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©2009 Caterpillar® All rights reserved.

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3. Sensor Description Type Alarm Down Trip Comments FUEL PRESSURE TO FILTER WORD X 4 0 FUEL PRESSURE TO WORD X lt 260kPa 0 1000 kPa lt 20 kPa LOW ENGINE JACKET WATER EE RPM EIER PRESSURE 35 kPa Hi RPM OPTIONAL CIRCUIT WATER 1 WORD X 35kPa 0 1000 kPa OPTIONAL SEA WATER PRESSURE WORD X lt 35 kPa 10 1000 kPa OPTIONAL ENGINE STARTING AIR Sag WORD X 750kPa 0 4000 kPa OPTIONAL ENGINE INLET AIR MANIFOLD SA E WORD X gt 230 kPa 0 1000 kPa RTD AND THERMOCOUPLE ENGINE LUBE OIL ER TUR WORD X gt 92C 0 150 INLET AIR MANIFOLD D ERAT WORD X gt 92C 0450 ENGINE AC OC CIRCUIT OUTLET WATER TEMP WORD TOPCT JP ENGINE JACKET WATER OUTLET TEMP SHUTDOWN WORD 00 ENGINE JACKET WATER OUTLET TEMP ALARM WORDS X 1000 MEIE EXHAUST TO TURBO TEMP ER WORD X gt 630C 0 700 EXHAUST TO TURBO TEMP 0 700 C 12 amp 16 CYL RIGHT SERBI gt 630 ENGINE ONLY EXHAUST FROM TURBO TEMP LEFT WORD X gt 550C 0 700 EXHAUST FROM TURBO 0 700 C 12 amp 16 CYL TEMP RIGHT MORD 75500 ENGINE ONLY TEMPERATURE WORD x se ORE gt CYLINDER TEMPERATURE WORD x VENUE 2 2 CYLINDER TEMPERATURE WORD x Sou 3 E Z CYLINDER TEMPERATURE WORD X gt 550 0 700 CYLINDER TEMPERATURE 2 5 WORD X gt 550 0 700 C
4. Sensor Description Type Alarm Down Trip Comments PRELUBE START SWITCH 2 DIGITAL RELAY BASED SYSTEM PRELUBE START SWITCH PEU DIGITAL RELAY BASED SYSTEM ENGINE CONTROL SWITCH CONTACT LOCK OUT ENGINE AND OFF RESET CLOSE RESET SYSTEM ALARMISHUTDOWN CONTACT 2 DIGITAL INDICATES ACK ALARMS METAL PARTICLE DETECTOR DIGITAL X X CONTACT SHUTDOWN ANALOG SPEED amp PRESSURE TRANSDUCER MAG PICK UP ENGINE a x 113 RATED SPEED SWITCH SPEED SWITCH 8L 4171 SPEED CONTROL SENSOR INPUT TO ENGINE MAG PICK UP PLC 8L 4171 FREQ 4 ENGINE SPEED FROM SE 113 RATED 005 115 7954 DA P SPEED OM 0 1000 kPa USED CALCULATE OIL FILTER DIFF PRESS lt 320 kPa amp lt LUBE OIL PRESSURE TO 55 L 120 1606 141 9880 x lt 260kPa amp lt HIGH SPEED SETPNT 8 105 kPa SPEED SETPNT FUEL PRESSURE TO FILTER 4 oma 0 1000 kPa USED FOR 141 9880 DIFF ALARM FUEL PRESSURE TO 42 420mA X 260kPa 0 1000 kPa lt 20 kPa LOW ENGINE JACKET WATER l_ RPM PRESSURE 141 9880 lt 35 kPa HIGH Go onal 2 CIRCUIT WATER 5 SS 4 20 X 35kPa 0 1000 KPa OPTIONAL 2 PRESSURE TEIE 4204 X 35kPa 0 1000 kPa OPTIONAL E ENGINE STARTING AIR 420mA X lt 750kPa 044000 KPa OPTIONAL C ENGINE STARTING AIR PRESSURE SENDING UNIT OHMS
5. 1 IS3HLNIUY al 17 3HL HOIHM OL INN 3Y ll HOIHM NI v 5 03 INOW ws as 17 101 Iu 3 2018 ONIMY 3 318143 4 3JGIND 000 0000 NINI AHL 3HL OL 134117 4 AHL 1 1 1391 173 Ha TYNOLL aly NYAL PACKAGED GENSET FOUNDATION AND MOUNTING zi 3HLO 31 3801 31 1snvHx3 NVA Iv 31 n IGNTONI aan AWOL 35001 4 30vdS TYNOLLIGOV 31 401 3NI9N3 1 0 440 1NH Iv 3083 3 v3 137 384173 TYNOLL 3 1 20 H1 WNOLL M3IdvOv LJVHSMNvHO 30 33 4 8 38 3NION3 30 3 2 1 5 3NIIN3IN3O NOLL 2009 Caterpillar All rights reserved ASVMIXNV 1432 3 SINN M3idv v 13 5 2 30 30 3 3 OL NIVLY3d LON OG SQV3H ANIONS 30 3NIhi3IN39 20 JJVHSXNYWO 30 0 MOuuY HLIM SNOISN3AIQ AIHL SWniva HOIHM OL INN 0 3HL
6. 97 IN FOQUGUON e 97 Generator Engine Governing System 97 Engine Monitoring and 5 99 Engine Sh td Wn asses a qawa LUE X IER EE VEDI ER 99 Engine Monitoring dac Ld ea o E ERR LER DA EX XR ER 99 Control and Monitoring System Diagram 100 Control System Inputs to PLC and Redundant Relay Logic 106 MODBUS Address LS 117 Packaged Genset Foundation and Mounting 131 Foundation Design Chun aka 131 MoU nting u aa 131 General M 131 General Arrangement Drawings J U 131 RU ananas 145 02009 Caterpillar amp rights reserved Engine WeightS noris rena tos re rip iae cii cnin es iw cian Se re n E FE VOR IR VR 145 C280 3600 Witness Test Description J
7. FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 792 552 847 853 843 823 810 785 FROM ENGINE 7M M im 562 1022 1017 1013 OVERALL 63 125 250 500 1000 2000 4000 8000 BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1086 1057 FROM ENGINE 071 1164 1130 103 7 989 940 950 936 882 M 1 5M 118 0 128 9 127 5 117 3 112 5 108 1 109 5 107 1 101 3 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions
8. 1311 n ANCL 31 LES v 12 8 N 882 2 e z z T un gt 2 x 00 QI 43H NOISNYdX3 gt L SSVN LI IWNOILSO ANV NOLILVANNOY LYSNYD GYOVMDVd PACKAGED GENSET FOUNDATION AND MOUNTING 3Sv8 30 396 1NON4 837000 1303 3sva 3sv8 30 3015 401 821003 1304 10 3 948 D OT N3g 535 i 101 NdINI 110031 8 2231 NI 3dIS10H 3907 avay NILIMYYW ANINNELSNI d9 ON 40 1 9130 0905 990 508 M3NV3TO 88 108INOO SND 40 130 d9 9
9. 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M 1980 1072 104 1 1033 104 8 1005 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 1075 1847 964 511 557 872 853 799 FROM ENGINE 7M 103 0 1154 112 0 1027 M 1 5M 117 0 127 9 126 5 116 3 111 5 107 1 108 5 106 1 100 3 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTOR
10. 13 C280 3600 Technical Data Sheets 13 Lubrication Oil System oodd don adi 54 General 54 Internal Lubrication System u 54 PrelUBDTICAUON G1 AE 55 Generator Bearing Lube Oil System U 56 Oil Requirements muy u Saa u 56 Oil Change Interval E RR Ex vba eR 57 Inclination Capability siisii sanii cauaa nana itn tender niu eae 58 02009 Caterpillar amp rights reserved Customer Piping 5 58 Lub Oil System a 58 Crankcase Ventilation System cui sioe La Dres rad 60 Crankcase Emissions 60 Grankcase Fumes Disposal 60 Customer Piping ConnectiOnS assswvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnr 61 Feen 62 General NR 62 Internal Fuel System taie tan 62 External Fuel System Design Considerations
11. 62 Fuel Recommendations u u uuu a een uin CH Ou eH ka 64 Customer Piping Connections J J J 65 Fuel System Schematic 66 6869111019 KNEET M 67 General augu 7 7 67 Internal Cooling SyStemu 055885 444689666 8 8489 8 8 67 External Cooling System Design Considerations 67 Heat T 72 Generator Cooling cx i asaka iain 72 Cooling Water 72 Customer Piping ConnectiOnS sssswvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnr 73 Cooling System Schematics J 73 Starting Alt SySteDmm uu 76 EET TN NN a Y 76 Internal Starting Air 76 External Starting Air System Design Considerations
12. 76 Engine Piping Connections J J J J J 80 Starting Air System Schematic U 81 Combustion Air System iere iron 82 General 62 2009 Caterpillar rights reserved Combustion Air System Design Considerations 82 Combustion Air Piping System J sass 84 Engine Room Ventilation 85 General mu suntu ns s usu s s 85 SIZING GONSIGCTALONS hS 85 Engine Room 86 Ventilation FANS 88 Exhaust m M 88 Routing Considerations asas asas asa ea aaa aaa aaa aa sasa uana dn 89 5b da I E e E27 Litt t aoe 94 c n 94 Exhaust System Design Considerations 94 Engine Piping Connections u 95 Exhaust Gas PipIng 96 Engine Governing and Control System
13. OLLvW3H2S LINON 001 006 FE 006 NIT INT 30m a1 l 98 41 91 81 gt ANIA 31043 53 19207 53 HI gt Te ONIMA 05 110 1310 4401085 SIV t r 14 4 OG NSSDO3 1 313 mn 14 126 13 ASSITIXDV JLYNIASAL DNV t ers v138 ILYNINSIL NY UR x r l SI 3133 oa 1 83 13 Av 132 9130 31vMInS31 OT NYAI 3NIDN3 Nos 918 y 34 10 1503 or me 3 Wavy 3 4 1336 D REH 91 INIT 1 41 IA 13938 440 3NI1 1 1 1 30 0 1 ver 2 1 001 3NTT 81 IND le e ois ma jx EE 4 og s wni s ass S le eel y g v ek an ds EV BEN cu I NMOGLNHS ANV ONIYOLINOW YANIONT Caterpillar All rights reserved 2009 cc e ENGINE MONITORING AND SHUTDOWN I Y
14. LSL 3600LOW WATER LEVEL SWITCH HEAT RE AND TEMPERATURE DATA BASED ON 3600 JACKET WATER PUMP PRESSURE TRANSMITTER DATA BASED ON 25 AMBIENT AND 32 WATER TO AC CATERPILLAR PT 3601 AC OC WATER PUMP PRESSURE TRANSMITTER HEAT REJECTION TOLERANCES COOLANT FLOW 105 PT 3602 RAWWATER PRESSURE TRANSMITTER ACCOUNT FOR ENGINE ENGINE VARIATION TEST DATA T I 3601 COOLANT TEMPERATURE GAUGE AS AMBIENT AND ALTITUDE TOLERANCE GUIDELINES CAN BE FOUND IN TS 3604 JACKET WATER TEMPERATURE SWITCH ALARM a S 3605 JACKET WATER TEMPERATURE SWITCH SHUTDOWN DROP SHALL NOT EXCEED CATERPILLAR GUIDE LINES FOR SPECIFIC 3 3602 WATER OUTLET TEMPERATURE TRANSMITTER 3600 APPLICATO AND NSIALLATON GUIDE COOUNG SYSTEM SECTON me P amp ID COOLING SYSTEM 3603 AC OC INLET TEMPERATURE TRANSMITTER CUSTOMER SUPPLIED FLOW SETTING ORIFICE 509 4954 oo 19 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Starting Air System General The air starting system supplied by Caterpillar includes air starters lubricator not required for turbine starters air relay valve strainer shut off valve and pressure regulator if required 3600 Series engines use vane type starters as standard equipment with optional turbine starters by design to order C280 Series engines use TDI turbine star
15. 149 Maintenance Interval 151 Storage Preservation Specification J 154 Preservation Procedr saun usant 154 Typical Supplied Auxiliary 156 Reference Material 158 02009 Caterpillar amp rights reserved CATERPILLAR Introduction Engine Selection The use of Caterpillar engines in Petroleum Offshore applications requires specific considerations for engine selection and installation to ensure dependable performance and a long trouble free life The table below provides guidance on selecting the appropriate Caterpillar C280 3600 engine based on the customer specification An IMO emissions certified engine is the minimum requirement for operation offshore and the 3600 IMO certified engine provides the customer with the lowest initial installation cost If the customer is interested in reducing their fuel cost the C280 IMO certified engine provides the best fuel consumption for this engine family Alternatively if the customer specifies Latest Engine Technology the C280 IMO certified engine provides an electronically controlled fuel system over the mechanically controlled 3600 IMO engine Lastly if the customer specification details either EPA Marine Tier 2
16. erpilla Cat 2009 SSANMOIHL 139MSV9 SF ONILNOOW ANV NOLLVANNOY LYSNYAD AYDVMOV dg PACKAGED GENSET FOUNDATION AND MOUNTING zi 6 6 605 30119 9NLEDISVN 30 13 BW SNOSIQNO CARIS 358803400 552 30 IV 300 Jevn R ao 101 2 110031 l Qvooinv 9NIMVHO 23l TSA31 N G ON SILAY BAT 4 CALNNOW Suv V LON SAAL 1310 431 1 2009 Caterpillar rights reserved ec ef mal 5 1 Z SW3L 380071 ATlddNS aa4vaNnNv Ls 53108 66 60 AIS NOON 2055307 ONY ML Nope Ear p THE
17. 110251 ABEL z 341 301 INIT 11 96 81 08 41 vI 81 ino 391 x 1 AOGLNH T 3NTI y vu sJ por s NG 855 _ va TEI INIT 1 ET as 1 111 IN 128 12 25 1 I01NY INIA vat il 1 T1 SH i oe lt e lt n NAUTIDHS relle t 34055344 35 38 Sad 4 OULNHS N34Dl m eee qe i 00185 4 1 4 114 t 4 4 01 3415534 4 0 lt 14 NI 2031 8 rik I INIT STO 11123 INIT 1 1 13532 440 3 AV133 NADTINHS 7 fos n 4 3enss3ed 110 325 0 533 lt ee 5 T 1 1 ha e021 Heg e AISU3 T 7 an 1 0 INT 3NL1 3 17 TIIHLSIA 41 99 41 91 81 02009 Caterpillar
18. gt 550C CYLINDER TEMPERATURE TYPE K 8 128 16 CYL 7 124 4596 6 gt 550C ENGINE ONLY CYLINDER TEMPERATURE TYPE 8 12 8 16 CYL 8 124 4596 te 990C ENGINE ONLY CYLINDER TEMPERATURE TYPEK 12 amp 16 CYL 9 124 4596 16 A gt 550 ENGINE ONLY CYLINDER TEMPERATURE TYPEK 12 amp 16 CYL 10 124 4596 He gt 550 ENGINE ONLY CYLINDER TEMPERATURE TYPE 12 8 16 CYL 11 124 4596 1 2 gt 550 ENGINE ONLY CYLINDER TEMPERATURE TYPE K 12 amp 16 CYL 12 124 4596 6 A gt 550 ENGINE ONLY CYLINDER TEMPERATURE TYPE K 16 CYL ENGINE 13 124 4596 19 gt 550 6 CYLINDER TEMPERATURE TYPE 16 CYL ENGINE 14 124 4596 16 gt 550 6 ONLY 124 4596 CYLINDER mA TYPE K 16 CYL ENGINE TEMPERATURE 15 x gt 550C CYLINDER TEMPERATURE TYPE 16 CYL ENGINE 16 124 4596 x gt 550C MARINE GEAR INPUTS GEAR LOW OIL PRESSURE x CUSTOMER CUSTOMER SUPPLIED SWITCH SETPOINT CONTACT AUXILIARY INPUTS ANALOG AND RTD 0 150 C CUSTOMER CUSTOMER AUX RTD 1 RID x CONEIGURED SUPPLIED PT100 385 CATERPILLAR Signal Shut Setpoint Sensor Description Type Alarm Down Trip Comments AUX RTD 2 RTD x eo PT100 385 AUX 4 20 1 4 20 X CONEIGURED CUSTOMER SUPPLIED AUX 4 208 2 4 20 X CONEIGURED CUSTOMER SUPPLIED AUXILIARY INPUTS SWITCHES CONTACT CUSTOMER SUPPLIED AUX SWITCH 1 DIGITAL X CLOSE CONTAC
19. INL MANIFOLD SKID LIMIT M 1 FILL CAP 1 OPTIONAL T sj 1 ACCESSORY MODULE LIMIT AC OC ORIFICE OR REMOTE MOUNTED EQUIPMENT 0 4 EXPANSION BYPASS FLOW 22 NOTE 6 32 HEAT EXCHANGER ORIFICE HEAT REJ H2 2997 0 KW H E FLOW D i TEMP RISE 12 28 0 u u u u u u u u FULL FLOW Q2 1560 L MIN L LEGEND DESCRIPTION dr 1 OPTIONAL 1 1 BYPASS VALVE FUEL SKID LIMIT COOLER i HEAT REJ H6 33 ELECTRICAL LINE PIPING BY YARD SEAWATER INLET SEAWATER OUTLET TEMP REGULATOR OPTIONAL RANGE 27 GENERATOR OPTIONAL SKID LIMIT 3350 L MIN LUBE MODULE Li SEAWATER I
20. lt 11 i 5504 ARR FILTER H SHIP i OPTIONAL IN EE 3600 i EE i SKID MOUNTED OR REMOTE GMS PANEL i SKID LIMIT NOTE ALL ITEMS OUTSIDE SKID LIMIT ARE NOT DEALER SCOPE OF SUPPLY UNLESS OTHERWISE STATED METRIG 1 2755 AUTOCAD 1E0013Y CONFIDENTIALITY DESCRIPTION 5 1 0011 INTPR amp TOL Yellow EXHAUST GAS SILENCER custom PROD X ENGINE vocc 280 gt FLEXIBLE FITTING UNES OTHERWISE SPEGIPED sar 1 20 DIMENSIONS W O TOL ARE BASIC 10mm 20 2 THERMOCOUPLE QE Sas PROCESS LINE n CATERPILLAR A PERL SOM TAG No DESCRIPTION an samasaa Es SKID LIMIT 3600 INLET AIR MANIFOLD PRESSURE TRANSMITTER MARKETING GUIDE GATE VALVE TE 3600 EXHAUST STACK TEMPERATURE THERMOCOUPLE 5 TT 3600 INLET AR MANIFOLD BOOST TEMPERATURE TRANSMITTER me P amp ID AIR INTAKE EXHAUST lt OPTIONAL SKID LIMIT TT 3601 EXHAUST TEMPERATURE INLET TO TURBO 509 4954 05570 T 2009 Caterpillar rights reserved CATERPILLAR Engine Governing and Control System Introduction This section and the following section describe the standard Caterpillar GMS control and governor arrangement The standard control system offering is a PLC based control and monitoring system with a relay
21. SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR engine day tank If the return fuel is cooled and not returned to the day tank provisions must be made to have the piping system vented for entrapped air and gasses Fuel Filtration System Primary Fuel Filter Caterpillar recommends the use of a primary filter strainer prior to the engine transfer pump and offers a duplex primary filter 178 micron for this purpose Water Separation Caterpillar also recommends the use of a water and sediment separator in the supply line ahead of the transfer pump and offers a Racor filter water separator for this purpose Miscellaneous Fuel System Considerations Flexible Connections Connections to the engine must be flexible hose and must be located directly at the engine inlet and outlet to accommodate engine motion Fuel Temperature Engines are power set at the factory with 30 C 3 C 86 F 5 F fuel to the engine transfer pump Higher fuel temperatures will reduce fuel stop power capability The fuel stop power reduction is 1 for each 5 6 C 10 F fuel supply temperature increase above 30 C 86 F If the engine is operating below the fuel stop limit the governor will add fuel as required to maintain the required engine speed The Classification societies have a maximum return to tank fuel temperature This temperature is related to the fuel flash point To obtain good fuel filter life the engine fu
22. 1 5 AO Lamm SNILL TY NEO Leg CONV NOILVANNOY LYSNYD GYOVMDVd ec ef nd SZ 133 79 ddv T39WN HI 84 3 0 NYG 23 101 HdINI 110031 0950119 CADNV 14 OLSNSHL dO 3 ALON 9 0 3 9 3 9312 81 49 39v9 286 9 3118 3 1 38 15 SOLVIIGNI 3LDN Hl 22 8 D JNON JIV PACKAGED GENSET FOUNDATION AND MOUNTING amp Js NI 1199 40 719130 53709 2 2 889810 X 3S0H 1 AINOLSNIQ ATEWASSY AOLINOW 0 88 6 1 40 719130 ANON 31925 1291 1914 ISNV 051 5 916 18 3 40 VLC I000000000000 1000000000000 og 40 133H8S TYNOILS0 SS VNAII 3 XION3E 8803 ANON 31925 ONILLI4 LSNYHX3 9912 9918 Lavd 40 YLI 885 1008 Vid 8855 8 1814 LS
23. FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 540 932 501 893 898 508 555 825 745 FROM ENGINE 100 0 M 1110 109 7 106 6 105 8 1073 1050 99 0 910 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1055 1056 560 921 872 852 552 804 FROM ENGINE 0 1154 1129 1042 089 949 949 95 0 882 M 1 5M 117 0 128 9 126 0 116 3 112 4 107 6 108 5 106 6 100 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambi
24. PRIORITY VALVE CENTRIFUGAL OIL FILTER COOLING JET BY PASS VALVE MAIN OIL MANIFOLD 1 i TO SUMP PS MEME 3604 ENGINE SUMP 9 1 p a x gt x ER ES NN MU SR a 3600 ENGINE OIL TEMPERATURE READOUT n me P amp ID LUBRICATION SYSTEM TT 3601 ENGINE OIL TEMPERATURE TRANSMITTER SKID LIMIT L oo LS 3600 ENGINE LOW OIL LEVEL SWITCH 509 4954 oo P L g SKID LIMIT SKID INTEGRATED COLLECTION SUMP a SUMP TANK LUBE OIL HEATER J 5 aE 5 ze E2 o53 55 262 5 amp amp 28 38 a 38 psc 45 523 LEGEND DESCRIPTION 3 5 L3 ES ot 1E2733 DRAWING AUTOCAD 1E0013Y CONFIDENTIALITY 1E0011 INTPR amp TOL ym NIH CHECK VALVE E Caterpillar Confidential Yellow CUSTOM PROD ENGINE MODEL C280 gt UNLESS OTHERWISE SPECIFIED STRAINER DIMENSIONS ARE IN MM snr 1 20 FI TAG NO DESCRIPTION DIMENSIONS W O TOL ARE BASIC 0 10 20 30 3600 ENGINE OIL DIFFERENTIAL PRESSURE READOUT sur 4
25. coe W118 PROCESS LINE CATERPILLAR DESCRIPTION EXHAUST GAS SILENCER moz rn TAG No DESCRIPTION gr SKID LIMIT 3600 INLET AIR MANIFOLD PRESSURE TRANSMITTER MARKETING GUIDE END USER CATE WAVE TE 3600 EXHAUST STACK TEMPERATURE THERMOCOUPLE TT 3600 INLET AR MANIFOLD BOOST TEMPERATURE TRANSMITTER me P amp ID AIR INTAKE EXHAUST OPTIONAL SKID LIMIT TT 3601 EXHAUST TEMPERATURE INLET TO TURBO 309 4954 4 0 AIR SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR Engine Room Ventilation General Although not part of the Caterpillar Scope of Supply for a typical diesel generator package the engine room ventilation system is a vital part of a successful installation The two primary aspects of a properly designed engine room ventilation system addressed in this document are cooling air and combustion air e Cooling Air The flow of air required to carry away the radiated heat of the engine s and other engine room machinery e Combustion Air The flow of air required to burn the fuel in the engine s Both of these have a direct impact on engine or packaged unit performance and must be considered in the design of an engine room ventilation system However it is important to note that all equipment within the engine room space not onl
26. ec ef rn 006043885 ON 1 T 6022 69 1 438 MOST LIMNI 06 51108 91 1561 gt 438 20 0v 40 3 UvIN3S3ud3H SI 5 4 Z lt gt 11 1YWNOILSO 02009 Caterpillar amp rights reserved 9 93 2 Q 930 09 50 o 930 0 5 z 2 93 ox 9 2 2 5 I MAA 3015 LHOk E Sue INO lt E b gt gt d o me ei 5 gt li T 5 gt se d 3 7 E v 180 pu NI 7 ilo ol ec lt M3l 401 S i HM dm b 4 RR N 1 E a p Q 1 eni
27. FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1055 1056 560 921 872 852 552 804 FROM ENGINE 0 1154 1129 1042 089 949 949 95 0 882 M 1 5M 117 0 128 9 126 0 116 3 112 4 107 6 108 5 106 6 100 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 th
28. LOUVERS b a a Outside air is brought into the engine room as far away as practical from heat sources utilizing fans or large intake ducts The air is discharged into the engine room as low as possible as illustrated in Figure 4 Allow air to flow across the engine room from the cool air entry point s toward sources of engine heat such as the engine exposed exhaust components generators or other large sources of heat Ventilation air exhaust fans should be mounted or ducted at the highest point in the engine room Preferably they should be directly over heat sources Engine heat will be dissipated with this system but a certain amount of heat will still radiate and heat up all adjacent engine room surfaces If the air is not properly routed it will rise to the ceiling before it gets to the engines This system will work only where the air inlets circulate the air between the engines for 2 engine applications Air inlets located at the end of the engine room will provide adequate ventilation to only the engine closest to the inlet Ventilation Type 4 Alternate Design If Ventilation Types 1 and 2 are not feasible the following method can be used however it provides the least efficient ventilation and requires approximately 2 5 times the air flow of Ventilation Types 1 and 2 Outside air is brought into the engine room using supply fans and discharged toward the turbocharger air inlets on the engines as illustrated
29. rT 6 6 AINO 03 JAV A18ISSOd ONY ED SIS3HIN3HVd NI NMOHS TINTON SNALSAS LSNYHXA SMINVATO ENTER SONIMVHG NOLIV TIVISNI SM3IA ASWMIXNV NI 1d3OX3 SINN SIELSAS ON 1000 ONIONIONI SKUI 228919 AHL OL LON OG 50 3 A 3294 TVNOLLIGOV 310N INTE NIVLYId 299961 Ze OL INN WnlvQ OL Tad 00 15 66 38 5 344 HOIHM NI MIA Wniva BRE LET V SV SI NNO 0822 AOON 3NION3 ER UNS O1v NMOHS 801 82 39 OL 21512348 CEN AINO JJV 8OIVHJN39 NO SNOISNAWIC 310N 701 110021 8 VIOLIN 9NIMVHO M3 INOY4H 5 38 P RM vy NMOHS 1311 ind JONAINLNID 0 MWA T ICON 3 mmm 43 1 801 Elus 5 19201 ONLI 148201 E 10 10 10 lt 1S3H9IH 2 0 4 TYNOLL td ml Ht N LY 305 Hl S 3NION3 OL ADIYA HIL 3 z N 19201 TYNOLL 31M va IONA OL HINN ALV Z HS 306 H1 TWNO
30. 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 8 Tier 2 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENGY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 284 8277 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 2981 2860 2421 42 7 41 5 100 2710 2600 2201 42 4 41 1 75 2033 1950 1651 39 5 38 3 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 25 C 101 3 kPaa AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSION
31. General The cooling system configuration for the Caterpillar C280 3600 series diesel engine in petroleum offshore applications can be either the separate circuit system or the combined circuit system also referred to as the single circuit two pump system The selection of either of these systems is based on several criteria 1 Applicable emission requirements i e EPA Tier 2 or IMO 2 Petroleum offshore rig site location and available sea water temperature The heat rejection data in this project guide are based on 32 C 90 F water to the aftercooler and 45 C 113 F air to the turbocharger inlet The cooling system is laid out for the following temperature levels 1 32 C 90 F nominal water temperature to the aftercooler and oil cooler IMO allows 38 C 104 F water with 25 C 77 F ambient sea water and EPA Tier 2 requires 32 C 90 F water with 27 C 81 F ambient sea water 2 90 C 194 F nominal jacket water temperature to the cylinder block 93 C thermostatic valve is used for heat recovery applications 3 85 C 185 F nominal oil temperature to bearings Internal Cooling System Fresh Water Pumps The C280 3600 engine has two identical gear driven centrifugal water pumps mounted on the front housing The right hand pump viewed from the flywheel end supplies coolant to the block and heads The left hand pump supplies coolant to the aftercooler and oil cooler External Cooling System Design Co
32. MMS 7W 2118 ENGINE INLET AIR MANIFOLD Stel 5 1 4 20 X gt 310 kPa 0 1000 kPa 2 ANALOG THERMOCOUPLE E ENGINE LUBE OIL Z TEMPERATURE 177 7245 RIE jA DE PR c INLET AIR MANIFOLD TEMPERATURE 177 7245 p suere ENGINE CIRCUIT INLET WATER TEMP 177 RTD x 60C PT100 385 E 7245 2 ENGINE JACKET WATER OUTLET TEMP 177 7245 EE T ae 107 2009 Caterpillar rights reserved Broene MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE Signal Shut Setpoint 2009 Caterpillar All rights reserved Sensor Description Type Alarm Down Trip Comments ENGINE JACKET WATER par eg gt 1030 PT100 385 2ND RTD OUTLET TEMP 177 7245 PER MARINE SOCIETY EXHAUST MANIFOLD TEMP Pee TC x gt 630C EXHAUST MANIFOLD TEMP 12 amp 16 CYL RIGHT 124 4598 16 e 7630C ENGINE ONLY EXHAUST STACK TURBO TEMP LEFT 124 4598 TC X EXHAUST STACK TURBO TYPE 12 8 16 CYL TEMP RIGHT 124 4598 25500 ENGINE ONLY CYLINDER TEMPERATURE Viene ias TC x gt 550C TYPE K CYLINDER TEMPERATURE x gt 550C TYPE K CYLINDER TEMPERATURE x gt 550C TYPE K CYLINDER TEMPERATURE Are x gt 550C TYPE K CYLINDER TEMPERATURE x gt 550C CYLINDER TEMPERATURE GN
33. 5 O Dd OIL TEMP REGULATOR J READO THIRD ANGLE 2 gt PI 3800 LUBE OIL TO FILTER PRESSURE READOUT BALL VALVE NORMALLY OPEN PI 3601 LUBE OIL TO ENGINE PRESSURE READOUT A PS 3602 LUBE OIL LOW PRESSURE SWITCH AT LOW SPEED SHUTDOWN CATERPILLAR BALL VALVE NORMALLY CLOSED PS 3603 LUBE OIL LOW PRESSURE SWITCH AT HIGH SPEED SHUTDOWN PS 3604 CRANKCASE PRESSURE SWITCH OTHERS AND ANY USE EXCEPT THAT FOR WHICH IS LOANED IS PROHIITED FLEXIBLE HOSE 3600 ENGINE OIL PRESSURE TO ENGINE TRANSMITTER MARKETING GUIDE lt OPT 3601 ENGINE OIL PRESSURE TO FILTER TRANSMITTER ME un PROCESS LINE C280 H 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Crankcase Ventilation System Crankcase Emissions Crankcase emissions result from combustion byproducts and or exhaust fumes escaping around the piston rings and into the crankcase commonly called blow by If not controlled this blow by can contaminate the lube oil and pressurize the crankcase possibly leading to an oil leak Venting the emissions to the atmosphere is a simple solution to release the pressure and trapped fumes Managing the emissions however adds complexity to crankcase ventilation systems Vent tubes and crankcase breathers are currently provided on the C280 3600 diesel engine and integral oil sump to allow this gas to escape However as emission laws become more stringen
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35. If the engine combustion air is supplied through a separate dedicated air system the engine room design should consider the following 1 The entire intake system including clean air filters should have an initial restriction of no greater than 122 mm 4 8 HO 2 The maximum inlet restriction with dirty air filters should not exceed 380 mm 15 in H20 3 Flexible connections are necessary to isolate engine vibration from the ducting system Locate the flex connection as close to the engine as possible but be aware of the excessive heat generated by the exhaust system 4 Avoid supporting excessive lengths of ductwork off the turbocharger The maximum allowable moment on the turbocharger is 300 Nm 221 ft lb 5 Caterpillar has specially designed the air intake components to provide the proper airflow pattern before the turbocharger Turbocharger performance may be adversely affected if these components are not used General The amount of combustion air necessary for the C280 3600 Engine is specified in the technical data section of this manual The amount of radiated heat emitted by each engine is also specified Installations intended for operation in extreme cold may require heated air for starting purposes In addition it may be necessary to control the inlet boost pressure for cold air installations Contact your Caterpillar dealer or the regional Caterpillar representative for further information when extr
36. M im 562 1022 1017 1013 OVERALL 63 125 250 500 1000 2000 4000 8000 BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1094 1088 FROM ENGINE 71 11641134 1042 999 950 954 848 902 M 1 5M 118 0 129 4 127 0 116 9 113 4 109 0 110 5 108 1 102 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your Site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 C and 150 m altitude To maintain a constant air inlet manifold temperature as the air to turbo temperature goes up so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 9696 generator power engine power x 0 96
37. ret 1 NL 4 NI 13 SI MODTS31NI 4 4 19915 3 3 043 440 e 14 e sr 4 224 19 135337 340 u 22 er 4 4 A AJ S a Lb E s an IN 311 DIHELIN re NMOGLNHS ANV ONIYOLINOW illar All r Caterp 2009 ENGINE MONITORING AND SHUTDOWN Y 211943 25 110281 ann 301 1 EL Hl 9 I N JUL 3 Sd INT H I7JOINY ONIMYST M i TA 1 v 1 t T M se PRIN E 2 cisco gelbe rebel EN 4 4 P 183 JHL NI 28 828 IYNINSJL 123NND e TNE 5 OL 371083N3 903 49300085 7303 gt D N
38. 0 93 0 91 0 88 0 85 083 080 0 78 10 0 95 0 2 0 89 087 084 082 0 79 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 118 112 120 127 180 134 137 140 144 147 150 1 54 116 119 122 125 128 131 134 1 10 1 13 1 16 1 19 1 22 1 25 1 28 190 100 100 100 102 104 107 10 120 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M FROM ENGINE 7M M 1 Tore 4023 e os 6 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 96 1071 1046 954 91 5 867 872 852 809 7 103 1144 111 4 1022 97 9 93 0 944 828 882 1 5 116 1274 125 0 114 9 111 4 107 0 108 5 106 1 100 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold t
39. 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 1096 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE 15 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water TIMING BASED ON AFM INJECTORS 0 EMMISSION DATA SHOWN ARE NOMINAL VALUES 9 1 10 17 2005 DM5428 05 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 6 Tier 1 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUXILIARY CERTIFICATION IMO EPA MARINE TIER 1 ENGINE SPEED rpm 900 TURBOCHARGER PART 157 5514 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER C 32 RATED ALTITUDE 25 C 150 JACKET WATER OUTLET C 90 ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM EUI A
40. SOO ET FO 51721 06825 SIS3HIN3MVd NI NMOHS SNOISN3MIQ SWILSAS SYINVITO 30 20 NOLLVTIVISNI 5 AMVMIXNV NI 14333 SINNT SMS ON O00 ONION TONI SNE 0 TT hu o EL INYO AHL OL NVINd JON OG S VN 8 33 45 7 310 INTE SNOISNANIG A3HL ss cs p OL 1 0 OL TVA 00 50 Fer SNOISN3NIO SuVaddv og me HOIHM NI Wniva RET 1 SV 0360 SI INC IHL T EQ as a OWN 099 3015 L1H9IM TOWN S DH 55 8 8 55 8 3 NM E T Tor 110031 Qvoolnv 201 WNOIL s ed T OLLWO0T 327 3 Vi 18193713 1 amp AJNI 30 4 1 3 R gt IOILYO0T 131 21 3 NOLLVNI 38 ONY 130 0 2 9 TU 8 5 8 E 1 5888 868 l 4 eV ec 36 y 9 p 5 138 5 5530 3 lt un ISNY Z 3 304 3003 FONYLSIO WAON3 MBlv solos 2 5 710 7 9 0
41. TVOINHOMYHL 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE C280 8 Tier 1 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM 32 90 EUI RATING CERTIFICATION TURBOCHARGER PART FUEL TYPE RATED ALTITUDE 25 ASSUMED GENERATOR EFFICIENCY ASSUMED GENERATOR POWER FACTOR MARINE AUXILIARY IMO EPA MARINE TIER 1 258 2288 DISTILLATE 150 96 0 8 EXHAUST MANIFOLD DRY FIRING PRESSURE MAXIMUM kPa 17300 MEAN PISTON SPEED m s 10 RATING NOTES LOAD 110 ENGINE POWER bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ISO 3046 1 NOMINAL ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION g bkw hr AIR FLOW 25 C 101 3 kPaa Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DAT
42. i 8 i i 63 1 i H PUMP 1560 LPM JW i PUMP T3 965 IMLL E 1 1 1 IT AC OC REG 360 320 JW REG 8 8 I7 40 EXPANSION TANK tt 90 pee OPTIONAL Ja I BYPASS pan p E aH Ve T 52 9 C VALVE 1 1 6 ANSI 1504 6 OPTIONAL 1 FLANGE AC OC HEAT EXCHANGER mo WATER SEAWATER To Rs nr 27C HEAT EXCHANGER SEAWATER Mer fT 2900 69 LPM 1500 LPM Re 00 00 OUTLET FU 6 aj 25 e I FLANGE 4144 1 1 OPTIONAL 120 LPM FUEL COOLER DROP ACROSS HEAT EXCHANGER OPTIONAL FUEL OIL COOLER HEAT REJ H6 33 KW 1 la 8 30 LPM GENERATOR I I MODULE OPTIONAL ACCESSORY MODULE LIMIT OR REMOTE MOUNTED EQUIPMENT eu fame METRIC 1E2733 DRAWING AUTOCAD CONFIDENTIALITY 1 0011 amp TOL Caterpillar Confidential Yellow lt OPTIONAL SKID LIMIT custom PROD X ENGINE MODEL C280 UNLESS OTHERWISE SPECIFIED 1 20 DIMENSIONS ARE IN DIMENSIONS W O TOL ARE BASIC ew erm 2 10 20 TAG 0 DESCRIPTION NOTES LG 3600 WATER LEVEL GAUGE RR ER LIRE someones
43. 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 792 552 847 853 843 823 810 785 FROM ENGINE 7M M im 562 1022 1017 1013 OVERALL 63 125 250 500 1000 2000 4000 8000 BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1086 1057 FROM ENGINE 071 1164 1130 103 7 989 940 950 936 882 M 1 5M 118 0 128 9 127 5 117 3 112 5 108 1 109 5 107 1 101 3 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The tota
44. 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M FROM ENGINE m 1010 M 1M 1072 1087 106 3 104 3 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature
45. For the single turbocharger 6 cylinder engine and the two turbocharger 12 cylinder engine the turbochargers are located at the flywheel end of the engine The turbocharger exhaust outlet is rectangular with an area equivalent to 311 mm 12 in diameter A cast adapter mounts to each turbocharger to provide a 355 mm 14 in diameter customer connection point Optional attachments for these turbochargers include 355 mm 14 in diameter flexible bellows expansion transitions from 355 mm 14 in to 457 mm 18 in diameter 457 mm 18 in diameter bellows and exhaust flanges with bolting and mounting hardware For the single turbocharger 8 cylinder engine and the two turbocharger 16 cylinder engine the turbochargers are located at the flywheel end of the engine The turbocharger exhaust outlet is 355 mm 14 in diameter with cast adaptors mounted to each turbocharger to provide a 457 mm 18 in diameter customer connection point Optional attachments for these turbochargers include 355 mm 14 in diameter flexible bellows 457 mm 18 in diameter bellows and exhaust flanges with bolting and mounting hardware Additionally there is an optional two turbocharger 16 cylinder engine with the turbochargers mounted opposite the flywheel end of the engine for a front mounted turbo engine configuration This engine includes the same cast adaptors and options as the previously mentioned rear mounted turbo engine configuration The exhaust bellows
46. LHS SONIMVEQ NOUVTIVISNI 4831 9 369 x 135 0822 3NION3 OWN 79 7 TOWN 9 BIY DUT 104 MdINI 110021 231 JISLIN HEBS ON 3401512 I3INI 3 101502 3100 A3 003 iva H ANANdIHS 01 801 SLNNON 38 35001 03 41 JAAVA LL Nall 3165 43 3 Lid 34S soe OL qo Legno ISAS 1230 Holds 3HvdS INAYA NN aur Y 016 4 NONE ats 2009 Caterpillar All rights reserved m 45183 86693 0 43 13 31 35v 1 m a ROHS 104 SLM NOL INSWN003 2 dis rs 36 OL v SION
47. e Test Cell Operator Test Conditions e Barometer kPa e Dew Point deg C e Fuel Density degree API Lastly the following temperatures are recorded during load testing at 50 75 100 3 separate recordings at this load and 110 2 separate recordings at this load power e Exhaust Manifold Left e Exhaust Manifold Right e Cylinders 1 through 16 individually or as a function of total cylinder count 6 8 or 12 Buscerraszous 02009 Caterpillar All rights reserved CATERPILLAR Maintenance Interval Schedule Ensure that all safety information warnings and instructions are read and understood before any operation or any maintenance procedures are performed The user is responsible for the performance of maintenance including all adjustments the use of proper lubricants fluids filters and the replacement of components due to normal wear and aging Failure to adhere to proper maintenance intervals and procedures may result in diminished performance of the product and or accelerated wear of components Use mileage fuel consumption service hours or calendar time whichever occurs first in order to determine the maintenance intervals Products that operate in severe operating conditions may require more frequent maintenance Every Service Hour o Trend Data Record Daily Air Starting Motor Lubricator Oil Level Check o Air Tank Moisture and Sediment Drain Cooling System Coolant Level Check
48. 101 3 Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV TO JACKET WATER NOMINAL ATMOSPHERE NOMINAL TO OIL COOLER NOMINAL TO EXH LHV TO 25 C NOMINAL TO EXH LHV TO 177 C NOMINAL TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POW
49. EXHAUST MANIFOLD C280 12 Tier 2 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENCY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 189 4427 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 4466 4287 2418 42 0 40 8 100 4060 3898 2198 42 1 40 9 75 3045 2923 1649 41 1 39 8 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 0 259 101 3 AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW
50. LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 C 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8394 00 Eos DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 6 Tier 2 Technical Data 900 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERAT
51. Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5821 02 TVOINHOMYHL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 12 Tier 1 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM 32 90 EUI RATING CERTIFICATION TURBOCHARGER PART FUEL TYPE RATED ALTITUDE 6 25 C ASSUMED GENERATOR EFFICIENCY 96 ASSUMED GENERATOR POWER FACTOR MARINE AUXILIARY IMO EPA MARINE TIER 1 189 4427 DISTILLATE 150 96 0 8 EXHAUST MANIFOLD DRY FIRING PRESSURE MAXIMUM kPa 17300 MEAN PISTON SPEED m s 10 RATING NOTES LOAD 110 ENGINE POWER bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ISO 3046 1 NOMINAL ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION g bkw hr AIR FLOW 25
52. RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 396 OF FULL LOAD DATA ENGINE POWER TOLERANCE IS 396 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 1 2 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5828 02 Eos DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 16 Tier 1 Technical Data 1000 rpm Sheet 2 of 2 C280 16 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 978 076 074 OM 039 067 055 oss 082 or 075 070 070 6851 os osr 094 oes oss ost
53. 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 40 822 882 877 883 873 553 840 816 FROM ENGINE 7M M 1090 957 1047 1042 104 8 103 5 101 8 100 5 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 an
54. 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD
55. 1 Year o Aftercooler Condensation Drain o Engine Valve Bridge Lash and Injector Fuel Timing Check Adjust o Engine Valve Rotators Inspect o Oil Mist Detector Clean Replace Every 4000 Service Hours or 1 Year o Aftercooler Core Clean Test o Starting Motor Inspect o Water Temperature Regulator Replace Every 8000 Service Hours or 1 Year o Engine Protection Devices Calibrate 02009 Caterpillar amp rights reserved CATERPILLAR Every 8000 Service Hours or 3 Years o Camshaft Roller Followers Inspect Cooling System Coolant DEAC Change Cooling System Coolant Extender ELC Add Crankshaft Vibration Damper Inspect Driven Equipment Check Engine Oil Temperature Regulator Replace Exhaust Shields Inspect Turbocharger Inspect Water Pump Inspect Between 16 000 and 24 000 Service Hours Top End Overhaul O O O O Every 16 000 Service Hours or 6 Years o Cooling System Coolant ELC Change Between 36 000 and 44 000 Service Hours o Major Overhaul ok 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Storage Preservation Specification This specification describes methods and materials used to provide for the preservation of engines as defined in Caterpillar Document No 1 2566 Processing Engine Preservation These procedures are intended for all C2
56. 56 9 Where HRG Heat Radiated by the Generator kW Btu min Generator Output at Maximum Engine Rating ekW Eff Generator Efficiency 100 Example Eff 94 100 0 94 Example A C280 16 4840 ekW generator set has a generator efficiency of 9596 What is the generator radiant heat for this genset Solution P 4840 ekW 95 Efficiency 400 0 95 0 4840 1 0 95 HRG 242 kW HRG 4840 1 0 95 x 56 9 HRG 13 770 Btu min Calculating Required Ventilation Air Flow Engine room ventilation air required for Caterpillar engines and packages can be estimated by the following formula assuming 38 100 F ambient air temperature H V Combustion Air Where V Ventilating Air m min cfm H Heat Radiation i e engine generator aux KW Btu min D Density of Air at 38 C 100 F 1 099 kg m 0 071 Ib ft Cp Specific Heat of Air 0 017 kW x min kg x 0 24 Btu F AT Permissible temperature rise in engine room F Note If duct work is used to bring in air for the engine combustion air the last term the equation can be dropped 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Example A C280 16 4840 ekW genset has the following data Heat rejection 242 kW 13 770 Btu min Temperature rise 11 20 F Solution The estimated engine room v
57. 6 FAULT ALARM RACK 0 GROUP 6 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 7 FAULT ALARM RACK 0 GROUP 7 FAULT ALARM ACKNOWLEDGED RACK 1 GROUP 0 FAULT ALARM RACK 1 GROUP 0 FAULT ALARM ACKNOWLEDGED RACK 1 GROUP 4 FAULT ALARM RACK 1 GROUP 4 FAULT ALARM ACKNOWLEDGED RACK 1 GROUP 6 FAULT ALARM RACK 1 GROUP 6 FAULT ALARM ACKNOWLEDGED LUBE OIL TO ENGINE PRESSURE LOW SHUTDOWN LUBE OIL TO ENGINE PRESSURE LOW SHUTDOWN ACKNOWLEDGED JACKET WATER OUTLET TEMPERATURE HIGH SHUTDOWN JACKET WATER OUTLET TEMPERATURE HIGH SHUTDOWN ACKNOWLEDGED REDUNDANT JACKET WATER OUTLET TEMPERATURE HIGH SHUTDOWN REDUNDANT JACKET WATER OUTLET TEMPERATURE HIGH SHUTDOWN ACKNOWLEDGED ALARM STATUS AUXILIARY 1 TEMPERATURE SHUTDOWN AUXILIARY 1 TEMPERATURE SHUTDOWN ACKNOWLEDGED AUXILIARY 2 TEMPERATURE SHUTDOWN AUXILIARY 2 TEMPERATURE SHUTDOWN ACKNOWLEDGED AUXILIARY 1 4 20 mA SHUTDOWN AUXILIARY 1 4 20 mA SHUTDOWN ACKNOWLEDGED AUXILIARY 2 4 20 mA SHUTDOWN AUXILIARY 2 4 20 mA SHUTDOWN ACKNOWLEDGED NON DRIVE BEARING TEMPERATURE HIGH SHUTDOWN NON DRIVE BEARING TEMPERATURE HIGH SHUTDOWN ACKNOWLEDGED DRIVE BEARING TEMPERATURE HIGH SHUTDOWN DRIVE BEARING TEMPERATURE HIGH SHUTDOWN ACKNOWLEDGED ENGINE OVERSPEED SHUTDOWN ENGINE OVERSPEED SHUTDOWN ACKNOWLEDGED CRANKCASE PRESSURE HIGH SHUTDOWN CRANKCASE PRESSURE HIGH SHUTDOWN ACKNOWLEDGED ALARM STATUS OIL MIST DETECTOR SHUTDOWN OIL MIST DETECTOR SHUTDOWN ACKNOWLEDGED PARTICLE DETECTOR SHUTDOWN PARTICLE DETECTOR SHU
58. 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your Site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 C and 150 m altitude To maintain a constant air inlet manifold temperature as the air to turbo temperature goes up so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 9696 generator power engine power x 0 96 If the actual generator is less than 9696 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5815 02
59. ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 118 112 120 127 180 134 137 140 144 147 150 1 54 116 119 122 125 128 131 134 1 10 1 13 1 16 1 19 1 22 1 25 1 28 190 100 100 108 1 02 104 107 10 120 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M FROM ENGINE 7M 3 5 M 1M Tore 30 3 L 4023 va 94 1 OVERALL 63 125 250 500 1 000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 96 106 6 1037 954 901 857 862 843 7 102 1144 1110 1017 96 9 920 930 916 1 5 116 1269 125 5 115 3 110 5 106 1 107 5 105 1 OVERALL 63 125 250 500 1000 2000 4000 BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude
60. ALARM ACKNOWLEDGED 40263 16 ALARM STATUS 40264 LOW BATTERY VOLTAGE ALARM 40264 01 LOW BATTERY VOLTAGE ALARM ACKNOWLEDGED 40264 02 RELAY POWER NOT AVAILABLE ALARM 40264 03 RELAY POWER NOT AVAILABLE ALARM ACKNOWLEDGED 40264 04 AUXILIARY 1 ALARM 40264 05 AUXILIARY 1 ALARM ACKNOWLEDGED 40264 06 AUXILIARY 2 ALARM 40264 07 AUXILIARY 2 ALARM ACKNOWLEDGED 40264 08 AUXILIARY 3 ALARM 40264 09 AUXILIARY 3 ALARM ACKNOWLEDGED 40264 10 SHUTDOWN OVERRIDE ALARM 40264 11 SHUTDOWN OVERRIDE ALARM ACKNOWLEDGED 40264 12 EXHAUST PORT 1 TEMPERATURE DEVIATION ALARM 40264 13 EXHAUST PORT 1 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40264 14 EXHAUST PORT 2 TEMPERATURE DEVIATION ALARM 40264 15 EXHAUST PORT 2 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40264 16 ALARM STATUS 40265 EXHAUST PORT 3 TEMPERATURE DEVIATION ALARM 40265 01 EXHAUST PORT 3 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 02 EXHAUST PORT 4 TEMPERATURE DEVIATION ALARM 40265 03 EXHAUST PORT 4 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 04 EXHAUST PORT 5 TEMPERATURE DEVIATION ALARM 40265 05 EXHAUST PORT 5 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 06 EXHAUST PORT 6 TEMPERATURE DEVIATION ALARM 40265 07 EXHAUST PORT 6 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 08 EXHAUST PORT 7 TEMPERATURE DEVIATION ALARM 40265 09 EXHAUST PORT 7 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 10 EXHAUST PORT 8 TEMPERATURE DEVIATION ALARM 40265 11 EXHAUST PORT 8 TEMPERATURE DEVIATION ALARM ACKNOWLE
61. CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5809 02 DATA 2009 Caterpillar All rights reserved CATERPILLAR C280 6 Tier 1 Technical Data 900 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS 50 094 091 45 0 95 0 93 40 087 0 94 35 058 096 0 i I i 30 25 20 I j 0 92 089 0 86 0 84 081 0 79 0 76 15 I 0 93 0 91 0 88 0 85 0 83 0 80 0 78 10 095 0 92 0 89 0 87 084 082 0 79 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS
62. CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7 HEAT REJECTION TO AFTERCOOLER TOLERANCE 15 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 9 TIMING BASED ON AFM INJECTORS 10 EMMISSION DATA SHOWN ARE NOMINAL VALUES 5 23 2003 DM5425 02 Eoo TVOINHOMYHL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 3608 Technical Data 900 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 175 6670 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER RATED ALTITUDE 25 200 JACKET WATER OUTLET ASSUMED GENERATOR EF
63. CONSUMPTION ARE BASED ON 35 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5827 02 BErecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 16 Tier 1 Technical Data 900 rpm Sheet 2 of 2 C280 16 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 978 076 074 OM 039 067 055 oss 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50
64. Driven Equipment Inspect Replace Lubricate o Engine Air Cleaner Service Indicator Inspect o Engine Air Precleaner Clean o Engine Oil Level Check Fuel System Primary Filter Water Separator Drain o Fuel Tank Water and Sediment Drain o Instrument Panel Inspect Walk Around Inspection Every Week o Jacket Water Heater Check Every 250 Service Hours Cooling System Coolant Sample Level 1 Obtain Cooling System Supplemental Coolant Additive SCA Test Add Every 250 Service Hours or 6 Weeks Air Shutoff Test o Engine Oil Sample Obtain Oil Mist Detector Check Every 500 Service Hours or 3 Months Engine Mounts Inspect o Engine Protective Devices Check Initial 1000 Service Hours or 6 Months o Engine Valve Bridge Lash and Injector Fuel Timing Check Adjust o Engine Valve Rotators Inspect Bi scosxvrtassin 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Every 1000 Service Hours or 6 Months o Barring Device Lubricate Cooling System Coolant Sample Level 2 Obtain Engine Mounts Check Engine Oil Filter Change Exhaust Piping Inspect Fuel System Primary Filter Water Separator Element Replace Fuel system Secondary Filter Replace Prelube Pump Lubricate Oo O O O o Speed Sensor Clean Inspect Every 2000 Service Hours o Air Starting Motor Lubricator Bowl Clean Every 2000 Service Hours or
65. MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 2783 2662 2512 42 9 41 6 100 2530 2420 2283 43 5 42 2 75 1898 1815 1712 41 0 39 8 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 25 C 101 3 kPaa AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFIN
66. OIL OUTLET 1 11 1 2 762 688 COOLANT PUMP SWITCH Box LUBE OIL INLET L JACKET WATER 1 1 2 11 1 2 Prelubrication Pump ELECTRICAL DATA PUMP DATA 3 PHASE CAPACITY 30 GPM 400 VOLT LIQUID SAE40 LUBE DIL 3 HP 4 AMP 1 1 LOAD MiSCHSITY ESI SS 15000 SSU en et 95 25 95 25 15 74 197 L 8737 406 DIA 4 HOLES Fuel Pre Filter lt Weight ca 130kg e Es gt 2 1450 O G un 157 2009 Caterpillar rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Reference Material The following information is provided as additional reference to subjects discussed in this guide LEBW4985 C280 Commissioning Guide SENR3593 Systems Operation Testing and Adjusting 3612 and 3616 Engines SEBU6965 Operation and Maintenance Manual 3600 Distillate Fuel Engines SEBU7003 3600 Series and C280 Series Diesel Engine Fluids Recommendations 1E2566L Processing Engine Preservation MATERIAL 2009 Caterpillar All rights reserved CATERPILLAR LEBW0006 00 2009 Caterpillar Printed in U S A All rights reserved CAT CATERPILLAR their respective logos ADEM S O S Caterpillar Yellow and the Power Edge trade dress as well as
67. OL T3TIVuvd 38V SNOISN3WIQ Suv3ddv HOIHM NI MAIA 3HL 303 Wniva WV3NI v SV 035 SI INN JHL 1004 101 INI 3 SNIWV 3 FOOL 19201244 117907 30 5 31 3807 SOLANA rved right erpilla Cat 30H 13131 2 e z z T un gt x 00 QI 31 3 d 4 4338 13 491051 33 19201 31 3 ONILNOOW ANV NOLLVANNOY LASNAS AYDVMOV dg 5 rese 2009 CATERPILLAR 1 1 CONNECTION DATA SHEET RIGHT HAND SERVICE ITEM CONNECTION DIMENSIONS OTHER DESCRIPTION SPECIFICATIONS 01 02 03 DETAIL WATER CIRCUIT INLET DETAIL ON 302 6302 SHEET 7 6887 PARTNER FLANGE 6 ANSI FLANGE PROVIDED WATER CIRCUIT DETAIL ON 302 6302 SHEET 7 6887 PARTNER FLANGE OUTLET 6 ANSI FLANGE PROVIDED JACKET WATER DRAIN 3 4 14 NPTF 6658 PARTNER FLANGE Ei ACCESSORY MODULE NOT NEEDED lt SCAC WATER DRAIN 3 4 14 NPTF 6673 PARTNER FLANGE ACCESSORY MODULE NOT NEEDED WATERMAKER INLET DETAIL
68. RIGHT SPEED SENSOR FAILURE ALARM TURBINE RIGHT SPEED SENSOR FAILURE ALARM ACKNOWLEDGED ENGINE SPEED SENSOR FAILURE ALARM ENGINE SPEED SENSOR FAILURE ALARM ACKNOWLEDGED BALL HEAD BACKUP MODE SENSOR FAILURE ALARM BALL HEAD BACKUP MODE SENSOR FAILURE ALARM ACKNOWLEDGED 2009 Caterpillar All rights reserved MODBUS ADDRESS 40254 40254 01 40254 02 40254 03 40254 04 40254 05 40254 06 40254 07 40254 08 40254 09 40254 10 40254 11 40254 12 40254 13 40254 14 40254 15 40254 16 40255 40255 01 40255 02 40255 03 40255 04 40255 05 40255 06 40255 07 40255 08 40255 09 40255 10 40255 11 40255 12 40255 13 40255 14 40255 15 40255 16 40256 40256 01 40256 02 40256 03 40256 04 40256 05 40256 06 40256 07 40256 08 40256 09 40256 10 40256 11 40256 12 40256 13 40256 14 40256 15 40256 16 ANV ONIYOLINOW ANIONGA Broene MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA ALARM STATUS CRANKCASE PRESSURE SENSOR FAILURE ALARM CRANKCASE PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED OIL MIST DETECTOR SENSOR FAILURE ALARM OIL MIST DETECTOR SENSOR FAILURE ALARM ACKNOWLEDGED LOW SPEED LOW OIL PRESSURE SENSOR FAILURE ALARM LOW SPEED LOW OIL PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED HIGH SPEED LOW OIL PRESSURE SENSOR FAILURE ALARM HIGH SPEED LOW OIL PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED LUBE OIL TO ENGINE TEMPERATURE HIGH ALARM LUBE OIL TO ENGINE TEMPERATUR
69. SHIPPING WEIGHT 37 6 kg TURBOCHARGER SHIPPING WEIGHT 775 0 kg Buiscerraszous 02009 Caterpillar All rights reserved CATERPILLAR C280 3600 Witness Test Description Caterpillar C280 3600 engines have an option for Witness Testing to be conducted in the Lafayette Package test cells No customers or dealer personnel are allowed in the test cell while the engines are running and no customer instrumentation may be connected to the engines packages or test cell data acquisition and reporting systems Standard testing includes a load test transient response test and vibration test described as follows 1 The load test uses 0 8 PF unless otherwise noted and is recorded at 30 minute intervals 30 minutes 50 rated load 30 minutes 75 rated load e 120 minutes 100 rated load e 60 minutes 110 rated load 1 0 PF The cylinder and exhaust temperatures are manually recorded All other data is recorded electronically and printed by computer The transient response test is performed at 0 8 PF with load stepping from 0 to 100 ekW with pre determined intervals depending on engine frequency then back to 0 with examples as follows e For 900 rpm 60 Hz C280 16 or 3616 engines o 0 1700 ekW 2880 ekW 3840 ekW 100 0 e For 1000 rpm 50 Hz C280 16 or 3616 engines 0 1900 ekW 3210 ekW 4275 ekW 100 0 2 The vibration test is taken at 0 100 load and printed by
70. SPARE 40180 WRITE SPARE 40181 WRITE SPARE 40182 WRITE SPARE 40183 WRITE SPARE 40184 WRITE SPARE 40185 WRITE SPARE 40186 WRITE SPARE 40187 WRITE SPARE 40188 WRITE SPARE 40189 WRITE SPARE 40190 WRITE SPARE 40191 WRITE SPARE 40192 WRITE SPARE 40193 WRITE SPARE 40194 WRITE SPARE 40195 WRITE SPARE 40196 WRITE SPARE 40197 WRITE SPARE 40198 WRITE SPARE 40199 WRITE SPARE 40200 Broene MONITORING AND SHUTDOWN 2009 Caterpillar rights reserved ANALOG DATA PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 VOLTAGE PM3000 CURRENT PM3000 CURRENT PM3000 CURRENT PM3000 POWER PM3000 POWER PM3000 POWER PM3000 POWER PM3000 POWER PM3000 POWER PM3000 POWER FACTOR PM3000 POWER FACTOR PM3000 FREQUENCY PM3000 FREQUENCY WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE WRITE SPARE CATERPILLAR 2009 Caterpillar All rights reserved MODBUS ADDRESS 40201 40202 40203 40204 40205 40206 40207 40208 40209 40210 40211 40212 40213 40214 40215 40216 40217 40218 40219 40220 40221 40222 40223 40224 40225 40226 40227 40228 4
71. To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekW listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 4 12 2006 DM5809 02 e a 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 6 Tier 1 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUXILIARY CERTIFICATION IMO EPA MARINE TIER 1 ENGINE SPEED rpm TURBOCHARGER PART 189 4427 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER C 32 RATED ALTITUDE 25 C 150 JACKET WATER OUTLET C 90 ASSUMED GENERATOR EFFICIENCY 96 IGN
72. Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 1 19 2007 DM8417 00 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Lubrication Oil System General The
73. a thin film of mixture of 50 1 E2359 VCI Oil and 50 engine oil on the flywheel ring gear and starter pinion To seal in vapors install the covers specified on engineering drawings for the flywheel housing and starter opening and the plugs specified for through holes Apply a heavy coating of 1 E0325 Grease to the bearing surfaces of all pin and joint connections and other non painted surfaces All tapped holes must be protected by painting or by applying MS2254 Coating or equivalent Tapped holes shall be free of water before applying MS2254 Coating or equivalent and sealed with a tightly fit plastic plug or equivalent saosasvaqaosiw 02009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Typical Supplied Auxiliary Equipment Thermostatic Valve 26 on th th Y mI L NOTE DN 125 5 Flanges drilled to DIN 2501 Incl manual override 254 Valve JW Thermostatic Valve p lada J 254 Incl manual override JW Valve Lube Cil Thermostatic Valve CH NOTE i Lube Dil Valve No manuel override Flanges drilled to DIN 2501 225 02009 Caterpillar amp rights reserved CATERPILLAR Jacket Water Lube Oil Combination Heater COOLANT OUTLET 1 11 1 2 NPTF
74. amp rights reserved s reserved ight E ILYWJH S LINIAN 0017 00 oTt AS ONISULINOA SRAZSRO 307 3m 41 2 41 5 94 v QNI uvT LHI a s N y m 3 4 133 1 t 4 435 v4 aentiv4 VIF 1 TT TF uam L ve 1 o 1 1HOIT SS3 1 1 1 110 T 2519 1 he 101 TSI Av 138 6201 171 HOSNI EG do 4 SN11391 X SOS e 39017384 V 31v3H 319 13909 l 3 a 224 z eG E E NS 1350 SI 83 JADRA 38r gt 10 100 14 e gt TaN 9 Te
75. and thus restricting the discharge of fumes Where horizontal runs are required install the pipe with a gradual rise of 41 7 mm m 0 5 in ft slope from the engine The weight of the vent pipes will require separate off engine supports as part of the installation design Further additional flexible connections will need to be installed to accommodate the engine movement The pipe should vent directly into the atmosphere at a well considered location and be fitted with a gooseneck or similar arrangement to keep rain or water spray from entering the engine Consideration should also be given to other equipment located near the discharge area If not located properly the oil carryover can accumulate over time and become unsightly An oil condensate trap as shown on the following drawing will minimize the amount of oil discharged from the vent pipe VENTILATION SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR The crankcase pressure should not vary more than 25 4 mm H20 1 0 in of water from ambient barometric pressure Measurement should be made at the engine dipstick location with the engine at operating temperature and minimum at 80 to 90 percent of rated load Customer Piping Connections Rubber boot for 60 3 mm 2 375 in O D Tubing In line engines require 1 boot and vee engines require 2 Bess NOLLVILLNYA X1SVOMNVHO 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE
76. and to fulfill society requirements The engine safety system is operationally independent from the monitoring system That means the engine will shut down for the safety functions high crankcase pressure overspeed and low lubrication pressure even when the PLC is not operational Engine Monitoring Engine monitoring switches and analog sensors 4 20 mA transmitters RTD s switches and thermocouples can vary from one installation to the next Pressure Sensors The engine is installed with a sensor package in accordance with the sensor list enclosed The pressure sensors are generally mounted on a common panel on either the front or side of the engine Temperature Sensors The exhaust temperature sensors are thermocouples and the remaining sensors are RTD s PT100 Engine Control Panel The Engine Control Panel contains the PLC start stop logic and man machine interface MMI touch screen for displaying the operating parameters The operator is able to view engine parameters from different screens for each system exhaust water and air on the engine The various screens are called to view by buttons located at the bottom of each screen All the engine parameters are further available to the vessel control system via P C communications The monitoring and alarm functions listed in the instrumentation list overleaf are typical for a C280 3600 Marine engine supply Marine Classification Society with notation Unmanned Machinery S
77. based backup safety shutdown system The system is capable of communicating with the vessel main control system through various communication protocols Generator Engine Governing System C280 ADEM III Optional Direct Rack PLC required Note Direct Rack is mutually exclusive with the load sharing module 3600 e Woodward e Heinzmann TOULNOD 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Done GOVERNING AND CONTROL SYSTEM 02009 Caterpillar rights reserved CATERPILLAR Engine Monitoring and Shutdown Engine Shutdown 280 3600 engine is installed with shutdown protection for overspeed low lubrication oil pressure high crankcase pressure high jacket water temperature and Metal Particle Detection High oil mist level alarm and or shutdown are available as an option to satisfy marine societies which typically require this feature on engines above 2250 bkW In addition the engine can be shutdown through the electrical control system via emergency shutdown buttons installed as required by the Marine Classification Society on the bridge and the engine control panel For the shutdowns the engine is stopped via the shutdown solenoid in the governor However in case of an overspeed or activated emergency stop button the engine will be stopped by an emergency air shutoff system Both of these measures are taken as a precaution
78. corporate and product identity used herein are trademarks of Caterpillar and may not be used without permission
79. e Generator Lube Module GLM for Kato Generators e For generators supplied by others generator manufacturer is responsible for providing any forced lubrication system that may be required for their generator to meet tilt requirements Starting System The Starting System is an indirect air starting system Included Components e Dual Starting Motors TDI Options e Pressure Reducing Valve Control System The control system uses a single Caterpillar ADEM A3 Electronic Engine Control Modules with Electronic Unit Injection Fuel System 2009 rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Included Components Rigid Wiring Harness Options Direct Rack Module available for C280 engines Protection System The protection system is a PLC programmable logic controller based system that provides protection monitoring and control housed a NEMA 4 66 enclosure All critical shutdowns have both relay and PLC based protection Sensors are factory wired directly to an engine mounted terminal box for a ship loose package or an engine only selection Sensors are wired directly to the control panel when an accessory module is ordered and is factory packaged otherwise control panel is shipped loose for customer mounting Use of PLC eliminates the need for a separate gauge panel and annunciator panel Features 254 mm 10 0 in color monitor to display all engine parameters and a
80. g bkw hr g bkw hr EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY DATA FUEL INPUT ENERGY LHV TO JACKET WATER NOMINAL ATMOSPHERE NOMINAL TO OIL COOLER NOMINAL TO EXH LHV TO 25 C NOMINAL TO EXH LHV TO 177 C NOMINAL TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 H
81. hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treate
82. i i RELIEF VALVE PRIMING i i FUEL PUMP PUMP i i i i i OPTIONAL i FUEL COOLER 2 ANSI 150 i i FLANGE i 1 FRESHWATER i i i FRESHWATER i j OUTLET i iz ANSI 150 FUEL FLANGE i SOLENOID HREFER TO COOLING i OPTIONAL SYSTEM DIG i i i 11 2 ANSI 150 1 1 2 ANSI 57 EEE SKID ______ NE an 4 DRAWING AUTOCAD CONFIDENTIALITY amp TOL Caterpillar Confidential Yellow DUPLEX FILTER CUSTOM PROD X ENGINE MODEL C280 ELT DUPLEX rs lt E SPECIFIED SCALE 1 O PUNP TAG NO DESCRIPTION LEGEND DESCRIPTION Tr TOL ARE BASIC 0 10 20 30 THIRD ANGLE PROJECTIO DWG CONTROL NIH CHECK VALVE FPDI 3600 FUEL FILTER DIFFERENTIAL PRESSURE READOUT FPI 3600 FUEL FILTER PRESSURE READOUT CATERPILLAR pw FLEXIBLE HOSE gt FPI 3801 FUEL UNFILTER PRESSURE READOUT 2 ELECTRICAL LINE FPT 3600 FILTERED FUEL PRESSURE TRANSMITTER ET MARKETING GUIDE 2 FPT 3601 UNFILTERED FUEL PRESSURE TRANSMITTER E o PROCESS LINE FTI 3600 FUEL TEMPERATURE READOUT me FUELING SYSTEM E SKID LIMIT FIT 3600 FUEL TEMPERATURE TRANSMITTER 309 4954 oD 5 D 02009 Caterpillar All rights reserved CATERPILLAR Cooling System
83. in Figure 5 Ventilation exhaust fans should be mounted or ducted from the corners of the engine room Bose WOOU ANION 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Ventilation Type 4 This system mixes the hottest air in the engine room with the incoming cool air raising the temperature of all air in the engine room It also interferes with the natural convection flow of hot air rising to exhaust fans Engine rooms can be ventilated this way but it requires extra large capacity ventilating fans Multiple Engine 3 Applications Multiple engine applications involving three or more engines or packaged units will generally require larger engine rooms than those needed for 1 and 2 engine applications In general the recommended ventilation systems outlined for 1 and 2 engine applications also apply to multiple engine applications However there are several additional considerations that are specific to multiple engines As previously mentioned the application of normal temperature rise guidelines for determining large multiple engine site ventilation requirements will generally result in extremely large volumes of air Therefore the guidelines used for these sites are significantly more generous however even with the increased temperature rise allowed the ventilation requirements will be significant Large multiple engine sites will generally utilize multiple ventilation fans often us
84. lube system is designed to provide constant supply of filtered oil at 430 kPa pressure under all engine operating conditions The major feature of the C280 3600 lube system is the priority valve shown in Figure 1 to regulate the oil pressure at the cylinder block main oil gallery rather than at the oil pump The oil gallery pressure thus becomes independent of the oil filter and oil cooler pressure drops Internal Lubrication System Oil Coolers The engines are equipped with a two element lube oil cooler with the water flow arranged in series three element lube oil cooler is available on vee engines to ensure proper cooling in high ambient conditions Thermostats Four thermostats in the lube system control the oil inlet temperature to 85 185 Oil Filters oil pan is equipped with 650 micron suction screen The duplex final 20 micron lube oil filters can be changed while the engine is operating The normal procedure specifies the filters to be changed at 100 kPa 14 5 psi pressure drop across the filters Centrifugal Bypass Filters Engine mounted centrifugal bypass oil filters are installed as standard The filters receive 3 to 4 percent of the oil pump flow and remove solid micron size particles and can extend the oil filter change periods The centrifugal filters each have dirt capacity of 3 6 kg 8 15 Typical cleaning intervals are outlined in the Maintenance Interval Schedule section of this guide and di
85. min 0 105 7 211 3 317 422 6 528 3 634 739 6 Operating Pump Rise kPa Pump Rise in Hg 0 0 400 800 1200 1600 2000 2400 2800 Fresh Water Flow L min 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Jacket Water and AC OC Pump C280 12 16 and 3612 16 Engines Fresh Water Flow in US Gal min 320 280 o Operating Pump Rise kPa 3 Pump Rise in Hg Operating Line 350 0 400 1200 2000 2800 3600 Fresh Water Flow L min Heat Recovery Water Maker For engines with a Combined Circuit Cooling System heat recovery connections are available for the customer to route Jacket Water or High Temperature Circuit water from the outlet of the engine block to water maker heat exchanger and then return the water to an inlet on the combined circuit mix box temperature regulator on the engine For engines with Separate Circuit Cooling System heat recovery connections are not required as the Jacket Water or High Temperature Circuit is already isolated For both types of cooling systems Caterpillar is able to provide complete cooling system to include water maker heat exchanger heat recovery circuit temperature regulator and required piping to meet the customer s project specific needs Generator Cooling Generators can be furn
86. or Latest Emission Technology the C280 EPA Marine Tier 2 engine is the engine of choice providing ECM software design to electronically control fuel injection to meet EPA Tier 2 emission requirements Specific rig cooling system requirements for each of these engines are detailed in the Cooling System section of this guide Engine Selection Table Customer Requirements rdp C280 IMO 3600 IMO EPA Marine Tier 2 yx Latest Emissions Technology Y Latest Engine Technology Better Fuel Consumption Lowest Installation Cost Engine and Generator Set Ratings For offshore drilling rigs Caterpillar provides Prime engine ratings designed for 6096 Load Factor and 6 000 operating hours per year These ratings have an additional 10 overload capability for one hour of operation over a 12 hour period Generators supplied by Caterpillar are rated for continuous operation This type of package allows the generator set to be operated above the 60 load factor for extended periods of time due to weather related situations with only a minor reduction in Time Before Overhaul hours For other applications site load requirements and number of operating hours should be reviewed with a Caterpillar dealer to determine the best product and rating fit for the application o 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Basic C280 3600 Diesel Engine Design The C280 3600 E
87. pressure lines are not used A 100 micron edge type filter is built into each unit injector External Fuel System Design Considerations Diesel fuel supply systems must ensure a continuous and clean supply of fuel to the engine fuel system The external fuel system typically has three major components a fuel storage system a fuel transfer system and fuel filtration system and each of these systems demand careful attention to ensure the success of each installation Fuel Storage System Tank Location The tanks should not exceed the height of the engine fuel injectors in order to prevent possible leakage of fuel into the cylinders If a higher position is unavoidable then an auxiliary fuel tank or head limiting tank may be required Otherwise check valves with backpressures set to the fuel column height must be installed Caterpillar fuel transfer pumps lifting capability is equivalent to 40 kPa 6 psi inlet restriction Fuel Transfer System Line Restriction The piping carrying fuel to the fuel transfer pump and the return line carrying excess fuel to the tank should be no smaller than the engine connections The maximum inlet flow restriction is 20 kPa 3 psi at rated speed Air in the system causes hard starting erratic engine operation and will erode injectors Return Line The return line should enter the top of the tank without shutoff valves Bypass return fuel leaving the engine pressure regulator should be returned to the
88. required for C280 3600 series engines and several types of automatic prelubrication systems are available from Caterpillar These automatic prelubrication systems include starting controls electric or air powered pumps a check valve and engine piping The prelube pumps whether electric or air powered must be powered from a source independent of any single failure that could prohibit the engine from starting A check valve is used to prevent pressurized oil from flowing through the prelube pump during engine operation Automatic prelubrication systems available for Caterpillar C280 3600 diesel engines are e Redundant Prelube System recommended system e Intermittent Prelube System e Continuous Prelube System Redundant Prelube System recommended system The redundant prelube system combines electric continuous and pneumatic intermittent prelube systems offering the benefits of both Under normal circumstances the electric continuous prelube pump keeps the engine ready for immediate start up but if the electric continuous pump should fail the pneumatic intermittent prelube pump will operate This system is typically selected for dynamic positioning rig applications DP2 and DP3 when it is critical that an engine is able to start Intermittent Prelube System The pneumatic intermittent prelube system uses an engine mounted pump that is engaged immediately prior to engine start up providing suitable performance for applications not req
89. rights reserved Air Tank Sizing for Engines with 2 TDI T109 Starters assuming 5 seconds start 620 kPa 2 e z z T un gt 00 QI O00 v v m glu Jue INW LSAS HIV 5 CATERPILLAR Air Tank Sizing for 3600 Engines with 1 Vane Starter Initall Tank ire kPa Time Start In Line Engine Air Storage Tank Volume m3 Final Tank Pr Number of Available Starts ULV 5 2009 Caterpillar rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Air Tank Sizing for 3600 Engines with 2 Vane Starters Initail Tank ressure Vee REngine Air Storage Tank Volume m3 Number of Available Starts Engine Piping Connections Vane and turbine type starters must be supplied with clean air Deposits of oil water mixture must be removed by traps installed in the lines Lines should slope towards the traps and away from the engine The air supply pipes should be short with number of elbows kept to a minimum and at least equal in size to the engine inlet connection w
90. section is insulated with a soft wrap insulation to comply with marine society rules for surface temperature The top covers of the three aftercooler sections are provided with a screen for protection and insulation The flexible bellow joints are connected by means of V shaped clamps and the use of metallic C rings The maximum inlet air temperature to the turbocharger is 49 C 120 F This temperature is in accordance with the marine society rules for equipment performance and will provide good engine component life For temperatures above 30 C 86 F the engine may be derated to a power output level that will provide for safe engine operation check with Caterpillar A amp I Engineering The C280 3600 Engine will normally draw engine combustion air in one of two ways 1 The engine room is supplied with filtered air for engine combustion as well as for removal of radiated heat from the engine room 2 The engine room is supplied with ventilation air for engine heat removal and the engine combustion air is supplied separately through a dedicated air intake system which provides filtered air for the combustion only Either system should be designed to provide sufficient clean air for combustion and heat removal based on the ambient conditions and the maximum ratings for each piece of installed equipment i e marine auxiliary engines pumps and switchgear For classed vessels the specific societies have well defined rules for the design p
91. within 8 5 to 12 5 C 15 to 22 5 F above the ambient air temperature ambient air temperature refers to the air temperature surrounding the power plant vessel etc Maximum engine room temperatures should not exceed 49 C 120 F If they do then outside air should be ducted directly to the engine air cleaners The primary reason for cooling an engine room is to protect various components from excessive temperatures Items that require cool air are e Electrical and electronic components Air cleaner inlets e Torsional dampers e Generators or other driven equipment e Engine room for the engine operator or service personnel In larger multiple engine sites the normal 8 5 to 12 5 C 15 to 22 5 F temperature rise guidelines for engine rooms may require unobtainable or uncomfortable air velocities For these larger sites a ventilation system that gives priority to the five items listed above and provides a bottom to top air flow can be designed for a temperature rise of 17 C 30 F ROOM VENTILATION 2009 Caterpillar All rights reserved CATERPILLAR Radiant Heat Engine Radiant Heat Engine generated heat must be taken into consideration This information can be found on the Engine Technical Data Sheets Generator Radiant Heat For generator set installations the heat radiated by the generator can be estimated by the following formulas _ 1 es 11 HRG Btu min P x EFF 1 x
92. 0 PISTON AND ROD R D FILTER REMOVAL DISTANCE 1980 78 1980 78 REDUCED HEIGHT LINEAR 8 0 HEAD R D 1587 mm 62 5 i LUBE OIL 407 mm CENTRIFUGAL 16 in FILTER REMOVAL DISTANCE 4186 mm 1648 ind CRANKCASE ACCESS ENVELOPE 2113 mm 83 in 2073 mm 81 6 in Buiscerraszous 02009 Caterpillar All rights reserved CATERPILLAR STANCES R D TYPICAL REMOVAL D 02 FLYWHEEL R D 9 3612 5 2 5 PISTON AND ROD R D CYLINDER 3 LINER RD HEAD RD amp 8 N N IO 3 DISTANCES ARE TO THE CENTER OF LIFTING EYES LUBE OIL 10 FILTER R D Y 1899 74 81 1 LINER RD 5 1876 73 81 2 CYLINDER HEAD R D H H 1844 72 6 PISTON AND gt R D R D CRANKCASE ACCESS CRANKCASE ACCESS ENVELOPE ENVELOPE 5 i Q DISTANCE BETWEEN ENGINE CENTERLINES FOR MIMIMAL SERVICE ACCESS IS 2500MM 02 0 2009 Caterpillar All rights reserved C280 PET
93. 00 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 40 822 882 877 883 873 553 840 816 FROM ENGINE 7M M 1090 957 1047 1042 104 8 103 5 101 8 100 5 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes s
94. 0229 40230 40231 40232 40233 40234 40235 40236 40237 40238 40239 40240 40241 40242 40243 40244 40245 40246 40247 40248 40249 40250 ANV ONIYOLINOW ANIONGA C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA MODBUS ADDRESS ALARM STATUS 40251 LUBE OIL TO ENGINE TEMPERATURE SENSOR FAILURE ALARM 40251 01 LUBE OIL TO ENGINE TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 02 LUBE OIL TO ENGINE PRESSURE SENSOR FAILURE ALARM 40251 03 LUBE OIL TO ENGINE PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 04 LUBE OIL TO FILTER PRESSURE SENSOR FAILURE ALARM 40251 05 LUBE OIL TO FILTER PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 06 INLET AIR MANIFOLD TEMPERATURE SENSOR FAILURE ALARM 40251 07 INLET AIR MANIFOLD TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 08 INLET AIR MANIFOLD PRESSURE SENSOR FAILURE ALARM 40251 09 INLET AIR MANIFOLD PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 10 FUEL TO ENGINE TEMPERATURE SENSOR FAILURE ALARM 40251 11 FUEL TO ENGINE TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 12 FUEL TO ENGINE PRESSURE SENSOR FAILURE ALARM 40251 13 FUEL TO ENGINE PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 14 FUEL TO FILTER PRESSURE SENSOR FAILURE ALARM 40251 15 FUEL TO FILTER PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40251 16 ALARM STATUS 40252 JACKET WATER OUTLET TEMPERATURE SENSOR FAILURE ALARM 40252 01 JACKET WATER OUTLET TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 02 R
95. 110 2009 Caterpillar All rights reserved CATERPILLAR Sensor Description Signal Type Alarm Shut Down Setpoint Trip Comments CYLINDER 2 TEMPERATURE DEVIATION FROM AVG BIT gt 50C CYLINDER 3 TEMPERATURE DEVIATION FROM AVG BIT gt 50C CYLINDER 4 TEMPERATURE DEVIATION FROM AVG BIT gt 50C CYLINDER 5 TEMPERATURE DEVIATION FROM AVG BIT gt 50C CYLINDER 6 TEMPERATURE DEVIATION FROM AVG BIT gt 50C CYLINDER 7 TEMPERATURE DEVIATION FROM AVG BIT gt 50C 8 12 amp 16 CYL ENGINE ONLY CYLINDER 8 TEMPERATURE DEVIATION FROM AVG CYLINDER 9 TEMPERATURE DEVIATION FROM AVG BIT BIT gt 50C gt 50 8 12 amp 16 CYL ENGINE ONLY 12 amp 16 CYL ENGINE ONLY CYLINDER 10 TEMPERATURE DEVIATION FROM AVG BIT gt 50 12 16 CYL ENGINE ONLY CYLINDER 11 TEMPERATURE DEVIATION FROM AVG BIT gt 50C 12 amp 16 CYL ENGINE ONLY CYLINDER 12 TEMPERATURE DEVIATION FROM AVG CYLINDER 13 TEMPERATURE DEVIATION FROM AVG BIT BIT gt 50C gt 50 12 16 CYL ENGINE ONLY 16 CYL ENGINE ONLY CYLINDER 14 TEMPERATURE DEVIATION FROM AVG BIT gt 50C 16 CYL ENGINE ONLY CYLINDER 15 TEMPERATURE DEVIATION FROM AVG BIT gt 50 16 CYL ENGINE ONLY CYLINDER 16 TEMPERATURE DEVIATION FROM AVG BIT gt 50 16 CYL E
96. 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 877 846 858 841 853 819 770 699 FROM ENGINE 957 506 898 901 813 87 0 830 750 M im 1047 1016 100 8 101 1 1023 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 107 1046 FROM ENGINE 7M 103 0 1144 1114 1022 M 1 5M 116 0 127 4 125 0 114 9 111 4 107 0 108 5 106 1 100 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your Site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 C and 150 m altitude To maintain a constant air inlet manifold temperature as the air to turbo temperature goes up so must the heat rejection As altitude increa
97. 277 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 5962 5720 2421 44 7 43 4 100 5420 5200 2201 44 1 42 8 75 4065 3900 1651 41 6 40 3 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 0 259 101 3 AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOL
98. 3 SPARE 40301 14 SPARE 40301 15 SPARE 40301 16 ANV ONIYOLINOW ANIONGA 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA MODBUS ADDRESS READ SPARE 40302 READ SPARE 40303 READ SPARE 40304 READ SPARE 40305 READ SPARE 40306 READ SPARE 40307 READ SPARE 40308 READ SPARE 40309 READ SPARE 40310 READ SPARE 40311 READ SPARE 40312 READ SPARE 40313 READ SPARE 40314 READ SPARE 40315 READ SPARE 40316 READ SPARE 40317 READ SPARE 40318 READ SPARE 40319 READ SPARE 40320 READ SPARE 40321 READ SPARE 40322 READ SPARE 40323 READ SPARE 40324 READ SPARE 40325 READ SPARE 40326 READ SPARE 40327 READ SPARE 40328 READ SPARE 40329 READ SPARE 40330 READ SPARE 40331 READ SPARE 40332 READ SPARE 40333 READ SPARE 40334 READ SPARE 40335 READ SPARE 40336 READ SPARE 40337 READ SPARE 40338 READ SPARE 40339 READ SPARE 40340 READ SPARE 40341 READ SPARE 40342 READ SPARE 40343 READ SPARE 40344 READ SPARE 40345 READ SPARE 40346 READ SPARE 40347 READ SPARE 40348 READ SPARE 40349 READ SPARE 40350 Broene MONITORING AND SHUTDOWN 2009 Caterpillar All rights reserved CATERPILLAR Packaged Genset Foundation and Mounting Foundation Design This section deals with packaged generator set foundations and their relationship to platform framing Exact analytical methods cannot always be used to design foundations The design is also influenced by several factors in
99. 3601 COOLANT TEMPERATURE GAUGE CATERPILLAR INC S 3604 JACKET WATER TEMPERATURE SWITCH ALARM EE S 3605 JACKET WATER TEMPERATURE SWITCH SHUTDOWN INSTALLATION DRAWINGS 3602 JACKET WATER OUTLET TEMPERATURE TRANSMITTER P amp ID COOLING SYSTEM 3603 AC OC INLET TEMPERATURE TRANSMITTER E280 GUIDH Es D 02009 Caterpillar amp All rights reserved CATERPILLAR C280 16 SEPARATE CIRCUIT COOLING SYSTEM 5060 BKW amp 900 RPM mme EE OIL COOLER i 4245 HEAT REJ H4 511 KW OPTIONAL TEMP RISE t4 105 i i 1 VENT BLOCK amp HEAD GENERATOR i MIX HEAT REJ H4 511 KW HEAT REJ H3 1029 KW INLET AR RSE Oye TEMP RISE 1056 1 TURBO 6 250 i 270 i I 360 LPM SEWER 03 SEAWATER INLET OUTLET 2630 LPM I 05 750 LPM AFTERCOOLER 665 __ __ __ i i w HEAT REC H5 1457 i 5 64 20 RISE 32 20 Se gt oe I e
100. 396 No 1 and No 2 Fuel Oils No 1 GT and No 2 GT ASTM D2680 Gas Turbine Fuels Classes A1 A2 and B2 British 59 4907 Engine Fuels BS 2869 Classes C2 and D Burner Fuels DIN 51601 Diesel Fuel DIN 51603 Heating Oil Australian AS 3570 Automotive Diesel Fuel Japanese JISK2204 lypes 1 spl 1 2 3 and 3 spl Gas Oil DF 1 DF 2 Conus and U S Government MEE BONE DF 20 Conus Diesel Fuel W F 815C FS 1 and FS 2 Burner Fuel Oil U S Military MIL L 16884G Marine Oil 1 These fuel standards are usually acceptable but are subject to change The distillate fuel chart for acceptable limits should be used as the guide for any fuel whether or not it is listed in this chart consult Caterpillar A amp I for acceptability of any other fuels West German Customer Piping Connections Engine Fuel Line Connections Fuel Supply Excess Fuel Return 38 mm 1 1 2 in ANSI Flange 38 mm 1 1 2 in ANSI Flange Boss TANA 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Fuel System Schematic A typical fuel system is illustrated below EEE EE EEE EEE i i i i i i i i i i i 3616 ENGINE i i Du i i DUPLEX MANUAL FILTER i i FUEL FILTER CONTROL VALVE i i i 3601 i i i i FUEL PRESSURE i REGULATING VALVE i MOUNTED ON ENGINE i PRESSURE HAND
101. 4 NI S12v1ND 3 40 531915 5319211 1 211 3 eu I31VAIL2V I31vVAILOV3O SLOVINO ann 197130 Gu 5 1351 SI ATlddNS AIAD D dOLS 2 3053 3 3Iveve3s 48 83 3 Di3 40111509 34D 384 NI 512 1 2 3411 te SET IT a 524 40 531915 S3LVOIUNI DNI 1 STOT 481 1 X re SET 1 vy 309170 tor 1437 8 x x ve 3 4 3448 MOT 4 S008 1353 oma LH 10 ON 440 SLOY4NOOV ON 31 310435 wot 543 4 82 S LND ee on f 5249 HOLIMS TDalND2 1303 223 HOLIMS HINDI id 1 02009 Caterpillar amp rights reserved A H un gt a e H 00 61 o
102. 438 9 9 CONV NOILVANNOY LYSNYD CATERPILLAR Miscellaneous Engine Weights The following weight schedule lists the weights of the C280 3600 series engines and optional supplied items Select the optional items and add to the engine dry weight to estimate the weight of an engine shipset Generator set package weights vary as discussed on page 131 280 3600 Engine Weights kg Ib Engine Model C280 6 3606 C280 8 3608 C280 12 3612 C280 16 3616 Engine Dry Weight See Note below 15 680 34 568 25 980 57 276 19 000 41 888 31 000 68 343 Optional Supplied Items Torsional Coupling 319 703 420 926 319 703 480 1 058 Plate Type Heat Exchanger 250 300 275 375 Water Temperature Regulator Primary Fuel Strainer Pressure Reduction Valve Freshwater Expansion Tank Exhaust Pieces Turbocharger Adapter Bellows Expander to 18 inch Fluids Weights Lube Oil 9097 kg liter Freshwater Coolant Heat Exchanger FW amp SW Total Weight per Engine Note Engine Dry Weight consists of the following engine mounted items a one piece gray iron cylinder block governor actuator two freshwater pumps one sea water pump one lube oil filter fuel and lube oil duplex filters centrifugal lube oil filters electric prelube pump exhaust shielding intake air si
103. 5 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 792 552 847 853 843 823 810 785 FROM ENGINE 7M M im 562 1022 1017 1013 OVERALL 63 125 250 500 1000 2000 4000 8000 BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 1094 1088 FROM ENGINE 71 11641134 1042 999 950 954 848 902 M 1 5M 118 0 129 4 127 0 116 9 113 4 109 0 110 5 108 1 102 8 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your Site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 C and 150 m altitude To maintain a constant air inlet manifold temperature as the air to turbo temperature goes up so must the heat rejection As altitude increases the tur
104. 5 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 5 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 6 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 6 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 7 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 7 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 8 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 8 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 9 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 9 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 10 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 10 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 11 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 11 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 12 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 12 TEMPERATURE SENSOR FAILURE ALARM ACKNOWELDGED ALARM STATUS EXHAUST PORT 13 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 13 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 14 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 14 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 15 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 15 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 16 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 16 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED TURBINE LEFT INLINE SPEED SENSOR FAILURE ALARM TURBINE LEFT INLINE SPEED SENSOR FAILURE ALARM ACKNOWLEDGED TURBINE
105. 56 083 881 0 78 076 074 071 689 067 065 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M 1980 1072 104 1 1033 104 8 100 5 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 1075 1847 964 511 557 872 853 799 FROM ENGINE 7M 103 0 1154 112 0 1027 M 1 5M 117 0 127 9 126 5 116 3 111 5 107 1 108 5 106 1 100 3 OVERALL 63 125 250 500 1000 2000 4000
106. 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 100 75 ENGINE POWER 2 4180 3800 2850 GENERATOR POWER 2 4004 3640 2730 ENGINE EFFICIENCY ISO 3046 1 42 0 42 2 42 3 ENGINE EFFICIENCY NOMINAL 40 7 41 0 41 0 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr 200 3 FUEL CONSUMPTION NOMINAL g bkw hr 204 2 FUEL CONSUMPTION 90 CONFIDENCE g bkw hr 206 7 AIR FLOW 925 C 101 3 Nm3 min 292 6 AIR MASS FLOW kg hr 19585 COMPRESSOR OUTLET PRESSURE abs 185 5 COMPRESSOR OUTLET TEMPERATURE 169 5 INLET MANIFOLD PRESSURE kPa abs 185 6 INLET MANIFOLD TEMPERATURE C 47 5 TIMING BTDC 12 5 EXHAUST STACK TEMPERATURE 375 2 EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min 311 0 EXHAUST GAS MASS FLOW kg hr 20169 EMISSIONS NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANGE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL NOMINAL HEAT REJ TO EXH LHV 25 NOMINAL HEAT REJ TO EXH LHV 177 NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTE
107. 80 16 UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN MM CATERPILLAR THE INFORMATION HEREON 15 THE PROPERTY OF CATERPILLAR INC AND OR TTS SUBSIDIARIES WITHOUT OTHERS AND ANY WRITTEN PERMSSION ANY COPYING TRANSMITTAL TO EXCEPT THAT FOR WHICH LOANED IS PROHIBITED INSTALLATION DRAWINGS MARKETING GUIDE 2009 Caterpillar rights reserved mq ONILNNON CNV NOILVANNOA LASNA 2 e z z T un gt 00 QI NILIAYYN gt 13 o L L33 5 380071 aa4vanvls G6 K6 1 40 13 238 OHL Y LL 4 439 LEN 9 Ll rved 5 rese SS3NMOIHL 4385 3 right
108. 80 3600 engines Preservation Procedures 1E2566L Processing After Assembly and Test e Al parts should be prepared and painted according to 1E2001 Fil Engine Jacket Water EJW system with solution of 20 379 and 80 water or equivalent solution regulator bypass line must be used to allow filling on both sides of the regulator Vent and EJW system at the highest point possible to assure complete filling For engines with Separate Circuit Aftercooler SCAC systems fill the SCAC system with a solution of 20 VCI 379 and water or equivalent solution Vent the SCAC system at the highest point possible to assure complete filling e Drain the VCI solution from the EJW system at multiple locations to assure complete drainage EJW pump 10 block face cover oil cooler etc Drain the VCI solution from engines with SCAC system at the SCAC water pump Close all EJW and SCAS system openings with the parts specified on engineering drawings Spray a mixture of 50 1 E2359 VCI oil and 50 engine oil into the air intake or turbocharger inlet Minimum application rate is 7 5 mL L of engine displacement Install covers specified on engineering drawing to seal in VCI vapors Spray a mixture of 50 1E2359 VCI oil and 50 engine oil into the exhaust opening Minimum application rate is 7 5 mL L of engine displacement Install covers specified on engineering drawing to seal in vapors e Fill oiler reservoir for air st
109. A FUEL INPUT ENERGY LHV TO JACKET WATER NOMINAL ATMOSPHERE NOMINAL TO OIL COOLER NOMINAL TO EXH LHV TO 25 C NOMINAL TO EXH LHV TO 177 C NOMINAL TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5816 02 BErec
110. AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5815 02 Eos DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 8 Tier 1 Technical Data 900 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 858 0
111. ATER LOW PRESSURE DIGITAL X 35kPa TRANSDUCER IS ORDERED lt 20 kPa LOW REMOVED IF LOW JACKET WATER RPM PRESSURE 144 0102 22 lt 35 kPa HIGH TRANSDUCER IS ORDERED RPM REMOVED IF M DIGITAL X lt 35 kPa TRANSDUCER IS ORDERED SWITCHES MISC CONTACTS BATTERY VOLTAGE 709 DIGITAL x lt 22 VDC MONITORS DC TO MMS JACKET WATER DETECTION DIGITAL x CONTACT ENERGIZES RJWDA 125 4340 CLOSE RELAY CONTACT 5 018 OFF FUEL AND EMERGENCY STOP LOCAL DIGITAL X ENGINE ENGINE SPEED SWITCH PER 170 RPM amp 0 CRANK TERMINATE 100 5675 2 SEC Rees d lisse 9 SEC AFTER ENABLES ALARMS AND SS 001 SHUTDOWNS ENGINE SPEED SWITCH OIL DIGITAL 75 RATED ENABLES HIGH SPEED PRESSURE STEP 100 5675 SPEED OIL CONTACTOR ENGINE OIL SUMP LEVEL 2 DIGITAL X ENGINE PRE LUBE ENGINE START PRESSURE 3N 1400 DIGITAL gt 9kPa NTERLOCK OIL MIST DETECTION era CONTACT OIL MIST DETECTOR SYSTEM STATUS READY CLOSE READY OIL MIST DETECTION OIL MIST DETECTOR AR DIGITAL CONTACT OPEN EXPANSION TANK LOW DIGITAL CONTACT OPEN CUSTOMER SUPPLIED ENGINE OVERSPEED ENGINE SPEED SWITCH DIGITAL ee ATED PROVIDER EY SPEED SPEED SWITCH 100 5675 FUEL CONTROL SWITCH DIGITAL RELAY BASED SYSTEM 02009 Caterpillar amp rights reserved CATERPILLAR Signal Shut Setpoint
112. ATER OUTLET C ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 ENGINE POWER 2 bkW 2233 GENERATOR POWER 2 ekW 2134 ENGINE EFFICIENCY ISO 3046 1 40 8 ENGINE EFFICIENCY NOMINAL 39 6 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr FUEL CONSUMPTION NOMINAL g bkw hr FUEL CONSUMPTION 90 CONFIDENCE g bkw hr FLOW 25 101 3 kPaa Nm3 min IAIR MASS FLOW kg hr COMPRESSOR OUTLET PRESSURE kPa abs COMPRESSOR OUTLET TEMPERATURE INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr EMISSIONS NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE
113. ATURE C 40023 STATOR B TEMPERATURE C 40024 STATOR C TEMPERATURE C 40025 TURBINE INLET LEFT INLINE TEMPERATURE C 40026 TURBINE INLET RIGHT TEMPERATURE C 40027 TURBINE OUTLET LEFT INLINE TEMPERATURE C 40028 TURBINE OUTLET RIGHT TEMPERATURE C 40029 EXHAUST PORT 1 TEMPERATURE C 40030 EXHAUST PORT 2 TEMPERATURE C 40031 EXHAUST PORT 3 TEMPERATURE C 40032 EXHAUST PORT 4 TEMPERATURE C 40033 EXHAUST PORT 5 TEMPERATURE C 40034 EXHAUST PORT 6 TEMPERATURE C 40035 EXHAUST PORT 7 TEMPERATURE C 40036 EXHAUST PORT 8 TEMPERATURE C 40037 EXHAUST PORT 9 TEMPERATURE C 40038 EXHAUST PORT 10 TEMPERATURE C 40039 EXHAUST PORT 11 TEMPERATURE C 40040 EXHAUST PORT 12 TEMPERATURE C 40041 EXHAUST PORT 13 TEMPERATURE C 40042 EXHAUST PORT 14 TEMPERATURE C 40043 EXHAUST PORT 15 TEMPERATURE C 40044 EXHAUST PORT 16 TEMPERATURE C 40045 WRITE SPARE 40046 WRITE SPARE 40047 WRITE SPARE 40048 WRITE SPARE 40049 TURBINE LEFT INLINE SPEED RPM 40050 TURBINE RIGHT SPEED RPM 40051 ENGINE SPEED RPM 40052 NMOGLNHS ONIYOLINOW ANIONG 2009 Caterpillar rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA MODBUS ADDRESS EXHAUST PORT 1 TEMPERATURE DEVIATION 40053 EXHAUST PORT 2 TEMPERATURE DEVIATION 40054 EXHAUST PORT 3 TEMPERATURE DEVIATION 40055 EXHAUST PORT 4 TEMPERATURE DEVIATION 40056 EXHAUST PORT 5 TEMPERATURE DEVIATION 40057 E
114. C ASSUMED GENERATOR EFFICIENCY 96 ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s RATING ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY NOTES LOAD MARINE AUXILIARY IMO EPA MARINE TIER 1 258 2288 DISTILLATE 150 96 0 8 10 ISO 3046 1 NOMINAL FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION ENGINE DATA ISO 3046 1 1 g bkw hr NOMINAL 1 g bkw hr 90 CONFIDENCE 1 g bkw hr AIR FLOW 25 101 3 kPaa Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE o EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30
115. C280 3600 Petroleum Offshore Project Guide s CATERPILLAR RE 9156919124 E NT 1 Engine Selections iss 1 Engine and Generator Set Ratings 1 Basic C280 3600 Diesel Engine 2 Example Diesel Generator Package Scope of Supply 3 e e e o J e e 3 Generators Tessa so EO 3 4 Exhaust VEN uyay u ayu au GSA 4 Cooling SVSISIYDS uuu uuu 4 EE EE EE 4 Lube Oil System 5 T 5 Control System asa 5 Protection System 6 Other Equipment in Main 10 Optional Engine 11 Optional Service Tools Shipping Protection and Factory Support 11 Optional Literature dde 12 Technical Data eere p REED
116. DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8393 00 BErecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 6 Tier 2 Technical Data 1000 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 078 076 974 OM 039 067 055 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30
117. DGED 40253 10 STATOR A TEMPERATURE SENSOR FAILURE ALARM 40253 11 STATOR A TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40253 12 STATOR B TEMPERATURE SENSOR FAILURE ALARM 40253 13 STATOR B TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40253 14 STATOR C TEMPERATURE SENSOR FAILURE ALARM 40253 15 STATOR C TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40253 16 MONITORING AND SHUTDOWN 2009 Caterpillar All rights reserved CATERPILLAR ANALOG DATA ALARM STATUS TURBINE INLET LEFT INLINE TEMPERATURE SENSOR FAILURE ALARM TURBINE INLET LEFT INLINE TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED TURBINE INLET RIGHT TEMPERATURE SENSOR FAILURE ALARM TURBINE INLET RIGHT TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED TURBINE OUTLET LEFT INLINE TEMPERATURE SENSOR FAILURE ALARM TURBINE OUTLET LEFT INLINE TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED TURBINE OUTLET RIGHT TEMPERATURE SENSOR FAILURE ALARM TURBINE OUTLET RIGHT TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 1 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 1 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 2 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 2 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 3 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 3 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED EXHAUST PORT 4 TEMPERATURE SENSOR FAILURE ALARM EXHAUST PORT 4 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED ALARM STATUS EXHAUST PORT
118. DGED 40265 12 EXHAUST PORT 9 TEMPERATURE DEVIATION ALARM 40265 13 EXHAUST PORT 9 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 14 EXHAUST PORT 10 TEMPERATURE DEVIATION ALARM 40265 15 EXHAUST PORT 10 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED 40265 16 MONITORING AND SHUTDOWN 2009 Caterpillar All rights reserved CATERPILLAR ANALOG DATA ALARM STATUS EXHAUST PORT 11 TEMPERATURE DEVIATION ALARM EXHAUST PORT 11 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED EXHAUST PORT 12 TEMPERATURE DEVIATION ALARM EXHAUST PORT 12 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED EXHAUST PORT 13 TEMPERATURE DEVIATION ALARM EXHAUST PORT 13 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED EXHAUST PORT 14 TEMPERATURE DEVIATION ALARM EXHAUST PORT 14 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED EXHAUST PORT 15 TEMPERATURE DEVIATION ALARM EXHAUST PORT 15 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED EXHAUST PORT 16 TEMPERATURE DEVIATION ALARM EXHAUST PORT 16 TEMPERATURE DEVIATION ALARM ACKNOWLEDGED FUEL FILTER PRESSURE DIFFERENTIAL ALARM FUEL FILTER PRESSURE DIFFERENTIAL ALARM ACKNOWLEDGED LUBE OIL FILTER PRESSURE DIFFERENTIAL ALARM LUBE OIL FILTER PRESSURE DIFFERENTIAL ALARM ACKNOWLEDGED ALARM STATUS PLC MEMORY BATTERY LOW ALARM PLC MEMORY BATTERY LOW ALARM ACKNOWLEDGED SLOT 1 FAULT ALARM SLOT 1 FAULT ALARM ACKNOWLEDGED SLOT 2 FAULT ALARM SLOT 2 FAULT ALARM ACKNOWLEDGED SLOT 3 FAULT ALARM SLOT 3 FAULT ALARM ACKNOWLEDGED SLOT 4 FAULT ALAR
119. DISTILLATE AFTERCOOLER WATER RATED ALTITUDE Q 252 150 JACKET WATER OUTLET ASSUMED GENERATOR EFFICIENCY 96 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD MEAN PISTON SPEED m s 9 FIRING PRESSURE MAXIMUM kPa RATING LOAD 75 ENGINE POWER bkW 1425 GENERATOR POWER ekW 1365 BMEP kPa 1715 ENGINE EFFICIENCY 180 3046 1 40 3 ENGINE EFFICIENCY NOMINAL 39 1 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr FUEL CONSUMPTION NOMINAL g bkw hr FUEL CONSUMPTION 90 CONFIDENCE g bkw hr FLOW 25 C 101 3 kPaa Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE c EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ TO ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH
120. E PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 1096 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7T HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water TIMING BASED ON AFM INJECTORS 0 EMMISSION DATA SHOWN ARE NOMINAL VALUES 9 1 5 22 2003 DM5431 05 Brecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR 3616 Technical Data 1000 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 200 8031 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER C RATED ALTITUDE 25 C 200 JACKET WATER OUTLET C ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD
121. E HIGH ALARM ACKNOWLEDGED LUBE OIL TO ENGINE PRESSURE LOW ALARM LUBE OIL TO ENGINE PRESSURE LOW ALARM ACKNOWLEDGED LUBE OIL TO FILTER PRESSURE HIGH ALARM LUBE OIL TO FILTER PRESSURE HIGH ALARM ACKNOWLEDGED INLET AIR MANIFOLD TEMPERATURE HIGH ALARM INLET AIR MANIFOLD TEMPERATURE HIGH ALARM ACKNOWLEDGED ALARM STATUS INLET AIR MANIFOLD PRESSURE HIGH ALARM INLET AIR MANIFOLD PRESSURE HIGH ALARM ACKNOWLEDGED FUEL TO ENGINE TEMPERATURE HIGH ALARM FUEL TO ENGINE TEMPERATURE HIGH ALARM ACKNOWLEDGED FUEL TO ENGINE PRESSURE LOW ALARM FUEL TO ENGINE PRESSURE LOW ALARM ACKNOWLEDGED JACKET WATER OUTLET TEMPERATURE HIGH ALARM JACKET WATER OUTLET TEMPERATURE HIGH ALARM ACKNOWLEDGED JACKET WATER PRESSURE LOW ALARM JACKET WATER PRESSURE LOW ALARM ACKNOWLEDGED WATER INLET TEMPERATURE HIGH ALARM WATER INLET TEMPERATURE HIGH ALARM ACKNOWLEDGED AC OC PUMP PRESSURE LOW ALARM AC OC PUMP PRESSURE LOW ALARM ACKNOWLEDGED RAW WATER PRESSURE LOW ALARM RAW WATER PRESSURE LOW ALARM ACKNOWLEDGED ALARM STATUS AUXILIARY 1 TEMPERATURE ALARM AUXILIARY 1 TEMPERATURE ALARM ACKNOWLEDGED AUXILIARY 2 TEMPERATURE ALARM AUXILIARY 2 TEMPERATURE ALARM ACKNOWLEDGED AUXILIARY 1 4 20mA ALARM AUXILIARY 1 4 20mA ALARM ACKNOWLEDGED AUXILIARY 2 4 20mA ALARM AUXILIARY 2 4 20mA ALARM ACKNOWLEDGED AIR START PRESSURE LOW ALARM AIR START PRESSURE LOW ALARM ACKNOWLEDGED NON DRIVE BEARING TEMPERATURE HIGH ALARM NON DRIVE BEARING TEMPERATURE H
122. E J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5810 02 Eos DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 6 Tier 1 Technical Data 1000 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS 50 094 091 45 0 95 0 93 40 087 0 94 35 098 096 0 i I i 30 25 20 I j 0 92 089 0 86 0 84 081 0 79 0 76 15 I
123. EAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5821 02 Brecnnicar DATA 2009 Caterpillar All rights reserved CATERPILLAR C280 12 Tier 1 Technical Data 900 rpm Sheet 2 of 2 C280 12 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 858 056 083 881 0 78 076 074 071 689 067 065 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL
124. EDGED EXHAUST PORT 2 TEMPERATURE HIGH ALARM EXHAUST PORT 2 TEMPERATURE HIGH ALARM ACKNOWLEDGED ALARM STATUS EXHAUST PORT 3 TEMPERATURE HIGH ALARM EXHAUST PORT 3 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 4 TEMPERATURE HIGH ALARM EXHAUST PORT 4 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 5 TEMPERATURE HIGH ALARM EXHAUST PORT 5 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 6 TEMPERATURE HIGH ALARM EXHAUST PORT 6 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 7 TEMPERATURE HIGH ALARM EXHAUST PORT 7 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 8 TEMPERATURE HIGH ALARM EXHAUST PORT 8 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 9 TEMPERATURE HIGH ALARM EXHAUST PORT 9 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 10 TEMPERATURE HIGH ALARM EXHAUST PORT 10 TEMPERATURE HIGH ALARM ACKNOWLEDGED ALARM STATUS EXHAUST PORT 11 TEMPERATURE HIGH ALARM EXHAUST PORT 11 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 12 TEMPERATURE HIGH ALARM EXHAUST PORT 12 TEMPERATURE HIGH ALARM ACKNOWELDGED EXHAUST PORT 13 TEMPERATURE HIGH ALARM EXHAUST PORT 13 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 14 TEMPERATURE HIGH ALARM EXHAUST PORT 14 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 15 TEMPERATURE HIGH ALARM EXHAUST PORT 15 TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 16 TEMPERATURE HIGH ALARM EXHAUST PORT 16 TEMPERATURE HIGH ALARM ACKNOWLEDGED TURBINE LEFT INLINE OVERSPEED ALARM T
125. EDUNDANT JACKET WATER OUTLET TEMPERATURE SENSOR FAILURE ALARM 40252 03 REDUNDANT JACKET WATER OUTLET TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGEL 40252 04 JACKET WATER PRESSURE SENSOR FAILURE ALARM 40252 05 JACKET WATER PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 06 AC OC WATER INLET TEMPERATURE SENSOR FAILURE ALARM 40252 07 AC OC WATER INLET TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 08 AC OC PUMP PRESSURE SENSOR FAILURE ALARM 40252 09 AC OC PUMP PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 10 RAW WATER PRESSURE SENSOR FAILURE ALARM 40252 11 RAW WATER PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 12 AUXILIARY 1 TEMPERATURE SENSOR FAILURE ALARM 40252 13 AUXILIARY 1 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 14 AUXILIARY 2 TEMPERATURE SENSOR FAILURE ALARM 40252 15 AUXILIARY 2 TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40252 16 ALARM STATUS 40253 AUXILIARY 1 4 20mA SENSOR FAILURE ALARM 40253 01 AUXILIARY 1 4 20mA SENSOR FAILURE ALARM ACKNOWLEDGED 40253 02 AUXILIARY 2 4 20mA SENSOR FAILURE ALARM 40253 03 AUXILIARY 2 4 20mA SENSOR FAILURE ALARM ACKNOWLEDGED 40253 04 AIR START PRESSURE SENSOR FAILURE ALARM 40253 05 AIR START PRESSURE SENSOR FAILURE ALARM ACKNOWLEDGED 40253 06 NON DRIVE BEARING TEMPERATURE SENSOR FAILURE ALARM 40253 07 NON DRIVE BEARING TEMPERATURE SENSOR FAILURE ALARM ACKNOWLEDGED 40253 08 DRIVE BEARING TEMPERATURE SENSOR FAILURE ALARM 40253 09 DRIVE BEARING TEMPERATURE SENSOR FAILURE ALARM ACKNOWLE
126. EMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 1096 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7T HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 9 TIMING BASED ON AFM INJECTORS 10 EMMISSION DATA SHOWN ARE NOMINAL VALUES 10 17 2002 DM5429 05 Boo IVOINHO ML 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 3612 Technical Data 900 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 157 5514 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER RATED ALTITUDE 25 C 150 JACKET WATER OUTLET C ASSUMED GENERATOR EFFICIENCY 96 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0
127. ER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8417 00 Bones DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 16 Tier 2 Technical Data 1000 rpm Sheet 2 of 2 C280 16 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS
128. ER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 4 12 2006 DM5822 02 Eos DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 12 Tier 1 Technical Data 1000 rpm Sheet 2 of 2 C280 12 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 858 056 083 881 0 78 076 074 071 689 067 065 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 3
129. ERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8401 00 Boris DATA 02009 Caterpillar amp rights reserved CATERPILLAR C280 8 Tier 2 Technical Data 1000 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 078 076 974 OM 039 067 055 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL
130. F 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8418 00 Brecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 16 Tier 2 Technical Data 900 rpm Sheet 2 of 2 C280 16 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 978 076 074 OM 039 067 055 oss 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 20
131. FICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 100 ENGINE POWER 2 2783 2530 GENERATOR POWER 2 2662 2420 ENGINE EFFICIENCY ISO 3046 1 43 6 43 6 ENGINE EFFICIENCY NOMINAL 42 2 42 3 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr FUEL CONSUMPTION NOMINAL g bkw hr FUEL CONSUMPTION 90 CONFIDENCE g bkw hr AIR FLOW 25 101 3 Nm3 min IAIR MASS FLOW kg hr COMPRESSOR OUTLET PRESSURE kPa abs COMPRESSOR OUTLET TEMPERATURE C INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 C 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED AL
132. FOLD RATING NOTES LOAD 110 100 75 ENGINE POWER 2 2981 2710 2033 IGENERATOR POWER 2 2860 2600 1950 ENGINE EFFICIENCY ISO 3046 1 42 3 42 7 42 4 ENGINE EFFICIENCY NOMINAL 41 0 41 4 41 1 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr 199 5 FUEL CONSUMPTION NOMINAL g bkw hr 203 4 FUEL CONSUMPTION 90 CONFIDENCE g bkw hr 205 9 AIR FLOW 25 101 3 Nm3 min 218 7 IAIR MASS FLOW kg hr 14634 ICOMPRESSOR OUTLET PRESSURE kPa abs 195 8 ICOMPRESSOR OUTLET TEMPERATURE 155 5 INLET MANIFOLD PRESSURE kPa abs 194 2 INLET MANIFOLD TEMPERATURE C 42 9 TIMING BTDC 12 5 EXHAUST STACK TEMPERATURE C 383 9 EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min 466 6 EXHAUST GAS MASS FLOW kg hr 15050 EMISSIONS NOx as NO g bkW hr g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ TO ATMOSPHERE HEAT REJ TO OIL COOLER HEAT REJ TO LHV 25 HEAT REJ TO LHV TO 177 HEAT REJ TO AFTERCOOLER CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR T
133. H OUT 1 24 HIGH 22 X PSHH 003 RCPHS RELAY LOW ENGINE OIL PRESSURE PSLL 001 OR SHUTDOWN 002 ENGINE OVERSPEED X SS 002 ROSR RELAY FUEL CONTROL RELAY NO NC X 2 RELAY LOW MARINE GEAR 22 4 X PSLL 020 RGOPLS RELAY ALARM OR ALARM HORN AND BEACON NO IEEE RHB RELAY SUMMARY SHUTDOWN RELAY ENGINE FAULT NE X SHUTDOWN DELAY ENGINE RUNNING CRANK ENGINE SPEED TERMINATE NO 170 RPM PETR RELAT PRELUBE ENGINE NO PS 008 gt 9 kPa RPR RELAY CIRCUIT BREAKER TRIP s AUX CONTACTS ON ALARM CIRCUIT BREAKERS OPENS REDUCE ENGINE LOAD REL RELAY ENGINE ALARM SUMMARY NO X 2009 Caterpillar rights reserved ANV ONIYOLINOW ANIONGA Broene MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE Signal Shut Setpoint Sensor Description Type Alarm Down Trip Comments CUSTOMER SUPPLIED INTERFACE 24VDC LUBE OIL STANDBY PUMP 24VDC 1195 JENS CUSTOMER INTERFACE AIR START SIGNAL TO SEAT REMOTE SSTART ONLY ENGINE RAS RELAY FUEL SHUTOFF SIGNAL TO SHUTDOWN OR E GNE DIGITAL X FUEL OFF RFR RELAY AIR SHUTOFF SIGNAL TO OVERSPEED amp 1 DIGITAL STOP ASOS SOLENOID ENGINE PRELUBE SIGNAL DIGITAL gt 9kPa RPR RELAY ENGINE PROTECTION ROVR RELAY SYSTEM OVERRIDE RELAY DIGITAL E SUMMARY GROUP ALARM awan re DIGITAL X ANY ALARM RSA
134. I 28 31 1 OL 928 123 NADGLNHS Dl 37104383 X04 e EBT 1 lt e d c S in teet bE ER 4 34 al ar 1 Se gt 4 0 is T ser M AH 311 N D SAD 4 ann 3 11 ANLI TI a ad 2009 Caterpillar All rights reserved Broene MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE Control System Inputs to PLC and Redundant Relay Logic Ensure that all safety information warnings and instructions are read and understood before any operation or any maintenance procedures are performed Signal Shut Setpoint Sensor Description Type Alarm Down Trip Comments PRESSURE CONTACTORS E OIL PRESSURE DIGITAL X lt 105 kPa LOW SPEED PING aa OIL PRESSURE DIGITAL X lt 260 kPa HIGH SPEED ENGINE HIGH ENABLE WHEN FUEL IS PRESSURE 117 1864 21999 REMOVED IF 2222 DIGITAL X lt 750 kPa TRANSDUCER IS ORDERED REMOVED IF SEAW
135. IGH ALARM ACKNOWLEDGED DRIVE BEARING TEMPERATURE HIGH ALARM DRIVE BEARING TEMPERATURE HIGH ALARM ACKNOWLEDGED STATOR A TEMPERATURE HIGH ALARM STATOR A TEMPERATURE HIGH ALARM ACKNOWLEDGED 02009 Caterpillar amp rights reserved MODBUS ADDRESS 40257 40257 01 40257 02 40257 03 40257 04 40257 05 40257 06 40257 07 40257 08 40257 09 40257 10 40257 11 40257 12 40257 13 40257 14 40257 15 40257 16 40258 40258 01 40258 02 40258 03 40258 04 40258 05 40258 06 40258 07 40258 08 40258 09 40258 10 40258 11 40258 12 40258 13 40258 14 40258 15 40258 16 40259 40259 01 40259 02 40259 03 40259 04 40259 05 40259 06 40259 07 40259 08 40259 09 40259 10 40259 11 40259 12 40259 13 40259 14 40259 15 40259 16 CATERPILLAR ANALOG DATA ALARM STATUS STATOR B TEMPERATURE HIGH ALARM STATOR B TEMPERATURE HIGH ALARM ACKNOWLEDGED STATOR C TEMPERATURE HIGH ALARM STATOR C TEMPERATURE HIGH ALARM ACKNOWLEDGED TURBINE INLET LEFT INLINE TEMPERATURE HIGH ALARM TURBINE INLET LEFT INLINE TEMPERATURE HIGH ALARM ACKNOWLEDGED TURBINE INLET RIGHT TEMPERATURE HIGH ALARM TURBINE INLET RIGHT TEMPERATURE HIGH ALARM ACKNOWLEDGED TURBINE OUTLET LEFT INLINE TEMPERATURE HIGH ALARM TURBINE OUTLET LEFT INLINE TEMPERATURE HIGH ALARM ACKNOWLEDGED TURBINE OUTLET RIGHT TEMPERATURE HIGH ALARM TURBINE OUTLET RIGHT TEMPERATURE HIGH ALARM ACKNOWLEDGED EXHAUST PORT 1 TEMPERATURE HIGH ALARM EXHAUST PORT 1 TEMPERATURE HIGH ALARM ACKNOWL
136. ION FACTORS ost 091 088 086 083 081 078 076 974 OM 039 067 055 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 115 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANGE 877 246 838 841 853 810 770 895 FROM ENGINE 957 506 898 901 813 87 0 830 750 M im 1047 1016 100 8 101 1 1023 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 06 0 1066 1037 954 90 1 857 862 843 789 FRO
137. ITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD DRY MEAN PISTON SPEED m s 10 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD 110 100 75 ENGINE POWER bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL FUEL CONSUMPTION ISO 3046 1 g bkw hr 199 8 201 5 FUEL CONSUMPTION NOMINAL g bkw hr 203 7 205 4 FUEL CONSUMPTION 90 CONFIDENCE g bkw hr 205 9 207 9 FLOW 25 101 3 kPaa Nm3 min 204 3 160 1 MASS FLOW kg hr 13674 10717 INLET MANIFOLD PRESSURE kPa abs 347 8 273 1 INLET MANIFOLD TEMPERATURE C 36 0 35 0 EXHAUST STACK TEMPERATURE 376 3 372 0 EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min 440 2 342 4 EXHAUST GAS MASS FLOW kg hr 14090 11031 EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 NOMINAL HEAT REJ TO LHV TO 177 NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SA
138. ITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8402 00 BErecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 8 Tier 2 Technical Data 900 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 858 056 083 881 0 78 076 074 071 689 067 065
139. If the actual generator is less than 9696 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 1 19 2007 DM8409 00 Boo IVOINHO ML 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 16 Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD C280 16 Tier 2 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENGY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 284 8281 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 5566 5324 252 44 6 43 3 100 5060 4840 2283 44 1 42 8 75 3795 3630 1712 42 9 41 6 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 25 C 101 3 kPaa AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TE
140. LAO 433HS 7191302 33 d BWW HIM OL 3NION3 40 2009 Caterpillar rights reserved 2 e z z T un gt 00 QI AINO 39N333333 803 38 NI NMOHS SNOISN3MIQ 1432 3 SINN 1 0 3HL 01 NIVIY3d LON 00 MOMNV SNOISN3WIQ 1 33 AIHL HOIHM OL INN 3HL OL T3TWavd 38 SNOISNINIG SHvaddV HOIHM NI SHL 303 Wniva 8 3 V SV 9351 SI 2 2 JHL SH3IHLO 4185504 ANY JINON JANI SWILSAS 15 SUINVITO SW31SAS 9 003 ONIGNTONI MINOLSNI 35001 5 403 NOLVTIVISNI A8 33 35 1 310 83 4 0 jO 33 3 0 3NION3 40 3NIRHGIN3O 20 IJVHSXNVHO 40 10 5 4 0
141. M SLOT 4 FAULT ALARM ACKNOWLEDGED SLOT 5 FAULT ALARM SLOT 5 FAULT ALARM ACKNOWLEDGED SLOT 6 FAULT ALARM SLOT 6 FAULT ALARM ACKNOWLEDGED SLOT 7 FAULT ALARM SLOT 7 FAULT ALARM ACKNOWLEDGED ALARM STATUS SLOT 8 FAULT ALARM SLOT 8 FAULT ALARM ACKNOWLEDGED SLOT 9 FAULT ALARM SLOT 9 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 0 FAULT ALARM RACK 0 GROUP 0 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 1 FAULT ALARM RACK 0 GROUP 1 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 2 FAULT ALARM RACK 0 GROUP 2 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 3 FAULT ALARM RACK 0 GROUP 3 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 4 FAULT ALARM RACK 0 GROUP 4 FAULT ALARM ACKNOWLEDGED RACK 0 GROUP 5 FAULT ALARM RACK 0 GROUP 5 FAULT ALARM ACKNOWLEDGED 2009 Caterpillar All rights reserved MODBUS ADDRESS 40266 40266 01 40266 02 40266 03 40266 04 40266 05 40266 06 40266 07 40266 08 40266 09 40266 10 40266 11 40266 12 40266 13 40266 14 40266 15 40266 16 40267 40267 01 40267 02 40267 03 40267 04 40267 05 40267 06 40267 07 40267 08 40267 09 40267 10 40267 11 40267 12 40267 13 40267 14 40267 15 40267 16 40268 40268 01 40268 02 40268 03 40268 04 40268 05 40268 06 40268 07 40268 08 40268 09 40268 10 40268 11 40268 12 40268 13 40268 14 40268 15 40268 16 NMOGLNHS ONIYOLINOW ANIONG Broene MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA ALARM STATUS RACK 0 GROUP
142. M ENGINE 7M 102 0 1144 1110 1017 969 920 930 916 862 M 1 5M 116 0 126 9 125 5 115 3 110 5 106 1 107 5 105 1 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekW listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor
143. MPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY O
144. NE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 25 C 101 3 kPaa AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13 018 g bkW hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ISO 3046 1 NOMINAL 90 CONFIDENCE g bkw hr g bkw hr g bkw hr Nm3 min kg hr kPa abs EMISSIONS NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPE
145. NGINE ONLY LOW BATTERY VOLTAGE SYSTEM BIT lt 22 VDC LOW PLC MEMORY BATTERY VOLTAGE JACKET WATER DETECTION BIT BIT CONTACT CLOSE RED BATT LIGHT ON PLC S CPU EMERGENCY STOP BIT CONTACT CLOSE ENGINE SPEED SWITCH CRANK TERMINATE BIT gt 170 RPM amp 0 25 2009 Caterpillar rights reserved ANV ONIYOLINOW ANIONGA C280 PETROLEUM OFFSHORE PROJECT GUIDE Bone MONITORING AND SHUTDOWN Sensor Description e Alarm en n p Comments LOW ENGINE OIL SUMP Bi x MECHANICAL LEVEL POSITION ENGINE PRE LUBE STARTING PRESSURE BIT some AVAILABLE OIL MIST DETECTION x SYSTEM READY STATUS OIL MIST DETECTION x CONTACT SHUTDOWN CLOSE LOW EXPANSION TANK y CUSTOMER CUSTOMER SUPPLIED LEVEL SWITCH DEFINED CONTACT 113 RATED PROVIDED BY SPEED ENGINE OVERSPEED BIT X PED SWITCH OB PLC MANUAL DECREASE REDUCE ENGINE LOAD LOAD MAG PICK UP ENGINE ST 008 AND SEDES X NOT 5 004 SPEED SWITCH PICKUP ENGINE CONTROL SWITCH CONTACT OFF CLOSE SENSOR FAILURES ENGINE LUBE OIL m x 50 OR TEMPERATURE 150 INLET AIR MANIFOLD Ee x 50 OR TEMPERATURE 150 ENGINE AC OC CIRCUIT Bir x 50 OR OUTLET WATER TEMP 150 ENGINE JACKET WATER Sm x 50 OR OUTLET TEMP SHUTD
146. NLET SEAWATER OUTLET E NOTES G CONNECTION LOCATIONS SHOWN IN THIS SCHEMATIC ARE FOR ILLUSTRATIVE PURPOSES ONLY HEAT REJ AND TEMPERATURE DATA BASED ON 50 50 GLYCOL MIXTURE DATA BASED 259 AMBIENT AND 32 WATER TO HEAT REJECTION TOLERANCES COOLANT FLOW 10 HEAT REJECTION 10 METRIC TOLERANCES ACCOUNT FOR VARIATION TEST DATA ACCURACY REPEATABILITY AND SCATTER THE HEAT REJECTION 1E2733 DRAWING AUTOCAD TOLERANCE BAND DOES NOT ACCOUNT FOR ON SITE CONDITIONS SUCH S 1E0011 INTPR amp TOL AS AMBIENT AND ALTITUDE TOLERANCE GUIDELINES CAN BE FOUND IN T SPEC NO NAME THE 3600 EPG APPLICATION AND INSTALLATION GUIDE LEKX1002 gt 9 MAXIMUM ALLOWABLE ENGINE EXTERNAL COOLING SYSTEM PRESSURE DROP SHALL CATERPILLAR GUIDE LINES FOR SPECIFIC NO DESCRIPTION GUIDELINES AND TEST POINT LOCATIONS SEE THE CATERPILLAR TON DP PRE PROD LG 3600 LEVEL GAUGE 3600 APPLICATION AND INSTALLATION GUIDE COOLING SYSTEM SECTION SEPT PROD m m ALL ORIFICES SHOWN ARE SUPPLIED BY OTHERS ENGINE MODEL 0 16 SL 360010 LEVEL SV 6 CUSTOMER SUPPLIED FLOW SETTING ORIFICE DIMENSIONS ARE IN MM un PT 3600 JACKET WATER PUMP PRESSURE TRANSMITTER 5 W O TOL gt PT 3601 AC OC WATER PUMP PRESSURE TRANSMITTER T N 3602 RAWWATER PRESSURE TRANSMITTER 1 or 1 1
147. NLY CYLINDER TEMPERATURE Te 14 gt 700 a TENPERSIUBE pr X lt 50 OR gt 700 16 CYL ENGINE ONLY 2 tees Bie yi lt 50 OR gt 700 16 CYL ENGINE ONLY ENGINE SPEED Es x lt 3 85mA OR gt TRANSDUCER 20 15mA LUBE OIL PRESSURE TO lt 3 85mA OR gt FILTER 20 15mA LUBE OIL PRESSURE TO iT lt 3 85mA OR gt ENGINE 20 15mA FUEL PRESSURE TO FILTER X lt ee gt USED FOR DIFF ALARM FUEL PRESSURE TO ENGINE X lt 9 85mA OR gt 20 15 ENGINE JACKET WATER lt 3 85mA OR gt PRESSURE d 20 15mA OPTIONAL CIRCUIT WATER lt 3 85mA OR gt PRESSURE BIT 20 15mA OPTIONAL lt 3 85mA OR gt gt SEA WATER PRESSURE BIT X gt OPTIONAL ENGINE STARTING AIR lt 3 85mA OR gt 2 PRESSURE BIT X 20 15mA OPTIONAL ENGINE INLET AIR MANIFOLD lt 3 85 OR gt Z PRESSURE 20 15 ENGINE LOW OIL PRESSURE NO SIGNAL gt CONTACTOR PH X N O AND N C LOW SPEED ENGINE LOW OIL PRESSURE NO SIGNAL CONTACTOR BH i NO AND N C SPEED ENGINE HIGH E F NO SIGNAL E PRESSURE CONTACTOR AND PRESSURE ENGINE SPEED ENGINE SPEED 113 RATED Z TRANSDUCER WORD SPEED 9 1200 RPM 5 LUBE OIL PRESSURE 0 1000 kPa a FILTER USED FOR DIFF ALARM lt 120 kPa 8 lt X 0 1000 kPa ER TO LOW SPEED amp HIGH 5 X a SPEED SETPOINTS 260 kPa 2 2 113 C280 PETROLEUM OFFSHORE PROJECT GUIDE Signal Shut Setpoint
148. NW 1196 315 3 NJAOMNON 83814 31 44 5 Addy 132945 11 093 91 Belo 5 iD ANON 5 JLI 0lZ v 719130 2 3LON 3LUN VOLUN 2009 Caterpillar rights reserved 2 e z T un gt 00 QI 1NO33 3015 1H9lN HL 19018 40 30v4 8 3 mJ ann 33 40 MilN32 7 AINO 339 9 2 aariddns YAWOLSND UVE 30 3 45 ATNO JONISIH4IM 2009 Caterpillar All rights reserved 33 8 SINAOW 9 79522 LNOHLIM OM SSWI DILYN3IHOS ONILSIT 9L oezo AINO
149. ON 302 6302 SHEET 7 6375 PARTNER FLANGE 4 ANSI FLANGE PROVIDED WATERMAKER OUTLET DETAIL ON 302 6302 SHEET 7 6123 PARTNER FLANGE 4 ANSI FLANGE PROVIDED GENERATOR COOLING DN50 PN16 DIN 2633 FLANGE 1912 PARTNER FLANGE INLET NOT PROVIDED GENERATOR COOLING DN50 PN16 DIN 2633 FLANGE 1912 PARTNER FLANGE OUTLET NOT PROVIDED FUEL INLET DETAIL ON 302 6302 SHEET 7 4598 PARTNER FLANGE 1 1 2 ANSI FLANGE PROVIDED Ej EXCESS FUEL RETURN DETAIL ON 302 6302 SHEET 4598 PARTNER FLANGE 1 1 2 ANSI FLANGE NOT PROVIDED AUXILIARY FUEL PUMP 1 5 16 12 THD 3916 PARTNER FLANGE CONNECTION NOT NEEDED CENTRIFUGE INLET DETAIL 302 6302 SHEET 4379 PARTNER FLANGE 1 1 2 ANSI FLANGE NOT PROVIDED CENTRIFUGE OUTLET DETAIL ON 302 6302 SHEET 2316 PARTNER FLANGE 1 1 2 ANSI FLANGE NOT PROVIDED EXHAUST RIGHT DETAIL ON 302 6302 SHEET 212 PARTNER FLANGE PART 2W 2682 PROVIDED EXHAUST LEFT DETAIL ON 302 6302 SHEET 212 PARTNER FLANGE PART 2W 2682 PROVIDED lt lt CRANKCASE BREATHER FOR 60 3 OD TUBING 1584 800 2574 PARTNER FLANGE OUTLET FRONT NOT NEEDED CRANKCASE BREATHER FOR 60 3 OD TUBING 1584 800 1654 PARTNER FLANGE OUTLET REAR NOT NEEDED NOTE THE DATA IN THIS CHART IS FOR MARKETING GU MARKETING GUIDE IDE USE ONLY METRIG 1E2755 DRAWING AUTOCAD INIPR amp TOL TON EXP PRE PROD I ENGINE MODEL 2
150. OTES LOAD ENGINE POWER 2 bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr FUEL CONSUMPTION NOMINAL g bkw hr FUEL CONSUMPTION 90 CONFIDENCE g bkw hr AIR FLOW 25 101 3 Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE C EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ TO ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 C HEAT REJ EXH LHV 177 NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL 3 6 7 CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL
151. OWN 150 ENGINE JACKET WATER 50 OR OUTLET TEMP ALARM 150 EXHAUST TO TURBO TEMP Bir x 50 OR LEFT 700 EXHAUST TO TURBO TEMP E x lt 50 OR 12 amp 16 CYL ENGINE RIGHT 700 ONLY EXHAUST FROM TURBO 7 x 50 OR TEMP LEFT 700 EXHAUST FROM TURBO ma x lt 50 OR 12 amp 16 ENGINE TEMP RIGHT 700 ONLY CYLINDER TEMPERATURE em 5 lt 50 OR 1 gt 700 CYLINDER TEMPERATURE x lt 50 OR 2 gt 700 CYLINDER TEMPERATURE Bir x 50 OR 3 700 CYLINDER TEMPERATURE x lt 50 OR 4 gt 700 CYLINDER TEMPERATURE x 50 OR 5 gt 700 CYLINDER TEMPERATURE x lt 50 OR 6 gt 700 CYLINDER TEMPERATURE Bim lt 50 OR 18 126 16 CYL ENGINE 7 gt 700 ONLY 2009 Caterpillar All rights reserved CATERPILLAR Signal Shut Setpoint 2009 Caterpillar All rights reserved Sensor Description Type Alarm Down Trip Comments CYLINDER TEMPERATURE Ern lt 50 OR 18 128 16 ENGINE 8 gt 700 ONLY CYLINDER TEMPERATURE me lt 5008 1128 16 ENGINE 9 gt 700 ONLY CYLINDER TEMPERATURE um x lt 50 OR 12 amp 16 ENGINE 10 700 ONLY CYLINDER TEMPERATURE x lt 50 OR 12 amp 16 ENGINE 11 700 ONLY CYLINDER TEMPERATURE Wm lt 50 OR 12 amp 16 ENGINE 12 gt 700 ONLY 2 TEMRERA TURE BIT X E 222 16 CYL ENGINE O
152. PERATURE F 40104 INLET AIR MANIFOLD PRESSURE psi 40105 FUEL TO ENGINE TEMPERATURE F 40106 FUEL TO ENGINE PRESSURE psi 40107 FUEL TO FILTER PRESSURE psi 40108 JACKET WATER OUTLET TEMPERATURE F 40109 REDUNDANT JACKET WATER OUTLET TEMPERATURE F 40110 JACKET WATER PRESSURE psi 40111 AC OC WATER INLET TEMPERATURE F 40112 AC OC PUMP PRESSURE psi 40113 RAW WATER PRESSURE psi 40114 AUXILIARY 1 TEMPERATURE F 40115 AUXILIARY 2 TEMPERATURE F 40116 AUXILIARY 1 4 20mA psi 40117 AUXILIARY 2 4 20mA psi 40118 AIR START PRESSURE psi 40119 NON DRIVE BEARING TEMPERATURE F 40120 DRIVE BEARING TEMPERATURE F 40121 STATOR A TEMPERATURE F 40122 STATOR B TEMPERATURE F 40123 STATOR C TEMPERATURE F 40124 TURBINE INLET LEFT INLINE TEMPERATURE F 40125 TURBINE INLET RIGHT TEMPERATURE F 40126 TURBINE OUTLET LEFT INLINE TEMPERATURE F 40127 TURBINE OUTLET RIGHT TEMPERATURE F 40128 EXHAUST PORT 1 TEMPERATURE F 40129 EXHAUST PORT 2 TEMPERATURE F 40130 EXHAUST PORT 3 TEMPERATURE F 40131 EXHAUST PORT 4 TEMPERATURE F 40132 EXHAUST PORT 5 TEMPERATURE F 40133 EXHAUST PORT 6 TEMPERATURE F 40134 EXHAUST PORT 7 TEMPERATURE F 40135 EXHAUST PORT 8 TEMPERATURE F 40136 EXHAUST PORT 9 TEMPERATURE F 40137 EXHAUST PORT 10 TEMPERATURE F 40138 EXHAUST PORT 11 TEMPERATURE F 40139 EXHAUST PORT 12 TEMPERATURE F 40140 EXHAUST PORT 13 TEMPERATURE F 40141 F F F EXHAUST POR
153. PROJECT GUIDE Fuel System General The fuel system utilizes unit injectors to deliver the correct amount of fuel to the cylinder at the precise moment it is needed enabling the C280 3600 diesel engine to produce maximum power at maximum efficiency with minimum of exhaust emissions Internal Fuel System The main fuel system components are the engine driven transfer pump secondary duplex media type fuel filters 5 micron fuel unit injectors and a fuel backpressure regulator manual fuel priming pump is also available This pump is recommended if no electrical priming pump is available Fuel Transfer Pump The engine driven fuel transfer pump is gear type pump that delivers the fuel through the filters to the injectors The recommended delivery pressure to the injectors is 800 840 kPa 116 to 122 psi at rated load and speed for C280 engines and 430 680 kPa 62 to 99 psi at rated load and speed for 3600 engines The delivery pressure is controlled by adjusting the fuel pressure regulator setting on site during commissioning of the engine The pump is equipped with pump mounted safety valve and the fuel flow at rated rpm is listed in the technical data and varies with engine speed Unit Injectors EUI The fuel unit injectors combine the pumping metering and injecting elements into a single unit mounted in the cylinder head External manifolds supply low pressure fuel from the transfer pump to the cylinder heads High
154. R C RATED ALTITUDE 25 C 150 JACKET WATER OUTLET C ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 100 75 ENGINE POWER 2 bkW GENERATOR POWER 2 ENGINE EFFICIENCY ISO 3046 1 1 ENGINE EFFICIENCY NOMINAL 1 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 1 g bkw hr FUEL CONSUMPTION NOMINAL 1 g bkw hr FUEL CONSUMPTION 90 CONFIDENCE 1 g bkw hr AIR FLOW 25 101 3 Nm3 min IAIR MASS FLOW kg hr COMPRESSOR OUTLET PRESSURE kPa abs COMPRESSOR OUTLET TEMPERATURE C INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr EMISSIONS NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO LHV TO 25 NOMINAL HEAT REJ TO LHV TO 177 NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M AL
155. R EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 100 ENGINE POWER GENERATOR POWER ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL ENGINE DATA FUEL CONSUMPTION ISO 3046 1 1 g bkw hr FUEL CONSUMPTION NOMINAL 1 g bkw hr FUEL CONSUMPTION 90 CONFIDENCE 1 g bkw hr FLOW 25 101 3 Nm3 min AIR MASS FLOW kg hr COMPRESSOR OUTLET PRESSURE kPa abs COMPRESSOR OUTLET TEMPERATURE MANIFOLD PRESSURE 855 MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATUR
156. RATING NOTES LOAD 110 ENGINE POWER 2 bkW IGENERATOR POWER 2 ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL ENGINE DATA FUEL CONSUMPTION ISO 3046 1 g bkw hr FUEL CONSUMPTION NOMINAL g bkw hr FUEL CONSUMPTION 90 CONFIDENCE g bkw hr FLOW 25 101 3 Nm3 min MASS FLOW kg hr ICOMPRESSOR OUTLET PRESSURE kPa abs ICOMPRESSOR OUTLET TEMPERATURE MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr EMISSIONS NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35
157. RATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8410 00 BErecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 12 Tier 2 Technical Data 900 rpm Sheet 2 of 2 C280 12 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 978 076 074 OM 039 067 055 oss 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or
158. RCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7T HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 9 TIMING BASED ON AFM INJECTORS 10 EMMISSION DATA SHOWN ARE NOMINAL VALUES 8 22 2006 DM5455 02 Brecnnicar DATA 2009 Caterpillar All rights reserved CATERPILLAR 3612 Technical Data 1000 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 189 4427 COMPRESSION RATIO FUEL DISTILLATE AFTERCOOLER WATER RATED ALTITUDE 25 200 JACKET WATER OUTLET ASS
159. RELAY SUMMARY GROUP PUN x SHUTDOWN SIGNAL SHUTDOWN GELT ON JACKET WATER DETECTION Digital x RELAY ENGINE SPEED PICKUP DRIVEN ENGINE HOUR METER DIGITAL STARTING PRESSURE METER OHMS RESISTIVE SENSOR SUMMARY ALARM LIGHT DIGITAL X ANY ALARM SUMMARY SHUTDOWN PROTECTIVE LIGHT DIGITAL X SHUTDOWN NO SIGNAL TO RPLCFA DE ENERGIZED PLG FAILURE DIGITALI lt RPLCFA FAILURE ENGINE PRELUBED DIGITAL gt 9 kPa 2009 Caterpillar All rights reserved CATERPILLAR MODBUS Address List ANALOG DATA MODBUS ADDRESS FUEL RACK POSITION 40001 LUBE OIL TO ENGINE TEMPERATURE C 40002 LUBE OIL TO ENGINE PRESSURE kPa 40003 LUBE OIL TO FILTER PRESSURE kPa 40004 INLET AIR MANIFOLD TEMPERATURE C 40005 INLET AIR MANIFOLD PRESSURE kPa 40006 FUEL TO ENGINE TEMPERATURE C 40007 FUEL TO ENGINE PRESSURE kPa 40008 FUEL TO FILTER PRESSURE kPa 40009 JACKET WATER OUTLET TEMPERATURE C 40010 REDUNDANT JACKET WATER OUTLET TEMPERATURE C 40011 JACKET WATER PRESSURE kPa 40012 AC OC WATER INLET TEMPERATURE C 40013 AC OC PUMP PRESSURE kPa 40014 RAW WATER PRESSURE kPa 40015 AUXILIARY 1 TEMPERATURE C 40016 AUXILIARY 2 TEMPERATURE C 40017 AUXILIARY 1 4 20mA kPa 40018 AUXILIARY 2 4 20mA kPa 40019 AIR START PRESSURE kPa 40020 NON DRIVE BEARING TEMPERATURE C 40021 DRIVE BEARING TEMPERATURE C 40022 STATOR A TEMPER
160. ROLEUM OFFSHORE PROJECT GUIDE s FTN de zd 2S 298 3385 967 5 PISTON CONNECTING ROD SHIPPING WEIGHT 19 1 kg SHIPPING WEIGHT 352 kg SHIPPING WEIGHT 56 2 kg 1 6 400 280 d CYLINDER LINER PISTON RING CYLINDER HEAD ASSEMBLE SHIPPING WEIGHT 127 9 kg SHIPPING WEIGHT 3 kg SHIPPING WEIGHT 235 kg r 300 Er 179 TES Be I 3924 DE CAMSHAFT SEGMENT CAM JOURNAL VALVE SHIPPING WEIGHT 30 0 kg SHIPPING WEIGHT 13 6 kg SHIPPING WEIGHT 1 4 kg 8 5 Lu 3 Lect dh wem 2 5 825 SS CONNECTING RO ARING CAM BEARING MAIN GRANKSHAETBEARING SPPN Pee Fa Ko ge 1 4 k SHIPPING WEIGHT 4 5 KG 2 ds wu P 9 ETTEN Z he s 5 T ay 2 S H IN 1 Es AR GR CLP 7 D OE 1 ere ky PROS gt b 1 e ers SF El 4 2 V 7 F Nr i 2 437 7 bk 1 0 434 3 55 504 3 55 CAMSHAFT DRIVE GEAR IDLER GEAR CRANKSHAFT GEAR SHIPPING WEIGHT 43 5 kg SHIPPING WEIGHT 35 4 kg
161. S This table shows the deration required for various air inlet temperatures and altitudes Use this information to help determine actual engine power for your Site The total deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 C and 150 m altitude To maintain a constant air inlet manifold temperature as the air to turbo temperature goes up so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 9696 generator power engine power x 0 96 If the actual generator is less than 9696 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 1 19 2007 DM8402 00 2009 Caterpillar rights reserved
162. S NOMINAL DATA NOx as NO THC molecular weight of 13 018 NOx as NO CO THC molecular weight of 13 018 Particulates g bkW hr g bkW hr g bkW hr g bkW hr bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ ATMOSPHERE HEAT REJ TO OIL COOLER NOMINAL NOMINAL NOMINAL HEAT REJ TO EXH LHV TO 25 C NOMINAL HEAT REJ TO EXH LHV TO 177 C NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 4 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO LUBE OIL TOL
163. S FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 1096 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water TIMING BASED ON AFM INJECTORS 0 EMMISSION DATA SHOWN ARE NOMINAL VALUES 9 1 5 23 2003 DM5510 02 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 3616 Technical Data 900 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 175 6670 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER RATED ALTITUDE 25 200 JACKET WATER OUTLET ASSUMED GENERATO
164. SSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD DRY MEAN PISTON SPEED m s 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD 110 100 75 ENGINE POWER bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL FUEL CONSUMPTION ISO 3046 1 g bkw hr 195 4 FUEL CONSUMPTION NOMINAL g bkw hr 199 2 FUEL CONSUMPTION 90 CONFIDENCE g bkw hr 201 4 FLOW 25 101 3 Nm3 min 181 2 AIR MASS FLOW kg hr 12129 INLET MANIFOLD PRESSURE kPa abs 357 8 INLET MANIFOLD TEMPERATURE 42 2 EXHAUST STACK TEMPERATURE 382 3 EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min 394 4 EXHAUST GAS MASS FLOW kg hr 12510 EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV HEAT REJ TO JACKET WATER HEAT REJ TO ATMOSPHERE HEAT REJ TO OIL COOLER HEAT REJ TO LHV 25 HEAT REJ TO EXH LHV TO 177 HEAT REJ TO AFTERCOOLER CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE
165. T REMOTE INPUT CUSTOMER CONTACT CUSTOMER SUPPLIED CLOSE CONTACT CONTACT CUSTOMER SUPPLIED CLOSE CONTACT CONTACT CUSTOMER SUPPLIED CLOSE CONTACT REMOTE ENGINE START DIGITAL REMOTE ENGINE STOP DIGITAL REMOTE EMERGENCY STOP DIGITAL MARINE GEAR PRESSURE SHUTDOWN GEAR LOW OIL PRESSURE BIT X CUSTOMER CUSTOMER SUPPLIED SWITCH DEFINED CONTACT TEMPERATURE ALARM SHUTDOWNS ENGINE PROTECTION CONTACT CUSTOMER SUPPLIED OVERRIDE CLOSE CONTACT PRESSURE ALARMS SHUTDOWNS ENGINE LOW OIL PRESSURE BIT X 105kPa LOW SPEED SHUTDOWN HIGH SPEED ENGINE LOW OIL PRESSURE BIT X 260 KPa TEM 120 kPa 320 LOW SPEED HIGH ENGINE LOW OIL PRESSURE BIT X s SEED ENGINE HIGH CRANKCASE PRESSURE BIT X gt 1 LOW AIR STARTING X 750 kPa LOW SEAWATER PRESSURE BIT X 35 kPa lt 20 kPa LOW LOW WATER RPM PRESSURE lt 35 kPa HIGH Z RPM 5 LOW AC OC CIRCUIT WATER ER UE BIT X 35 kPa ENGINE OIL FILTER Z PRESSURE DIFFERENTIAL BIT X gt 70kPa CALC PT 009 PT 040 4 HIGH ENGINE LOW FUEL PRESS her BIT x lt 260 kPa 2 ENGINE FUEL FILTER PRESSURE DIFFERENTIAL BIT X 75kPa CALC PT 011 PT 012 2 ENGINE INLET AIR MANIFOLD g 51 BIT X 230 kPa T z 2 109 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Signal Shut S
166. T 14 TEMPERATURE F 40142 EXHAUST PORT 15 TEMPERATURE F 40143 EXHAUST PORT 16 TEMPERATURE 40144 WRITE SPARE 40145 WRITE SPARE 40146 WRITE SPARE 40147 WRITE SPARE 40148 ANV ONIYOLINOW ANIONGA 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA MODBUS ADDRESS EXHAUST PORT 1 TEMPERATURE DEVIATION F 40149 EXHAUST PORT 2 TEMPERATURE DEVIATION F 40150 EXHAUST PORT 3 TEMPERATURE DEVIATION F 40151 EXHAUST PORT 4 TEMPERATURE DEVIATION F 40152 EXHAUST PORT 5 TEMPERATURE DEVIATION F 40153 EXHAUST PORT 6 TEMPERATURE DEVIATION 40154 EXHAUST PORT 7 TEMPERATURE DEVIATION F 40155 EXHAUST PORT 8 TEMPERATURE DEVIATION F 40156 EXHAUST PORT 9 TEMPERATURE DEVIATION F 40157 EXHAUST PORT 10 TEMPERATURE DEVIATION 40158 EXHAUST PORT 11 TEMPERATURE DEVIATION F 40159 EXHAUST PORT 12 TEMPERATURE DEVIATION 40160 EXHAUST PORT 13 TEMPERATURE DEVIATION F 40161 EXHAUST PORT 14 TEMPERATURE DEVIATION 40162 EXHAUST PORT 15 TEMPERATURE DEVIATION 40163 EXHAUST PORT 16 TEMPERATURE DEVIATION 40164 WRITE SPARE 40165 WRITE SPARE 40166 WRITE SPARE 40167 WRITE SPARE 40168 FUEL FILTER PRESSURE DIFFERENTIAL psi 40169 LUBE OIL FILTER PRESSURE DIFFERENTIAL psi 40170 WRITE SPARE 40171 WRITE SPARE 40172 WRITE SPARE 40173 WRITE SPARE 40174 WRITE SPARE 40175 WRITE SPARE 40176 WRITE SPARE 40177 WRITE SPARE 40178 WRITE SPARE 40179 WRITE
167. TDOWN ACKNOWLEDGED LOW SPEED LOW OIL PRESSURE SHUTDOWN LOW SPEED LOW OIL PRESSURE SHUTDOWN ACKNOWLEDGED HIGH SPEED LOW OIL PRESSURE SHUTDOWN HIGH SPEED LOW OIL PRESSURE SHUTDOWN ACKNOWLEDGED AUXILIARY 1 SHUTDOWN AUXILIARY 1 SHUTDOWN ACKNOWLEDGED AUXILIARY 2 SHUTDOWN AUXILIARY 2 SHUTDOWN ACKNOWLEDGED CUSTOMER SHUTDOWN CUSTOMER SHUTDOWN ACKNOWLEDGED EMERGENCY STOP SHUTDOWN EMERGENCY STOP SHUTDOWN ACKNOWLEDGED 02009 Caterpillar amp rights reserved MODBUS ADDRESS 40269 40269 01 40269 02 40269 03 40269 04 40269 05 40269 06 40269 07 40269 08 40269 09 40269 10 40269 11 40269 12 40269 13 40269 14 40269 15 40269 16 40270 40270 01 40270 02 40270 03 40270 04 40270 05 40270 06 40270 07 40270 08 40270 09 40270 10 40270 11 40270 12 40270 13 40270 14 40270 15 40270 16 40271 40271 01 40271 02 40271 03 40271 04 40271 05 40271 06 40271 07 40271 08 40271 09 40271 10 40271 11 40271 12 40271 13 40271 14 40271 15 40271 16 CATERPILLAR MODBUS ADDRESS 40272 40273 40274 40275 40276 40277 40278 40279 40280 40281 40282 40283 40284 40285 40286 40287 40288 40289 40290 40291 40292 40293 40294 40295 40296 40297 40298 40299 40300 40301 ACKNOWLEDGE ALL SIGNAL FROM MODBUS SCADA 40301 01 SPARE 40301 02 SPARE 40301 03 SPARE 40301 04 SPARE 40301 05 SPARE 40301 06 SPARE 40301 07 SPARE 40301 08 SPARE 40301 09 SPARE 40301 10 SPARE 40301 11 SPARE 40301 12 SPARE 40301 1
168. TITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 API 16 C FUEL HAVING A LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water TIMING BASED ON AFM INJECTORS 0 EMMISSION DATA SHOWN ARE NOMINAL VALUES 9 1 5 22 2003 DM5430 05 DATA 2009 Caterpillar All rights reserved CATERPILLAR 3608 Technical Data 1000 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 200 8031 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER C RATED ALTITUDE 25 C 200 JACKET WATER OUTLET C ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANI
169. TITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVES FOR APPLICATIONS ABOVE MAXIMUM RATED ALTITUDE AND OR TEMPERATURE PERFORMANCE AND FUEL CONSUMPTION ARE BASED ON 35 16 FUEL HAVING LOWER HEATING VALUE OF 42 780 KJ KG USED AT 29 C WITH A DENSITY OF 838 9 G LITER NOTES 1 FUEL CONSUMPTION TOLERANCE ISO 3046 1 IS 0 5 OF FULL LOAD DATA NOMINAL IS 3 OF FULL LOAD DATA 2 ENGINE POWER TOLERANCE IS 3 OF FULL LOAD DATA 3 EMISSION DATA SHOWN ARE NOT TO EXCEED VALUES 4 HEAT REJECTION TO JACKET WATER AND EXHAUST TOLERANCE IS 10 OF FULL LOAD DATA heat rate based on treated water 5 HEAT REJECTION TO ATMOSPHERE TOLERANCE IS 50 OF FULL LOAD DATA heat rate based on treated water 6 HEAT REJECTION TO LUBE OIL TOLERANCE IS 20 OF FULL LOAD DATA heat rate based on treated water 7 HEAT REJECTION TO AFTERCOOLER TOLERANCE IS 5 OF FULL LOAD DATA heat rate based on treated water 8 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water TIMING BASED ON AFM INJECTORS 0 EMMISSION DATA SHOWN ARE NOMINAL VALUES 9 1 8 22 2006 DM5427 02 Wrecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR 3606 Technical Data 1000 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 189 4427 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER C RATED ALTITUDE 25 C 200 JACKET W
170. UEL TYPE DISTILLATE AFTERCOOLER WATER C 32 RATED ALTITUDE 25 C 150 JACKET WATER OUTLET C 90 ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD DRY MEAN PISTON SPEED m s 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD 110 100 75 ENGINE POWER bkW GENERATOR POWER BMEP ENGINE EFFICIENCY ISO 3046 1 ENGINE EFFICIENCY NOMINAL FUEL CONSUMPTION ISO 3046 1 g bkw hr 188 4 190 5 FUEL CONSUMPTION NOMINAL g bkw hr 192 1 194 2 FUEL CONSUMPTION 90 CONFIDENCE g bkw hr 194 3 196 7 FLOW 25 101 3 kPaa Nm3 min 239 1 173 0 MASS FLOW kg hr 16004 11576 INLET MANIFOLD PRESSURE kPa abs 358 2 259 8 INLET MANIFOLD TEMPERATURE C 34 5 33 5 EXHAUST STACK TEMPERATURE 361 8 400 9 EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min 503 8 387 4 EXHAUST GAS MASS FLOW kg hr 16492 11946 EMISSIONS NOT TO EXCEED DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr EMISSIONS NOMINAL DATA NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr ENERGY BALANCE DATA FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV TO 25 NOMINAL HEAT REJ TO LHV TO 177 NOMINAL HEAT REJ TO
171. UMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD RATING NOTES LOAD 110 100 75 ENGINE POWER 4466 4060 3045 GENERATOR POWER 4268 3880 2910 ENGINE EFFICIENCY ISO 3046 1 40 8 41 4 41 5 ENGINE EFFICIENCY NOMINAL 39 6 40 2 40 2 ENGINE DATA FUEL CONSUMPTION ISO 3046 1 1 g bkw hr FUEL CONSUMPTION NOMINAL 1 g bkw hr FUEL CONSUMPTION 90 CONFIDENCE 1 g bkw hr FLOW 25 101 3 Nm3 min AIR MASS FLOW kg hr COMPRESSOR OUTLET PRESSURE kPa abs COMPRESSOR OUTLET TEMPERATURE MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE TIMING BTDC EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr NOx as NO g bkW hr CO g bkW hr THC molecular weight of 13 018 g bkW hr Particulates g bkW hr FUEL INPUT ENERGY LHV NOMINAL HEAT REJ TO JACKET WATER NOMINAL HEAT REJ TO ATMOSPHERE NOMINAL HEAT REJ TO OIL COOLER NOMINAL HEAT REJ TO EXH LHV 25 NOMINAL HEAT REJ TO EXH LHV TO 177 NOMINAL HEAT REJ TO AFTERCOOLER NOMINAL CONDITIONS AND DEFINITIONS ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046 1 AND SAE J1995 JAN90 STANDARD REFERENCE CONDITIONS OF 25 100 kPa 30 RELATIVE HUMIDITY AND 150M ALTITUDE AT THE STATED AFTERCOOLER WATER TEMPERATURE CONSULT ALTITUDE CURVE
172. URBINE LEFT INLINE OVERSPEED ALARM ACKNOWLEDGED TURBINE RIGHT OVERSPEED ALARM TURBINE RIGHT OVERSPEED ALARM ACKNOWLEDGED 2009 Caterpillar All rights reserved MODBUS ADDRESS 40260 40260 01 40260 02 40260 03 40260 04 40260 05 40260 06 40260 07 40260 08 40260 09 40260 10 40260 11 40260 12 40260 13 40260 14 40260 15 40260 16 40261 40261 01 40261 02 40261 03 40261 04 40261 05 40261 06 40261 07 40261 08 40261 09 40261 10 40261 11 40261 12 40261 13 40261 14 40261 15 40261 16 40262 40262 01 40262 02 40262 03 40262 04 40262 05 40262 06 40262 07 40262 08 40262 09 40262 10 40262 11 40262 12 40262 13 40262 14 40262 15 40262 16 ANV ONIYOLINOW ANIONGA C280 PETROLEUM OFFSHORE PROJECT GUIDE ANALOG DATA MODBUS ADDRESS ALARM STATUS 40263 BALL HEAD BACKUP MODE ALARM 40263 01 BALL HEAD BACKUP MODE ALARM ACKNOWLEDGED 40263 02 ENGINE CRANK TERMINATE ALARM 40263 03 ENGINE CRANK TERMINATE ALARM ACKNOWLEDGED 40263 04 ENGINE CRANK TERMINATE TIME DELAY ALARM 40263 05 ENGINE CRANK TERMINATE TIME DELAY ALARM ACKNOWLEDGED 40263 06 ENGINE OIL STEP ALARM 40263 07 ENGINE OIL STEP ALARM ACKNOWLEDGED 40263 08 OIL LEVEL LOW ALARM 40263 09 OIL LEVEL LOW ALARM ACKNOWLEDGED 40263 10 PARTICLE DETECTOR ALARM 40263 11 PARTICLE DETECTOR ALARM ACKNOWLEDGED 40263 12 WATER LEVEL LOW ALARM 40263 13 WATER LEVEL LOW ALARM ACKNOWLEDGED 40263 14 JACKET WATER DETECTOR ALARM 40263 15 JACKET WATER DETECTOR
173. XHAUST PORT 6 TEMPERATURE DEVIATION 40058 EXHAUST PORT 7 TEMPERATURE DEVIATION 40059 EXHAUST PORT 8 TEMPERATURE DEVIATION 40060 EXHAUST PORT 9 TEMPERATURE DEVIATION 40061 EXHAUST PORT 10 TEMPERATURE DEVIATION 40062 EXHAUST PORT 11 TEMPERATURE DEVIATION 40063 EXHAUST PORT 12 TEMPERATURE DEVIATION 40064 EXHAUST PORT 13 TEMPERATURE DEVIATION 40065 EXHAUST PORT 14 TEMPERATURE DEVIATION 40066 EXHAUST PORT 15 TEMPERATURE DEVIATION 40067 EXHAUST PORT 16 TEMPERATURE DEVIATION 40068 WRITE SPARE 40069 WRITE SPARE 40070 WRITE SPARE 40071 WRITE SPARE 40072 FUEL FILTER PRESSURE DIFFERENTIAL kPa 40073 LUBE OIL FILTER PRESSURE DIFFERENTIAL kPa 40074 WRITE SPARE 40075 WRITE SPARE 40076 WRITE SPARE 40077 WRITE SPARE 40078 WRITE SPARE 40079 WRITE SPARE 40080 WRITE SPARE 40081 WRITE SPARE 40082 WRITE SPARE 40083 WRITE SPARE 40084 WRITE SPARE 40085 WRITE SPARE 40086 WRITE SPARE 40087 WRITE SPARE 40088 WRITE SPARE 40089 WRITE SPARE 40090 WRITE SPARE 40091 WRITE SPARE 40092 WRITE SPARE 40093 WRITE SPARE 40094 WRITE SPARE 40095 WRITE SPARE 40096 WRITE SPARE 40097 WRITE SPARE 40098 WRITE SPARE 40099 WRITE SPARE 40100 Broene MONITORING AND SHUTDOWN 2009 Caterpillar All rights reserved CATERPILLAR ANALOG DATA MODBUS ADDRESS LUBE OIL TO ENGINE TEMPERATURE F 40101 LUBE OIL TO ENGINE PRESSURE psi 40102 LUBE OIL TO FILTER PRESSURE psi 40103 INLET AIR MANIFOLD TEM
174. YLINDER TEMPERATURE WORD x ors SUNG O 6 C CYLINDER TEMPERATURE 0 700 C 8 12 amp 16 CYL 7 MORD S 2 9500 ENGINE ONLY CYLINDER TEMPERATURE 0 700 C 8 12 amp 16 CYL FOR ENGINE ONLY TEMPERATURE wORD x 0 700 128 16 CYL CYLINDER TEMPERATURE 0 700 C 12 amp 16 CYL gt 10 VERE 522 25000 ENGINE ONLY 02009 Caterpillar amp All rights reserved CATERPILLAR Signal Shut Setpoint Sensor Description Type Alarm Down Trip Comments CYLINDER TEMPERATURE 0 700 12 amp 16 CYL 11 WORD A ENGINE ONLY CYLINDER TEMPERATURE 0 700 12 8 16 CYL 12 WORD ENGINE ONLY CYLINDER TEMPERATURE 0 700 16 CYL ENGINE 13 WORD X gt 550 CYLINDER TEMPERATURE 0 700 16 CYL ENGINE 14 ONLY CYLINDER TEMPERATURE 0 700 16 CYL ENGINE 15 29200 ONLY CYLINDER TEMPERATURE 0 700 16 CYL ENGINE 16 gt 550 ONLY AVG OF EXHAUST PORT TEMP FOR DEVIATION CALC WORD DEDOS CONTROL SENSORS MAG PICK UP ENGINE 113 RATED SD D 4 20mA 0 1200 RPM LUBE OIL PRESSURE TO NES 320kPa 0 1000 kPa ENGINE 120kPa ENGINE HIGH EXHAUST TEMPERATURE FROM 4 20 X gt 630 0 700 TURBO RIGHT SIDE ENGINE HIGH EXHAUST TEMPERATURE FROM 4 20mA X gt 630 0 700 TURBO LEFT SIDE CONTROLLED AT AUX SWITC
175. alve Kit Distillate Fuel Optional Engine Testing e Turbocharger and Crankshaft Work Certificates e Torsional Vibration Analysis of Generator Set e Customer Witness Test e Marine Society Certification Witness Test Optional Service Tools Shipping Protection and Factory Support e Factory Commissioning e Specialized Tooling Group e Turbocharger Tool Group e Cylinder Head Repair Tool Group 2009 Caterpillar rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Protection System Calibrator e Oil Mist Detector Tool Kit e Storage Preservation Optional Literature e Installation Drawings e Additional Literature Set e Additional Parts Book CD e Additional Service Manual e Additional Technical Manual Paper Parts Book English Bons 02009 Caterpillar amp rights reserved CATERPILLAR Technical Data C280 3600 Technical Data Sheets The following Technical Data Sheets represent the latest available 3600 and C280 series technical information at the time of publication and are subject to change Consult with a Caterpillar dealer to obtain the most current data 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 3606 Technical Data 900 rpm DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUX ENGINE SPEED rpm TURBOCHARGER PART 157 5514 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATE
176. anical pump failure The GLM is a prepackaged unit that is typically base mounted but can be remote mounted to suit site specific application requirements The typical GLM package includes e Oil tank e Electric motor driven oil pump e Air operated oil pump e Oil cooler e Oil filter e Flow divider to split oil flow to bearings e Piping valves and fittings on package The redundant GLM air prelube pump is available for black start conditions and will operate in parallel with the engine air prelube pump For generators supplied by others the generator manufacturer is responsible for providing any forced lubrication system that may be required to meet tilt requirements Oil Requirements Due to significant variations in the quality and performance of commercially available lubrication oils Caterpillar recommends the oils listed in the following table for C280 3600 Series Engines that use distillate diesel fuel usrication OIL SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR CAT DEO Diesel Engine Oil for C280 3600 Series Diesel Engines Operating on Distillate Diesel Fuel EG SAE 30 0 C 32 40 C 104 F SAE 40 5 4 50 122 1 DEO Multigrade SAE 15W 40 15 C 5 F 50 C 122 F Lubricant Viscosity The primary recommendation for the C280 3600 family of engines is an SAE 40 grade oil SAE 30 and some multigrade oils may be used if the application requires SAE 30 is prefera
177. arameters Combustion Air System Design Considerations Engine Room Supplied Air The location and design of the engine room air intakes should consider the following 1 The supply air outlets should be close to and directed at the engine turbocharger air intakes 2 Additional air should flow along the engine coupling and reduction gear to absorb the radiated heat 3 The engine room air inlets should be placed such that water or dirt cannot enter A typical combustion air piping system is illustrated on page 85 Separate Combustion Air System Supplying the engines with direct outside air for combustion if possible is beneficial to the installation for a number of reasons It will bring down the air movement in the engine room may reduce the cooling load on the charge air cooler and thus reduce the maximum heating load on the cooling water heat exchanger This in turn will reduce the required sea water circulation in the system Direct air to the turbocharger inlet will provide a bigger margin to the point where engine load reduction is needed due to high air inlet temperatures It would be expected that if the turbocharger inlets are supplied with engine room supplied air a temperature rise above ambient of 5 to 10 C 9 to 18 F AIR SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR would take place By supplying the engines with direct outside air the vessel will also save on the required fan work
178. are intended to compensate for thermal growth and movement of the engine The exhaust system structure immediately after the engine exhaust bellows must be a fixed rigid point The supplied exhaust bellows will only handle the engine movement and thermal growth No additional external loading is allowed on the turbochargers Exhaust Slobber Extended Periods of Low Load Prolonged low load operation should be followed by periodic operation at higher load to burn out exhaust deposits Low load operation is below 400 kPa bmep 58 psi bmep approximately 2096 load depending on rating The engine should be operated above 800 kPa bmep 116 psi bmep about 4096 load depending on rating periodically to burn out the exhaust deposits The 3600 C280 engine can be run well over 24 hours SYSTEM 2009 Caterpillar rights reserved CATERPILLAR before exhaust slobber becomes significant The amount of additional time depends upon the engine configuration water temperature to the aftercooler inlet air temperature to the engine and type of fuel Exhaust Piping A common exhaust system for multiple installations is not acceptable An exhaust system combined with other engines allows operating engines to force exhaust gases into engines not operating The water vapor condenses in the cold engines and may cause engine damage Additionally soot clogs turbochargers aftercoolers and cleaner elements Valves separating engine exhau
179. arter with a mixture of 50 1 E2359 VCI Oil and 50 engine oil All other lubricating oil compartments are to be protected by 1E2359 VCI Oil by one of the following methods Run engine for the final to 5 minutes with oil which has to 4 of 1 E2359 VCI Oil by volume This oil may be drained or left in the engine Seal VCI vapors in the engine with covers specified on engineering drawings The vapor phase of the VCI oil evaporates rapidly at engine operating conditions If further instructions are needed consult with the Engineering Materials Section of the Engine Division e Install a mixture of 50 1 E2359 VCI Oil and 50 engine oil in the lubricating oil compartments at the rate of 1 part of mixture per 15 parts of compartment capacity at full level Seal VCI vapors in the engine with covers specified on engineering drawings This method can be used with an empty or partially filled lubricating oil compartment If the compartment is already full it may be necessary to drain some lubricant to facilitate the addition of the mixture 02009 Caterpillar amp rights reserved CATERPILLAR e Install 30 mL of a mixture of 50 1 E2359 VCI and 50 engine oil in each cylinder and rotate crankshaft two turns Tighten all fittings to the correct torque Check the fuel system to verify that it is full of fuel Install covers specified on engineering drawing to seal in fuel and vapors Spray
180. available with an initial starting air receiver pressure as shown on the curves The starting air receiver size is normally determined by the requirements of the classification society for the number of starts or start attempts The size of the air receivers should be increased if the starting air receiver also supplies air for purposes other than the main engine starting e g engine air prelube work air auxiliary gensets The Caterpillar intermittent air prelube pump consumption rate is 28 2 7 45 gal sec based on free air at 21 C 70 F at 100 kPa 15 psi The pump motor operating pressure is 690 kPa 100 psi With the redundant prelube system and the continuous prelube pump running at startup the pneumatic intermittent prelube pumps for the engine and generator will operate for no longer than 15 seconds For generator sets with pneumatic intermittent prelube pump only the prelube pump will normally operate 1 to 5 minutes before the engine begins to crank AIR SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR Air Tank Sizing for Engines with 1 TDI T109 Starter assuming 5 seconds start 620 kPa Tank Pressure 1400 kPa 1600 kPa Inline Engines Tank Volume m3 0 1 2 3 4 5 6 7 8 9 10 Number of Starts ULV ONLLUVLS 2009 Caterpillar All rights reserved Tank Pressure 1400 kPa 1600 kPa 2000 kPa Number of Starts 2009 Caterpillar
181. ble to multigrade oil Total Base Number TBN 280 3600 engines operating on distillate fuel require TBN of 10 times the sulfur level measured in percent of weight Example For a sulfur content of 1 weight the TBN would be 10 The minimum TBN level regardless of the sulfur content is 5 Excessively high TBN or high ash oils should not be used in C280 3600 Series engines on distillate fuel as these oils may lead to excessive piston deposits and loss of oil control Successful operation of C280 3600 series engines has generally been obtained with new TBN levels between 10 and 15 SAE Ambient Temperature Caterpillar Oil Viscosity TBN Grade 1 3 Use of Commercial Oil Caterpillar does not recommend the names of other commercial brands of lube oils but has established guidelines for their use Commercially available lubrication oils may be used in Caterpillar C280 3600 Series Diesel Engines but they must have proof of performance in Caterpillar s Field Performance Evaluation included in Caterpillar document SEBU7003 3600 Series and C280 Series Diesel Engine Fluids Recommendations Oil Change Interval To achieve maximum life from the engine oil and provide optimum protection for the internal engine components a Scheduled Oil Sampling program S O S should be used This program is available through the Caterpillar dealer network If an S O S analysis program is not available the oil change interval is recommended in accordan
182. bo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 9696 generator power engine power x 0 96 If the actual generator is less than 9696 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5822 02 D TIVOINHOUL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 16 Tier 1 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUXILIARY CERTIFICATION IMO EPA MARINE TIER 1 ENGINE SPEED rpm TURBOCHARGER PART 258 2292 COMPRESSION RATIO FUEL TYPE DISTILLATE AFTERCOOLER WATER 32 RATED ALTITUDE 25 150 JACKET WATER OUTLET 90 ASSUMED GENERATOR EFFICIENCY 96 IGNITION SYSTEM EUI ASSUMED GENERATOR POWER FACTOR 0 8 EXHAUST MANIFOLD DRY MEAN PISTON SPEED m s 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING N
183. ce with the following table Oil Change Intervals for C280 3600 Series Diesel Engines Operating on Distillate Diesel Fuel Engine Model Lube Oil Capacity Oil Change Interval C280 6 3606 880 L 229 US gal 1400 Service Hours C280 8 3608 1112 L 289 US gal 1350 Service Hours C280 12 3612 1302 L 339 US gal 1000 Service Hours C280 16 3616 1677 L 443 US gal 1000 Service Hours 02009 Caterpillar amp rights reserved TIO NOLLVOIYUYNT 280 PETROLEUM OFFSHORE PROJECT GUIDE Scheduled Oil Sampling TBN viscosity and oil consumption trends must be analyzed every 250 hours The 5 5 analysis involves two part test program A Wear Analysis The Wear Analysis identifies engine wear elements present in the oil These elements indicate the condition of the engine B Oil Condition Analysis The Oil Condition Analysis identifies the wear status of the oil The program will determine oil change intervals based on trend analysis and condemning limits established for the engine Increasing Oil Change Intervals Oil change intervals can only be increased when the S O S analysis indicates that the condemning limits have not been reached and only when trend lines indicate a stable constant slope Oil change intervals should only be increased in 250 hour increments especially in situations where the turn around time for the oil analysis is long Change Interval without Oil Analysis Results I
184. cluding previous successful installations the designer s experience and the basic dimensions of the specific package being installed C280 3600 packaged generator set weights can vary from 38 900 kg 86 000 Ib for a 6 cylinder low voltage package with air cooling excluding radiator weight up to 95 500 kg 210 000 Ib for a 16 cylinder high voltage package including a plate type heat exchanger cooling system and generator forced lubrication module The generator set foundation must resist vertical horizontal and fore and aft deflection If the engine foundation has too little resistance against deflection it may show up during the alignment of the engines as the mount depressions may be influenced by the combination of foundation deflection and engine forces and may be out of tolerance The generator set foundation must have sufficient rigidity to transmit static and dynamic forces from the package into the foundation Mounting C280 3600 Packaged Offshore Generator Sets are furnished on rigid bases designed by Caterpillar in order to maintain alignment between engine generator and other engine driven equipment and must be mounted on spring isolators unless hard mounting has been approved by Caterpillar General All mounting systems must have provisions for alignment retention collision stops and engine thermal growth General Arrangement Drawings C280 16 Diesel Generator Package General Arrangement Drawings Note These drawing
185. computer This is 14 point 1 dimensional test around the operating genset package to ensure no unusual vibration is occurring on the as built configuration The standard testing also includes the following data as obtained through the data acquisition system Performance Data e Current Phase A e rpm Current Phase Real Power ekW Current Phase C Reactive Power KVAR Average Current Power Factor Pressures kPa e Frequency JW Pump Inlet e Fuel Rate g min e JW Pump Outlet Specific Fuel Consumption g min AC Outlet F Electrical data e Engine Fuel Voltage e Supply Fuel Voltage Oil z e Voltage C A Boost e Average Voltage AC OC Pump In 02009 Caterpillar amp rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE AC OC Pump Out General Information Generator RTD e Customer Name e Stator Phase A e Test Date e Stator Phase B e ESO Number e Stator Phase C Engine Data e Front Bearing e Engine Serial Number e Rear Bearing e Engine Arrangement Temperatures Deg C Model e JW Inlet e Engine e JW Outlet e Engine Setting bkW rpm e Oil OTor2T Inlet Manifold Generator Data e AC Outlet e Generator Serial Number e AC OC In e Generator Arrangement e AC OC Out e Volts Phase Hertz e Inlet Fuel 9 ekW e Inlet Air ekVA e Turbocharger Outlet e Power Factor Test Operation Data e Test Cell East or West
186. cussed in the system sections Scope of Supply Caterpillar C280 16 Diesel Generator Package General Technical Data Model Caterpillar C280 16 Diesel D G Package 5060 bkW at 900 rpm prime power IMO EPA Marine Tier 2 4840 ekW 11 000 vac 3 phase 60 hertz Ambient 45 C 113 Air 38 C 100 F water to aftercooler IMO Conditions 45 C 113 F Air 32 C 90 F water to aftercooler Tier 2 TBO Between 36 000 and 40 000 Hours Engine Rating BSFC 166 4 g bkW HR 5 Tolerance ISO No of Cylinders 16 Cylinder Configuration VEE Bore 280mm 11 in Stroke 300mm 11 8 in Compression Ratio Ta Rotation SAE Standard CCW viewed from flywheel end Service Side Optional Left or Right Side Water Connections Optional Left or Right Side Contact Caterpillar for the latest Technical Data Generators Caterpillar C280 3600 Offshore Generator Sets are packaged with free standing two bearing generators matched to the engine output to provide the customer maximum electrical output to meet their requirements as well as marine classification requirements for the application Generator specifications and generator testing requirements will need to be reviewed during the pre sale phase of the project and established prior to order placement Options to be considered should include sub transient reactance needed to meet transient responses required and type of cur
187. d 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 4 12 2006 DM5827 02 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 16 Tier 1 Technical Data 1000 rpm Sheet 1 of 2 Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD FIRING PRESSURE MAXIMUM kPa DIESEL ENGINE TECHNICAL DATA RATING CERTIFICATION TURBOCHARGER PART ft FUEL TYPE RATED ALTITUDE 25
188. d water 7 TOTAL AFTERCOOLER HEAT AFTERCOOLER HEAT X ACHRF heat rate based on treated water 1 19 2007 DM8409 00 BErecusicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 12 Tier 2 Technical Data 1000 rpm Sheet 2 of 2 C280 12 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 091 088 086 083 081 978 076 074 OM 039 067 055 oss 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 4 00 097 054 092 055 086 084 081 076 076 074 071 0 69 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os Love 750 1000 1 250 1 500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 792 552 847 853 843 823 810 785 FROM ENGINE 7M
189. deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5828 02 TIVOINHOUL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 6 Tier 2 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUXILIARY CERTIFICATION IMO EPA MARINE TIER 2 ENGINE SPEED rpm TURBOCHARGER PART 157 5514 COMPRESSION RATIO FUEL TYPE
190. e System Monitoring During the design and installation phase it is important that provisions are made to measure pressure and temperature differentials across major system components This allows accurate documentation of the cooling system during the commissioning procedure Future system problems or component deterioration such as fouling are easier to identify if basic data is available Serviceability Suitable access should be provided for cleaning removal or replacement of all system components Isolation valves should be installed as deemed necessary to facilitate such work SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR System Pressures and Velocities The following pressure and velocity limits apply to C280 3600 series engines Water Pump Pressures Maximum allowable Static Head 145 kPa 21 psi Minimum AC OC Inlet Pressure dynamic 5 kPa 0 7 psi Minimum JW inlet Pressure dynamic 30 kPa 4 psi Minimum Sea Water Inlet Pressure dynamic 5 kPa 0 7 psi Maximum Operating Pressures 500 kPa 73 psi 150 kPa 22 psi Type Specific Engine Cooling Circuits aterpillar Expansion Tanks IJO 9 m X 2 2 D gt o Water Velocities 4 5 m s 15 ft s 2 0 to 2 5 m s 7 to 8 ft s uction Lines Pump Inlet 1 5 m s 5 ft s ow Velocity De aeration Line 0 6 m s 2 ft s Jacket Water and AC OC Pump C280 6 8 and 3606 8 Engines Fresh Water Flow US in Gal
191. e generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5816 02 5 TIVOINHOUL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 12 Tier 1 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM 32 90 EUI RATING CERTIFICATION TURBOCHARGER PART FUEL TYPE RATED ALTITUDE 25 C ASSUMED GENERATOR EFFICIENCY ASSUMED GENERATOR POWER FACTOR MARINE AUXILIARY MARINE TIER 1 157 5514 DISTILLATE 150 96 0 8 EXHAUST MANIFOLD DRY FIRING PRESSURE MAXIMUM kPa 17300 MEAN PISTON SPEED m s 9 RATING NOTES 110 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ISO 3046 1 NOMINAL ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION g bkw hr AIR FLOW 25 C 101 3 kPaa Nm3 min AIR MASS FLOW kg hr INLET MANIFOLD PRESSURE kPa abs INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE C EXHAUST GAS FLOW Stack temp 101 3 kPa m3 min EXHAUST GAS MASS FLOW kg hr ISO 3046 1 NOMINAL 90 CONFIDENCE
192. eat exchanger configuration for either the separate circuit system or combined circuit system must provide coolant temperature at the AC OC pump inlet in accordance with applicable emission requirements and must consider the following 1 Maximum expected ambient temperature 2 Maximum engine power capability rack stop setting 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 3 Maximum expected sea water temperature 4 Expected sea water fouling factor 5 Anticipated coolant composition i e 50 glycol See the technical data section of this project guide for specific heat rejection figures Jacket Water Heaters Jacket water heaters may be required to meet cold starting and load acceptance criteria To provide for the optimum usage of the heater Caterpillar routes the heater water into the top of the cylinder block and exit at the bottom to maintain block temperature Caterpillar offers an optional 15 KW heater for 3606 C280 06 engine installations and 30 kW heater for 3608 C280 08 amp larger engine installations System Pressures Correct cooling system pressure minimizes pump cavitation and increases pump efficiency The combination of static and dynamic pressure heads must meet the pressure criteria listed in the technical data Venting Proper venting is required for all applications Vent lines should be routed to an expansion tank constant upward slop
193. el supply temperature should be less than 40 C 104 F The minimum allowable viscosity of the fuel entering the engine is 1 4 cSt Fuel Coolers The need for fuel coolers is project specific and depends greatly on day tank size and location See the following table for fuel heat rejection data TANA 2009 Caterpillar All rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Fuel Cooler Fuel Flow amp Heat Rejection Fuel Flow to Fuel Heat Engine Rejection L min gal min kW Btu min Rated Speed rpm Engine 1000 41 5 11 0 900 38 0 10 0 1000 41 5 11 0 900 38 0 10 0 1000 78 5 20 7 900 72 0 19 0 20 7 19 0 280 6 3606 280 8 3608 280 12 3612 1000 78 5 20 7 900 72 0 280 16 3616 19 0 Fuel Recommendations The fuels recommended for use in Caterpillar 3600 C280 series diesel engines normally No 2 D diesel fuel and No 2 fuel oil although No 1 grades are also acceptable The following table lists worldwide fuel standards which meet Caterpillar requirements Fuel with CIMAC designation DB commonly referred to as Marine Diesel Oil MDO is an acceptable fuel provided the fuel complies with Caterpillar fuel recommendations SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR Worldwide Fuel Standards Standard Name Description No 1 D and No 2 D ASTM D975 Diesel Fuel Oils American ASTM D
194. eme ambient conditions are expected ULV NOLLSNYNOD 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Combustion Air Piping System A typical combustion air piping system is illustrated below 20 FILTER SHIP LOOSE OPTIONAL f s SKID MOUNTED OR REMOTE 4 EXHAUST GAS m TURBOCHARGER EXHAUST SILENCER 18 OPTIONAL OPTIONAL 3600 32 152 I N INTAKE AIR 2 CHARGE AIR COOLER I 181 Y CONNECTOR SHIP LOOSE SHIP LOOSE 1 TO DRAIN SHIP LOOSE OPTIONAL TURBOCHARGER 1 EXHAUST GAS l AR FILTER SHIP OPTIONAL SKID MOUNTED OR REMOTE M GMS PANEL SKID LIMIT NOTE ALL ITEMS OUTSIDE SKID ARE NOT DEALER SCOPE OF SUPPLY UNLESS OTHERWISE STATED METRIC 1E2733 DRAWING AUTOCAD 1 0013 CONFIDENTIALITY 1 0011 amp TOL lar Yellow custom PROD X ENGINE vocc 280 UNLESS OTHERWISE SPECIFIED FLEXIBLE FITTING DIMENSIONS ARE IN MM sue 1 20 DIMENSIONS W O To ARE BASIC 10 20 THERMOCOUPLE ANOLE sug 3 or 5
195. emperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekW listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 12 2006 DM5810 02 5 TVOINHOMYHL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 8 Tier 1 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset RATING MARINE AUXILIARY CERTIFICATION IMO EPA MARINE TIER 1 ENGINE SPEED rpm 900 TURBOCHARGER PART 258 2292 COMPRESSION RATIO F
196. emperature regulators to provide uniform coolant temperature to the aftercooler oil cooler and cylinder block For the combined circuit system the circuit is externally regulated to provide nominal 32 C 90 F coolant temperature The high temperature jacket water system uses the AC OC outlet water to maintain 90 194 F inlet water to the block For the separate circuit system both the AC OC and jacket water systems are externally regulated using sea water to maintain the required 32 C 90 F AC OC and 90 194 F jacket water temperatures Sea Water Pump customer furnished The seawater pump is typically supplied by the customer because the optionally supplied Caterpillar engine mounted sea water pump does not have sufficient suction capability to lift water from sea level to the engine room on a typical offshore platform Expansion Tanks Expansion tanks are available from Caterpillar as standard options The combined circuit expansion tank is full flow For separate circuit cooling the jacket water expansion tank is full flow and the AC OC expansion tank is a shunt type Heat Exchangers Caterpillar offers heat exchangers of the plate and frame type Heat exchanger sizing and performance depends on emission requirements water flow and temperature differential Control of the sea water velocity must be maintained to avoid erosion problems with the heat exchangers Heat Exchanger Sizing The minimum acceptable h
197. enerator rear bearing temperature Genset only e Generator front bearing temperature Genset only e Generator stator A temperature Genset only e Generator stator B temperature Genset only e Generator stator C temperature Genset only Switches e Jacket water detector e Metal particle detector e Starting oil pressure or detector Thermocouples e Exhaust thermocouples one per cylinder plus inlet to turbine and stack Interfacing The engine is factory equipped with the required sensors needed for the PLC It accepts remote signals for starting interlock stopping and emergency stop All monitored parameters and status are available on DH network An Ethernet connection is available by Custom Quote MODBUS communication is available in optional feature code selection Alarms Pressure e Low oil pressure e High oil filter differential e Low fuel pressure e High fuel filter differential e High inlet air manifold pressure e Low starting air pressure e Low jacket water pressure Low AC OC water pressure e Low raw sea water pressure customer supplied contact Temperature e High lube oil temperature e High inlet air manifold temperature e High fuel temperature 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE High inlet temperature High jacket water outlet temperature High generator rear bearing temperature Genset only High generator fr
198. ent and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 1 19 2007 DM8401 00 TIVOINHOUL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 12 Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD C280 12 Tier 2 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 C ASSUMED GENERATOR EFFICIENCY 96 ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 157 5514 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW kPa ISO 3046 1 NOMINAL 110 4180 4004 2515 43 1 41 8 100 3800 3640 2286 42 7 41 4 75 2850 2730 1715 41 1 39 8 ENGI
199. entilation required for this arrangement 242 3 ES V s 40 400 cfm 0 071 x 0 24 x 20 Ventilation Fans In modern installations except for special applications natural draft ventilation is too bulky for practical consideration Adequate quantities of fresh air are best supplied by powered fan assisted ventilation systems Fan Location Fans are most effective when they withdraw ventilation air from the engine room and exhaust the hot air to the atmosphere However ideal engine room ventilation systems will utilize both supply and exhaust fans This will allow the system designer the maximum amount of control over ventilation air distribution Fan Type Ventilation fans are typically of the vane axial tube axial or propeller type or the centrifugal type squirrel cage blowers The selection of fan type is usually determined by ventilation air volume and pressure requirements and also by space limitations within the engine room When mounting exhaust fans in ventilation air discharge ducts which is the most effective location the fan motors should be mounted outside the direct flow of hot ventilating air for longest motor life The design of centrifugal fans squirrel cage blowers is ideal in this regard but their size relative to the vane axial or tube axial fans sometimes puts them at a disadvantage Fan Sizing Fan sizing involves much more than just selecting a fan that will deliver the air flow volume
200. etpoint Sensor Description Type Alarm Down Trip Comments ENGINE HIGH JACKET E ENGINE HIGH JACKET USE ENGINE HIGH AC OC CIRCUIT WATER BIT X gt 60 TEMPERATURE ENGINE LUBE OIL TEMPERATURE BIG x MER HIGH INLET AIR MANIFOLD TEMPERATURE 2i TO TURBO TEMP 8 TOTURBOTEMP gr 25 16 CYL ENGINE EXHAUST FROM TURBO TEMP LEFT BIT 28575 EXHAUST FROM TURBO 12 amp 16 CYL ENGINE TEMP RIGHT ui 7990 lonty Lene ENDE TEMPERATURE E x uus TENDER TEMPERATURE um mn DE TEMPERATURE pm 7 sma TEMPERATURE x DUE TEMPERATURE Ems i CYLINDER TEMPERATURE Ens um 8 128 16 CYL ENGINE gt 7 CYLINDER TEMPERATURE wa 5 8 126 16 CYL ENGINE CYLINDER TEMPERATURE m gt 50C 12816 CYL ENGINE 5 09 ONLY UNDER TEMPERATURE re 128 16 CYL ENGINE A CYLINDER TEMPERATURE 12 amp 16 CYL ENGINE 2 s BIT X gt 5506 lt UNDER TEMPERATURE 7 SIE 128 16 CYL ENGINE 4 bea TEMPERATURE BIT X gt 550C 16 CYL ENGINE ONLY E acia TEMPERATURE BIT X gt 550C 16 CYL ENGINE ONLY Z 2 TEMPERATURE BIT X gt 550C 16 CYL ENGINE ONLY gt TEMPERATURE BIT X gt 550C 16 CYL ENGINE ONLY Z SWITCHES MISC STATUS 5 CYLINDER 1 gt TEMPERATURE DEVIATION BIT X gt 50 4 AVG
201. f S O S analysis results are not available the initial oil change interval should be used to determine oil change intervals Even though oil sampling results may not be available on the recommended 250 hour intervals oil samples should be analyzed at every oil change period even if the turn around time for the data is long Inclination Capability For offshore applications with tilt requirements the Offshore Generator Sets packaged by Caterpillar utilize a shallow dry sump mounted on the engine which gravity drains into a wet sump that is integral to the base assembly This design allows for a reduced engine room footprint eliminates the need for a second lube oil pump and provides 15 static and 25 dynamic tilt capability Customer Piping Connections Engine Connections Oil Fill and Drain 38 mm 1 1 2 150 ANSI Flange Package Connections Lube Centrifuge Inlet and Outlet Connections 38 mm 1 1 2 in 150 ANSI Flange Lube Oil System Schematic Engine internal and typical external lube oil systems are illustrated on the schematic shown on the following page usrication OIL SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR mmm VENT TO ENGINE SUNP FILTER CHANGE OVER MANUAL VALVE OIL PUMP ORIVEN BY ENGINE X 0 75KW ELECTRIC PRELUBE PUMP AR PRELUBE PUMP VENT TO ENGINE SUMP 480V 36 AC SUPPLY BY YARD
202. hich is 1 1 2 in NPTF For the engines with dual starters supply line should be at least 63 5 mm 2 5 in in diameter If the supply line must be longer than 6 m 20 ft the piping size should be increased to ensure proper starters performance The flexible connection between engine starting line and supply line should be used to prevent vibration induced fatigue pressure reducing valve is required valve with Cv40 should be used to provide sufficient air flow Locate the pressure reducing valve as close to the engine as possible to minimize the air pressure reduction valve supply pipe diameter Bene AIR SYSTEM 02009 Caterpillar amp rights reserved CATERPILLAR Starting Air System Schematic A typical starting air system is illustrated on the following page STARTING AIR SYSTEM With Emergency Air Shutoff and Oil Mist Detector DRAN AR PRESSURE FOR MISCELLANEOUS AR TDOLS FOR MAINTENANCE er 7 BAR sears 2 PRESSURE REDUCING VALVE YARD 30 BAR PRESSURE 3 AIR STARTER SOLENOID Y CAT ENERGENGY SHUT GFF AIR COMPONENTS EMERGENCY SHUT DFF SOLENOID OIL MST DETECTOR COMPONENTS OL NIST DETECTOR CAT 2009 Caterpillar All rights reserved ULV ONLLUVLS 280 PETROLEUM OFFSHORE PROJECT GUIDE Combustion Air System General The aftercooler system is High Performance Air Cooling HPAC system designed in a modular layout The aftercooler inlet
203. ined in the engine room but normally not in excess of 12 7 mm H20 0 5 The excess exhaust ventilation air accomplishes several things t compensates for the thermal expansion of incoming air It creates an in draft to confine heat and odor to the engine room Two Speed Fan Motors Operation in extreme cold weather may require reducing ventilation airflow to avoid uncomfortably cold working conditions in the engine room This can be easily done by providing ventilation fans with two speed 100 and 50 or 67 speeds motors Routing Considerations Correct Ventilation Air Routing is Vital for creating and maintaining the optimum engine room environment required to properly support the operation of Caterpillar engines and packaged units Maintaining recommended air temperatures in the engine room is impossible without proper routing of the ventilation air Fresh air inlets should be located as far from the sources of heat as practical and as high as possible and since heat causes air to rise it should be exhausted from the engine room at the highest point possible preferably directly over the engine Where possible individual exhaust suction points should be located directly above the primary heat sources in order to remove the heat before it has a chance to mix with engine room air and raise the average temperature However it must be noted that this practice will also require that ventilation supply air be properly distrib
204. ing one or two fans for each engine This practice allows for a very simple arrangement requiring minimal ductwork The use of multiple ventilation fans either supply or exhaust will require that air flow between the engines be arranged either by fan placement or by distribution ductwork Figure 6 and Figure 7 show examples of correct and incorrect air flow patterns for multiple engine sites Bor ROOM VENTILATION 02009 Caterpillar amp rights reserved CATERPILLAR Correct Air Flow Louvers To Direct Fiow i MAL EI s Bones ANION 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Exhaust System General 280 3600 engine uses pulse exhaust manifold system The front and rear three cylinders are connected to separate turbine inlets Exhaust System Design Considerations Exhaust Backpressure Limits total C280 3600 exhaust backpressure limit is 254 mm H20 This level was established with an emphasis on low specific fuel consumption and exhaust valve temperatures Therefore to achieve proper performance of the engine the exhaust backpressures must be kept below this limit System backpressure should be measured straight length of the exhaust pipe at least 3 to 5 pipe diameters away from the last size transition from the turbocharger outlet System backpressure measurement is part of the engine commissioning Turbochargers
205. is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 4 1 19 2007 DM8394 00 gt gt gt 2009 Caterpillar rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 6 Tier 2 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENCY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 189 4427 DISTILLATE 150 96 0 8 9 FIRING PRESSURE MAXIMUM kPa 17300 RATING NOTES LOAD bkW ekW kPa ISO 3046 1 NOMINAL 110 2233 2144 2418 42 0 40 8 100 2030 1949 2198 42 1 40 8 75 1523 1462 1649 39 6 38 4 ENGINE POWER GENERATOR POWER BMEP ENGINE EFFICIENCY ENGINE EFFICIENCY ENGINE DATA FUEL CONSUMPTION FUEL CONSUMPTION FUEL CONSUMPTION FLOW 0 259 101 3 AIR MASS FLOW INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW Stack temp 101 3 kPa EXHAUST GAS MASS FLOW EMISSIONS NOT TO EXCEED DATA NOx as NO THC molecular weight of 13
206. ished either air cooled or water cooled Air cooled generators must be included in the ventilation system sizing considerations Water cooled generators are typically sea water cooled and similar to the engine s sea water pump the generator sea water pump will be customer furnished This pump must have sufficient suction capability to lift water from sea level to the engine room on a typical offshore platform Depending on the overall cooling system configuration generator cooling water can be supplied from a separate pump or combined with the engine s sea water pump supply capacity Cooling Water Requirements Water Quality Rust Inhibitors and Antifreeze Maintaining water quality is very important in closed cooling systems Excessive hardness will cause deposits fouling and reduced effectiveness of cooling system SYSTEM 02009 Caterpillar amp All rights reserved CATERPILLAR components Caterpillar has available coolant inhibitor to properly condition the cooling water When using Caterpillar inhibitor the cooling water piping must not be galvanized and aluminum should not be used If the piping is galvanized the zinc will react with the coolant inhibitor and form clogs which will interfere with the system operation Customer Piping Connections Water Maker Supply Return 4 in ANSI Flange Package Connections Package Sea Water Inlet Outlet 6 in ANSI Flange Available in CAT standard ANSI standard or DIN sta
207. kPa PSI Full cooler flow C280 3600 Differential Press kPa PSI Full by pass flow 130 of 91 13 130 of 71 10 C280 3600 Differential Press kPa PSI Full by pass flow 130 of 85 12 130 of 66 9 6 280 6 and 280 8 3606 3608 Separate Circuit Low Temperature Circuit Engine Speed RPM 1000 104 15 900 1 84 12 C280 3600 Differential Press kPa PSI Full cooler flow C280 3600 Differential Press kPa PSI Full by pass flow 130 of 104 15 130 of 84 12 C280 6 and C280 8 3606 and 3608 Separate Circuit High Temperature Circuit Engine Speed RPM SYSTEM C280 3600 Differential Press kPa PSI Full cooler flow 2009 Caterpillar All rights reserved C280 3600 Differential Press kPa PSI Full by pass flow 130 of 99 14 130 of 77 11 CATERPILLAR C280 12 and C280 16 3612 and 3616 Separate Circuit Low Temperature Circuit C280 3600 C280 3600 Engine Speed Differential Press kPa RPM Differential Press kPa PSI PSI Full cooler flow Full by pass flow 130 of 85 12 130 of 66 9 6 C280 12 and C280 16 3612 and 3616 Separate Circuit High Temperature Circuit C280 3600 C280 3600 Engine Speed Differential Press kPa RPM Differential Press kPa PSI PSI Full cooler flow Full by pass flow 130 of 103 15 130 of 81 12 Coolant Temperature Control The C280 3600 engine uses fluid inlet control t
208. l deration factor includes deration due to altitude and ambient temperature and air inlet manifold temperature deration AFTERCOOLER HEAT REJECTION FACTORS Aftercooler heat rejection is given for standard conditions of 25 and 150 altitude To maintain constant air inlet manifold temperature as the air to turbo temperature goes so must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekW listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 1 19 2007 DM8410 00 Boo TVOINHOMYHL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 12 Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM
209. larm annunciation The color monitor has a general overview screen an exhaust screen lube oil screen cooling screen air and fuel screen and an auxiliary screen e The alarms are annunciated with a time amp date stamp Annunciation of all engines shutdowns alarms and status points Start prelube control switch fuel control switch and emergency stop button Selection of local remote control of engine Selection of idle rated control of engine Equipped for remote communication Four 4 20 mA outputs programmable Relay contact signals to the remote monitoring system summary shutdown summary alarm local operation remote engine running PLC failure fuel control and idle rated Engine Sensors All package mounted sensors are wired to a common junction box The following are the different sensor types and their descriptions Contactors Lube oil pressure hi low speed 9 Jacket water pressure AC OC pressure e Start air pressure Crankcase pressure 4 20 mA Transducers Lube oil pressure to filter to engine Fuel pressure to filter to engine e Inlet air manifold pressure Boss 02009 Caterpillar amp rights reserved CATERPILLAR RTD PT100 e Lubricating oil to engine temperature e Inlet air manifold temperature e Fuel to engine temperature AC OC inlet temperature e Jacket water outlet temperature alarm e Jacket water outlet temperature shutdown e G
210. late type J W and AC OC Heat Exchangers Fuel System The fuel system is designed for distillate fuel requiring viscosity ranging from 1 4 cSt to 20 cSt at 38 C 100 F Included Components e Direct Injection System with Electronically C280 or Mechanically 3600 Controlled Unit Injectors 2009 Caterpillar amp rights reserved CATERPILLAR e Fuel Transfer Pump Engine Driven Mounted on Left Hand Side e Duplex Fuel Filters with Service Indicators Engine Mounted Options e Manual Fuel Priming Pump e Duplex Primary Fuel Strainer e Flexible Hoses Custom Attachments e Fuel Cooler Plate Type Mounted on Accessory Module Lube Oil System The Lube Oil System utilizes a custom dry sump base assembly with an integral sump in the base for 15 static and 25 dynamic tilt capability Included Components e Lube Oil Pump Engine Driven e Lube Oil Cooler Shell amp Tube Type Engine Mounted e Thermostatic Valve for Lube Oil Temperature Control e Duplex Oil Filter Engine Mounted e Oil Filler and Dipstick e Priority Valve for Oil Pressure Regulating Crankcase Explosion Relief Valves e Redundant Pre Lube System with Air Driven Intermittent Pre Lube Pump and Electric Motor Driven Continuous Pre Lube Pump e Lube Oil System Options include e Manual Oil Pan Drain Valves Front and rear e Electric oil heater 9 kW for In line engines and 11 kW for Vee engines e Lube Oil System Custom Attachments include
211. lencer air starting motors barring device oil mist detector flywheel and 6 x anti vibration mounts 2009 Caterpillar All rights reserved 0 snon ANV NOLLVANNOY LYASNYD C280 PETROLEUM OFFSHORE PROJECT GUIDE 1610 63 in 9 ENGINE JUNCTION BOX eS FUEL OIL FILTER N i REMOVAL DISTANCE OPENING REQUIREMENT 500 mm lt 24 ind un I b el PE 02 3 615 mm 24 in CAMSHAFT REMOVAL DISTANCE FLYWHEEL REMOVAL DISTANCE 583 mm 25 H f Caterpillar service tool is used 555 mm is required if service tool is not used 3608 ENGINES 8 2095 82 NORMAL LINEAR R D LUBE OIL 2035 8
212. ndard CAT standard weld flanges at every connection point ANSI or DIN can be furnished Cooling System Schematics Typical Combined Circuit and Separate Circuit Cooling Systems are illustrated on the following pages 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE 280 16 COMBINED COOLING SYSTEM 5060 BKW 900 RPM I WATER MAKER LEGEND 1029 KW RR 1 CUSTOMER SUPPLIED PARTS BYPASS CATERPILLAR SUPPLIED PARTS ORIFICE mam mum VALVE OPTIONAL Z 90 HR REG ORIFICE T i 2 95 7 C i 1 ul CYL BLOCK amp HEADS 4 mE OPTIONAL 3 1029 GENERATOR E 27C TEMP RISE t3 5 7 C Las 03 2630 90 0 C 360 L MIN L MIN PUMP JW SEAWATER SEAWATER 9 C REG OUTLET 04 810 OIL COOLER S T4 41 2 C MIX 1 MIX 2 L MIN HEAT REJ 4 511 KW T6 5040 12 TEMP RISE t4 9 2 C 1 INLET AIR TURBO o 0 25 02 1560 L MIN L MIN AFTERCOOLER T5 60 3 C LA LL HEAT REJ H5 1457 TEMP RISE t5 28 3 C
213. needed to meet the cooling air and combustion air requirements determined earlier in this section It requires a basic understanding of fan performance characteristics and ventilation system design parameters Similar to a centrifugal pump a fan operates along a specific fan curve that relates a fan s volume flow rate m min or cfm to pressure rise mm H20 or in H20 constant fan speed Therefore fan selection not only requires that the volume flow rate be known but also that the ventilation distribution system be known in order to estimate the system pressure rise This information allows the optimum fan to be selected from a set of manufacturers fan curves or tables Exhaust Fans Ventilation air exhaust systems should be designed to maintain a slight positive or negative pressure in the engine room depending on the specific application ENGINE ROOM VENTILATION 2009 Caterpillar All rights reserved CATERPILLAR Generally maintaining a slight positive pressure in the engine room is recommended but should normally not exceed 5 mm 0 2 This positive pressure accomplishes several things prevents the ingress of dust and dirt which is especially beneficial for those applications involving engines that draw their combustion air from the engine room It creates an out draft to expel heat and odor from the engine room Some applications require that a slight negative pressure be mainta
214. ngine Family for offshore platform applications is a modern highly efficient IMO certified engine series consisting of in line engines of 6 and 8 cylinders and vee engines of 12 and 16 cylinders These are four stroke non reversible engines rated at speeds from 900 to 1000 rpm and intended for use as generator drivers for offshore platforms The engines are turbocharged charge air cooled and with a direct injection fuel system using unit fuel injectors The use of individual fuel injectors eliminates the need for high pressure piping and provides for an accurate high injection pressure The engine block is a nodular cast iron block The intake plenum runs the full length of the engine providing even air distribution to the cylinders The crankshaft is a pressed forging that is induction hardened A counter weight for each cylinder is bolted to the crankshaft using a robust 3 bolt design Crankshaft end flanges are identical so full power can be taken off from either end The main rod and camshaft bearings are steel backed nickel bonded aluminum with a lead tin overlay copper bonded to the aluminum Experience has shown this produces the best bearing construction available for the longest possible life The connecting rods are forged heat treated and shot peened before machining The special four bolt design allows for an extra large bearing which reduces bearing load and extends bearing life The cylinder liners are high alloy iron casti
215. ngs induction hardened plateau honed and water jacketed over their full length The liners are equipped with an anti polishing ring cuff to avoid piston liner carbonizing and thus improve lube oil control and liner life The pistons are two piece with a steel crown and forged aluminum skirt for excellent strength and durability yet light weight Each piston has four rings two in hardened grooves in the crown and two in the skirt The top compression ring is asymmetrically faced with a chrome ceramic matrix coating to provide extended ring and liner life The two middle rings are taper faced and chrome plated while the lower lube oil control ring is double rail chrome faced with a spring expander Oil is jet sprayed into passageways within the pistons for cooling and lubrication of the piston pin The valve configuration features induction hardened replaceable valve seat inserts Positive rotators on all the valves maintain a uniform temperature and wear pattern across the valve face and seat The exhaust and air inlet valves are both manufactured from Nimonic 80A material Does 02009 Caterpillar amp rights reserved CATERPILLAR Example Diesel Generator Package Scope of Supply The following is a typical scope of supply for an offshore semi submersible drilling rig diesel generator package This is an example only the scope of supply varies with the application to meet specific customer needs based on additional options dis
216. nsiderations Coolant Flow Control The correct coolant flows are obtained by factory installed orifices on the engine combined with proper external circuit resistance set at each site during commissioning either with customer installed orifices or balancing valves although a lockable plug valve is recommended The external circuit resistance setting establishes the total circuit flow by balancing total circuit losses with the characteristic pump performance curves Correct external resistance is very important Too high a resistance will result in reduced flows to the aftercooler and oil cooler and their effectiveness will decrease If there is too low a resistance the fluid velocity limits may be exceeded and cavitation early wear could be the result Note Factory packaged cooling systems eliminate the need for the customer to set external resistance for engine cooling circuits at site Proper flow rates for the engine cooling circuits of a factory packaged cooling system are designed by Caterpillar and tested during the Factory Acceptance Test Listed below are the recommended external resistance maximum pressure drops for C280 3600 engines 02009 Caterpillar amp rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE C280 6 and C280 8 3606 and 3608 Combined Circuit Engine Speed RPM Engine Speed RPM C280 3600 Differential Press kPa PSI Full cooler flow C280 3600 Differential Press
217. o must the heat rejection As altitude increases the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 96 generator power engine power x 0 96 If the actual generator is less than 96 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 1 19 2007 DM8418 00 TIVOINHOUL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 16 Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD C280 16 Tier 2 Technical Data 1000 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENCY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 284 8
218. ont bearing temperature Genset only High generator stator temperature Genset only High generator stator temperature Genset only High generator stator temperature Genset only High individual exhaust port temperature High turbine inlet temperature High exhaust stack temperature High exhaust port deviation temperature Other Low battery voltage e Low oil level Jacket water detection Low coolant level Switch supplied with an expansion tank or customer supplied if an expansion tank is not selected e Metal particle detection Shutdowns Pressure Lowoil pressure High crankcase pressure Temperature High jacket water temperature High lube oil temperature High generator bearing temperature Genset only Other e Metal particle detection Engine overspeed Customer shutdown normally open contact customer supplied Programmable Inputs The customer can wire display and alarm on two customer supplied RTD s and two customer supplied 4 20 mA 0 10 VDC sensors three discrete alarms and three discrete shutdowns Gauges In addition to the 254 mm 10 in color monitor that displays all engine parameters there are three engine mounted gauges and three control panel gauges The three engine mounted gauges are fuel pressure lube oil pressure and inlet air restriction The three control panel gauges include an engine hour meter digital tachometer and a starting ai
219. ost 858 056 083 881 0 78 076 074 071 689 067 065 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M FROM ENGINE m 1010 M 1M 1072 1087 106 3 104 3 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz FREE FIELD EXHAUST NOISE SOUND PRESSURE LEVEL dB A DISTANCE FROM ENGINE M OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz TOTAL DERATION FACTORS This table shows the deration required for various air inlet temperatures and altitudes
220. oup VTC Air Restrict Provides air restriction instrument panel lines for VTC turbocharger Magnetic Pickup 4hole Magnetic Speed Pickup Bracket Bracket provides four locations for the installation of additional magnetic pickups Does not include magnetic pickups Other Equipment in Main Components 9 Integral Sump Base Assembly 9 Vertically Restrained Vibration Isolators for Packaged Diesel Generator Set Torsional Coupling MCS Engine Certificate GL Approved IMO Certificate Engine Lifting Eyes Shipped Loose Accessory Module High Inertia Flywheel with Guard Damper with Guard Electric Barring Device Shrink Wrap Tarpaulin Protection for Transportation and Storage Bons 02009 Caterpillar amp rights reserved CATERPILLAR Other Optional Equipment e Isolator Weld Plates for Connection of Vibration Isolators to Customer Foundation Optional Marine Safety Requirements e Spray Shielding Optional Spare Part Kits Intake and Air System Air Exhaust Common e Exhaust Bellows Kit e Turbo Kit Basic Engine e Basic Engine Kit e Piston Assembly Kit e Cuffed Liner Kit e Bearing Spare parts Kit e Rod Assembly Kit Cylinder Head Head Kit Common e Gasket Cuffed Liner Fuel System Fuel Kit Common e Injector Kit Distillate Fuel Cooling System Cooling System Kit Common Instrumentation e Instrument Kit Distillate Fuel Cylinder Valve Kit e V
221. outside of the engine room via ductwork in which case the combustion air is not a factor in the ventilation system design calculations However many installations require that combustion air be drawn directly from the engine room In these installations combustion air requirements become a significant ventilation system design parameter Engine specific combustion air requirements can be found in the Technical Data section for the specific engine and rating 02009 Caterpillar amp All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Ventilation Air Flow Required ventilation air flow depends on the desired engine room air temperature as well as the cooling air and combustion air requirements outlined above While it is understood that total engine room ventilation air flow must take all equipment and machinery into account the following sections provide means for estimating the air flow required for the successful operation of Caterpillar engines and packages In general changing the air in the engine room every one or two minutes will be adequate if flow routing is proper Provisions should be made by the installer to provide incoming ventilation air 0f 0 1 to 0 2 m min 4 to 8 per installed horsepower This does not include combustion air for the engines Engine Room Temperature A properly designed engine room ventilation system will maintain engine room air temperatures
222. pace UMS ANV ONIYOLINOW NISN 2009 Caterpillar All rights reserved Bone MONITORING AND SHUTDOWN C280 PETROLEUM OFFSHORE PROJECT GUIDE Control and Monitoring System Diagram The standard drawings consist of approximately 24 pages few pages are shown to describe the layout The following drawings and sensor list are for reference only and are not to be used for installation purposes CATERPILLAR SUMMARY ENGINE SPEED SHUTDOWN SUMMARY ALARM CONTROL FAI STARTING AIR PRESSURE SPEED SWITCH FAILURE ENGINE PRELUBE GOVERNOR SPEED CONTROL HORN LAMP DECREASE ICREASE SILENCE TEST LOCAL RUN PRELUBE START TED EMERGENCY STOP SPEED CONTROL gt Z N N 02009 Caterpillar amp rights reserved ENGINE MONITORING AND SHUTDOWN
223. quency kW hours and KVAR hours on the GMS monitor Turbocharger Speed Sensor e Provides two speed sensors one for each turbocharger so turbocharger speed may be monitored Cylinder Pressure Relief Valve e Includes sixteen relief valves e Meets major marine society requirements e Engine mounted in cylinder heads qo 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Automatic combustion chamber pressure relief at marine society specified over pressure level Mechanical Cylinder Pressure Gauge Valve Includes sixteen valves Engine mounted on cylinder heads Accepts mechanical cylinder pressure gauge not included Manual compression release capability when gauge is not installed Software thermal shielding is included Oil Mist Detector Installed on side opposite of service side on rear mounted turbo configurations System required by marine societies for Alarm and Safety Requirements for Unmanned Machinery Space 0 5 under the following conditions o ForDNV An engine rating greater than or equal to 2250 kW or an engine bore size greater than 200 mm o ForABS BV GL LRS RINa An engine rating greater than or equal to 2250 kW or an engine bore size greater than 300 mm Oil Mist Detector Drain Group e Provides oil drain for use with oil mist detector Protection System Components Fuel Temperature Sensor Provides fuel temperature sensor gr
224. r pressure gauge 2009 Caterpillar rights reserved CATERPILLAR Lights Four lights are included on the control panel for displaying prelube status summary alarm summary shutdown and PLC failure Construction Enclosure NEMA 4 IP66 PLC Monitoring System Options AC OC JW Air Start Upgrade Vee e Upgrades AC OC JW and starting air pressure from contactors to 4 20mA transducers Raw Sea Water Pressure Transducer e Adds a raw sea water transducer MODBUS Communications Adds MODBUS card to panel Beacon and Horn e Provides a beacon and horn assembly to panel e Assemblies are shipped loose Single Engine REM Display Monitor e Aremote 254 mm 10 in color PLC display monitor to display all engine parameters and annunciation e The monitor is identical to the one in the face of the standard PLC panel e The unit is shipped loose Cabinet Cooler e Customer mounted air powered cabinet cooler e Includes cooler filter solenoid and thermostat requires 552 to 690 kPa 80 to 110 psig clean dry air e Recommended for applications where ambient air temperature exceeds 50 C 122 F but does not exceed 60 C 140 F Power Monitoring Gen Set e multifunction digital power monitor is shipped loose for installation within the switchgear or generator control panel e The power monitor communicates with the PLC and displays parameters such as voltage current kW KVAR pf fre
225. rent transformers to be mounted and supplied for the project 2009 Caterpillar rights reserved C280 PETROLEUM OFFSHORE PROJECT GUIDE Air Inlet System Included Components Aftercooler Fresh Water Corrosion Resistant Coated Air Side Air Inlet Shutoff Crankcase Breather Top Mounted Turbochargers Rear Mounted Engine Oil Lubricated 90 Air Inlet Elbows with Air Cleaner Adapters Options Air Cleaners Standard Duty Normal Volume with Soot Filters Exhaust System Included Components Dry Gas Tight Exhaust Manifold with soft Manifold Shield Options Outlet Expanders 355 mm 14 in to 457 mm 18 in e Flexible Exhaust Fittings 457 mm 18 in Exhaust Weld Flanges 457 mm 18 in Cooling System Included Components Engine Coolant Water Drains Separate Circuit optional Combined Circuit Cooling System see Cooling System section for description of these systems e Separate Circuit 3 Element Oil Cooler Thermostat Valves 3 Way 90 C 194 F for JW Circuit and 32 C 90 F for AC OC Circuit High Volume Accessory Module Mounted Expansion Tank Fresh Water Pumps Engine Driven JW and AC OC Pumps Options 9 Jacket Water Heater Base Mounted 30 kW Heat Recovery Connections with 3 Way Thermostatic Valve Optional 93 C 199 JW Circuit Thermostats for Heat Recovery Cooling System Custom Attachments Include Accessory Module with P
226. rger 6 cylinder engine and the two turbocharger 12 cylinder engine the turbocharger exhaust outlet is rectangular with an area equivalent to 311 mm 12 in diameter For the single turbocharger 8 cylinder engine and the two turbocharger 16 cylinder engine the turbocharger exhaust outlet is 355 mm 14 in diameter with cast adaptors mounted to each turbocharger to provide a 457 mm 18 in diameter customer connection point 5 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Exhaust Gas Piping System A typical exhaust system arrangement is shown below r 20 FILTER SHIP LOOSE OPTIONAL f s SKID MOUNTED OR REMOTE 4 EXHAUST GAS m TURBOCHARGER EXHAUST SILENCER 18 OPTIONAL OPTIONAL 3600 32 152 I N INTAKE AIR 2 CHARGE AIR COOLER I 181 Y CONNECTOR SHIP LOOSE SHIP LOOSE 1 TO DRAIN SHIP LOOSE OPTIONAL TURBOCHARGER 1 EXHAUST GAS 1 em 522221 EE 1420 lt
227. s are based on the Rear Mounted Turbocharger Option ONILNNON ANV NOLLVANNOT LASNAD l 2009 Caterpillar All rights reserved aL La 756 60 KINO 30N383438 804 38 41815504
228. scussed in detail in the Caterpillar Operation amp Maintenance Manual An additional shipped loose lube oil centrifuge customer mounted off package can be provided to circulate the oil sump in order to extend the oil life Oil Pumps The oil pumps provide more than the required engine oil flow at rated conditions This allows high oil pressure early in the operating speed range and provides flow margin Lube Oil Heaters The Caterpillar lube oil heating system is a package mounted unit that is used in combination with a jacket water heater The typical package includes e Circulating pump Electric oil heater 9 KW for In line engines and 11 kW for Vee engines e Control panel including pump control and temperature control etc Lube oil heaters may be necessary when ambient temperatures are below 10 C 50 F or when quick start capability is required In some applications jacket water heaters in conjunction with continuous prelubrication may satisfy lube oil heating requirements however this method of heating should be carefully considered before ordering B usrication OIL SYSTEM 2009 Caterpillar All rights reserved CATERPILLAR FRONT HOUSING TO PISTON COOLING JETS AT 140 kPa REGULATED BYPASS AT 430 kPa TO MAIN OIL GALLERY TO ENGINE SUMP PCV AT 140 430 kPa RELIEF FLOW AT 1000 kPa MAIN LUBE OIL PUMP DISCHARGE FROM LUBE OIL FILTERS amp COOLERS Prelubrication Prelubrication is
229. ses the turbo charger must work harder to overcome the lower atmospheric pressure This increases the amount of heat that must be removed from the inlet air by the aftercooler Use the aftercooler heat rejection factor to adjust for ambient and altitude conditions Multiply this factor by the dtandard aftercooler heat rejection GENERATOR EFFICIENCY Generator power determined with an assumed generator efficiency of 9696 generator power engine power x 0 96 If the actual generator is less than 9696 and greater than 94 5 the generator power ekWI listed in the technical data can still be achieved The BFSC values must be increased by a factor The factor is a percentage 96 actual generator efficiency SOUND DATA Data determined by methods similar to ISO Standard DIS 8528 10 Accuracy Grade 3 1 19 2007 DM8393 00 TVOINHOMYHL 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE C280 8 Tier 2 Technical Data 900 rpm Sheet 1 of 2 DIESEL ENGINE TECHNICAL DATA Genset ENGINE SPEED rpm COMPRESSION RATIO AFTERCOOLER WATER JACKET WATER OUTLET IGNITION SYSTEM EXHAUST MANIFOLD RATING CERTIFICATION TURBOCHARGER PART ff FUEL TYPE RATED ALTITUDE 0 25 ASSUMED GENERATOR EFFICIENGY ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED m s MARINE AUXILIARY IMO EPA MARINE TIER 2 284 8281 DISTILLATE 150 96 0 8 9 FIRING PRESSURE
230. st systems are also discouraged High temperatures warp valve seats and soot deposit causes leakage The exhaust pipe diameter is based on engine output gas flow and length of pipe and number of bends The maximum gas velocity should not exceed 50 m s 164 ft sec at full load Sharp bends should be avoided and where necessary should have the largest possible radius The minimum radius should be 1 pipe diameters The piping should be as short as possible and insulated The insulation should be protected by mechanical lagging to keep it intact All flexible exhaust fittings should be insulated using removable quilted blankets It is recommended to provide the system with a valve drain arrangement to prevent rainwater from entering the engine during prolonged shutdown periods For testing purposes the exhaust system must have a test port installed after the turbocharger outlet This test port should be a 10 to 13 mm 0 39 to 0 51 in plugged pipe welded to the exhaust piping and of sufficient length to bring it to the outer surface of the insulated piping Exhaust piping must be able to expand and contract It is required that one fixed point be installed directly after the flexible exhaust fitting at the turbocharger outlet This will prevent the transmission of forces resulting from weight thermal expansion or lateral displacement of the external exhaust piping from acting on the turbocharger Engine Piping Connections For the single turbocha
231. t it is inevitable that crankcase emissions will be included in total system emission values In the future ventilating crankcase emissions to the atmosphere will be discouraged or prohibited Current C280 3600 diesel engines still require that crankcase fumes be vented to atmosphere A closed loop on engine crankcase filtration system ingestive system for the C280 3600 series diesel engine is available when requested during the pre sale phase of the project Crankcase Fumes Disposal Do not vent crankcase and integral oil sump fumes into the engine room The oily fumes will have a tendency to clog air filters Crankcase fumes should be discharged directly to the atmosphere through a venting system individual for each engine The engine has breathers located on each cylinder bank on the engine Crankcase fumes vent pipes must be of sufficient size to prevent the build up of excessive backpressure in the crankcase Blow by on a new engine will be approximately 0 02 m hr bkW 0 5 bhp pipes should adequately sized to accommodate worn engine Size vent piping for 0 04 m hr bkW 1 0 ft hr bhp with a maximum of 13 mm H20 0 5 in HO pressure drop in the piping Formulas for calculating backpressure can be found in the Crankcase Ventilation section of the current Application and Installation Guide Loops or low points in a crankcase vent pipe must be avoided to prevent liquid locks from the condensation in the pipe
232. ters Internal Starting Air System The standard vane air starters and turbine starters operate on air inlet pressures from 700 to 1040 kPa 102 to 151 psi These pressures are required at the starter inlet port An air tank pressure below 700 kPa 102 psi will not start the engine because of the pressure drop associated with the air supply lines For initial system evaluation assume a 200 kPa 29 psi pressure drop between the tank and the air starter inlet A pressure regulator available as an option in the pricelist is necessary when the supply pressure exceeds the starter operating pressure The pressure regulator should be set from 700 to 1040 kPa 102 to 151 psi It should have the capacity to flow 300 79 gal sec per starter at regulator inlet pressures above 860 kPa 125 psi regulators with Cv of 40 or higher are recommended The quantity of air required for each start and the size of the air receiver depend upon cranking time and air starter consumption A typical first start at 25 C 77 F ambient will take five to seven seconds Restarts of warm engines normally take place in two to three seconds The control system will shut off the air to the air starters at 170 rpm engine speed At this firing speed the governor is activated to allow fuel to the engine External Starting Air System Design Considerations The charts on the following pages are for typical air receiver sizing The chart shows the number of starts
233. uiring quick start capability TIO NOLLVOIYUNT 02009 Caterpillar amp rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Continuous Prelube System The electric continuous prelube system eliminates the delay of waiting for the completion of the intermittent prelube cycle This system is for immediate starting applications and is typically used in conjunction with jacket water and lube oil heating systems Postlubrication C280 3600 diesel engines have standard postlubrication cycle of 60 seconds that maintains the oil flow after engine shutdown to protect the turbocharger bearings However an engine will not postlube if the Emergency Stop E Stop button is depressed to shutdown the engine Since an oil leak could potentially require the use of the E Stop button the postlube is disabled to stop the flow to a possible leak Since no postlube occurs with the use of the E Stop button it should be used for emergency shutdowns only Generator Bearing Lube Oil System The large generators packaged with C280 3600 Series Offshore Generator Set packages will typically require a forced bearing lubrication system which typically utilizes a mechanical generator driven pump to supply lubrication to both front and rear generator bearings Caterpillar supplies a Generator Lubrication Module GLM for Kato Generators to provide for prelubrication of the generator bearings prior to start up and to operate in the event of the mech
234. usicar DATA 02009 Caterpillar All rights reserved CATERPILLAR C280 8 Tier 1 Technical Data 1000 rpm Sheet 2 of 2 DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ost 858 056 083 881 0 78 076 074 071 689 067 065 082 or 075 070 070 6851 os osr 094 oes oss ost 076 036 087 oss 082 080 or 075 073 070 088 100 087 054 052 089 086 084 081 079 076 074 071 069 0 50 0 88 0 85 0 82 0 80 0 77 0 75 190 100 099 036 09 0st os 078 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 ALTITUDE METERS ABOVE SEA LEVEL AFTERCOOLER HEAT REJECTION FACTORS 50 123 127 130 45 40 35 30 25 110 143 116 119 122 125 128 20 I 105 107 110 1 13 116 119 121 15 i 1 00 102 104 107 110 112 1 15 10 1000 1250 1500 1750 2000 2250 2500 ALTITUDE METERS ABOVE SEA LEVEL FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB A DISTANCE 15M 540 932 501 893 898 508 555 825 745 FROM ENGINE 100 0 M 1110 109 7 106 6 105 8 1073 1050 99 0 910 OVERALL 63 125 250 500 1000 2000 4000 8000 OCTAVE BAND Hz
235. uted around the primary heat sources Avoid ventilation air supply ducts that blow cool air directly toward hot engine components This mixes the hottest air in the engine room with incoming cool air raising the temperature of all the air in the engine room and leaves areas of the engine room with no appreciable ventilation For offshore applications where the potential exists for sea water to be drawn into the ventilation air supply the combustion air should be delivered in a manner that will preclude any sea water from being ingested by the turbochargers through the air intake filters These general routing principles while driven by the same basic principles of heat transfer will vary with the specific application This section discusses the general considerations relating to 1 and 2 engine applications multiple engine 3 applications and several special applications 1 and 2 Engine Applications These applications will generally require smaller engine rooms which may sometimes preclude the use of good routing practices Recommended ventilation systems for these applications presented in order of preference are described below and illustrated in Figure 2 and Figure 3 Bsomvissas ANION 2009 Caterpillar All rights reserved 280 PETROLEUM OFFSHORE PROJECT GUIDE Ventilation Type 1 Ll EXHAUST 4 1 0 LOUVERS Figure 2 Ventilation T
236. y the diesel generator packages must be given consideration in the overall ventilation system design process Sizing Considerations Cooling Air Engine room ventilation air cooling air has two basic purposes e To provide an environment that permits the machinery and equipment to function properly with dependable service life provide an environment in which personnel can work comfortably A small percentage of fuel consumed by an engine is lost to the environment in the form of heat radiated to the surrounding air In addition heat from generator inefficiencies and exhaust piping can easily equal engine radiated heat Any resulting elevated temperatures in the engine room may adversely affect maintenance personnel switchgear and engine or generator set performance The use of insulated exhaust pipes silencer and jacket water pipes will reduce the amount of heat radiated by auxiliary sources Radiated heat from the engines and other machinery in the engine room is absorbed by engine room surfaces Some of the heat is transferred to atmosphere but the remaining radiated heat must be carried away by the ventilation system A system for exhausting ventilation air from the engine room must be included in the ventilation system design The engine s will not be able to carry all of the heated ventilation air from the engine room by way of the exhaust piping Combustion Air In many installations combustion air is drawn from
237. ypes 1 and 2 Preferred Design Outside air is brought into the engine room through a system of ducts These ducts should be routed between engines at floor level and discharge air up at the engines and generators The most economical method is to use a service platform built up around the engines to function as the top of this duct See Figure 5 Ventilation Type 2 9 ER 1 0 Fi EXHAUST FAN INTAKE AIR SERVICE WALKWAY AS u This requires the service platform to be constructed of solid nonskid plate rather than perforated or expanded grating The duct outlet will be the clearance between the decking and oilfield base Ventilation air exhaust fans should be mounted or ducted at the highest point in the engine room They should be directly over heat sources This system provides the best ventilation with the least amount of air required In addition the upward flow of air around the engine serves as shield which minimizes the amount of heat released into the engine room Air temperature in the exhaust air duct will be higher than engine room air temperature Dos ROOM VENTILATION 02009 Caterpillar amp rights reserved CATERPILLAR Ventilation Type 3 Alternate Design If Ventilation Type 1 is not feasible the following method is recommended however it will require approximately 50 more air flow Ventilation Type 3 F 5 INTAKE OUTING LJ EXHAUST c

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