Sheet 1 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 0. DATARELEVAT EGIE DESIG COFIGURATIO 1 Fuelconsuption optiized x 2 16 17 18 8 12 Exhausteissions optiized (liit values see Exhaust Eissions, Chapter 21) Coplies with: "TALuft" (Edition 1986) (Geran cleanair standard) Coplies with: Regulations for stationary power plants in France (arrêté du Juillet 1997) Coplies with: US EPA, regulation for nonroad engines (40 CFR 89 Tier 1 ) Coplies with: US EPA, regulation for nonroad engines (40 CFR 89 Tier 2 ) Engine rated speed switchable (1500/1800 rp) Engine with sequential turbocharging (turbochargers with cutin/cutout control) Engine without sequential turbocharging (turbochargers without cutin/cutout control) x 31 Engine with aircooled charge air x 32 Engine with watercooled charge air (external) 1. POWERRELATED DATA (power ratings are net brake power to ISO 3046) 1 Engine rated speed A rp 1500 3 Mean piston speed /s 7.5 4 Continuous power ISO 3046 (10% overload capability) (design power DI 6280, ISO 8528) A kw 890 5 Fuel stop power ISO 3046 A kw 979 8 9 Mean effective pressure (MEP) (Continuous power ISO 3046) Mean effective pressure (MEP) (Fuel stop power ISO 3046) 2. GEERAL CODITIOS (for axiu power) bar 22.4 bar 24.6 1 Intake air depression (new filter) A bar 15 2 Intake air depression, ax. L bar 50 3 Exhaust back pressure A bar 30 4 Exhaust back pressure, ax. L bar 85 5 Fuel teperature at fuel feed connection R 6 Fuel teperature at fuel feed connection, ax. L 60 3. COSUMPTIO 17 18 19 20 Specific fuel consuption (be) % CP (+ 5 %; E 590; 42.8 MJ/kg) Specific fuel consuption (be) 75 % CP (+ 5 %; E 590; 42.8 MJ/kg) Specific fuel consuption (be) 50 % CP (+ 5 %; E 590; 42.8 MJ/kg) Specific fuel consuption (be) % CP (+ 5 %; E 590; 42.8 MJ/kg) G g/kwh 198 R g/kwh 196 R g/kwh 201 R g/kwh 222 X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 2 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 21 Specific fuel consuption (be) FSP (+ 5 %; E 590; 42.8 MJ/kg) R g/kwh 200 73 oload fuel consuption R kg/h 16 61 62 Lube oil consuption after h of operation (B = fuel consuption per hour) Lube oil consuption after h of operation, ax. (B = fuel consuption per hour) 4. MODELRELATED DATA (basic design) R % of B 0.5 L % of B 1.0 3 Engine with exhaust turbocharger (ETC) and intercooler x 4 Exhaust piping, noncooled x 5 Exhaust piping, liquidcooled 33 Working ethod: fourcycle, diesel, singleacting x 34 Cobustion ethod: direct injection x 36 Cooling syste: conditioned water x 37 Direction of rotation: c.c.w. (facing driving end) x 6 uber of cylinders 16 7 Cylinder configuration: V angle degrees 90 10 Bore 0 11 Stroke 150 12 Displaceent, cylinder liter 1.99 Displaceent, total liter 31.84 14 Copression ratio 16 40 Cylinder heads: singlecylinder x 41 Cylinder liners: wet, replaceable x 24 uber of inlet valves, per cylinder 2 uber of exhaust valves, per cylinder 2 15 uber of turbochargers 2 18 uber of intercoolers 1 28 Standard flywheel housing flange (engine ain PTO) SAE 0 43 Flywheel interface DISC 18" 46 Engine ass diagra, drawing o. 47 Engine ass diagra, drawing o. (cont.) 5. COMBUSTIO AIR / EXHAUST GAS 39 Pressure differential in external airtoair intercooler, ax. L bar 0 8 Chargeair pressure before cylinder CP R bar abs 3.2 27 Chargeair pressure before cylinder FSP R bar abs 3.5 9 Cobustion air volue flow CP R ³/s 1.1 10 Cobustion air volue flow FSP R ³/s 1.2 11 Exhaust volue flow (at exhaust teperature) CP R ³/s 2.95 12 Exhaust volue flow (at exhaust teperature) FSP R ³/s 3. 15 Exhaust teperature after turbocharger CP R 530 16 Exhaust teperature after turbocharger FSP R 535 6. HEAT DISSIPATIO X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 3 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 15 16 Heat dissipated by engine coolant CP with oil heat, without chargeair heat Heat dissipated by engine coolant FSP with oil heat, without chargeair heat R kw 400 26 Chargeair heat dissipation CP R kw 170 27 Chargeair heat dissipation FSP 33 Radiation and convection heat, engine CP R kw 45 34 Radiation and convection heat, engine FSP 7. COOLAT SYSTEM (highteperature circuit) 17 Coolant teperature (at engine outlet to cooling equipent) A 95 20 Coolant teperature after engine, alar R 97 21 Coolant teperature after engine, shutdown L 102 Coolant antifreeze content, ax. L % 50 30 Cooling equipent: coolant flow rate A ³/h 40 35 Coolant pup: inlet pressure, in. L bar 0.4 36 Coolant pup: inlet pressure, ax. L bar 1.52 41 Pressure loss in offengine cooling syste, ax. L bar 0.7 47 48 Breather valve (expansion tank) opening pressure (excess pressure) Breather valve (expansion tank) opening pressure (depression) R bar R bar 49 Pressure in cooling syste, ax. L bar 54 Cooling equipent: height above engine, ax. L 15.2 53 Cooling equipent: operating pressure A bar 2.2 73 74 76 75 Coolant level in expansion tank, below in. alar Coolant level in expansion tank, below in. shutdown 8. COOLAT SYSTEM (lowteperature circuit) Teperature differential between intake air and chargeair coolant before intercooler Teperature differential between intake air and chargeair coolant before intercooler, ax. 10. LUBE OIL SYSTEM L L x A K L K 1 Lube oil operating tep. before engine, fro R 88 2 Lube oil operating tep. before engine, to R 98 5 Lube oil teperature before engine, alar R 6 Lube oil teperature before engine, shutdown L 105 8 Lube oil operating press. bef. engine, fro R bar 5.5 9 Lube oil operating press. bef. engine, to R bar 6.5 10 Lube oil pressure before engine, alar R bar 4.4 11 Lube oil pressure before engine, shutdown L bar 3.9 19 20 Lube oil fine filter (ain circuit): nuber of units Lube oil fine filter (ain circuit): nuber of eleents per unit 1 2 X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 4 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 21 32 1 2 Lube oil fine filter (ain circuit): particle retention Lube oil fine filter (ain circuit): pressure differential, ax. 11. FUEL SYSTEM Fuel pressure at fuel feed connection, in. (when engine is starting) Fuel pressure at fuel feed connection, ax. (when engine is starting) R 0.009 L bar 0.8 L bar 0.3 L bar +0.5 37 Fuel supply flow, ax. R liter/in 10 8 Fuel return flow, ax. R liter/in 4.5 10 Fuel pressure at return connection on engine, ax. L bar 0.5 15 Fuel prefilter: nuber of units A 16 Fuel prefilter: nuber of eleents per unit A 17 Fuel prefilter: particle retention A 18 Fuel fine filter (ain circuit): nuber of units A 1 19 Fuel fine filter (ain circuit): nuber of eleents per unit A 1 20 Fuel fine filter (ain circuit): particle retention A 0.005 21 Fuel fine filter (ain circuit): pressure differential, ax. L bar 1.0 12. GEERAL OPERATIG DATA 1 2 Cold start capability: air teperature (w/o starting aid, w/o preheating) (case A) Additional condition (to case A): engine coolant teperature R 0** R 3 Additional condition (to case A): lube oil teperature R +10** 4 Additional condition (to case A): lube oil viscosity R SAE 30** 9 10 Cold start capability: air teperature (w/o starting aid, w/ preheating) (case C) Additional condition (to case C): engine coolant teperature R 10** R +40** 11 Additional condition (to case C): lube oil teperature R 5** 12 Additional condition (to case C): lube oil viscosity R SAE 10W30 21 Coolant preheating, heater perforance (standard) R kw 4 22 Coolant preheating, preheating teperature (in.) R 32 28 Breakaway torque (without driven achinery) coolant teperature +5 R 770 Breakaway torque (without driven achinery) 30 coolant teperature +40 Cranking torque at firing speed (without driven 29 achinery) coolant teperature +5 Cranking torque at firing speed (without driven 31 achinery) coolant teperature +40 Starting is blocked if the engine coolant teperature is 96 below R 440* R 510* R 405* 0 37 High idling speed, ax. (static) L rp 1660 38 Liit speed for overspeed alar / eergency shutdown L rp 1800 42 Firing speed, fro R rp 43 Firing speed, to R rp 120 X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 5 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 44 Engine coolant teperature before starting fullload operation, recoended in. (for eergency/standby sets with coolant preheating: at least the preheating teperature) L 40 48 Miniu continuous load R % 20 49 50 51 Extended low or noload operation possible (consultation required) Engine ass oent of inertia (without flywheel) Engine ass oent of inertia (with standard flywheel) R kg² 3.73 R kg² 6.55 x 52 Standard flywheel ass oent of inertia R kg² 2.82 69 Speed droop (with electronic governor) adjustable, fro R % 0 70 Speed droop (with electronic governor) adjustable, to R % 5 95 uber of starter ringgear teeth on engine flywheel 118. STARTIG (electric) 12 Starter, rated power (ake DELCO) (standard design) R kw 9.5 2 Starter, rated voltage (standard design) R V= 24 14 Starter, power requireent ax. (ake DELCO) R A 1600 15 Starter, power requireent at firing speed (ake DELCO) R A 800 16 Start attept duration (engine preheated) R s 17 Start attept duration (engine not preheated) R s 18 Start attept duration, ax. L s 6 15. STARTIG (pneuatic/oil pressure starter) 5 Starting air pressure before starter otor, in. R bar 17 6 Starting air pressure before starter otor, ax. R bar 7 Starting air pressure before starter otor, in. L bar 8 Starting air pressure before starter otor, ax. L bar 18 Start attept duration (engine preheated) R s 19 Start attept duration (engine not preheated) R s 20 Start attept duration, ax. L s 21 Air consuption / start attept (engine preheated) R ^3n 0.83 23 24 26 27 28 Starting air tank for 3 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 3 start attepts (ax. 30 bar) (engine preheated) Starting air tank for 6 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 6 start attepts (ax. 30 bar) (engine preheated) Starting air tank for 10 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 10 start attepts (ax. 30 bar) (engine preheated) R liter R liter R liter R liter R liter R liter 16. ICLIATIOS STADARD OIL SYSTEM (ref.: waterline) 15 Longitudinal inclination, continuous ax. driving end down (Option: ax. operating inclinations) L degrees 5 X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 6 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 17 19 Longitudinal inclination, continuous ax. driving end up (Option: ax. operating inclinations) Transverse inclination, continuous ax. (Option: ax. operating inclinations) 18. CAPACITIES L degrees 5 L degrees 10 1 Engine coolant capacity (without cooling equipent) R liter 0 11 Onengine fuel capacity R liter 5 14 20 28 29 9 10 Engine oil capacity, initial filling (standard oil syste) (Option: ax. operating inclinations) Oil change quantity, ax. (standard oil syste) (Option: ax. operating inclinations) Oil pan capacity, dipstick ark in. (standard oil syste) (Option: ax. operating inclinations) Oil pan capacity, dipstick ark ax. (standard oil syste) (Option: ax. operating inclinations) 19. WEIGHTS / DIMESIOS Engine weight, dry (basic engine configuration acc. to scope of supply specification) Engine weight, wet (basic engine configuration acc. to scope of supply specification) 20. FA / FA COOLER R liter 102 R liter 99 L liter 69 L liter 92 R kg 3 R kg 3310 3 Fan, pushertype x 18 Fan arrangeent: vertical above crankshaft x 9 Fan drive: echanical via Vbelt x Fan: speed R rp 19 21 54 22 55 56 57 27 Standard fan cooler, supplied by MTU, design and specific data acc. to case A / B / C (Case A) fan cooler, designed for: abient teperature (Case A) fan cooler, designed for: site altitude, ax. (Case A) fan cooler, designed for: coolant antifreeze content, ax. (Case A) fan: power consuption at 1 bar / Pa duct allowance (Case A) fan: power consuption at 2 bar / 200 Pa duct allowance (Case A) fan: power consuption at 3 bar / 300 Pa duct allowance (Case A) coolingair flow rate at 1 bar / Pa duct allowance A A A % X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 7 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 28 29 (Case A) coolingair flow rate at 2 bar / 200 Pa duct allowance (Case A) coolingair flow rate at 3 bar / 300 Pa duct allowance 58 (Case A) fan: weight R kg 59 (Case A) fan cooler: weight, dry (incl. pipework) R kg 31 (Case A) fan cooler: coolant capacity R liter 32 60 33 61 62 63 38 39 40 (Case B) fan cooler, designed for: abient teperature (Case B) fan cooler, designed for: site altitude, ax. (Case B) fan cooler, designed for: coolant antifreeze content, ax. (Case B) fan: power consuption at 1 bar / Pa duct allowance (Case B) fan: power consuption at 2 bar / 200 Pa duct allowance (Case B) fan: power consuption at 3 bar / 300 Pa duct allowance (Case B) coolingair flow rate at 1 bar / Pa duct allowance (Case B) coolingair flow rate at 2 bar / 200 Pa duct allowance (Case B) coolingair flow rate at 3 bar / 300 Pa duct allowance A A A % 64 (Case B) fan: weight R kg 65 (Case B) fan cooler: weight, dry (incl. pipework) R kg 42 (Case B) fan cooler: coolant capacity R liter 43 66 44 67 68 69 49 (Case C) fan cooler, designed for: abient teperature (Case C) fan cooler, designed for: site altitude, ax. (Case C) fan cooler, designed for: coolant antifreeze content, ax. (Case C) fan: power consuption at 1 bar / Pa duct allowance (Case C) fan: power consuption at 2 bar / 200 Pa duct allowance (Case C) fan: power consuption at 3 bar / 300 Pa duct allowance (Case C) coolingair flow rate at 1 bar / Pa duct allowance A A A % X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 8 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 50 51 (Case C) coolingair flow rate at 2 bar / 200 Pa duct allowance (Case C) coolingair flow rate at 3 bar / 300 Pa duct allowance 70 (Case C) fan: weight R kg 71 (Case C) fan cooler: weight, dry (incl. pipework) R kg 53 (Case C) fan cooler: coolant capacity R liter 21. EXHAUST EMISSIOS 307 308 309 310 366 311 312 3 314 316 317 318 319 320 321 323 141 143 Regulation: "TALuft" (Edition 1986) CP itric oxide (Ox) (5% O2) Regulation: "TALuft" (Edition 1986) CP Carbon onoxide (CO) (5% O2) Regulation: "TALuft" (Edition 1986) CP Unburned hydrocarbons (HC) Regulation: "TALuft" (Edition 1986) CP Dust (5% O2) Regulation: "TALuft" (Edition 1986) CP Foraldehyde (5% O2) Regulation: stationary power plants in France CP itric oxide (Ox) (5% O2) Regulation: stationary power plants in France CP Carbon onoxide (CO) (5% O2) Regulation: stationary power plants in France CP Unburned hydrocarbons (MHC) Regulation: stationary power plants in France CP Dust / particulates (5% O2) (40 CFR 89 Tier 1 ) itric oxide (Ox) (40 CFR 89 Tier 1 ) Carbon onoxide (CO) (40 CFR 89 Tier 1 ) Unburned hydrocarbons (HC) (40 CFR 89 Tier 1 ) Particulates (40 CFR 89 Tier 2 ) itric oxide (Ox) + unburned hydrocarbons (HC) (40 CFR 89 Tier 2 ) Carbon onoxide (CO) (40 CFR 89 Tier 2 ) Particulates Exhaust volue flow, dry CP (standard conditions) Exhaust ass flow CP (reference conditions) G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/kwh G g/kwh G g/kwh G g/kwh G g/kwh G g/kwh G g/kwh R ³/h R kg/h X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"
Sheet 9 of 9 Printout: (yd) 200707 EGIE DATA MTU Project o. Chargeair coolant teperature Rawwater inlet teperature bar 0 144 Residual oxygen content (O2) in dry exhaust CP (standard conditions) R % (vol.) 145 Total cobustion calorific value CP 37 Soke index, BOSCH FSP R 0.3 22. ACOUSTICS 101 201 Exhaust noise, unsilenced CP (freefield soundpressure level Lp, 1 distance, ISO 6798) Exhaust noise, unsilenced CP (sound power level LW, ISO 6798) R db(a) R db(a) 103 203 Exhaust noise, unsilenced FSP (freefield soundpressure level Lp, 1 distance, ISO 6798) Spectru o. Exhaust noise,unsilenced CP (sound power level LW, ISO 6798) Spectru o. 109 209 Engine surface noise with attenuated intake noise (filter) CP (freefield soundpressure level Lp, 1 distance, ISO 6798) Engine surface noise with attenuated intake noise (filter) CP (sound power level LW, ISO 6798) R db(a) R db(a) 111 211 1 Engine surface noise with attenuated intake noise (filter) CP (freefield soundpressure level Lp, 1 distance, ISO 6798) Spectru o. Engine surface noise with attenuated intake noise (filter) CP (sound power level LW, ISO 6798) Spectru o. Structure borne noise at engine ounting brackets in vertical direction above resilient engine ounts CP Spectru o. 129 Test stand ipedance spectru, Diagra o. 0 Test stand ipedance spectru, Diagra o. (cont.) 23. TBO AD LOAD PROFILE (case A) 15 Maintenance schedule o. 16 Maintenance schedule o. (cont.) X = Applicable = ot applicable = ot yet defined value Z = See notes provided after "EGIE DATA"