8 I 7 I 6 I 5 v 4 I 3 I 2 I 1 REV REV REV REV REV REV THIS PRINT IS PROVIDED ON A RESTRIClED BASIS AND IS NOT TO BE USED

I I I I ~~Mcl~c IN ANY WAY DETRIMENTAL TO SOLAR TURBINES INCORPORATED.

REVISIONS

00 INITIAL SUBMITTAL - OUTLINE 09/29 T. BOGOWfll

H ,

H INITIAL RELEASE OF FULL MID 12/15 AD T. BOGOWITZ

TABLE OF CONTENTS , DESCRIPTION SHT

NO.

COVER SHEET 1 -

PACKAGE CONNECTION SUMMARY 2 t--

DRAWING NOTES 3

DRAWING NOTES (CONT'D) 4

DRAWING NOTES (CONT'D) 5

G RIGHT SIDE ELEVATION 6 G LEFT SIDE ELEVATION 7

PLAN VIEW 8

FORWARD END ELEVATION 9

AFT END ELEVATION 10

ENCLOSURE ACCESS LAYOUT 11 -

FORWARD/AFT END CUSTOMER CONNECTIONS t--

12

RIGHT/LEFT SIDE EXTERNAL CONNECTIONS 13

PACKAGE TIE -DOWN DETAIL 14

ANCILLARY SUPPORT TIE -DOWN DETAIL 15

F PACKAGE CENTER OF GRAVITY AND LIFT POINTS 16 F ALIGNMENT INFORMATION 17

ALIGNMENT INFORMATION (CONT'D) 18

GENERATOR ARRANGEMENT 19

GENERATOR TERMINAL CONNECTION 20

LOOSE SHIPPED COMPONENTS INDEX 21 - t--

E E

---1> f:J-

D D

- t--

c c

- t--

B Chevron CUSTOMER/END USER/PROJECT

B SYMBOL EXAMPLES ........_-- CHEVRON

0 ~ CVX GOM VK 900 DENOTES EXTERNAL CONNECllONS POINT CVX-VK9

ffi INDICATES REFERENCE TO NOTES 2 & DENOTES REVISION

~ APPROVED DRAWHG TTTlf

- DENOTES REVISION BEFORE SHIPMENT ";';~~N~~~""" ~~·;15/11 t--tAKIII 8FT, SATURN 20 0 DENOTES COMPONENT OR INSTRUMENTATION PROJECT ENGINEER DATE GENERATOR SET ~ATO(

T. BOGOWITZ 09/15/11 MECHANICAL INTE FAC MECHANICAL ENGINEER DATE

M. HURT 09/15/11 UC>OuN CNuoNCC"

~~·;15/11 Solar Turbines A L. BENNET A u~~ ~~LLINS ~~·;15/11 A Caterpillar Company

FSCM NO. DRAWING NO. ISIZE s rEV AO

66195 3M511-149607 ISH 1 OF 37

Lf THIS COPYRIGHTED WORK AND THE INFORW.TION HEREIN IS PROPRIETARY TID CATERPIUAR

W~r+J~~~~~~~~~ ~~~~~~iu.M0~~ 8~~g~ESruWs~~E~J;~g\U,JXJ'R,W I R T WHI I IT •

8 I 7 I 6 I 5 v 4 I 3 I 2 I 1 TABLE 1 - EXTERNAL CONNECTIONS

REFERENCE OPERATION MAXIMUM BACK VELOCI1Y ITEM DESCRIPTION SIZE & 1YPE SERVICE RATINGS FLUID 1YPE FT/SEC SHEET

H NOTE MODE PRESSURE (M/SEC) H

MECHANICAL 1 TURBINE AIR INLET FLANGE SEE DETAIL C 2.10, 211 12,000 CFM AIR CONllNUOUS 4" [102 MM] H20 N/A -

3 LUBE OIL TANK VENT 3" 150 LB ANSI RF FLANGE 5.3 14" [356 MM] H20 AIR/OIL (MIST) CONllNUOUS 2" [51 MM] H20 10.0 [3.1] 8

- 6 PNEUMATIC START VENT 3" 150 LB ANSI RF FLANGE 3.2 5 - 25 PSIG AIR/GAS STARTUP 5 PSIG F(l, P) 8 t--7 LUBE OIL COOLER VENT RETURN 1/2" NPT FEMALE - 14" [356 MM] H20 AIR/OIL CONllNUOUS 10" [254 MM] H20 20.0 [5.1] 7

19 ENGINE EXHAUST COLLECTOR & COMBUSTOR DRAIN 1 /2" 150 LB ANSI RF FLANGE 2.14 N/A AIR/OIL/WATER/FUEL STARTUP, SHUTDOWN 0 PSIG] N/A 12

20 NATURAL GAS FUEL INLET 1 1 /2" 150 LB ANSI RF FLANGE 4.0 130 - 185 PSIG GAS CONllNUOUS N/A 100.0 [30.5] 12

22 ENGINE AIR INLET DUCT DRAIN 1 /2" 150 LB ANSI RF FLANGE 3.0, 9.3 N/A AIR, WATER STARTUP, SHUTDOWN NONE N/A 12

G 25 LUBE OIL FILTER DRAIN - FILTERED 1 /2" 150 LB ANSI RF FLANGE 5.0 150 PSIG OIL MAINTlENANCE NONE N/A 12 G 26 LUBE OIL TANK DRAIN 2" NPT FEMALE 5.0 14" [356 MM] H20 OIL MAINTlENANCE 0 PSIG 7.0 [2.1] 13

27 PNEUMATIC START INLET 1 1 /2" 150 LB ANSI RF FLANGE 3.1 120 - 150 PSIG AIR/GAS STARTUP N/A F(l, P) 6

30 GAS VENT 1 /2" 150 LB ANSI RF FLANGE 4.2 N/A GAS STARTUP, SHUTDOWN 5 PSIG 194.0 [59.1] 12

31 ENGINE SEAL VENT 1 /2" 150 LB ANSI RF FLANGE 2.9, 5.8 N/A OIL MIST CONllNUOUS 0 PSIG N/A 12

- 33 LUBE OIL TO COOLER 1 1 /2" 150 LB ANSI RF FLANGE 2.8, 5.2 150 PSIG OIL INTlERMITTENT N/A N/A 7 t--34 LUBE OIL FROM COOLER 1 1 /2" 150 LB ANSI RF FLANGE 2.8, 5.2 150 PSIG OIL INTlERMITTENT N/A N/A 7

36 PACKAGE AIR SUPPLY 1/2" 150 LB ANSI RF FLANGE 4.1 100 - 200 PSIG AIR CONllNUOUS N/A 46.0 [14.0] 12

54 LUBE OIL FILTER DRAIN - UNFILTERED 1/2" 150 LB ANSI RF FLANGE 5.0 150 PSIG OIL MAINTlENANCE 0 PSIG 7.0 [2.1] 12

97 ENCLOSURE FIRE EXT. MEDIUM INLET - PRIMARY 3/4" NPT FEMALE 8.1 750 PSIG C02 EMERGENCY N/A N/A 8

F 98 ENCLOSURE FIRE EXT. MEDIUM INLET - EXTENDED 1 /2" NPT FEMALE 8.1 750 PSIG C02 EMERGENCY N/A N/A 8 F 122 ON CRANK CLEANING FLUID INLET 1/2" 150 LB ANSI RF FLANGE 3.0, 9.0 85 - 100 PSIG WATER / CLNG SOW. MAINTlENANCE N/A N/A 12

126 OIL DRAIN FROM DRIP PAN (2 PLACES) 2" NPT FEMALE 5.0 1.0 PSIG OIL. WATER MAINTlENANCE 0 PSIG 1.0 [0.3] 12

127 OIL DRAIN FROM DRIP PAN GENERATOR 2" NPT FEMALE 5.0 1.0 PSIG OIL. WATER MAINTlENANCE 0 PSIG 1.0 (0.3) 13

* 147 VENT FAN FAIL, LOW PRESSURE (2 PLACES) 3/8" TUBE FITTING - N/A AIR CONllNUOUS N/A N/A 6,8

- t--

ELECTRICAL - NEC

E 301 AC VOLTS, J-BOX (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), 1X 4.95" X 10.50" (126 X 267) GLAND PLATE 6.0, 6.4, 6.7 VARIOUS N/A CONllNUOUS N/A N/A 12

E 308 GENERATOR POWER LEADS CONNECTION BOX 48.50" X 9.13" (1232 X 232) X 7 GA. GLAND PLATE 6.0, 6.4, 6.7 N/A N/A CONllNUOUS N/A N/A 9

313 AC VOLTS, LUBE OIL TANK HEATER 3/4" NPT FEMALE 6.0 460 VAC, 3 PH, 50/60 HZ, 4.5 KW N/A INTlERMITTENT N/A N/A 13

315 AC VOLTS, PRE/POST LUBE OIL PUMP MOTOR (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), (DEVICE) 3/4 NPT FEMALE 6.0, 6.4, 6.7 460 VAC, 3 PHASE. 1 HP [0.75 KW] N/A INTlERMITTENT N/A N/A 13

331 GROUND, PACKAGE FRAME 1/2"-13 UNC 6.0, 6.2 N/A N/A CONllNUOUS N/A N/A 13

335 DC VOLTS, CONTROL CONSOLE (8 PLACES) 2X 7.00" X 21.00" (178 X 533) & 2X 7.00" X 7.00" (178 X 178) GLAND PLATES TOP & BOTTOM 2.1. 6.0, 6.3, 6.4. 6. 7 24 VDC N/A CONllNUOUS N/A N/A 30

-t> 336 DC VOLTS, BACKUP LUBE OIL PUMP MOTOR (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), (DEVICE) 3/4 NPT FEMALE 6.0, 6.4, 6.7 24 VDC, 0.95 HP [0.71 KW], 40 FLA N/A INTlERMITTENT N/A N/A 13 ~ 342 GROUND, CONSOLE FRAME BUS BAR (2 PLACES) 3/8" - 16 UNC-2A STUD 2.1, 6.0, 6.2, 6.3 N/A N/A N/A N/A N/A 30

350 AC VOLTS, LUBE OIL COOLER MOTOR 1 1/4" NPT FEMALE 2.1, 6.0 460 VAC, 3 PH, 60 HZ, 7.5 HP (5.6 KW) N/A CONllNUOUS N/A N/A 25

354 DC VOLTS, FIRE SYSTEM 1 /2" NPT FEMALE 2.1, 6.0, 8.1 24 VDC N/A EMERGENCY N/A N/A 29

D 357 AC VOLTS, ENCLOSURE VENT FAN 1" NPT FEMALE 6.0, 10.2 460 VAC, 3 PH, 60 HZ, 10 HP (7.5 KW) N/A CONllNUOUS N/A N/A 6 D 360 AC VOLTS, BACKUP ENCLOSURE VENT FAN 1" NPT FEMALE 6.0, 10.2 460 VAC, 3 PH, 60 HZ, 10 HP (7.5 KW) N/A CONllNUOUS N/A N/A 6

374 DC VOLTS, TURBINE AIR INLET FILTER ANALOG 1/0 1 /2" NPT FEMALE 6.0 24 VDC N/A CONllNUOUS N/A N/A 7

379 DC VOLTS, ENCLOSURE VENT FILTER PRESSURE SWITCH 1 /2" NPT FEMALE 6.0, 10.2 24 VDC N/A CONllNUOUS N/A N/A 7

399 DC VOLTS, OIL COOLER VIBRATION SWITCH 1 /2" NPT FEMALE 2.1, 6.0 24 VDC N/A CONllNUOUS N/A N/A 25

414 DC VOLTS, DRIVER J-BOX NON I.S. (2 PLACES) (SKID) 5X RGS-4 MCT 4.75" X 6.28" (121 X 160), 1X 4.95" X 10.50" (126 X 267) GLAND PLATE 6.0, 6.4, 6.7 24 VDC N/A CONllNUOUS N/A N/A 13

- REMOTE MECHANICAL t--

203 FLAME ARRESTOR, LUBE OIL TANK VENT 3" 150 LB ANSI RF FLANGE 5.3 N/A AIR CONllNUOUS 2" [51 MM] H20 10.0 [3.1] 28

218 FLANGED STRAINER INLET 1 1/2" 150 LB ANSI RF FLANGE 4.0, 10.2 130 - 185 PSIG GAS CONllNUOUS N/A N/A 22

219 FLANGED STRAINER OUTLET 1 1/2" 150 LB ANSI RF FLANGE 4.0, 10.2 130 - 185 PSIG GAS CONllNUOUS N/A N/A 22

c 228 FLANGED STRAINER INLET, PNEUMATIC START 1 1/2" 150 LB ANSI RF FLANGE 3.1, 10.2 120 - 150 PSIG GAS/AIR STARTUP, UAINTlENANCE N/A N/A 22 c 229 FLANGED STRAINER OUTLET, PNEUMATIC START 1 1/2" 150 LB ANSI RF FLANGE 3.1, 10.2 120 - 150 PSIG GAS/AIR STARTUP, UAINTlENANCE N/A N/A 22

233 LUBE OIL COOLER INLET 2" 150 LB ANSI RF FLANGE 5.2, 10.2 150 PSIG OIL CONllNUOUS N/A N/A 25

234 LUBE OIL COOLER OUTLET 2" 150 LB ANSI RF FLANGE 5.2, 10.2 150 PSIG OIL CONllNUOUS N/A N/A 25

235 OIL COOLER VENT RETURN TO TANK (ORIFICED) 3/4" NPT FEMALE 5.2. 10.2 14" [356 MM] H20 AIR/OIL STARTUP N/A N/A 25

271 FUEL FLOWMETER RUN INLET 1" 300 LB ANSI RF FLANGE 4.0, 10.2 505 PSIG MAX 0 200'F GAS CONllNUOUS N/A N/A 23 - 272 FUEL FLOWMETER RUN OUTLET 1" 300 LB ANSI RF FLANGE 4.0, 10.2 505 PSIG MAX 0 200'F GAS CONllNUOUS N/A N/A 23 t--

287 LUBE OIL MIST SEPARATOR INLET 3" 150 LB ANSI RF FLANGE 5.7 N/A AIR/OIL (MIST) CONllNUOUS 2" [51 MM] H20 10.0 [3.1] 27

288 LUBE OIL MIST SEPARATOR OIL FILL 1 /2" NPT FEMALE 5.7 14" [356 MM] H20 OIL CONllNUOUS 10" [254 MM] H20 20.0 [5.1] 27

289 LUBE OIL MIST SEPARATOR OUTLET 3" 150 LB ANSI RF FLANGE 5.7 N/A AIR/OIL (MIST) CONllNUOUS 2" [51 MM] H20 10.0 [3.1] 27

B 297 FIRE SYSTEM DISCHARGE - MAIN 3/4" NPT FEMALE 8.1, 10.2 750 PSIG C02 EMERGENCY N/A N/A 29 CUSTOMER/END USER/PROJECT

B 298 FIRE SYSTEM DISCHARGE - EXTENDED 1 /2" NPT FEMALE 8.1, 10.2 750 PSIG C02 EMERGENCY N/A N/A 29 CHEVRON

452 VENT, FIRE EXTINGUISHANT, MAIN 3/4" NPT FEMALE 8.1, 10.2 N/A C02 EMERGENCY N/A N/A 29 CVX GOM VK 900

1 /2" NPT FEMALE N/A N/A N/A CVX-VK9

453 VENT, FIRE EXTINGUISHANT, EXTENDED 8.1, 10.2 C02 EMERGENCY 29

522 AIR INLET FILTER DRAIN, UNPLUGGED 2" 150 LB ANSI FLANGE 10.2, 12.7 N/A WATER CONllNUOUS N/A N/A 7

* FIELD CONNECTION BY SOLAR TURBINES DRAWING llTLE

- tAKIII 8FT, SATURN 20 t--

GENERATOR SET ~ATO( MECHANICAL INTE FAC

A Solar Turbines A A Caterpillar Company

DRAWING NO. ISIZE 8 rEV AO 3M511-149607 1,, 2

Lf THIS COPYRIGHTED WORK ~D lHE INFIORIAATION HEREIN IS PROPRIETARY TO CATERPILlAR

~~mm~.m~~i1,~ ~~~~~~iu.M0~~ ~B~~~uWslwr~Er~J=g\U,JXt.R~ I R T WHI I I

H

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G

-

F

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E

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D

-

c

1.0

1.1

1.2

8 GENERAL NOTES

SYMBOLS AND ABBREVIATIONS: " INCHES

FEET ALTERNATING CURRENT BAR BAR GAGE BRITISH THERMAL UNIT DEGREE CELSIUS CUBIC FEET PER MINUTE

I 7

AC BAR BARG BTU 'C CFM cs DC 'F

CENTISTOKES (MILLIMETER SQUARED PER SECOND) DIRECT CURRENT DEGREE FAHRENHEIT

KPAG KW L LPM LBS M M3 mm MIN

I

KILOPASCAL GAGE KILOWATT LITER LITERS PER MINUTE POUNDS METER CUBIC METER MILLIMETER MINUTE NEWTONS NORMAL CUBIC METER

6

FT GAL GPM HR KG KJ KPA

FEET GALLONS GALLONS PER MINUTE HOUR

N NM3 PSI PSIG SCF SCFM ssu VAC VDC

POUNDS PER SQUARE INCH POUNDS PER SQUARE INCH GAGE STANDARD CUBIC FOOT

KILOGRAM KILOJOULE KILOPASCAL

STANDARD CUBIC FEET PER MINUTE SAYBOLT SECONDS UNIVERSAL VOLTS ALTERNATING CURRENT VOLTS DIRECT CURRENT

NOTE: FLOW, PRESSURE AND TEMPERATURE VALUES SHOWN ON THIS DRAWING ARE INTENDED FOR USE IN THE DESIGN OF EXTERNAL SYSTEMS AND EQUIPMENT ONLY, AND CANNOT BE USED IN ANY TURBINE PERFORMANCE CALCULATIONS.

SPECIFICATIONS: THE FOLLOWING SOLAR DOCUMENTS APPLY TO THIS DRAWING.

ES 9-54 ES 9-62 ES 9-98 ES 9-224 ES 9-414 ES 2184 ES 2201 PIL 149 PIL 181

FASTENER INSTALLATION AND TORQUE VALUES INGESTIVE CLEANING SOLAR GAS TURBINE ENGINES FUEL, AIR, AND WATER (OR STEAM) FOR SOLAR GAS TURBINE ENGINES LUBRICATING OIL FOR SOLAR GAS i'URBINES ELEVATING AND LEVELING PACKAGE BASES CLEANING AND FLUSHING OF HYDRAULIC SYSTEMS/COMPONENTS AUXILIARY SERVICE AIR DIRECT -DRIVE AC START SYSTEM PACKAGE TIE-DOWN OPTIONS

INSTALLATION INSTRUCTIONS FOR:

INTAKE DUCTING FOR SOLAR TURBINE ENGINES ES 1733 ES 1740 ES 1745

INSTALLATION INSTRUCTIONS FOR LUBE OIL TANK VENT PIPING INSTALLATION INSTRUCTIONS FOR LUBE OIL TANK VENT WITH SEPARATOR WITH OR WITHOUT A FLAME ARRESTOR

SYSTEM DRAWINGS: 3M511-149455 LUBE OIL SCHEMATIC 3M511-149456 GAS FUEL SCHEMATIC 3M511-149457 DIRECT AC START SCHEMATIC 3M511-149459 ENGINE AIR/DRAIN SCHEMATIC

PACKAGE INSTALLATION

3M511-149450 3M511-149451 3M511-149452

ELECTRICAL SCHEMATIC WIRING DIAGRAM INTERFACE/INTERCONNECT

2.0 ESTIMATED COMPONENT WEIGHTS:

2.1

2.2

DRIVER FRAME WITH ACCESSORIES ENGINE ASSEMBLY (with TAl & EXH. DUCTS) GEARBOX ENCLOSURE GENERATOR

TOTAL (TURBINE SKID) "DRY LIFT" WEIGHT

TURBINE AIR INLET EQUIPMENT

ENCL. EXHAUST VENT DUCTING LUBE OIL TO FILL SYSTEM (1 00 GAL)

TOTAL INSTALLED (TURBINE SKID) 'WET" WEIGHT

ENCL. VENT INLET EQUIPMENT

LOOSE SHIPPED FOR CUSTOMER INSTALILATION.

13,500 LBS ( 6124KG) 1,200 LBS ( 544 KG) 1,215 LBS ( 551KG) 7,000 LBS ( 3175KG)

12,000 LBS ( 5443 KG)

34,915 LBS (15837KG)

2,298 LBS ( 1 042 KG)

550 LBS ( 250 KG) 760 LBS ( 345 KG)

38,523 LBS (17474 KG)

1,420 LBS ( 644 KG)

WHEN A CONVENTIONAL REINFORCED CONCRETE SLAB IS TO BE USED, TIHE THICKNESS MUST BE DETERMINED BY THE CUSTOMER BASED ON LOCAL SOIL CONDITIONS. AN EMBEDDED PLATE AT EACH MOUNTING PAD IS REQUIRED TO SUPPORT JACKING SCREW (REF PIL 181 ). THE SLAB OR DECK SHOULD PROVIDE ADEQUATE, CLEAN WALKWAYS THAT PERMIT ACCESS FOR MAINTENANCE AND ALLOW PROPER CLEARANCE FOR HINGED ENCLOSURE DOORS. THE ACCESS PATH AROUND TIHE PACKAGE IS RECOMMENDED TO BE A MINIMUM OF 1 0' [3048mm] WIDE ON ALL SIDES FOR ENGINE REMOVAL.

2.3 THE SKID ASSEMBLY IS PROVIDED WITH FOUR LIFT POINTS FOR INDIVIDUAL - SKID LIFTING AND TOTAL PACKAGE LIFTING. ALL FOUR SPECIFIED LIFT

POINTS MUST BE USED AND SPREADER BARS ARE REQUIRED TO PREVENT DAMAGE TO PACKAGE.

B

-

A

2.4 NOTE NOT USED.

2.5 BASE LEVELING PROCEDURE: INITIAL LEVELING IS ACCOMPLISHED BY ADJUSTING BASE USING JACKING BOLTS AND LEVELING FEATURES ON EACH SIDE OF THE SKID. WHEN THE TOPS OF ALL LEVELING FEATURES ARE COPLANAR WITHIN ±1/16" [1.6mm], PROCEED WITH FINAL LEVELING OF EQUIPMENT MOUNTING PADS. THE FINAL LIEVELING CHECK IS MADE USING A PRECISION MACHINIST LEVEL, TRANSIT, OR EQUIVALENT ON THE EQUIPMENT MOUNTING PADS. EQUIPMENT USED MUST BE CAPABLE OF MEASURING THE REQUIRED TOLERANCES AT THE MOUNTING PADS. THE PACKAGE FRAMES ARE CONSIDERED LEVEL WHEN THE MACHINED PADS UNDER THE ENGINE AND DRIVEN EQUIPMENT ARE LEVEL WITHIN .005" [.127mm] PER FOOT AND COPLANAR WITHIN .010" [.254mm]. INSERT SHIMS OR POUR GROUTED PEDESTALS UNDER BASE MOUNTING PADS. SHIMMED BASES MAY BE TORQUED IMMEDIATELY. GROUTED PEDESTALS MUST BE ALLOWED TO CURE BEFORE TORQUING ANCHOR BOLTS. TORQUE ANCHOR BOLTS TO 1,050 FT -LBS (1424 N-M) AND VERIFY THAT BASE LEVEL HAS BEEN MAINTAINED.

CAUTION: PRIOR TO GROUTING, FINAL ROTATING EQUIPMENT ALIGNMENT AND COUPLING FIT SHOULD BE VERIFIED.

I 5 4

2.6 THE BOTTOM SURFACE OF THE PACKAGE FRAME, INCLUDING THE PACKAGE TIE DOWN LOCATIONS, IS PAINTED WITH THE SAME PROCESS AS THE OTHER SURFACES OF THE FRAME. THIS PAINT PROCESS IS COMPLETELY COMPATIBLE WITH GROUT PROCESSES AND DOES NOT REQUIRE REMOVAL OF THE PAINT WHEN GROUT IS UTILIZED. THE GROUT CAN BE APPLIED DIRECTLY TO THE PAINTED SURFACE.

2.7 REVERSE ROTATION OF THE DRIVEN EQUIPMENT DURING OPERATION IS DEFINITELY NOT PERMITTED. SEVERE DAMAGE TO SHAFT BEARINGS WILL OCCUR.

2.8 ENGLISH UNITS ARE PRIMARY AND METRIC CONVERSIONS SHOWN IN BRACKETS ARE DERIVED FROM THE ENGLISH UNITS. OVERALL DIMENSIONS SHOWN ON THIS DRAWING ARE NOMINAL AND SMALL VARIATIONS CAN BE EXPECTED. TOLERANCES ARE ±1/4" [±6mm] ON INLET AND EXHAUST DUCTING AND PIPING INTERFACE CONNECTIONS. TOLERANCES ARE ±1/8" [±3mm] ON HOLD DOWN FOUNDATION POINTS. IT IS RECOMMENDED THAT SUFFICIENT ALLOWANCE BE LEFT ON MATING PIPES AND FLANGES FOR FINAL FIELD ALIGNMENT. DO NOT SCALE THIS DRAWING, WORK TO DIMENSIONS GIVEN. DIMENSIONS IN PARENTHESES ARE FOR REFERENCE ONLY.

CUSTOMER CONNECTION PIPE FLANGES CONFORM TO AMERICAN NATIONAL STANDARDS INSTITUTE STANDARD (ANSI) B.16.5. ALL FLANGE HOLES STRADDLE THE VERTICAL CENTERLINE SYMMETRICALLY.

ALL EXTERNAL PIPES, DUCTS OR VENTS CONNECTED TO TIHE PACKAGE MUST BE FULLY SELF-SUPPORTING. MINIMUM PIPE SIZES ALLOWAIBLE ARE DETERMINED BY PACKAGE CONNECTION POINT. NO REDUCTIONS ARE ALLOWED.

EXTERNAL OIL LINES ARE TO BE CLEANED BY CONTRACTOR PRIOR TO CONNECTION TO THE TURBINE SKID OR EXTERNALLY MOUNTED OIL COOLERS. EXTERNAL PIPING IS TO BE CLEANED OF ALL DIRT AND RUST AND IS TO BE TREATED WITH A RUST INHIBITOR. SOLAR RECOMMENDS THAT OIL PIPING BE FLUSHED WITH A MINIMUM REYNOLDS NUMBER OF 4000 UNTIL THE FLUSHING FLUID MEET AN ISO CLEANLINESS CODE (4406) OF 14/12, AND THERE ARE NO PARTICLES COLLECTED ON A 100 MESH SCREEN AT THE LINE OUTLET AFTER FLUSHING FOR AT LEAST ONE HOUR. REFERENCE SOLAR ES 2184.

TIHE REYNOLD'S NUMBER CAN BE CALCULATED BY:

Nr = 3160 X GPM CS X D

GPM = Nr(CS X D) 3160

WHERE: GPM = FLUSHING FLUID FLOW RATE - GALLONS PER MINUTE CS = FLUSHING FLUID VISCOSITY - CENTISTOKES D = PIPE/TUBE INSIDE DIAMETER - INCHES

GPM REQUIRED FOR Nr - 4000 W C32 OIL PIPE/TUBE SIZE 80'F OIL 120'F OIL 150'F OIL

48 cs 21 cs 12.5 cs .375¢ X .049wl TUBE .277" I.D. 16.8 7.4 4.4 .500¢ X .049wl TUBE .402" I.D. 24.4 10.7 6.4 .750¢ X .065wl TUBE .620" I.D. 37.7 16.5 9.8 1.00¢ X .083wl TUBE .834" I.D. 52.9 23.1 13.8 1.25¢ X .1 09wl TUBE 1.032" I.D. 62.7 27.4 16.3 . 75 X SCH 80 PIPE .742" I.D. 45.1 19.7 11.7 1.0 X SCH 80 PIPE .957" I.D. 58.1 25.4 15.1 1.5 X SCH 80 PIPE 1.500" I.D. 91.1 39.9 23.7 2.0 X SCH 80 PIPE 1.939" I.D. 117.8 51.5 30.7 3.0 X SCH 40 PIPE 3.068" I.D. 186.4 81.6 48.5 4.0 X SCH 40 PIPE 4.026" I.D. 244.6 107.0 63.7

EXAMPLE OF FLOW RATE FOR REYNOLD'S NUMBER (Nr) - 4000 W/C32 OIL

CARBON STEEL PIPING MUST BE PICKLED AND PASSIVATED PRIOR TO FLUSHING. UNDER NO CIRCUMSTANCES ARE TIHE EXTERNAL PIPES TO BE CLEANED WHILE THEY ARE CONNECTED TO THE TURBINE OR EXTERNALLY MOUNTED OIL COOLERS.

ALL CUSTOMER PIPING INTERFACE CONNECTIONS 4" [102mm] OR LESS IN DIAMETER ARE STAINLESS STEEL UNLESS OTHERWISE SPECIFIED. CUSTOMER PIPING INTERFACE CONNECTIONS GREATER THAN 4" [ 1 02mm] IN DIAMETER ARE CARBON STEEL UNLESS OTHERWISE SPECIFIED.

2.9 FLOW, PRESSURE AND TEMPERATURE VALUES SHOWN ON THIS DRAWING ARE INTENDED FOR USE IN THE DESIGN OF EXTERNAL SYSTEMS AND EQUIPMENT ONLY, AND CANNOT BE USED IN ANY TURBINE PERFORMANCE CALCULATIONS.

2.1 0 EXTERNAL ENGINE LIFTING CRANE (PROVIDED BY OTHERS) TO BE SIZED FOR ENGINE WEIGHT PLUS THE WEIGHT OF LIFTING TOOL. LIFTING TOOLS AND DATA ARE AVAILABLE FROM SOLAR TURBINES CUSTOMER SERVICES GROUP.

2.11 UNDER NO CIRCUMSTANCES SHOULD EXTERNALLY IMPOSED LOADING BE APPLIED IN ANY DIRECTION ON THE AIR INLET OR EXHAUST DUCTING CONNECTIONS WHICH EXCEEDS 200 LBS (890 N). EXHAUST DUCT ALIGNMENT MUST BE MAINTAINED WITHIN ±3/8" [±1 Omm] OF EXHAUST DUCT CENTERLINE IN BOTH HOT AND COLIO CONDITIONS. MAXIMUM THERMAL GROWTH OF EXHAUST DUCTING BACK TOWARDS TURBINE EXHAUST EXPANSION JOINT SHALL NOT EXCEED 1" [25.4mm].

2.12 TURBINE AIR FLOW VALUES ARE FOR DUCT SIZING CALCULATION PURPOSES ONLY AND DO NOT CORRESPOND TO ANY GIVEN TURBINE CONDITIONS. INLET AND EXHAUST SYSTEMS SHOULD BE DESIGNED SUCH THAT PRESSURE LOSSES DO NOT EXCEED 4" [102mm] H20 FOR TIHE INLET, 6" [152.4 mm] H20 FOR THE EXHAUST AND 1 0" [254mm] H20 FOR EXHAUST SYSTEM WITH HEAT RECOVERY.

A. SATURN INLET AMBIENT TEMPERATURE RANGE FROM -65'F ( -53.8'C) TO 140F (60'C)

MAXIMUM EXHAUST TEMPERATURE 910'F (488'C)

MAXIMUM EXHAUST GAS FLOW 28000 CFM ( 784 M3/MIN)

MAXIMUM AIR INLET FLOW VOLUME 12000 CFM (339 M3/MIN

IF NORMAL OPERATING TEMPERATURE OF TURBINE IS OUTSIDE OR EXCEEDS TIHE AMBIENT TEMPERATURE RANGE CONSULT SOLAR ENGINEERING. REFERENCE SOLAR SPECIFICATION ES 1733.

2.13 THE BELLOWS IS TO BE STRETCHED TO FIT USING EQUALLY SPACED STRETCHING BOLTS. TYPICALLY, THE MATING FLANGE IS LOCATED SUCH THAT THE COLD INSTALLED LENGTH OF TIHE BELLOWS IS 17" [ 432mm]. THE SPRING RATE OF THE BELLOWS IS 83 LIBS/IN. (1.5 KG/MM) AND THE FREE LENGTH OF THE BELLOWS IS 16" [ 406mm]. THE THERMAL GROWTH OF THE EXHAUST COLLECTOR IS 3/16" [5mm].

I 3 I 2 I

2.14 THE EXHAUST COLLECTOR AND COMBUSTOR DRAIN ARE INTERCONNECTED AND WILL COLLECT ANY WATER IN THE EXHAUST STACK FROM RAIN, SNOW, ETC., AND SHOULD BE PIPED TO A SUITABLE CONTAINER.

2.15 TOTAL PACKAGE HEAT REJECTION (CONVECTIVE AND RADIATIVE) IS APPROXIMATELY 110,000 BTU/HR (116057 KJ/HR) EXCLUSIVE OF OIL COOLIER AND DRIVEN EQUIPMENT HEAT LOAD AT NORMAL OPERATING CONDITIONS.

2.16 DIRECTION REFERENCES TO THE PACKAGE - LEFT SIDE, RIGHT SIDE, FORWARD, AND AFT ARE ESTABLISHED BY VIEWING THE PACKAGE FROM THE EXHAUST END (AFT), LOOKING FORWARD TO THE AIR INLET (FWD).

2.17 NOTE NOT USED.

2.1 8 SUPPLIED BY OTHERS.

2.19 NOTE NOT USED.

2.20 NOTE NOT USED.

2.21 CUSTOMER SHOULD INSTALL LOCKABLE ISOLATING VALVES FOR ALL EXTERNALLY SUPPLIED, PRESSURIZED NATURAL GAS SOURCES. VALVES TO BE LOCATED IN A READILY ACCESSIBLE AND SAFE AREA (AWAY FROM POSSIBLE FIRE OR GAS RELEASE ZONES). GAS FUEL AND GAS START SYSTEM OFFSKID SUPPLY LINES SHOULD FEATURE VALVES THAT ARE LOCKABLE ONLY IN THE CLOSED POSITION. GAS SUPPLY LINE VALVES FOR EMERGENCY LUBE OR SEAL OIL PUMP APPLICATIONS REQUIRE A CUSTOMER HAZ-OP STUDY TO DETERMINE THE MOST APPROPRIATE LOCKING CONFIGURATION.

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO.

3M511-149607

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START SYSTEMS

3.0 PRIOR TO STARTING THE ENGINE, ENSURE THAT THE TURBINE AIR INLET DRAIN CHECK VALVE IS NOT RESTRICTED AND THAT THE AIR INLET DUCT IS FREE OF ACCUMULATED WATER. THE AIR INLET DUCT SHALL BE FREE OF COMBUSTIBLE AND CORROSIVE ELEMENTS.

3.1 PNEUMATIC STARTER INLET GAS FLOW IS 1034 SCFM [29.3 NM3/MIN] MAXIMUM AND MUST BE EXTERNALLY REGULATED BETWEEN 120 PSIG [827 kfb G] AND 150 PSIG [1034 kPc G] AT THE PACKAGE CONNECTION. MAXIMUM GAS USED PER START IS 3074 SCF [86.5 NM3] BASED ON A 30 SECOND PURGE TIME.

3.2 STARTER EXHAUST FLOW RATE IS 1034 SCFM [29.3 NM3/MIN] AND MAXIMUM ALLOWABLE VENT BACK PRESSURE IS 5 PSIG [34.5 kPa G]. WHEN GAS IS USED, THIS VENT MUST BE CONNECTED TO A SAFE LOCATION OR COLLECTOR. THE EXTERNAL STARTER VENT PIPE MUST BE FULLY SELF-SUPPORTING.

3.3 NOTE NOT USED

3.4 NOTE NOT USED

FUEL SYSTEMS

4.0

4.1

4.2

GAS FUEL IS TO BE IN ACCORDANCE WITH SOLAR SPECIFICATION ES 9-98. NO LIQUIDS ARE ALLOWED IN THE FUEL GAS. SOLAR RECOMMENDS THE FUEL TEMPERATURE TO BE AT LEAST 50'F (28'C) ABOVE THE DEW-POINT TEMPERATURE OF BOTH THE NATURAL GAS LIQUIDS AND WATER AT SKID EDGE. IF THE FUEL GAS EXCEEDS THE SYSTEM COMPONENT CAPABILITIES. CONSULT SOLAR ENGINEERING. MAXIMUM FLOW DEMAND RATE IS 375 SCFM /MIN). MINIMUM FUEL PRESSURE REQUIRED AT PACKAGE CONNECTION IS 150 PSIG (1034 KPAG). MAXIMUM FUEL SYSTEM PRESSURE RATING IS 180 (1241 KPAG) THE ACTUAL MINIMUM FUEL ACCEPTABLE PRESSURE IS A FUNCTION OF AMBIENT TEMPERATURE IF AMBIENT CONDITIONS ARE WARMER, A LOWER FUEL PRESSURE CAN BE USED. PLEASE CONSULT SOLAR ENGINEERING FOR ASSISTANCE. IT IS RECOMMENDED THAT A QUICK CLOSING AND EASILY ACCESSIBLE HAND OPERATED VALVE BE INSTALLED IN THE EXTERNAL SUPPLY LINE TO PROVIDE IMMEDIATE SHUTOFF CAPABILITY. GAS FUEL OPERATION TEMPERATURE IS BETWEEN -40'F ( -40'C) AND 200'F (71'C). OPERATION ABOVE 160'F (93'C) WILL SHORTEN THE LIFE OF FUEL SYSTEM COMPONENTS.

CLEAN AND DRY PILOT AIR SUPPLY IS REQUIRED FOR GAS FUEL VALVE OPERATION. REGULATED SUPPLY PRESSURE MUST BE BETWEEN 100 PSIG (689 KPAG) AND 200 PSIG (1379 KPAG) PER ES 2201. MAXIMUM FLOW RATE OF LESS TIHAN 10 SCFM. TOTAL PILOT VENT VOLUME PER START OR SHUTDOWN IS APPROXIMATELY 6 SCF. SEE WARNING NOTE 10.B.

GAS FUEL SYSTEM VENT FLOW RATE IS 2 SCFM (0.05 SM3/MIN) FOR 1 /2 SECOND. THE GAS FUEL VENT MUST BE CONNECTED TO A SAFE LOCATION OR COLLECTOR. MAXIMUM ALLOWABLE BACK PRESSURE 5 PSIG (34 KPAG). THE VENT TERMINATION SHALL AFFORD PROTECTION FROM RAIN AND SNOW BY MEANS OF A SHIELD OR BY PIPE GEOMETRY AND BE SCREENED TO PREVENT ENTRY OF LARGE FOREIGN OBJECTS. SEE WARNING NOTE 1 0.8.

I 5 4

B. PACKAGE HEAT LOAD: COOLER REJECTION CAPACITY: MAX OIL FLOW: MAX. AMBIENT TIEMP.: MAX. DESIGN LUBE OIL COOLER OUTLET TIEMPERATURE:

I

204,000 BTU/HR (215,230 KJ/HR) 225,000 BTU/HR (237,386 KJ/HR) 56 GPM (212 L/MIN) 110 T (43.3 'C) C46 OILS: 165 'F (73.8 ·c)

C. PREVAILING WINDS MUST BE CONSIDERED TO PREVENT THE LUBE OIL COOLER FROM EXHAUSTING INTO THE ENGINE AIR INLET SYSTEM OR FROM TAKING AIR IN FROM THE ENGINE EXHAUST SYSTIEM.

5.3 THE EXTIERNAL OIL TANK VENT PIPE MUST BE SELF-SUPPORTING AND HAVE AN UPWARD SLOPE OF .25" PER FOOT [21 MM/M ] WITH NO TRAPS OR RESTRICTIONS AND MUST BE ROUTED SUCH THAT OIL VAPORS WILL NOT MIX WITH TURBINE INLET OR :fXHAUST GAS. THE TANK VENT AIR AND OIL VAPOR FLOW IS APPROXIMATIELY 30 SCFM (0.2 NM /MIN.). MAXIMUM ALLOWABLE VENT PIPING

~~6~S~~~N L~~~ ~N:0B~~HE1~~] 0~2~· sHYf~ri 6:~:EP~~~N~~g~E~~L~N';iF~:Ds~~~~Egl~~ PREVENT ENTRY OF LARGE FOREIGN OBJECTS. THE FLAME ARRESTOR, WHEN INSTALLED, WILL PREVENT POSSIBLE FLASH BACK INTO THE LUBE OIL TANK. SEE WARNING NOTE 1 0.8. (REFERENCE SOLAR SPECIFICATION ES 1740.)

5.4 NOTIE NOT USED.

5.5 NOTIE NOT USED.

5.6 NOTIE NOT USED.

5.7 THE FLAME ARRESTOR IN CONJUNCTION WITH APPROVED AIR/OIL SEPARATOR MUST BE USED WHEN THE OIL TANK VAPORS ARE TO BE DISPERSED BY TURBINE EXHAUST DRAFT. THE FLAME ARRESTOR IS NOT INTIEGRAL WITH THE PACKAGE AND MUST BE LOCATIED AND INSTALLED SEPARATELY. THE FOLLOWING INSTALLATION REQUIREMENTS APPLY. (REFERENCE SOLAR SPECIFICATION ES 1745):

A. THE FLAME ARRESTOR IS REQUIRED TO PREVENT FIRE FLASHBACK INTO THE OIL TANK AND SHALL BE INSTALLED AS CLOSE TO THE EXHAUST DRAFT AS POSSIBLE.

B. THE VENT PIPE TO THE FLAME ARRESTOR MUST CONFORM TO REQUIREMENTS OF NOTE 5.3.

5.8 MECHANICAL CONNECTION 31, ENGINE SEAL VENT, DOES NOT REQUIRE AN EXTIERNAL CONNECTION THE LINE MUST BE LEFT OPEN TO THE ATIMOSPHERE. EXCESSIVE OIL LEAKAGE FROM THIS PORT (ENGINE FRONT BEARING) INDICATIES THE NEED FOR CORRECTIVE ACTION.

ELECTRICAL SYSTEMS

6.0 PACKAGE ELECTRICAL INSTALLATION REQUIREMENTS ARE AS SHOWN ON ELECTRICAL SCHEMATIC NO. 3H671-149450 AND WIRING DIAGRAM NO. 3H671-149451.

6.1 NOTIE NOT USED.

3

6.2 GROUNDING LUGS/BUS BARS ARE PROVIDED FOR SEPARATELY GROUNDING THE PACKAGE FRAME, CONTROL CONSOLE/BOX, AND BATTERY CHARGER TO THE CUSTOMERS GROUNDING CONDUCTOR. GROUNDING CONDUCTOR TO BE SIZED IN ACCORDANCE WITH REQUIREMENTS OF APPLICABLE ELECTRICAL CODES. LUG/BUS BAR SURFACE TO BE FREE OF DIRT, GRIME, PAINT AND OIL TO ALLOW METAL-TO-METAL CONTACT. LUG/BUS BAR ALSO SUITABLE FOR CONNECTION OF MAIN BONDING JUMPER FOR GROUNDING SYSTIEMS. MAIN BONDING JUMPER TO BE SIZED IN ACCORDANCE WITH THE APPLICABLE ELECTRICAL CODE.

THE CONTROL SYSTEM MAY HAVE UP TO 4 DIFFERENT GROUND CLASSIFICATIONS TO ADDRESS PERFORMANCE AND PROTIECTION. EVERY CONTROL CONSOLE/BOX WILL REQUIRE AT LEAST ONE (1) OF THESE GROUND CONNECTION. REFERENCE THE ELECTRICAL SCHEMATIC FOR SPECIFIC DETAILS AND

LUBE SYSTEMS CONNECTION LOCATIONS.

5.0 A. LUBE OIL USED IN TIHIS PACKAGE MUST BE IN ACCORDANCE WITIH SOLAR SPECIFICATION ES 9-224. INITIAL FILL OF TIHE PACKAGE OIL TANK SHALL FULLY COMPLY WITIH OIL CLEANLINESS LEVEL ISO 14/12. TIHE FOLLOWING EQUIPMENT AND PROCEDURES ARE RECOMMENDED TO OBTAIN TIHE REQUIRED CLEANLINESS LEVEL:

-- A HIGH EFFICIENCY (3 MICRON) OIL FILTER INSTALLED AT TIHE FlLL HOSE DISCHARGE END. -- ALL HOSES, CONNECTORS. ETC .. SHOULD BE PRE-FLUSHED (USING AN OIL COMPATIBLE FLUID AT REYNOLDS NUMBER 4000) TO AN ISO 14/12 CLEANLINESS LEVEL AND NO PARTICLE COLLECTED ON A 100 MESH SCREEN AFTER A ONE HOUR FLUSHING PERIOD. -- TIHE DISPENSING OIL STORAGE TANK AND ITS BULK FILL SHOUUD BE PRE-FILTERED TO ISO 14/12 PRIOR TO TIHE PACKAGE OIL TANK FlLL OPERATION.

B. TIHE PACKAGE OIL TANK CAPACITY AT FULL LEVEL (SYSTEMS OPERATING) IS 100 GALLONS (379 UTTERS). AN ADDITIONAL 35 GALLONS (133 LITTERS) ARE REQUIRED FOR PACKAGE FILTERS AND PIPING. TIHE OIL COOLER CAPACITY IS 5 GALLONS (18.9 LITTERS) TOTAL REFER TO NOTE 5.2 FOR EXTERNAL PIPING REQUIREMENTS.

5.1 TIHE LUBE OIL SHALL HAVE A POUR POINT WHICH IS AT LEAST 11T (6'C) BELOW TIHE MINIMUM AMBIENT TEMPERATURE TO INSURE FLOW IN EXPOSED LINES AND VESSELS. TIHE MAXIMUM OIL VISCOSITY IN TIHE LUBE OIL TANK FOR STARTUP IS 700 SSU (154 CENTISTOKES). CONTROL SYSTEM PROHIBITS PACKAGE FROM STARTING UNLESS LUBE OIL TEMPERATURE REACHES AT LEAST 65T (18'C). REFERENCE SOLAR SPECIFICATION ES 9-224.

5.2 A. THE PACKAGE OIL COOLER IS NOT INTIEGRAL WITH THE PACKAGE AND MUST BE LOCATIED AND INSTALLED SEPARATIELY. THE FOLLOWING INSTALLATION REQUIREMENTS APPLY:

1. THE TOP OF THE COOLER SHALL NOT BE MORE THAN 30' [9144 mmL-.., ABOVE THE BOTTOM OF THE PACKAGE FRAME. REFERENCE PLANE i..::£=j.

2. THE TOTAL OIL VOLUME OF THE 'OUTGOING' AND 'RETURN' LINES EXCLUDING COOLER SHALL BE LIMITIED TO 35 GALLONS (132.5 LITTERS). THIS IS TO PREVENT OIL TANK FLOODING DURING DRAIN BACK.

3. EITHER COOLER HEADER MAY BE USED FOR OIL INLET AND THE OTHER FOR OIL OUTILET.

4. THE MAXIMUM TOTAL DESIGN PRESSURE DROP OF THE COMBINED 'OUTGOING' AND 'RETURN' LINES AND COOLER SHALL NOT EXCEED 50 PSID (344.7 kPa DIFF) AT 80 GPM (302.8 LITERS/MIN) FLOW, USING AN OIL VISCOSITY OF 10.5 CS (60 SSU). COOLER DP AT THIS CONDITION IS 10 PSID (68.9 kPa DIFF). NO CHECK VALVES ARE ALLOWIED IN THE OIL COOLER LOOP. OIL COOLER SUPPLY • RETURN AND OPTIONAL VENT VENT LINES MUST SLOPE FROM THE OIL COOLER TO THE TURBINE PACKAGE TO FACILITATIE DRAINING WHEN THE UNIT IS NOT OPERATING. SEE WARNING NOTE 10.8.

6.3 THE TURBOTRONIC CONTROL IS CONTAINED IN A DUST TIGHT, STIEEL CONSOLE/BOX DESIGNED TO LIMIT THE EFFECTS OF ELECTROMAGNETIC INTIERFERENCE. THE CONTROL CONSOLE/BOX IS DESIGNED WITH INTIERNAL FANS TO PROVIDE AIR CIRCULATION WITHIN THE CONSOLE/BOX TO THE HEAT GENERATING COMPONENTS.

THE CONTROL CONSOLE (IF USED) MUST BE LOCATIED IN A CLEAN, DRY ENVIRONMENT CONSISTENT WITH GOOD OPERATING PRACTICES FOR PLC AND COMPUTIER SYSTIEMS. ENVIRONMENTAL CONDITIONS WITHIN 32 DEG F (0 DEG C) AND 122 DEG F (50 DEG C) WITH 95 PERCENT NON-CONDENSING HUMIDITY ARE REQUIRED.

THE EXACT LOCATION FOR EXTIERNAL CONNECTIONS INTO THE CONTROL CONSOLE/BOXES IS TO BE DETIERMINED ON THE SITIE DURING INSTALLATION. THE AREA AVAILABLE IN THE CONSOLE/BOX FOR THESE CONNECTIONS IS SHOWN. THE CONSOLE/BOXES ARE SUPPLIED WITH FACTORY CUTOUTS AND REMOVABLE GLAND PLATIES ON THE BOTTOM.

6.4 AC AND DC CIRCUITS MUST BE RUN SEPARATELY FROM EACH OTHER TO AVOID ELECTRICAL CONTROL INTIERFERENCE PROBLEMS. INTRINSICALLY SAFE CIRCUITS MUST BE SEPARATIE FROM NON-INTRINSICALLY SAFE CIRCUITS.

6.5 BATTERIES AND BATTIERY CHARGER ARE DEDICATED TO THE SOLAR ELECTRICAL SYSTEM AND MUST NOT BE SHARED WITH OTHER SITIE/CUSTOMER SYSTEMS WITHOUT WIRITTEN APPROVAL FROM SOLAR ENGINEERING.

6.6 NOTIE NOT USED.

6.7 AN ADDITIONAL WIRING LENGTH ALLOWANCE SHOULD BE MADE FROM SKID EDGE TO TERMINATION AT THE ELECTRICAL COMPONENTS.

6.8 REFER TO THE LOCAL CONTROLLING ELECTRICAL CODE TO DETIERMINE THE REQUIREMENTS FOR CONDUIT SEALS. WHERE ELECTRICAL CONDUIT AT THE SKID EDGE PASSES FROM CLASS 1, GROUP D, DIY. 2 TO AN UNCLASSIFIED LOCATION, SEALING REQUIREMENTS MUST BE FOLLOWED.

6.9 REFERENCE HEAT REJECTED BY:

CONTROL CONSOLE - 400 WATTS (1366 BTU /HR)

I 2 I

SEAL SYSTEM

7.0 NOT REQUIRED FOR GENERATOR SETS.

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO.

3M511-149607

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ENCLOSURE SYSTEMS

8.1 ENCLOSURE IS EQUIPPED Wl"fl-1 A FIRE DETECTION/SUPPRESSION SYSTEM. CONSISTING OF MULTI-SPECTRUM FLAME DETECTORS AND RATE COMPENSATED HEAT DETECTORS. TIHE EXTINGUISHANT DISCHARGE PRESSURE ACTIVATES PNEUMATICALLY RELEASED FIRE DAMPERS ON ALL VENT OPENINGS.

FIRE EXTINGUISHANT CABINET SHIPS LOOSE FOR FIELD INSTALLATION BY OTIHERS.

CABINET MUST BE LOCATED NO MORE TIHAN 50 LINEAR FEET [15.2 m ] OF THE ENCLOSURE CONNECTION.

ALL INTERCONNECT PIPING, FOR THE PRIMARY SYSTEM TO BE 3/4" PIPE. ALIL INTERCONNECT PIPING, FOR EXTENDED SYSTEM, TO BE 1/2" PIPE. ASTIM-A-53 OR ASTIM-A-106, SCHEDULE 40 PIPE SHOULD BE USED FOR INTERCONNECT, RUNS SHOULD BE ROUTED TO MINIMIZE PIPE LOSS. REDUCERS MAY BE REQUIRED AT EXTINGUISHANT CONNECTIONS TO ACCOMMODATE CALCULATED INTERCONNECT PIPING. REMOVE DISCHARGE NOZZLIES AND BLOW OUT ALL PIPING AFTER INTERCONNECT PIPING IS COMPLETE.

TO PREVENT EXTINGUISHANT LEAKAGE ENSURE TIHE FOLLOWING:

- SKID BASE IS SEALED AFTER CONDUIT/PLUMBING INSTALLATION IS COMPLETE. ALL UNUSED AND/OR OVERSIZED HOLES MUST BE SEALED.

- INSPECT TIHE UNIT FROM WITIHIN FOR DAYLIGHT. SEAL ANY OPEN AREAS.

EXTINGUISHANT SHOULD BE LOCATED IN AN ENVIRONMENT PROTECTED FROM TIHE WEATIHER AND WHERE TIHE AMBIENT TEMPERATURE DOES NOT EXCEED +130"F (54"C) NOR FALL BELOW -40"F (-40"C).

8.2 ANCILILARY EQUIPMENT SKID AND ENCLOSED PACKAGE SHIP SEPARATELY. TIHESE INTERCONNECTIONS ARE TO BE MADE DURING FIELD ERECTION.

8.3 A MAINTENANCE FRAME AND TROLILEY RAIL ARE BUlL T INTO TIHE ENCLOSURE STRUCTURE. ENGINE MAY BE REMOVED OUT RIGHT SIDE.

8.4 ONE (1) 1-TON (907 KG) TROLLEY HOIST AND ONE (1) 1 0-FOOT [3148 mm] TROLILEY BEAM EXTENSION ARE SUPPLIED WITIH UNIT. TIHESE ITEMS ARE SHIPPED LOOSE.

8.5 ENCLOSURE IS EQUIPPED WITIH THREE (3) FLUORESCENT LIGHTS WITIH DC BACKUP AND ONE (1) EXPLOSION PROOF LIGHT SWITCH.

8.6 VENTILATION INLET AND EXHAUST SYSTEM EQUIPMENT SHIP SEPARATELY FROM ENCLOSED PACKAGE.

6

THESE INTERCONNECTIONS ARE TO BE MADE DURING FIELD ERECTION. INTERCONNECTING HARDWARE IS SUPPLIED BY SOLAR TURBINES.

8. 7 ENCLOSURE IS EQUIPPED WITIH GAS DETECTION SYSTEM.

8.8 ENCLOSURE IS EQUIPPED WITIH A RTD FOR HIGH TEMPERATURE ALARM.

8.9 ENCLOSURE IS CONSTRUCTED OF 14 GAGE STEEL SIDE PANELS AND 12 GAGE STEEL ROOF PANELS WITIH 2" [51] FIBERGLASS INSULATION AND PERFORATED STEEL LINER. ALL SIDE AND ROOF

9.0

9.1

PANELS ARE REMOVABLE FOR EQUIPMENT ACCESS. ALL HINGES, LATCHES AND DOOR HANDLES ARE 316SS.

ENGINE CLEANING

TURBINE CLEANING SUPPLY CONNECTION 122 MUST BE CAPPED, OR PLUGGED WHEN NOT IN USE TO AVOID THE ENTRANCE OF DIRT, AND DEBRIS. (IT IS SUGGESTED THAT A HAND OPERATED VALVE BE INSTALILED AT THE PACKAGE SKID CONNECTION FOR EASE OF MAINTENCE.) USE CONNECTION 122 FOR ON-CRANK CLEANING ONLY. FOR ON-CRANK AND ON-LINE CLEANING THE WATER/SOLVENT SOLUTIONS SUPPLY IS TO BE REGULATED BETWEEN 85 PSIG AND 100 PSIG (586.1 KPAG AND 689.5 KPAG) AT THE PACKAGE SKID CONNECTION. THE FLUID TEMPERATURE SHOULD BE AT AMBIENT CONDITIONS EXCEPT IN EXTREME COLD AMBIENTS. PLEASE REFER TO ES 9-62 OR THE OPERATIONS AND MAINTENANCE MANUAL FOR ADDITIONAL TURBINE CLEANING REQUIREMENTS AND PROCEDURES. WASH FLOW RATES AND TREATIMENT QUANTITIES PER WASH CYCLE ARE SHOWN IN THE TABLE BELOW.

I ON-CRANK FLOW I TREATMENT QUANTITY I I 2.1 GPM (7.9 LITERS/MIN) 110 GAL (37.9 LITERS) I

WHEN AMBIENT TEMPERATURES FALIL BELOW 50"F (10"C), CONSULT SOLAR SPECIFICATION ES 9-62 AND THE OPERATION AND MAINTENANCE MANUAL FOR PROPER COLD WEATHER OPERATING PROCEDURES.

9.2 NOTE NOT USED.

9.3

9.4

THE TURBINE AIR INLET DUCT MUST BE FREE OF ALL ACCUMULATED WATER AND SOLVENTS PRIOR TO STARTING THE TURBINE. INSURE THAT THE TURBINE AIR INLET DUCT AND DRAINS ARE COMPLETELY DRAINED AFTER CLIEANING AND NOT TERMINATED IN A COMBUSTIBLE ENVIRONMENT.

NOTE NOT USED.

MISCELLANEOUS NOTES

10.0 NOTE NOT USED.

10.1 NOTE NOT USED.

10.2 TIHESE ITEMS SHIP LOOSE WITIH ATIACHING HARDWARE REQUIRED FOR FIELD INSTALLATION.

10.3 NOTE NOT USED.

I 5 4

10.4 NOTE NOT USED.

10.5 NOTE NOT USED.

10.6 SOLAR-SUPPLIED FILTER IS TO BE INSTALLED IN TIHE GAS FUEL SYSTEM EXTERNAL SUPPLY LINES AT OR AS CLOSE TO TIHE PACKAGE CONNECTION AS POSSIBLE. REFER TO SHEET 23 FOR FILTER REMOVAL CLIEARANCE.

10.7 GENERATOR COOLING AIR FLOW IS APPROXIMATELY 6000 CFM (170 NM 3 /MIN). GENERATOR EXHAUST HEAT REJECTION IS APPROXIMATELY 206,000 BTU/HR (217,000KJ/HR) AT NORMAL OPERATION CONDITIONS. TOTAL PACKAGE HEAT REJECTION IS APPROXIMATELY 330,000 BTU/HR (348,000 KJ/HR).

10.8 WARNING: FAILURE TO LIMIT BACK PRESSURE TO SPECIFIED VALUE CAN RESULT IN SYSTEM OR COMPONENT MALFUNCTION AND CAN CAUSE PERSONAL INJURY OR DEATIH AND/OR PROPERTY DAMAGE. TIHE USE OF BLOCK VALVES IN THE VENTS IS STRONGLY NOT RECOMMENDED.

WARNING: IF TIHE EQUIPMENT WILL BE USING COMBUSTIBLE GAS FOR SERVICE, CARE MUST BE TAKEN TO PROPERLY VENT TIHE EXHAUST TO A SAFE LOCATION.

TURBINE EXHAUST SYSTEM

11.0 GENERAL EXHAUST SYSTEM DESIGN GUIDELINES:

A. SUPPORT OF TIHE EXHAUST SYSTEM SHOULD PREVENT DAMAGE TO SOLAR TURBINES SUPPLIED COMPONENTS DUE TO THERMAL EXPANSION. SEE PACKAGE INSTALLATION SECTION OF TIHE NOTES FOR APPLICABLE PACKAGE LIMITS AND CRITERIA.

B. MOUNTING BRACKETS MAY BE WELDED TO THE SHELIL OF THE DUCTING. TIHE TYPICAL METAL TIHICKNESS AND TYPE IS 3/16 IN (5 MM) TIHICK AND ASTM A515 UNLESS OTIHERWISE STATED IN TIHESE NOTES.

C. TIHE EXPANSION JOINT, (IF SUPPLIED) WILL NOT SUPPORT TIHE WEIGHT OF DUCTING OR COMPONENTS. TIHE ALLOWABLE DISPLACEMENTS OF TIHE EXPANSION JOINT ARE : AXIAL ~ 1 1/2 IN (38 MM), LATERAL ~ 1/2 IN (13 MM), RADIAL ~ 0 DEGREES. TIHE EXPANSION JOINT HAS NO APPRECIABLE SPRING RATE.

11.1 WHEN ASSEMBLING OR DISASSEMBLING TIHE SYSTEM, USE TIHE LIFTING LUGS PROVIDED TO HANDLE EACH COMPONENT INDIVIDUALLY. EMPLOY INDUSTRY ACCEPTED LIFTING TECHNIQUES WHEN LIFTING LUGS ARE NOT PROVIDED. REFlER TO COMPONENT WEIGHTS AND ASSUME A GEOMETRIC CENTER OF GRAVITY. DO NOT USE TIHE LIFTING LUGS FOR PERMANENT MOUNTING, (SEE NOTE 11.0, PARAGRAPH B).

11.2 TIHE DRAIN CONNECTIONS SHOWN ON TIHE ANCILLARY COMPONENTS ARE DESIGNED TO REMOVE EXCESSIVE AMOUNTS OF RAIN OR MOISTURE FROM TIHE SYSTEM DURING EXTENDED SHUT DOWN PERIODS. CONNECTION TO TIHESE DRAINS IS OPTIONAL FOR TIHE CUSTOMER. RAIN AND MOISTURE IS ALSO REMOVED VIA TIHE EXHAUST COLLECTOR DRAIN ON THE PACKAGE.

11.3 ATIACHING HARDWARE KITS ARE INCLUDED FOR ALL FLANGES IN SOLAR TURBINES SCOPE OR TIHE TURBINE EXHAUST INTERFACE FlLANGE, (AS APPLICABLE). HARDWARE IS NOT SUPPLIED FOR ANY OTIHER DOWNSTREAM CONNECTIONS. HARDWARE IS NOT SUPPLIED FOR FOUNDATION OR SUPPORT STEEL INTERFACES, UNLESS INCLUDED IN SOLAR TURBINES SCOPE.

11.4 TIHE STATIC PRESSURE DROP ACROSS ALL ITEMS SHOWN ON TIHIS INSTALLATION DRAWING IS LIESS TIHAN

~~ :FfE~s~~~ ~~0~ t'/ ~A *Dg~~~~~L g~~~~~EO~H~~~gE~E S~~~~~C~D OF~~:s~~ ~~~~WABLE DROP ALLOCATED FOR IN THE TURBINE PERFORMANCE GUARANTEE.

11.5 INDIVIDUAL COMPONENTS OF TIHE TURBINE EXHAUST SYSTEM ARE DESIGNED TO WITIHSTAND A WINDLOAD OF 120 MI/HR (193 KM/HR) OR 0.5G LATERAL ACCELERATION. ASSEMBLIES OF INDIVIDUAL COMPONENTS CANNOT BE CONSIDERED TO BE STRUCTURALLY ADEQUATE TO TIHE SAME LOADS WITIHOUT ADDITIONAL ENGINEERING. (NON-STANDARD SYSTEMS REQUIRE ADDITIONAL ANALYSIS)

11.6 BARE METAL EXHAUST SURFACES TYPICALLY OPERATE AROUND 900 DEG F (482 DEG C). PERSONNEL PROTECTION IS RECOMMENDED AND CARE MUST BE TAKEN IN THE LOCATION OF HOT EXHAUST SURFACES. DO NOT LOCATE EXHAUST COMPONENTS ON OR NEAR FLAMMABLE SURF ACES.

11.7 TIHE ALLOWABLE FLANGE LOADS ON TIHE EXHAUST SILENCER, (IF SUPPLIED) ARE 2000 LBS (907 KG) DEAD LOAD, 750 LBF (3.3 KN) SHEAR AND 5400 LBS*FT (7.3 KN*M) MOMENT. CARE SHOULD BE TAKEN TO ENSURE TIHAT TIHE STACK DESIGN DOES NOT EXCEED TIHESE LOADS.

TURBINE AIR INLET SYSTEM

12.0 A MINIMUM CLEARANCE OR CLEAR AREA IS REQUIRED TO SERVICE TIHE FILTER ELEMENTS AND TO ENSURE PROPER AIRFLOW TO TIHE TURBINE. DO NOT BLOCK DOOR SWINGS OR ACCESS AREAS.

12.1 MOUNTING BRACKETS MAY BE WELDED TO TIHE SHELL OF TIHE DUCTING. TIHE TYPICAL METAL TIHICKNESS AND TYPE IS 10 GAUGE, (0.134 IN (3.4 MM) TIHICK NOMINAL), AND ASTM A36/A569 UNLESS OTHERWISE STATED IN TIHESE NOTES. DO NOT WELD ON FILTERS, EVAPORATIVE COOLIERS OR SILENCERS. WELDING ON TIHESE DEVICES MAY RESULT IN FIRE OR DAMAGE TO TIHE DEVICE.

12.2 WHEN ASSEMBLING OR DISASSEMBLING TIHE SYSTEM, USE TIHE LIFTING LUGS PROVIDED TO HANDLE EACH COMPONENT INDIVIDUALLY. EMPLOY INDUSTRY ACCEPTED LIFTING TECHNIQUES WHEN LIFTING LUGS ARE NOT PROVIDED. REFER TO COMPONENT WEIGHTS AND ASSUME A GEOMETRIC CENTER OF GRAVITY. DO NOT USE THE LIFTING LUGS FOR PERMANENT MOUNTING, (SEE NOTE 12.1 ).

12.3 UNLESS OTIHERWISE STATED ALL STRAIGHT SECTIONS OF INLET DUCTING ARE A KNOCKDOWN DESIGN WITIH APPROXIMATELY 100 BOLTED CONNECTIONS PER DUCT. ALL ASSEMBLY AND ATIACHING HARDWARE IS SUPPLIED IN KIT FORM WITH TIHE DUCTING.

12.4 ATIACHING HARDWARE KITS ARE INCLUDED FOR ALL FLANGES IN SOLAR SUPPLIED COMPONENTS OR THE TURBINE INLET INTERFACE FLANGE, (AS APPLICABLE). HARDWARE IS NOT SUPPLIED FOR ANY OTIHER UPSTREAM CONNECTIONS. HARDWARE IS NOT SUPPLIED FOR FOUNDATION OR SUPPORT STEEL INTERFACES, UNLESS INCLUDED IN SOLAR SCOPE.

12.5 INDIVIDUAL COMPONENTS OF TIHE TURBINE INLET SYSTEM ARE DESIGNED TO WITIHSTAND A WINDLOAD OF 120 MI/HR (1 93 KM/HR) OR 0.5G LATERAL ACCELERATION. ASSEMBLIES OF INDIVIDUAL COMPONENTS CANNOT BE CONSIDERED TO BE STRUCTURALIL Y ADEQUATE TO TIHE SAME LOADS WITHOUT ADDITIONAL ENGINEERING. (NON-STANDARD SYSTEMS REQUIRE ADDITIONAL ANALYSIS)

12.6 TIHE TOTAL PRESSURE DROP ACROSS ALL ITEMS SHOWN ON TIHIS INSTALLATION DRAWING IS

~;E~~u~tD~~~ ~~ ~~·D1~c~~~TIS~NO~L~UB~TI~~B~~Ag~~EF~g~NT~:~L~~:::L~S P~~~~U~~EDROP IN TIHE TURBINE PERFORMANCE GUARANTEE.

I 3 I 2 I

12.7 TIHE DRAIN CONNECTIONS SHOWN ON TIHE ANCILLARY COMPONENTS ARE DESIGNED TO REMOVE EXCESSIVE AMOUNTS OF RAIN OR MOISTURE FROM THE SYSTEM DURING EXTENDED SHUT DOWN PERIODS. CONNECTION TO TIHESE DRAINS IS OPTIONAL FOR TIHE CUSTOMER. RAIN AND MOISTURE IS ALSO REMOVED VIA TIHE EXHAUST COLLECTOR DRAIN ON TIHE PACKAGE.

12.8 DUCTING DESIGN, IF DONE BY OTHERS, SHOULD FOLLOW API 616/RP 11-PGT AND/OR SMACNA AND/OR SOLAR ES 1733 STANDARDS AND SPECIFICATIONS. RECOMMENDED WALL TIHICKNESS IS NOT LESS TIHAN 10 GAUGE, (0.134 IN (3.4 MM) THICK NOMINAL), WITIH 1 IN X 1 IN X 1/8 IN (25 MM X 25 MM X 3 MM) ANGLE STIFFENERS ON 4 FT (1219 MM) SPACING MINIMUM. LEAKS IN DUCTING OR DUCTING INTERCONNECTS CANNOT BE ALLOWED AND MAY CAUSE ENGINE DAMAGE OR FREQUENT ENGINE MAINTENANCE. CARE SHOULD BE TAKEN IN TIHE DESIGN TO ENSURE TIHAT NO LOOSE OBJECTS CAN BE INGESTED INTO THE ENGINE. TIHE DESIGN PRESSURE DIFFERENTIAL FOR TIHE DUCTING

~~~~~D T~E B~O A~~~~A~A~O~O ~~L <g~~R~~~~ t~.N~io~~S~FN ~~R~~~~~EE~S A~~~~~~~ ~~~~ ~~~SI~~~N CONDITIONS OTIHER TIHAN NOMINAL OPERATING SUCH AS LIGHT-OFF, FLAME-OUT OR COMPRESSOR SURGE/STALL.

12.9 NOTE NOT USED

12.10 DO NOT INSTALIL TIHE AIR INLET FILTER IN CLOSE PROXIMITY TO THE EXHAUST STACK. AIR HEATED BY TIHE EXHAUST STACK AND INGESTED BY TIHE AIR INLET FILTER WILL REDUCE ENGINE PERFORMANCE.

12.11 FOR DETAILED INFORMATION ON TIHE AIR FILTER, REFER TO VENDOR SUPPLIED INSTALLATION, OPERATION, AND MAINTENANCE MANUAL INCLUDED IN TIHE SOLAR TURBINES OPERATION AND MAINTENANCE SUPPLEMENTAL DATA. AIR FILTER TECHNICAL DATA:

- INITIAL CLEAN DELTA P: 1 IN (25 MM) H 2o

- HIGH DELTA P SET POINTS: 3 IN (76 MM) H20 ALARM, 6 IN (152 MM) H 20 SHUTDOWN.

- HIGH DELTA P SET POINTS: 2 IN (51 MM) H 20 START CLEAN CYCLE, 1.5 IN (38 MM) H20 STOP CLEAN CYCLE.

CLEAN DRY AIR REQUIRED AT 80-100 PSIG (5.6-7.0 KG/CM2) FLOWING 4.5 - 9.0 CFM (.13 - .25 M3/MIN) WHEN CLEANING.

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFAC~

Solar Turbines A Caterpillar Company

DRAWING NO.

3M511-149607

H

G

r--

F

r--

E

D

r--

c

r--

B

1--

A

8 7 6 5

TURBINE AIR INLET SYSTEM

H ITEM DESCRIPTION SOLAR P /N LBS KGS

1 00 SILENCER f-

AX 1260 1 08 525 238 - -FEl 101* DUCT, OFFSET 42" 11 04043-300 257 117

101* DUCT, OFFSET 30" 11 04044-300 240 109

102 DUCT, STRAIGHT 24" AX-1222-1 05 225 102

103 AIR FILTER W/ INSECT SCREEN 1 039339-3M511 1291 586

TURBINE EXHAUST SYSTEM

TEM DESCRIPTION SOLAR P/N LBS KGS

G 200 BELLOWS AX-1619-300 90 41 7'-1 5/8"

201 EXHAUST ELBOW 45' AX-1629-202 126 57 [2175mm] TURBINE AIR I

103

INLET i ro1 • /v u

• • \ ~ 3'-0 5/8"

f----"[930mmJ-

w F. - 2 3/8" 1i6omm] 04044-300)

FFSET)

(P /N-11 04043-300)

ENCLOSURE i (3'-6" OFFSET)

EXHAUST '~ I * 101

~~\ ~ 27

ENCLOSURE +-t (REF)(REF) EXHAUST

12'-11 15/16" [3961mm]

8 '--- --, D I ·+r -/J @

F

E

D . . • "I . . Ia~ C[D 13·: 8'-10 9/16"

. . [2707mm] 2'-1 5/8"

CONN. 3 & 6 r ,~,-~r l Ia~ 13·: . C[D .

- l ___ ' I

~ TURBINE & GENERATOR 1.. 1+--- -- 1- r---------

7 11~ . C[D ~: .

'1t 3'-9"

[1143mm] . . . . . . . . . .

~I 0 D II D 0 li"ii ll Jl

c

t=£=..1

el el 9'-6 7/16" [2906mm]

3'-9 1/2" 21'-10 1/2" -[1156mm] [6668mm] B

23'-3 9/16" [7100mm]

1 1/2" 24'-9 9/16" [38mmJ [7557mm]

25'-3 9/16"

FWD;:::> [7710mm]

PACKAGE ORIENTATION

A rn

RIGHT SIDE ELEVATION

4 3

TURBINE AIR INLET EQUIPMENT AND ENCLOSURE VENTILATION EQUIPMENT TO BE SUPPORTED BY OTHERS THAN SOLAR TURBINES INC.

fJ1~irr IIIII IIIII IIIII IIIII

m-~-T' ::: \\ l.) nf/T ::://

r~~

rJr'"" .mtl ..

. C[D ~

.

' C[D ~

. C[D ~ .. . .

D D

30'-1 9/16" [9183mm]

32'-0 5/16" [9761mm]

2

TABLE EXTERNAL CONNECTIONS

ITEM DESCRIPTION

27 PNEUMATIC START INLET 1 1 /2" 150 LB ANSI RF FLANGE

147 VENT FAN FAIL, LOW PRESSURE

357 AC VOLTS, ENCLOSURE VENT FAN

360 AC VOLTS, BACKUP ENCLOSURE VENT FAN

rB I

II 357

VJ1~:rr l = I

~ IIIII IIIII IIIII IIIII

m-~- t! -ffi--U.

Ill II fLJ nf/T :::// I

r~~ I

= I h

t ENCLOSURE t

AIR INLET

3'-J5/8" [1159mm]

CON . 27

3/8" TUBE FITTING

1" NPT FEMALE

1" NPT FEMALE

TURBINE AIR INLET EQUIPMENT AND ENCLOSURE VENTILATION EQUIPMENT TO BE SUPPORTED BY OTHERS THAN SOLAR TURBINES INC.

:- 17'-1 7/1 6" [52 18m m]

OT) (FILTER FO

13'-6 15/16" [4139mm]

11'-6 15/16" [3529mm]

CONN. 57 & 360

9'-5 15/16" [2894mm]

t=£=..1

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

tAKIII 8FT, SATURN 20 GENERATOR SET ~ATO( MECHANICAL INTE FAC

Solar Turbines A Caterpillar Company

DRAWING NO. SIZE EV

31.1511-149607 8 AD

6

H

G

F

E

D

c

B

A

H

G

F

E

D

c

B

A

8 7 6 5 4 3

26'-2 7/16" ~ ~----------------------· [7987mm]-------------------------------~~

AIR FLOW

10'-1 1/2" ~--------[3086mm]---------l

~ '--- 011------,F-4----

~ \. ·v

2

TURBINE AIR INLET • ~~ r .---------------------------------r------------------------------+------~------~m~~-~d~~~~=4~-----+------------------~--------------------------------~

FILTER vr; ~

19'-7 5/8" [5985mm]

401 402

\ ni!1'K-- t~,- \ ,----------7'-T--------tlt-- -f-1---tll- ::::: :II I

/

\ ' IIIII IIIII 1\ IIIII IIIII

~ I \ rr-~-m rr-H-m "tin ~-m

\\ ::: \\ ::: .-----(-f--------HH---+-\+11- ll // ::: ll // :::

1\ ~&- ~&-~~~~' L_ _ _jti\\...<:C....f r---""-~lf\=11=~~=7'

el \e ~~-J m I

12'-7" [3835mm]

11'-6 15/16" [3529mm]

CiZi 13

374

405

@

I I

i

I

• LIJ! !I.·'= \

~ / ~\~' AIR FLOW

500 501 502

\\ 522

I pVf->-· I n

.. . . . Ci::&:i:o .

[';;:

~

1\· -~:0

.I NON I.S. .I JUNCTION BOX I]~

I NON I.S.

JUNCTION BOX

a ll jl I I ] I I 1:r1

c! (REF)

6'-3 15/16" [1930mm]-

6'-0 7/16" [1841mm

5'-8 15/16" [1752mm]-

9'-4 7/8" ~--------i[2868mm]---------l

9'-6 3/8" l----------[2906mm]-------~-l

14'-10 1/8" 1----------------- [4525mm] _____________ __,

p

32'-0 5/16" 3'-9 1/2" 1----------------------------------· [9761mm] --------------------------------~---~[1156m~]-----

TABLE EXTERNAL CONNECTIONS

I TElA DESCRIPTION ITEM

7 LUBE OIL COOLER VENT 1 /2" NPT FEMALE

33 LUBE OIL TO COOLER 1 1 /2" 150 LB ANSI RF FLANGE 400

34 LUBE OIL FROM COOLER 1 1 /2" 150 LB ANSI RF FLANGE 401

374 DC VOLTS, TURBINE AIR INLET FILTER AINALOG 1/0 1 /2" NPT FEMALE CONDUIT 402

379 DC VOLTS, ENCLOSURE VENT FILTER PRESSURE SWITCH 1 /2" NPT FEMALE 403 522 AIR INLET FILTER DRAIN, UNPLUGGED 2" 150 LB. ANSI RF FLANGE 404

405

LEFT SIDE ELEVATION

ENCLOSURE AIR INLET SYSTEM ENCLOSURE EXHAUST SYSTEM

DESCRIPTION SOLAR P/N LBS KGS ITEM DESCRIPTION SOLAR P/N LBS

VENT SCREEN 42" X 42" 70-25014-20 5 2.3 500 FIRE DAMPER 70-450132-100 125

ELBOW SILENCER 42" X 42" 70-30262-30 300 136 501 ELBOW SILENCER 36" X 36" 70-30263-30 250

BARRIER FILTER 42" X 42" X 30" 1 063238-200 235 107 502 BACKDRAFT DAMPER 1 088340-400 60

VENT FAN 42" X 42" X 24" 70-45030-3H671 300 136 503 WEATHER LOUVER 70-45258-1 00 60

ELBOW 42" X 42" 70-22018-20 155 70

FIRE DAMPER 42" X 42" 1 066933-300 125 57

KGS

57

113

27

27

c:::::c FWD

PACKAGE ORIENTATION

,._t. [1451mm]

19'-6" [5943mm]

16'-6" [5030mm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

8

H

G

F

E

,._l .. [1073mm]

~

D 3'-6 1/16"

''T c

FWD~

B

A

98

97

7 6 5

~ 15'-3 13/16" / (REF~'

[4669mm] I (DISTANCE REQUIRED) (TO OPEN DOORS FOR)

(FILTER MAITENANCE)

11'-0 3/16" 1------------ [3358mm] ------------i

4 3

*

3'-6" - [1067mm]

2

TABLE EXTERNAL CONNECTIONS

ITEM DESCRIPTION

3 LUBE OIL TANK VENT 3" 150 LB ANSI RF FLANGE

6 PNEUMATIC START VENT 3" 150 LB ANSI RF FLANGE

97 ENCLOSURE FIRE EXT. MEDIUM INLET - MAIN 3/4" NPT FEMALE

98 ENCLOSURE FIRE EXT. MEDIUM INLET - EXllENDED 1/2" NPT FEMALE

147 VENT FAN FAIL, LOW PRESSURE 3/8" TUBE FITIING

* FIELD CONNECTION BY SOLAR TURBINES

8'-6 5/8" l---------'[2606mm]---------l~

I

4 1/2" [114mmr -

-

--

.------------- \_j __ / CONNECTION BOX _ _L, f!!- /GENERATOR POWER LEAD

~~~ r~:~=~v---; --. ~ ~ ~ i ------~ .. --~~~--~:~:~ .. ,~----------~~----------------------~ I

1\l f ~ I

6'-6 9/16" [1996mm]

--- --l- --~--+~~*----------r------~

i x+

ln====r!=~G==JQ'L=~=-~~:rll ~=j!.__~ -------------- 1'-9 b/16"

I I [54rm]

I l I

1'-9 5/16"

[54rm]

t,..---.---.--,--r-o::h:--,Jtr----------'-

./1 I I

~ 0 0 .. '. I

f.-' I ~ill IIIII 11111 Ill II 111 II m-_jl..-n

ftt-7rj) IIIII lll/1

~~~~

. .

f~~IIT IIIII 11111 Ill II 111 II m-_jl..-n

~ \1\-@~ (REF) (REF)

147

23'-3 9/16" 1-------------------------~ [7101mm] --------------------------i (REF)

(REF)

24'-9 9/16" ~----------------------------' [7558mm] -------------------------~

(REF)

25'-3 9/16" ~-------------------------- [7710mm] --------------------------~

(REF)

rn 35'-9 13/16"

8'-2" ~ [2489mm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

1------------------------------------ [10917mm ------------------------------------------~

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE OVERALL

Solar Turbines A Caterpillar Company

PLAN VIEW DRAWING NO. EV

(THIS VIEW REPRESENTS THE 3' -6" OFFSET TURBINE AIR INLET DUCT) 3M511-149607 AO

H

G

F

E

D

c

B

A

H

G

F

E

D

c

B

A

8

-o· [6706mm]

(REF)

(REF)

16'-6" [5030mm]

(REF)

3'-9 5/8" [1159mm]

(REF)

___,.RIGHT

PACKAGE ORIENTATION

7 6

FORWARD END VIEW ENCLOSURE AIR INLET DUCTING

REMOVED FOR CLAIRI"IY (THIS VIEW REPRESENTS THE 2' -6" OFFSET TURBINE AIR INLET DUCT)

5 4

-o· [6706mm]

(REF)

17'- 7/8" [5229mm]

(REF)

I NORTH I

3'-9~ [1159mm]

(REF)

___,.RIGHT

PACKAGE ORIENTATION

3 2

TABLE EXTERNAL CONNECTIONS

DESCRIPTION

GENERATOR POWER LEAD CONNECTION BOX 48.50" X 9.13" (1232 X 232) X 7 GA GLAND PLATE

FORWARD END VIEW ENCLOSURE AIR INLET DUCTING

REMOVED FOR CLAIRI"IY

(REF)

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9 (THIS VIEW REPRESENTS THE 3' -6" OFFSET TURBINE AIR INLET DUCT)

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AD

H

G

F

E

D

c

B

A

H

-

G

-

F

-

E

D

c

-

B

-

A

8

22'-o" [6706mm]

I

L._d-------'------11 NORTH I

7 I

6'-5 3/8" l-------1[1965mm]----l

(REF)

6'-1" 1-------rl 1854mm·Jr----l

6'-0 3/4" f------i[1846mm]---l

3' 6" !l106lmmj

(REF)

f l

6 I 5

~r:;==.· ~==t=~~----------.

19'-s• [5942mm]

(REF)

522

(REF)

16'-6" [5030mm]

(REF) ~~ 6'-2" '=

[1880mm]

I V· (~',"

4'-0" 2 1/2" h1219mmr- ~64mm]

8'-o" [2438mmj

8'-5" [2565mmJ

AFT END VIEW (THIS VIEW REPRESENT5 THE 3' -6" OFFSET TURBINE AIR INLET DUCT)

8'-11 1/8" [2722mm]

RIGHT,__...

PACKAGE ORIENTATION

13'-5 7/8" [4113mm]

4

22'-o· [6706mm]

(REF)

I 3 I

5'-5 3/8" l----[1662mm]-

5' 1" IL1549mmy-----

l L J

/ v

/

4'-0" 2 1/2" h1219mmr- ~64mm]

8'-o" [2438mmj

8'-5" [2565mmJ

AFT END VIEW (THIS VIEW REPRESENTS THE 2' -6" OFFSET TURBINE AIR INLET DUCT)

2

~ (REF)

8'-11 1/8" [2722mm]

I

13'-5 7/8" [4113mm]

16'-6" [5030mm]

(REF)

19'-6" [5942mm]

(REF)

RIGHT,__...

PACKAGE ORIENTATION

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. SIZE rEV 81 Ml

3M511-149607

H

G

1--

F

1--

E

D

c

1--

B

1--

A

8 I 7

H

5 1/8" - [131mmJ

G

-

F l=..§..=J

-

E

5 1/8"

--{::: [131mmr

D

-

c

-

B

-

l=.£=..1

A

I 6 I 5 v 4 I

FE 18'-7 3/8" [5673mm]

6'-5 7/8" , . ., .. '=ll r;;~.::.:;l

~~::::--/---=-~lr--"" ---"" I \ 1 I I \ I \

I I I I I I I I

I my~ I I m\ m ~J \ . . . . . . .. . . . 0 . . 0 0 0 0 0 .. 0 ":

:a r:::~l

r:::~l :0, 0

0 .. 0 0 0 0 0 0 a o • •

.. . . . . . . . .

I A~

I \w

I I X I I =x I I I I I I I I I I I I I I I I I \ I I I I I I I I I I I

L~~--~~~--~-~l~~---~~l:~--~~~ L ,._, ,; .. ____J__J

[1775mm] 9,_

2 318•

[2804mm]

9'-10 3/8" 1-----------' [3007mm]----------j

15'-3 1/8" l-------------[4651mm]----------------j

15'-11 1/8" 1-------------- [4854mm] ------------------1

21'-3 7/8" l----------------------'[6498mm]-------------------l

I~

• ([D ;t3·: ---,------ r-- ~----- --------t----- -- I"'

I~

It . ([D ;t3·: . . . . ..

~I . DIID 0 ll Jl .J D

rn ENCLOSURE ACCESS LAYOUT

3

. .

. .

6'-9 1/4" [2063mm]

l=..§..=J

8'-3 3/4" [2534mm]

4'-5 1/4" [1353mm]

2

13'-6 1/2" [4127mm]

I 1

FWD

,_ PACKAGE :J:

" ORIENTATION ii2

FWDl?'"

PACKAGE ORIENTATION

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

H

G

t--

F

t--

E

D

t--

c

t--

B

t--

A DRAWING NO. !SIZE rEV AQ

3M511 -149607 :mr-,,....:8:...J1'------t I 11

H

G

F

E

D

c

B

A

8

--------- FORWARD

+X)

b SECTION [g)= [g)

AFT END SERVICE CONNECTIONS

0 PACKAGE TIE-DOWN SLOT

t:E PACKAGE TIE-DOWN SLOT

m BOTTOM OF TIE-DOWN PAD

ORIENT~tiWNM DETAIL

(MKIII GEN SET)

11 3/4" [299mm]

7

1 5/a" [41mm

___,. RIGHT

PACKAGE ORIENTATION

DETAIL ~ 2-PORT MCT (2 PLACES)

-B-

6

4'-1 13/16" 1-------------- [1265mm] ------------~

31

11 1/2" 2'-2 5/a" 292mm,-1-----· [676mm]

-B-

AFT END

5

2" [51mm]

4

ITE~

19

20

22

25

30

31

36

54

122

126

301

SEE DETAIL ~

2'-7 7/16" [799mm]

3 2

TABLE 1 - EXTERNAL CONNECTIONS

DESCRIPTION X DI~ENSION SEE SECTION X-X

ENGINE EXHAUST AND COMBUSTOR DRAIN 1 /2" 150 LB ANSI RF FLANGE r-\a~~l NATURAL GAS FUEL INLET 1 1 /2" 150 LB ANSI RF FLANGE r-\a~~J ENGINE AIR INLET DUCT DRAIN 1 /2" 150 LB ANSI RF FLANGE [~ llrr1 ~] -3 mm

LUBE OIL FILTER DRAIN - FILTERED 1 /2" 150 LB ANSI RF FLANGE r~3v~~l PILOT VALVES, AIR GAS VENT 1/2" 150 LB ANSI RF FLANGE [~3v~~l ENGINE SEAL VENT 1 /2" 150 LB ANSI RF FLANGE r~3v~~l PACKAGE AIR SUPPLY 1 /2" 150 LB ANSI RF FLANGE [~3v~~l LUBE OIL FILTER DRAIN - UNFILTERED 1 /2" 150 LB ANSI RF FLANGE r~N~~l ON CRANK CLEANING FLUID INLET 1 /2" 150 LB ANSI RF FLANGE [~3v~~l OIL DRAIN FROM DRIP PAN (2 PLACES) 2" NPT FEMALE ?1.,4 [· mm]

AC VOLTS, J-BOX (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), 1X 4.95" X 10.50" (126 X 267) GLAND PLATE -

a'-5" ~----------------------------- [2565mmr-------------------------------~

(REF)

3'-1 5/8" ~---------' [956mm]---------l

AC JUNCTION BOX FOR MORE DETAILS SEE SHEET 13.

301

L,.~,;,.· [B49mm] --------1

-B-

-B-

FWD END

a· [204mm]

RIGHT......­

PACKAGE ORIENTATION

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines FORWARD/AFT END CUSTOMER CONNECTIONS A Caterpillar Company

ENCLOSURE AIR INLET DUCTING & GENERATOR TERMINAL BOX REMOVED FOR CLARI1Y

DRAWING NO.

3M511-149607

EV MJ

H

G

F

E

D

B

A

H

-

G

-

F

-

E

D

-

A

8 I 7

2'-3 5/16" ::::x::J I [693mrm'~:

JUNCTION BOX 1 I ~ ~

6 I 5

JUNCTION BOX 1

4

3'-0 13/16" 1----- [936mm] ----1

2'-2 3/16" r[666mm]-

I 3 I 2 I TABLE 1 - EXTERNAL CONNECTIONS

ITEM DESCRIPTION

26 LUBE OIL TANK DRAIN 2" NPT FEMALE

127 OIL DRAIN FROM DRIP PAN GENERATOR 2" NPT FEMALE

313 AC VOLTS, LUBE OIL TANK HEATER 3/4" NPT FEMALE

315 AC VOLTS, PRE/POST LUBE OIL PUMP MOTOR (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), (DEVICE) 2X M25 X 1.5

331 GROUND, PACKAGE FRAME (4 PLACES) (2/0 GAGE SID WIRE) 1 /2"- UNC

CUSTOMER USE REMOVABLE GLAND PLATES ! !

- -+-----+--·-jiH._·-+--------. t l

336 DC VOLTS, BACKUP LUBE OIL PUMP MOTOR (SKID) RGS-4 MCT 4.75" X 6.28" (121 X 160), (DEVICE) 3/4" NPT FEMALE

414 DC VOLTS, DRIVER J-BOX NON I.S. (2 PLACES) (SKID) 5X RGS-4 MCT 4.75" X 6.28" (121 X 160), 4X 4.95" X 10.50" (126 X 267) GLAND PLATE lYP. 2 PLACES

414 JUNCTION BOX 2

i i i

i I I

SEE DETAIL IF~i-r~1-~ I I

,---~" .----,.,

4'-10 3/16" [1478mm]

4, _

2 518•

2'-6 3/16" [767mm]

[1286mm]

JUNCTION BOX 2

~ 1'-10 5/8"

0

1

./ II ( D./

- - -<D 0

<1> 0 t---1-- -+ 1--+1--++tt++-----. '--------' '------,., 7 'T' _QI oo 0

I l=.£=..1

a· - [203mm] l._, ,;,·

[531mm]-

1±1 LEFT SIDE PACKAGE CONNECTION AFT END PACKAGE CONNECTION

331

FWD J?"

PACKAGE ORIENTATION

336 315

SEE DETAIL ~ SHEET 12.

0 ' ' 0

--~·- -·~--

6'-2 1/4" .r+---1--------[1885mm]-----------l

313

\ .----1-;;p 4 1/2" J [114mmj

9'-7 5/8" t------------------[2936mmj,-----------------~

26

11'-8 1/4" r---------------------[3564mm]----------------------l

l::B PACKAGE TIE-DOWN SLOT

t:[j PACKAGE TIE-DOWN SLOT

rn BOTIOM OF TIE-DOWN PAD

ORIENT~~iWtSA DETAIL

(MKIII GEN SET)

6 1/4" [160mml_

(lYPICAL) (6 PLACES)

2'-8 5/8" t----------·[829mm]---------l

1'-4 5/16" 1----- [415mm]~

I --~-

T I

I

--~ T 1--

I

I

4 3/4" [121mm]

(lYPICAL) (6 PLACES)

2'-7 1/8" 1---------- [791mm·J,---------I

DETAIL IF 6-PORT MCT CONNECTION

AC JUNCTION BOX\ I

CUSTOMER USE

• \. I

I

I GLAND PLATE

- --~-- -

1

'"('1'"

¢9/16" [¢14mm]

(THRU-HOLE) (6 PLACES)

I 2'-7 7/16"

[799mm]

I

L 2" l=.£=..1 [51mm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTI.E

r-----------------------------19'-7 15/16"-------------------------------------------~ [5992mm]

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines 21'-5 3/8"

r----------------------------------------· [6538mmj,-----------------------------------------l

A Caterpillar Company DRAWING NO. !SIZE rEV

1 8 1 AO RIGHT SIDE PACKAGE CONNECTIONS 3M511-149607

H

G

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c

B

A

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-

G

-

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c

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8

ffi PACKAGE TIE-DOWN SLOT

~ PACKAGE TIE-DOWN SLOT

~ BOTTOM OF TIE-DOWN PAD

ORIENT~tjlQU~ DETAIL (MKIII GEN SET)

7 I

!

:

6 I 5 4 I

I SHUTDOWN LEVEL DYNAMIC LOADS-HORIZONTAL AND VERTICAL {SEE NOTES) I ROTOR

DESCRIPTION

S20 ENGINE

GENERATOR

TOTAL LOAD

FORCEO SHAFT CL,

lbf(kN)

±125 (0.56)H

±188 (0.84)V

±4268 (19.0)H

±6718 (29.9)V

±4393 (19.5)H

±6906 (30.7)V

ROTATING FREQUENCY

(RPM)

22,516

1500

NOTES:

PAD A DYNA~IC LOAD lb(kN)

±88 (0.39)H

±133 (0.59)V

±88 (0.39)H

±133 (0.59)V

PAD 81,82 DYNA~IC LOAD (each),lb(kN)

±18 (0.08)H

±60 (0.27)V

±2134 (9.49)H

±3359 (14.9)V

±2152 (9.57)H

±3419 (15.2)V

1. H=HORIZONTAL, V=VERTICAL. HORIZONTAL LOADS ARE PERPENDICULAR TO THE PACKAGE CENTERLINE. 2. THE DYNAMIC FORCE AT THE CENTERLINES ARE BASED ON SHUTDOWN VIBRATION LEVELS OF THE ROTORS. 3. IT IS ASSUMED THAT THE ROTOR DYNAMIC FORCES ARE TRANSMITTED UNATTENUATED TO THE TIE-DOWN PADS. 4. THE FREQUENCY OF THE DYNAMIC PAD LOADS CORRESPONDS TO THE RPM OF THE ROTOR PRODUCING THE LOAD. 5. THE DYNAMIC PAD LOADS ARE ADDITIVE TO THE STATIC PAD LOADS.

3

6. A SHUTDOWN DISPLACEMENT LIMIT OF 0.55 MIL (P-P) WAS CALCULATED BASED ON THE VELOCITY TRANSDUCER SHUTDOWN LIMIT OF 0.65 IN/S RMS AT THE ENGINE STEADY STATE RUNNING FREQUENCY OF 375.2 HZ.

22'-o" [6706mm]

I 2 I

PACKAGE TIE-DOWN LOADS

APPROXIMATE APPROXIMATE PAD STATIC PAD LOAD GE~f:t~~R L6~gRT

A

81

82

7900 LBS [3583 KG]

15000 LBS [6804 KG]

±5813 LBS [±2637 KG]

NOTE: FULL TORQUE LOADS AND SHORT CIRCUIT LOADS ARE A COUPLE. THEY ACT IN THE UPWARD DIRECTION IN ONE PAD AND THE DOWNWARD DIRECTION OF THE OTHER PAD.

~--~ I

---~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~~[--~~+~~~-·~·\=J~·~-~~--~~=-~-~~~--~~~--~~~~~~~~r~~=~=~=:=l~~--~ SEE DETAIL [){ [IDJ ) i

'-,,_///

3'-10 1/2" [1181mm]

f---t -,---..,

0 \

I I 7'-9"

[2362mm]

8'-0" [2438mm]

2" [51mm] THICK

FWD

PACKAGE ORIENTATION

3 3/8" l [86mm]-

SEE DETAIL

1 1/2" [38mm

2 1/2" [64mm] SLOT ¢1 1/2" [38mm] ;~

J. [20T8

;mm]

YD_+--+[1 2T___,_m] 1 ·-4·

1~ J. [406mm]

5" [127mm]

+-+++-----l~ I".

1 1/2"­[38mm

.... -.._¢1" [25.4] -12 UNF 2B

JACKING BOLT (2 PLACES)

DETAIL [f{] FRAME TIE -DOWN

f/ --~\ : ---~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~--~S-E-E~~;A-;-:-J '-::: __ :::,~,~-::::+f.-~-~~/.;;':::Tt'=:::-==-=-====--===:::--===:::_:::_~~h=P=A=C=KA=G=E=O=U=TL=I=N=E=====::::!~~~_l

14'-7" r----------------------------------,L4445mmJ,---------------------------------~

¢1 1/2" [38mm] x--..._

1'-4" 1----------T L•·406mmJ,------I

PACKAGE TIE-DOWN DETAIL PAD LOADS ARE BASED ON THE INSTALLED "WET"

PACKAGE WEIGHT SHOWN IN NOTIE 2.0

¢1 1/2" [38mm] X-....._

1'-4" I-----,L406mm•J,---------~

2 1/2" [64mm] SLOT '-.

/

r ¢1" [25.4] -12 UNF 2B JACKING BOLT

2" [25mm] THICK [-~~"""""'-....._---~~ ,~~~~,--r-~-;-~~~~,

~ I 31/8"

2 1/2" [64mm] SLOT '-.

2" [25mm1"""" ~ THICK .... '7--n 1

-¢1" [25.4] -12 UNF 2B JACKING BOLT

1 1/2" I [38mm]

I I 31/8"

'--t--' -+11+-- j [86tm]

L ;~ ~ L11;2· 7 3/16" 5" [38mm] [182mm 127mm

DETAIL Jl FRAME TIE -DOWN

" '-f.-/

7 3/16" ~ [182mm

5" 127mm

DETAIL [){ FRAME TIE DOWN

[86lm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOW VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO.

3M511-149607

H

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-5/8" ------r2o~~mq.. 2"

[-16mmJ-......_ l [102mm] [51mm] (2 PLACES) -.........._

~ -~ J.

l 6

4 3/4"

l [120Ffm] 1 7/8" 48mm]

1" _____[125mm]

~-+------'

r---1-h 8 7/8"

I 5 4

11'-o· ..-------------~-1 l--------------,[3353mmj

10'-11 3/4" ~-----------[3347mm] -----------~

8'-11 3/4" ~---------·[2737mm]---------~

8'-11" I------------,L2718mm·j-r-------------jl

I 3 I 2

TIE-DOWN LOADS

01

02

700 LBS [318 KG]

[2251mm] I I I I I I L----1--.ffi...- I PACKAGE OUTLINE

/i{~~~v,.· ~~ ,;;:(~., it-------- -- -- -- -- - -:-":.- = -- - -,_, .: ... - -- --

--+--~mm]

I

DETAIL l TURBINE HANDLING KIT

FOOT PRINT (2 PLACES) ,~.1->-- " ,l'::,"!;"~"ioo., i ·~ ~·"~!iii~--- ·-., - J. r;;:.!'.:; [nwmm]

j ( __ 1 __ 1_ i I I t ,._,! v.~,., •• ,

11'-0" 1----------- [3353mm]

10'-11 3/4" 1--------- [3347mm]

8'-11 3/4" 1------- [2737mm]

DETAIL ll¥IJ TURBINE AIR INLET FILTER

TIE-DOWN FOOT (OPPOSITE SIDE -MIRROR IMAGE)

FWD

1'-3 5/16" [566lmm] n [38rm]

u !

! i

i

-

l r - ---- - - - -- - - ---- -,- ''~" ~~'~ - - - = - - -- - - -- --l l;;~;j [3681mm] ROTOR REMOVAL DISTANCE

8'-11" - 1\ I---- [2718mm] y'--------;161 '1---------t=t'l-------------.

I! I Ill

3 5/16~ [84mm]

t

UNIT B TURBINE AIR INLET FILTER

TIE DOWN FOOT TO DATUM -A- & -8-

4'-8 11/16" [1440mm] hi;;:?~~:;,~.~VSEE DETAIL l

! __L [QI] [@ I I I I I i I LW LW ! : I I I

I ~16~1~·m~ ! i (REF) J L ___________ , ___ --------------

~MINIMUM AREA EE REQUIRED FOR

EQUIPMENT REMOVAL (THIS SIDE ONLY)

~--------8'-10 15/16"------------l [2716mm]

ANCILLARY SUPPORT TIE-DOWN DETAIL

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

1SIZE s rEV AO

1" 15

DRAWING NO.

3M511-149607

t--

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6 5 4

14'-8 1/8"-----------------J 1-----------------[4474mm]

CENTER OF GRAVITY INFORMATION

LIFT POINT INFORMATION

APPROXIMATE DRY PACKAGE C.G. WITH ENCLOSURE (WITHOUT L.O., ANCILLARY OR VENT DUCTING)

3

APPROXIMATE GENERATOR C.G.

2

6"

4 112 .. f[[152mm] [114mm

1---------,-, ' '

SECTION ~~~ LIFTING LUG DETAIL

(4 PLACES)

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AD

H

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EQUIPMENT ALIGNMENT

PRELIMINARY ALIGNMENT CONSIDERATIONS: PRELIMINARY ALIGNMENT CHECKS ARE ESSENTIAL. THEY MUST BE COMPLETED BEFORE AUGNMENT

THIS ALIGNMENT PROCEDURE ASSUMES THAT NO SOFT FOOT OR SHORT FOOT CONDITION EXISTS ON ANY OF THE MACHINES AND THE BASE(S) HAVE BEEN QUALIFIED IN ACCORDANCE WITH SOLAR QUALITY ASSURANCE PROCEDURES. THAT THE DIAL INDICATORS ARE CALIBRATED AND IN GOOD WORKING ORDER.

BASE LEVEUNG PROCEDURE: THE PURPOSE OF LEVELING BASE IS TO PLACE THE BASE IN THE SAME POSITION AS DURING FACTORY ALIGNMENT AND TESTING.

BASE/PACKAGE LEVELING IS ACCOMPLISHED BY ADJUSTING BASE JACKING BOLTS ON EACH SIDE OF THE BASE.

THREE POINT MOUNT: IF THE BASE/PACKAGE IS INTENDED TO BE A THREE (3) POINT MOUNT UNIT. THERE WILL BE ONE JACKING BOLT ON EACH SIDE OF THE SKID AND ONE AT THE END OF THE BASE. IN SOME CASES THE MIDDLE (OR THIRD MOUNT) MAY BE LOCATED INTERNAL TO THE BASE IN THE CENTER OF THE CROSS BEAM. THE FINAL CUSTOMER SITE REQUIREMENTS SHOULD BE SIMULATED DURING FACTORY BUILD AND TESTING.

FINAL LEVEUNG: USE A PRECISION LEVEL OF .0005"" (.0127) RESOLUTION OR EQUIVALENT ON THE MACHINED MOUNTING PAD SURFACES. THE LEVELING TOOL MUST BE CAPABLE OF MEASURING THE REQUIRED TOLERANCES ON THE MOUNTING PADS. THE BASE/PACKAGE IS CONSIDERED LEVEL WHEN THE MACHINED PADS AT THE CONTACT AREA UNDER THE ENGINE AND REDUCTION GEARBOX ARE LEVEL WITHIN .005" (0. 127). SHIMS MAY BE USED UNDER THE BASE MOUNTING PADS AT THE JACKING BOLT LOCATIONS TO ACHIEVE EQUIPMENT PAD LEVELING.

SITE INSTAlLATION: SECURE THE BASE/PACKAGE TO THE FOUNDATION VIA ANCHOR BOLTS AT ALL BASE TIE-DOWN POINTS AND TORQUE TO THE SPECIFIED VALUE. RECHECK MOUNTING PADS FOR LEVELNESS. PROCEED WITH ROTATING EQUIPMENT ALIGNMENT AND COUPLING FIT.

PAD CLEANLINESS: VERIFY THAT THE SHIMMABLE EQUIPMENT PADS ARE CLEAN AND FREE OF OIL. GREASE AND DEBRIS.

SHIPPING BRACES: REMOVE SHIPPING BRACES BEFORE STARTING ALIGNMENT.

RUNNING POSITION THRUSTS: THE PURPOSE OF "RUNNING POSITION THRUSTS" IS TO PLACE THE ROTORS OF ALL THE MACHINES IN THEIR OPERATING THRUSTS POSITION TO SET THE PROPER DISTANCE.

GENERATOR MAGNETIC CENTER: SET THE GENERATOR SHAFT AT THE MAGNETIC CENTER. NOT REQUIRED FOR GENERATORS USED IN "FLOATER" OR STANDBY APPLICATIONS.

COLD AUGNMENT: ALL MEMBERS NEED 12-24 HOURS TO COOL FROM OPERATING TEMPERATURE.

OIL TANK: IT IS PEFERRABLE TO HAVE OIL TANK FILLED TO ITS OPERATING LEVEL AT THIS TIME.

AUGNING OUTDOORS: WHEN ALIGNING OUTDOORS OR IN ENVIRONMENTS WITH VARYING TEMPERATURE CONDITIONS. BE AWARE OF THERMAL GROWTH EFFECTS ON THE PACKAGE AND ALIGNMENT TOOLING. WHEN PRACTICAL. ALIGNMENT SHOULD TAKE PLACE DURING THE MOST STABLE TEMPERATURE CONDITIONS.

MANIFOLDS/DUCTING: VERIFY THAT ALL MANIFOLDS (I.E. LUBE OIL) ARE LOOSENED TO ALLOW ALLOW FOR FREE MOVEMENT OF THE MACHINES.

DUCTING: THE EXHAUST BELLOWS HAVE A PRE-STRETCH GAP AT COLD INSTALLATION.

SETTING DISTANCE BETWEEN MACHINES: AFTER THE MACHINERY IS IN ITS RUNNING THRUST POSITION. USE THE PACKAGES JACKING BOLTS TO MOVE THE MACHINE AXIALLY AS REQUIRED TO ACHIEVE THE PROPER ""CALCULATED FLANGE TO FLANGE"" DISTANCE BETWEEN MACHINES OF 12.56" (319.02). SEE FIGURE I.

6 5 4

10.53" [267.46]

DISTANCE BETWEEN HUBS

TORQUE 62 FT -LBS

(LOCTITE 262)

VERIFY DISTANCE:

FIGURE I COUPLING 192780-300

USE AN INSIDE MICROMETER TO VERIFY DISTANCE TOP AND BOTIOM AND SIDES OF FLANGES. AVERAGE THE READINGS.

TIEDOWN BOLTS: VERIFY THAT ALL TIEDOWN BOLTS ARE LUBRICATED WITH ANTI-SEIZE LUBRICANT.

MOUNTING OF AUGNMENT TOOL: FOR THE STATION UNDERGOING ALIGNMENT. MOUNT THE APPROPRIATE TOOLING AS SHOWN IN FIGURE II.

GEARBOX OUTPUT

SHAFT

FACE INDICATOR

GENERATOR COUPLING HUB

GENERATOR INPUT SHAFT

FIGURE II ALIGNMENT TOOLING FT20005-1 DO

REAR MOUNT TURNBUCKLE: LOOSEN AND REMOVE THE TURNBUCKLE FROM THE REAR MOUNT ASSEMBLY. REMOVE THE BRACKETS FROM ASSEMBLY. SAVE THESE FOR FUTURE TRANSPORTATION.

SHEAR COUPLING GUARD REMOVAL: REMOVE THE SHEAR COUPLING GUARD SHROUDS.

ALIGNMENT CONVENTIONS: DIAL INDICATOR SETUP:

DIAL INDICATOR BORE AND FACE READINGS ARE ILLUSTRATED IN FIGURE Ill. BB~BORE BOTTOM. BL~BORE LEFT. BR~BORE RIGHT. BT~BORE TOP. FACE READING ARE THE SAME. SEE FIGURE Ill.

12 O"CLOCK

;] (Y)(X)

IFLIBLI 0 IBRIFRI 9 3

O"CLOCK fB8l O"CLOCK

~ 6 O"CLOCK

VIEW LOOKING BOTH FORWARD AND AFT IMPORTANT: ACCURATELY LOCATE THE 90" CLOCKING POSITIONS

FIGURE III

IDENTIFICATION OF AUGNMENT STATIONS: ALIGNMENT STATIONS AS IDENTIFIED IN FIGURE IV_

T.I.R.

GENERATOR SHAFT

OR

2 X ~ ----+-~~-+---- -------------tl ACTUAL VERTICAL OFFSET

TYPICAL T. I. R. REFERENCE

GEARBOX SHAFT

3 2

l-o5_j FIGURE IV

STATION DISTANCE INCHES/MM

D1 BETWEEN FAR FOOT TO NEAR FOOT OF GEARBOX 14.000 355.60 D2 BETWEEN NEAR FOOT TO COUPLING FLANGE FACE 9.750 247.65 D3 GEAR BOX FLANGE FACE TO GEN SHAFT END 12.560 319.02 D4 GEN SHAFT END TO GEN FORWARD FOOT 18.750 476.25 D5 BETWEEN FOOT TO FOOT GENERATOR S8.DOO 1473.20

STATION THERMAL GROWTH INCHES/MM

FAR FOOT OF GEARBOX .018 .457 NEAR FOOT OF GEARBOX .018 .4S7 GENERATOR FORWARD FOOT .008 .203 GENERATOR AFT FOOT .008 .203

MEASUREMENTS: ALL MEASUREMENTS ARE GIVEN IN INCHES AND MILLIMETERS.

DIAL INDICATOR READINGS: DIAL INDICATOR READINGS ARE ALWAYS "TOTAL INDICATOR READINGS"" (T.I.R.).

FIXED REFERENCE POINT: THE FIXED REFERENCE POINT IS DENOTED BY A * IN FIGURE IV. IT IS NOT TO BE SHIMMED OR MOVED.

NEAR FOOT/FAR FOOT: NEAR FOOT IS FOOT OR PAD CLOSEST TO THE MACHINES FACE END. FAR FOOT IS FOOT OR PAD FARTHESTS AWAY FROM MACHINES FACE END.

SIGHT/FROM MACHINE: MACHINE WITH ALIGNMENT TOOL ATIATCHED.

TARGET/TO MACHINE: MACHINE WITHOUT ALIGNMENT TOOL ATIATCHED.

BEARING PRE-LUBRICATION: IT IS RECOMMENDED TO PRELUBE THE MACHINERY PRIOR TO ROTATION TO PREVENT POSSIBLE BEARING DAMAGE.

MACHINE ROTATION: ROTATE MACHINERY IN THE SAME DIRECTION OF NORMAL ROTATION.

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOW VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFAC~

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AD

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ALIGNMENT CONVENTIONS AND PROCEDURES 12 O'CLOCK

ALIGNMENT CONVENTIONS: DIAL INDICATOR SETUP:

[;E DIAL INDICATOR BORE AND FACE READINGS ARE ILLUSTRATED IN FIGURE IV. 88~BORE BOTTOM, BL~80RE LEFT, BR~BORE RIGHT, 8T~BORE TOP. FACE READING ARE THE SAME.

MEASUREMENTS:

IFLIBLI 0 I8RIFRI 9 3

O'CLOCK ~ O'CLOCK

~ ALL MEASUREMENTS ARE GIVEN IN INCHES AND MILLIMETERS. 6 O'CLOCK

DIAL INDICATOR READINGS: DIAL INDICATOR READINGS ARE ALWAYS 'TOTAL INDICATOR READINGS" (T.I.R.). VIEW LOOKING BOTH FORWARD AND AFT

IMPORTANT: ACCURATELY LOCATE THE 90' CLOCKING POSITIONS FIXED REFERENCE POINT:

BECOMES THE FIXED REFERENCE POINT AS DENOTED BY * IN FIGURE Ill. FIGURE IV

NEAR FOOT/FAR FOOT: NEAR FOOT IS FOOT OR PAD CLOSEST TO THE MACHINES SHAFT END. FAR FOOT IS FOOT DIAL INDICATOR READINGS: OR PAD FARTHEST AWAY FROM MACHINES SHAFT END. DIAL INDICATOR READINGS ARE ALWAYS 'TOTAL INDICATOR READINGS" (T.I.R.).

SIGHT/FROM MACHINE: MACHINE WITH ALIGNMENT TOOL ATTACHED.

TARGET/TO MACHINE: MACHINE WITHOUT ALIGNMENT TOOL ATTACHED.

ALIGNMENT PROCEDURES: BEARING PRE-LUBRICATION:

IT IS RECOMMENDED TO PRELUBE THE MACHINERY PRIOR TO ROTATION TO PREVENT POSSIBLE BEARING DAMAGE.

MACHINE ROTATION: ROTATE MACHINERY IN THE SAME DIRECTION OF NORMAL ROTATION.

SWEEP ALIGNMENT: WITH THE BT AND FT READING 0.0 IN THE 12 O'CLOCK POSITION, SLOWLY ROTATE THE ALIGNMENT TOOL WHILE PULLING AFT, ONE COMPLETE ROTATION AND RECORD THE FOLLOWING DIAL INDICATOR READINGS: FL. FR. FB, BL, BR, AND BB.

DIAL INDICATOR REPEATIBILITY:

REPEAT THE ABOVE STEP AS NECESSARY TO VERIFY REPEATABILITY OF THE DIAL INDICATORS.

VERTICAL SHIM ADJUSTMENT: WHEN THE LATERAL ADJUSTMENT IS SATISFIED, SWEEP THE SHAFT AND RECORD BB AND FB.

NEAR FOOT/FAR FOOT SHIM ADJUSTMENT:

FROM THE BB AND F8 READINGS RECORDED IN STEP I ABOVE, ADD OR REMOVE SHIMS FROM THE NEAR FEET AND FAR FEET TO APPROXIMATE FIGURES ON TABLES lA AND IB, DIAL INDICATOR AND LASER RESPECTIBLY.

SEE FIGURE III AND TABLES !A AND IB FOR CORRECT DIMENSIONS AND READINGS

ONCE A SHIM CORRECTION IS MADE. RETORQUE TIEDOWN BOLTS TO 70% OF VALUE GIVEN IN TABLE II. RECHECK ALIGNMENT AND SHIM ADJUSTMENTS AS NECESSARY UNTIL READINGS ARE WITHIN THE ALLOWABLE LIMITS.

SHIM CARE: USE CLEAN SHIMS. SHIMS WHICH ARE OILY, RUSTED, OR DEFORMED SHOULD NOT BE USED.

FINAL AIJGNMENT VERIFICATION:

WHEN ALL ALIGNMENT READINGS ARE WITHIN THE ALLOWABLE LIMITS, MONITOR THE ALIGNMENT READINGS AS THE FOLLOWING IS BEING COMPLETED. ALL MANIFOLDS ARE TIGHTENED IN PLACE. ALL TIE-DOWN BOLTS ARE TORQUED IN A "STAR" PATTERN TO THEIR SPECIFIED VALUE. THE INLET AND EXHAUST DUCT ARE TIGHTENED IN PLACE. ALL JACKING BOLTS ARE FULLY RETRACTED. THE OIL TANK IS FILLED TO ITS OPERATING LEVEL. AFTER THE ABOVE IS COMPLETED, RESWEEP ALIGNMENT AND VERIFY THAT THE INDICATOR READINGS ARE STILL WITHIN ALLOWABLE LIMITS. MAKE ADJUSTMENTS IF NECESSARY. RESWEEP, RESHIM, RECHECK.

NOTE: IF MISAIJGNMENT HAS BEEN CAUSED BY ATTACHMENT OF HEADER PIPES OR DUCTING, MAKE CORRECTIONS TO THE OFFENDING ITEM (S). DO NOT REPOSITION THE DRIVER OR DRIVEN MACHINES AS A METHOD OF CORRECTING THE MISAIJGNMENT CONDmON.

WHEN ALL ALIGNMENT IS ACCEPTABLE. DOWEL THE DRIVEN EQUIPMENT IN PLACE AND VERIFY ALIGNMENT.

ALIGNMENT TOOL REMOVAL: REMOVE THE ALIGNMENT TOOL(S).

LASER ALIGNMENT: IF USING VISIBLE LIGHT LASER ALIGNMENT TOOLING, CONSULT THE USERS MANUAL FOR PROPER OPERATION.

T.I.R. OR

2 X OFFSET

( K

TYPICAL T.I.R. REFERENCE

1 GENERATOR SHAFT

l ACTUAL VERTICAL OFFSET

GEARBOX SHAFT

I 3 I 2 I

TABLE I - DIAL INDICATOR AUGNMENT - BORE AND FACE OFFSETS SIGKT TARGET OFFSET {BORE OFFSET) ANGULARITY {FACE OFFSET) FACE SHAFT

BORE ·rnoM· "TO" liD'] [§iJ OOjJ ~ liT] liT] lffil 100 DIAMETER RELATIONSHIPS

OFFSET ~ +.008" +.ooa· ±.oo2· +.01s· ±.oos·

T.I.R. 0 0 00 (+.203) ( +.203 ±.051) ( +0.406±.127) 00 .000" .oao· ±.oo1 .. .oao· ±.OD2" OUTSIDE TIR OUTSIDE TIR OUTSIDE TIR (.000) (.000 ±.025) (.000 ±.051)

11.5" (292)

GEARBOX COUPLING

HUB

CAUTION: DIAL INDICATOR READINGS ABOVE ARE TOTAL INDICATOR READINGS (T.I.R.).

THE FACE DIAMETER IS DEFINED AS THAT DIAMETER ON THE SPECIFIC HOUSING FACE FOR WHICH THE FACE OFFSET IS GIVEN (SHOULD NOT BE AN INTERRUPTED SURFACE).

BORE LEFT (BL) READINGS AND FACE LEFT (FL) READINGS ARE RECORDED FROM EQUIPMENT DURING A 360" SWEEP.

BORE RIGHT (BR) READING AND FACE RIGHT (FR) READING MUST BE WITHIN THE TOLERANCE NOTED ABOVE.

+ -- ~ LASER

-$- ~ DETECTOR/RECEIVER

GENERATOR Ef-1~ TARGETS AT COUPLING CENTER_/ LLJ,-.,------,---LJ-1

TABLE I - LASER ALIGNMENT - BORE AND FACE OFFSETS

0

----i

LASER STATIONARY

DETECTOR MOVEABLE

COLD TARGET COLD TARGET OFFSETS (BORE OFFSETS) COLD TARGET ANGLES (FACE OFFSETS) AT lcV-cO~("'B"'B:;c) "FH"'o""''='s"'L _:..:Bo,Rs:.cT::...O.::LE:..:.R::.A=.:N.:oC'-E+.VA.,---("F"'B")'T'H"-A,.::.C,:OF

00L -'-FO:'R~rD'-IA.;:M.:.:E:::T::...E.::Rc;.::T=.:O.:oLE'-R-A_N_C---iE

GEARBOX GENERATOR couPLING +.oos" I .ooo .. ±.oos· .ooo" I .ooo" I 1 o"

CENTER (+0.20) (.000 ) (. 1 27) (.000) (.000) I ±.002" (±.05)

(ALL COLD TARGETS ARE MOVEABLE MACHINE RELATIVE TO STATIONARY MACHINE)

ROTALIGN TERMINOLOGY:

VO ~ VERTICAL OFFSET HO ~ HORIZONTAL OFFSET VA ~ VERTICAL ANGULARITY HA ~ HORIZONTAL ANGULARITY

SOLAR TERMINOLOGY:

BORE BOTIOM BORE LEFT OR BORE RIGHT

FACE BOTIOM FACE LEFT OR FACE RIGHT

WHEN STATIONARY MACHINE IS ON YOUR LEFT AND MOVEABLE MACHINE IS ON YOUR RIGHT:

+VO ~ MOVEABLE MACHINE HIGHER THAN STATIONARY MACHINE -VO ~ MOVEABLE MACHINE LOWER THAN STATIONARY MACHINE +VA ~ COUPLING OPEN AT TOP -VA ~ COUPLING OPEN AT BOTTOM

+HO ~ MOVEABLE MACHINE AWAY FROM YOU RELATIVE TO STATIONARY MACHINE -HO ~ MOVEABLE MACHINE TOWARDS RELATIVE TO STATIONARY MACHINE +HA ~ COUPLING OPEN AWAY FROM YOU -HA ~ COUPLING OPEN TOWARDS YOU

TABLE II - TORQUE VALUES

THREAD TIGHTENING TORQUE TIGHTENING TORQUE GRADE SIZE ENGLISH (FOOT -LBS) METRIC (NEWTON-METERS)

.75 10 211 (LUBRICATED) 2B6 (LUBRICATED) 87 1.DD-B 423 (LUBRICATED) 574 (LUBRICATED) 87 1.25 7 806 (LUBRICATED) 1 D94 (LUBRICATED) 87 1.50 6 1437 (LUBRICATED) 1950 (LUBRICATED) 87

2.00 4 1 2 3408 (LUBRICATED) 4624 (LUBRICATED) 87

0 f----

FOR ADDITIONAL TORQUE VALUES REFERENCE SOLAR SPECIFICATION ES 9-54. CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. IS'ZE B rEV AO

ISH 18 3M511-149607

H

r--

G

F

E

D

c

r--

B

A

H

G

F

E

D

c

B

A

8

NOTES:

1. ALL TERMINAL BOXES, COVERS AND SCREENS ARE 316 STAINLESS STEEL AND NOT PAINTED.

7

2. ALL FASTENERS ~· AND SMALLER OF 316 STAINLESS STEEL

3. THE TOLERANCE OF THE OIL INLET/OUTLET POSITION IS 1 INCH.

4. BOTH BEARINGS REQUIRE EXTERNAL LUBRICATION.

5. APPROX. WEIGHTS:

TOTAL UNIT WEIGHT: 12,000 LB

SHIPPING DIMENSIONS: 85.26 X 1 08.88 X 49.19

6. THIS GENERATOR IS SUITAIBLE FOR OPERATION IN CLASS 1, GROUP B, C, AND D, T3 BY CSA.

OIL INLET 1/2 TUBE (THIS SIDE)

OIL OUTLET SAE 2.0" FLANGE WITH 4X 0.5-13 UNC-2B

(THIS SIDE)

6'-6 1/2" [1

4'-8 1/2" [1

4'-5" [1

4X -1.25 MOUNTING

6

EXCITER END BEARING OIL OUTLET DETAILS

5 4 3 2

7'-1 1/4" 1------------ [2166mm.,-------------l

3'-4 9/16" 3'-3 1/2" f-----· [1031mm,-------Jt----- [1003mm,-------l

1'-9 7/16" [544mm]

1'-7" 483mm

FRAME

(AS VIEWED FROM EXCITER END OF MACHINE)

6 3/4" [171mm]

6 5/8" [168mm]

1 3/8" [35mm]

OIL INLET 1/2 TUBE (THIS SIDE)

4'-1 11/16" [1262mm]

3'-1 1/4" [946mm]

2'-9 3/4" [857mm]

2'-5" [737mm]

7 GA X 11.63 X 51.00 STAINLESS STEEL GLAND PLATE 9.13 X 48.50 X OPENING

1.00 X 1.00 X 5.00 KEY

UNPAINTED STAINLESS STEEL GROUND PADS WITH 2X 0.500-13 UNC-2B HOLES ON EACH (LOCATED DIAGONALLY OPPOSITE)

4 1/2" [114mm]

"KATO" GENERATOR GENERAL ARRANGEMENT APPROX. WEIGHT: 12,000 LBS. (5443 Kg.)

STRAIGHT ROTOR

REMOVAL 71.00

STRAIGHT EXCITER

REMOVAL 21.00

FOOT THICKNESS

6 1/8" [156mm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

H

G

F

E

D

B

A

8

CT'S

7 6

4'-5" l-----------------------~[1~mm~]-------------------------i

1 4 2 5 3 6 n n n n n n

r . ~ , L __ ...J

:@ . t . ):lJ [r:l (6) I -

I ' ' ' ' ' ' - I I ' ' ' ' t ' I I II Ill I I I

~ I II Ill

I I I

I I

II Ill I I

II ,-- H II ,-, lol[

II II II H I II II II I

5

/ CT AUXILIARY BOX

E J II Ill -VL'S

:I: I L-Jd -I

I~

I :;=~ ~ ~

~ ,---

1 2 3

5 3/B" 9 7/B" 9 7/B" 11 11/18" - [137mmli--t2s1mmjl--t2s1mmj1-.[297mm]-

SSTL GROUND PAD (2X 112-13 TAPPED HOLES)\

0 u 0~

() () I I I

() () I

II Ill

[tfr 1tll

N

VL'S~

I

""C

o I d I I

o I I

~ I I I

.0: ,I"="" I I I

d I I I I

~ I I I I ~ I

1/8' NEOPRENE GASKET

GLUED TO INSIDE OF COVER\

7 GA COVER~

~--------fo~~-~-~~~-~-~-~-~~~-~-~-~-~~~-~-~-~-~~~-~-~-~-~-~~~-~-~-~-~-=~=-=-=-=-=~~=-=-=-=-=~=-=-=-=-=-=~=-=-~~0

II 4'-4 5/B"_-111 l-----------------------_;[1337mm]

4'-7 1/2" l--------------------------[1410mm]-------------------------~

~1/8' NEOPRENE GASKET GLUED TO INSIDE OF COVER

~7 GA COVER

1 3/4" [44mm

4 3

PHASE BUSS BAR ASSEMBLY

TYPICAL CUSTOMER CONNECTION PLATE

2X -l-+-----2 1/16" [52mm]

2

NEUTRAL BUSS BAR ASSEMBLY

6 3/4" l [171mm] I-

(01

3/18" m]

2'-1 [840m

~ -~0 1 I I I I

~ g

: ~I I

0 0 0 I

0 0 0 I

Q [~ ,..., I I I I I I I 1, 2, 3

()> ()> I I

II Iii"" .. ~] II II

II !i ()> ()> II I (I]) .. I I

II I I 4, 5, 6 II I

I ~ 0 =>

II Iii"" .. ~] : p: II II

[: 0 => II !i I I II I em ..

I I ) I

I ~ "l J

~1 5/B" 295mm] I 2'-4"

[711mmJ

3'-6" L1087mmJ

NOTES:

1. SEE DIMENSIONAL DRAWING FOR LOCATION OF OUTLET BOX ON GENERATOR

2. ALL TERMINAL BOXES ARE 316 SSTL, NOT PAINTED.

2'-9 [857

3/4" mm]

3. THESE TERMINAL BOXES, AS INSTALLED ON THE GENERATOR, ARE SUITABLE FOR HAZARDOUS LOCATION AS DEFINED BY CSA STANDARDS FOR CLASS 1 DIV 2, GROUP C & D, T3

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

KATO GENERATOR POWER LEAD BOX DRAWING NO. EV

3M511-149607 MJ

H

G

F

E

D

c

B

A

8 I 7 I 6 I 5 v 4 I 3 I 2 I 1

H H

- t--

G G

- t--

F F

LOOSE SHIP COMPONENTS - t--

SHT DESCRIPTION QTY.

NO.

22 FLANGED STRAINER. GAS FUEL INLET & PNEUMATIC START 1

E 23 GAS FUEL MASS FLOWMETER 1 E 24 CONTACTOR / 100 AMP RELAY FOR DC BACKUP LUBE OIL PUMP 1

25 AIR/OIL COOLER. HIGH AMBIENT 1

26 SWITCH. HAND-OFF-AUTO 3

27 LUBE OIL MIST ELIMINATOR 1

---!> 28 FLAME ARRESTOR. LUBE OIL TANK VENT 1 f:J-29 FIRE CYLINDER CABINET 2

30 UNIT CONTROL PANEL (UCP) 1

31 TURBINE AIR INLET FILTER 1

32 TURBINE AIR INLET SILENCER 1

D 33 EXHAUST BELLOWS 1 D 34 EXHAUST ELBOW 1

35 AIR INLET DUCT -30" OFFSET 1

36 AIR INLET DUCT -42" OFFSET 1

37 AIR INLET DUCT-24" 1

- t--

c c

- t--

B CUSTOMER/END USER/PROJECT

B CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

- tAKIII 8FT, SATURN 20 t--

GENERATOR SET ~ATOJ MECHANICAL INTE FAC

A Solar Turbines A A Caterpillar Company

DRAWING NO.

1SIZE s rEV AO

3M511-149607 1,, 21

Lf THIS COPYRIGHTED WORK AND TI-lE INFORW.TION HEREIN IS PROPRIETARY TO CAlERPIUAR

W~1l-r~~~ER1JI~~rb~ ~~~~~~iU.:0~~ 8~~8~ESTU~I~E:JlrJcg~~\U,JXJ'R,W I R T WHI I IT •

8 7 6

H

G

F

7 1/8" 181mm

218

E

D

c

B

A

' '

""' '

5

219

> 21/4" [57mm]

""' BASKET REMOVAL

',~// CLTNCE

4

DRAIN

FLANGED STRAINER. GAS FUEL INLET & PNEUMATIC START

APPROX. WEIGHT: 17 LBS [7.7 KG.]

LOOSE SHIPPED ITEM

P/N 120835-13

3

ITEM

A tl

2

TABLE 1 EXTERNAL CONNECTIONS

FLANGED STRAINER INLET

FLANGED STRAINER OUTLET

DESCRIPTIONS

1 1 /2" 150 LB ANSI RF FLANGE

1 1 /2" 150 LB ANSI RF FLANGE

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

8

H

G

F

E

D

c

B

A

7

2X 1/2"-14 NPT CONDUIT CONNECTION

5 5/8" [143mm

6 5 4 3 2

TABLE 1 - EXTERNAL CONNECTIONS

ITEM DESCRIPTION

~7J) FUEL FLOWMETER RUN INLET 1" 300 LB ANSI RF FLANGE

~7~ FUEL FLOWMETER RUN OUTLET 1" 300 LB ANSI RF FLANGE

2'-1 3/8"±1/8" f--------------· [645±3] ----------~-~

1'-5 7/8" f------------ [454mm,-------~~

1'-2" f-------- [356mm,-----------l

( ___ )

NORMAL FLOW>

2X 1/2"-14 NPT FEMALE PURGE CONNECTION

WITH MALE HEX PLUG INSTALLED (OPTIONAL)

2 7/16".------+---l [62mm

GAS FUEL MASS FLOWMETER (SHOWN IN INSTALLED ORIENTATION) APPROX. WEIGHT: 27 LBS [13 KG.]

LOOSE SHIPPED ITEM

P/N 1065718-100

¢4 11/16 [119mm]

1'-0 9/16" [319mm]

7 13/16" [182mm]

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

8 7

H

G

F

E

D

c

B

A

3 5/8" [92mm]

¢5/16" [¢8mm

AI, A2 TERMINAL MARKINGS ARE ON

THIS SIDE OF SHELL

6 5

3" [76mm]

4

NAME PLATE

CONTACTOR / 100 AMP RELAY FOR DC BACKUP LUBE OIL PUMP

APPROX. WEIGHT: 3 L8S [1.3 KG.]

LOOSE SHIPPED ITEM

P/N 918693C1

3 2

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFAC~

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AD

H

G

F

E

D

c

B

A

8 7 6 5 4 3 2

H H

G G

F F

E

H~S SH E ~N EN ~ONAL Y LE T B ANK E

LUBE 0~ L COOLER ~NFORMA ~ON 0 OLLOW D D

c c

B CUSTOMER/END USER/PROJECT

B CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTLE

tAKIII 8FT, SATURN 20 GENERATOR SET ~ATO( MECHANICAL INTE FAC

A Solar Turbines A A Caterpillar Company

DRAWING NO.

3M511-149607

THIS COPYRIGHTED WORK AND THE INFORW.TION HEREIN IS PROPRIETARY TO CATERPIUAR

W~~~~11~~~~~ ~~~~~~iu.M0~~ g~~g~ESruWsi~E~J;~g\U,JXJ'R,W I R T WHI I IT •

H

G

F

E

D

c

B

A

8 7

5 1/2"

[140mm] (2 P CES)

3/4" [19mm]

(4 PLACES)

6

4 1/2"

[114mm] (2 PLACES)

3 1/4"

[81mm] (2 PLACES)

3/8"

[10mm] (4 PLACES)

~3/4" [~20mm]

(NPT -FEMALE) (2 PLACES)

5

6 5/8"

[168mm]

[38mm]

BOX, SWITCH ASSEMBLY-HOA

APPROXIMATE WEIGHT : 4.5 LBS [2 KG]

LOOSE SHIPPED ITEM

P/N-1010416 (ASSEMBLY) P/N-969408C1 (SWITCH) P /N-1 020222 (OPERATOR)

4

USED FOR ENCLOSURE VENT FANS (2) AND LUBE OIL COOLER FAN

3 2

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

8 I 7 I 6 I 5 v 4 I 3 I 2 I 1

TABLE 1 - EXTERNAL CONNECTIONS

H ITEM DESCRIPTIONS H 8 LUBE OIL MIST SEPARATOR INLET 3" 150 LB ANSI RF FLANGE

8 LUBE OIL MIST SEPARATOR OIL RETURN 1/2" NPT FEMALE

8 LUBE OIL MIST SEPARATOR OUTLET 3" 150 LB ANSI RF FLANGE

r-- r--

G ~ ,ioo~mr G

5" (REF) [127mm]

r-- ~0 0 ~1'-5" r--

h ~~ 0 ~432mm]

~:~-0

D

F 0 F u 0 v 0

0 0 0 0

r-- r--,;: _--,

___ J 203\ (REF) \ .. _ . .'

10" 7" [254mm] [178mmj

E 5" ~.. ~~X ~1· [25mm] E [127mmj

UFTING LUG

roJ (c)' 4" '/To\ ro{ 6X ~ 1/21;~

' [102mm]

f--1> [13mm]

f:J-,-------' f--- --

0 f--- -- 4'-2" [1270mm]

D >-------- -- ry:~ D ~ liP CONNECTION (1/2" NPTF)

4" 6"

'---- [102mm] r [152mm]

'/ I-- I I

2'-8" I --1 I--[813mm] t-'

1'-6"

c [457mm] c FILL SUMP

288 DURING INITIAL INSTALLATION

·~ I-- I--

, .. -.. , 287 ---J 3 \(REF)

\. .. _ .. /

B CUSTOMER/END USER/PROJECT

B CHEVRON CVX GOW VK 900

CVX-VK9

DRAWING TITlE

I-- MKIII 8FT, SATURN 20 I--

GENERATOR SET ~ATOJ MECHANICAL INTE FAC

LUBE OIL MIST ELIMINATOR Solar Turbines A APPROX. WEIGHT: 360 LBS [163 KG.] A LOOSE SHIPPED ITEM A Caterpillar Company

COMPONENT SHELL AND FASTENERS 316 STAINLESS STEEL

P/N 186147-3 DRAWING NO.

1SIZE rEV

3M511-149607 8 AO

ISH 27

If w~~~2~~~~~w;i~:~~~~i::~~~%~Ng~~~~~&~~~~w~~~gm~~kt; PY I R THATFRWHI I

8 I 7 I 6 I

H

-

G

-

F

-

E

D

-

c

-

B

-

A

5 4

I I

\)---------+----! J I ! \

I I I

203

FLAME ARRESTOR, LUBE OIL TANK VENT

APPROX. WEIGHT: 14.3 LBS [6.5 KG.] LOOSE SHIPPED ITEM

P/N 1065667-7

I

6 11/16" [170mm]

3 I 2 I

TABLE 1 - EXTERNAL CONNECTIONS

ITEM DESCRIPTIONS

~0~ FLAME ARRESTOR, LUBE OIL TANK VENT 6" 150 LB ANSI RF FLANGE

CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFAC~

Solar Turbines A Caterpillar Company

DRAWING NO. !SIZE I'EV 1 8 1 AO

3M511-149607

H

-

G

-

F

-

E

<J-

D

-

c

-

B

-

A

8 7

H

G

F

E

D

c

B

A

2X ¢1 3/8" [35mm] LIFTING EYE

2X 7'-1 7/8" [2181mm]

4'-o" [1219mm]

6

., ,. ~

. , ,. -.-. ~ -.-.

.1..----'----~~ - C6 X 13

C1·-7 1/2" [496mm]

3'-11 13/16" [1214mm]

DOOR SWING

5

5'-0 13/16" 1-------- [1545mm] ---------1

3'-8 7/8" r--l-++-----'[1139mm]-----l

2'-1 1/8"

T~'t::::::====c::;;;======~

ANUAL ACTIVATION PULL STATION FIRE

CYLINDER CABINET

C02

2X 3'-8" l---------.'1118mmr-------l

4

453 REF

452 REF

6'-2 5/16" [1888mm]

8 1/8" [206mm

GROUND (3/8"-16 X 1-1/4")

4X ¢5/8" [16mm] MOUNTING HOLE

C02 CYLINDER CABINET W/ 3-WAY ISOLATION VALVES APPROXIMATE WEIGHT (LESS CYLINDERS): 780 LBS [354 KG]

APPROXIMATE WEIGHT (WITH CYLINDERS INSTALLED): 1,644 LBS [746 KG]

MATERIAL CARBON STEEL

LOOSE SHIPPED ITEM

P/N 1086603-200 QTY. 2

., , . -.-. ~

3

ITEM

9

9

()5 45

~-

· · · ·o [1g;6~·m]

~J ,._, w] [562mm]

2

TABLE - EXTERNAL CONNECTIONS

DESCRIPTION

EXTINGUISHANT DISCHARGE MAIN

EXTINGUISHANT DISCHARGE EXTENDED

DC VOLTS, FIRE SYSTEM POWER INPUT 24 VDC

VENT, FIRE ExnNGUISHANT, MAIN

VENT, FIRE ExnNGUISHANT, EXTENDED

3/4" NPT FEMALE

1 /2" NPT FEMALE

5-1/4" X 8-1/8" BLANK PLATE

3/4" NPT FEMALE

1/2" NPT FEMALE

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING llTL.E

tAKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

H

G

F

E

D

c

B

1--

A

8 I 7 I 6 I

2'-7" [787mm]

5" I [127mm]

~J_i-----_J_---i r-----11 ----;~--+-------f..-l------r[1 ;;mm] 335~~~~T--r====~-----------------~~

CABLE ENTRY/~---....1 I PLATE AREA L_j

2'-9"

€L ________________ [.8;~~~rnJ _________________ ,,.@

4'-9 15/16" [1471mm] MAXIMUM

DOOR SWING -'----------

11 /\ I!! 7.. i i / \ I I 7"

[178mmj 1 1 / \ 1----1+~1+-1 [178mm]

II / \ : i II / \ 'I I I //// ',,, I I I -"/ ' I ll ________ / ',,'',,, i i

........ ____ f VIEW~"'~

ELECTRICAL ACCESS AREAS CONSOLE TOP

ri~IN;/~P8J (4) PLACES

~ ~ r""'-©---------""-, ---'-=~-----.

TURBINE---------- ...­CONTROL

PANEL /

HMIVIDEO~ DISPLAY

~E ~ I

II • ............. il

KEYBIIARD DRAWER

I='"""'" I

I 7" [178mm]

t

5 4 I 3 I 2 I

TABLE 1 - EXTERNAL CONNECTIONS

ITEM DESCRIPTION

335 DC VOLTS, CONTROL CONSOLE (7 PLACES) 2X 7.00" X 21.00" (178 X 533) & 2X 7.00" X 7.00" (178 X 178) GLAND PLATES TOP & BOTIOM

342 GROUND, CONSOLE FRAME BUS BAR

7" 2'-9" 7" [178mmjr--t----t--~------,L838mm·jr-----t--~--l--.l 178mm]

-5/8" [-16mm]

FOR TIE DOWN BOLT (4) PLACES

'/ tr------------r---1+-+----------.

-'-------+:-l!~==~;!~~r: : ~" -~~" 2'-o" [610mm]

I H- PLATE AREA

.-----~++IL_----- c_ -----~1--+-----------L

,._J,. ,,r, 1'-9"

~ [533mm 1'-9"

~ [533mmj 5"

[127mm]

[2 1/2" [64mm]

4'-2" [1270mmj

4'-5" [1346mmJ

VIEW U"'U ELECTRICAL ACCESS AREAS

CONSOLE BOTIOM

3 1/2" - [89mm]

2" 51mm]

3/8-16 UNC -2A STUD

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFAC~

Solar Turbines UNIT CONTROL PANEL (CONTROL CONSOLE IPSO RATED) A Caterpillar Company

APPROXIMATE WEIGHT : 1,400 LBS (640 KG)

LOOSE SHIPPED ITEM DRAWING NO.

3M511-149607

H

G

F

E

D

c

B

1--

A

H

G

t--

F

t--

E

D

t--

c

t--

B

t--

A

8 I 7 I 6 I

¢3/4" [¢19mm] 2'-o" ,---ti-~------3'-0 1/8~-

.--------(-{~-R-~LA_-H_C~-~l_1_\_~\,----+f-----------~-1-0m_m_]----+!,.K®+--O~''[i:,;(~j l ["'mm]

r J&,i,.b I

2'-11 3/8" [899mm]

2'-6" [762mm]

(UNIT A)

3'ls· [1067mm] (UNIT B)

2'-2 3/4" [678mm]

\I n=

1\ '

lo'

1M 0 0 . . Footprint

2'-2 3/4" [678mm]-

4 Spaces 2 5/8" [67mm]-

@ 5" 2 5/8" - ~ 1'-8"- I-- [67mm]

5/8" [16mm]­

Typ.

4'-4" [1321mm]

[508mm] 2 1/8" [54mm]

2' o" -[610mm]

Opening t

2" - - [51mm]

Typ.

4'-o" [121 mm] Openin

9 Spaces @ 5" ~ 3'-9" [1143mm]

I. I

L [16mm] ·~2_J 2 1/8",J [54mm] Typ.

2'-4" [711mm]

NOTE: FOR TIEDOWN FOOT DETAILS AND POSITIONING RELATIVE TO DATUM -A- & DATUM -B- SEE SHEET 15 FOR MORE DETAILS.

5

3'-3 1/2"

J [1003mm]

1'-7 3/4"

'T'

4'-5 3/8" [1356mm]

4

5'-1 1/2" [1562mm]

AIRFLOW

5'-6" [1676mm] Overall

t

I 3 I 2

0 0 .=::; 0

0

I> 0

I>·

J

0

tbofPanel

1'-3"

I [380mm]l

I~ r ctJI==--+:....::J---

~ R=· ~-~. \ p ~~ 1 \r 11~

~~ J

4'-7 3/4" [1416mm]

~---------s~~~o ____ ~

TURBINE AIR INLET FILTER APPROXIMATE WEIGHT : 1290 LBS [586 KG]

LOOSE SHIPPED ITEM

P/N-1039339-3M511

17'-1 3/8"

[5218mm]

t 11 1/8" [282mm]'--i-----

7 3/8" [188mmr

CUSTOMER/END USER/PROJECT

CHEVRON CVX GOM VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO.

3M511-149607

H

t--

G

t--

F

t--

E

D

t--

c

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t--

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8 I 7 I 6 I 5 v 4 I 3 I 2 I 1

H H

r-- r--

G G

4'-3" L1295mmj

r-- 4'-0" 1 1/2" r--L1219mmJ -(38mm]

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3'-9" [013mm]

F [1143mm] /em"""'" F (9 EQ. SPCS) 30 PLACES)

I/ r- ....,

0 0 0 0 0 0 0 0 0

r-- r--0 0

00000000000000 0 0000000000000 0

00000000000000 E 0000000000000 1'-8" 2'-0" E 0 0

[508mm] [610mm]

00000000000000 (4 EQ. SPCS)

0 0000000000000 0

0 00000000000000

0

f--1> b. """ 0 0 0 0 0 0 0 0 0 0 f:J-

1 1/2" [38mm]

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B CUSTOMER/END USER/PROJECT

B CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

r-- MKIII 8FT, SATURN 20 r--T .A. I. SILENCER GENERATOR SET ~ATOJ

MECHANICAL INTE FAC APPROX. WEIGHT: 450 LBS [204 KG.]

LOOSE SHIPPED ITEM Solar Turbines A P/N AX-1260-108 A Caterpillar Company

A DRAWING NO.

1SIZE rEV

3M511-149607 8 AO

ISH 32

If Tl-IIS COPYRIGHTED WCRK AND THE INFOR~TION HEREIN IS PROPRIETARY TO CATERPILlAR

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8 7 6

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5

¢1/2" [¢13mm]

(THRU-HOLE) (12 PLACES)

(ON A 23.00 DIA. BOLT CIRCLE)

4

2 3/8"

[60mm1 [

-

-

-

TURBINE EXHAUST BELLOWS APPRO X. WEIGHT: 90 LBS [ 41 KG.]

LOOSE SHIPPED ITEM P/N AX-1619-300

-

-

+ 1'-10 [572

3

1/2" mm]

2

CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

G

F

E

D

c

B

A

8 7 6

H

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D

c

B

A

5

¢1/2" [¢13mm]

(THRU-HOLE) (12 PLACES)

(ON A 23.00 DIA. BOLT CIRCLE)

TURBINE EXHAUST SCARF APPROX. WEIGHT: 45 LBS [21 KG.]

LOOSE SHIPPED ITEM P /N AX-1629-400

4

1'-7 7/8" [505mm]

3 2

CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. EV

3M511-149607 AO

H

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c

B

A

8

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I 7 I 6 5

1--------------------. 6'-9" L2057mm·J,-----------------

1----------4'-1 1/4'_', -------­[1251mmj

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3'-9" f-- 1----- [22mm] [1143mm] -------1 (1YPICAL)

(9 EQUAL SPACES)

~--------~ 4'-3" 11295mmj,---------~~

1

4

2'-o" [610mm]

2'-1 1/4" [641mm]

TURBINE AIR INLET DUCT. OFFSET 30.00" APPROX. WEIGHT: 240 LBS [1 09 KG.]

LOOSE SHIPPED ITEM

P /N 1 104044-300

I 3 I

f-----------

f-------------

2

3'-2 1/4" [972mm]

I

CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

H

t--

G

t--

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t--

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7'-9" ~----------------------------------.L2362mmj,---------------------------------~

4'-1 1/4" ~--------------- [1251 mmJ,-----------------~

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3'-9" [1143mm]

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(9 EQUAL SPACES)

4'-3" ~----------------~L1295mmj,-----------------~

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TURBINE AIR INLET DUCT. OFFSET 30.00" APPROX. WEIGHT: 257 LBS [117 KG.]

LOOSE SHIPPED ITEM P /N 1104043-300

I

2'-o" [610mm]

3

r-----------

f-----------

I 2

3'-2 1/4" [972mm]

I

CUSTOMER/END USER/PROJECT

CHEVRON CVX GON VK 900

CVX-VK9

DRAWING TITLE

MKIII 8FT, SATURN 20 GENERATOR SET (KATO) MECHANICAL INTERFACE

Solar Turbines A Caterpillar Company

DRAWING NO. !SIZE fEV 1 8 1 AO 3M511-149607 ISH 36

H

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F

r--

E

D

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c

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4'-1 1/4" [1251mm]

4'-o" - -------- 11219mm

4'-3" 1295mm

~~-------- l1245mm] 4'-1" --------

2'-3" [686mm]

¢1/2" [-13mm]

(THRU-HOLE) (20 PLACES) ASSY)

ETHER DUCT (TO BOLT TOG

DUCT 24.00" R INLET . TURBINE AI LBS [68 KG.]

IGHT· 150 APPROX. WE S~IPPED ITEM

LOOSE 1222-105 P/N AX-

-

----::::-:;::;:;;;;;;AAMD~US5EEIR/PROJECT CUSTOMER/EN

CHEVRON CVX GON VK 900

CVX-VK9