Document Reference
CG-58C-04-C017-160002 API 616 COMBUSTION GAS TURBINE DATA SHEETS
Revision 1.0 Status IFI
Document Type DTS System / Unit 60 Discipline MEC Rev. Date 18-10-2013
Contractor Reference 3N911-API616 Class 3 Page 1 / 15
This document is the property of Total. It must not be stored, reproduced or disclosed to others without written authorization from the COMPANY
CG-58C-04-C017-160002-1.0.doc
YAQ PROJECT
COMMANDE No.: 4540040218
Project No. PJ-0550 / DDM No. YAM 09/010
API 616 COMBUSTION GAS TURBINE DATA SHEETS
1.0 IFI 27/09/13 ISSUED FOR INFORMATION DC KDD JJK
00 IFI 27/09/13 ISSUED FOR INFORMATION DC KDD JJK
Rev. Status Date Revision Memo Issued by Checked by Approved by
Reserved to COMPANY
This document is:
Review with comments Code 1 Review without comment Code 2
Rejected Code 3 Approved with comments Code 4 Approved without comments Code 5
Date : Signature :
Document Reference
CG-58C-04-C017-160002 API 616 COMBUSTION GAS TURBINE DATA SHEETS
Revision 1.0 Status IFI
Document Type DTS System / Unit 60 Discipline MEC Rev. Date 18-10-2013
Contractor Reference 3N911-API616 Class 3 Page 2 / 15
This document is the property of Total. It must not be stored, reproduced or disclosed to others without written authorization from the COMPANY
CG-58C-04-C017-160002-1.0.doc
TABLE OF MODIFICATIONS
Revision Description
00 ISSUED FOR INFORMATION
1.0 ISSUED FOR INFORMATION
Document Reference
CG-58C-04-C017-160002 API 616 COMBUSTION GAS TURBINE DATA SHEETS
Revision 1.0 Status IFI
Document Type DTS System / Unit 60 Discipline MEC Rev. Date 18-10-2013
Contractor Reference 3N911-API616 Class 3 Page 3 / 15
This document is the property of Total. It must not be stored, reproduced or disclosed to others without written authorization from the COMPANY
CG-58C-04-C017-160002-1.0.doc
TABLE OF CONTENTS
1. API 616 Data Sheet…………………………………………….………………………..Page 4 - 15
JOB NO. ITEM NO.
PURCHASE ORDER NO.
SPECIFICATION NO.
REVISION NO. DATE
PAGE OF BY
1 APPLICABLE TO: PROPOSAL X PURCHASE AS BUILT
2 FOR UNIT
3 SITE SERIAL NUMBER
4 SERVICE NUMBER REQUIRED
5 X CONTINUOUS INTERMITTENT STANDBY DRIVEN EQUIPMENT
6 MANUFACTURER Solar Turbines X MODEL ISO RATING (3.17) @ RPM
7 NOTE: INFORMATION TO BE COMPLETED: BY PURCHASER BY MANUFACTURER BY MFR IF NOT BY PURCHASER
8 GENERAL
9 CYCLE: REGEN X SIMPLE EXHAUST HEAT RECOVERY TYPE: SINGLE SHAFT X MULTI SHAFT
10 DRIVEN EQUIPMENT: NORMAL SHAFT, kW @ RPM RATED SHAFT, kW @ RPM
11 OUTPUT SHAFT SPEED RANGE (4.1.5) X MIN X MAX RPM
12 DESIRED MINIMUM SITE POWER kW @ RPM
13 OPERATION ATTENDED UNATTENDED X POTENTIAL MAXIMUM POWER (3.33) kW
14 PREDICTED PERFORMANCE LOCATION (4.1.19)
15 GAS TURBINE INCLUDING ALL LOSSES INDOOR X OUTDOOR X GRADE
16 SITE NORMAL SITE SITE HEATED UNDER ROOF MEZZANINE
17 RATED DUTY MAX MIN UNHEATED X PARTIAL SIDES
18 (3.45) (3.26) TEMP TEMP ELECRICAL AREA CLASSIFICATION (4.1.14)
19 DRY BULB TEMP., deg C NON-HAZARDOUS X HAZARDOUS
20 RELATIVE HUMIDITY, % APPLICABLE CODE: CENELEC NEC 505 IEC
21 BAROMETER, CLASS: GROUP: TEMP CODE: T3
22 OUTPUT, kW AREA CLASSIFICATION: DIVISION ZONE 2
23 HEAT RATE, LHV, kj/kW-hr X THIRD PARTY CERTIFICATION REQUIRED (Note 2)
24 WINTERIZATION REQUIRED
25 OUTPUT SHAFT SPEED, RPM TROPICALIZATION REQUIRED (5.4.6.6)
26 AIR FLOW, kg/hr UNUSUAL CONDITIONS: DUST FUMES
27 EXHAUST FLOW, kg/hr CORROSIVE AGENTS (4.10.1.1)
28 FIRING TEMP. (Note 3), deg C
29 EXHAUST TEMP., deg C OTHER (5.5.34)
30 PT EXIT TEMP., deg C NOISE SPECIFICATIONS: (4.1.10) (Note 1)
31 CERTIFIED POINT (3.26) APPLICABLE TO MACHINE: (5.7.4.1)
32 (1) INCLUDING STEAM WATER EFFECTS FOR SEE SPECIFICATION
33 EMISSION CONTROL AUGMENTATION (4.1.9) APPLICABLE TO NEIGHBORHOOD: (5.7.4.2)
34 STEAM FLOW, kg/HR SEE SPECIFICATION
35 WATER FLOW, m3/HR
36 PAINTING:
37 APPLICABLE SPECIFICATIONS: X MANUFACTURER'S STANDARD
38 API 616 GAS TURBINES FOR THE PETROLEUM, CHEMICAL OTHER
39 & GAS INDUSTRY SERVICES
40 GOVERNING SPECIFICATION (IF DIFFERENT) NOTE: All Data Sheets References to GG=Gas Generator
41 SS = Single Shaft and PT = Power Turbine
42 X VENDOR HAVING UNIT RESPONSIBILITY (4.1.2) REMARKS:
4343
44 SHIPMENT: (6.4)
45 DOMESTIC EXPORT EXPORT BOXING REQUIRED
46 OUTDOOR STORAGE MORE THAN 6 MONTHS (6.4.1)
47 SPARE ROTOR ASSEMBLY PACKAGED FOR (6.4.3.10) N/A
48 DOMESTIC EXPORT SHIPMENT
49 COMMENTS:
50
3N911
4540040218
B 10/17/2013
MARS 100-16000
A.Chouhan1 10
COMBUSTION GAS TURBINE (API 616-4TH)
DATA SHEET, S.I. UNITS
MARS 100-16000
TOTAL EP CONGO Solar Turbines Mars 100-16000 Generator Set
1390MYANGA Platform - FR3 Turbogenerator Replacement
Power Generation
MARS 100-16000 16000 hp See line 11
1
ABB Generator
4000 9500
See line 22
33.7 25.5 40 18.9
74 74 74 74
IIB
10063 8946 105109465
11887 11632 12142 11485
1500 1500 1500 1500
136683 142627 131274 146957
737 738 737 738
138988 145025 133502 149430
503 495 510 490
503 495 510 490
85 dBA at 1 meter
N/A N/A N/A N/A
N/A N/A N/A N/A
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS WRITTEN
PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
Note 1: 85 dBA @ 1 m, Refer to proposal
Solar
Note 2: Not Applicable
Note 3: Solar uses Compensated PTIT instead.
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 FUEL SYSTEM (5.8)
2 TYPE GAS (5.8.2) LIQUID (5.8.3) DUAL (5.8.1.5.1)
3 DUAL SYSTEM REQMTS (5.8.1.5.1) GAS/GAS GAS/LIQUID LIQUID/LIQUID
4 COMPLETE FUEL RECEIVING SYSTEM (5.8.1.1) MAX. TIME ALLOWED TO COMPLETE TRANSFER SECONDS5
6 GAS FUELS (5.8.2) LIQUID FUELS (5.8.3)
7 FUEL ANALYSIS - MOL % (5.8.2.1) (Note 1) FUEL GRADE (5.8.3.3)
8 COMPOSITION: M.W. NORMAL STARTING ALT ASTM D1655 ASTM 0GT 1GT
9 Methane (CH4) JET A A-1 B D2880 2GT 3GT 4GT
10 Ethane (C2H6) OTHER, INDICATE ANALYSIS BELOW (5.8.3.3 c)
11 Propane (C3H8) LIQUID FUEL TREATMENT REQUIRED YES NO
12 I-Butane (C4H10) TREATMENT SYSTEM BY VENDOR OTHER
13 N-Butane (C4H10) FUEL TRANSFER EQUIP REQUIRED (5.8.1.4.5) YES NO
14 I-Pentane (C5H12) HEATER REQUIRED (5.8.1.4.4) YES NO
15 N-Pentane (C5H12) X LIQUID FUEL PRESS REQUIRED, MAX/MIN, kPag Note 3 / Note 3
16 Hexane (C6H14) FUEL ANALYSIS DATA (5.8.3.3) ASTM MEASURED
17 Heptane (C7H16) PROPERTY METHOD VALUE
18 Octane (C8H18) VISCOSITY SSU, 38°C D-445
19 Carbone Dioxide (C02) DISTILLATION DATA D-86
20 Water Vapor (H20) 50% RECOVERY, °C MAX
21 Nitrogen (N2) END POINT, °C MAX
22 N-Nonane (C9H20) SULFUR CONTENT %WT. MAX. (SELECT APPL. METHOD)
23 N-Decane (C10H22) BOMB METHOD D-129
24 Hydrogen Sulfide (H2S) LAMP METHOD D-1266
25 HIGH-TEMP METHOD D-1552
26 CARBON RESIDUE (ON 10%)
27 BOTTOMS) % WT. MAX.
28 CONRADSON D-189
29 RAMSBOTTOM D-524
30 COPPER STRIP CORROSION PLATE D-130
31 3 HOURS AT 100°C MAXIMUM
32 AROMATIC CONTENT D-1319
33 ASH CONTENT D-482
34 SPECIFIC GRAVITY, 15°C D-1298
35 TOTAL FLASH POINT, °C D-56
36 AVG. MOL. WT. 22.5 POUR POINT, °C D-97
37 CORS AGNTS (5.8.2.3) PPM WATER D-95
38 CONTMNTS (5.8.2.2.1) PPM FILTERABLE DIRT. MG/100ML D-2276
39 LHV (kJ/Std. m3) (5.8.2.4) TRACE METALS (ATOMIC
40 FUEL PRESS.MAX/MIN, kPag Note 3 / / ABSORPTION PREFERRED) D-3605
41 FUEL TEMP MAX/MIN, °C Note 3/Note 2 SODIUM
42 X FUEL PRESSURE REQUIRED POTASSIUM
43 MAX/MIN, kPag Note 3 VANADIUM
44 COMPRESSION SYS REQD (5.8.1.2.2) YES NO CALCIUM
45 HEATER REQD (5.8.2.1) YES NO LEAD
46 RATE OF CHANGE OF LHV (5.8.2.4) OTHER METALS
47 REMARKS:
48
49 Note 2: At least 28°C above fuel dewpoint (per ES 9-98).
50 Note 3: Please refer to Mechanical Interface Drawing. LOWER HEATING VALUE, MJ/kg D-2382
51 FUEL SYSTEM PIPING
52 BY PASS AND VENT VALVE (3.7.1.3) ISOLATION BLOCK VALVES ANSI FLANGE RATING 300 RF
53 TWIN Y-TYPE STRAINER WITH CONTINUOUS FLOW NACE MATERIAL STANDARDS (4.10.1.8)
54 TRANSFER VALVE (5.8.1.2.4)
55
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
0.0546
0.0143
0.0100
3N911
B
DATA SHEET, S.I. UNITS
0.0577
1.4923
1.4556
MARS 100-16000
Note 3
0.4089
10/17/13
2 10 A.Chouhan
MARS 100-16000
5.7930
0.0341
4.4452
0.0081
1.4067
0.0045
0.0105
100
Note 1: If C6+ is greater than 0.3%, must specify C7 through C14.
40133.3
72.1636
12.6409
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 *Gas Producer Rotor CONSTRUCTION FEATURES (NOTE 1)
2 X SPEEDS: MATERIALS OF CONSTRUCTION (4.10)
3 MAX. CONT. RPM TRIP RPM COMPRESSOR ROTOR BLADES
4X
LATERAL CRITICAL SPEEDS (DAMPED) COMPRESSOR STATOR VANES
5 FIRST CRITICAL RPM MODE SHAFT BLADE/VANE COATING
6 SECOND CRITICAL RPM MODE TURBINE WHEELS OR
7 THIRD CRITICAL RPM MODE STAGE NOZZLES BLADES DISCS
8 FOURTH CRITICAL RPM MODE 1
9 PROTOTYPE OR MODIFIED ROTOR SUPPORT (4.7.3.5) 2
10 TRAIN LATERAL ANALYSIS REQUIRED (D.1.3) 3
11 TRAIN TORSIONAL ANALYSIS REQUIRED (2.7.4.5) 4
12 TORSIONAL CRITICAL SPEEDS:
13 FIRST CRITICAL RPM
14 SECOND CRITICAL RPM
15 THIRD CRITICAL RPM
16 FOURTH CRITICAL RPM COMBUSTORS
17 VIBRATION: (4.7.4.5) (7.2.3 o) COMPRESSOR CASING
18X ALLOWABLE TEST LEVEL SHAFT
COMBUSTOR CASING
19 CASE mm/SEC TURBINE CASING
20 X ROTATION, VIEWED FROM DRIVE END X CW CCW GAUGE BOARDS AND CONTROL PANELS
21 AIR COMPRESSOR:
22 STAGES MAX. TIP SPEED m/SEC GAUGE BOARDS
23 TYPE Axial PRESSURE RATIO X LOCATION
24 CASING SPLIT (2.2.3) X AXIAL RADIAL CONTROL PANELS (5.4.5.1.1) ON-SKID LOCAL OFF SKID LOCAL
25 ROTOR SOLID X BUILT UP X OFF SKID REMOTE
26 TURBINE: WEATHER PROTECTION REQUIRED YES NO
27 STAGES MAX. TIP SPEED m/SEC SPECIFICATION
28 CASING SPLIT (4.2.3) AXIAL X RADIAL ANNUNCIATOR REQUIRED (5.4.4.8.5)
29 ROTOR SOLID X BUILT UP X VISUAL DISPLAY UNIT (VDU) X KEYBOARD
30 COMBUSTORS: (4.3.2)
31 X SINGLE MULTIPLE, NUMBER
32 X GAS LIQUID DUAL FUEL
33 MAXIMUM ALLOW TEMP. VARIATION °C CONTROL SYSTEMS
34 APPLICABLE PLANE TYPE (5.4.1.5)
35 FUEL NOZZLES PER COMBUSTOR MECH PNEU HYDRA ELECTRIC X ELECTRONIC
36 X WOBBE INDEX NO. REQD (4.3.7) X MAX X MICROPROCESSOR BASED COMBINED
MIN
37 MAINTENANCE INTERVALS, HOURS SIGNAL SOURCE
38 X HOT GAS PATH INSPECTIONS SENSITIVITY RANGE TO
39 X MAJOR OVERHAULS TIME OF AC OUTAGE RIDEOUT MIN (5.4.1.6)
40 OTHER SHUT OFF VALVES FOR SHUT DOWN SENSORS (5.4.4.9) N/A
41 STARTING SYSTEM (5.4.2.1)
42 GOVERNOR (5.4.3) MANUAL SEMI AUTOMATIC X AUTOMATIC
43 X MFR'S STD. OTHER X MAKE X MODEL X PURGE (5.4.2.2) 4 minimum MINUTES (Note 2)
44 CONSTANT SPEED X VARIABLE SPEED SEPARATE SHUTDOWN VALVE TEST DURING OPERATION N/A
45 ISOCHRONOUS DROOP NOTE (1) FOR MULTIPLE SHAFT TURBINES, COMPLETE ALL
46 REMOTE SHUTDOWN SIGNAL X ELECTRIC APPLICABLE PROTIONS FOR EACH SHAFT.
47 PNEUMATIC HYDRAULIC NONE REMARKS:
48 MANUAL SPEED CHANGER, RPM MAX. MIN.
49 MAINTAIN TURBINE SPEED UPON FAILURE OF CONTROL
50 SIGNAL OR ACTUATOR
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
Note 3: Control Logix
Note 1: Refer to train torsional report.
Note 2: Purge time is set during commissioning per Service Bulletin 3.0/105.
30000 hrs N/A
A.B. Note 3
N/A
4000 hrs N/A 4 20 mA
40969
93 from avg
T5 (PT Inlet)
21
2 466.34
IN 903
17.3:1 Digital Gauge Panel (VDU On Skid)
15 355
Nodular Iron & WCI
410 Stainless Steel50.8 std 26.3 API w/SER
MIC P/P
3N911
B 10/17/2013
3 10 A.Chouhan
MARS 100-16000
11319 718 Ni Alloy
DATA SHEET, S.I. UNITS
MARS 100-16000
11170
17-4PH SS (variable) & 410 SS (fixed)
3032 Critically damped AISI 4340 Platinum Aluminide
4650 Critically damped
10385 Critically damped
- CM-247LC CMSX-4
Note 1
Note 1 Haynes 230 (Conv); Haynes 230 & 214 (SoLoNOx)
Waspaloy
Waspaloy
Note 1
Note 1
CM-247LC CMSX-3
-
JOB NO. ITEM NO. MARS 100-16000
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 *Power Turbine Rotor CONSTRUCTION FEATURES (NOTE 1)
2 X SPEEDS: MATERIALS OF CONSTRUCTION (4.10)
3 MAX. CONT. RPM TRIP RPM COMPRESSOR ROTOR BLADES
4X
LATERAL CRITICAL SPEEDS (DAMPED) COMPRESSOR STATOR VANES
5 FIRST CRITICAL RPM MODE SHAFT BLADE/VANE COATING
6 SECOND CRITICAL RPM MODE TURBINE WHEELS OR
7 THIRD CRITICAL RPM MODE STAGE NOZZLES BLADES DISCS
8 FOURTH CRITICAL RPM MODE 1
9 PROTOTYPE OR MODIFIED ROTOR SUPPORT (4.7.3.5) 2
10 TRAIN LATERAL ANALYSIS REQUIRED (D.1.3) 3
11 TRAIN TORSIONAL ANALYSIS REQUIRED (2.7.4.5) 4
12 TORSIONAL CRITICAL SPEEDS:
13 FIRST CRITICAL RPM
14 SECOND CRITICAL RPM
15 THIRD CRITICAL RPM
16 FOURTH CRITICAL RPM COMBUSTORS
17 VIBRATION: (4.7.4.5) (7.2.3 o) COMPRESSOR CASING
18X ALLOWABLE TEST LEVEL SHAFT
COMBUSTOR CASING
19 CASE mm/SEC TURBINE CASING
20 X ROTATION, VIEWED FROM DRIVE END X CW CCW GAUGE BOARDS AND CONTROL PANELS
21 AIR COMPRESSOR:
22 STAGES MAX. TIP SPEED m/SEC GAUGE BOARDS
23 TYPE PRESSURE RATIO X LOCATION
24 CASING SPLIT (2.2.3) AXIAL RADIAL CONTROL PANELS (5.4.5.1.1) ON-SKID LOCAL OFF SKID LOCAL
25 ROTOR SOLID BUILT UP X OFF SKID REMOTE
26 TURBINE: WEATHER PROTECTION REQUIRED YES NO
27 STAGES MAX. TIP SPEED m/SEC SPECIFICATION
28 CASING SPLIT (4.2.3) AXIAL X RADIAL ANNUNCIATOR REQUIRED (5.4.4.8.5)
29 ROTOR SOLID X BUILT UP X VISUAL DISPLAY UNIT (VDU) X KEYBOARD
30 COMBUSTORS: (4.3.2)
31 SINGLE MULTIPLE, NUMBER
32 X GAS LIQUID DUAL FUEL
33 MAXIMUM ALLOW TEMP. VARIATION °C CONTROL SYSTEMS
34 APPLICABLE PLANE TYPE (5.4.1.5)
35 FUEL NOZZLES PER COMBUSTOR MECH PNEU HYDRA ELECTRIC X ELECTRONIC
36 WOBBE INDEX NO. REQD (4.3.7) MAX X MICROPROCESSOR BASED COMBINED
MIN
37 MAINTENANCE INTERVALS, HOURS SIGNAL SOURCE
38 X HOT GAS PATH INSPECTIONS SENSITIVITY RANGE TO
39 X MAJOR OVERHAULS TIME OF AC OUTAGE RIDEOUT MIN (5.4.1.6)
40 OTHER SHUT OFF VALVES FOR SHUT DOWN SENSORS (5.4.4.9) N/A
41 STARTING SYSTEM (5.4.2.1)
42 GOVERNOR (5.4.3) MANUAL SEMI AUTOMATIC X AUTOMATIC
43 X MFR'S STD. OTHER X MAKE X MODEL X PURGE (5.4.2.2) 4 minimum MINUTES (Note 2)
44 CONSTANT SPEED VARIABLE SPEED SEPARATE SHUTDOWN VALVE TEST DURING OPERATION N/A
45 ISOCHRONOUS DROOP NOTE (1) FOR MULTIPLE SHAFT TURBINES, COMPLETE ALL
46 REMOTE SHUTDOWN SIGNAL X ELECTRIC APPLICABLE PROTIONS FOR EACH SHAFT.
47 PNEUMATIC HYDRAULIC NONE REMARKS:
48 MANUAL SPEED CHANGER, RPM MAX. MIN.
49 MAINTAIN TURBINE SPEED UPON FAILURE OF CONTROL
50 SIGNAL OR ACTUATOR
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
Note 3: Control Logix
Note 1: Refer to train torsional report.
Note 2: Purge time is set during commissioning per Service Bulletin 3.0/105.
30000 hrs N/A
A.B. Note 3
N/A
4000 hrs N/A 4 20 mA
Digital Gauge Panel (VDU On Skid)
2 567.53
Note 1
50.8 std 28.4 API w/SER
MIC P/P
Note 1
Note 1
Note 1
N 155 IN 792 718 Ni Alloy
N 155 IN 792 718 Ni Alloy
- -
8670 Critically damped
20000 Critically damped
N/A
3,085 Critically damped AISI 4340 N/A
MARS 100-16000
98999500 N/A
3N911
B 10/17/2013
DATA SHEET, S.I. UNITS 3b 10 A.Chouhan
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 CONSTRUCTION FEATURES CONTINUED (NOTE 1)
2 *Gas Producer Rotor BEARINGS AND BEARING HOUSINGS (4.8)
3 RADIAL BRG#1 BRG#2 BRG#3 THRUST ACTIVE INACTIVE
4 X TYPE X TYPE
5 X MANUFACTURER X MANUFACTURER
6 X LENGTH, mm X UNIT LOAD (ULTIMATE), kPA
7 X SHAFT DIAMETER, mm UNIT LOAD (SITE RATED), kPA
8 X UNIT LD (ACT/ALLOW), kPA X UNIT LOAD (MAX POTEN), kPA
9 X BASE MATERIAL X NO. OF PADS/AREA, cm2
10 X BABBITT THICKNESS, mm X BASE MATERIAL
11 X NO. PADS X BABBITT THICKNESS, mm
12 X LOAD: BETWEEN/ON PAD X PIVOT: CENTER/OFFSET, %
13 X PIVOT: CENTER/OFFSET, % LUBRICATION: FLOODED X DIRECTED
14 X DAMPER BEARING THRUST COLLAR: INTEGRAL X REPLACEABLE
15 BEARING MATERIAL
16 BEARING TEMPERATURE DEVICES SEE ATTACHED API-670 VIBRATION DETECTORS (4.8.5.3) SEE ATTACHED API-670
17 (4.8.5.5) DATA SHEET RADIAL VIBRATION DETECTORS: DATA SHEET
18 THERMOCOUPLES X TYPE Proximity Probes X MODEL
19 SELECTOR SWITCH & IND. BY: PURCH MFR X MFR
20 X RESISTANCE TEMPERATURE DETECTORS X NO. AT EACH SHAFT BEARING TOTAL NO.
21 X RESISTANCE MAT'L platinum X OHMS X OSCILLATOR-DEMODULATOR SUPPLIED BY
22 X SELECTOR SWITCH & IND. BY: PURCH X MFR X MFR X MODEL
23 X LOCATION-JOURNAL BEARING X MONITOR SUPPLIED BY (5.4.7.8.2)
24 NUMBER EA PD EVERY OTH PAD PER BRG X LOCATION ENCLOSURE
25 OTHER X MFR X MODEL
26 X LOCATION-THRUST BEARING X SCALE RGE X ALARM SET @ 63.5 µm
27 NO. (ACT) EA PD EVERY OTH PAD 2 PER BRG X SHTDWN X SET @ 101.6 µm X TIME DELAY 1 SEC
28 OTHER AXIAL POSITION DETECTOR (4.8.5.3):
29 NO.(INACT) EA PD EVERY OTH PAD 0 PER BRG SEE ATTACHED API-670 DATA SHEETS
30 OTHER X TYPE X MODEL
31 X MONITOR SUPPLIED BY (5.4.7.5) X MFR X NO. REQUIRED
32 X LOCATION ENCLOSURE X OSCILLATOR-DEMODULATOR SUPPLIED BY
33 X MFR X MODEL X MFR X MODEL
34 X SCALE RGE X ALARM SET @ °C X MONITOR SUPPLIED BY (3.4.7.8.2)
35 X SHTDWN X SET @ °C TIME DLY 0 SEC X LOCATION ENCLOSURE
36 REMARKS: X MFR X MODEL
37 X SCALE RGE X ALARM SET @ 101.6 µm
38 X SHTDWN X SET @ 177.8 µm X TIME DELAY 1 SEC
39 ACCELERATION TRANSDUCERS
40 SEE ATTACHED API-670 DATA SHEETS
41 X MFR X MODEL
42 X LOCATION X NUMBER
43 X MONITOR SUPPLIED BY (3.4.7.8.4) X
44 X LOCATION ENCLOSURE
45 X MFR X MODEL
46 X SCALE RGE 2.5 X ALARM SET @ 0.64 cm/s
47 X SHTDWN X SET @ 0.71 cm/s X TIME DELAY 1 SEC
48 NOTES (1) FOR MULTIPLE SHAFT TURBINES, COMPLETE ALL APPLICABLE PORTIONS FOR EACH SHAFT.
49 (2) Alarm @ 61.1°C, Shutdown @ 69.4°C, bearing drain temperature above bearing oil inlet temperature.
50 (3) Additional settings are: Alarm @ 50°C, Shutdown @ 55.6°C, thrust bearing temperature above bearing oil inlet temperature.
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
No No No
100 Solar
Bently Nevada 3300XL
Solar
Control Console
56%
Between Between Between
56% 56%
1.524 Chrome Copper
5 5 5 1.52
1.524 1.524
3N911
B 10/17/2013
4 10 A.Chouhan
MARS 100-16000
Tilt Pad Tilt Pad Tilt Pad Fixed TaperedTilt Pad
DATA SHEET, S.I. UNITS
MARS 100-16000
Waukesha Solar
57.252 57.252 57.252 76 >68.94
Waukesha
114.491114.491 114.491
Waukesha Waukesha
33.43 N/A
AISI 1010-1030 SteelAISI 1010-1030 SteelAISI 1010-1030 Steel 10 / 20,258 8 / 21,290
4.31 / 17.2 4.93 / 17.2 6.36 / 17.2
3300XL
Bently Nevada
2 6
Carbon Steel
0.62
N/A70%
3300XL
Non EP
Total of 2 (# 1, # 2&3 bearing common drains, Note 2) Bently Nevada 1701
0-254
Proximity Probes
Solar Bently Nevada 2
Control Console Non EP Solar
Allen Bradley Logix5000 Bently Nevada 3300XL
Bently Nevada 1701
635-0-635
-18 to 150 115.6 (3) Solar
121.1 (3) Control Console Non EP
1701
Bently Nevada
Accessory Gearbox
Control Console
Bently Nevada
4-131
1
Solar
Non EP
X
X
JOB NO. ITEM NO. MARS 100-16000
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 *Power Turbine Rotor CONSTRUCTION FEATURES CONTINUED (NOTE 1)
2 BEARINGS AND BEARING HOUSINGS (4.8)
3 RADIAL THRUST ACTIVE INACTIVE
4 X TYPE X TYPE
5 X MANUFACTURER X MANUFACTURER
6 X LENGTH, mm X UNIT LOAD (ULTIMATE), kPA
7 X SHAFT DIAMETER, mm UNIT LOAD (SITE RATED), kPA
8 X UNIT LD (ACT/ALLOW), kPA X UNIT LOAD (MAX POTEN), kPA
9 X BASE MATERIAL X NO. OF PADS/AREA, cm2
10 X BABBITT THICKNESS, mm X BASE MATERIAL
11 X NO. PADS X BABBITT THICKNESS, mm
12 X LOAD: BETWEEN/ON PAD X PIVOT: CENTER/OFFSET, %
13 X PIVOT: CENTER/OFFSET, % LUBRICATION: FLOODED X DIRECTED
14 X DAMPER BEARING THRUST COLLAR: INTEGRAL X REPLACEABLE
15 BEARING MATERIAL
16 BEARING TEMPERATURE DEVICES SEE ATTACHED API-670 VIBRATION DETECTORS (4.8.5.3) SEE ATTACHED API-670
17 (4.8.5.5) DATA SHEET RADIAL VIBRATION DETECTORS: DATA SHEET
18 THERMOCOUPLES X TYPE Proximity Probes X MODEL
19 SELECTOR SWITCH & IND. BY: PURCH MFR X MFR
20 X RESISTANCE TEMPERATURE DETECTORS X NO. AT EACH SHAFT BEARING TOTAL NO.
21 RESISTANCE MAT'L platinum X OHMS X OSCILLATOR-DEMODULATOR SUPPLIED BY
22 X SELECTOR SWITCH & IND. BY: PURCH X MFR X MFR X MODEL
23 X LOCATION-JOURNAL BEARING X MONITOR SUPPLIED BY (5.4.7.8.2)
24 NUMBER EA PD EVERY OTH PAD PER BRG X LOCATION ENCLOSURE
25 OTHER X MFR X MODEL
26 X LOCATION-THRUST BEARING X SCALE RGE X ALARM SET @ 63.5 µm
27 NO. (ACT) EA PD EVERY OTH PAD 2 PER BRG X SHTDWN X SET @ 101.6 µm X TIME DELAY 1 SEC
28 OTHER AXIAL POSITION DETECTOR (4.8.5.3):
29 NO.(INACT) EA PD EVERY OTH PAD 0 PER BRG SEE ATTACHED API-670 DATA SHEETS
30 OTHER X TYPE X MODEL
31 X MONITOR SUPPLIED BY (5.4.7.5) X MFR X NO. REQUIRED
32 X LOCATION ENCLOSURE X OSCILLATOR-DEMODULATOR SUPPLIED BY
33 X MFR X MODEL X MFR X MODEL
34 X SCALE RGE X ALARM SET @ °C X MONITOR SUPPLIED BY (3.4.7.8.2)
35 X SHTDWN X SET @ °C TIME DLY 0 SEC X LOCATION ENCLOSURE
36 REMARKS: X MFR X MODEL
37 X SCALE RGE X ALARM SET @ 101.6 µm
38 X SHTDWN X SET @ 177.8 µm X TIME DELAY 1 SEC
39 ACCELERATION TRANSDUCERS
40 SEE ATTACHED API-670 DATA SHEETS
41 MFR MODEL
42 LOCATION NUMBER
43 MONITOR SUPPLIED BY (3.4.7.8.4)
44 LOCATION ENCLOSURE
45 MFR MODEL
46 SCALE RGE ALARM SET @
47 SHTDWN SET @ TIME DELAY SEC
48 NOTES (1) FOR MULTIPLE SHAFT TURBINES, COMPLETE ALL APPLICABLE PORTIONS FOR EACH SHAFT.
49 (2) Alarm @ 25°C, Shutdown @ 27.8°C, bearing drain temperature above bearing oil inlet temperature.
50 (3) Additional settings are: Alarm @ 50°C, Shutdown @ 55.6°C, thrust bearing temperature above bearing oil inlet temperature.
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT
EXPRESS WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS
PROHIBITED."
Bently Nevada 1701
635-0-635
-18 to 150 115.6 (3) Solar
121.1 (3) Control Console Non EP
Control Console SolarNon EP
Allen Bradley Logix5000 Bently Nevada 3300XL
3300XL
Solar Bently Nevada 2
0-254
Proximity Probe
Solar
Control Console Non EP
Total of 1 (# 4&5 bearing common drain, Note 2) Bently Nevada 1701
100 Solar
Bently Nevada 3300XL
3300XL
Bently Nevada
2 4
56% 56%
No No
Between On 70% N/A
5 5 1.524 0.62
1.524 1.524 Chrome Copper Carbon Steel
AISI 1010-1030 SteelAISI 1010-1030 Steel 11 / 24,516 10 / 17,806.4
6.03 / 17.2 0.61 / 17.2 23.78 N/A
133.571 114.491
66.777 57.252 >68.9 >68.9
Tilt Pad Fixed Tapered
Waukesha Waukesha Waukesha Solar
MARS 100-16000
BRG#4 BRG#5
Tilt Pad Tilt Pad
3N911
B 10/17/2013
DATA SHEET, S.I. UNITS 4b 10 A.Chouhan
X
JOB NO. ITEM NO. MARS 100-16000
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
DATA SHEET, S.I. UNITS PAGE OF BY
1 UTILITIES: CONNECTIONS
2 UTILITY CONDITIONS: TOTAL UTILITY CONSUMPTION:
3 STEAM: AUXILIARYDRIVERS HEATING COOLING WATER m3/HR
4 INLET MIN kPag °C kPag °C STEAM LEVEL kPag kPag kPag
5 NORM kPag °C kPag °C STEAM, NORMAL kPag kPag kg/HR
6 MAX kPag °C kPag °C STEAM, MAX kPag kPag kg/HR
7 EXHST MIN. kPag °C kPag °C INSTRUMENT AIR Nm3/HR
8 NORM kPag °C kPag °C MOTORS (AUXILIARIES) kW
9 MAX kPag °C kPag °C BATTERY CHARGERS kW
10 STARTING INJECTION HEATERS kW
11 INLET MIN kPag °C kPag °C PURGE (AIR OR N2) Nm3/HR
12 NORM kPag °C kPag °C TURBINE AIR EXTRACTION REQUIRED: (4.1.22)
13 MAX kPag °C kPag °C Nm3/HR @ kPag
14 EXHST MIN. kPag °C MAX. PRESSURE AVAILABLE AT MIN. SPEED: kPag
15 NORM kPag °C MINIMUM SPEED: RPM
16 MAX kPag °C DISCHARGE TEMPERATURE °C
17 ELECTRICITY: (5.4.6.1) PILOT LIGHT INDICATORS COMPRESSOR EXTRACTION STAGE NUMBER:
18 MOTORS HEATING CONTROL SHUTDOWN REMARKS:
19 VOLTAGE
20 HERTZ
21 PHASE
22 COOLING WATER:
23 INLET TEMP. °C MAX RETURN °C
24 DESIGN TEMPERATURE °C
25 NORM PRESS kPag MIN RETURN kPag
26 DESIGN PRESS kPag MAX ALLOW ∆ P kPag
27 WATER SOURCE
28 INSTRUMENT AIR PRESSURE DESIGN, kPag
29 MAX NORMAL MIN
30 REMARKS:
31
32
33
34
35
36
37
38 PURCHASER CONNECTIONS
39
40 DESIGN FACING FLANGED MATING FLG GAS
41 CONNECTION APPROVAL SIZE and POSITION OR & GASKET VELOCITY
42 REQ'D RATING (4.4.1) STUDDED BY VENDOR M/SEC
43 (4.10.4.6.4) (4.4.1) (4.4.5.4)
44 INLET
45 EXHAUST
46 FUEL SUPPLY
47 STEAM
48 WATER
49
50
51
52
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT
EXPRESS WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS
PROHIBITED."
MARS 100-16000
3N911
B 10/17/2013
5 10 A.Chouhan
By customer, if required
By customer, if required
Note 1: For Utility information please refer to
Utility List document provided separately.
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 INSTRUMENTS
2 TRANS- CONTROL
3 INSTRUMENT INSTRUMENT SIGNAL MITTERS ROOM
4 TYPE VIEWING LOCATION FURNISHED RECEIVERS
5 DESCRIPTION BY FURN BY
6
.. 7
..8
..9
10
IND
ICA
TIN
G
RE
CO
RD
ING
LO
CA
L
LO
CA
L P
AN
EL
CO
NT
RO
L
RO
OM
VE
ND
OR
OT
HE
RS
VE
ND
OR
OT
HE
RS
11 GAS GENERATOR OR SINGLE SHAFT GAS TURBINE
TACHOMETER(S) (NO. )
13 ∆ P AIR INLET SYSTEM
14 COMPRESSOR DISCHARGE PRESSURE
15 FUEL FILTER ∆ P
16 FUEL SUPPLY PRESSURE
17 STARTING GAS SUPPLY PRESSURE
18 STARTING GAS EXHAUST PRESSURE
19 TEMP COMBUSTOR MEASUREMENT (6 PTS MIN) (4.3.2)
20 TEMP GAS TURB CONTROL PLANE (6 PTS MIN)
21 INLET AIR TEMPERATURE
22 TEMPERATURE, GG COMPRESSOR DISCHARGE
23 TEMPERATURE, THRUST BEARING OIL DRAIN
24 TEMPERATURE, EACH BEARING SUMP (ROLLING ELEMENT TYPE)
25 TEMPERATURE, FUEL MANIFOLD
26 TEMPERATURE, LUBE OIL RESERVOIR
27 FIRED HOUR METER
28 A) NUMBER STARTS COUNTER
29 B) START SEQUENCE TIMER
30 LUBE OIL RESERVOIR LEVEL
LUBE OIL PUMP PRESSURE INDICATORS (NO )
32 LUBE OIL COOLER OIL INLET TEMPERATURE
33 LUBE OIL COOLER OIL OUTLET TEMPERATURE
34 LUBE OIL COOLER COOLANT INLET TEMPERATURE
35 LUBE OIL COOLER COOLANT OUTLET TEMPERATURE
36 LUBE OIL FILTER ∆ P
LUBE OIL PRESSURE EACH LEVEL (NO. ) Same as 31
38 CONTROL OIL PRESSURE
SITE FLOW INDICATOR EACH DRAIN (NO. )
40 INLET GUIDE VANE POSITION INDICATOR
41 EXHAUST DUCT DIFFERENTIAL PRESSURE INDICATOR
42 ENCLOSURE COOLING AIR EXHAUST TEMPERATURE
43 POWER TURBINE
TACHOMETER(S) (NO. )
45 EXHAUST TEMPERATURE (2 PTS MIN)
46 JOURNAL BEARING TEMPERATURE
47 THRUST BEARING TEMPERATURE
48 BEARING DRAIN TEMPERATURE
SITE FLOW INDICATOR EACH DRAIN (NO. )
50 LUBE OIL INLET PRESSURE Same as 31
51 LUBE OIL INLET TEMPERATURE Same as 33
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT
EXPRESS WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS
PROHIBITED."
MARS 100-16000
3N911
B 10/17/2013
DATA SHEET, S.I. UNITS
MARS 100-16000
6
6 10 A.Chouhan
1
1
1
2
6
44
49
12
31
37
39
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 ALARMS AND SHUTDOWNS (5.4.4)
2
3
4
5 DESCRIPTION
APPLIES TO: (5.4.4.8.5)
ANNUNCIATOR
POINT IN
VENDOR FURNISHED
CONTROL PANEL
SENSING
DEVICES TO
BE FURNISHED
BY
IND
ICA
TIN
G
LIG
HT
ON
LY
6 SINGLE SEP (1)
7 SHAFT PWR ALARM SHUT- VENDOR OTHERS
8 OR G.G. TURB. DOWN (2)
RADIAL SHAFT VIBRATION (NO. )
AXIAL THRUST POSITION (NO. )
OVERSPEED (1) (NO. )
CASING VIBRATION (NO. ) Accessory Gearbox
13 HIGH THRUST BEARING TEMPERATURE
14 HIGH RADIAL BEARING TEMPERATURE (Note 3)
15 LOW FUEL SUPPLY PRESSURE
16 HIGH FUEL FILTER ∆ P
17 GAS TURBINE TEMPERATURE SPREAD HIGH
18 EXHAUST OVER TEMPERATURE (Note 4)
19 FAILURE OF OVER-TEMPERATURE SHUTDOWN DEVICE
20 HIGH INLET AIR ∆ P EACH FILTER
21 COMBUSTOR FLAME-OUT (1)
22 CHIP DETECTOR, ANTI FRICTION BEARING
23 FAILURE STARTING CLUTCH TO ENGAGE OR DISENGAGE
LOW OIL PRESSURE (NO. )
25 HIGH LUBE OIL TEMPERATURE
26 LOW LUBE OIL RESERVOIR LEVEL
27 HIGH LUBE OIL RESERVOIR LEVEL
HIGH OIL FILTER ∆P (NO. )
29 LUBE OIL SPARE (AC) PUMP OPERATING
30 LOW CONTROL OIL PRESSURE
31 LOW STARTING GAS PRESSURE
32 ANTI-ICING SYSTEM - NOT OPERATING
33 LOW D.C. VOLTAGE
34 EMERGENCY D.C. PUMP OPERATING
35 RESERVOIR HEATER "ON"
36 IMPLOSION DOOR OPEN
37 EXTERNAL PERMISSIVE START SIGNAL
38 EXTERNAL SHUTDOWN SIGNAL
39 LOSS OF AUXILIARY COOLING AIR
40 LAMP TEST PUSH BUTTON
41 ENCLOSURE HIGH TEMPERATURE
42 CONTROL SIGNAL FAILURE (Microprocessor Failure)
43 CONTROL SYSTEM ACTUATOR FAILURE
44 GOVERNOR FAILURE Same as 42
45 ENCLOSURE VENT FAN FAILURE
46
47
48
49 NOTES: (1) VENDOR TO ADVISE METHOD OF ANNUNCIATION (3) RADIAL BEARING DRAIN TEMPERATURE IS USED INSTEAD.
50 (2) VDU MAY USE MESSAGE INDICATOR (4) TURBINE ROTOR INLET TEMPERATURE (T5) IS USED INSTEAD.
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT
EXPRESS WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS
PROHIBITED."
3N911
B 10/17/2013
10 A.Chouhan
MARS 100-16000
DATA SHEET, S.I. UNITS
MARS 100-16000
109
7
9
1
1
1
128
10
11
12
24
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 ACCESSORIES SUPPLIED BY GAS TURBINE MANUFACTURER
2 STARTING AND HELPER DRIVERS (5.1) GEARS: SEE SEPARATE API 613 GEAR DATA SHEETS (5.2.1.1)
3 X STARTER ONLY (5.1.1.2) STARTER/HELPER (5.1.1.3) X DRIVEN EQUIPMENT, SEE SEPARATE API DATA SHEETS
4 TYPE (5.1.1.1) X MOTOR STEAM TURBINE X FIRE PROTECTION EQUIPMENT (5.7.3.1)
5 GAS EXPANDER IC ENGINE HYDRAULIC TYPE HALON 1301 HALON 1211 CO2 Note 3
6 GAS TURBINE X STARTER IS CLUTCHED (5.1.1.7) X TYPE OF SENSOR X NO. OF DETECTORS
7 HELPER RATING (5.1.2.2) kW X MULTI SPECTRUM IR NUMBER
8 STARTER RATING (5.1.2.1) kW UV/IR NUMBER
9 SHAFT TURNING DEVICE REQUIRED (5.1.3.1) N/A ADDITIONAL LEVELS (5.7.3.2)
10 X MOTOR:
11 TYPE RATING kW MOUNTING PLATES (5.3)
12 MFR MODEL TYPE (5.3.1.1) SOLEPLATE X BASEPLATE
13 STEAM TURBINE (REFERENCE API DATA SHEETS) (Note 1) X SHIM PACK THICKNESS mm (5.3.1.2.9)
14 MFR MODEL
15 kW MAX. STEAM FLOW kg/HR BASEPLATE (5.3.2)
16 TOTAL/START kg X FURNISHED BY (5.3.2.1)GAS TURBINE ONLY EXTENDED FOR (3.3.2.7)
17 GAS EXPANDER GAS TURBINE ONLY EXTENDED FOR
18 APPLICABLE SPEC. (5.1.1.6) SUB-SOLEPLATES REQ'D (5.3.2.7) N/A DRIP RIM N/A
19 MFR MODEL COLUMN MOUNTING (5.3.2.4) (3-POINT) LEVELING PADS (5.3.2.3)
20 kW MAX. GAS FLOW kg/HR
21 TOTAL/START kg X ENCLOSURE REQUIRED
22 GAS FOR EXPANSION TURBINE: REQUIREMENTS (5.7.5.1)
23 MIN MAX NORMAL X ACOUSTICAL
24 INLET PRESSURE, kPa X WEATHERPROOF
25 EXHAUST PRESS, kPa X SAFETY
26 GAS TEMPERATURE, °C INLET X FIRE PROTECTION
27 GAS TEMP., °C EXHAUST ADDITIONAL VENTILATION (5.7.5.6.3)
28 MOLECULAR WEIGHT COUPLINGS AND GUARDS (5.2.2)
29 SPEED CONTROL GOVERNOR PRESSURE REGULATOR SEE ATTACHED API-671 DATA SHEETS
30 YES NO X MANUFACTURER X TYPE
31 INLET CONTROL VALVE FURNISHED X MODEL X GUARD SUPPLIED BY
32 STAINLESS STEEL PIPING MANIFOLD X MAXIMUM OUTSIDE DIAMETER mm
33 CARBON STEEL FLANGES X HUB WEIGHT kg
34 Y-STRAINER W/BREAKOUT FLANGES X SPACER LENGTH mm SPACER WEIGHT kg
35 LOW SPEED CAPABILITY IDLING ADAPTER REQ'D N/A SOLO PLATE REQUIRED
36 (FOR COMPRESSOR CLEANING) X GUARD SUPPLIED BY
37 RELIEF VALVE PRESSURE SET POINT kPag TYPE: X FULLY ENCLOSED SEMI-OPEN OTHER
38 CASING MATERIAL LUBRICATING REQUIREMENTS:
39 SEAL TYPE X NON-LUBE GREASE CONT. OIL LUBE
40 QUANTITY PER HUB kg or m3/HR
41 INTERNAL COMBUSTION ENGINE REMARKS:
42 TYPE SPARK IGNITED DIESEL
43 APPLICABLE SPECIFICATION (5.1.1.6)
44 MFR MODEL
45 SPEED RPM POWER kW
46
47 GAS TURBINE
48 APPLICABLE SPECIFICATION (5.1.1.6)
49 MFR MODEL
50 SPEED RPM POWER kW
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
859
N/A
Note 1: Solar does not use steam turbines.
Note 3: Fire suppression system is Water Mist type
Note 2 (Refer to Leveling Pads on line 19): Solar uses internal machined surfaces,
where the rotating equipment is mounted (and shimmed) for equipment softfoot and
alignment procedures.
N/A
Solar
10/17/2013
8 10 A.ChouhanDATA SHEET, S.I. UNITS
MARS 100-16000
93
3N911
B
4
14 Gas Detectors
VFD Induction 93
Reliance Mars Starter
N/A
Solar
ENCLOSURES (5.7.5)
Kopflex Dry Coupling
304 RZ Solar
MARS 100-16000
36
230.9
19.1 (Driving), 16.9 (Driven)
JOB NO. ITEM NO. MARS 100-16000
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
DATA SHEET, S.I. UNITS PAGE OF BY
1 ACCESSORIES SUPPLIED BY GAS TURBINE MANUFACTURER
2 INLET SYSTEM EXHAUST SYSTEM
3 X AIR FILTER (5.5.4.1) EXTENT OF FURNISHED INSULATION (SEE SKETCH) (5.7.1.2)
4 INERTIAL TYPE SEPARATOR MEDIA FILTERS (RELIEF) (DIVERSION) VALVE (5.5.8.8)
5 PAD TYPE PREFILTERS COMBINATION EXHAUST HEAT RECOVERY SYSTEM (5.5.3.1)
6 SELF CLEANING (PULSE TYPE) X EMISSION CONTROL SYSTEM (5.5.3.1)
7 SINGLE STAGE WITH PROVISION FOR PLATE ELEMENT MATERIAL (5.5.5.2.3)
8 FUTURE EXTRA STAGES YES NO
9 X NORMAL DUST LOADING EMISSIONS SAMPLING SYSTEM (5.5.6.10)
10 X WIND DESIGN VELOCITY X EXPANSION JOINT MFR TYPE
11 X SNOW LOAD DUCTING GAUGE/MATERIAL /
12 X SEISMIC ZONE X SILENCER MFR ∆P
13 LOCATION: GROUND LEVEL ELEVATED (5.5.4.6) HEAT RECOVERY DEVICE (Note 1)
14 X FILTRATION EFFICIENCY % (5.5.4.3) MFR TYPE ∆P mm H2O
15 X MAINTENANCE INTERVAL MONTHS STEAM GEN: PRESS kPag TEMP °C
16 X CLEANING FREQUENCY DAYS RATE kg/HR
17 IMPLOSION DOOR (5.5.4.5) N/A MANOMTR MFR MODEL RANGE mm H2O
18 EVAPORATIVE COOLER (5.6.1.1) ANTI-ICING (5.5.3.10) ATMOSPHERIC RELIEF DEVICE (5.5.6.8) (Note 2)
19 LIQUID TO AIR EXCHANGER (5.6.2.2) N/A TYPE MFR LOCATION
20 WALKWAY, LADDERS, HANDRAILS REQUIRED (5.6.1.5) SYSTEM SITE RATED PRESSURE DROP mm H2O
21 COMP CLEANING SYSTEM, TYPE (5.5.3.9)
22 PLATE ELEMENT MAT'L (5.5.5.1.4) ATMOSPHERIC EMISSIONS
23 X FILTER MFR. MODEL EMISSION SUPPRESSION SYSTEM REQUIRED (5.8.4.1)
24 110% RATED AIR FLOW NOx REQUIREMENTS (5.5.3.1.1)
25 CLEAN ALARM NOx EMITTED
26 COOLER MFR. MODEL ∆ P mm H2O EMISSIONS REDUCTION METHOD (IF REQUIRED) (5.8.4.2)
27 EXCHANGER MFR (5.8.2.3) WATER INJECTION SCR
28 MODEL ∆ P STEAM DRY COMBUSTOR
29 X DUCTING GAUGE / MATERIAL OTHER
30 X EXPANSION JOINT MFR TYPE SOx REQUIREMENTS
31 X SILENCER MFR ∆ P SULFUR CONTENT OF FUEL
32 MANOMETER MFR MODEL SOx EMITTED (BASED ON STATED SULFUR CONTENT)
33 RANGE mm H2O
34 SYSTEM SITE RATED PRESSURE DROP mm H2O CO REQUIREMENTS
35 @ 110% RATED AIR FLOW CO EMITTED
36 REMARKS: PARTICULATE REQUIREMENTS
37 PARTICULATE EMITTED
38 UNBURNED HC REQUIREMENTS
39 UNBURNED HC EMITTED
40 APPLICABLE EMISSION CODES OR REGULATIONS
41 EPA - TITLE 40 - CFR OTHERS
42
43
44 SPECIALIZED INSTRUMENTS
45 TACHOMETERS (5.4.7.2.2) SWITCHES: (5.4.4.8.2)
46 TYPE ELECTRICAL X ELECTRONIC CIRCUIT SHALL
47 ANALOG X DIGITAL CRT ENERGIZE X DEENERGIZE TO ALARM
48 X MANUFACTURER ENERGIZE X DEENERGIZE TO SHUTDOWN
49 OIL FILLED PRESSURE GAUGES (5.4.7.6) ENCLOSURES
50 EXPLOSION PROOF WEATHER PROOF
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
33.7 m3/s
Note 1: Heat recovery device is not applicable.
Note 2: Atmospheric relief devices are not applicable as isolation dampers are
not provided with our exhaust system.
3/16" (4.76 mm) Thk./316 SS
36 mm H20Camfill Farr
Medium Velocity, 4-stage, LHS Access
40lb/ft2 (195.3 kg/m2)
Site Specific
120mph (193km/hr)
49 mm H2O 127 mm H2O
1
MARS 100-16000
Allen Bradley
101.6
Solar Fabric
101.6
316SS
Camfill Farr See line 3 above.
Site Specific
98
Badger Fabric
4 Cullum Detuners TBD
316 SS
3N911
B 10/17/2013
9 10 A.Chouhan
409 SS
JOB NO. ITEM NO.
COMBUSTION GAS TURBINE (API 616-4TH) REVISION DATE
PAGE OF BY
1 INSPECTION AND TESTING; LUBRICATION, WEIGHTS
2 SHOP INSPECTION AND TESTS: (6.1.1) WIT- OBSER- LUBRICATION SYSTEMS (4.9)
3 REQ NESSED VED SEE API 614 DATA SHEETS
4 SHOP INSPECTION (6.1.2) X LUBE OIL VISCOSITY (4.9.8) ISO GRADE
5 CLEANLINESS (6.2.3.3) COMMON TO X GAS GENERATOR/SINGLE SHAFT TURBINE
6 HYDROSTATIC (6.3.2) X X X FREE POWER TURBINE LOAD GEAR
7 MECHANICAL RUN (6.3.3) X X X DRIVEN EQUIPMENT AUXILIARIES
8 CONTRACT X IDLING (COMBINED) (SEPARATE) LUBE/SEAL SYSTEM (4.9.5)
9 COUPLING ADAPTOR(S) SYSTEM DESIGNED FOR SYNTHETIC LUBRICANT (4.9.2)
10 X CONTRACT SHOP LUBE SPECIFICATION
11 PROBES PROBES COMMON TO X GAS GENERATOR X POWER TURBINE
12 VIBRATION PLOTS (6.3.3.3.4) LOAD GEAR X DRIVEN EQUIPMENT
13 TAPE RECORD VIB DATA (6.3.3.3.6) AUXILIARIES
14 PERFORMANCE TEST (6.3.4.1) X X
15 COMPLETE UNIT TEST (6.3.4.2) FLOW PRESSURE HEAT LOAD
16 PACKAGE TEST (6.3.4.2.1) X OIL REQUIREMENTS m3/HR kPag MJ/HR
17 LOAD GEAR TEST (6.3.4.3) X X GG OR SS TURBINE
18 SOUND LEVEL TEST (6.3.4.4) DRIVEN EQUIPMENT
19 AUXILIARY EQUIPMENT (6.3.4.5) GEAR
20 POST TEST INSPECTION (6.3.4.6) COUPLINGS
21 HYDRAULIC COUPLING INSPECTION POWER TURBINE
22 GOVERNOR RESPONSE TEST (6.3.4.8) TOTAL
23 SPARE PARTS (6.3.4.9)
24 FIRE PROTECTION (6.3.4.10) X MOUNTING ARRANGEMENT
25 OTHER (6.3.4.11) CONSOLE COLUMN X BASEPLATE
26
27 MATERIALS INSPECTION REQUIREMENTS (6.2.1.3) X WEIGHTS DRY
28 SPECIAL CHARPY TESTING (4.10.5.3) INSTALLED SHIPPING DIMEN
29 RADIOGRAPHY REQUIRED FOR WT. (kg) WT. (kg) LxWxH (m)
30 MAGNETIC PARTICLE REQUIRED FOR GG OR SS TURBINE (A) (C)
31 LIQUID PENETRANT REQUIRED FOR SS TURB. ROTOR
32 ULTRASONIC REQUIRED FOR POWER TURBINE
33 WELD INSPECTION (4.10.4.6.1) P.T. ROTOR
34 WELDING HARDNESS TESTING (6.2.3.4) LUBE SYSTEM
35 DRIVEN EQUIP.
36 MISCELLANEOUS: FILTER
37 VENDOR'S REVIEW & COMMENTS ON PURCHASER'S INLET SILENCER
38 PIPING & FOUNDATION (4.1.18) EXHAUST SILENCER
39 FINAL ASSEMBLY CLEARANCES (6.2.1.1.e) DUCTING
40 COORD. MEETING SITE (7.1.3)
41 SPEED-TORQUE CURVE (7.2.4-a)
42 INCREASE POWER FOR STEAM/WATER (7.2.4-b)
43 EFFECTS OF AMB. COND. ON EXHAUST FLOW (7.2.4-c) MAX ERECTION
44 RUN DOWN CURVES (7.2.4-d) WEIGHT (kg) ITEM
45 PURCHASER REVIEW OF CAMP./GOODMAN DIAG. (4.5.3.3) MAX MAINTENANCE
46 VENDOR WITNESS ALIGNMENT (4.1.18) WEIGHT (kg) ITEM
47 TECHNICAL DATA MANUAL (7.3.6.4) REMARKS:
48 NO OF PROPOSAL COPIES (7.2.1)
49
50
51
52
53
"THIS COPYRIGHTED WORK AND THE INFORMATION HEREIN IS PROPRIETARY TO CATERPILLAR INC., SOLAR TURBINES INCORPORATED, AND/OR SUBSIDIARIES OF EITHER. WITHOUT EXPRESS
WRITTEN PERMISSION FROM CATERPILLAR INC. OR SOLAR TURBINES INCORPORATED. ANY COPYING, DISCLOSURE, OR USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED."
MARS 100-16000
Note B: Refer to Driven Equipment Data Sheet.
Note C: Turbine overall dimensions only. Excludes shipping crate.
Note A: Turbine weight excludes Acc Drive, Air Inlet & Exhaust Diffuser.
N/A
N/A
N/A
1598
N/A N/A
N/A N/A N/A
N/A N/A
N/A N/A N/A
N/A N/A
(B) (B) (B)
N/A N/A
Included N/A N/A
N/A ?
N/A N/A N/A
7940/9072
74 241 1,633
above.
N/A N/A N/A
Included in GG
2 241 60
26 241 532
46 (C46)
ES 9-224
46 241 1,041
DATA SHEET, S.I. UNITS
3N911
B 10/17/2013
10 10 A.Chouhan
MARS 100-16000