1270.004

-0.122

-0.0180.009

-0.008

-0.0050.0080.004

0.0000.0050.005

•0.048-0.026-0.074

-0.046-0.030-0.076

-0.044-0.032-0.077

-0.040-0.036-0.076

-0.033 .-0.038-0.071

-0.031-0.038-0.069

-0.025-0.038-0.063

-0.021-0.035-0.057

-O.O21-0.006-0.027

-0.016•0.002-0.018

-0.0050.000

-0.005

-0.134-0.012-0.146

-0.171-0.016•0.188

-0.174-0.016-0.191

-0.203-0.015-0.218

-0.220-0.010-0.230

-0.222-0.011-0.232

-0.237-0.009-0.246

-0.266-0.012-0.277

-0.270-0.012-0.282

-0.242-0.009-0.251

-0.208-0.007-0.215

0.0340.0170.051

0.035-0.0030.032

0.035-0.0040.031

0.042-0.0170.025

0.055-0.0300.025

0.055-0.0300.024

0.067-0.0450.022

0.071-0.0590.012

0.071-0.0660.005

0.073-0.0660.006

0.075-0.0660.009

-0.0660.011

-0.054

-0.0790.010

-0.069

-0.0800.009

-0.071

-0.075O.O11

-0.064

-0.0690.010

-0.060

-0.0690.009

-0.060

-0.0750.004

-0.071

-0.0810.001

-0.080

-0.069-0.002-0.071

•0.066•0.003-0.068

-0.058-0.003-0.061

AY02A1R2.0UT 3-12-97 9:03a Page 10 of 23

AY02A1R2 PROJECT U-320: TANK03/12/97 AY-02A-U11-A JUMPER

Point Loadnam

A20

A21

A22

***

***

A10

B01

B02

802

B03

B03

B04

A11

combination

GRT1GR*T1

GRT1GR*T1

GR. T1GR+T1

Segment A end

Segment 8 begin

GRT1GR*T1

GR. T1

GR+T1

N GRT1GR+T1

F GRT1GR+TI

N GRT1GR+T1

F GRT1GIHT1

GRT1GR*T1

GRT1GR*T1

Segment B end

D I S


P L A C

TRANSLATIONS (X

0.0010.0000.001

0.0000.0000.000

0.0000.0000.000

***

***

-0.0180.005-0.013

-0.0050.0260.021

-0.0030.0280.025

0.0000.0330.033

0.0000.0330.033

-0.0030.0280.025

-0.0050.0260.021

-0.0180.005-0.013

Y

0.0000.0040.004

0.0000.0040.004

0.0000.0000.000

-0.027-0.012-0.039

0.000•0.008-0.008

0.003-0.007-0.004

-0.002-0.003•0.005

-0.0210.002-0.020

-0.0400.004-0.036

-0.0430.003-0.040

-0.070-0.001-0.071

E I E I T S

n )Z

-0.0020.000-0.002

0.0000.0000.000

0.0000.0000.000

-0.0140.0230.009

-0.0140.0230.009

-0.0140.0230.009

-0.0180.0180.000

-0.0230.010-0.014

-0.0270.004•0.022

-0.0270.004-0.022

-0.0270.004-0.022


ROTATIONS Cdeg )X

•0.207-0.007-0.214

-0.0040.000-0.004

0.0000.0000.000

-0.065•0.011•0.075

-0.065-0.011-0.075

-0.065-0.011-0.075

•0.065-0.011-0.075

-0.065-0.011-0.075

-0.065-0.011•0.075

-0.065-0.011-0.075

-0.065-0.011-0.075

Y

0.075-0.0660.009

0.0000.0000.000

0.0000.0000.000

O.O330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

0.0330.0490.082

Z

-0.057-0.003-0.061

-0.0010.000-0.001

0.0000.0000.000

-0.1110.028-0.083

-0.1110.028-0.083

-0.1110.028•0.083

-0.1110.028-0.083

-0.1110.028-0.083

-0.1110.028-0.083

-0.1110.028-0.083

-0.1110.028-0.083

AY02A1R2 PROJECT U-320: TANK03/12/97_ AY-02A-U11-A JUMPER

Pointname

Loadcombination

*** Segment C begin

A14

C01

C01A

C02 N

C02 «

C02 F

C03

C04

C05 N

C05 M

C05 F

•

GRT1GR+TI

GRT1GR+T1

GRT1GR+T1

GRTlGR+T1

GRT1GR+T1

GRT1GR+T1

GRTlGR+T1

GRT1GR+T1

GRT1GR+T1a

GRnGR+T1GRT1GR+T1

D I S


P L A C

TRANSLATIONS (X

***

-0.0180.0240.006

•0.0190.0230.004

-0.0200.0220.001

-0.0220.019•0.003

-0.0230.016-0.007

-0.0200.014-0.006

-0.0200.014-0.006

-0.0160.012-0.004

-0.0130.011•0.002

-0.0110.009-0.002

-0.0100.006-0.004

Y

-0.1090.010-0.099

-0.1110.010-0.102

-0.1150.009-0.105

-0.1210.009-0.112

-0.1260.010-0.116

-0.1280.014-0.114

;0.1280.014-0.114

-0.1280.018•0.110

-0.1280.022-0.106

-0.1270.024-0.1O3

-0.1260.025-0.101

E H E N T S

n )Z

-0.041-0.016-0.056

•0.041-0.017 •-0.058

•0.041-0.020-0.060

-0.041-0.024-0.065

-0.043-0.028•0.071

-0.048-0.030-0.079

-0.048-0.031-0.079

-0.054-0.031-0.085

-0.058-0.032-0.089

-0.060-0.031-0.091

-0.060-0.030-0.090

FLUOR DANIEL NORTHWEST. INC.AutoPIPE+4.60 RESULT PAGE 7

ROTATIONS (deg )X

-0.099•0.010-0.108

-0.099-0.010•0.108

-0.099-0.010-0.108

-0.099-0.010-0.108

-0.095-0.010-0.105

-0.091•0.010-0.101

-0.091-0.010-0.101

-0.089-0.010-0.099

-0.085-0.010-0.095

-0.073-0.010-0.083

-0.068-0.010-0.077

Y

0.0340.0430.077

0.0340.0430.077

0.0340.0430.077

0.0340.0430.077

0.0340.043,0.078

0.0350.0430.079

0.0350.0430.079

0.0350.0430.079

0.0350.0430.079

0.0380.0430.082

0.0410.0430.085

Z

-0.0670.025-0.042

-0.0670.O25-0.042

•0.0670.025-0.O42

-0.0660.025•0.041

-0.0650.025-0.040

-0.0630.025-0.038

-0.0630.025-0.038

-0.0610.025-0.036

-0.0590.025-0.034

-0.052O.O25-0.027

-0.0470.025•0.022

Af02A1R2.0t/r 3-12-97 9:03a Page 11 oi 23

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PACE I



Pointname

C06

C06

C06

C07

...

A09

1

2

3

4

A12

5

6

N

M

F

Loadcombination

GRT1GR*T1

GRTlGR+T1

GRT1GR+T1

GRTlGR+T1

Segment C end

GRT1GR*T1

GRT1GR*T1

GRTlGR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR*T1

GRT1GR+T1

TRANSLATIONS (in )

x r z-0.0100.006•0.005

-0.0100.004-0.006

•0.0080.004-0.004

-0.0020.0110.009

-0.0180.005-0.013

-0.0050.002-0.003

-0.0050.002-0.003

-0.0050.002-0.003

-0.0050.002-0.003

-0.01B0.005•0.013

0.0090.0220.032

0.0160.0330.049

-0.1260.024-0.101

-0.1230.024-0.099

-0.1200.024-0.097

-0.113O.O25-0.088

-0.009-0.017-0.026

-0.009-0.017-0.026

-0.028-0.012-0.040

-0.071-0.001-0.072

-0.0880.003-0.085

-0.0880.003-0.085

-0.0430.003-0.040

-0.0210.005-0.016

•0.060-0.030•0.090

-0.058-0.027-0.085

-0.058-0.024-0.081

-0.058-O.013-0.070

•0.0090.0310.022

-0.0170.0300.013

•0.0220.0220.000

-0.0350.003-0.032

-0.040-0.005-0.045

-0.032-0.004-0.036

-0.0350.003-0.032

-0.0350.003-0.032

ROTATIONS (degX Y

-0.068-0.010-0.077

-0.062-0.010

. -0.071

-0.052-0.010-0.062

-0.048-0.010-0.058

-0.065-0.011-0.075

-0.064-0.011-0.075

-0.061-0.011-0.072

•0.055-0.011-0.065

-0.065-0.011-0.075

-0.065-0.011-0.075

-0.091-0.011•0.102

-0.108-0.012-0.120

0.0410.0430.085

0.0410.0430.085

0.0410.0430.085

0.0410.0430.085

0.0330.0490.082

0.0320.0490.082

0.0330.0490.082

0.0330.0490.083

0.0330.0490.083

0.0330.0490.082

0.0340.0490.083

0.0340.0490.083

)Z

-0.0470.025-0.022

-0.0420.025-0.017

-0.0390.025-0.014

-0.0390.025-0.014

-0.1110.028-0.083

-0.1110.028-0.083

-0.1160.028-0.087

-0.1060.028-0.078

-0.1080.028-0.080

-0.1110.028-0.083

-0.1120.028-0.084

-0.1140.028-0.086


Point Load TRANSLATIONS (in )name combination X Y 2


GRT1GR+T1

GRTlGR+T1

GRT1GR+T1

GRTlGR+T1

T1GR+T1

GRT1GR+T1

0.0160.0330.049

0.0160.0330.049

0.0090.0220.031

0.0050.0260.021

0.0050.0020.003

0.0040.0260.021

0.0000.0000.000

0.017-0.0050.011

0.000-0.008-0.008

0.000-0.008-0.008

-0.030-0.012-0.042

•0.0430.003 .-0.040

-0.0580.013-0.016

-0.0220.0220.000

•0.0220.0220.000

-0.0140.0230.009

-6.0220.0220.000

-0.0240.004-0.019

-0.097-0.011-0.108

-0.086-0.011-0.097

-0.067-0.011-0.078

-0.065-0.O11-0.075

-0.073-0.011•0.084

-0.091-0.011-0.102

0.0340.0490.083

0.0330.0490.083

0.0330.0490.083

0.0330.0490.082

0.0330.0490.083

0.0340.0490.083

-0.0990.028-0.070

-0.0830.029-0.055

-0.1100.028-0.082

-0.1110.028-0.083

-0.1100.028-0.082

-0.1120.028-0.084

AY02A1R2.OUT 3-12-97 9:03a Page 12 of 23

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING. FLUOR DANIEL HORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 10

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 11

Point/ Connect/ LoadSupp. ID Type Combina

S U P P 0

ion D im

downrghtforw

downleftforw

downrghtforw

downleftback

downrghtback

downleftback

down-Z

• +X

down+Z+X

down-Z•X

R T F

L 0 C AForce

26

1

26

47

1

48

146

2

147

0 R C E S

LDeform

0.0000.0130.008

0.0000.0030.001

0.0000.0100.009

0.0000.0140.008

0.0000.0030.001

0.0000.0100.009

0.0000.0280.016

0.0000.0130.033

0.0000.0160.049

GD i m

XYZ

XY2

XYZ

XYZ

XYZ

XYZ

XYZ

XY •2

XYZ

L 0 B AForce

-26

-1

-26

-47

-1

-48

-146

-2

-147

LDeform

-0.0130.0000.008

0.0030.0000.001

-0.0100.0000.009

-0.0140.0000.008

0.0030.0000.001

-0.0100.0000.009

0.0160.000

-0.028

0.0330.0000.013

0.0490.000

-0.016

R E S T R A I N T R E A C T I O N S


MOMENTS (ft-lb )Y Z Result

B01 9B01 1 GuideStiff :RIGID

B04 5804 1 GuideStiff :RIGID

7 1 Y - StopStiff :RIGID

03 to

AY02A1R2.OUT 3-12-97 9:03a

AnchorGRT1GR+T1

AnchorGRT1GR*T1

GuideGRT1GR*T1

GuideGRT1GR+T1

Y - StopGRT1GR+T1

19-82•63

-198263

000

000

000

-42433

-390

-531-32

-563

-26-1

-26

-47-1

-48

-146-2

-147

0-52- 5 ? '

05252

000

000

000

424102399

532102569

261

26

471

48

1462

147

191-8

183

-4211

-420

000

000

000

54-3420

23-20

3

000

000

000

-33-2

-35

-112-31

-142

000

000

000

20135

187

43636

443

000

000

000

Page 13 of 23




L O C A L

X

F O R C E S

FORCES ( I bY Z

M O M E N T S

MOMENTS (ft-lb )

L O C A L F O R C E S & M O M E N T S

Point Loadname' combination

FORCES (Ib )

Y 2 Result

MOMENTS (ft-lb >X Y Z Result

: Segment A begin '

) GRT1GR+T1

GRT1GR+T1

i GRT1GR+T1

, N GRT1GR+T1

, H GRT1GR+T1

1 F GRT1GR+T1

T1GR+T1

GRT1GR*T1

GRT1GR*T1

GRT1GR+T1

GRT1GR-JT1

05252

05252

05252

05252

19252

140

26722

245

25922

237

17852

126

05252

05252

05252

424-33390

282-33249

282-33249

•27622

-254

•192-21

-213

54-85-31

05252

17821

199

250-33217

243-33210

239-33205

19-82-63

19-82-63

' 19-82-63

•568530

•558530

0-52-52

53-85•32

52-85-33

19-82-63

19-82•63

19•82-63

424102 •399

283102262

283102262

282102261

277102256

273102252

264102244

258102238

251102231

244102225

239102221

332

35

332

35

332

35

332

35

531164

322961

322961

84-3846

102-108

•6

102-108

-6

102-108

-6

-5434

-20

-5014

-36

-485

•42

501

51

-11918

-66-4

-70

76-65

11

50-97-47

-31-77

-108

-24-107-131

-18-134-152

191-8

183

851

86

504

54

-25-6

-31

40-633

•5126

•25

•66•27•94

-103-43

-146

-189-32

-221

-280-20

-300

-360-9

-369

20135

187

10414

100

777

77

657

69

672374

903996

10677

112

142113160

217136246

299153328

374172399

GRT1GR<

GRT1GR<

GRT1

GRT1GR<

GRT1GR<

GRT1GR<

GRT1GR̂

GRT1GR-

GRT1GR-

GRT1GR-

GRT1GR-

GRT1GR-

•T1

•T1

•T1

-T1

HT1

»T1

»T1

HT1

H1

HT1

I-Tl

•-T1

05252

139481

198263

198263

498133

498133

489344

489344

528129

528129

198263

198263

-198263

-13218

232-33198

232-33198

132-3399

132-3399

201-32169

201-32169

203-31172

203-31172

-163-32

-194

-174-32

-206

239-33205

235-33202

05252

05252

25254

25254

04343

04343

15253

15253

• o5252

05252

239102221

236102218

232102214

232102214

141102117

141102117

207107180

207107180

210101182

210101182

164102211

175102221

102-108

-6

354-74280

449-4

446

449-4

446

451-4

447

451-4

447

213-6

207

213-6

207

256-9

247

256-9

247

256-9

247

256-9

247

3619

370

24674

319

-11-146-156

-11-145-156

-8-145-154

-7-105-112

-4-70-75

-495

-11-11-22

-102919

-102919

-107969

-18-134-152

-13-150-163

15-95-81

13•95-82

19-95-76

-83-69

-152

1-61-61

-367-3

-370

-365-10

-374

-52215

-507

-52515

-510

-36445

-318

376173400

431183455

450174479

450174479

451174479

458126485

21394

228

42411

424

44617

449

58134

564

58434

568

44591

409

AY02A1R2.OUT 3-12-97 9:03a Page 14 of 23

AY02A1R203/12/97

PROJECT U-320: TANK 241-CAY-02A-U11-A JUMPER HYDRO

I O C -


A13A

A14 •

A14 •

A15

A15A

A16 N

A16 M

A16 F

A17 N

A17 H

A17 F

A18 N

S"5 3IB too

GRT1GR*T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRTlGR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR+T1

GRT1GR*T1

GRT1GR+T1

GRT1GR+T1

A L F O R C

. FORCES (IbY

-198263

-198263

-198263

-198263

-198263

-198263

51' 2981

93-4052

93-4053

153-7182

134-6569

135-6569

•196-32-228

-198-32

-229

-283-32

-315

-285-32

-316

-307-32

-339

91-4050

78-86-8

-307-45

-353

122-6261

28-1910

-306-58

-364

05252

-106 SLUICINGSTATIC ANAL.

E S

)Z . Re

05252

05252

05252

05252

05252

-301-45-346

-304-45

-350

-198263

•286-70-357

-290-70-360

0-52-52

-307-58

-365

£ H O

suit

197102242

198102243

284102326

285102327

308102349

315102356

318102359

322102362

325102365

329102370

334102374

335102375


MEN T S

MOMENTS (ftX Y

256-9

247

256-9

247

238-9

229

238•9

229

238-9

229

238-9

229

157-9464

-82•134-216

•82-134-216

-335-155-490

-465-107•572

•465-107-572

-108777

-109382

-109382

-109888

-1010696

32-117-86

-226-89

-315

-42154112

-372-73-445

-28520

-265

-201184-17

-225028

Ib )Z

-33450

•284,

-31453

-261

-29453

-240

-26557

-209

-21862

-156

-1108107

-27128101

3528

361

-181154•28

-201164-37

-2-55-57

-201180•21

Result

421101384

405107369

378107342

357113322

323123294

240160267

277182337

364204435

422217496

484226558

506220575

507215573

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL.

L O C


A18 M GRT1GR+T1

A18 F GRT1GR+T1

A19 N GRT1GR+T1

A19 M GR• T 1

GR+T1

A19 F GRT1GR*T1

A20 GRT1GR+T1

A21 GRT1GR+T1

A22 GRTlGR+T1

*** Segment A end *

*** Segment B begin *

A10 GRT1GR+T1

B01 - GRT1GR+T1

801 + GRT1GR+T1

A L F 0 R C

FORCES (IbY

96-1087

05252

05252

27059

329

38732

418

52732

559

52732559

53132563

;;

2911

2911

1910

-9683•13

-344-32

-376

37732

409

270-14256

05252

05252

05252

05252

•69•2

-70

-69-2

-70

•45-1

-46

E S

)

311-58370

19-82-63

-198263

-198263

19-82-63

19-82-63

19-82-63

19-82-63

01212

01212

41216

& M O

Result

340102380-

344102384

378102417

383102422

387102426

527102565

527102565

532102569

691572

691572

451549


MEN T S

MOMENTS (ft-lb )X Y Z

-375-46

-421

-12631-95

-12631-95

-10225-78

•2320-3

•2320-3

-2320-3

-2320-3

-84-8

-91

-84-8

-91

-80-8

-87

24098

338

-19163143

-16-7

-24

73-865

-1194

-116

-118-2

-120

-116-10

-126

-112-31

-142

-2-35-38

-2-12-14

-2-12-14

-188161-26

-392-33

-425

-294-27

-321

-384-30

-413

42121

442

42117

438

42112

433

421-1

420

-238-2

-240

-1011

-99

-482

-46

Result

483194540

412169459

32042336

40439426

43829

457

43826

454

43725

451

43636

443

25336260

13114

136

9315100

AV02A1R2.OUT 3-12-97 9:03a Page 15 of 23


AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 17

P o i n tname

L O C A L F O R C E S

Load FORCES <lb )combination X Y Z Re:

M O M E N T S

MOMENTS < f t - l b )X Y 2 R e s u l t

L O C A L F O R C E S & M O M E N T S

P o i n t Loadname c o m b i n a t i o n

FORCES Clb )X Y 2 R e s u l t

MOMENTS ( f t - l b )X Y Z R e s u l t

B02 N GRT1GR*T1

B02 F GRT1GR+T1

803 N GRT1GR+T1

B03 F GRT1GR+T1

B04 - GRT1GR+T1

B04 + GRT1GR+T1

A11 GRT1GR*T1

*** Segment B end 1

*** Segment C begin 1

A H GRT1GR+T1

C01 GRT1GR+T1

GRT 1 -GR+T1

GRT1GR*T1

19

10

-4-12-16

-4-12-16

-1-9

-10

-1-9

-10

-1-9

-10

-1-9

-10

-4-12-16

-45-1

-46

-1-9

-10

•45• 1

• 4 6

• 4 5-1

• 4 6

203

203

-45• 1

-46

19

10

-45-1

-46

-4-12-16

-4-12-16

-4-12-16

-4-12-16

451549

451549

451549

451549

451549

51519

51519

-80-8

-87

17-314

17-314

-264

-264

-264

-264

39-237

212

207

27

178

045

045

-7-19-27

-1-10-11

-57-7

•65

38

11

39-237

48• 246

48-246

44-341

891395

608

66

261132

399

38

488

46

488

46

442049

000

000

000

000

810

81

800

80

570

57

540

54

000

000

000

000

810

81

800

80

570

57

540

54

210

21

210

21

210

21

210

21

000

000

000

000

180

18

100

10

-10

-1

•170

-17

270

27

230

23

210

21

270

27

GRT1GR+T1

GRT1GR*T1

GRT1GR+T1

GRT1GR*T1

GRT1GR*I1

GRT1GR*T1

GR

T1

> N GRT1GR+T1

. M GRT1GR+T1

i F GRT1GR*T1

GR'T1GR+T1 .

1 Segment C e n d

360

36

470

47

470

47

440

44

430

43

300

30

000

000

000

000

000

360

36

000

000

000

000

-300

-30

410

41

000

000

390

39

350

35

000

410

41 •

400

40

000

000

500

50

470

47

470

47

440

44

430

43

0 420 00 42

410

41

410

41

400

40

390

39

350

35

150

15

000

000

000

000

260

26

360

36

360

36

210

21

000

000

-150

-15

-210

-21

-210

-21

-210

-21

360

36

260

26

000

-100

-10

-250

-25

000

000

-310

-31

-360

-36

-360

-36

-360

-36

-210

-21

-170

-17

100

10-

000

000

260

26

000

370

37

420

42

420

42

420

42

420

42

400

40

370

37

370

37

330

33

260

26

000

AY02A1R2.OUT 3-12-97 9:03a Page 16 of 23

AY02A1R2 PROJECT U-320: TANK 241-C-106 SLUICING FlUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 18


FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.'60 RESULT PAGE 19

i E A M F O R C E S S M O M E N T S E A M F O R C E S & M O M E N T S

Beam Load PointID combi net i on name

FORCES (Ib )Axial Y-Shear Z-Shear

MOMENTS (ft-lb )Torsion Y-Y Mom. Z-Z Mom.

Beam Load PointID combi nat i on name

FORCES (Ib ) MOMENTS (ft-lb )Axial Y-Shear Z-Shear Torsion Y-Y Mom. 2-2 Mom.

GR

T1

GR+T1

GR

T1

GR+T1

GR

T1

GR+T1

GR

T1

GR*T1

GR

T1

GR*T1

GR

T1

GR+T1

GR

T1

GR+T1

A091A091A091

121212

232323

343434

4A124A124A12

353535

565656

6966006966

3030003030

3030003030

3434003434

8790008790

000000

000000

-303000

-3030

-2200-22

-2200-22

-1100-11

1-1001-1

4-4004-4

4-4004-4

-2200-22

•151100

-15•11

-11100

•111

32•360032•36

34-340034•34

-251400

•251536•411-137•42

220022

000000

000000

110011

000000

000000

000000

100010

11-10012-1

11000110

-10-1600

-10-16

-16-400

-16-4 '

13801139

-38-1-10

-39-1

-6-1100-6-12

2-4002-4

4-7004•7

-1000-10

100010

8-1008-1

130013

GR

T1

GR+T1

GR

T1

GR+T1

GR

T1

GR+Tl

GR

T1

GR+T1

GR

T1

GR+T1

GR

T1

GR+T1

676767

787878

898989

910910910

5E055B055B05

9B019B019B01

440044

440044

000000

000000

300030

220022

000000

000000

-4400-44

000000

000000

000000

41-461-142-47

-4843-11

-4944

-4338-11

-4439

-110

• o

0-110

000000

-4400-44

1-1001-1

1-1001-1

-2200-22

000000

000000

000000

0-400-10

•41

40210412

-14101-142

11000110

000000

-2 '400

•2

4

-3300

•3

3

-3400-34

-4000-40

000000

000000

•5253-11

-5353

AY02A1R2.OUT 3-12-97 9:03a Page 17 of 23

to to

£5

AY02A1R2 PROJECT « 320: TANK03/12/97 AY-02A-U11-A JUMPER

Pointname

Loadcombination

*•• Segment A begi

A00

A01

A03

A04 N-

A04 N+

A04 H

A04 F-

A04 F+

A05 N-

A05 N+

A05 M

Max PGR + Max PCold to T1




Max PGR * Max PCold to T1







ASME B31


FLUOR DANIELAutoPIPE

3c (1992) CODE COMPLIANCE(Moments in

In-Pl. Out-Pl.Moment Moment

., ***

1918

851

504

316

256

406

664

5126

7665

6627

10343

5434

5014

485

460

501

119

5126

664

6627

7665

5097

ft- Ib )TorsionMoment

2

2

2

2

2

11

29

29

29

29

38

S.IIn

1.001.00

1.001.00

1.001.00

1.001.00

2.562.56

2.562.56

2.562.56

1.001.00

1.001.00

1.951.95

1.951.95

.FOut

1.001.00

1.001.00

1.001.00

1.001.00

2.132.13

2.132.13

2.132.13

1.001.00

1.001.00

1.631.63

1.631.63

•4.60

(Stress

no.

(3a)(18)(17)

(3a)(18)(17)

(3a)<18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

Loadtype

HOOPSUSTDISP

HOOPSUSTOISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTOISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTOISP

NORTHWEST, INC.RESULT

in psiCodeStress

73044066130

7304358851

7304344726

7304338324

7304371259

73043602168

73044081238

73043516147

73043598286

73043973457

73044159681

PAGE 20

)CodeAllou.

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050


Pointname

A05 F-

A05 F+

A06

A07

A08 N-

A08 N*

A08 M

A08 F-

A08 F+

A09

A12

A13

Loadcombination













ASME B31


FLUOR DANIELAutoPIPE+4.60



19142

18932

28020

3609

3619

18134

13150

1 1 •

146

1595

1395

52515

36445

672

3177

24107

18134

18134

3619

24674

1595

11146

11145

1029

1079

ft-lb )TorsionMoment

108

108

108

108

108

108

74

4

4

4

9

9

S.IIn

1.951.95

1.001.00

1.001.00

1.001.00

1.001.00

1.781.78

1.781.78

1.781.78

1.001.00

1.001.00

1.001.00

1.001.00

.FOut

1.631.63

1.001.00

1.001.00

1.001.00

1.001.00

1.481.48

1.481.48

1.481.48

1.001.00

1.001.00

1.001.00

1.001.00

(StressEq-no.

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

<3a>(18)(17)

<3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

Loadtype

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

NORTHUEST, INC.RESULT

in psiCodeStress

73044908669

73044033509

73044464573

645160431199

645160541202

645176451827

645160812074

645130102052

645129131212

645129041210

64517553236

64516076636

PAGE 21

)Code

Allow.

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

AY02A1R2.0UT 3-12-97 9:03a Page 18 of 23

CO t o


Pointname

A13A

A14 -

A14 +

A15

A15A

A16 N-

A16 N+

A16 M

A16 F-

A16 F+

A17 N-

A17 N+

Loadcombination













241-C-106 SLUICIN(HYDRO STATIC ANAL

FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60 RESULT PAGE 22

ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-lb ) (Stress

In-Pl. Out-PL Torsion S.I.F Eq. LoadMoment Moment Moment In Out no. type

33450

1093

1093

26557

21862

3081

1108

27128

42154

3528

41117

181154

1087

31453

29453

1098

10106

10137

32117

22689

3528

42154

46170

37273

AY02A1R2.

1.009 1.00

1.229 1.22

1-.229 1.22

1.009 1.00

1.009 1.00

1.009 1.00

1.789 1.78

1.7894 1.78

1.78134 1.78

1.00134 1.00

1.00134 1.00

2.56134 2.56

3UT 3-12-97

1.001.00

1.301.30

1.301.30

1.001.00

1.001.00

1.001.00

1.481.48

1.481.48

1.481.48

1.001.00

1.001.00

2.132.13

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

!3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

9:03a

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTOISP

HOOPSUSTOISP

HOOPSUSTDISP

HOOPSUSTDISP

i n ps iCodeStress

64515805704

64516476925

64516232925

64515177788

64514744856

645130371111

645131761803

645158431940

645175692122

73044818763

73045101809

730475241658

CodeAllow.

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050


Pointname

A17 M

A17 F-

A17 F+

A18 N-

A18 N+

A18 M

A18 F-

A18 F*

A19 N-

A19 N+

A19 M

A19 F-

Loadcombination



Max PGR * Max PCold to-T1










241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 23

ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-lb ) (Stress

In-Pl. Out-PL Torsion S.I.F Eq. LoadMoment Moment Moment In Out no. type

201164

194162

255

2250

201180

188161

155141

39233

29427

29427

38430

42121

28520

52103

201184

201180

2250

24098

36188

19163

167

167

738

1194

Pa

155

107

107

107

107

46

31

31

31

31

25

20

ie 19 of

2.56 2.132.56 2.13

2.56 2.132.56 2.13

1.00 1.001.00 1.00

1.00 1.001.00 1.00

2.56 2.132.56 2.13

2.56 2.132.56 2.13

2.56 2.132.56 2.13

1.00 1.001.00 1.00

1.00 1.001.00 1.00

2.56 2.132.56 2.13

2.56 2.132.56 2.13

2.56 2.132.56 2.13

23

<3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

(3a)(18)(17)

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

in psiCodeStress

730469351678

730455541797

73044078821

73044084804

730455901808

730464821733

7304•72701520

73045000630

73044528156

73046729291

73047883305

73048426213

CodeAllow.

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

AY02A1R2 PROJECT W-320: TANK03/12/97 AY-02A-U1


A19 F+ Max PGR * Max PCold to T1

A20 Max PGR + Max PCold to Tt

A21 Max PGR + Max PCold to T1


*** Segment A end

-A JUMPER

ASME B31



3c (1992) .CODE COMPLIANCE(Moments in


42121

42117

42112

4211

•**

*** Segment B begin ***

*** Segment 8 end

*** Segment c begi


C01 Max PGR + Max PCold to T1

C01A Max PGR • Max PCold to Tl

C02 N- Max PGR * Max PCold to T1

C02 N+ Max PGR • Max PCold to T1

C02 M Max PGR + Max PCold to T1

•**

00

100

10

170

170

310

1194

1182

11610

11231

180

00

00

00

00

150

ft-lb )Torsion S.Moment In

1.0020 1.00

1.0020 1.00

1.0020 1.00

1.0020 1.00

1.220 1.22

1.000 1.00

1.000 1.00

1.000 1.00

1.780 1.78

1.780 1.78

(Stress.F Eq.Out no.

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.30 (18)1.30 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.48 (18)1.48 (17)

(3a)1.48 (18)1.48 (17)

Loadtype

HOOPSUSTOISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP


in psiCodestress

73045215108

7304521399

7304521195

73045205136

64512952

0

64512839

0

64512758

0

64512903

0

64513022

0

64513285

0

PAGE 24

)CodeAllow.

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER HYDRO

Pointname

C02 F-

C02 F+

C03

C04

C05 N-

C05 N+

C05 M

C05 F-

C05 F+

C06 N-

C06 N*

C06 M

Loadcombination





Max PGR + Max PCold to Tl








STATIC ANALFLUOR DANIELAutoPIPE+4.60


In-Pl.Moment

360

360

360

360

360

210

170

100

100

100

00

00

Out-Pl.Moment

210

210

210

210

210

360

260

00

00

00

100

250


0

0

0

0

0

0

0

0

0

0

0

0

S.In

1.781.78

1.001.00

1.001.00

1.001.00

1.001.00

1.731.73

1.731.73

1.731.73

1.001.00

1.001.00

1.731.73

1.731.73

(Stress.F Eq.Out no.

(3a)1.48 (18)1.48 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

<3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.44 (18)1.44 (17)

(3a)1.44 (18)1.44 (17)

(3a)1.44 (18)1.44 (17)

<3a)1.00 (18)1.00 (17)

(3a)1.00 (18)1.00 (17)

(3a)1.44 (18)1.44 (17)

(3a)1.44 (18)1.44 (17)

Loadtype

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

HOOPSUSTDISP

NORTHWEST. INC.RESULT

in psiCodeStress

64513398

0

64513129

0

64513129

0

75624444

0

75624444

• 0

75625145

0

75624643

0

75623664

0

75623424

0

75623421

0

75623572

0

75624287

0

PAGE 25

)CodeAllow.

1670016700 •25050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

167001670025050

AY02A1R2.OUT 3-12-97 9:03a Page 20 of 23

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE*4.60 RESULT PAGE 26


FLUOR DANIEL NORTHWEST, INC.AutoPIPE*4.60 RESULT PAGE 27

ASHE B31.3C (1992) CODE COMPLIANCE(Moments in ft-tb ) (Stress in psi )


S Y S T E M S U M M A R Y

C06 F- Max PGR + Max PCold to T1

C06 F+ Max PGR * Max PCold to T1

C07 Max PGR + Max PCold to T1

*** Segment C end

00

260

00

260

00

00

(3a) HOOP 7562 167001.73 1.44 (18) SUST 4324 16700

0 1.73 1.44 (17) OISP 0 25050

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP

7562 167003947 16700

0 25050

(3a) HOOP 7562 167001.00 1.00 (18) SUST 3095 16700

0 1.00 1.00 (17) DISP 0 25050

Maximum displacements (in)

Maximum X : 0.049 PointMaximum Y : -0.150 PointMaximum Z : -0.091 PointMax. total: 0.160 Point

Maximum rotations (deg)

Maximum X : -0.282 PointMaximum Y : 0.085 PointMaximum 2 : -0.126 PointMax. total: 0.291 Point


Maximum X : -82 PointMaximum Y : -563 PointMaximum Z : 52 PointMax. total: 569 Point

Maximum restraint moments(ft-lb)

Maximum X : -421 PointMaximum Y : 54 PointMaximum Z : -142 PointMax. total: 443 Point

A17 FC05 MA17 F

A19 NC05 FA0S UA19 N

A00A22A22A22

A22A00A22A22

Load Comb.Load Comb.Load Comb.Load Comb.




GR+T1GRGR+T1GR+T1

GR+T1GR+T1GRGR+T1

T1GR+T1GR+T1GR+T1

GRGRGR+T1GR+T1

Ar02A1R2.OUT 3-12-97 9:03a Pase 21 of 23

AY02A1R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AV-02A-U11-A JUMPER HYDRO STATIC ANAL. AutoPIPE+4.60 RESULT PAGE 2:



Maximum pipe forces (Ib)

Maximum XMaximum YMaximum ZMax. total

flaximum pipe moment


563424-370569

5 (ft-lb)

-572-445-525584



A22A00A18 MA22

A17 FA17 NA12A12



GR+T1GRGR+T1GR*T1

GR+T1GR+T1GRGR



PointStress psiAllouable psiRatioLoad combination


Maximum hoop stress

PointStress psiAllouable psiRatioLoad combination





PointStress psiAllowable psiRatioLoad combinati-on



A19 F8426167000.50GR + Max P

A16 F2122250500.08Cold to T1

C047562167000.45Max P

A19 F8426167000.50GR + Max P

A16 F2122250500.08Cold to T1

C047562167000.45Max P

AY02A1R2.OUT 3-12-97 9:03a Page 22 of 23

AY02A1R203/12/97

PROJECT U-320: TANK 241-C-106 SLUICINGAY-02A-U11-A JUMPER HYDRO STATIC ANAL.



* * * The system satisfies ASME B31.3 code requirements * '* * * for the seLected options ' * '

AY02A1R2.0UT 3-12-97 9:03a Page 23 of 23


POINTNAME TYPE

*** SEGMENTA00A01

A03A04

A05

A06A07

V M A08

? ̂CD to

^ 5ff A10< A11o A12

A13

A13AA14A15

A15AA16

A16 FA17

RunFlex

RunBend

Bend

ReduRunBend

RunTeeTeeRunValv

RunTeeValv

RunBend

FarBend

P 0 I

OFFSETSX Y

A00

00

-0.17 -1.

000

0.380.771.830.770.96

0.160.100.10

0.160.98

0 -0

N T

(ft )

00

00

28

000

00000

000

00

25

241-c -106 SLUICING FLUOR DANIEL NORTHUEST, INC.DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 3

D A

Z

00.25

0.100.40

0

0.870.330.38

00000

000

00

-0.83

AY02A2R2.

T A L I S T I N G

PIPE ID DESCRIPTION

4"PIPEUt= 137 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID • Bend= 2080.02-Shear= RIGID Bend= 2080.0



3"PIPELong Elbow, Radius = 4.50 inchBend angle change = 90.00 degMid point at 50.00 percentSIF - In 1.78, Out = 1.48Flex = 4.577

RIGID

3"PIPERating = 300, Weight = 22 IbSurface factor = 4.40, SIF = 1.00



4"PIPEShort Elbow, Radius = 4.00 inch

OUT 3-12-97 9:53a

AY02A2R2 PROJECT U-320 TANK03/12/97 AY-02A-U11-A JUMPER

POINTNAME

A18

A19

A20

A21A22

***A10B01802

803

B04A11

***A14C01

C01AC02

TYPE

Bend

Bend

Flex

RunRun

EGMENTTeeRunBend

Bend

RunT£e

SEGMENTTeeValv

RunBend

P 0

OFFSETS.X Y

N T

(ft )

-0.67 -0.25

0

0 -0

0 -00 -0

80.98 -1

00

1.83

00

C4.80 -1

0

00

0

40

1025

2800

0

00

280

00

241-C -106 SLUICING FLUOR DANIEL NORTHWEST. INC.DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 4

D A

2

0

2.57

0

00

2.332.000.71

0

-0.71-2.00

2.33-0.10

-0.16-0.66

T A L I S T I N G

PIPE ID DESCRIPTION




Wt= 139 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID Bend= 2080.0Z-Shear= RIGID 8end= 2080.0

RIGID

Elbow, Radius = 6.00 inchBend angle change = 90.00 degSIF - In 1.00, out = 1.00Flex = 1.000

Elbow, Radius = 6.00 inchBend angle change = 90.00 degSIF - In 1.00, Out = 1.00Flex = 1.000

3"PIPERating = 300, Ueight = 22 IbSurface factor = 4.40, SIF = 1.00

Long Elbow, Radius = 4.50 inchBend angle change = 90.00 deg

Pane 2 of 26


POINTNAME

C03C04COS

C06

C07

TYPE

ReduRunBend

Bend

Run

P O I N T

OFFSETS (ft )X Y

0 0.380 0.290 0.48

•0.50 . 0

0 0

Total weight of empty pipes

S3 EiJ

§ 4jBJ li>1 .£.

<o

241-C-106 SLUICINGDYNAMIC ANALYSIS

D A T A

2 PIPE

0

L I S T

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 HODEL PAGE 5

ING

ID DESCRIPTION

Hid point at 50.00 percentSIFFlex

0 2"-PIPE0

0

0.96

: 132 Ib

AY02A2R2.OUT

LongBend

In 1.78, Out = 1.48= 4.577

Elbow, Radius = 3.00 inchangle change = 90.00 deg

Mid point at 50.00 percentSIFFlex

LongBend

In 1.73, Out = 1.44= 4.404

Elbow, Radius = 3.00 inchangle change = 90.00 deg

Hid point at 50.00 percentSIFFlex

3-12-97

In 1.73, Out = 1.44= 4.404

9:53a

AY02A2R203/12/97

POINT •NAME

*•»A00

A01A03A04A04A04A04A05A05A05A05A06A07A08A08A08A08A09

A10

A11

A12

A13

PROJECT W-320AY-02A-U11-A

COM

•-COOROINATECftX

SEGHEN

N

MFN

HF

H

HF

A13AA14

A15A15AA16A16A16A16A17A17A17A17A18A18A18

N

HFN

HFN

H

0

0000

A00

00000000

-0.01-0.04-0-0-0-0-0-0-0-0-0

101715171717171706

0.210

0

2

3

444

4556

21

98

81

58

547080

90066604

5.936.046.04655

04.96.76

5.685.375.46

Y

0.00

0.000.000.000.00-0.10-0.33-0.78.28.13.28.28.28.28.28.28

-1.28-1.28

-1.28

-1.28

-1.28

.28

.28

.28

.28

.28

.28

.28

.31-1.39-1.44-1.53-1.54-1.64-1.66-1.78-1.75

: TANKJUMPER

P O

j

2

H E

0.00

00000000011112

.25

.35

.42

.75

.65

.75

.75

.75

.90

.25

.62

.95

.95

.332.2222

2

2

2

222

2222

.33

.33

.33

.33

.33

.33

.33

.33

.33

.33

.33

.332.2211111111

.97

.79

.50

.58

.50

.50

.50

.60

241-C-106 SLUICINGDYNAHIC

N T

DATATYPE

ANCHOR

TI

TI

TI

FLANGE

FLANGE

TEE

TEE

ANALYSIS

D A T A LI

DESCRIPTION

Rigid

FLUOR DANIEL NORTHWEST, INC.tutoP!PE*4.60 HOOEL PAGE 6

S T I N C

Thermal movements : None

Weld neckRating = 300,Weld neckRating = 300,B16.9 weldingSIF - In = 1.B16.9 weldingSIF - In = 1.

FLANGE Weld neck

FLANGE

TEE

WEIGHT

TI

TI

TI

Rating = 300,Weld neckRating = 300,

816.9 weldingSIF - In = 1.5 Ib , No

Paae 3 of 26

SIFWeight =

SIFWeight =tee

00, Out =tee

00, Out =SIF

Weight =SIF

Weight =

tee22, Out =offsets

= 1.0015 Ib= 1.0015 Ib

1.00

1.00= 1.00138 Ib= 1.00138 Ib

1.30

AY02A2R203/12/97

POINT -NAME

A18 FA19 NA19A19 MA19 FA20A21A22

PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 7

C 0 M P

-COORDINATEDX

5.375.375.375.375.375.375.375.37

*** SEGMENT BA10

B01

B02 N802B02 FB03 NB03B03 F804

A11

0.98

0.98

0.980.981.482.312.812.812.81

2.81

*** SEGMENT CA14

C01C01AC02 NC02C02 HC02 FCO3C04C05 NCO5C05 MC05 F

4.80

4.804.804.804.804.804.804.804.804.804.804.734.55

Y

-1.78-1.78•1.78-1.88-2.11-2.18-2.28-2.53

-1.28

-1.28

-1.28-1.28-1.28-1.28-1.28-1.28-1.28

-1.28

-1.28

•1.28-1.28-1.28-1.28-1.17-0.90-0.90-0.61-0.38-0.13-0.20•0.13

0 N E N T

)--- DATA2 TYPE

1.833.744.07 TI3.974.074.074.074.07 ANCHOR

2.33 TEE

4.33 GUIDE

4.545.04 TI5.045.045.04 TI4.544.33 GUIDE

2.33 TEE

2.33 TEE

2.232.071.781.41 TI1.521.411.411.411.411.41 TI1.411.41


DESCRIPTION


B16.9 welding teeSIF - In = 1.00, Out = 1.00ID : B01 1, Connected to 9Stiffness = RIGIDGap-down = 0.00, Above = 0.06Gap-left = 0.06, Right = 0.06Friction = 0.30Gaps set Weightless

ID : B04 1, Connected to 5Stiffness = RIGIDGap-down = 0.00, Above = 0.06Gap-left = 0.06, Right = 0.06Friction = 0.30Gaps set WeightlessB16.9 welding teeSIF - In = 1.00, Out = 1.00

816.9 welding teeSIF - In = 1.22, Out = 1.30

AY02A2R2.0UT 3-12-97 9:53a

inchinch

inchinch

AY02A2R203/12/97

POINT -NAME

C06 NC06C06 HC06 FC07

PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST. INC.AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 8

C O M P

-COORDINATEDX Y

4.55 -0.134.30 -0.134.37 -0.134.30 -0.134.30 -0.13

Number of points in the

O N E N T D A T A L I S T I N G

)--- DATAZ TYPE DESCRIPTION

1.411.41 TI1.481.662.37 WEIGHT 35 Ib , No offsets

system : 73

Paae 4 of 26

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 9



Pipe 10/ Mom/ 0.0. Thickness(inch) Spec Ueight<lb/ft )Material Sch inch U.Th. CorrMUl Insu Ling Grav Pipe Other Total

4"PIPE 4 4.500 0.237 0.06 0.03 0A312-TP304L STD

3"PIPE 3.000 3.500 0.216 0.06 0.03 0A312-TP304L STO

2"-PIPE 2.000 2.375 0.154 0.06 0.02A312-TP304L STD

0 1.20 11.04 0 17.66

0 1.20 7.75 0 11.60

0 0 1.20 3.74 0 5.48



A312-TP304L 4"PIPE

A312-TP304L 3"PIPE

A312-TP304I 2"-PIPE

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

501.0 0.30 40.0 28.42 16700.0180.0 1.5442 16700.0

AY02A2R2.OUT 3-12-97 9:53a Page 5 of 26




POINT ---COORDINATECft )--- DATANAME X Y 2 TYPE DESCRIPTION

BEAM DATA LISTING

BEAKID

M1

M2

M3

M4

M5

M6

M7

M8

M9

M10

M11

M12

M13

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

POINTNAME

A091

12

23

34

4A12

35

.56

67

78

89

910

5B05

9B01

LENGTH(ft )

0.58

0.77

1.83

0.77

0.58

2.00

1.00

0.92

. 0.91

1.00

2.00

0.58

0.58

SECTION 10/MATERIAL ID

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

C4X5.4A36

BETAANGLE

0.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

90.00

RIGIDEND(ft)

0.00O.OO

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

RELEASEAx Y-Y Z-Z

NN

NN

NN

NN

NN

NN

NN

NN

NN

11N

NN

NN

NN

NN

NH

NN

NN

NN

NN

NII

NN

NN

NN

IIN

NN

NN

NN

NN

NN

NN

NN

NN

NN

II11

NN

1!N

NN

NN

NII

A091234A1256789B0110BOS

0.210.210.982.813.583.582.812.811.890.980.980.980.982.81

-1.28-0.70-0.70-0.70-0.70•1.28-0.70-0.70-0.70-0.70-0.70-1.28-0.70-1.28

2.332.332.332.332.332.334.335.335.335.334.334.332.334.33

UEIGHT

UEIGHTUEIGHT

WEIGHT

51

851

51

Ib

IbIb

Ib

, Ho offsets

, No offsets, No offsets

, No offsets

td to

AS

AY02A2R2.0UT 3-12-97 9:53a Page 6 of 26

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-O2A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 13

AY02A2R203/12/97

PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 MODEL PAGE 14

CROSS SECTION LISTING BEAM MATERIAL LISTING

Section ID Area(sq.in )ID Axial Y-Shear Z-Shear

Inertia (in**4 )Torsion Y-Y Bend Z-Z Bend

C4X5.4MATERIAL ID

A36

Elasticmodulus PoissonsE6 psi ratio

YieldStresspsi

DensityIb/cu.ft

UltimateExpansion stressE-6 /F psi

490.00 6.50000

AY02A2R2.OUT 3-12-97 9:53a Page 7 of 26

AY02A2R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE*4.60 MODEL PAGE 15

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 1



***A00A07A09A12A16A22

***A10A11

•«•A14C04C07

SEGMENT A325325325325

F 325325

SEGMENT B325325

SEGMENT C325325325

1S0180180180180180

180180

180180180

1.5441.5440.0001.5441.5441.544

0.0000.000

1.5441.5441.544



Modal - Date and Time of analysis Mar 12, 1997 9:52 AMModel Revision Number 2Number of modes 7Cutoff frequency (Hz) ..'. 33,0Weight of contents included Yes'Pressure stiffening case 0Water elevation for buoyancy loads Not considered

Response - Date and Time of analysis Mar 12, 1997 9:53 AMModel Revision Number ; 2Number of load cases •.. 3Load cases analyzed R1 R2 R3Date and time of modal analysis Mar 12, 1997 9:52 AMNumber of modes , 7Cutoff frequency (Hz) 33.0Model revision of modal analysis 2Weight of contents included YesPressure stiffening case 0

1 Water elevation for buoyancy loads Not considered

AY02A2R2.0UT 3-12-97 9:53a Page S of 26




Combination Category Method Load Factor A.l Iowabte Remarks

Sus. + R1 Occasion Abs sum Response 1 1.00 Automatic Default-Max Sus 1.00

Sus. + R2 Occasion Abs sum Response 2 1.00 Automatic DefaultMax Sus 1.00




R1

R2

R3

RESPONSE

Sum

Sum

Sum

SRSS

Response 1 1.00 Default



Response 1 1.00 User

Response 2 1.00Response 3 1.00

CODE COMPLIANCE

Y - Factor 0.40Weld efficiency factor 1.00Range reduction factor 1.00Design Pressure Factor 1.00Minimum stress ratio used in reports 0.00Include corrosion in stress calcs YInclude torsion in code stress NInclude axial force in code stress .... NLongitudinal pressure calculation PD/4tInclude rigorous pressure Not analyzed



Load case 1 - R1

Missing mass : Yes2PA : No


X- Spectrum : SCIMultiplier : 1.00

SCI

Freq(Hz) Grav( ) Freq(Hz) Grav( ) Freq(Hz) Grav<

0.1000.4001.640

20.000

0.010.100.420.26

0.1600.6008.000

33.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20

AY02A2R2.0UT 3-12-97 9:53a

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE .4


Missing mass : YesZPA : No


Y- Spectrum : SC1Multiplier : 1.00

FreqCHz) Grav( ) Freq(Hz) Grav( ) FreqCHz) Grav(

0.1000.4001.640

20.000

0.01 0.1600.10 0.6000.42 8.0000.26 33.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20



2- Spectrum : SC1Multiplier : 1.00

Freq(Hz) Grav( ) FreqCHz) Grave ) FreqCHz) Grave

0.1000.4001.640

20.000

0.010.100.420.26

0.1600.6008.00033.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20

AY02A2R2.OUT 3-12-97 9:53a Page 10 of 26

AY02A2R203/12/97

ModeNumber

1

2

3

4

5

6

7

p ZB '

00 0)

3o

PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 6

F R i

Frequency<Rads/sec)

48.5389

54.6772

68.3506

133.5456

171.4149

178.9405

202.7504

Q U E N C

Frequency(Hertz)

7.7252

8.7021

10.8783

21.2544

27.2815

28.4793

32.2687

E S

Period(Sec)

0.129

0.115

0.092

0.047

0.037

0.035

0.031

AY02A2R2.OUT

Participation factorsX Y

0.484 1.076

1.292 -0.231

0.340 -0.688

0.033 0.301

0.027 -0.092

-0.041 0.068

0.026 -0.300

3-12-97 9:53a

Z

0.195

0.123

-0.621

-1.046

0.352

0.088

0.323

AY02A2R2 PROJECT W-320: TANK03/12/97 AY-02A-U11-A

Pointname

Loadcombination

*** Segment A begin *

A00

A01

A03

A04 N

A04 M

A04 F

A05 N

A05 M

A05 F

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2 'R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

JUMPER

D I S

241-C-106 SLUICINGDYNAMIC

P L A C

TRANSLATIONS (X

.

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0010.0000.0000.001

0.0020.0010.0000.002

0.0060.0030.0010.007

0.0120.0040.0010.013

0.0200.0050.0020.021

0.0280.0070.0030.029

0.0350.0100.0040.036

Y

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0010.0000.001

0.0010.0020.0000.002

0.0040.0060.0010.007

0.0050.0080.0020.010

0.0060.0080.0020.010

0.0080.0110.0030.014

0.0130.0200.0040.024

Page

ANALYSIS

E M E N T S

n )Z

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0010.0020.0000.002

0.0030.0070.0020.008

0.0080.0170.0040.019

0.0130.0250.0060.029

0.0150.0290.0060.033

11 of 26

nFLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 RESULT PAGE 7

ROTATIONS (desX

0.0000.0000.0000.000

0.0010.0020.0000.002

0.0430.0790.0180.091

0.0430.0790.0180.092

0.0490.0910.0200.105

0.0550.1020.0230.118

0.0570.1040.0230.120

0.0630.1120.0240.130

0.0690.1180.0250.139

Y

0.0000.0000.0000.000

0.0020.0010.0000.002

0.0580.0350.0140.069

0.0580.0350.0140.069

0.0640.0390.0150.076

0.0640.0410.0160.078

0.0650.0420.0160.079

0.0620.0420.0160.077

0.0550.0420.0160.071

)z

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0860.0210.0150.090

0.0870.0210.0150.090

0.0880.0210.0150.092

0.0880.0210.0150.092

0.0870.0210.0150.091

0.0760.0210.0160.081

0.0700.0210.0170.075

AY02A2R2 PROJECT U-320: TANK03/12/97 AV-02A-U11-A JUMPER

Pointname

A06

A07

A08 N

A08 H

A08 F

A09

A10

A11

A12

A13

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

D I S


P L A C E H E N T S

TRANSLATIONS ( i n )X Y Z

0.0390.0130.0040.041

0.0420.0150.0050.045

0.0420.0150.0050.045

0.0440.0170.0050.048

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0180.0290.0060.035

0.0230.0370.0080.045

0.0230.0380.0080.045

0.0270.0440.0090.052

0.0270.0460.0090.054

0.0270.0460.0090.054

0.0240.0430.0080.049

0.0170.0360.0090.041

0.0160.0340.0110.039

0.0140.0300.0140.036

AY02A2R2.OU1

0.0150.0290.0060.033

0.0150.0290.0060.033

0.0150.0290.0060.033

0.0150.0280.0060.032

0.0140.0270.0060.031

0.0140.0270.0060.031

0.0120.0230.0050.026

0.0070.0150.0060.017

0.0060.0120.0070.015

0.0070.0100.0070.014

3-12-97 !


ROTATIONS (decX Y

0.0700.1190.0250.140

0.0700.1190.0260.141

0.0700.1190.0260.141

0.0780.1190.0290.146

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0740.0990.0330.128

:53a

0.0540.0410.0160.070

0.0510.0410.0150.067

0.0510.0410.0150.067

0.0240.0330.0130.043

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0280.0210.0090.036

)Z

0.0660.0210.0170.071

0.0600.0220.0180.067

0.0600.0220.0180.067

0.0480.0220.0180.055

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.027-0.0180.041

0.0250.0270.0180.041

0.0250.0380.0180.049


Pointname

A13A

A14

A15

A15A

A16 N

A16 M

A16 F

A17 N

A17 M

A17 F

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

• TANKJUMPER

0 I S


P L A C

TRANSLATIONS (X Y

0.0450 .0180.0060 .049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.049

0.0450.0180.0060.048

0.0460.0170.0050.049

0.0490.0170.0060.052

0.0510.0170.0060.054

0.0540.0160.0060.056

0.0550.0160.0060.058

0.0140.0300.0140.036

0.0140.0290.0140.035

0.0140.0290.0150.035

0.0140.0280.0150.035

0.0140.0260.0170.034

0.014O.0250.0180.034

0.0160.0250.0200.036

0.0170.0260.0210.037

0.0180.0270.0230.039

0.0180.0270.0230.040

Page

E H E N T S

n )Z

0.0080.0090.0070.014

0.0080.0090.0070.014

0.0090.0090.0070.015

0.0100.0090.0070.015

0.0130.0090.0080.018

0.0150.0090.0080.019

0.0160.0080.0070.019

0.0150.0080.0070.018

0.0130.0070.0060.016

0.0100.0060.0050.013

12 of 26


ROTATIONS (desX Y

0.0740.0990.0330.128

0.0720.0970.0340.126

0.0710.0950.0340.124

0.0710.0950.0340.124

0.0640.0840.0340.111

0.057•0.0750.0350.100

0.0440.0570.0360.080

0.0430.0560.0360.079

0.0380.0480.0380.072

0.0390.0450.0390.071

0.0280.0210.0090.036

0.0290.0200.0090.037

0.0300.0200.0100.037

0.0300.0200.0100.037

0.0360.0180.0100.041

0.0480.0160.0090.052

0.0610.0150.0070.063

0.0620.0150.0070.064

0.0690.0130.0080.071

0.0770.0170.0090.079

)2

0.0250.0380.0180.049

0.0250.0390.0170.049

0.0250.0390.0170.050

0.0250.0390.0170.050

0.0230.0400.0170.049

0.0160.0310.0160.038

0.0120.0240.0170.031

0.0110.0230.0170.031

0.0120.0240.0160.031

0.0120.0230.0150.030

AY02A2R2 PROJECT W-320: TANK03/12/97 AY-02A-U11-A

Pointname

A13 N

A18 M

A18 F

A19 N

A19 M

A19 F

A20

A21

A22

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

* * * Segment A end

* * * Segment B begin

JUMPER

D I S


P L A C E

TRANSLATIONS ( i nX

0.0550.0160.0060.058

0.0530.0160.0060.056

0.0490.0140.0050.051

0.0080.0030.0010.008

0.0030.0010.0010.003

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

***

Y

0.0180.0270.0220.039

0.0170.0250.0210.037

0.0160.0230.0190.034

0.0020.0030.0030.005

0.0010.0010.0010.001

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

0.0000.0000.0000.000

I E 1 I S

)z

0.0080.0060.0050.011

0.0040.0050.0040.007

0.0030.0040.0030.006

0.0030.0040.0030.006

0.0020.0030.0020.004

0.0010.0010.0010.001

0.0000.0000.0000.001

0.0000.0000.0000.000

0.0000.0000.0000.000


ROTATIONS (desX

0.0380.0450.0390.071

0.0380.0440.0390.070

0.0350.0470.0400.071

0.0320.0500.0400.072

0.0290.0460.0360.065

0.0250.0400.0320.057

0.0250.0400.0320.057

0.0010.0010.0010.001

0.0000.0000.0000.000

Y

0.0770.0170.0090.079

0.0870.0230.0100.091

0.0990.0280.0110.103

0.1040.0300.0110.109

0.1030.0300.0110.108

0.1030.0300.0110.107

0.1020.0300.0110.107

0.0000.0000.0000.000

0.0000.0000.0000.000

)z

0.0120.0230.0150.030

0.0090.0190.0150.026

0.0090.0170.0150.024

0.0090.0150.0130.022

0.0090.0140.0130.021

0.0090.0130.0110.019

0.0090.0130.0110.019

0.0000.0000.0000.000

0.0000.0000.0000.000



A10 R1R2R3RESPONSE

601 R1R2R3RESPONSE

B02 N R1R2R3RESPONSE

B02 F R1R2R3RESPONSE



B04 R1R2R3RESPONSE

A11 R1R2R3RESPONSE

* * * Segment B end

* * * Segment c b e g i n

A14 R1R2R3RESPONSE

D I S


P L A C E

TRANSLATIONS ( i nX

0.0450.0180.0060.049

0.0410.0270.0080.050

0.0400.0280.0090.050

0.0390.0310.0100.051

0.0390.0310.0100.051

0.0400.0280.0090.050

0.0410.0270.0080.050

0.0450.0180.0060.049

* • *

* * *

0.0450.0180.0060.049

Y

0.0240.0430.0080.049

0.0580.0910.0200.110

0.0620.0970.0210.117

0.0680.1070.0230.129

0.0640.1030.0210.123

0.0530.0890.0170.105

0.0500.0840.0160.099

0.0170.0360.0090.041

0.0140.0290.0140.035

I E 1 I S

)2

0.0120.0230.0050.026

0.0120.0230.0050.026

0.0120.0230.0050.026

0.0100.0210.0050.023

0.0080.0170.0050.019

0.0070.0150.0060.017

0.0070.0150.0060.017

0.0070.015 .0.0060.017

0.0080.0090.0070.014


ROTATIONS (decX

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0840.1180.0320.148

0.0720.0970.0340.126

Y

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0170.0260.0100.032

0.0290.0200.0090.037

)Z

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0270.0180.041

0.0250.0390.0170.049

AY02A2R2.OUT 3-12-97 9:53a Page 13 of 26

AY02A2R203/12/97

Pointname

C01

C01A

C02 N

C02 M

C02 F

C03

C04

C05 N

C05 M

C05 F

PROJECT W-320: TANKAY-02A-U11-A JUMPER

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

D I S


P L A C

TRANSLATIONS (X

0.0450.0180.0060.049

0.0460.0170.0050.050

0.0480.0160.0060.051

0.0490.0160.0060.052

0.0490.0180.0060.052

0.0490.0180.0060.052

0.0480.0200.0070.052

0.0470.0210.0070.053

0.0470.0230.0080.053

0.0470.0230.0080.053

Y

0.0140.0280.0150.034.

0.0140.0260.0150.033

0.0150.0240.0170.033

0.0170.0220.0180.034

0.0180.0220.0190.034

0.0180.0220.0190.034

0.0180.0220.0190.034

0.0180.0220.0190.034

0.0180.0220.0190.034

0.0180.0220.0180.034

AY02A2B2.0U1

ANALYSIS

E M E N T

n >2

0.0080.0090.0070.014

0.0080.0090.0070.014

0.0080.0090.0070.014

0.0090.0090.0080.015

0.0130.0110.0100.019

0.0130.0110.0100.019

0.0170.0150.0120.026

0.0200.0190.0130.031

0.0230.0230.0150.035

0.0230.0230.0150.036

3-12-97


S

ROTATIONS (decX

0.0730.0970.0340.126

0.0730.0970.0340.126

0.0730.0980.0340.126

0.0740.0990.0350.129

0.0750.1010.0360.131

0.0750.1010.0360.131

0.0750.1010.0360.131

0.0760.1020.0370.132

0.0770.1040.0380.135

0.0780.1040.0390.136

9:53a

Y

0.0290.0200.0090.037

0.0290.0200.0090.037

0.0290.0200.0100.037

0.0280.0200.0110.036

0.0280.0200.0110.036

0.0280.0200.0110.036

0.0270.0200.0120.036

0.0250.0210.0130.035

0.0220.0210.0160.035

0.0180.0220.0210.036

)Z

0.0250.0390.0170.049

0.0250.0390.0170.049

0.0240.0390.0180.050 '

0.0240.0400.0180.050

0.0240.0410.0180.050

0.0240.0410.0180.050

0.0240.0410.0180.051

0.0230.0420.0170.051

0.0230.0430.0170.052

0.0230.0440.0160.052


Pointname

C06 N

C06 M

C06 F

C07

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

* * * Segment c end **

A09

1

2

3

4

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1 'R2R3RESPONSE

: TANKJUMPER

D I S


P L A C

TRANSLATIONS (X

0 .0470.0230 .0080.053

0.0470.0240.0080.053

0.0470.0250.0080.053

0.0460.0280.0100.055

*

0.0450.0180.0060.049

0.0420.0200.0070.047

0.0420.0200.0070.047

0.0420.0200.0070.047

0.0420.0200.0070.047

Y

0.0180.0220.0180.034

0.0170.0230.0170.033

0.0150.0250.0170.033

0.0160.0350.0150.042

0.0270.0460.0090.054

0.0270.0460.0090.054

0.0240.0430.0080.049

0.0170.0360.0090.041

0.0160.0340.0110.039

Page

ANALYSIS

E K E M I S

n )z

0.0230.0230.0150.036

0.0230.0230.0160.036

0.0220.0220.0160.035

0.0220.0220.0160.035

0.0140.0270.0060.031

0.0060.0130.0050.015

0.0050.0100.0050.012

0.0090.0080.0080.014

0.0110.0100.0090.017

14 of 26


ROTATIONS (decX

0.0790.1040.0390.136

0.0790.1050.0400.137

0.0790.1060.0410.139

0.0790.1070.0420.140

0.0840.1180.0320.148

0.0870.1200.0340.152

0.0850.1180.0330.149

0.0820.1120.0310.142

0.0840.1170.0310.147

Y

0.0180.0220.0210.036

0.0150.0240.0250.038

0.0130.0260.0280.040

0.0130.0270.0290.041

0.0170.0260.0100.032

0.0180.0270.0110.034

0.0180.0260.0110.O33

0.0150.0230.0080.028

0.0150.0240.0080.029

)Z

0.0230.0440.0160.052

0.0240.0440.0160.052

0.0240.0450.0160.053

0.0240.0450.0160.053

0.0250.0270.0180.041

I0.0250.0260.0180.040

0.0260.0280.0190.043

0.0240.0250.0180.039

0.0230.0260.0180.039


AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE*4.60 RESULT PAGE 15


Pointname

A12

5

6

7

8

9

B01

10

BOS

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

RlR2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

RlR2R3RESPONSE

RlR2R3RESPONSE

TRANSLATIONS ( i n )X Y 2

0.0450 . 0 1 80.0060.049

0.0410.0270.0080.050

0.0390.0330.0100.052 •

0.0390.0330.0100.052

0.0390.0330.0100.052

0.0410.0270.0080.050

0.0410.0270.0080.050

0.0450.0170.0050.049

0.0460.0200.0060.051

0.0160.0340.0110.039

0.0500.0840.0160.099

0.0700.1120.0230.134

0.0740.1160.0250.140

0.0770.1180.0270.143

0.0580.0910.0200.110

0.0580.0910.0200.110

0.0240.0430.0080.050

0.0500.0840.0160.099

0.0060.0120.0070.015

0.0090.0080.0080.014

0.0090.0080.0080.014

0.0060.0080.0070.012

0.0050.0100.0050.012

0.0050.0100.0050.012

0.0120.0230.0050.026

0.0050.0100.0050.012

0.0070.0160.0060.018

ROTATIONS (degX Y

0.0840.1180.0320.148

0.0930.1310.0350.164

0.0990.1400.0380.176

0.0960.1360.0350.170

0.0950.1310.0360.166

0.0850.1190.0320.150

0.0840.1180.0320.148

0.0840.1160.O320.147

0.0930.1310.0350.164

0.0170.0260.0100.032

0.0130.022

. 0.0070.026

0.0150.0240.0090.030

0.0180.026O.0100.033

0.0190.0280.0110.035

0.0190.0280.0120.036

0.0170.0260.0100.032

0.0190.028O.0120.036

0.0130.0210.0070.026

)Z

0.0250.0270.0180.041

0.0670.0790.0510.116

0.0300.0310.0210.048

0.0230.0220.0180.037

0.0170.0160.0150.027

0.0100.0100.0070.016

0.0250.0270.0180.041

0.0060.0110.0070.015

0.0670.0790.0510.116

Point/Supp. ID

S01801 1Stiff

B04804 1Stif f

Connect/Type

9Guide

.•RIGID

5Guide

:RIGID

S U

LoadCombinat ion

Rl

R2

83

RESPONSE

R1

R2

R3

RESPONSE

P P O

D i m

downleft

downleft

downleft

downleft

downleft

downleft

downleft

downleft

R T F

L O C AForce'

23233

31270

9186

40402

2837

4156

1134

5175

O R C E S

LDeform

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

GDim

XYz

XY

z

XY

z

XY

z

XY

z

XY

z

XY

z

XY

z

L O B AForce

23323

27031

1869

40240

3728

5641

3411

7551

LDeform

0.0000.0000.010

0.0000.0000.014

O.OOO0.0000.004

0.0000.0000.018

0.0000.0000.010

0.0000.0000.015

0.0000.0000.004

0.0000.0000.018

AY02A2R2.OUT 3-12-97 9:53a Page 15 of 26

AY02A2R2 PROJECT U-320: TANK0 3 / 1 2 / 9 7 AY-02A-U11-A JUMPER

Pointname

A00

A22

B01

BO',

a 59 2CO to

o

Loadcombination

AnchorR1R2R3RESPONSE

AnchorR1R2R3RESPONSE

GuideR1R2R3RESPONSE

GuideR1R2R3RESPONSE

R E S


T R A I

FORCES ( I bX Y

1897329

205

80291386

233270186402

37563475

2

488336

102

5913046

150

2331

940

28411151

N T

)

R E A

Result

46426590

30518099

0000

0000

20111880

246

10414393

200

234272186404

46693691

FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60 RESULT

C T I t N S


10018039

209

529479

133

0000

0000

Y 2

1739337

. 200

3193

32

0000

0000

)

2664

27

38322556

0000

0000

PAGE 16

Result

20220254

291

7210083

148

0000

0000


L O C


* * * Segment A begin

A00 R1R2R3RESPONSE

A01 R1R2R3RESPONSE

A03 R1R2R3RESPONSE

A04 N R1R2 'R3RESPONSE

A04 M R1R2R3RESPONSE

A04 F R1R2R3RESPONSE

A05 N R1R2R3RESPONSE

A05 M R1R2R3RESPONSE

A05 F R1R2R3RESPONSE

A L F


O R C

FORCES ( I bx r

***

46426590

46425986

46425583

46425583

39364369

37793494

37793493 .

39354267

47395179

488336

102

48783698

47753696

37803494

448247

105

1896732

203

46415381

448046

102

46733693

E S

7

1897329

20S

1887329

204

1877329

203

1896832

204

1896732

203

46415482

1876732

202

1866732

200

1827229

198

£ M

Result

20011880

246

19911575

242

19811372

239

19811372

239

19811272

239

19811271

238

19611170

236

19511070

235

19310969

232

FLUOR DANIEL NORTHUEST. INC.AutoPIPE+4.60

O M E N T S

MOMENTS ( f tX

2664

27

2664

• 27

266U

27

2664

27

33261545

35231244

35231244

1406332

157

2178643

237

Y

1739337

200

1267529

150

1086827

130

984522

110

4317

747

7212532

148

1245227

137

1294522

138

69141171

RESULT

-Ib )2

10018039

209

8916336

189

8515735

182

7815937

181

7213934

160

38221345

8111239

144

899554

141

817965

130

PAGE 17

Result

202202

54291

15717947

243

13917145

225

12816543

213

9014338

173

8812936

161

15212649

203

21012367

252

24211779

280

3-12-97 9:53a Page 16 of 26

rAY02A2R2 PROJECT W-320: TANK03/12/97 AY-02A-U11-A JUMPER

Pointname

A06

A07

A08 N

A08 H

A08 F

A09 -

A09 t

A10 -

A10 +

A11 -

L

Load

0 C A L F

241 C-106 SLUICINGDYNAMIC ANALYSIS

O R C E S

FORCES ( l b -combination X Y

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

47385078

47375078

47375078

1586940

177

1777029

193

1777029

193

1009650

147

1009650

147

1398242

166

1398242

166

45723692

45713692

1797129

194

943941

109

44703690

44703690

32523973

32523973

32503670

32503670

AY02A2R2

2

1807129

196

1797129

195

45713691

44703690

47364977

47364977

34333660

34333660

13192332

13192332

.OUT

& MO

Result

19210868

230

19110768

229

19010768

228

18910667

227

18810567

226

18810567

226

11011472

175

11011472

175

1439860

183

1439860

183

3-12-97 9

FLUOR DANIELAutoP IPE+4 .60

M E N T S

HORTHUEST, INC.RESULT

MOMENTS ( f t - l b )X

2178643

237

2178643

237

2178643

237

12810284

184

609391

143

609391

143

508482

127

508482

127

31654987

31654987

:53a

Y

1353316

140

1955523

204

648081

130

1827348

202

2457335

258

2457335

258

2397536

253

2145747

227

1145329

129

943654

114

Z

717573

126

648081

130

1955624

205

2387130

250

2079934

232

2079934

232

17011344

209

15813230

208

10015367

195

9319537

219

PAGE 18

Result

26611986

303

29913094

339

29913094

339

326144101370

327154103376

326154103375

29815999

352

27116699

333

15517587

249

13620882

262

AY02A2R203/12/97

Point

PROJECT U-320: TANKAY-02A-U11

L O

Loadname combination

A11 +

A12 -

A12 +

A13

A13A

A14 -

A14 +

A15

A15A

A16 N

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

-A JUMPER

C A L F


0 R C

FORCES ( I bX Y

1053213

111

1053213

111

559

12

117

1016

158

1019

158

1019

4620

951 .

50221055

55231060

57241062

2

3765

•5291

37655291

509921

112

5010121

115

5110321

117

5110321

117

5511631

133

5611833

135

5712135

138

37596494

E S

21443560

21443560

36284262

36304564

35314666

35314666

31446685

30456786

30466988

5311645

135

Paoe 17

8 MO

Result

1138464

155

1138464

155

6110348

129

6310650

133

6410852

136

6410852

136

7812674

165

8112876

170

85132

78175

8613379

176

of 26


M E N T S



117189

58230

11718958

230

10017654

210

10017654

210

10017654

210

10017654

210

10617742

211

10617742

211

10617742

211

10617742

211

Y

180116106239

17293

116227

17094

115225

1367175

170

1306768

161

1276563

156

1235955

147

1205649

141

1165139

133

83211086

2

110239

52268

10221046

238

10021146

238

7611835

145

7410333

131

739332

122

558131

103

53702892

51522376

83441495

PAGE 19

Resul t

242326132427

232298138402

221291135389

18522498

306

180215

93295

17721089

288

171204

76277

16919870

270

16519162

260

15818346

247

AY02A2R2 PROJECT U-320: TANK03/12/97 AY-02A-U11

Pointname

A16 M

A16 F

A17 N

A17 H

A17 F

A18 N

A18 M

A18 F

A19 N

A19 M

L 0

Loadcombination

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

RlR2R3RESPONSE

R1R2HRESPONSE

-A JUMPER

C A L F


O R : E S

FORCES < l bX Y

61435090

37606495

37616496

38733991

60631889

61641890

595858

101

29497191

29507192

409165

118

31484170

5311746

136

59602187

60465694

6110938

131

29487090.

37554379

5912746

147

59127

46147

5210355

128

Z

5311746

136

59251165

5510443

125

5510444

125

29487090

6111038

131

6211039

132

74281280

75291381

75291381

AY02A2R2.OUT

& M

Result

87133

79178

8813480

179

89134

80180

9013581

181

9113581

182

92136

82183

9313682

184

9913985

190

10014086

192

10014086

192

3-12-97


O M E N T S



4810431

119

905923

110

905923

110

16219052

255

164242

66300

164242

66300

9815951

194

24212037

24212037

28171636

9:53a

Y

13316537

215

976430

120

141207

53256

6813938

159

129146

29197

38371354

128169

40216

1355526

148

7448

10141322

Z

835525

103

124220

51257

9614335

176

11015332

191

42441362

130146

29198

12814134

193

126235

59273

48414175

48605192

PAGE 20

Result

164203

54266

181237

63305

193258

68330

207281

72356

213286

73364

213285

73363

205272

73349

186242

67313

54464584

576455

101

AY02A2R203/12/97

Point

PROJECT W-320: TANKAY-02A-U11

L O C


A19 F

A20

A21

A22

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

* * * Segment A end

* * * Segment B begin

A10

B01 -

801 +

B02 N

802 F

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

RlR2R3RESPONSE

«rR2R3RESPONSE

A JUMPER

A L F

241 -C-106DYNAHIC

O R C E

FORCES ( l bX Y

5912746

148

59128

46148

59130

46150

5913046

150

* * *

* * *

22161430

22161430

13271735

13271735

55111458

Z

30507292

30517595

30518099

30518099

259

10

259

10

24291340

55111458

24291340

Paae

SLUICINGANALYSIS

S

75291381

77291383

80291386

80291386

45191952

45191952

55111458

24291340

13271735

£ HO

Result

10014086

192

10114189

195

104143

93199

10414393

199

50252561

50252561

62412578

62

2578

62412578

18 of 26


H E N T S

NORTHWEST, INC.RESULT PAGE 21


3193

32

3193

32

31" 9

332

3193

32

806054

114

806054

114

65103

48131

6510348

131

17221934

Y

12242235

15252237

20272341

38322556

1022331

109

18241433

19231333

9171524

23111027

Z Re

507760

110

508062

113

508466

118

529479

133

32403663

33352855

9181424

11231429

538943

113

>ult

608164

119

618466

123

638870

129

7210083

148

1347572

169

897362

131

68107

52137

6610752

136

609348

121

w£

AY02A2R2 PROJECT U-320: TANK03 /12 /97 AY-02A-U11-P

L 0 C

Po in t Loadname combina t ion X



B04 - R1R2R3RESPONSE

B04 + R1R2R3RESPONSE

A11 R1R2R3RESPONSE

* * * Segment 8 end

* * * Segment C b e g i n

A14 RlR2R3RESPONSE

5 C01 R1q R2

3 R3•c RESPONSE

^ C01A R1

S R23 R3O : RESPONSE

C02 N R1R2R3RESPONSE

241-C-106JUMPER DYNAMIC

A L F 0 R C E

FORCES (1bY

55111458

13271735

13271735

13271735

13271735

* *

* *

11132026

10121824

9111722

9111722

2

13271735

24291340

24 ,291340

52702189

52702189

10202131

8171927

7141723

6141622

SLUICINGANALYSIS

S

24291340

55111458

55111458

39553576

39553576

29121033

25111029

20101024

199

1023

8 MO

Result

62412578

62412578

62412578

669344

123

669344

123

32273152

28242846

23212640

22202539

FLUOR DANIEL NORTHUEST. INC.AutoPIPE*4 .60 RESULT

M E N T S


17221934

26533167

26533167

56533167

26533167

19139

25

19139

25

19139

25

19139

25

Y Z

35673583

15271735

24271841

24271841

898559

137

469

12

259

11

44

10• 12

94

1215

21138

26

9171524

9181424

9181424

10614737

185

12151927

11142027

11132127

10132329

PAGE 22

Result

44724093

32623879

37633882

37633882

14117876

240

23212339

23202438

22192538

24192841

AY02A2R203/12/97

Point

PROJECT U-320: TANKAY-02A-U11

L 0


C02 M

C02 F

C03

C04

C05 N

C05 M

C05 F

C06 N

C06 H

C06 F

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

RlR2R3RESPONSE

R1R2R3RESPONSE

R1R2R3RESPONSE

-A JUMPER

C A L F

241-C-106DYNAMIC

O R C E

FORCES ( I bX Y

6111922

6131521

6121520

5121520

5121419

109

1621

158

1020

148

1019

7109

16

78

1317

Z

9131220

8101621

8101621

8101520

158

1020

12118

18

5121419

79

1519

146

1521

5111318

SLUICINGANALYSIS

S

179

1022

179

1022

169

1021

169

1021

8101520

8101519

89

1519

5111419

5111418

138

1018

S M O

•

Resul t

20192537

20192436

19182436

18182435

18172334

17172334

17172333

17172333

16162232

15162131

FLUOR DANIEL NORTHWEST. INC.AutoPIPE+4

M E N T S

MOMENTSX Y

22111428

166

1523

16• 6

1523

166

1523

166

1523

11107

16

4101317

4101317

368 '

10

0000

.60 RESULT

( f t - l bZ

368

11

13106

17

13106

17

885

12

4111519

117

1823

146

1220

1345

379

12

957

13

9142429

7132226

7132226

5111822

576

10

3568

1345

146

1220

126

1017

38

1013

PAGE 23

Result

24192942

21172739

21172739

18152434

17142231

16132029

15131827

15131827

13121523

109

1218

AY02A2R2.OUT 3-12-97 9:53a Page 19 of 26

AV02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE*4.60 RESULT PAGE 24

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE*4.60 RESULT PAGE 25

L O C A L F O R C E S M O M E N T S E A M F O R C E S & M O M E N T S

Point Load FORCES <lb )name combination X Y z Result

MOMENTS ( f t - l b )Y Z Result

Beam Load PointID combination name

FORCES <lb )Ax ia l Y-Shear Z-She;

MOMENTS <ft-lb )Torsion Y-Y Mom. Z-Z Horn.

R1R2R3RESPONSE

: Segment C end

7 5 13 158 11 8 1613 13 10 2117 18 18 31

0000

0000

0000

0000

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1 '

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

A091A091A091A091

12121212 .

23232323

34343434

4A124A124A124A12

88

161610102020

6060454531318181

5858464631318080

667755

1010

55

111199

1616

7676404028289090

1717181813132828

1717181813132828

3737313125255454

3232272729295151

1717181816162929

332222

' 44

3. 3

332255

33553377

12123333

1313

66332277

11111122

11111122

33332255

22222244

111

111

101

192

42312152

25141327

21231133

17331238

414

203

142

485

683

11277

15

8391144

7311566

262

222

172

384

3223

192

185

34

AY02A2R2.0UT 3 -12 -97 9 :53a Page 20 of 26

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTKUEST, INC.03/12/97 AV-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 26

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS


i E A M F O R C E S & M O M E N T S B E A M F O R C E S M O M E N T S


FORCES <lb ) MOMENTS ( f t - l b )Ax ia l Y-Shear Z-Shear Torsion Y-Y Mom. Z-Z Mom.


FORCES (Ib ) MOMENTS (ft-lb )Axial Y-Shear Z-Shear Torsion Y-Y Mom. Z-Z Mom.

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

35353535

56565656

67676767

78787878

89898989

910910

2121141413132929

2222151512122929

11114466

1414

77

121299

1717

2525171713133333

0011

4949545436368181

13135566

15. 15

2222151512123030

2525171713133333

99

1414101019-19

22

121233

1515

16162424

77

2929

14142020

66

2525

1616212166

2727

1818252577

3232

33332244

33332255

22111133

2211 •

1133

11222233

0000

21522216327

152

. 22161273

31532127527

15. 121272273

22012618334

2030

64346642462710360

3445424227306069

4525422930206943

256291420104318

66141101186

4010

R3

RESPONSE

R1

R2

R3

RESPONSE

R1

R2

R3

RESPONSE

910910

580558055B055B05

9B019B019B019B01

1 01 01 21 2

1 01 01 01 0) 0) 01 01 0

0 250 250 180 180 140 140 340 34

1122

11000011

239239255255176176391391

0000

00000000

22111122

2040

00 .000000

11372

1462

1003

224

1040

00000000

193323318153148

AY02A2R2.COT 3-12-97 9:53a Page 21 of 26


AY02A2R2 PROJECT W-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS




: Segment A begin •

A00

A01

A03

A04

A04

A04

A04

A04

A05

A05

A05

N-

N+

M

F-

F+

N-

N+

M

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

+++

++

+++

++

+

+

+++

+++

+++

+++

++

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

RlR2R3

10018039

8916336

8515735

8215235

7815937

7213934

7212532

382213

1245227

8111239

899554

1739337

1267529

• 1086827

956325

984522

43177

382213

7212532

8111239

1245227

1294522

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.001.001.00

.00 (18) OCC

.oo (18) occ

.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.95 1.63 (18) OCC1.95 1.63 (18) OCC1.95 1.63 (18) OCC

1.95 1.63 (18) OCC1.95 1.63 (18) OCC1.95 1.63 (18) OCC

959 22211971 22211258 22211

741 22211861 22211224 22211

657 22211819 22211213 22211

603 22211791 22211206 22211

1391 222112001 22211505 22211

983 222111718 22211428 22211

961 222111555 22211413 22211

389 22211611 22211165 22211

711 22211593 22211229 22211

1231 222111125 22211424 22211

1308 22211958 22211537 22211

ASME B31.3C (1992) CODE COMPLIANCE(Moments i n f t - l b ) (Stress in psi )

Point Load I n - P l . Out-Pl . Torsion S.I .F Eq. Load Code Codename combination Moment Moment Moment In Out no. type Stress Allow.

A05

A05

A06

A07

A08

A08

A08

A08

A08

A09

A12

A13

F-

F*

N-

H+

M

F-

F+

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.sus.Sus.

+ R1+ R2• R3

• R1+ R2+ R3

* R1+ R2* R3

+ R1+ R2+ R3

+ R1+ R2+ R3

+ R1+ R2+ R3

* R1• R2* R3

* R1t R2+ R3

+ R1+ R2+ R3

+ R1+ R2+ R3

* R1+ R2+ R3

+ R1+ R2+ R3

897966

817965

717573

648081

648081

1955624

2387130

2457335

2079934

2079934

10021146

7611835

58136

691411

1353316

1955523

1955624

. 648081

1827348

2079934

2457335

2457335

17094115

1367175

1.95 1.63 (18) OCC1.95 1.63 (18) OCC1.95 1.63 (18) OCC

1.00 1.00 ( 1 8 ) ' OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.78 1.48 (18) OCC1.78 1.48 (18) OCC1.78 1.48 (18) OCC

1.78 1.48 ( 18 ) OCC1.78 1.48 ( 18 ) OCC1.78 1.48 ( 18 ) OCC

1.78 1.48 ( 18 ) OCC1.78 1.48 (18) OCC1.78 1.48 (18) OCC

1.00 1.00 ( 1 8 ) OCC1.00 1.00 (18) OCC1.00 1.00 ( 1 8 ) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

951 22211744 22211616 22211

511 22211383 22211316 22211

733 22211393 22211357 22211

1874 22211888 22211769 22211

1881 22211891 22211771 22211

3293 222111410 222111160 22211

4583 222111525 22211811 22211

4874 222111789 22211732 22211

2936 222111124 22211

2934 222111125 22211447 22211

1803 222112114 222111132 22211

1420 222111263 22211755 22211

AY02A2R2.OUI 3-12-97 9:53a Page 22 of 26

AV02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 30

AY02A2R2 PROJECT U-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-LI11-A JUMPER DYNAMIC ANALYSIS


ASME 831.3c (1992) CODE COMPLIANCE(Moments in ft-Lb ) (stress in psi )


ASME B3i.3c (1992) CODE COMPLIANCE(Moments in ft-Ib ) (Stress in psi )

Point Load In-Pl. Out-Pl. Torsion S.I.F. Eq. Load Code Codename combinat i on Moment Moment Moment In Out no. type Stress A11ow.

A13A

A14

A14

A15

A15A

A16

A16

A16

A16

A16

A17

A17

+

N-

H*

M

F-

F*

N-

II*

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

sus.Sus.Sus.

Sus.Sus.Sus.

sus.Sus.Sus.

Sus.Sus.Sus.

Sus.sus.Sus.

+ R1• R2• R3

+ R1• R2+ R3

+ R1+ R2• R3

• R1• R2+ R3

+ R1• R2+ R3

+ R1• R2* R3

* R1+ R2+ R3

• R1+ R2* R3

+ R1+ R2+ R3

+ R1+ R2+ S3

+ +

+

* R2+ R3

7410333

1276563

1235955

537028

515223

572710

834414

835525

976430

12422051

133242

57

9614335

1306768

739332

558131

1205649

1165139

1024015

832110

13316537

124220

51

976430

1086830

141207

53

1.00 1.00 (18) OCC 1367 222111.00 1.00 (18) OCC 1125 222111.00 1.00 (18) OCC 692 22211

1.221.221.22

1.221.221.22

1.001.001.00

1.001.001.00

1.001.001.00

1.781.781.78

1.781.781.78

1.781.781.78

1.001.001.00

2.562.562.56

1.301.301.30

1.301.301.30

1.001.001.00

1.001.001.00

1.001.001.00

1.481.481.48

1.481.481.48

1.481.481.48

1.001.001.00

1.001.001.00

2.132.132.13

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

(18)(18)(18)

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

OCCOCCOCC

16571321806

15191170

717

1202820515

1161665412

1073442161

1754763270

22572405

639

22943157

844

7531100283

8201207308

18672751699

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

A17

A17

A17

A18

A18

•A18

A18

A18

A19

A19

A19

A19

M

F-

F+

N-

N*

M

F-

F+

N-

N+

M

F-

Sus.Sus.Sus .

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus .Sus.

Sus.Sus.Sus.

Sus.Sus .Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

Sus.Sus.Sus.

+ R1+ R2* . R 3

• R1• R2* R3

* R1+ R2+ R3

+ R1+ R2+ R3

• R1• R2* R3

+ R1+ 82+ R3

+ R1+ R2* R3

+ R1+ R2+ R3

+ R1+ R2* R3

+ R1* R2• R3

+ R1+ R2+ R3

+ Rl* R2* R3

110153

32

118152

29

424413

383713

130146

29

12814134

115126

35

126235

59

484141

484141

486051

507760

6813938

661612

129146

29

13014629

383713

12816940

144206

54

1355526

744

744

101413

122422

2.56 2.13 (18) OCC 1519 222112.56 2.13 (18) OCC 2356 222112.56 2.13 (18) OCC 555 22211

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

2.56 2.13 (18) OCC2.56 2.13 (18) OCC2.56 2.13 (18) OCC

1599 222111873 22211377 22211

649 22211733 22211151 22211

649 22211724 22211153 22211

1642 222111835 22211382 22211

' 2043 222112448 22211590 22211

2042 222112617 22211697 22211

885 222111159 22211308 22211

232 22211196 22211197 22211

592 22211502 22211502 22211

599 22211746 22211640 22211

623 22211978 22211769 22211

AY02A2R2.0UT 3-12-97 9:53a Page 23 of 26


Point Loadname comb

A19 F+ Sus.Sus.Sus.

A20 Sus.Sus.Sus.

A21 SUS.Sus.Sus.

A22 Sus.Sus.Sus.

*** Segment

*** Segment

*** Segment

*** Segment

A14 Sus.Sus.Sus.

C01 Sus.Sus.Sus.

C01A Sus.Sus.Sus.

C02 N- Sus.Sus.Sus.

C02 N+ Sus.Sus.Sus.

C02 M Sus.Sus.Sus.

ASME B31

241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.DYNAMIC ANALYSIS AutoPIPE+4.60

3c (1992) CODE COMPLIANCE(Moments in ft-lb )

n-Pl. Out-Pl. Torsionnation Moment Moment Moment

+ R1+ R2• R3

* R1* R2• R3

+ R1+ R2+ R3

+ R1• R2• R3

A end

B begin

8 end

C begin

+ R1+ R2+ R3

+ R1• R2* R3

+ R1+ R2+ R3

+ R1+ R2+ R3

* R1• R2•• R3

+ R1+ R2* R3

507760

508062

508466

529479

***

***

**•

***

469

111420

111321

101323

101323

91424

122422

152522

202723

383225

121519

259

4410

9412

9412

368

(StressS.I.F Eq.In Out no.

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.22 1.30 (18)

.22 1.30 (18)

.22 1.30 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

.00 1.00 (18)

1.00 1.00 (18)1.00 1.00 (18)1.00 1.00 (18)

1.78 1.48 (18)1.78 1.48 (18)1.78 1.48 (18)

1.78 1.48 (18)1.78 1.48 (18)1.78 1.48 (18)

Loadtype

OCCOCCoccoccoccoccoccoccoccoccoccocc

occoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccocc

RESULT

in psiCode

Stress

246388306

250401317

261422336

311477396

143182240

106138199

103128210

123128238

202224410

150236412

PAGE 32

)Code

Allow.

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211 •

222112221122211

222112221122211

AY02A2R2 PROJECT J-320: TANK03/12/97 AY-02A-U11-A JUMPER

Point Loacname combination

C02 F- Sus. +Sus. +Sus. +

C02 F+ Sus. +Sus. +Sus. +

C03 Sus. +Sus. +Sus. +

C04 Sus. +Sus. +Sus. +

C05 N- Sus. *Sus. +Sus. +

C05 N+ Sus. +Sus. +Sus. +

C05 M Sus. +Sus. +Sus. +

C05 F- Sus. +Sus. +Sus. +

C05 F+ Sus. +Sus. +Sus. +

C06 N- Sus. +Sus. +Sus. +

C06 N+ Sus. +Sus. +Sus. +

C06 M Sus. +Sus. +Sus. *

R1R2R3

R1R2R3

R1R2R3

R1R2R3

RlR2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

R1R2R3

ASME B31

241-C -106 SLUICING FLUOR DANIELDYNAMIC ANALYSIS AutoPIPE+4.60



71322

71322

7'1322

51118

41115

576

356

134

134

133

14612

12610

13106

13106

13106

885

576

41115

11718

14612

14612

14612

134

379

ft-lb ) (StressTorsion S.I.F Eq.Moment In Out no.

1.78 1.48 (18)1.78 1.48 (18)1.78 1.48 (18)

1.00 1.00 (18)1.00 1.00 (18)1.00 1.00 (18)

1.00 1.00 (18)1.00 1.00 (18)1.00 1.00 (18)

.00

.00

.00

.00

.001.00

.00 (18)

.00 (18)

.00 (18)

.00 (18)

.00 (18)

.00 (18)

1.73 1.44 (18)1.73 1.44 (18)1.73 1.44 (18)

1.73 1.44 (18)1.73 1.44 (18)1.73 1.44 (18)

1.73 1.44 (18)1.73 1.44 (18)1.73 1.44 (18)

1.00 1.00 (18)1.00 1.00 (18)1.00 1.00 (18)

.00 1.00 (18)

.00

.00

.73

.73

.73

1.731.731.73

.00 (18)

.00 (18)

.44 (18)

.44 (18)

.44 (18)

.44 (18)

.44 (18)

.44 (18)

Loadtype

OCCOCCoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccoccocc

II


in psiCode

Stress

207243366

133145208

132145208

315441610

214402532

344616789

541444910

669342597

463229407

463228406

800386695

700498689

PAGE 33

)Code

Allow.

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

222112221122211

AY02A2R2.OUT 3-12-97 9:53a Page 24 of 26

AY02A2R2 PROJECT W-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHUEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 3

AY02A2R2 PROJECT W-320: TANK 241-C-106 SLUICING03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS





C06 F- Sus. + R1Sus. + R2Sus. + R3

C06 F+ Sus.Sus.Sus.

C07 Sus.Sus.Sus.

957

• 000

1.73 1.44 (18) OCC1.73 1.44 (18) OCC1.73 1.44 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

545 22211465 22211602 22211

320 22211301 22211388 22211

0 222110 222110 22211


*** Segment C end

Maximum XMaximum YMaximum 1Max. total

•laximum rotations (c


•Jaximum restraint f


Maximum restraint m

• Maximum XMaximum YMaximum ZMax. total

0.0580.1430.0360.153

eg)

0.1760.1090.1160.203

>rces(lb)

402. 150

99404

3ments(ft-l

20920056291





A17 F8C05 F

6A19 NB05B05

B01A22A22B01

A00A0OA22A00





RESPONSERESPONSERESPONSERESPONSE




AY02A2R2.OUT 3-12-97 9:53a

AY02A2R2 PROJECT H-320: TANK 241-C-106 SLUICING FLUOR DANIEL NORTHWEST, INC.03/12/97 AY-02A-U11-A JUMPER DYNAMIC ANALYSIS AutoPIPE+4.60 RESULT PAGE 36


S Y S T E M S U M M A R Y S Y S T E M S U M M A R Y

Maximum pipe forces Clb> Maximum occasional stress


Maximum pipe moment


193203205246

. (ft-lb)

300258273427



A08 FA04 FA00A00

A1S NA08 fA18 FA11







Pointstress psiAllowable psiRatioLoad combination

A08 F4874222110.22Sus. +

A08 F4874222110.22Sus. +

: The system satisfies ASME B31.3 code requirements' for the selected options

AY02A2R2.0UT 3-12-97 9:53a Page 26 of 26

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS

POINTNAME TYPE

•** SEGMENTAOOA01A

A018A01

A02A03

A03A

RunFlex

RunBend

RunBend

Valv

P 0 I

OFFSETSX Y

A00 0

0 00 0

00

1.76

N T

(ft

025

0434

00

0

D A T A L

)Z PIPE ID

0 4PIPE0

00

-0.81-0.65

0

PIT FLUOR DANIEL NORTHUEST, INC.AutoPIPE*4.60 MODEL PAGE 3

I S T I N G

DESCRIPTION

Wt= 144 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID Bend= 2080.0Z-Shear= RIGID Bend= 2080.0



Rating = 350, Height = 93 IbSurface factor = 4.50, SIF = 1.00 .

AY02E-R2 PROJECT U-320,03/04/97 JUMPER

POINTIIAHE

804B05306B07B08B09

B10

B10A

810BB11

241-AY-02E SLUICEASSEMBLY STRESS

F O I

OFFSETSTYPE X

RunRunRunRunTeeBend

Bend 1.

Flex

RunSend

00000 •

0

07

0

00

Y

0.0.2.1.0.0.

-0

•0

-0

N T D

(ft )•--Z

507512003586

0

40

0469

ANALYSIS

A T A L

PIPE ID

000000

0

0

00

PIT

I S T

FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60 MODEL PAGE 4

I N G

DESCRIPTION

LoneBendMidSIFFlex

ShorBendMidSIFFlex

Ut=

Elbow, Radius = 6.00 inchangle change = 90.00 deg>oint at 50.00 percent- In 1.95, Out = 1.63= 5.272

t Elbow, Radius =4.00 inchangle change = 90.00 deg

point at 50.00 percent- In 2.56, Out = 2.13= 7.908

144 Ib , Ar= 3.2 sq.inAxial= 23300000 Tors= 304.0Y-Shear= RIGID Bend= 2080.0Z-Shear= RIGID Bend= 2080.0

Long Elbow. Radius = 6.00 inchA03BA04A05A06A07

RunRunRunRunBend

0.720.690.090.090.50

00000

00000 Long Elbow, Radius = 6.00 inch


A08A09A102

***3BOOB01BO2B03

ReduRunRunRun

SEGMENT IRunRunReduRunBend

0000

33.85

0000

0000

0.940

• 0

00

0.600.330.630.46

0.560.460.630.331.27

3"PIPE10

103"PIPE

4PIPELong Elbow, Radius = 6.00 inchBend angle change = 90.00 degHid point at 50.00 percentSIF - In 1.95, Out = 1.63Flex = 5.272

*** SEGMENT CB08 Tee 3.85 5.66C01 Bend -0.46 0

C02 Bend 0 0.54

C03 Flex -0.25

3.25 2PIPE0

g , 0Bend angle change = 90.00 degMid point at 50.00 percentSIF - In 1.95, Out = 1.63Flex = 5.272



Ut= 87 Ib , Ar= 1.1 sq.inAxial= 13500000 Tors= 107.0Y-Shear= RIGID Bend= 659.0Z-Shear= RIGID 8end= 659.0

AY02E-R2.OUT 3-4-97 10:30a Page 2 of 32

AY02E-R2 PROJECT W-320, 241-AY-02E SLUICE PIT FLUOR DANIEL NORTHWEST, INC.03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS AutoPIPE+4.60 MODEL PAGE 5


POINT OFFSETS (ft )NAME TYPE X Y 2 PIPE ID DESCRIPTION

C04 Run -0.04 0 0

Total weight of empty pipes : 291 Ib

o 3re *T]

H to

* Ul

JO5o

AY02E-R203/04/97

POINT -NAME

PROJECTJUMPER

W-320, 241-AY-02E SLUICE PIT FLUOR DANIEL NORTHWEST. INC.ASSEM8LY STRESS ANALYSIS AutoPIPE+4.60 MODEL PAGE 6

COM

-COORDINATE(ftX

*** SEGMEN1A00

A01AA018A01 NA01A01 M

. A01 FA02

A03 NA03A03 MA03 EA03AA03BA04

A05A06

A07 NA07A07 MA07 FA08A09

A102

0

00

A00

0000

0.00000000

0.000.00

0000123

33

33333

00001550764817

2635

3585708585

3.85

3 853.85

*** SEGMENT B3BOOB01

3.853 853.85

Y

0.00

0.250.290.300.630.530.630.63

0.630.630.630.630.630.630.63

0.630.63

0.630.630.630.630.630.63

0.630.63

0.940.940.94

P O

j

Z

0

0000

•0

-0-0

N

00

00000000103381

-0.96•1.46-1 31-1.46-1 46•1.46-1 46

-1.46-1

-1-1-1-0-0-0

00

011

46

464631968653

1056

560265

N T

DATATYPE

ANCHOR

TI

GUIDE

TI

FLANGE

WEIGHTFLANGE

TI

GUIDE

GUIDE


DESCRIPTION


ID : A02 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.15Gaps set Weightless

Weld neck SIF = 1.00Rating = 400, Weight = 35 Ib12 Ib , No offsetsWeld neck SIF = 1.00Rating = 400, Weight = 35 Ib

ID : A09 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.06, Right = 0.06 inchFriction = 0.00Gaps set Weightless

ID : B01 1, Connected to GroundStiffness = RIGIDGap-down = 0.00, Above = 0.06 inchGap-left = 0.00, Right = 0.06 inchFriction = 0.00Gaps set Weightless

AY02E-R2.OUT 3-4-97 10:30a Page 3 of 32

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS


AY02E-R2 PROJECT W-320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 MODEL PAGE I


POINTDAME

B02B03 HB03B03 HB03 FB04B05B06B07B08

B09 NB09B09 MB09 FB10 NB10BIO MB1O FB10AB1OBB11 HB11B11 MB11 FB12

---COORDINATECftX

3.853.853.853.853.853.853.853.853.853.85

3.853.854.004.354.594.924.824.924.924.924.924.924.924.924.92

**• SEGMENT C608

C01 NCOIC01 MC01 FC02 NC02C02 MC02 FC03C04

3.85

3.563.393.443.393.393.393.343.223.143.10

Y

0.940.940.941.091.441.442.194.315.315.66

6.026.526.376.526.526.526.426.196.126.085.895.395.545.395.39

5.66

5.665.665.715.836.036.206.156.206.206.20

)- --2

1.982.753.253.103.253.253.253.253.253.25

3.253.253.253.253.253.253.253.253.253.253.253.253.403.753.75

3.25

3.253.253.253.253.253.253.253.253.253.25

DATATYPE

TI

HEIGHT

HEIGHTTEE

TI

TI

TI

ANCHOR

TEE

TI

TI

DESCRIPTION

27 Ib , No offsets •

35 Ib , No offsetsB16.9 welding teeSIF - In = 1.34, Out = 1.45


B16.9 welding teeSIF • In = 1.34, Out = 1.45


Pipe ID/ Norn/ O.D. Thickness(inch) Spec Weight(lb/ft )Material Sch inch W.Th. Corr Mill Insu Ling Grav Pipe Other Total

3"PIPE 3.000 3.500 0.216 0.06 0.03AU STD

4PIPEAU

4 4.500 0.237 0.06 0.03STO

2PIPE 2.000 2.375 0.154 0.06 0.02AU STD

10CS

10 10.750 1.000 0.06 0.13XXS

0 0 1.12 7.75 0 11.34

0 0 1.12 11.04 0 17.22

0 0 1.12 3.74 0 5.37

0 0 1.12 104 0 133

Number of points in the system : 64

" AY02E-R2.OUT 3-4-97 10:30a Page 4 of 32

sOB

AY02E-R203/04/97

MaterialName

AU

AU

cs

AU

to

.Rev.

o

PROJECT U-320, 241-AY-02E SLUICE PIT FLUOR DANIELJUMPER ASSEMBLY STRESS ANALYSIS

1 M A

Pipe

4PIPE

3"PIP

10

2PIPE

T E R I A L

DensityD Ib/cu.ft

501.0

501.0

489.0

501.0

D A T A L

Pois. Temper.Ratio deg F

0.30 40.0180.0

0.30 40.0180.0

0.30 40.0180.0

0.30 40.0180.0

NORTHWEST, INC.AutoPIPE*4.60 MODEL PAGE 9

I S T I N

ModulusE6 psi

28.42

28.42

29.62

28.42

G

:xpans.in/100ft

1.5442

1.5442

1.0406

1.5442

AllOH.psi

16700.016700.0

16700.016700.0

20000.020000.0

16700.016700.0

AY02E-R203/04/97

POINT --NAME

21

3456

7A028

PROJECTJUMPER

W-320H

241-AY-02E SLUICE PIT FLUOR DANIEL NORTHWEST, INC.ASSEMBLY STRESS ANALYSIS AutoPIPE+4.60 MODEL PAGE 10

-COORDINATEDX

3.853.85

3.853.853.853.85

3.850.005.60

Y

0.630.38

0.941.443.645.50

8.600.635.50


)--- DATAZ TYPE

0.560.56 Y-STOP

0.560.56 WEIGHT0.560.56 WEIGHT

0.56-0.81-1.00 ANCHOR

DESCRIPTION

ID : 1 1, Connected to GroundGap-Below = 0.00, Above = 0.06 inchFriction = 0.00Gaps set Weightless

1000 Ib , No offsets

2250 Ib , Offsets in ftOX = 0.00, DY = 0.00, 01 = 0.04


Ar02E-R2.OUr 3-4-97 10:30a Page 5 of 32




FLUOR DANIEL NORTBUEST, INC.AutoPIPE+4.60 MODEL PAGE 12

BEAM DATA LISTING CROSS SECTION LISTING

BEAMID

M1

H2

M3

M4

M5

H6

M7

M8

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

FromTo

POINTNAME

21

23

34

45

56

67

5A02

68

LENGTH(ft )

0.25

0.31

0.50

2.20

1.86

3.10

5.08

2.34

SECTION ID/MATERIAL ID

XS10A36

XS10A36

XS10A36

XS12A36

XS12A36

XS12A36

C3X4.1A36

C3X4.1A36

BETA RIGID RELEASEANGLE END(ft) Ax Y-Y Z-Z

Section ID Areatsq.in )ID Axial Y-Shear 2-shear

Inertia (in**4 )Torsion Y-Y Bend Z-Z Bend

"8 !

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

0.000.00

IIN

NN

NN

NN

N

IIN

NN

NN

NN

NN

NN

NN

NN

N

NN

NN

NN

NN

NN

NII

NN

IIN

NN

NN

xsioXS12XS12C3X4.1

16.19.19.1.

10202021

8.059.609.600.51

8.059.609.600.51

424.0724.0724.00.0

212.0362.0362.0

0.2

212.362.362.

1.

0007

Ar02E-R2.0UT 3-4-97 10:30a Page 6 of 32





BEAM MATERIAL LISTING

MATERIAL ID

A36

Elasticmodulus PoissonsE6 psi ratio

YieldStresspsi

DensityIb/cu.ft

UltimateExpansion stressE-6 /F psi



490.00 6.50000 •*• SEGMENT AA00 325A09 325A10 3252 325

*** SEGMENT 83 325BOO 325B02 325B12 325

*** SEGMENT CB08 325C04 325

180 1.544180 1.544180 1.041180 1.041

180180180180

180180

1.0411.5441.5441.544

1.5441.544

AV02E-R2.OUT 3-4-97 10:30a Page 7 of 32







Static - Date and Time of analysisModel Revision NumberNumber of Ioad casesLoad cases analyzedGaps/Friction/Yielding consideredTolerance - Force, DisplacementFriction - Factor, toleranceHanger des i gn runCut short includedOccasional load analysis typeNon-linear analysis summary fileBase load cases for nonlinear analysis

Weight of contents includedPressure stiffening caseWater elevation for buoyancy loads .

Modal - Date and Time of analysisModel Revision NumberNumber of modesCutoff frequency (Hz)Weight of contents includedPressure stiffening case ,Water elevation for buoyancy loads. ,

Response - Date and Time of analysisModel Revision NumberNumber of load casesLoad cases analyzedDate and time of modal analysis ...Number of modesCutoff frequency (Hz)

h3 m Model revision of modal analysis ..^ 2? Weight of contents includedo ^3 Pressure stiffening caseCO to Water elevation for buoyancy loads

Mar 4, 1997 10:27 AM12GR T1Yes100.00 Ib 0.0600 in1.00 0.10NoNoNonlinearAY02E-R2.LOG

GR = NoneT1-= GR

Yes0Not considered

Mar 4, 1997 10:27 AM1

, 433.0Yes

. 0, Not considered

, Mar 4, 1997 10:27 AM. 1. 3. R1 R2 R3. Mar 4, 1997 10:27 AM. 4, 33.0, 1, Yes. 0. Not considered



GR + Max P Sustain Sum Gravity 1.00 Automatic DefaultMax Long 1.00

Cold to T1 Expansion Sum Thermal 1 1.00 Automatic Default




Hoop Max Hoop 1.00 Automatic Default



Default

Default

Default

Default

Default

User

G«

T1

R1

R2

R3

GR*T1

RESPONSE

Sum

Sum

Sum

Sum

Sum

Sum

Gravity 1.00

Thermal 1 1.00

Response 1 1.00

Response 2 1.00

Response 3 1.00

Gravity 1.00

Thermal 1 1.00

Response 1 1.00 UserResponse 2 1.00Response 3 1.00

Abs sum GR+T1 1.00 UserRESPONSE 1.00

CODE COMPLIANCE

Y - Factor 0.40Weld efficiency factor 0.80Range redaction factor 1.00

AY02E-R2.0UT 3-4-97" 10:30a Page 8 of 32


FLUOR DANIEL NORTKUEST, INC.AutoPIPE+4.60 RESULT PAGE 3



Design Pressure Factor 1.00Minimum stress ratio used in reports... 0.00Include corrosion in stress calcs YInclude torsion in code stress tiInclude axial force in code stress NLongitudinal pressure calculation PD/4tInclude rigorous pressure Not analyzed



Load case 1 - R1



X- Spectrum : SC1Multiplier : 1.00

SCI

Freq(Hz) Grave Freq(Hz) Grav( > Freq(Hz) Grav(

0.1000.4001.640

20.000

0.010.100.420.26

0.1600.6008.000

33.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20

AY02E-R2.OUT 3-4-97 10:30a Page 9 of 32





Load case 2

Missing mass : Yes2PA : No


Y- Spectrum : SC1Multiplier : 1.00

FreqCHz) Grave Freq(Hz) Grav< ) Freq(Hz) Grave

0.1000.4001.640

20.000

0.01 0.1600.10 0.6000.42 8.0000.26 33.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20

Load case 3 - R3



Z- Spectrum : SC1Multiplier : 1.00

Freq(Hz) Grave ) FreqCHz) Grave ) Freq(Hz) Grave

0.1000.4001.640

20.000

0.010.100.420.26

0.1600.6008.00033.000

0.030.160.420.20

0.2501.10012.000100.000

0.060.280.340.20

AY02E-R2.0UT 3-4-97 10:30a

AY02E-R203/04/97

PROJECT W-320, 241-AY-02E SLUICE PITJUMPER ASSEMBLY STRESS ANALYSIS



FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60 RESULT PAGE I

F R E Q U E N C I E S

Mode Frequency Frequency PeriodNumber (Rads/sec) (Hertz). (Sec)


Participation factorsX Y 2

Point . Load TRANSLATIONS (in )name combi nat i on X Y Z

ROTATIONS (deg )X Y 2

1

2

3

4

75.5913

110.5581

122.1752

139.4641

12

17

19

22

.0307

.5959

.4448

.1964

0

0

0

0

.083

.057

.051

.045

-0.013

-0.930

1.476

0.452

0.065

0.025

0.063

0.559

-1.079

-2.747

0.491

0.054

' * * Segment A begin 5

GRT1GR+T1RESPONSETOTAL

GRT1GR*T1RESPONSETOTAL






0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.000-0.002•0.0020.0000.002

•0.000-0.005-0.0060.0000.006

-0.001-0.013-0.0140.000

• 0.014

0.0000.0000.0000.0000.000

0.0000.0040.0040.0000.004

0.0000.0040.0040.0000.004

0.0000.0040.0040.0000.004

0.0000.0070.0070.0000.007

0.0000.0060.0060.0000.006

0.0000.0020.0020.0000.002

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.000 .0.000

0.0000.0000.0000.0000.000

0.000-0.004-0.0040.0010.004

0.000-0.008-0.0080.0010.009

0.000-0.016-0.0160.0010.016

0.0000.0000.0000.0000.000

0.000-0.001-0.0010.0010.002

0.001-0.039-0.0380.0100.048

0.001-0.039-0.0380.0100.048

0.001-0.044-0.0430.0060.049

0.000-0.044-0.0440.0010.045

-0.001-0.042-0.0430.0020.045

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0070.0800.0870.0000.087

0.0070.0800.0870.0000.087

0.0070.0800.0860.0010.087

0.0060.0780.0840.0030.087

0.0060.0760.0820.0040.087

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

-0.001-0.002•0.0040.0050.009

•0.001-0.OO2-0.0040.005

. 0.009

-0.002-0.004-0.0060.0040.010

•0.002•0.005-0.0080.0030.011

•0.003-0.007-0.0100.0030.012

Ar02E-R2.0UT 3-4-97 10:30a Page 11 of 32

AY02E-R2 PROJECT03/04/97 JUMPER

Pointname

A03 N

A03 H

A03 F

A03A

A03B

A04

A05

Load

U-320, 241-AY-02E SLUICE PITASSEMBLY STRESS ANALYSIS

0 I S P L A C E M E N T

TRANSLATIONS (in )combination X








-0.001-0.016•0.0170.0000.017

-0.001•0.018-0.0200.0010.021

-0.002-0.015-0.0160.0010.017

-0.0020.0050.0030.0010.004

-0.0020.0160.0140.0010.015

-0.0020.0260.0250.0010.026

-0.0020.0280.0260.001

. 0.027

Y

0.0000.0000.0000.0000.000

0.000-0.003-0.0030.0000.003

-0.001-0.004-0.0050.0000.005

-0.002-0.003-0.0050.0010.006

-0.002-0.003-0.0050.0010.005

-0.002-0.002-0.0040.0010.005

-0.002-0.002-0.0040.0010.005

Z

0.000-0.018-0.0180.0010.019

0.000-0.026-0.0260.0010.027

0.000-0.032-0.0320.0020.034

-0.001-0.041-0.0420.0060.048

-0.001-0.046-0.0460.0080.054

-0.001-0.049-0.0500.0100.060

-0.001-0.049-0.0500.0100.060

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60

S

RESULT PAGE 9

ROTATIONS (deg )X

-0.002-0.041-0.0430.0020.045

-0.005-0.032-0.0370.0020.039

-0.006-0.027•0.0330.0020.035

-0.007-0.018-0.0250.0030.028

-0.007-0.018-0.0250.0030.028

-0.008-0.014-0.0210.0030.024

-0.008-0.013-0.0210.0030.024

Y

0.0060.0760.0810.0050.086

0.0040.0630.0660.0110.077

0.0020.0430.0450.0150.060

0.0010.0280.0290.0150.043

0.0010.0280.0290.0150.043

0.O010.0150.0160.0130.029

0.0010.0130.0140.0130.027

2

-0.003-0.007-0.0100.0020.012 •

-0.004-0.004•0.0080.0020.010

-0.0040.001-0.0030.0020.005

-0.0010.0030.0020.0010.003

-0.0010.0030.0020.0010.003

0.0020.0050.0070.0010.007

0.0020.0050.0070.0010.008


Pointname

A06

A07 N

A07 M

A07 f

A08

A09

A10

Load

U-320, 241-AY-02E SLUICE PITASSEMBLY STRESS ANALYSIS

D I S P L A C E M E N T

TRANSLATIONS (in )combination X




GRT1 'GR+T1RESPONSETOTAL




-0.0020.0290.0280.0010.029

-0.0020.0290.0280.0010.029

-0.0020.0340.0330.0010.033

-0.0010.0320.0310.0000.032

-0.0010.0310.0300.0000.030

-0.0010.0260.0240.0000.024

-0.0010.0140.0130.0010.013

Y

-0.002-0.002-0.0040.0010.005

-0.002-0.002-0.0040.0010.005

-0.001-0.001-0.0020.0010.003

0.0000.000-0.0010.0000.001

0.0000.0000.0000.0000.001

0.0000.0000.0000.0000.000

0.0000.0000.0000.0010.001

z-0.001-0.049-0.0500.0110.061

-0.001-0.049-0.0500.0110.061

-0.001-0.046-0.0470.0110.059

-0.001-0.039-0.0410.0120.052

-0.001-0.038-0.0390.0120.051

-0.001-0.033-0.0340.0120.046

-0.001-0.023-0.0240.0120.036

FLUOR )ANIEL NORTHWEST, INC.AutoPIPE+4.60 RESULT PAGE 10

S

ROTATIONS (degX

-0.008-0.012-0.0200.0030.024

•0.008-0.012•0.0200.0030.024

-0.008-0.010-0.0190.0040.022

-0.006-0.003-0.0090.0050.014

-0.006-0.003-0.0080.0050.013

-0.004-0.001-0.0040.0050.009

0.000•0.003-0.0030.0060.009

Y

0.0010.0110.0120.0130.025

0.0010.0110.0120.0130.025

0.001-0.031-0.0300.0080.038

0.002-0.071-0.0690.0050.074

0.002-0.072-0.0710.0050.076

O.002-0.080-0.0780.0050.083

0.003-0.099-0.0960.0010.097

)z0.0020.0060.0080.0010.009

0.0020.0060.0080.0010.009

0.0040.0100.0140.0010.015

0.0030.0110.0140.0020.015

0.0030.0110.0140.0020.016

0.0020.0140.0160.0020.018

0.0000.0220.0220.0030.026

AY02E-R2.OUT 3-1-97 10:308 Page 12 of 32


FLUOR DANIEL NORTHWEST, INC.AutoPlPE+4.60 RESULT PAGE 11





TRANSLATIONS ( i n )X Y 2


GRT1GR+T1RESPONSETOTAL •

-0.0010.0040.0030.0010.004

0.0000.0000.0000.0000.000

-0.001-0.018-0.0190.0120.031

0.000-0.003-0.0030.0060.009

0.-0.-0.0.0.

003099096001097

0.0000.0230.0220.0030.026

*** Segment A end '

*** Segment B begin '

3 GRT1GR+T1RESPONSETOTAL

BOO GRT1GR+T1RESPONSETOTAL

B01 GRT1GR+T1RESPONSETOTAL


B03 N GRT1GR+T1RESPONSETOTAL

B03 M GRT1GR+T1RESPONSETOTAL

-0.0010.0030.0020.0010.002

0.000-0.007-0.0070.0010.008

0.000-0.020-0.0200.0000.020

0.000-0.028-0.0270.0010.028

0.001-0.045-0.0440.0030.046

0.002-0.053-0.0510.0040.055

0.0000.0000.0000.0000.000

0.0000.0000.0000.0010.001

0.0000.0000.0000.0000.000

-0.001-0.003-0.0040.0000.004

•0.003-0.014-0.0170.0010.018

-0.004-0.016-0.0200.0020.021

-0.001-0.019-0.0200.0110.031

-0.001-0.014-0.0150.0110.026

-0.001-0.004-0.0050.0110.016

-0.0010.0010.0000.0110.011

-0.0010.0130.0120.0110.023

-0.0010.0200.0190.0110.031

0.000-0.003-0.0030.0070.010

0.000-0.003-0.0030.0060.010

0.0060.0350.0410.0050.046

0.0100.0540.0640.0050.069

0.0130.0640.0770.0060.083

0.0120.0410.0520.0100.062

0.003•0.099-0.0960.0010.097

0.003•0.099-0.0960.0010.097

0.005•0.106-0.1010.0080.109

0.006-0.107-0.1010.0110.111

0.007-0.106-0.0990.0150.114

0.008-0.096-0.0870.0250.113

0.0000.0230.0220.0030.026

0.0000.0230.0220.0030.026

0.0000.0140.0140.0040.018

0.0000.0120.0110.0040.015

-0.0010.0080.0070.0050.012

-0.0010.0020.0010.0040.004


Pointname

B03 F

B04

605

B06

B07

B08

B09 N

Loadcombination




GRT1 •GR+T1

RESPONSETOTAL




TRANSLATIONS (1X

0.002•0.055-0.0530.0050.058

0.002-0.055-0.0530.0050.058

0.002-0.053-0.0510.0040.055

0.002-0.037-0.0360.0030.038

0.001-0.023-0.0220.0020.024

0.000-0.016-0.0160.0010.018

-0.001-0.009-0.0100.0010.011

Y

-0.004-0.011-0.0150.0020.017

-0.004•0.011•0.0150.0020.017

-0.0040.000-0.0040.0020.006

-0.0040.0330.0280.0020.030

-0.0040.0480.0440.0020.046

-0.0040.0530.0490.0020.051

-0.0040.0590.0550.0020.056

n )Z

0.0000.0240.0240.0110.035

0.0000.0240.0240.0110.035

0.0010.0220.0230.0100.033

0.0020.0060.0080.0120.020

0.002-0.004-0.0020.0140.016

0.002-0.007-0.0050.0160.021

0.002-0.011-0.0090.0170.026

ROTATIONS (degX

0.007-0.0040.0030.0150.018

0.006-0.0040.0030.0150.018

0.005-0.019•0.0150.0170.032

0.001-0.045-0.0440.0210.065

0.000-0.048-0.0490.0210.070

0.000-0.048-0.0490.0210.070

•0.001-0.047-0.0480.0210.068

Y

0.008-0.088-0.0800.0290.109

0.008-0.088-0.0800.0290.109

0.009-0.082•0.0730.0350.108

0.010-0.064-0.0540.0520.107

0.011-0.056-0.0450.0600.106

0.011-0.053-0.0420.0630.106

0.011-0.050-0.0390.0650.104

)Z

-0.001-0.012-0.0130.0030.016

-0.001-0.012-0.0130.0030.016

0.000-0.019-0.0190.0040.023

0.004-0.057-0.0530.0060.059

0.007-0.084-0.0760.0070.083

0.009-0.094-0.0850.0080.093

0.010-0.106-0.0970.0080.105

AY02E-R2.OUT 3-4-97 10:30a Page 13 of 32

AY02E-R2 PROJECT W-320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEM8LY STRESS ANALYSIS





Pointname

B09 M

B09 F

B10 N

BIO M

B10 F

B10A

B10B

Loadcombination








TRANSLATIONS (X

-0.0020.0040.0020.0010.004

-0.0020.0150.0130.0020.015

-0.0020.0190.0170.0020.018

-0.0020.0180.0160.0010.018

-0.0010.0090.0080.0010.009

-0.0010.0060.0050.0010.006

-0.0010.0050.0040.0010.005

Y

-0.0040.059.0.0560.0020.057

•0.0030.0460.0440.0010.045

-0.0020.0350.0330.0010.034

-0.0010.0220.0220.0000.022

0.0000.0140.0140.0010.014

0.0000.0130.0130.0010.013

0.0000.0130.0130.0010.013

in )Z

0.002-0.013-0.0110.0160.027

0.001-0.011-0.0100.0110.021

0.000•0.009-0.0090.0080.016

-0.001'-0.006-0.0060.0040.010

•0.001-0.004-0.0050.0020.006

-0.001-0.004-0.0040.0020.006

-0.001-0.004-0.0040.0010.006

ROTATIONS (degX

-0.001-0.042-0.0430.0190.062

-0.001-0.039-0.0400.0180.059

-0.001-0.037-0.0380.0190.057

-0.001-0.032-0.0340.0190.052

-0.002-0.023-0.0240.0190.043

-0.002-0.022-0.0240.0190.043

-0.0050.0280.0230.0120.035

Y

0.012-0.048-0.0370.0670.104

0.012-0.043-0.0310.0700.102

0.012-0.043-0.0300.0710.101

0.012-0.037-0.0250.0710.096

0.012-0.033-0.0210.0710.093

0.012-0.033-0.0210.0710.092

0.002-0.020-0.0180.0050.023

)Z

0.014-0.175-0.1610.0090.170

0.017-0.222-0.2050.0100.215

0.017-0.224-0.2070.0100.217

0.017-0.221-0.2040.0100.214

0.016-0.200-0.1850.0090.194

0.016-0.199-0.1840.0090.193

0.004-0.044-0.0400.0050.046





B11

B11

B11

B12

* * *

* * *

808

C01

C01

N

M

F





Segment B end

Segment C begin

N

M




0.0000.0030.0030.0010.004

0.0000.0010.0010.0000.001

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

. . *

. . .

0.000-0 .016•0 .016

0.0010.018

0.000-0.021-0.0210.0010.022

0.000-0.022-0.0220.0010.023

0.0000.0100.0100.0010.010

0.0000.0040.0030.0000.004

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

-0.0040.0530.0490.0020.051

-0.0050.0590.0540.0020.057

-0.0050.0620.0570.0030.059

-0.001-0.005-0.0050.0010.006

0.000-0.005-0.0050.0000.005

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.002-0.007-0.0050.0160.021

0.003-0.011-0.0080.0200.028

0.003-0.012•0.0090.0220.031

-0.0050.0290.0240.0120.036

-0.0050.0280.0230.0070.030

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.000-0.048-0.0490.0210.070

0.000-0.048-0.0490.0290.078

0.000-0.048-0.0490.0380.087

0.002-0.020-0.0180.0050.023

0.002-0.012-0.0110.0040.014

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.011-0.053-0.0420.0630.106

0.011-0.053-0.0420.0700.113

0.011-0.053-0.0420.0860.129

0.004-0.042-0.0380.0050.043

0.001-0.014-0.0130.0030.015

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.009-0.094-0.0850.0080.093

0.016-0.094-0.0790.0110.090

0.028-0.094-0.0660.0210.087

AY02E-R2.OUT 3-4-97 10:30a Page 14 of 32






Pointname

C01

C02

C02

C02

C03

C04

***

2

F

N

M

F

Loadcombination







Segment C end


TRANSLATIONS (in )X

-0.001-0.020-0.0210.0020.023

-0.003-0.016-0.0190.0030.022

-0.004-0.015•0.0180.0040.022

-0.004•0.015-0.0200.0040.024

-0.004-0.017-0.0210.0040.025

-0.004-0.017-0.0210.0040.025

-0.0010.0040.0030.0010.004

Y

-0.0060.0650.0590.0030.062

-0.0060.0680.0620.0030.065

-0.0060.0710.0650.0030.068

-0.0080.0740.0660.0040.070

-0.0080.0760.0670.0050.072

-0.0090.0760.0670.0050.072

0.0000.0000.0000.0000.000

z0.003-0.014-0.0110.0240.035

0.003-0.016-0.0130.0260.039

0.003-0.018-0.0150.0290.043

0.003-0.020-0.0160.0320.048

0.004-0.021-0.0170.0340.051

0.004-0.021-0.0170.0350.052

-0.001-0.018-0.0190.0120.031

ROTATIONS (degX

0.000-0.048-0.0490.0540.102

0.000-0.048-0.0490.0560.105

0.000-0.048-0.0490.0610.110

0.000-0.048-0.0490.0630.112

0.000-0.048-0.0490.0630.112

0.000-0.048-0.0490.0630.112

0.000-0.003-0.0030.0060.009

Y

0.011-0.053-0.0420.0940.136

0.011-0.053-0.0420.0970.139

0.011-0.053-0.0420.1010.143

0.011-0.053-0.0420.1060.148

0.011-0.053-0.0420.1060.148

0.011-0.053-0.0420.1070.150

0.003-0.099-0.0960.0010.097

)z0.038-0.094-0.0570.0300.087

0.040-0.094-0.0550.0320.086

0.048-0.094-0.0460.0360.082

0.054-0.094-0.0410.0390.079

0.054-0.094-0.0410.0390.079

0.055-0.094-0:0390.0390.079

0.0000.0230.0220.0030.026


Loadcombination








TRANSLATIONS CX

-0.0010.0050.0050.0010.005

-0.0010.0030.0020.0010.002

-0.0010.0000.0000.0000.001

-0.001-0.010-0.0110.0020.012

0.000-0.019-0.0190.0040.023

0.000-0.034-0.0340.0080.042

-0.001-0.013-0.0140.0000.014

Y

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0000.0000.0000.000

0.0000.0020.0020.0000.002

in

-0-0-000

-0-0-00

)2

.001

.018

.019

.012

.031

.001

.019

.020

.0110.031

-0.001-0.019-000

-0-0

.020

.011

.030

.001

.020-0.02100

0-0-000

0-0-000

0-0•0

.007

.028

.000

.021

.022

.005

.027

.000

.023

.023

.007

.030

.000

.016

.0160.0010.016

ROTATIONS (degX

0.000-0.003•0.0030.0060.009

0.000-0.003-0.0030.0070.010

0.000-0.003-0.0030.0080.010

0.001-0.003-0.0020.0090.011

0.001-0.003-0.0020.0090.012

0.001-0.003-0.0020.0090.012

-0.001-0.042-0.0430.0020.045

Y

0.003-0.099-0.0960.0010.097

• 0.003-0.099-0.0960.0010.097

0.003-0.099-0.0960.0010.097

0.003-0.099-0.0960.0010.097

0.002-0.099-0.0960.0010.097

0.002-0.099-0.0960.0010.097

0.0060.0760.0820.0040.087

)Z0.0000.0230.0220.0030.026

0.0000.0230.0220.0030.026

0.0000.0230.0220.0040.026

0.0000.0230.0220.0050.027

0.0000.0230.0220.0060.028

0.0000.0230.0220.0060.028

-0.003-0.007-0.0100.0030.012

Ar02E-R2.OUT 3-4-97 10:30a Page 15 of 32






Pointname

8

Loadcombination


TRANSLATIONSX

0.0000.0000.0000.0000.000

Y

0.0000.0000.0000.0000.000

(in )

z0.0000.0000.0000.0000.000

ROTATIONS (degX

0.0000.0000.0000.0000.000

Y

0.0000.0000.0000.0000.000

)2

0.0000.0000.0000.0000.000

S U P P O R T

Point/ Connect/ Load L O C A LSupp. ID Type Combi nat i on 0 i rn Force Deform

G L O B A LD i m Force Deform

A02A02 1 GuideStiff :RIGID

A09A09 1 GuideStiff :RIGID

B01B01 1 GuideStiff :RIGI0

GR

T1

GR+T1

RESPONSE

TOTAL

GR

T1

GR*T1

RESPONSE

TOTAL

GR

T1

downleft

upleft

upleft

downleft

downleft

downrght

downleft

downleft

downleft

downleft

downleft

downrght

216

216

11601388

11601388

361

461

822

633347

1455347

67048

270948

0.0000.001

0.0020.013

0.0020.014

0.0000.000

0.0020.014

0.0000.001

0.0000.026

0.0000.024

0.0000.000

0.0000.024

0.0000.000

0.0000.020

XYZ

XY

zXYzXYZ

XYZ

XYZ

XYZ

XYZ

XYZ

XYZ

XYZ

XYZ

-216

216

13881160

13881160

-361

-461

-822

347633

3471455

48-670

•48-2709

-0.0010.0000.000

-0.0130.002-0.016

-0.0140.002•0.016

0.0000.0000.001

0.0140.0020.016

-0.0010.000-0.001

0.0260.000-0.033

0.0240.000-0.034

0.0000.0000.012

0.0240.0000.046

0.0000.000-0.001

-0.0200.000-0.004

AY02E-R2.OUT 3-4-97 10:30a Page 16 of 32


FLUOR DANIEL NORTHUEST, INC.AutoPlPE+4.60 RESULT PAGE 19



S U P P O R T FO. R C E S

Point/ Connect/ Load L O C A L G L O B A ISupp. ID Type Combination D im Force Deform D im Force

R E S T R A I N T R E A C T I O N S


FORCES (Ib )X Y 2 Result

MOMENTS (ft-lb )X Y Z Result

11 1 Y - StopStiff :RIGI0

GR+T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

downrght

downleft

downleft

down

up

down

down

down

3379

714284

4093284

3248

2031

1217

1161

2378

0.0000.020

0.0000.000

0.0000.020

0.000

0.000

0.000

0.000

0.000

XYzXYz

XYz

XYz

XYz

XY

zXY

zXY

z

-3379

284714

2844093

-3248

2031

-1217

1161

2378

-0.0200.000

-0.005

0.0000.0000.011

0.0200.0000.016

-0.0010.000

-0.001

0.0050.000

-0.018

0.0050.000

-0.019

0.0010.0000.012

0.0050.0000.031

AnchorGRT1GR+T1RESPONSETOTAL

GuideGRT1GR+T1RESPONSETOTAL



AnchorGRT1GR+T1RESPONSETOTAL

Y - StopGRT1GR+T1RESPONSETOTAL

-33-158-190

133323

000

13881388

0. 0

0347347

48-48

0284284

-23147125102227

00000

-67-262-330221551

-216216

011601160

-361-461-822633

1455

-670-2709-3379

7144093

-2431108865

86950

-32482031

-121711612378

-1-74-75477552

00000

00000

00000

13144157125282

00000

75315388542844

216216

018091809

361461822722

1496

67227103379

7684102

2451127888183

1017

32482031121711612378

2-99-97147244

00

• 000

00000

00000

-103553449

94543

00000

22426

026

00000

00000

00000

14-78-6353

117

00000

637434588

00000

00000

00000

40-427-387

68456

00000

6108109154261

00000

00000

00000

112703596128719

00000

AY02E-R2.OUT 3-4-97 10:30a Page 17 of 32

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT0 3 / 0 4 / 9 7 JUMPER ASSEMBLY STRESS ANALYSIS


AY02E-R2 PROJECT W-320, 241-AY-02E SLUICE PIT0 3 / 0 4 / 9 7 JUMPER ASSEMBLY STRESS ANALYSIS

FLUOR DANIEL NORTHUEST, INC.Au toP IPE+4 .60 RESULT PAGE 22

R E S T R A I N T R E A C T I O N S L O C A L F O R C E S M O M E N T S

Pointname

8

Loadcombination

AnchorGRT1GR4T1RESPONSETOTAL

X

85865

580645

FORCESY

-10786852

121

( I b2

-12-70-82533615

)Result

18120125789899


6-32-27-2350

Y

-4-46-492373

Z

7-45-383270

Result

10726846

113

Point Load

name combination

FORCES (lb

Y 2

MOMENTS (ft-lb >

Y Z Result

*** Segment A begin '




GRTlGR+T1RESPONSETOTAL

GRTlGR+T1RESPONSETOTAL



67262330221551

-81262182217399

-81262182218399

-81262181218399

-6113372

486558

-1-74-75471546

-1• 7 4-75471546

17475

477552

17475

473549

17475

471547

-1-74-75471547

59-238-178

181360

-90262172218390

-98262164218382

33158190133323

33158190123313

33158190120310

-33-158-190

120310

-33-158-190

120310

33158190120310

33158190120310

75315388542844

87315273535747

87315273533745

87315273533745

91315270533733

96315267533740

103315262533735

-2-24-26

026

• 2-24• 2 6

026

-2-24-26

026

-2-24-26

026

. - 7-39-47

754

-15-62-7733

110

-15-62-7733

110

-6-37-434588

225

1217

48

128

20

-4-9

-137

20

-9-27-362459

9283740

77

2410312897

225

-29997

147. 244

-2807828

106

-277759

85

2-77-75

681

-6-34-4084

123

27-35

-97988

71

-161-8933

122

6108109154261

4848331

111

581811291

58180

988

13587187

147

32

778695

161

77201174108279

AY02E-R2.OUT 3-4-97 10:30a Page 18 of 32

AY02E-R203/04/97

Point

PROJECTJUMPER

L

Load

W-320, 241-AY-02E SLUICEASSEMBLY STRESS ANALYSIS

0 C A L F 0 R C

FORCES ( I bname combination X

A02 +

A03 N

A03 M

A03 F

A03A

A038

A04 -








8-86-7846

125

8-86-7846

124

9768534

119

4194198

70269

419419867

266

419419866

265

419419866

265

Y

8923

11218

130

4194198

72270

-2198196

78273

73239613

108

512374

277

-4623

-231134

-5823

-351146

E S

)

PIT

£ M

2 Resu l t

4194198

72270

-87-23

-10917

126

• 8 0-23

-10315

118

-8867845

123

-8867833

112

-886782098

-886782098

90213241

88325

87213240

87323

80213237

86321

74213234

84315

52213226

75298

47213214

70284

59213216

70286


O M E N T S

RESULT


-1817-11414

-1817-11414

17-77-60

2383

18-132-114

19133

18-132-114

19133

18-132-114

19133

18-132-114

19133

Y

2288

11095

205

59-121

-622284

25-105

-818

88

21257278

34312

11365376

24401

6427433

47. 480

0486487

60547

Z

72-117

-452469

-22•117-140

85225

-23-198-221

57279

-21-28-50

1464

-100-57

-15725

182

-101-74

•17525

200

-65-90

-15520

175

PAGE 23

Result

7714811999

216

6516915389

240

38237243

62304

35290304

42345

102393423

40460

103453481

57537

68512523

66589

AY02E-R203/04/97

Point

PROJECTJUMPER

L

Load

U-320, 241-AY-02E SLUICEASSEMBLY STRESS ANALYSIS

0 C A L F 0 R c


A04 +

A05 -

A05 +

A06 -

A06 +

A07 N

A07 M




GR .T1GR+T1RESPONSETOTAL




419419867

265

419419867

265

419419867

266

419419867

266

419419869

267

419419869

268

-219819644

239

Y

-9323

-701989

-9523

-721991

-10723

-8422

106

-10823

-8522

107

-14323

-12029

149

-885781492

-9-76-85

57141

E S

)Re

• 88678

886

-88678

886

-88678

684

-88678

684

-886781391

143-2312030

150

150-2312731

158

PIT

i M

u l t

93213224

70293

95213225

70293

107213229

71298

108213230

71299

143213245

76320

143213245

77320

150213248

78320


O M E N T S

RESULT


18-132-114

19133

18-132-114

19.133

18-132-114

19133

18-132-114

19133

18-132-114

19133

18-132-114

19134

1-163-162

11174

Y

0486487

60547

0494494

61554

0494494

61554

-1502501

61562

-1502501

61562

-47-93

-14117

158

619242044

2

-65-90

-15520

175

-57-92

-14918

167

-57-92

-14918

167

-47-94

-14117

158

-47-94

-14117

158

1-502-501

61562

4-504-500

49549

PAGE 24

Result

68512523

66589

60520528

66594

60520528

66594

51527533

66599

51527533

66599

50528533

66599

7530526

54577

AY02E-R2.0UT 3-4-97 10:30a Page 19 of 32

AY02E-R2 PROJECT W-320, 241-AY-02E03/04/97 JUMPER ASSEMBLY

L 0 C

Po in t Loadname combinat ion

A07 F GRT1GR+T1RESPONSETOTAL

A08 GRT1GR+T1RESPONSETOTAL

A09 - GRT1GR+T1RESPONSETOTAL

A09 + GRT1GR+T1RESPONSETOTAL

A10 GRT1GR+T1RESPONSETOTAL


* * * Segment A end

* * * Segment B beg in


A L

SLUICE PITSTRESS ANALYSIS

F 0 R C

FORCES < l bK

-886781896

-886781997

-886781997

-886782199

-8867834

112

-8867834

112

* • •

* * *

1314415732

190

Y

-15723

-13432

166

-15823

-13533

168

-16323

-14033

173

198484682636

1318

190484675635

1309

129484613635

1248

-391-1601-1992

7092701

E S

)2 R

-4-194-198

70268

-4•194-198

70269

-4-194-198

70269

-4-194-198277476

-4•194-198274473

-4-194-198274473

•25-100-125269393

a M

esult

157213252

79330

159213253

80332

16321325580

334

198529714694

1404

191529708692

1396

129529649692

1339

39216112002

7592736

FLUOR OANIEL NORTHWEST, INC.AutoPIPE+4.60

O M E N T S

RESULT


27-105

-781593

27-105

-781593

27-105

-781593

27-105

-781593

27-105

-781593

27-105

-781593

210210438

142

Y

-7448441

36477

-842942135

457

-9365356

43399

-936535643

399

-12243231155386

-14153140280419

-21186166263429

Z

5812117820

198

7311819222

213

12611123729

266

126111237

29266

• 4-194-190386576

-69-417-486678

1164

-241-611-852724

1576

PAGE 25

Result

64476482

44525

78457469

44513

130396435

54488

130396435

54488

30328309416700

76457512733

1241

242647874771

1640


Pointname

BOO

B01 -

B01 +

B02

B03 N

B03 M

B03 F

L

Load

U-320, 241-AY-02EASSEMBLY

O C A L

SLUICSTRESS ANALYSIS

F O R C

FORCES < lbcombination X




•GRT1 'GR*T1RESPONSETOTAL


GR-T1GR+T1RESPONSETOTAL


1314415723

180

1314415723

180

1314415722

179

1314415720

177

14146160

18178

141887

102843

1070

17911081287

501338

Y

-452-1601-2053

7102763

-459-1601-2060

7102770

21111081319

541373

20611081314

531367

19311081300

521352

122680802

33835

13144157

17175

E S

)

PIT

& M

Z Resu l t

-25-100-125272396

-25-100-125272396

23•147-125

26150

23-147-125

24148

23-147-125

22147

23-147-125

21145

-2314712520

145

45316112063

7612797

46016112070

7612804

21211271334

641393

20811271329

621386

19411271316

591372

18811271309

581365

18111271303

571357


O M E N T S



210210438

142

210210438

142

210210438

142

210210438

142

2102104.38

142

-11-9

-21133153

-11-158-169

154323

Y

-32141109172281

-487830

159189

-487830

159189

-40.29-11157168

-23-85

-107154261

-9-184-193

86279

-917616636

203

Z

-4712578

400479

24011341374

851459

24011341374

851459

171768940

781017

18-85-67

75142

-47-455-502

80581

69566635

79714

PAGE 26

Result

57214170437573

24511411378184

1478

24511411378

1841478

176776946179

1041

29157164175329

49491538177663

71613677177809

AY02E-R2.OUT 3-4-97 10:30a Page 20 of 32

PaeeB

-83


Pointname

804

B05 -

BOS +

B06

B07 -

B07 +

B08 -

©

L

Load

U-320, 241-AY-02E SLUICEASSEMBLY STRESS ANALYSIS

0 C A L F 0 R C

FORCES ( l bcombination X








17911081287

501337

16611081274

501324

13911081247

431290

10311081211

401251

8511081193

401234

5011081158

371195

4411081152

371189

Y

1314415717

174

13144157

17174

1314415721

179

1314415722

179

1314415722

179

1314415722

179

1314415722

179

E S

PIT

& M

Result

-23147125

19144

-23147125

19144

-2314712512

136

-23147125

10135

-2314712510

135

-23147125

13138

-2314712513

138

18111271303

561356

16811271290

561343

14211271263

501310

10611271227

471271

8911271210

471254

5711271176

451216

5211271170

451210

FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60

O M E N T S

RESULT


-11-158-169

154323

-11-158•169

154323

-11-158-169

154323

•11-158-169

154323

-11-158-169

154323

-11-158-169

154323

-11-158-169

154323

Y

-917616736

203

-2628726038

299

-2628726038

299

•7559952445

569

-97746649

48697

-97746649

48697

-105798693

48740

Z

69565634

79714

59457516

71588

59457516

71588

3015318327

210

179

268

34

179

268

34

12-41-29

735

PAGE 27

Result

71613677177809

66562602174734

66562602174734

81638581162687

99763671161769

99763671161769

107814713161808

AY02E-R203/04/97

Point

PROJECTJUMPER

L

Load

W-320, 241-AY-02EASSEMBLY

O C A L

SLUICESTRESS ANALYSIS

F O R C


B08 +

B09 N

809 M

B09 F

B10 N

B10 M

BIO F




GRT1 'GR+T1 •RESPONSETOTAL




-4811081059

311091

-5511081053

321085

-60888828

39867

-2314712553

177

-2314712553

178

38-679-641

50691

81-1108-1027

341061

Y

1314415795

253

-2314712551

176

27-679-652

48700

-6811081040

331073

72-1108-1036

341069

70-888-817

39857

13144157100258

E S

PIT

& M

Z Resu l t

-2314712550

175

-13-144-157

97254

-13-144-157

99256

13144157100257

-13-144-157

100257

-13-144-157

100257

23-147-125

54179

5511271078

1121133

6111271072

1141128

6711271066

1161143

7311271059

1171117

7711271055

1181114

8111271051

1191130

8511271046

1191106

FLUOR DANIELAutoPIPE*4.60

O M E N T S



-11•158-169

85254

-11-158-169

85254

-5-198-203

64267

1-165-164

36200

1-165-164

36200

0-94-9426

120

-341

2122

Y

-3979875835

794

8-93-85

. 23109

9-54

3943

-5-86-9136

127

252531366

-3119117

. 15131

22-310-288

16304

Z

12-41-295382

48-851-803

23827

47-741-694

19713

-27371343

20364

11-108

-9822

119

-916715821

179

-5117112

16128

PAGE 28

Result

43814778107838

50870825

91872

48767723

77762

28415391

55434

1120419844

242

9226218

37252

23331309

31330

AY02E-R2.OUT 3-4-97 10:30a Page 21 of 32

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE03/04 /97 JUMPER ASSEMBLY STRESS ANALYSIS

L 0

Po in t Loadname combinat ion

B10A GRT1GR+T1RESPONSETOTAL

810B GRT1GR+T1RESPONSETOTAL

811 N GR• T1

GR+T1RESPONSETOTAL

B11 M GRT1GR+T1RESPONSETOTAL

B11 F GRT1GR+T1RESPONSETOTAL


* * * Segment B end

C A L F O R C

FORCES ( I bX

226-1108

-882.56

937

226-1108

-88283

964

230-1108

-87884

962

176-680-504118621

13144157125282

13144157125282

• • •

* * * Segment C beg in * * *


000

4343

Y

13144157108266

13144157123280

13146159124283

-15888772894

823

-2431108865

86950

-2431108865

86950

930

9345

138

E S

j

PIT

& M

2 Resul t

23-147-125

75200

23-147-125

100224

23•147-125

101225

23-147-125

102226

23-147-125

102227

23-147-125102227

000

9696

2281127904143994

2281127904179

1029

2311127901180

1027

2381127894182

1055

2451127888183

1017

2451127888183

1017

930

93114173


O M E N T S



-341

2122

-341

2122

-330

2121

22-269-248

29277

40-427-387

68456

40-427-387

68456

000

5151

Y

24-320-296

14311

24-326-301

14315

29-354-325

22347

30-305-274

52326

14-78-6353

116

14-78-6353

117

000

6969

2

-6107101

18119

-71029520

115

-9746537

102

20-139•119

76194

103-550-447

94542

103-553-449

94543

660

6644

110

PAGE 29

Result

25338313

31334

26341316

32336

30362331

47362

43430388

96470

111701595128717

112703596128719

660

6697

140

AY02E-R203/04/97

Point

PROJECT W-320, 241-AY-02E SLUICEJUMPER.ASSEMBLY STRESS ANALYSIS

L 0


C01 N

C01 M

C01 F

C02 N

. C02 M

C02 F

C03




GR .T1GR+T1RESPONSETOTAL

GRT1GR<-T1RESPONSETOTAL


GRT1GRtT1RESPONSETOTAL

C A L F O R C

FORCES ( I bX

000

4343

640

6438

102

900

9045

134

890

8944

133

620

6237

100

000

4242

000

2121

Y

910

9145

136

640

6449

113

000

9595

000

4242

-620

-6248

111

870

8744

132

000

2323

E S

Re

000

9595

000

9595

000

4242

000

9595

000

9494

000

9494

00 •

04848

PIT

I M

suit

910

91114172

910

91113179

900

90113170

890

89113169

880

88112176

870

87112167

000

5757


O M E N T S

RESULT

MOMENTS ( f t - l b >X

000

5151

000

1212

000

2525

000

2525

000

1111

00000

o0000

Y

000

4141

000

5454

-240

-242246

000

1616

000

1818

000

1010

00022

2

390

393472

280

282856

000

3535

•240

-241539

-190

-191130

9095

14

20213

PAGE 30

Result

390

397498

280

286279

240

244963

240

243449

190

192437

909

1117

20223

AY02E-R2.OUT 3-4-97 10:30a Page 22 of 32

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT0 3 / 0 4 / 9 7 JUMPER ASSEMBLY STRESS ANALYSIS


AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT03 /04 /97 JUMPER ASSEMBLY STRESS ANALYSIS


L O C A L F O R C E S M O M E N T S i E A M F O R C E S S M O M E N T S


FORCES ( I bY 2

MOMENTS ( f t - l b )Y Z Result

Beam Load P o i n t10 comb ina t i on name

FORCES ( I b )A x i a l Y-Shear Z-Shear

MOMENTS ( f t - l b )T o r s i o n Y -1 Mom. 2-2 Horn.


Segment C end

000

2121

000

2323

000

4848

000

5757

GR

T1

GR*T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

2121212121

2323232323

3434343434

4545454545

3234324820312031120312171160116023632377

3363334615461546181718001582158233993382

37373710

55-55

379237641170117049624934

27102566

55-55

276426211045104538103666

0000001111

-44

-194194

-198198270270468468

20-20-9494

-7474

509509583583

20-20-94

94-74

74479479553553

0000003333

-88

86-8678

•785353

131131

-2121

-5858

-7979

101101180180

-2121

-5858

-7979

467467546546

0000000000

-1414

153-153

140-140280280419419

7-7

-3333

-262620204747

7-7

-3333

-262620204747

0000001010

-6972

-417390

-486462677662

11631124

169-159221

-192390

-3501384133717741688

159-112

192-65350

-1771337

5451688

722

0000000000

27-28

-10545

-7817159693

113

26-16

-147100

-12184

122365243449

1629

-100-107

-84-78365

1390449

1468

AY02E-R2.OUT 3-4-97 10:30a Page 23 of 32





B E A M F O R C E S S M O M E N T S ASME B31.3C (1992) CODE COMPLIANCE


FORCES (Ib )Axial Y-Shear Z-Shear

MOMENTS <ft-lb )Torsion Y-Y Mom. Z-Z Mom.

(Moments in ft-lb )Point Load In-Pl. Out-Pl. Torsionname combination Moment Moment Moment

S.I.FIn Out

(Stress in psi )Eq. Load Code Codeno. type Stress Allow.

W to

GR

T1

GR*T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

GR

T1

GR+T1

RESPONSE

TOTAL

5656565656

6767676767

5A025A025A025A025A02

6868686868

2574-2452

78-78

2652•253050550531573035

203000

2030202022320

28-41-171712-241597159716091621

14-1490-90103--103787787890890

-88

-5858-6565729729795795

00000033333333

115

-4242-3047883855

-11078-7878-685252130121

-1212-7070-8282269269350350

00000035353535

-111-1002222

-44

-1414-181820203838

5-51414-8824243232

0000000000

00-33-221133

006-65-54499

115-934090155-35521097071 1 2 •

000000

1070

1070

23

-2621-2424643028

54

-1446-84924233273

-172

-15-93-32-901386.87

1417177

000000

1030

1030

132

-123-89-111-871922129109

-4-91295512546834020986

Segment A begin

A00 MaxGR +ColdSus.Sus.Sus.

A01A MaxGR +ColdSus.Sus.Sus.

A01B MaxGR +ColdSus.Sus.Sus.

A01 N- MaxGR +ColdSus.Sus.Sus.

A01 N+ MaxGR +ColdSus.Sus.Sus.

A01 H MaxGR •ColdSus.Sus.Sus.

Max Pto T1+ R1+ R2+ R3

>Max Pto T1+ R1* R2+ R3




?Max Pto T1t R1+ R2* R3

299564

139

28012228

2776210

277428

277428

63437734

63727645

227314

487511

497510

497510

927181031

24

24

24

24

24

39

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

2.562.562.562.562.56

2.562.562.562.562.56

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

>.13>.132.132.132.13

2.132.132.132.132.13

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a>(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

HOOPSUSTDISPOCCOCCOCC






48442094404237221042779

48442081312213620852218

48442086303210820912139

48442087302210420922128

48442113741215321232208

48442184412258122033164

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2.OUT 3-4-97 10:30a Page 24 of 32


FLUOR DANIEL NORTHUEST, INC. 'AutoPIPE+4.60 RESULT PAGE 35



ASME B31.3c. (1992) CODE COMPLIANCE(Moments in ft-lb ) (Stress in psi )


A01

A01

A02

A03

A03

A03

A03

F-

F-t

N-

N+

M

F-

Max PGR +ColdSus.Sus.Sus.






Max FGR +ColdSus.Sus.Sus.

Max Pto T1+ R1+ R2• R3

Max Pto T1* R1• R2+ R3

Max Pto T1• R1+ R2* R3

Max Pto T1• R1+ R2+ R3


Max Pto T1* R1+ R2+ R3

Max Pto T1* R1+ R2• R3

2735593199

2735593199

72117828688

59121697175

221175624101

23198512473

21257412248

928241046

928241046

22885724109

221175624101

59121697175

25105303028

2128262634

62

62

17

17

17

77

132

2.562.562.562.562.56

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.951.951.951.951.95

1.951.951.951.951.95

1.951.951.951.951.95

2.132.132.132.132.13

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.631.631.631.631.63

1.631.631.631.631.63

1.631.631.631.631.63

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)








48442404468282724653371

48442200287237022242591

48442427551260324972855

48442368631253624252751

484425711127289526653315

484423551607261723952826

484423221946251123582598

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211


Pointname

A03 F*

A03A

A03B

A04

A05

A06

A07 II-

Lcadcombination



Max ?GR +ColdSus.Sus.Sus.





Max Pto T1• R1* R2• R3


MaxGR +ColdSus.Sus.Sus.


Max Pto T1* R1* R2• R3

>

Max Pto T1* R1* R2• R3

Max Pto T1+ R1• R2• R3

In-Pl.Moment

2128262634

10057104120113

10174107122

• 1 1 5

6590727978

5792636970

4794545760

4794545760

Out-Pl.Moment

21257412248

11365191134

642725749

048627254

049427255

150228255

150228255

TorsionMoment

132

132

132

132

132

132

132

S.IIn

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

1.00.00.00.00.00

.FOJt

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001-.001.001.001.00

1.001.001.001.001.00

Eq.no.

(3a>(18)(17)(18)(18)(18)

(3a>(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

Loadtype


HOOPSUSTOISPOCCOCCOCC






CodeStress

484422081084230622302354

484425471466259226432673

484425531692265026522770

484423801911251124442647

484423401940247223962608

484422931969242723402561

484422921969242623392560

CodeAllow.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2.OUT 3-4-97 10:30a Page 25 of 32


Pointname

A07 N+

A07 M

A07 F-

A07 F+

A08

A09

A10 -

<

Loadcombination



Max PGR •ColdSus.sus.Sus.

Max PGR *ColdSus.Sus.Sus.






Max Pto T1• R1• R2+ R3



Max Pto T1• R1* R2+ R3


PIT FLUOR DANIELAutoPIPF.

ASME 831.3c (1992) CODE COMPLIANCE(Moments in

In-Pl.Moment

150228255

450430647

744834930

58121666972

73118818887

126111133152140

419425517297

Dut-Pl.Moment

4793545760

61912724

58120666972

744834930

8429371027

' 9365471229

122437415154

AY02E-R2.

ft-lbTorsionMoment

132

163

106

105

105

105

105

S.I FIn Out

1.951.951.951.951.95

1.951.951.951.951.95

1.951.951.951.951.95

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.63

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

1.001.001.00'1.001.00

1.001.001.001.001.00

OUT 3-4-97 10:30

+4.60

(StressEq.no.

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

a

Loadtype









in psiCodestress

484424343736269325102953

484421263725236721412549

484425213370278426132767

484423441777248124002476

484424201706256424912537

427929822753333432153197

427919382284430520604915

PAGE 37

)Code

Allow.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEM8LY STRESS ANALYSIS

Point Loadname

A10

2

***

***

3

BOO

BOO

B01

combination

+ Max PGR +ColdSus.Sus.Sus.


Segment

Segment


- Max PGR +ColdSus.Sus.Sus.

+ Max PGR +ColdSus.Sus.Sus.

- Max PGR +ColdSus.Sus.Sus.

Max Pto T1• R1+ R2• R3


A end

B begi


Max Pto 11+ RI+ R2+ R3


Max Pto 11+ R1+ R2+ R3


ASHE B31.3C (1992) CODE COMPLIANCE(Moments in

In-Pl.Moment

419425517297

6941750899585

• **

n ***

241611712297787

4712531063348

4712531063348

2401134279290297

Out-Pl.Moment

122437415154

1415313820264

2118613726256

321419040194

321419040194

48788060203

Pa


S.IIn

.00105 1.00

105

102

102

102

102

ne 26 of

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

12

.FOut

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

(StressEq-no.

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

Loadtype








in psiCodeStress

201393158979934991

201394280

10269481047

2013974114

10639841083

2013940389899431002

427923431491480525035475

427940627943452645325575

PAGE 38

)Code

Allow.

160002000030000266002660026600

160002000030000266002660026600

160002000030000266002660026600

160002000030000266002660026600

133601670025050222112221122211

133601670025050222112221122211


Pointname

B01 +

B02

B03 N-

B03 N+

B03 M

B03 F-

B03 Ft

Pase

B-89H

NF-2475. B

Loadcomb

Max FGR tColdSus.Sus.Sus.

Max FGR tColdSus.Sus.Sus.

MaxGR tColdSus.Sus.Sus.


MaxGR *ColdSus.Sus.Sus.


MaxGR tColdSus.sus.Sus.

nation

Max Pto T1t R1t R2t R3


Max Pto T1t R1+ R2t R3

>Max Pto T1t R1+ R2t R3



Max Pto T1+ R1+ R2t R3

FLUOR DANIELAutoPIPEt4.60


In-Pl.Moment

2401134279290297

171768204207232

1885442288

1885442288

474557660120

6956610086140

6956610086140

Out-Pl.Moment

48788060203

40296552195

23843232176

23853232176

. 9184181594

9176161245

9176161245

ft-lb )Torsion S.IMoment In

1.00102 1.00

1.001.001.00

1.00102 1.00

1.001.001.00

1.00102 1.00

1.001.001.00

1.95102 1.95

1.951.951.95

1.959 1.95

1.951.951.95

158

158

.95

.95

.95

.95

.95

.00

.00

.00

.001.00

.FOut

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.631.631.631.631.63

1.631.631.631.631.63

1.631.631.631.631.63

1.001.001.001.001.00

(StressEq.no.

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

Loadtype









in psiCodeStress

427940627943452645325575

484429112895310830883708

48442205587233922533015

48442310889256923923677

484425123498279026413465

484427164299300828813438

484424002288255024842782

PAGE 39

CodeAllow.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2 PROJECT U-320, 241-AY-O2E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS

Pointname

B04

B05

B06

807

B08 -

B08 ^

B09 N

Load

FLUOR DANIEL NORTHWEST, INC.AutoPIPE

ASME 831.3c (1992) CODE COMPLIANCE(Moments in

In-Pl.combination Moment








Max Pto T1+ R1* R2t R3



>Max Pto T1t R1t R2* R3

>Max Pto T1t R1t R2+ R3



6956510086140

594578973122

30153443853

179212122

105798139132127

39798616454

893141030

Out-Pl.Moment

9176161245

26287403262

7559910593102

97746132122121

1241141518

1241181665

48851606162


1158 1

11

S.IIn

.00

.00

.00

.001.00

1.00158 1.00

.001.00

158-

158

158

158

158

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.34

.34

.34

.34

.34

.34

.34

.34

.34

.34

.00

.00

.00

.00

.00

,FOut

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.001.001.001.001.00

1.451.451.451.451.45

.45

.45

.45

.45

.45

.00

.001.001.001.00

+4.60

(StressEq.no.

<3a)(18)(17)(18)(18)(18)

(3a)

(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

Loadtype







HOOPSUSTDI.SPOCCOCCOCC

RESULT

in psiCodeStress

484424002287255024842782

484423762100253424512722

484424522381261125462623

484425402848270626582654

484427474032296229172891

484423334032247624902713

484422973249236523642423

PAGE 40

)Code

Allow.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2.OUT 3-4-97 10:30a Page 27 of 32

AY02E-R2 PROJECT U-320. 241-AY-02E SLUICE03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS

Pointname

B09 N+

B09 M

B09 F-

B09 F+

B10 N-

B10 N+

B10 H

h

Loadcombination


Max PGR *ColdSus.Sus.Sus.





Max FGR •ColdSus.Sus.Sus.

Max Pto Tl• R1• R2* R3

Max Pto Tl+ Rl* R2+ R3

Max Pto T1• R1• R2* R3

Max Pto Tl+ R1+ R2+ R3


Max Pto T1+ R1• R2+ R3


PIT FLUOR DANIELAutoPIPE+4.60


In-Pl.Moment

48851606162

47741595658

27.371433933

27371433933

11108282317

11108282317

9167252019

Dut-Pl.Moment

893141030

95131148

5867

' 741

5867741

2523214

2523214

31198416

ft-lbTorsionMoment

158

198

165

165

165

165

94

S.IIn

1.951.951.951.951.95

1.951.951.951.951.95

1.951.951.951.951.95

1.001.001.001.001.00

1.001.001.001.001.00

2.562.562.562.562.56

2.562.562.562.562.56

.FOut

1.631.631.631.631.63

1.631.631.631.631.63

1.631.631.631.631.63

1.001.00.00.00.00

.00

.00

.00

.00

.00

2.132.132.132.132.13

2.132.132.132.132.13

(StressEq.no.

<3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

Loadtype









in psiCodeStress

484425166255264426462733

484425115449263225962832

484423242818247524312611

484421991548227622532374

48442117761220021762185

484421981272240823472348

484421801891237823132364

PAGE 41

)CodeAllou.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211


Pointname

810 F-

B10 F+

B10A

B10B

B11 N-

B11 «*

B11 M

Loadcombination

Max FGR *ColdSus.Sus.Sus.


MaxGR •ColdSus.Sus.Sus.


Max Pto T1+ R1* R2+ R3


Max PGR +ColdSus.Sus.sus.




Max Pto Tl* R1* R2• R3

Max Pto T1+ R1+ R2* R3

>Max Pto T1t R1* R2* R3


PIT FLUOR DANIEL NORTHUEST, INC.AutoPIPE+4.60

ASME B31.3c (1992) CODE COMPLIANCE(Moments in

In-Pl.Moment

22310.322733

511712720

6.10712823

•7

10213925

974'161245

974161245

20139293095

Dut-Pl.Moment

511712720

22310322733

24320322835

24326312935

29354443940

29354443940

30305725253


4

4

4

4

4

3

269

2;;

S.I FIn Out

.56

.56

.562.56.56

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.95

.95

.95

.95

.95

.95

.95

.95

.95

.95

.13

.13

.13

.13>.13

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.00

.63

.631.631.63.63

1.631.631.631.631.63

(StressEq.no.

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

Loadtype








RESULT

in psiCodeStress

484423423105247524092545

484421751237222922012263

484421831260223222072279

484421881274223322132292

484422111350229122632392

484423072216244223932656

484423712337270225643090

PAGE 42

)Code

Allou.

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

AY02E-R2.0UT 3-4-97 10:30a Page 28 of 32





ASME B31.3C (1992) CODE COMPLIANCE(Moments in ft-Ib ) (Stress in psi )

Point Load In-PL. Out-PL. Torsion S.I.F Eq. Load Code Codename combination Moment Moment Moment In Out no. type Stress Allow.

ASME B31.3c (1992) CODE COMPLIANCE(Moments in ft- Lb ) (Stress in psi )

point Load In-Pl. Out-PL. Torsion S.I.F Eq. Load Code Codename combination Moment Moment Moment In out no. type Stress Allow.

B11 F- Max 1GR +ColdSus.Sus.Sus.

B11 F* Max IGR +ColdSUS.Sus.SUS.

B12 Max 1GR +coldSus.Sus.

' Sus.

>Max Pto T1+ R1+ R2+ R3

Max Pto T1+ m* R2+ R3


103550118140188

103550118140188

103553118141189

1478593535

1478593535

1478593535

1.95427 1.95

1.951.951.95

1.00427 1.00

1.001.001.00

1.00427 1.00

1.001.001.00

1.631.631.631.631.63

1.001.001.001.001.00

1.001.001.001.001.00

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

HOOPSUST0ISPOCCOCCOCC



484430374342341034243853

484425652617278927702986

484425672624279227732988

133601670025050222112221122211

133601670025050222112221122211

133601670025050222112221122211

*** Segment B end '

*** Segment C begin '

B08

coi

coi

si

Max PGR + Max PCold to T1Sus. + R1Sus. + R2Sus. + R3

N- Max PGR * Max PCold to T1SUS. + R1Sus. + R2Sus. + R3

H* Max PGR + Max PCold to T1Sus. + R1Sus. + R2Sus. + R3

660959875

390606445

390606445

007569

004341

004341

(3a) HOOP1.34 1.45 (18) SUST

0 1.34 1.45 (17) DISP1.34 1.45 (18) OCC1.34 1.45 (18) OCC1.34 1.45 (18) OCC

(3a) HOOP1.00 1.00 (18) SUST

0 1.00 1.00 (17) DISP1.00 1.00 (18) OCC1.00 1.00 (18) OCC1.00 1.00 (18) OCC

(3a) HOOP2.27 1.89 (18) SUST

0 2.27 1.89 (17) DISP2.27 1.89 (18) OCC2.27 1.89 (18) OCC2.27 1.89 (18) OCC

5016 133604110 16700

0 250505064 222115115 222116460 22211

5016 ,133603313 16700

0 250504030 222114127 222114660 22211

5016 133604913 16700

0 250506529 222116756 222117472 22211

C01 M

C01 F-

C01 Ft

C02 N-

C02 N+

C02 M

C02 F-

Max PGR •ColdSus.Sus.Sus.


Max PGR +ColdSus.Sus.Sus. •




Max PGR •ColdSus.Sus.Sus.

Max Pto Tl* R1+ R2+ R3







280464933

240384028

004235

002116

240343527

190272622

90121210

006454

004235

240384028

240343527

002116

002118

001110

0

0

0

0

0

0

0

2.272.272.272.272.27

2.272.272.272.272.27

1.001.001.001.001.00

1.001.001.001.001.00

2.272.272.272.272.27

2.272.272.272.272.27

2.272.272.272.272.27

1.891.891.891.891.89

1.891.891.891.891.89

1.001.001.001.001.00

1.001.001.001.001.00

1.891.891.891.891.89

1.891.891.891.891.89

1.891.891.891.891.89

(3a>(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

<3a)(18)(17)(18)(18)(18)








50164122

0548156877446

28210

133601670025050222112221122211

5016 133603797 16700

0 250504866 222115023 222115971 22211

5016 1336016700

. 250503297 222113363 222113968 22211

5016 133602821 16700

0 250503162 222113177 222113338 22211

5016 133603797 16700

0 250504567 222114603 222114783 22211

5016 133603479 16700

0 250504038 222114009 222114587 22211

5016 133602717 16700

0 250502969 222112943 222113314 22211

AY02E-R2.OUT 3-4-97 10:30a Page 29 of 32

AY02E-R2 PROJECT W:320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS




ASME B31.3C (1992) CODE COMPLIANCE


C02 F+ Max PGR +ColdSus.Sus.Sus.

C03 Max 1GR +coldSus.Sus.Sus.

*** Segment

Max Pto T1• R1• R2• R3

s

Max Pto T1+ R1• R2 '+ R3

C end

(Moments inIn-Pl.Moment

90121210

20222

••*

Out-Pl.Moment

001110

00002

ft-lb )Torsion S.Moment In

1.000 1.00

1.001.001.00

1.000 1.00

1.001.001.00

l.FOut

1.001.001.001.001.00

1.001.001.001.001.00

(StressEq-no.

(3a)(18)

Loadtype

HOOPSUST

(17) D1SP(18)(18)(18)

(3a)(18)(17)(18)(18)(18)

OCCOCCOCC


in psiCodeStress

50162345

0245824462661

50162109

0213221292171

)Code

Allou.

133601670025050222112221122211

133601670025050222112221122211




Maximum rotations (deg)


0.0580.0760.0610.093

0.1120.150

-0.2240.246



B03 FC04A07 NC04

C02 FC04B10 N810 N




TOTALT1TOTALTOTAL

TOTALTOTALT1TOTAL


Maximum restraint m


138840936154102

ments(ft-lb)

553117456719



A02B018601

B12B12B12B12

LoadLoadLoadLoad

LoadLoadLoadLoad



RESPONSETOTALTOTALTOTAL

T1TOTALTOTALTOTAL

AY02E-R2.0UT 3-4-97 10:30a Page 30 of 32

AY026-R2 PROJECT U-320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS


AY02E-R2 PROJECT W"320, 241-AY-02E SLUICE PIT03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS

FLUOR DANIEL NORTHWEST, INC.AutoPIPE+4.60 RESULT PAGE 4i

S U M M A R Y

Maximum pipe forces Clb)


Maximum pipe moment


133827704762804

(ft-lb)

45679815761640

pointpointPointPoint


B03 FB01A09B01

B11 FB0833




TOTALT1TOTALTOTAL






Maximum occasional stress

Maximum hoop stress

Pointstress psiAllowable psiRatioLoad combination





PointStress psjAllowable psiRatioLoad combination

C01 N4913167000.29GR + Max P

B017943250500.32Cold to T1

C01 N7472222110.34Sus. + R3

B085016133600.38Max P

C01 H4913167000.29GR + Max P

B017943250500.32Cold to T1

AY02E-R2.OUT 3-4-97 10:30a Page 31 of 32

AY02E-R2 PROJECT U-320, 241-AY-02E SLUICE PIT FLUOR DANIEL NORTHWEST, INC.03/04/97 JUMPER ASSEMBLY STRESS ANALYSIS AutoPIPE+4.60 RESULT PAGE 49



PointStress psiAllowable psiRatio

C01 N7472222110.34

Load combination : sus. + R3


PointStress psiAllowable psiRatio

501613360

; 0.38Load combination : Max P

* * * The system satisfies ASHE B31.3 code requirements * •* * * for the selected options * •

AY02E-R2.OUT 3-4-97 10:30a Page 32 of 32

VERIFY AT ASSEM8L"

PLAN

( 3 2 ) - ADJUST TO CONTACTv

—/ WfTH EXST FLOOR

ELEVATION

ASSEMBLY/TN ASSEMBLY\J_y SCALE: 1 " " 1"-0"

ELEVATION

SUPPORT FRAME SUB-ASSYSCALE: 1"= I'-O"

HNF-2475, Rev. 0

•2-818413 DRAWING LIST

TO INCOfiP ECN W-320-X

TO INCORP ECN W-320-401

PARTS/MATERIAL LIST

X

2

2

2

X1

1

1

1

1

2

1

1

1

1

1

AR

2

AR

-010 ;

-020 '

-001

-002

-003

H-2-32440-1

H-2-32440-2

H-2-9018S-2

H-2-3194-2

H-2-3':97-3

H-2-90161-15

H-2-818509-1

H-M0I7I-5

MODELCMfXOM356NU

H V - 0 6 2 4 ,

SEE IIOTE 5

UE-0621

BLUE GARD

STYLE 3 7 0 0

HOME HCLAT URCOESCRIPI ION

ASSEMBLY

SUPPORT FRAME SUB-ASSEMBLY

BRACKET, PLATE 1 / 2 " 1HK

BRACKET. PLATE 1 / 2 " THK

U-BOLT. BAR 0 1 / 2 "

CONN, HOKIZ A"

CONN, VERT. 4 "

N 0 2 Z L E . MALE 2 "

KICKQFF PLATE. 2 " ROUND

GASKET 4 " TYPE I I I

L I F T I N G BA IL

JUMPER FLUSHING BLANK HEAD /

FUNNEl ASSEMBLY

OENSIIY/FLOW/TEMPERATURESENSOR tVD

BALL VALVE, 3T-3 WAY

CGB FITTING, 3 / 4 " NPT. W/FLAXPACKIMG BUSHING i : CABLE CLAMP

INSTRUMENT CA8LE

GASKET. 3" 300H RAISED FACE.1/8" THK COMPRESSED FIBER

CABLE TIE. ) 8 " LG. NWON

UATERIAL/RCKWNCE

ASTM A 36

ASTM A 36

ASTM A 36

FISHER-ROSEMOUNTMICRO-UOIJON

P B M

COMMERICAL

SEE LEGEND

GARLOCK

COWMERICAL

SHEET

1

2

2

2

1

2

3

A

5

6

7

8

9

1 0

11

12

13

14

15

16

17

18

19

2 0

21

22

23

24

25

26

27

28

29

F

1

PARTS/MATERIAL LIST [CONTINUED TO SHEET 2) '

(HftS-XX-XX) WIRING RUN NUMBER. SEE ELECTRICAL DRAWINGH-2-81899 FOR CABLE TYPE. WIRE NUMBERSAND DESTINATION.

WITH i2. HYOROSTATIC TEST AT 480 PSIC.3. JUMPER WEIGHT IS 775 LB APPROX.4. USE I!) COAT OF AMERLOCK 400 IN PLACE OF

AMERCOAT 187 PRIMER AND AMERCOAT 33, WHEREREOUIREO BY JUMPER FABRICATION SPECIFICATION.

b. VALVE SHAR BE 3"-3 WAY PBM MULT-PORT SERIES.T-PORT 180* TURN. FLOW PATTERN *5 . 3" SCHEEb 40

APPRFITTING, SST. »3" MP-H-39-8W-2/P0C0S9 ORO SUBSTITUTE.

pic CONSTRUCT^??

« • SEE PR/AT FORM

i .» t« C 0 JONES

1tfsag^

U.S. DEPARTMENT OF ENERGY

JUMPER ASSEM8LYPUMP PIT

AY-02A-U11-A-(C)W-320 TANK 241

SHQWM \^tfH-2-818501 I 2

2 PLOT SCALE; 1

4*

iBALLPORT FUNNEL SLOT

ROTATION POSITION

NOZ A

=24 z f l f t z CONN A

I CONN A ( Q

(5>- 2 9/16" RAD

BRACKETSCALE: 3" - V-0"

SCALE: t 1/2"= f - 0 "

UE-O621-1 (BROWN)JE-0621-2 (RED)

SHIELD fCUT WIRE SH E

UE-0621-4 fWHlTE>SHIELD (CUT WlRg SH SACK)

UE-0621-6 (GRAY)SHIELD (CUT WIRE SH BAO

UE-0621-8 (VlOLETI

WIRING CONNECTION DIAGRAM

HNF-2475, Rev. 0PageB-96 OHAWIHC TSACEABILITT LIST

REOUIRED

X

1

1

AR

AR

1

X1

8

S

64

4

AR

AR

Aft

1

2

3

1

1

i

2

1

2

PARl/llASH NUWSER MOuSNCLAIliRE'OESCRIPTIOM

(CONT FROM SHEET 1)

ASSEMBLY

SUPPORT FRAME SUB-ASSEMBLY

STUD BOLT, 3/4"-10UNO2A x 6" LG

STUD BOLT, 3/4"-10UNC-2A x 6 1/2" LG

MACHING SCREW. 3/4"-10UNO2Ax 3" L HEX HD

HEAVY HEX NUT. 3/4"-10UNC-2B

HEX NUT. l /2"-13UNC-2B

CHANNEL. C4 x 5.4

PLATE, 1 /2"

PLATE 1 /2" x 6" x 6"

BAR 1 /2" DIA

PIPE. 4" SCHEO 40S

PIPE. 2" SO-

EL80W. 90s

ELBOW. 90°

ELBOW, 90°

ELBOW, 45° A

eo 4os

R 4 " SCHED 40S BW

R 3 " SCHEO 40S BW

R 2 " SCHEO 40S BW

" SCHED 40S BW

ROCR ELBOW. 90" LR 4" x 3"SCHED 40S BW

CONC RDCR 3" x 2" SCHEO 40S 8W

FLANGE. 3" 300* RF WELD NECK

ECC ROCR. 1 " x 3" SCHED 40S BW

ELBOW. 90° SR 4 " SCHED 40S SW

MAT

ASTM

ASTU

A N S I

ASIM

A N S I

A S T M

A S T M

A S T M

A S T M

ASTM

ASTM

ASTM

ASTM

ASTU

ASTU

ASTM

ASTU

ASTM

ASTM

ASTM

RIAL/ftEFERENCE

A 193 CR B8 304

A 19J GR 68 304

818.2.1 CS

A 194 GR Sf 303

618.2.2 CS

A 36

A 36

A 36

A 36

A 312 GR TP 3<ML

A 312 GR TP 304L

A 403 W - S 304L

A 403 W - S 304L

A 403 WP-S 304L

A 403 WP-S 304L

A 403 WP-S 3041.

A 403 WP-S 304L

A 1B2 GR f 304L

A 403 WP-S 304L

A 403 WP-S 304L

|

1 1 12

30

31

32

33

34

l»I 36

|37

33

39

40

41

42

I 43

| 4 4

] 45

1 4647

43

49

I 50

| 5 1

|S2

| 5 3 -

F

Z

0

"• ""SEE PR/AT TOR).

JUMPER ASSEMBLYPUMP PIT

AY-02A-U11-A-(C)

•« I H-2-818501 10

PLOT SCALE: 1 - 1 2

I iI3 33s il 1

2* ?S

~2JS ;>£;3— CSss | i z%i %ii isi i; ; Sal:»?IIII l°l ill sll pf II ill Bgli

0

NORTH FOR CONT OFINSTRUMENTATION CABLES

SEE DWG H-2-818695. SK 2

INSTRUMENT AT IONACCESS SLOT

(IN COVER BLOCK)

SLUICE PIT 24I-AY-02E<H-2-643t4l

COVER BLOCKS REMOVED FOR CLAR1T

EXST \ \/T RW-352E i V .PIT~SPRAY NOZZLES

FROM VALVE PIT

ELECTRICALACCESS SLOT

ilN COVER BLOCK) -

AK DETECTOR ELEMENTLDE-102-21(H-2-64423)

VALVE ACTUATOR

-JUMPER ASSEMBLYH-2-818503(MOOIFIED)

(FROM TRANSFER BOX

- REMOTE ND22LE SEAlt'1 HOftIZ ASSV(H-2-73453-1)

SLUICE PUMP ASSEMBLYH-2-818494-2

34" RISER BELOW

" SN-2CO-M9 W/ 6" ENC-M26aaERNATE TO SLUICE "PIT C-O6C

UICE PUMP ASSEM8LY(H-2-B18494)

34" RISER 8ELOW

SECTION

SLUICE PIT241-AY-02E

1. FOR GENERAL NOTES. LEGEND AND KEY PLAN. SEE H-2-818S18.2. FOR CONTINUATION OF NEW LINES SEE H-2-818540.3. FOR CONTINUATION PF EXISTING LINES SEE H-2-64406.


I23| DRAWING LIST

• R W SCHROEOCS *&•

• • " C D J O N E S

-•• »-»-3S

388PIPING

JUMPER ARRANGEMENTSLUICE PIT AY-02EW-320 TANK 241-C-106 SLUICIN

I I I II I »l I I " ' "™

45AR11» - ER«I8 1 ^ ~

2 PLOT SCALE: 1-12 KEHCAO

a ti>

,i

ill3 S S

is

1" LUBC RW-3S2J-USFfiOM VALVE PIT

m^Vr:4- — — -K ;* c°"m"1""

HNF-2475, Rev. 0

W320-27-030

W320 Tank 241-C-106 HVAC Seal Loop

C-i

KAISER ENGINEERSHNF

CALCULATION IDENTIFICATION AND INDEXPaga /,<!,/,

This sheet shows tha status and dascription of tha attached Design Analysis sheets.

Discipline M£C/-/fiA// CA L- WO/Jah U« \J3lO I izfa &Q!fi Calculation No.

Project No. & Nama W ZIP TANfC 24-/-C-/0& V is A C $ £~A L Un &

Calculation Jtam ,

Those calculations apply to:

owg.NO. H-2~ n/&4~77Dwg. No.

Other (Study, COR)

R«v. No.

Rov. No.


I I Preliminary Calculations

Q'Finat Calculations

LJ Chock Calculations (On Calculation Datod

LJ Void Calculation (Reason Voided


This calculation vorified by independent "check" calculations?

Original end Revised Calculation Approvals:

Q No

Rav. 0Signature/Data

Rev. 1Signature/Data


Originator Q'i»HL/n*dA 3-/0-7SChecked by

Approved by

Checked AgainstApproved Vendor Data 4.ii.q*1

Design AnalysisPage No.

A X

T-D-,/cu crnct iv) JJ ,

A<!^n.4M,06/o-f,.r

CcA(cu fa. -fio-nS

HNF-2475, Rev. 0Page C-l KEH 0378.00 106/92)

CALCULATION CROSS INDE~ (Typical)

Subject Calculation No. \,l %9.t\ - ->.1^3>Q

SubjectCalculation

RevisionNo.

9&to 3

©

Supersededby

CalculationNo.

These interfacing cateulation/cprovide input to the subject ca

and if revised may require rethe subject calculator


ocumentsculation,/isionof

RevisionNO.



Calculation/Document No. .RevisionNo.

Does the outputinterface calculation/documents require

revision?

Yes NO

Has the outputinterface calculation/


Yes No

page £,J. of AJ,J'


complete.

KEH 1975.00 (12/88)

SFS No. / / j s> -f

DESIGN VERIFICATION SCREENING CRITERIA

Project/Document No. \JJ3X 0 - 2 7 - 3 0 "

When the design or design change affects hardware, formal design verification must be performed if one or moreof the following questions must be answered affirmatively (YES).

YES NO

1. Does the design or design change involved meet the established criteria to beconsidered Safety Class 1 ?

2. Does this design or design change cause or permit changes to Safety Class 1instrument or alarm setpoints outside of previously approvedoperational limits?

3. Does this design or design change significantly affect the nuclear orenvironmental safety consequences of a malfunction or failure of thestructure, system, or component?

4. Does this design or design change involve or change design that haspreviously undergone formal design verification?

Assigned Lead Engineer Dite

Responsible Discipline Manager Date

Original Design Package Distribution:

Project Manager

Design Verification Officer

Engineering Document Control

Design Change Distribution:

Attach to Engineering Change Notice

KEH-1981.00 (09/32)

HNF-2475, Rev. 0Page C-3

KAISER ENGINEERS ? a l c No W320-27- 30Revision 0

HANFORD DESIGN ANALYSIS Page No. 1 of 2

Client WHC WO/JobNo. ER4319/W320Subject HVAC Seal Loop Date 2/6/95 By AW McNichols

Checked i / i o / 1 5 By MLocation: Tank 241-C-106 Revised By

OBJECTIVE:

Determine that the weight of the overhanging seal loop will not over stress the 6 inch verticalpipe flange weld.

DESIGN INPUTS:

Criteria and Sources:

Project W320, Tank 241-C-106 Slucing, Functional Design Criteria.(WHC document No. WHC-SD-W320-FDC-001, Rev. 0)

References/Souces:

1. Drawing No. H-2-818477, Rev. 0.

2. Flowline Catalog No.92, Fittings and Flanges.

3. Piping Engineering, 3rd edition.

4. Design of Welded Structures, Blodgett.

5. ASMEB31.1,1993

6. Machinery Handbook, 24 th edition.

Method Used:

Math Cad

Assumptions:

The strength of the pipe will be 16,700 PSI.

The strength of the welds will be the same strength as the pipe material.

Two 90 degree elbows and a 3" section of 6" dia. pipe will be filled with water.

HNF-2475, Rev. 0Page C-4

KAISER ENGINEERSHANFORD

Client WHCSubject HVAC Seal Loop

Location: Tank241-C-106

DESIGN ANALYSIS

Calc. No. W320-27- 30Revision 0Page No. 2 of 2

WO/Job No. ER4319/W320Date 2/6/95 By AW McNicholsChecked 3/10/<* 5 By tJ. j u p u oRevised By

Calculations:

Determine that the bottom weld on the Pressure Relief Seal Loop 6" flange is strong enough towithstand the moment imposed bv the cantilevered seal loop piping. Ref. 1,Sh.2

Ref. 6, Pg.164 Torus

Weight of water in 180 degree return =Ww r : = —-—

Weight of water, 3" section of 6" pipe = W3 :

Ww r+W3=22.7-lb

Weight of 180 degree return = W 1 8 0 := 35 lb

Weight of 90 degree elbow = W9Q:= 17.51b

Weight of 3" of 6" dia. pipe = W 6 :=4.751b

Ref. 2, Pg. 20R:=6in r: = 3.03in

W,, = 19.572-lb

12 inW , =3.127-lb

Ref.2,Pg.2O 2x45ell.

Ref. 2, Pg. 20

Ref. 3, Pg. 9

Momentarm from 180 returnto centerline of vertical pipe=M j :=21in

Moment arm from 3" - 6" dia. pipe to centerline of vertical pipe =M 2 :=7.5in

Moment arm from 180 return (attached to vertical pipe) to centerline of vertical pipe =M 3 :=6in

Ref 1 Sh 2

For simplicity the weight of both 180's is included in M 9

Because the weight vector is small it was not included in M ^i

Moment Total = M t o t:= (M24 + M7 s ) 2 + M 92 M ,

Determine weld strength. Ref. 4, Pg. 7.4 - 6 & 7

S •=— d: = 6.345-inw 4

M,

1.442M<f -lbin

Weld line stress = 0 :=

Minimum weld size

tot

w

5 = 45.608-in

16700-

Ref. 5, Pg. 172Assume:Material

Because of the light loads column buckling will not be considered.

0.003 in weld < Normal weld size on 6" pipe, Strength OK HNF-2475, Rev. 0Page C-5

HNF-2475, Rev. 0

W3Z0-27-031

Booster Pump Restraint Analysis

D-i

KAISER ENGINEERSHANFORO

CALCULATION IDENTIFICATION AND INDEXPage

This sheet shows the status and description of the ettBched Design Analysis sheets.

Discipline 2 7 - Piti/K WOMob No. Z(H3l9/ 'fJ 3ZO Calculation No. W.32O - 2 7 - 31

Project No. Si Name U?7-P . To

Calculation Item SoO^t-C PafAj> i?efl+ro,'^ \

211-C- IOC f.lili/'/trio


Dwg. No. H -I- SlS-i

Dwg. No. H -,

Rev. No.

Rev. No. .

P..

Other (Study, CDR) ,


I } Preliminary Calculations

[ ^ final Calculations

I 1 Check Calculations (On Calculation Dated

CU Void Calculation (Reason Voided


This calculation verified by independent "check" calculations?


Jx¥yiu^_ ztehs

DesigPii

i

it

( t

fcr,<

n|Q'

I

Analysiss No.

•;/AV ft

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HNF-2475, Rev. 0Page D-l KEH 0378.00 106/92)

CALCULATION CROSS INDE/v (Typical)

Subject Calculation No. W.5Z0--27-31

SubjectCalculation

RevisionNo.

O

£>

HN

F-Page

?K

Rev.

Supercecledby

CalculationNo.

These interfacing calculation/documentsprovide input to (he subject calculation,and if revised may require revision of

the subject calculation.


H-Z-2/&50?,

K -x- ms*/3

RevisionNo.

O

D

• • - • -




»,

RevisionNo.

Docs the outputinterface calculation/documents require

revision?

Yes No

(las the outputinterface calculation/


Yes No

Page Cc of {£C

Discipline manager's signature amdate indicating evaluation

complete.

KFH 1975 nn

DESIGN VERIFICATION SCREENING CRITERIA

Project/Document No. U)3Zfl -7-1 - 31

When the design or design change affects hardware, formal design verification must be performed if one or moreof the following questions must be answered affirmatively (YES).

YES NO

1. Does the design or design change involved meet the established criteria to beconsidered Safety Class 1?

2. Does this design or design change cause or permit changes to Safety Class 1instrument or alarm setpoints outside of previously approvedoperational limits?

3. Does this design or design change significantly affect the nuclear orenvironmental safety consequences of a malfunction or failure of thestructure, system, or component?

}\ 4. Does this design or design change involve or change design that haspreviously undergone formal design verification?

Assigned Lead Engineer

Responsible Discipline Manager

Air

» Date

Original Design Package Distribution:

Project Manager

Design Verification Officer

Engineering Document Control

Design Change Distribution:

Attach to Engineering Change Notice

KEH-1981.OO (09/92:

HNF-2475, Rev. 0Page D-3

ICF Kaisar Han ford caic. NO. W320-27-031Company Revision 0


Client WHC WO/Job No. ER4319/W320Subject Booster Pump Restraint Analysis Date 2-15-95 By Rodney C. Campbell

Checked S - ^ - I S By A- J0PL.OLocation: Sluice Pit AY-02E Revised By

OBJECTIVE:

The objective of this calculation is to verify that the pump restraint system is adequate to keep the booster pump in pit AY-02Efrom overturning during a seismic event.

CRITERIA:

1. Functional Design Criteria WHC-SD-W320-FDC-001, Rev. 2.2. Standard Design Criteria 4.1, Rev. 12, Design Loads for Facilities.3. Standard Design Criteria 4.2, Rev. 0, Design and Installation of Expansion Anchors.4. W320-QAPP-001, Rev. 0, Project Specific Quality Assurance Plan.

GIVEN DATA:

1. The pit is safety class 1.2. The horizontal components of the acceleration due to an earthquake are 0.2.3. The compression strength of concrete in pit is 3000 psi.

ASSUMPTIONS:

None

METHODS:

1. Hand calculations using Mathcad.

REFERENCES:

1. Drawing H-2-818503, Rev. 0.2. Drawing H-2-818543, Rev. 0.3. Drawing H-2-818545, Rev. 0.4. AISC Manual of Steel Construction, Ninth Ed.5. Calculation W320-27-029, Rev. 0,6. Biodgett, Design of Welded Structures

CALCULATION:

E s = 29 106 psi Modulus of Elasticity for steel. Ref. 4.

F a 3 6 = 22000 psi Allowable stress in A36 steel. Ref. 4.

F = 2774- lbf Dynamic load at center of gravity of pump motor. Ref. 5.

A c c = 1.21-in2 Cross-sectional area of C3x 4.1 channel. Ref. 4.

A c h := 1.5 in2 Cross-sectional area of 3" x 112" plate. Ref. 1

D n = 26- in Diameter of hoop made from rolled plate. Ref. 1, Sht. 2.

W h = 3 i n Width of hoop made from rolled plate. Ref. 1, Sht. 2.

T h = .5 in Thickness of hoop made from rolled plate. Ref. 1 , Sht. 2.

ICF Kaiser HanfordCompany

Client WHCSubject Booster Pump Restraint Analysis

Location: Sluice Pit AY-02E

DESIGN ANALYSIS

Calc. No. W320-27-031Revision 0Page No. 2 of 5

WO/Job No. ER4319/W320Date 2-15-95 By Rodney C. CampbellChecked - i - V f S By fJRevised By

1. Verify that stress in hoop is less than allowable.

FFigure 1

The stress in the hoop was analyzed by Images 3-D and found to be within acceptable level. See appendix A.

2. Verify that stress in C3 x 4.1 channel is below the allowable.

Assume that the two channels shown are replaced by one channel of the same size, colinear with force. If one channel cancarry the load, two in the configuration shown can carry the load.

c := Formula for calculating stress in tension.A c c

a = 2292.56 -psi Calculated stress in channel.

c<F 35 = 1 The calculated stress is less than the stress allowable. The two channels can carry the seismic load.

3. Verify that welds on each end of channels can carry the load.

Calculate the required size of the fillet weld holding the plates on each end.

Assume that the two channels shown are replaced by one channel of the same size, colinear with force. If the welds of onechannel can carry the load, the welds in the configuration shown can carry the load.

to := .1875 in Size of fillet weld. Ref. 1, Sht 2.

1 = 3 in + 2 1.41- in Conservative length of weld. Weld all around C3 x 4.1 channel.

t = 9600- psi Allowable shear stress. Ref. 6, Chapter 7, Table 6.

ft,-l ft = 476.63.i5_f

' 1 * in

Required size of fillet weld to carry load in tension. Ref. 6, Chapter 7.

Calculated size of the fillet weld required to carry the load. HNF-2475, Rev. 0PageD-5


Client WHCSubject Booster Pump Restraint Analysis


DESIGN ANALYSIS


WO/Job No. ER4319/W320Date 2-15-95 By Rodney C. CampbellChecked j - < ) - ^ s By »1Revised By

<o r < » = 1 This weld is strong enough to carry the maximum load.

The welds on each end of the channels are strong enough to carry the load imposed during a seismic event.

4. Verify that the weld holding item 46 (bar) to the plate attached on the end of the channels is adequate to carry the load.

Calculate the required size of the fillet weld holding the bar to the plate.

a := .1875- in Size of fillet weld. Ref. 1, Sht 2.

1 = 2 3 in Conservative length of weld. Weld all around bar.

% = 9600 psi . Allowable shear stress. Ref. 6, Chapter 7, Table 6.

tt:-l ft = 4*2.33 i f

I in

a r ' i Required size of fillet weld to carry load in tension. Ref. 6, Chapter 7.

co r = 0.04S2 • in Calculated size of the fillet weld required to carry the load,

to r<<o = 1 This weld is strong enough to carry the maximum load.

The weld attaching the bar to the plate is strong enough to carry the load imposed during a saismic event.

5. Verify that the pin will not shear the bar during a seismic event.

A = 2 i n - T n Area of plate carrying load.

Fcr -= —

Aa=2774-psi Calculated stress.

F a 3 6 =22000-psi Allowable stress.

The allowable stress is greater than the calculated stress. The pin will not pull through the bar during a seismic event.

The plate that the pin is attached to (Ref. 2, Item 3) is 0.5" thick. The pin will not shear the plate during a seismic event nor willthe pin shear since it has the same area.

6. Verify that the weld holding the plate with the pin (Ref. 2, Item 3) to the plate attached to the pit wall (Ref. 2, Item 2) is capablecarrying the load imposed during an earthquake.

Figure 2


ICF Kaiser Hanford caic. NO. W320-27-031Company Revision 0


Client WHC WO/JobNo. ER4319/W320Subject Booster Pump Restraint Analysis Date 2-15-95 By Rodney C. Campbell

Checked -i-t-HS By tJ .Location: Sluice PitAY-02E Revised By

The weld is subjected to the combined loading of a tensile load, shear load and bending.

<o := .1875- in Size of fillet weld. Ref. 2, Sht. 2.

I = 10 in Length of weld.

a m : = 3 i n Length of moment arm.

t := 9600- psi Allowable shear stress. Ref. 6, Chapter 7, Table 6.

f t := F ' s m ( " 4 S ) f t = -236.04 - ^ Calculated tensile load per inch of weld.

= Fcos(-45) f =145.72-— Calculated shear load per inch of weld.1 in

S w := — S w = 33.33 • in2 Section modulus of weld treating it as a line. Ref. 6, Table 5.

M := F c o s ( - 4 5 ) a m M = 4371.73 -lbf in Calculated moment on weld.

f •=— ' • Ibfm s f_, = 131.15 • — Calculated bending load per inch of weld,

w ra in

+ f v2 + f _ 2 f r = 306.84 — Calculated combined load per inch of weld,v m r i n

ffi r " x Required size of fillet weld to carry combined load. Ref. 6, Chapter 7.

(o r = 0.032 -in Calculated size of the fillet weld required to carry the load.

<o r<co = 1 This weld is strong enough to carry the maximum load.

7. Verify that the expansion anchors attaching the plate to the pit wall are adequate to carry the load.

A. Verify the edge distance to obtain maximum allowable load.

The minimum required edge spacing to obtain maximum allowable load is 6 3/4" for shear and 5" for tension. The actualedge distances are greater than this (Ref. 2). The maximum allowable load can be used.

B. Verify the bolt spacing to obtain maximum allowable load.

The minimum required bolt spacing to obtain maximum allowable load is 6". The actual bolt spacing is 9" (Ref. 2). Themaximum allowable load can be used.

C. Verify that the load imposed does not exceed the maximum allowable load.

V a = 1470 lbf Allowable shear load per bolt. (SDC 4.2)

HNF-2475, Rev. 0T = 1230 lbf Allowable tension load per bolt. (SDC 4.2) PageD-7


Client WHC

Subject Booster Pump Restraint Analysis


DESIGN ANALYSIS


WO/Job No. ER4319/W320Date 2-15-95 By Rodney C. CampbellChecked J . ^ - ^ S By <J- J O P L ORevised By

V :=Fcos(45)

V = 364.31 • Ibf Calculated shear load per bolt.

Fsin(45) Fcos(45)-3inT = :

T = 832.98-lbf

0,93

2-9 in

Calculated tension load per bolt.

The combined load is less than the allowable combined load (by the sum of the loads divided by the allowable being lessthan one). The anchor bolts are adequate to carry the seismic load.

CONCLUSIONS:

The design of the seismic restraint system is adequate to carry the load.


APPENDIX A

HNF-24-75, Rev. 0Page D-9

KAISER ENGINEERS HANFORD S/N:801854 02/13/95PAGE 1 RUN ID=TA62753 15:06:38

=============== I M A G E S 3 D ================ Copyright (c) 1984 Celestial Software Inc. =

CHECK GEOMETRY Version 2.0 07/01/90

MaterialNo

MATERIAL PROPERTIES

Modulus of Weight Coeff of Poisson's Shear WebElasticity Density Thermal Exp. Ratio Modulus

3.00000E+07 2.83000E-01 6.33000E-06 3.00E-01 0.00000E+00

NODE COORDINATES

Node

1234567891011121314151617181920212223242526

X-Coord.

0.O0O00E+OO4.14310E-011.63120E+003.57423E+006.12128E+009.11234E+001.23595E+011.56586E+011.88025E+012.15935E+012.38564E+012.54489E+012.62710E+012.62710E+012.54489E+012.38564E+012.15935E+011.88025E+011.56586E+011.23595E+019.11234E+006.12129E+003.57423E+001.63121E+004.14313E-011.31875E+01

Y-Coord.

O.O0000E+O00.00000E+00O.O0O0OE+O0O.OOO00E+O00.O0O00E+OOO.OOOOOE+00O.OOOOOE+00O.00000E+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.0000OE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.OOOOOE+00O.00000E+00

Z-Coord.

O.O0000E+O03.27960E+006.35313E+009.02746E+001.11346E+011.25421E+011.31615E+011.29539E+011.19324E+011.01611E+017.75142E+004.85464E+001.65283E+00-1.65283E+00-4.85464E+00•7.75142E+00-1.01611E+01-1.19324E+01-1.29539E+01-1.31615E+01-1.25421E+01-1.11346E+01•9.02747E+00-6.35313E+00-3.27960E+00O.OOOOOE+00

KAISER ENGINEERS HANFORD S/N:801854 02/13/95PAGE 2 RUN ID=TA62753 15:06:38


CHECK GEOMETRY Version 2.0 07/01/90

BEAM PROPERTIES

Mul t i p l i e r = 1 (For AISC database propert ies only)

Prop X-Section Moment of Ine r t iaNo Area Iy / Iz

TorsionalConst.- J

1.500E+00 3.125E-02 1.125E+00 1.250E-019.000E+00 6.750E+00 6.750E+00 2.700E+01

Prop Max. Fiber DistNo Cy / Cz

Shear Shape FactSSFy / SSFz

Shear Stress FactorSSTRFy / SSTRFz

1 2.50E-01 1.50E+00 1.20E+00 1.20E+002 1.50E+00 1.50E+00 1.20E+00 1.20E+00

1.00E+00 1.50E+00 1.50E+001.00E+00 1.50E+00 1.50E+00

BEAM CONNECTIVITY

Seam Nodes Prop MatNo From/ To / Ref No No

pincodes Rigid End Offset Length BeamI / J I / J Type

12345678910111213141516171819202122232425

12345678910111213141516171819202122232425

23456 .789

1 0 •1112131415161718192021222324251

0000000000000000000000000

1111111111111111111111111

1111111111111111111111111

00E+00OOE+0000E+0000E+00OOE+0000E+0000E+00OOE+0000E+0000E+0000E+0000E+00OOE+00OOE+0000E+0000E+00OOE+0000E+0000E+0000E+00OOE+0000E+0000E+0000E+0000E+00

0.OOE+000.OOE+000.00E+000.00E+000.00E+000.00E+000.00E+000.00E+000.00E+000.00E+000.00E+000.OOE+000.00E+000.00E+000.OOE+000.00E+000.00E+000.OOE+000.OOE+000.00E+000.00E+000.00E+000.00E+000.OOE+000.00E+00

0.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+010.33E+01

BeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeamBeam

U3202731.3OU 2-13-95 3:07p Page 2 of 11

KAISER ENGINEERS HANFORD S/N:801854 02/13/95PAGE 3 RUM I0=TA62("53 15:06:39


CHECK GEOMETRY

Beam Nodes Prop HatNo From/ To / Ref No No

Version 2.0 07/01/90

pincodes Rigid End Offset Length SeamI / J I / J Type

282930313233343536373839

262626262626262626262626

8910111213141516171819

000000000000

NodeNo

222222222222

111111111111

NANANANANANANANANANAHANA

NANANANANANANANANANANANA

RESTRAINTS

Global/Local


RestraintDirections


0.13E+020.13E+020.13E+020.13E+020.13E+020.13E+02O.13E+020.13E+020.13E+020.13E+020.13E+020.13E+02

TrussTrussTrussTrussTrussTrussTrussTrussTrussTrussTrussTruss

23242526

GLOBALGLOBALGLOBALGLOBALGLOBAL

X V Z RX RY RZX Y Z RX RY RZX Y Z RX RY RZX Y Z RX RY RZ. y - - - -

KAISER ENGINEERS HANFORD S/N:801854 02/13/95PAGE 4 Run ID=TA62753 15:06:39


RENUMBER NODES Version 2.0 07/01/90

Node Renumbering Cross Reference List

Has Is Uas Is Was Is Uas Is Was Is

1611162126

2617721610

27121722

25156118

38131823

23135920

49141924

211141222

510152025

19831424

U3202731.3OU 2-13-95 3:07p Page 3 of 11

KAISER ENGINEERS HANFORDPAGE 5

S/N:801854 02/13/95Run I0=TA62753 15:06:54I M A G E S 3 D ===============

Copyright (c) 1984 Celestial Software Inc. =

ASSEMBLE STIFFNESS MATRIX Version 2.0 07/01/90

STIFFNESS ASSEMBLY SUMMARY

Number of Node Points 26Number of Truss and Beam Elements 39Number of Plate Elements 0Number of Spring Elements 0Number of Solid Elements 0Number of Axisymmetric Elements 0Number of Nodes with Restraints 5Number of Equations to be Solved 128Number of Blocks in the Matrix 1

B L O C K I N F O R M A T I O N

BLCK SIZENO (Byte)

BLCK SIZENO (Byte)

BLCK SIZENO (Byte)

BLCKNO

SIZE(Byte)



ASSEMBLE STIFFNESS MATRIX Version 2.0 07/01/90

E O U A T I O N N U M B E R L I S T

NODEHAS

1234567891011121314151617181920212223242526

IS

262523211917151311a765432191214161820222410

TRANSLATIONX

12300

117105938169574337312519137149637587991110055

STIFFNESS

Y

12400

118106948270584438322620148250647688100112000

SUMMARY

Z

12500

1191079583715945393327211593516577891011130056

IN

ROTATIONX

12600

1201089684726046403428221610452667890102114000

Y

12700

1211099785736147413529231711553677991103115000

1 BLOCKS

z12800

1221109886746248423630241812654688092104116000

Minimum Diagonal Stiffness 9999D+06Eq No of Minimum Diagonal 123Maximum Diagonal Stiffness 1280D+09Eq No of Maximum Diagonal 55

U3202731.30U 2-13-95 3:07p Page 4 of 11

KAISER ENGINEERS HANFORD S/N:801854PAGE 7 Run ID=TA62753

=============== I M A G E S 3 D =============:= Copyright Cc) 1984 Celestial Software Inc.

02/13/9515:07:14

SOLVE DISPLACEMENTS Version 2.0 07/01/90

L O A D C A S E

GRAVITY LOADING

GravityFactor

LoadFactor

X .OOOOE+00 .1000E+01Y .0000E+00 .1000E+01Z .OOOOE+00 .1000E+01

INERTIA LOADING

Translational Rotational RotationalDirection Accel. Accel. Velocity Origin

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0O00E+00 .0000E+00

.OOOOE+00 .0000E+00

.OOOOE+00 .OOOOE+00

Gravity Acceleration = .3864E+03

CONCENTRATED LOADS

Node Fx Fy Fz Mx Ny Mz

26 .2774E+04 .OOOOE+00 .OOOOE+00 .OOOOE+00 .OOOOE+00 .OOOOE+00

REFERENCE TEMPERATURE = .0000E+00

KAISER ENGINEERS HANFORD S/N:801854PAGE 8 Run ID=TA62753


02/13/9515:07:15

SOLVE DISPLACEMENTS Version 2.0 07/01/90

L O A D C A S E . 1

APPLIED LOAD VECTOR

Node Fx Fy Fz Hx My Mz

26 .2774E+04 .OOOOE+00 .OOOOE+00 .OOOOE+00 .OOOOE+00. .OOOOE+00

W3202731.3OU 2-13-95 3:07p Page 5 o f 11

•tf g

o

2475, Rev. 0

KAISERPAGE

Node

1234567891011121314151617181920212223242526

ENGINEERS HANFORD S/N9

= Copyright (c)

SOLVE

1

T r aX

.0000E+00

.OOOOE+00

.0000E+00

.9349E-02

.1974E-01

.2164E-01

.1983E-01

.2073E-01

.2090E-01

.2102E-01

.2116E-01-2125E-01.2130E-01.2130E-01.2125E-01.2116E-01.2102E-01.2090E-01.2073E-01.1983E-01.2164E-01.1974E-01.9349E-02.OOOOE+00.OOOOE+00.2133E-01

:801854Run ID=TA62753

T M fl f* C O "*C T\ ——' '

02/13/9515:07:15

1984 Celestial Software Inc. =

DISPLACEMENTS Version 2.0

L

n s I a t •y

.0000E+00

.OOOOE+00

.0000E+00

.3012E-19

.8335E-19

.1281E-18

.1566E-18

.1870E-18

.2457E-18-3218E-1S.3851E-18.4262E-18.4427E-18.4323E-18.3944E-18.3302E-18.2410E-18.1296E-18.2895E-19

-.3987E-19-.8675E-19-.7458E-19-.3011E-19.0000E+00.0000E+00.OOOOE+00

0 A D C A S E 1

DISPLACEMENTS

0 n s /2 /

.OOOOE+00 /

.0000E+00 /

.OOOOE+00 /-.6676E-02 /-.1907E-01 /-.2284E-01 /-.1277E-01 /.3083E-04 /.2270E-03 /.2207E-03 /.2096E-03 /.1441E-03 /.5141E-04 /

-.5146E-04 /-.1442E-03 /-.2096E-03 /-.2208E-03 /-.2270E-03 /-.3087E-04 /.1277E-01 /.2284E-01 /.1907E-01 /.6676E-02 /.OOOOE+00 /.OOOOE+00 /

-.1276E-07 /

R cX

.OOOOE+00

.OOOOE+00

.OOOOE+00-.1056E-19-.1437E-19-.7240E-20-.8113E-20-.8199E-20-.3527E-20-.7792E-21-.1986E-20-.2773E-20-.3148E-20-.3153E-20-.2884E-20-.2152E-20-.3783E-20-.6317E-21.3548E-20.3429E-20

-.3249E-21-.7628E-20-.1048E-19.OOOOE+00.OOOOE+00.OOOOE+00

07/01/90

t a t i oY

.OOOOE+00

.OOOOE+00

.0000E+00

.5325E-02

.3555E-02-.U40E-02-.4404E-02-.1974E-02.4339E-03

-.1376E-03.4716E-05

-.18176-04-.2440E-05.2443E-05.1817E-04

-.4713E-05.1376E-03

-.4339E-03.1974E-02.4404E-02.1140E-02

-.3555E-02-.5325E-02.OOOOE+00.0000E+O0.OOOOE+00

n sZ

.OOOOE+00

.OOOOE+00

.OOOOE+OO

.9611E-20

.1619E-19

.3109E-20

.1018E-19

.8176E-20

.2377E-19

.2950E-19

.2983E-19

.3087E-19

.3225E-19

.3371E-19

.3506E-19

.3602E-19

.3882E-19

.3493E-19

.2264E-19

.2063E-19

.4531E-20-.8478E-20-.9705E-20.OOOOE+00.OOOOE+00.OOOOE+00

KAISERPAGE

Load C

GLoadsLLoadsStressStress

GLoadsGLoadsLLoadsLLoadsStressStressStressStress




ENGINEERS HANFORD S/N:80185410

ise

NodeNodeNodeNode

12121122

23232233

34343344

45454455

Run ID=TA62753

= Copyright (c) 1984

SOLVE BEAM

:

FxAxialAxialMaximum

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+0O

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.O0O0E+00

.OOOOE+00

-.1387E+04.1387E+04

-.1285E+04.1285E+04.8567E+03.2326E+05.8567E+03.2614E+04

-.1387E+04.1387E+04

-.1439E+04.1439E+04.9592E+03.2717E+04.9592E+03.1075E+05

Celestial

LOADS/STRESSES Vers

BEAM LOADS

FyY-ShearY-ShearMinimum

02/13/9515:07:16

Software Inc. =

on 2.0 07/01/90

AND/OR STRESSES

FzZ-ShearZ-Shear

Cmb. Shear

MXTorsionTorsion

"••BEAM NO. 1***.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00.0000E+00.0000E+00.OOOOE+00.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+O0

.OOOOE+00"•BEAM NO. 2

.OOOOE+00

.0000E+O0

.0000E+00

.00OOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.00O0E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

***BEAH NO. 3***-.8331E-17.8331E-17.2125E-14

-.2125E-14.2125E-14

-.2155E+05.2125E-14

-.9011E+03

-.5807E+03.5807E+03.7808E+03

-.7808E+03.7808E+03.1163E+05.7808E+03.1307E+04

BEAn nui H-.8331E-17 -.5807E+03.8331E-17

-.1897E-14.1897E-14

-.1897E-14-.7985E+03-.1897E-14-.8831E+04

.5807E+03

.4367E+03-.4367E+03.4367E+03.1358E+04.4367E+03.5375E+04

.7903E-17

.3018E-16

.6846E-15

.6846E-15

.5477E-14

.5477E-14

.3018E-16

.4774E-16

.5487E-15

.5487E-15

.4389E-14

.4389E-14

MyY-BendingY-Bending

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

-.2801E+04.2197E+03

-.2801E+04.2197E+03.2241E+05

.1758E+04

-.2197E+03-.1224E+04-.2197E+03-.1224E+04.1758E+04

-.9790E+04

MzZ-BendingZ-Bending

.OOOOE+00

.OOOOE+00

.0000E+OO

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.00O0E+00

-.8405E-15.8243E-15.7164E-14

-.1402E-15-.9553E-14

-.1870E-15

-.8243E-15.8031E-15

-.1566E-14-.4706E-14.2089E-14

-.6274E-14

U3202731.3OU 2-13-95 3:07p Page 6 of 11



SOLVE BEAM LOADS/STRESSES Version 2.0 07/01/90

Load Case 1:

GLoads NodeLLoads NodeStress NodeStress Node

FxAxialAxialMaximum

Fy FzY-Shear Z-ShearY-Shear Z-ShearMinimum Cmb. Shear

MxTorsionTorsion

My MzY-Bending Z-BendingY-Bending Z-Bending





.1387E+04

.1387E+04

.1502E+04

.1502E+04

.1001E+04

.1079E+05

.1001E+04

.1251E+05

.1387E+04

.1387E+04

.1471E+04

.1471E+04

.9808E+03

.1249E+05

.9808E+03

.4282E+04

.1387E+04

.1387E+04

.'1348E+04

.1348E+04

.8985E+03

.4199E+04

.8985E+03

.1523E+05

.1075E+04

.1075E+04

.1348E+04

.1348E+04

.8989E+03

.1523E+05

.8989E+03

.4302E+04

GLoads 9 -.1278E+04 -

***BEAM.8331E-17 -•8331E-17.2049E-15.2049E-15 -.2049E-15 ..8789E+04.2049E-15.1051E+05

***BEAM.8331E-17 •.8331E-17.6801E-15 -.6801E-15.6801E-15 -.1053E+05.6801E-15 -.2320E+04

•••BEAM.8331E-17 -.8331E-17.5780E-15 -.5780E-15.5780E-15 -.2402E+04.5780E-15 -.1343E+05

•••BEAM.8331E-17.8331E-17 -.4634E-14.4634E-14 -.4634E-14.1343E+05.4634E-14.2505E+04

•**BEAH.8331E-17

.1634E-14 -.3301E+04 -.2521E-15

NO. 5***5807E+03 -.4774E-165807E+03 .5946E-166513E+02 -.3851E-156513E+02 .3851E-156513E+O2 .3081E-145396E+046513E+02 .3081E-146257E+04NO. 6***5807E+03 -.5946E-165807E+03 .6462E-16 -3105E+03 -.2042E-153105E+03 .2042E-15 -3105E+03 .1634E-14 -6247E+043105E+032141E+04NO. 7*»*5807E+03 -.6462E-16.5807E+03 .6289E-166666E+03 -.1733E-166666E+03 .1733E-166666E+03 .1387E-15 -.2100E+04.6666E+03.7614E+04NO. 8**«1054E+O4 -.6289E-161054E+04 .5438E-16.6705E+03 .1638E-15.6705E+03 -.1638E-15.6705E+03 -.1310E-14.7614E+04.6705E+03 -.1310E-14.2151E+04NO. 9***6225E+03 -.5438E-16

1224E+041439E+041224E+041439E+049790E+04

.8031E-15

.7782E-15

.4713E-14

.5391E-14

.62S4E-U

-.1151E+05 .7188E-14

1439E+044126E+031439E+044126E+031151E+05

.7782E-15

.7511E-15

.2437E-14

.1891E-15

.3250E-14

4126E+03.1791E+044126E+031791E+043301E+04

.7511E-15

.7236E-15

.3908E-15

.2302E-14

.5210E-15

.1387E-15 .1433E+05 .3069E-14

1791E+044255E+031791E+044255E+031433E+05

.7236E-15

.6974E-15

.1169E-13

.3625E-14

.1559E-13

-.3404E+04 .4834E-14

4255E+03 -.6974E-15


=============== I M A G E S 3 D ================ Copyright Cc) 1984 Celestial Software Inc. =


Load Case 1:


FxAxialAxialMaximum


MXTors ionTors ion

My MzY-Bending Z-BendingY-Bending Z-Bending

GLoadsLLoadsLLoadsStressStressStressStress




109

1099

1010

10 •11101110101111

11121 1 •1211111212

1213121312121313

GLoads 13GLoads 14LLoads 13

.1278E+04

.1413E+04

.1413E+04 •

.9419E+03

.4346E+04

.9419E+03

.1752E+04

.9297E+03 •

.9297E+03

.1397E+04

.1397E+04

.9316E+03

.1742E+04

.9316E+03 •

.1096E+04

.6824E+03 •

.6824E+03

.1401E+04 •

.1401E+04

.9340E+03 •

.1098E+04

.9340E+03

.9943E+03

.3464E+03

.3464E+03

.1400E+04 •

.1400E+04

.9334E+03 •

.9937E+03

.9334E+03

.9445E+03

.1665E-05

.1665E-05

.1400E+04 •

.8331E-17 -

.1785E-14 -

.1785E-14

.1785E-14 -

.2462E+04

.1785E-14 -

.1318E+03»**BEAM

.8331E-17

.8331E-17 -

.1953E-15

.1953E-15 -

.1953E-15

.1215E+03

.1953E-15

.7674E+03•••BEAM

.8331E-17

.8331E-17 -

.9152E-16 -

.9152E-16

.9152E-16 -

.7698E+03

.9152E-16 -

.8737E+03

•**BEAM.8331E-17.8331E-17 -.1258E-16.1258E-16 -.1258E-16.8731E+03.1258E-16.9223E+03

***BEAM.8331E-17.8331E-17 -.8331E-17 -

6225E+03 .3963E-161593E+03 .3278E-151593E+03 -.3278E-15

.1593E+03 -.2622E-142173E+041593E+03 -.2622E.-14,8760E*03NO. 10***1044E+04 -.3963E-161044E+04 .1955E-163684E+02 .4643E-153684E+02 -.4643E-15.3684E+02 -.3715E-148709E+033684E+02 -.3715E-145479E+03NO. 11***1224E+04 -.1955E-16.1224E+04 -.4581E-17.8488E+01 .5648E-15.8488E+01 -.5648E-15.8488E+01 -.4519E-14.5491E+03.8488E+01 -.4519E-14.4971E+03

NO. 12**»1357E+04 .4581E-17

.1357E+04 -.3125E-161861E+01 .6230E-151861E+01 -.6230E-151861E+01 -.4984E-144969E+031861E+01 -.4984E-14

.4723E+03NO. 13** *

.1400E+04 .3125E-161400E+04 -.5879E-161665E-05 .6352E-15

.1013E+03

.4255E+03

.1013E+03

.3404E+04

.6742E-15

.4170E-14

.1730E-14

.5560E-14

.8101E+03 .2307E-14

.1013E+03

.2052E+02

.1013E+03

.2052E+02

.8101E+03

.6742E-15

.6553E-15

.1004E-14

.3587E-15

.1339E-14

-.1642E+03 .4783E-15

.2052E+02

.7538E+01

.2052E+02

.7538E*01

.1642E+03

.6553E-15

.6421E-15

.5340E-15

.2314E-15

.7119E-15

.6031E+02 .3086E-15

.7538E+01

.1385E+01

.7538E*01

.1385E+01

.6031E+02

.64216-15

.6352E-15

.1724E-15

.1309E-15

.2299E-15

.1108E+02 .1745E-15

.1385E+01

.1385E+01

.1385E+01

.6352E-15

.6352E-15

.3125E-16

U3202731.3OU 2-13-95 3:07p Page 7 of 11


=============== I M A G E S 3 D ================ Copyright Co) 1984 Celestial Software Inc. =


Load Case 1:


FxAxialAxialMaximum


HxTorsionTorsion

My MzY-Bendjng Z-BendingY-Bending Z-Bending


S/N:801854Run ID=TA62753

:============= I M A G E S 3 D ==============Copyright Cc) 1984 Ce les t i a l Software Inc . •

02/13/9515:07:17


Load Case 1:


Fx Fy Fz Mx My MzAxial Y-Shear Z-Shear Torsion Y-Bending Z-BendingAxial Y-Shear Z-Shear Torsion Y-Bending Z-BendingMaximum Minimum Cmb. Shear

LLoads 14Stress 13Stress 13Stress 14Stress 14




GLoadsGLoadsLLoadsLLoadsStressStress

1415 -14 -1514141515

1516 -15 -1615151616

1617 -16 •1716161717

1718 •17 •181717

.1400E+04

.9336E+03

.9447E+03

.9336E+03

.9447E+03

.3464E+03

.3464E+03

.1400E+04

.1400E+04

.9334E+03

.9445E+03

.9334E+03

.9937E+03

.6824E+03

.6824E+03•.1401E+04.1401E+04.9340E+03.9943E+03.9340E+03.1098E+04

.9297E+03

.9297E+03

.1397E+04

.1397E+04

.9316E+03

.1096E+04

.9316E+03

.1742E+04

.1278E+04•.1278E+04•.1413E+04.1413E+04.9419E+03.1752E+04

.8331E-17

.8331E-17 -

.9225E+03

.8331E-17 -

.9225E+03 .***BEAM

.8331E-17

.8331E-17 -

.1792E-17 -

.1792E-17

.1792E-17 -

.9223E+03

.1792E-17 -

.8731E+03•**BEAM

.8331E-17

.8331E-17 -

.9152E-16

.9152E-16 -

.9152E-16

.8737E+03

.9152E-16

.7698E+03•**BEAM

.8331E-17

.8331E-17 -

.8041E-15 -

.8041E-15

.8041E-15 -

.7674E+03

.8041E-15 -

.1215E+03***8EAM

.8331E-17

.8331E-17 -

.1453E-14

.1453E-14 -

.1453E-14

.1318E+03

1665E-051665E-054723E+031665E-054723E+03

NO. 14'1357E+041357E+041861E+011861E+011861E+014723E+031861E+014969E+03

NO. 151224E+041224E+048488E+018488E+018488E+014971E+038488E+015491E+03

NO. 16'1044E+041044E+043684E+023684E+023684E*025479E+033684E+028709E+03

NO. 17'.6225E+03.6225E+03.1593E+03.1593E+03•1593E+03.8760E+03

.6352E-15

.5082E-14.1385E+01.1108E+02

.5879E-16

.4167E-16

-.5082E-14 .1108E+02 -.7839E-16

.5879E-16

.8547E-16

.6006E-15

.6006E-15

.4805E-14

.1385E+01

.7538E+01

.1385E+01

.7538E+01

.1108E+02

.6352E-15

.6421E-15

.2100E-15

.2160E-15

.2801E-15

-.4805E-14 .6031E+02 -.2880E-15

.8547E-16

.1096E-15

.5215E-15

.5215E-15

.4172E-14

.7538E+01 •

.2052E+02

.7538E+01

.2052E+02

.6031E+02

.6421E-15

.6553E-15

.3103E-15

.6129E-15

.4138E-15

-.4172E-14 -.1642E+03 -.8172E-15

.1096E-15

.1297E-15

.4027E-15

.4027E-15

.3221E-14

.2052E+02

.1013E+03

.2052E+02

.1013E+03

.1642E+03

.6553E-15

.6742E-15

.9810E-15

.1677E-14

.1308E-14

-.3221E-14 .8101E+03 .2236E-14

.1297E-15

.1444E-15

.2518E-15

.2518E-15

.2014E-14

.1013E+03

.4255E+03

.1013E+03

.4255E+03

.8101E+03

.6742E-15

.6974E-15

.2792E-15

.4523E-14

.3722E-15

Stress 18Stress 18





.9419E+03

.4346E+04

.1075E+04

.1075E+04

.1348E+04

.1348E+04

.8989E+03

.4302E+04

.8989E+03

.1523E+05

.1387E+04

.1387E+04

.1348E+04

.1348E+04

.8985E+03

.1523E+05

.8985E+03

.4199E+04

.1387E+04

.1387E+04•-1471E+04.1471E+04.9808E+03.4282E+04.9808E+03.1249E+05

.1387E+04

.1387E+04•.1502E+04.1502E+04.1001E+04.1251E+05.1001E+04.1079E+05

•-1453E-14-.2462E+04

***BEAM-.8331E-17.8331E-17 -.•.3745E-14 -..3745E-14 .-.3745E-14 -.-.2505E+04 .-.3745E-14 -.-.1343E+05 .

**»BEAM-.8331E-17 -..8331E-17.5780E-15-.5780E-15 -.5780E-15-.1343E+05.5780E-15-.2402E+04

•**BEAM-.8331E-17 -.8331E-17-.1631E-14.1631E-14 -.-.1631E-14 .-.2320E+04 .-.1631E-14 .-.1053E+05 .

***BEAM-.8331E-17 -.

.8331E-17 .

.2049E-15 --.2049E-15 ..2049E-15 --.1O51E+O5.2049E-15 --.8789E+04

1593E+03 -.2014E-14.2173E+04

NO. 18***.1054E+04 .1444E-151054E+04 --1529E-156705E+03 .7815E-16,6705E*03 -.7815E-166705E+03 -.6252E-152151E*046705E+03 -.6252E-157614E+04NO. 19***5807E+03 .1529E-155807E+03 -.1547E-15.6666E+03 -.1072E-156666E+03 .1072E-156666E+03 .8576E-15.7614E+046666E+03.2100E+04NO. 20***

.5807E+03 .1547E-15

.5807E+03 -.1495E-15

.3105E+03 -.2927E-153105E+03 .2927E-153105E+03 .2341E-142141E+043105E+036247E+04

NO. 21***5807E+03 .1495E-155807E+03 -.13786-15.6513E+02 -.4666E-156513E+02 .4666E-15.6513E+026257E+046513E+02.5396E+04

-.3404E+04 -.6030E-14

.4255E+03

.1791E+04

.4255E+03

.1791E+04

.3404E+04

.6974E-15

.7236E-15

.1663E-14

.1072E-13

.2217E-14

.1433E+05 -.1429E-13

.1791E+04

.4126E+03

.1791E+04

.4126E+03

.1433E+05

.7236E-15

.7511E-15

.2307E-14

.3964E-15

.3076E-14

.8576E-15 -.3301E+04 -.5286E-15

.4126E+03

.1439E+04

.4126E+03

.1439E+04

.3301E+04

-7511E-15.7782E-15.2865E-14.8257E-14.3820E-14

.2341E-14 -.1151E+05 -.1101E-13

.1439E+04

.1224E+04

.1439E+04

.1224E+04

.1151E+05

.7782E-15

.8031E-15

.5352E-14

.4675E-14

.71366-14

.3733E-14 -.9790E+04 -.6233E-14

U3202731.30U 2-13-95 3:07p

KAISERPAGE

ENGINEERS HANFORD15

Load Case 1

GLoadsLLoadsstressStress

jLoadsGLoadsLLoadsLLoadsStressStressStressStress




GLoads

NodeNodeNodeNode

2223222322222323

2324232423232424

2425242524242525

251251252511

26

= Copyright

S/N:801854Run ID=TA62753j ^ ^ ^ c c in

<c) 1984 Celestial Software

02/13/9515:07:17

nc. =


FxAxialAxialMaximum

.1387E+04 --.1387E+04-.1439E+04.1439E+04 -.9592E+03.1075E+05 -.9592E+03.2717E+04 -

.1387E+04 --.1387E+04-.1285E+04.1285E+04 -.8567E+03.2614E+04 -.8567E+03.2326E+05 -

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.3119E+03

fyY-ShearY-Shear

FzZ-ShearZ-Shear

Minimum Cmb. Shear

•••BEAM.8331E-17 -.8331E-17.7066E-15 -.7066E-15.7066E-15 -.8831E+04-7066E-15 -.7985E+03

***BEAM.8331E-17 -.8331E-17-2125E-14 -.2125E-14.2125E-14 -.9010E+03.2125E-14 -.2155E+05

***BEAH.0000E+00.OOOOE+00.0000E+00.0000E+00.0000E+00.0000E+00.0000E+00.0000E+00

•**BEAM.0000E+00.OOOOE+00.0000E+00.OOOOE+00.OOOOE+00.OOOOE+00.0000E+00.OOOOE+00

NO. 22.5807E+03.5807E+03.4367E+03.4367E+03.4367E+03.5375E+04.4367E+03.1358E+04NO. 23

.5807E+03

.5807E+03

.7808E+03

.7808E+03

.7808E+03

.1307E+04

.7808E+03

.1163E+05

MxTorsionTorsion

.1378E-15

.1202E-15

.6181E-15

.6181E-15

.4944E-14

.4944E-14

***.1202E-15.9795E-16.7375E-15.7375E-15.5900E-14

.5900E-14

NO. 24***.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00.OOOOE+00NO. 25

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

**.OOOOE+00.OOOOE+00.OOOOE+00.0000E+00.0000E+00

.OOOOE+00

•••TRUSS NO. 28***.OOOOE+00 .1635E+04 .OOOOE+00


.1224E+04

.2197E+03

.1224E+04

.2197E+03- .9790E+04

.1758E+04

-.2197E+03.2801E+04

-.2197E+03.2801E+04.1758E+04

.2241E+05

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00


-.8031E-15.8243E-15.2534E-14-.1988E-15-.3379E-14

--2650E-15

-.8243E-15.8405E-15

-.2131E-15.7237E-14.2841E-15

.9650E-14

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

KAISERPAGE

ENGINEERS HANFORD S/N:S0185416

i

Load Case

GLoadsLLoadsStressStress

GLoadsLLoadsLLoadsStressStressStressStress



GLoadsGLoadsLLoadsLLoadsstressStressStressStress

GLoadsGLoadsLLoads

NodeNodeNodeNode

8268262688

269269262699

2610261026261010

2611261126261111

261226

Run D=TA627531 P I H U C S 3 l>

= Copyright (c) 1984 Celestial

SOLVE BEAM

:

FxAxialAxialMaximum

-.3119E+03.1665E+04

-.1665E+04-.1849E+03-.1849E+03-.1849E+03-.1849E+03

-.2032E+03.2032E+03

-.4773E+03.4773E+03.5303E+02.5303E+02.5303E+02.5303E+02

.3486E+03-.3486E+03.5469E+03

-.5469E+03-.6076E+02-.6076E+02-.6076E+02-.6076E+02

.2474E+03-.2474E+03.3058E+03

-.3058E+03-.3397E+02-.3397E+02-.3397E+02-.3397E+02

.3360E+03-.3360E+03.3613E+03

02/13/9515:07:18

Software Inc. =

LOADS/STRESSES Version 2.0 07/01/90

FyY-ShearY-ShearMinimum

.OOOOE+00-.6416E-29.6416E-29

-.1069E-29-.1849E+03-.1069E-29-.1849E+03

FzZ-ShearZ-Shear

Cmb. Shear

-.1635E+04.5974E-12

-.5974E-12.9956E-13.9247E+02.9956E-13.9247E+02

HxTorsionTorsion

.OO00E+00

.000OE+00

.00OOE+00

.OOOOE+00

.0000E+00

***TRUSS NO. 29***.OOOOE+00.0000E+00.1921E-28

-.1921E-28.3202E-29.5303E+02.3202E-29.5303E+02

-.4318E+03-4318E+03.7491E-12

-.7491E-12.1249E-12.2651E+02.1249E-12.2651E+02

***TRUSS NO. 30.OOOOE+00.0000E+00.5041E-27

-.5041E-27.8402E-28

-.6076E+02.8402E-28

-.6076E+02

.4214E+03-.4214E+03.80846-11

-.8084E-11.1347E-11.3038E+02.1347E-11.3038E+02

•"TRUSS NO. 31".OOOOE+00.OOOOE+00

-.4321E-28.4321E-28

-.7202E-29-.3397E+02-.7202E-29-.3397E+02

.1797E+03-.1797E+03-.1899E-11.1899E-11

-.3166E-12.1699E+02

-.3166E-12.1699E+02

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

**.0000E+O0.0000E+O0.0000E+00.0000E+00.OOOOE+00

.0000E+00

**.0000E+00.0000E+00.0000E+00.OOOOE+00.0000E+00

.0000E+00

•**TRUSS NO. 3 2 " *.0000E+00.0000E+00.3994E-28

.1330E+03-.1330E+03.6639E-11

.OOOOE+00

.0000E+00

.0000E+O0


.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.OOOOEtOO

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.000OE+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00


.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.O000E+OO

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

. 0000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+OO

.OOOOE+00

.O000E+OO

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+O0

o U3202731.30U 2-13-95 3:07p Page 9 of 11




Load Case 1


Fx Fy Fz Mx My MzAx ia l ' Y-Shear Z-Shear Torsion Y-Bending Z-BendingAx ia l Y-Shear Z-Shear Torsion Y-8ending Z-Bending

Maximum Minimum Cmb. Shear


S/N:801854Run ID=TA62753

- I M A G E S 3 D ================ Copyright (c) 1984 Celestial Software Inc. =

02/13/9515:07:18


Load Case 1:


Fx Fy Fz Hx My MzAxial Y-Shear Z-Shear. Torsion Y-Bending Z-BendingAxial Y-Shear Z-Shear Torsion Y-Bending Z-BendingMaximum Minimum Cmb. Shear

LLoads 12 -.3613E+03 -.3994E-28 -.6639E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.4015E+02 .6657E-29 .1107E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.4015E+02 -.4015E+02 .2007E+02Stress 12 -.4015E+02 .6657E-29 .1107E-11Stress 12 -.4015E+02 -.4015E+02 .2007E+02

***TRUSS NO. 33***GLoads 26 .3464E+03 .OOOOE+00 .4376E+02 .OOOOE+00 .OOOOE+00 .OOOOE+00GLoads 13 -.3464E+03 .OOOOE+00 -.4376E+02 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 26 .3491E+03 -.1415E-27 .6236E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 13 -.3491E+03 .1415E-27 --6236E-11 -0000E+00 .OOOOE+00 .OOOOE+00Stress 26 -.3879E+02 -.2358E-28 .1039E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.3879E+02 -.3879E+02 .1940E+02Stress 13 -.3879E+02 -.2358E-28 .1039E-11Stress 13 -.3879E+02 -.3879E+02 .1940E+02

***TRUSS NO. 34***.3464E+03 .OOOOE+00 -.4376E+02 .OOOOE+00 .OOOOE+00 .OOOOE+00.3464E+03 .OOOOE+00 .4376E+02 .OOOOE+00 .OOOOE+00 .OOOOE+00.3491E+03 .4832E-30 .7870E-13 .OOOOE+00 .OOOOE+00 .OOOOE+00.3491E+03 -.4832E-30 -.7870E-13 .OOOOE+00 .OOOOE+00 .OOOOE+00.3879E+02 .8054E-31 .1312E-13 .OOOOE+00 .OOOOE+00 .OOOOE+00.3879E+02 -.3879E+02 .1940E+02.3879E+02 .8054E-31 .1312E-13.3879E+02 -.3879E+02 .1940E+02

***TRUSS NO. 35***GLoads 26 .3360E+03 .OOOOE+00 -.1330E+03 .OOOOE+00 .OOOOE+00 .OOOOE+00GLoads 15 -.3360E+03 .OOOOE+00 .1330E+03 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 26 .3613E+03 -.5202E-28 -.1619E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 15 -.3613E+03 .5202E-28 .1619E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.4015E+02 -.8669E-29 -.2698E-12 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.4015E+02 -.4015E+02 .2007E+02Stress 15 -.4015E+02 -.8669E-29 -.2698E-12Stress 15 -.4015E+02 -.4015E+02 .2007E+02

***TRUSS NO. 36***GLoads 26 .2474E+03 .OOOOE+00 -.1797E+03 .OOOOE+00 .OOOOE+00 .OOOOE+00GLoads 16 -.2474E+03 .OOOOE+00 .1797E+03 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 26 .3058E+03 .7326E-28 .6189E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00LLoads 16 -.3058E+03 -.7326E-28 -.6189E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.3397E+02 .1221E-28 .1031E-11 .OOOOE+00 .OOOOE+00 .OOOOE+00Stress 26 -.3397E+02 -.3397E+02 .1699E+02

GLoads 26GLoads 14LLoads 26LLoads 14Stress 26Stress 26Stress 14Stress 14

.0000E+00 .OOOOE+00 .0000E+00

.OOOOE+00 .0000E+00 .OOOOE+00

.OOOOE+00 .OOOOE+00 .0000E+00

.0000E+00 .OOOOE+00 .0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

Stress 16 -.3397E+02 .1221E-28 .1031E-11Stress 16 -.3397E+02 -.3397E+02 .1699E+02

***TRUSS NO. 37***GLoads 26 .3486E+03 .0000E+00 -.4214E+03 .0000E+00GLoads 17 -.3486E+03 .0000E+00 .4214E+03LLoads 26 .5469E+03 -.6802E-27 .1088E-10LLoads 17 -.5469E+03 .6802E-27 -.1088E-10Stress 26 -.6076E+02 -.1134E-27 .1813E-11Stress 26 -.6076E+02 -.6076E+02 .3038E+02Stress 17 -.6076E+02 -.1134E-27 .1813E-11Stress 17 -.6076E+02 -.6076E+02 .3038E+02

***TRUSS NO. 38'GLoads 26 -.2032E+03 .0000E+00 .4318E+03GLoads 18 .2032E+03 .0000E+00 -.4318E+03LLoads 26 -.4773E+03 .1030E-28 .3045E-12LLoads 18 .4773E+03 -.1030E-28 -.3045E-12Stress 26 .5303E+02 .1717E-29 .5076E-13Stress 26 .5303E+02 .5303E+02 .2651E+02Stress 18 .5303E+02 .1717E-29 .5076E-13Stress 18 .5303E+02 .5303E+02 .2651E+02

•"TRUSS NO. 39***GLoads 26 .3119E+03 .0000E+00 -.1635E+04 .0000E+00GLoads 19 -.3119E+03 .0000E+00 .1635E+04LLoads 26 .1665E+04 .2450E-28 .2150E-11LLoads 19 -.1665E+04 -.2450E-28 -.2150E-11Stress 26 -.1849E+03 .4083E-29 .3583E-12Stress 26 -.1849E+03 -.1849E+03 .9247E+02Stress 19 -.1849E+03 .4083E-29 .35S3E-12Stress 19 -.1849E+03 -.1849E+03 .9247E+02

.OOOOE+00 .00O0E+O0 .OOOOE+00

.OOOOE+00

.0000E+00

.0000E+00

.0000E+00

.OOOOE+00

.OOOOE+00

.00O0E+0O

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00 .0000E+00 .OOOOE+00

.0000E+00

.O000E+00

.0000E+00

.OOOOE+00

.0000E+00

.0000E+00

.OOOOE+00

.0000E+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00

.OOOOE+00

.OOOOE+00

.0000E+00 .0000E+00 .OOOOE+00

.O000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.0000E+00

.O000E+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.OOOOE+00

.0000E+00 .0000E+00 .0000E+00

U3202731.30U 2-13-95 3:07p Page 10 of 11

KAISER ENGINEERS HANFORD S/N:801854 02/13/95PAGE 19 Run I0=TA62753 15:07:18



Load Case 1:

MAXIMUM STRESS SUMMARY FOR BEAMS/TRUSSESWITHIN SPECIFIED RANGE 1- 39

Maximum (absolute) Stress = .2326E+05 at BEAM 3

;am Axial Y-Shear Z-Shear Torsion Y-Bending Z-Bending

3 .8567E+03 .2125E-H .7808E+03 .5477E-14 .2241E+05 -.9553E-14Maximum Minimum Cmb. Shear

.2326E+05 -.2155E+05 .1163E+05



SOLVE REACTIONS Version 2.0 07/01/90

1

Load Case 1:

REACTIONS

Node Fx Fy Fz Mx My Mz

2 .OOOOE+00 .000OE+O0 .0000E+00 .OOOOE+00 .0000E+00 .0000E+003 -.1387E+04 -.8331E-17 -.5807E+03 -.7903E-17 -.2801E+04 -.8405E-1524 -.1387E+04 -8331E-17 .5807E+03 -.9795E-16 .2801E+04 .8405E-1525 .0000E+00 .0000E+00 .0000E+00 .0000E+O0 .0000E+00 .0000E+0026 .0000E+00 .OOOOE+00 .0000E+00 .0000E+00 .0000E+00 .0000E+00

U3202731.3OU 2-13-95 3:07p Page 11 of 11

IMAGES-3DUer. 2.0Geometry Plot

Uirefrane Plot2/13/9514:49:25

IMAGES-3DUER. Z.BL Case 1S= 1.800E+01

Deflected Shape - Wireframe Plot2/13/9E14:52:

APPENDIX B


SDC 4.2Rev. 0Page 22

TABLE 11

ALLOWABLE ANCHOR VALUES FORCARBON STEEL HILTI KWIK-BOLT II

Concrete Minimum Strength 3000 psi

The following tabulated data also apply to these specific sites:Bid. 236-Z of Z-Plant. Tank Farms 241-SX-115.

feifiioiwili:i;;:itameterS:S;yii-;n>iCHES):ij;|;

M-v§Bgjy3;

1/4

3/8

1/2

5/S

3/4

1

WliCINCHES^S

1/2

3/4

3/4

3/4

3/4

3/4

•fe::C:>j::'Etffoedment;v;*v'*::':'::::S'i)epth: tINCHES):-i>S|»<Hin./Stahdard>:^';

1 1/8

2

1 5/8

2 1/2

2 1/4

3 1/2

2 3/4

4

3 1/4

4 3/4

4 1/2

6

?• ' :: .•: «aximumi:j:S;.v:':::'•' ::'AllowabU:tbad. ::: :/-::, . ..}'•?:,(KIP/BOLT)sj:s;J'V

T=0.31V=0.32

T=0.55V=0.32

T=0.61V=0.78

T=1.21V=0.88

T=1.23V=1.47

T=2.00Va1.47

T=1.75V=2.53

T=2.67V=2.75

1=2.17V«3.41

T=3.87V=3.71

T=3.80V=6.27

T=5.81V=7.59 :

.:• I n s t a l l a t f on ; .:'-' • ; " ' Torque7:•; i •-'.• (FT-LBS)>

:•:•:".••••'••: <,>:\:: • • • ' . '• 7 . : • ' . • > .

4-7

5-8

20-25

22-28

30-45

45-60

75-90

95-115

150-175

225-240

200-350

350-450

General Mote: For bolt length, use as a minimum that which will satisfy the requiredentoednent depth and "T".

1) T - maximum thread length above nut after torquing, minimLm length equals two threads above

nut.

2) The design shall not consider anchor pretension;

V applied + T applied < 1.0V T " •

3) Hinirmm embedment = Absolute minimun embedment depth allowed HNF-2475 R n

PageD-23'

DISTRIBUTION SHEETTo

DistributionProject Title/Work Order

Project W-320 Tank 106-C,

Name

From

JW

HNF-2475,

Bai 1 ey

Piping Calculations,

MSINText

With AllAttach.

V o l .

Text

5

Page 1 of 1

Date 23 July 1998

EDT No. 622233

ECN No. n/a

Only Attach./Appendix

Only

EDT/ECNOnly

JW BaileyW-320 Project Files

S2-48Rl-29

A-6000-135 (01/93) VEF067

international nuclear information system...jul24199b engineering data transmittal 622233 2. to:...

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