fbpx
Wikipedia

Brake-specific fuel consumption

Brake-specific fuel consumption (BSFC) is a measure of the fuel efficiency of any prime mover that burns fuel and produces rotational, or shaft power. It is typically used for comparing the efficiency of internal combustion engines with a shaft output.

It is the rate of fuel consumption divided by the power produced. In traditional units, it measures fuel consumption in pounds per hour divided by the brake horsepower, lb/(hp⋅h); in SI units, this corresponds to the inverse of the units of specific energy, kg/J = s2/m2.

It may also be thought of as power-specific fuel consumption, for this reason. BSFC allows the fuel efficiency of different engines to be directly compared.

The term "brake" here as in "brake horsepower" refers to a historical method of measuring torque (see Prony brake).

The BSFC calculation (in metric units)

To calculate BSFC, use the formula

 

where:

  is the fuel consumption rate in grams per second (g/s)
  is the power produced in watts where   (W)
  is the engine speed in radians per second (rad/s)
  is the engine torque in newton metres (N⋅m)

The above values of r,  , and   may be readily measured by instrumentation with an engine mounted in a test stand and a load applied to the running engine. The resulting units of BSFC are grams per joule (g/J)

Commonly BSFC is expressed in units of grams per kilowatt-hour (g/(kW⋅h)). The conversion factor is as follows:

BSFC [g/(kW⋅h)] = BSFC [g/J] × (3.6 × 106)

The conversion between metric and imperial units is:

BSFC [g/(kW⋅h)] = BSFC [lb/(hp⋅h)] × 608.277
BSFC [lb/(hp⋅h)] = BSFC [g/(kW⋅h)] × 0.001644

The relationship between BSFC numbers and efficiency

To calculate the actual efficiency of an engine requires the energy density of the fuel being used.

Different fuels have different energy densities defined by the fuel's heating value. The lower heating value (LHV) is used for internal-combustion-engine-efficiency calculations because the heat at temperatures below 150 °C (300 °F) cannot be put to use.

Some examples of lower heating values for vehicle fuels are:

Certification gasoline = 18,640 BTU/lb (0.01204 kW⋅h/g)
Regular gasoline = 18,917 BTU/lb (0.0122222 kW⋅h/g)
Diesel fuel = 18,500 BTU/lb (0.0119531 kW⋅h/g)

Thus a diesel engine's efficiency = 1/(BSFC × 0.0119531) and a gasoline engine's efficiency = 1/(BSFC × 0.0122225)

The use of BSFC numbers as operating values and as a cycle average statistic

 
BSFC [g/(kW⋅h)] map

Any engine will have different BSFC values at different speeds and loads. For example, a reciprocating engine achieves maximum efficiency when the intake air is unthrottled and the engine is running near its peak torque. The efficiency often reported for a particular engine, however, is not its maximum efficiency but a fuel economy cycle statistical average. For example, the cycle average value of BSFC for a gasoline engine is 322 g/(kW⋅h), translating to an efficiency of 25% (1/(322 × 0.0122225) = 0.2540). Actual efficiency can be lower or higher than the engine’s average due to varying operating conditions. In the case of a production gasoline engine, the most efficient BSFC is approximately 225 g/(kW⋅h), which is equivalent to a thermodynamic efficiency of 36%.

An iso-BSFC map (fuel island plot) of a diesel engine is shown. The sweet spot at 206 BSFC has 40.6% efficiency. The x-axis is rpm; y-axis is BMEP in bar (bmep is proportional to torque)

The significance of BSFC numbers for engine design and class

BSFC numbers change a lot for different engine designs, and compression ratio and power rating. Engines of different classes like diesels and gasoline engines will have very different BSFC numbers, ranging from less than 200 g/(kW⋅h) (diesel at low speed and high torque) to more than 1,000 g/(kW⋅h) (turboprop at low power level).

Examples of values of BSFC for shaft engines

The following table takes values as an example for the specific fuel consumption of several types of engines. For specific engines values can and often do differ from the table values shown below. Energy efficiency is based on a lower heating value of 42.7 MJ/kg (84.3 g/(kW⋅h)) for diesel fuel and jet fuel, 43.9 MJ/kg (82 g/(kW⋅h)) for gasoline.

kW hp Year Engine Type Application lb/(hp⋅h) g/(kW⋅h) efficiency
48 64 1989 Rotax 582 gasoline, 2-stroke Aviation, Ultralight, Eurofly Fire Fox 0.699 425[1] 19.3%
321 431 1987 PW206B/B2 turboshaft Helicopter, EC135 0.553 336[2] 24.4%
427 572 1987 PW207D turboshaft Helicopter, Bell 427 0.537 327[2] 25.1%
500 670 1981 Arrius 2B1/2B1A-1 turboshaft Helicopter, EC135 0.526 320[2] 25.6%
13.1 17.8 1897 Motor 250/400[3] Diesel, four-stroke Stationary industrial Diesel engine 0.533 324 26.2%
820 1,100 1960 PT6C-67C turboshaft Helicopter, AW139 0.490 298[2] 27.5%
515 691 1991 Mazda R26B[4] Wankel, four-rotor Race car, Mazda 787B 0.470 286 28.7%
958 1,285 1989 MTR390 turboshaft Helicopter, Tiger 0.460 280[2] 29.3%
84.5 113.3 1996 Rotax 914 gasoline, turbo Aviation, Light-sport aircraft, WT9 Dynamic 0.454 276[5] 29.7%
88 118 1942 Lycoming O-235-L gasoline Aviation, General aviation, Cessna 152 0.452 275[6] 29.8%
1,770 2,380 1973 GE T700 turboshaft Helicopter, AH-1/UH-60/AH-64 0.433 263[7] 31.1%
3,781 5,071 1995 PW150 turboprop Airliner, Dash 8-400 0.433 263[2] 31.1%
1,799 2,412 1984 RTM322-01/9 turboshaft Helicopter, NH90 0.420 255[2] 32.1%
63 84 1991 GM Saturn I4 engine gasoline Cars, Saturn S-Series 0.411 250[8] 32.8%
150 200 2011 Ford EcoBoost gasoline, turbo Cars, Ford 0.403 245[9] 33.5%
300 400 1961 Lycoming IO-720 gasoline Aviation, General aviation, PAC Fletcher 0.4 243[10] 34.2%
5,600 7,500 1989 GE T408 turboshaft Helicopter, CH-53K 0.4 240[7] 33.7%
7,000 9,400 1986 Rolls-Royce MT7 gas turbine Hovercraft, SSC 0.3998 243.2[11] 34.7%
2,000 2,700 1945 Wright R-3350 Duplex-Cyclone gasoline, turbo-compound Aviation, Commercial aviation; B-29, Constellation, DC-7 0.380 231[12] 35.5%
57 76 2003 Toyota 1NZ-FXE gasoline Car, Toyota Prius 0.370 225[13] 36.4%
8,251 11,065 2005 Europrop TP400 turboprop Airbus A400M 0.350 213[14] 39.6%
550 740 1931 Junkers Jumo 204 diesel two-stroke, turbo Aviation, Commercial aviation, Junkers Ju 86 0.347 211[15] 40%
36,000 48,000 2002 Rolls-Royce Marine Trent turboshaft Marine propulsion 0.340 207[16] 40.7%
2,340 3,140 1949 Napier Nomad Diesel-compound Concept Aircraft engine 0.340 207[17] 40.7%
165 221 2000 Volkswagen 3.3 V8 TDI Diesel Car, Audi A8 0.337 205[18] 41.1%
2,013 2,699 1940 Deutz DZ 710 Diesel two-stroke Concept Aircraft engine 0.330 201[19] 41.9%
42,428 56,897 1993 GE LM6000 turboshaft Marine propulsion, Electricity generation 0.329 200.1[20] 42.1%
130 170 2007 BMW N47 2L Diesel Cars, BMW 0.326 198[21] 42.6%
88 118 1990 Audi 2.5L TDI Diesel Car, Audi 100 0.326 198[22] 42.6%
620 830 Scania AB DC16 078A Diesel 4-stroke Electricity generation 0.312 190[23] 44.4%
1,200 1,600 early 1990s Wärtsilä 6L20 Diesel 4-stroke Marine propulsion 0.311 189.4[24] 44.5%
3,600 4,800 MAN Diesel 6L32/44CR Diesel 4-stroke Marine propulsion, Electricity generation 0.283 172[25] 49%
4,200 5,600 2015 Wärtsilä W31 Diesel 4-stroke Marine propulsion, Electricity generation 0.271 165[26] 51.1%
34,320 46,020 1998 Wärtsilä-Sulzer RTA96-C Diesel 2-stroke Marine propulsion, Electricity generation 0.263 160[27] 52.7%
27,060 36,290 MAN Diesel S80ME-C9.4-TII Diesel 2-stroke Marine propulsion, Electricity generation 0.254 154.5[28] 54.6%
34,350 46,060 MAN Diesel G95ME-C9 Diesel 2-stroke Marine propulsion 0.254 154.5[29] 54.6%
605,000 811,000 2016 General Electric 9HA Combined cycle gas turbine Electricity generation 0.223 135.5 (eq.) 62.2%[30]
640,000 860,000 2021 General Electric 7HA.3 Combined cycle gas turbine Electricity generation (proposed) 0.217 131.9 (eq.) 63.9%[31]

Turboprop efficiency is only good at high power; SFC increases dramatically for approach at low power (30% Pmax) and especially at idle (7% Pmax) :

2,050 kW Pratt & Whitney Canada PW127 turboprop (1996)[32]
Mode Power fuel flow SFC Energy efficiency
Nominal idle (7%) 192 hp (143 kW) 3.06 kg/min (405 lb/h) 1,282 g/(kW⋅h) (2.108 lb/(hp⋅h)) 6.6%
Approach (30%) 825 hp (615 kW) 5.15 kg/min (681 lb/h) 502 g/(kW⋅h) (0.825 lb/(hp⋅h)) 16.8%
Max cruise (78%) 2,132 hp (1,590 kW) 8.28 kg/min (1,095 lb/h) 312 g/(kW⋅h) (0.513 lb/(hp⋅h)) 27%
Max climb (80%) 2,192 hp (1,635 kW) 8.38 kg/min (1,108 lb/h) 308 g/(kW⋅h) (0.506 lb/(hp⋅h)) 27.4%
Max contin. (90%) 2,475 hp (1,846 kW) 9.22 kg/min (1,220 lb/h) 300 g/(kW⋅h) (0.493 lb/(hp⋅h)) 28.1%
Take-off (100%) 2,750 hp (2,050 kW) 9.9 kg/min (1,310 lb/h) 290 g/(kW⋅h) (0.477 lb/(hp⋅h)) 29.1%

See also

References

  1. ^ (PDF). Rotax. Sep 2010. Archived from the original (PDF) on 2017-07-22. Retrieved 2018-06-08.
  2. ^ a b c d e f g (PDF). Aviation Week. January 2008.
  3. ^ Günter Mau: Handbuch Dieselmotoren im Kraftwerks- und Schiffsbetrieb, Vieweg (Springer), Braunschweig/Wiesbaden 1984, ISBN 978-3-528-14889-8, p. 7
  4. ^ Shimizu, Ritsuharu; Tadokoro, Tomoo; Nakanishi, Toru; Funamoto, Junichi (1992-02-01). Mazda 4-Rotor Rotary Engine for the Le Mans 24-Hour Endurance Race. SAE International. p. 4. doi:10.4271/920309. ISSN 0148-7191.
  5. ^ (PDF). Rotax. Apr 2010. Archived from the original (PDF) on 2017-06-11. Retrieved 2018-06-08.
  6. ^ O-235 and O-290 Operator's Manual (PDF), Lycoming, Jan 2007, p. 3-8 version-L
  7. ^ a b Peter deBock (September 18, 2019). GE turbines and small engines overview (PDF). ARPA-e INTEGRATE meeting. Global Research. General Electric.
  8. ^ Michael Soroka (March 26, 2014). "Are Airplane Engines Inefficient?".
  9. ^ "Advanced Gasoline Turbocharged Direct Injection (GTDI) Engine Development" (PDF). Ford Research and Advanced Engineering. May 13, 2011.
  10. ^ IO-720 Operator's Manual (PDF), Lycoming, October 2006, p. 3-8
  11. ^ (PDF). Rolls-Royce. 2012. Archived from the original (PDF) on 2017-04-20. Retrieved 2018-07-09.
  12. ^ Kimble D. McCutcheon (27 October 2014). (PDF). Archived from the original (PDF) on 1 August 2016.
  13. ^ Muta, Koichiro; Yamazaki, Makoto; Tokieda, Junji (8 March 2004). "Development of New-Generation Hybrid System THS II - Drastic Improvement of Power Performance and Fuel Economy". SAE Technical Paper Series. Vol. 1. Society of Automotive Engineers. doi:10.4271/2004-01-0064.
  14. ^ Kaiser, Sascha; Donnerhack, Stefan; Lundbladh, Anders; Seitz, Arne (27–29 July 2015). A composite cycle engine concept with hecto-pressure ratio. AIAA/SAE/ASEE Joint Propulsion Conference (51st ed.). doi:10.2514/6.2015-4028.
  15. ^ inter-action association, 1987
  16. ^ "Marine Trent". Civil Engineering Handbook. 19 Mar 2015.
  17. ^ "Napier Nomad". Flight. 30 April 1954.
  18. ^ "The new Audi A8 3.3 TDI quattro: Top TDI for the luxury class" (Press release). Audi AG. July 10, 2000.
  19. ^ "Jane's Fighting Aircraft of World War II". London, UK: Bracken Books. 1989.
  20. ^ (PDF). General Electric. 2016. Archived from the original (PDF) on 2016-11-19.
  21. ^ "BMW 2.0d (N47)" (in French). Auto-innovations. June 2007.
  22. ^ Stock, Dieter; Bauder, Richard (1 February 1990). "The New Audi 5-Cylinder Turbo Diesel Engine: The First Passenger Car Diesel Engine with Second Generation Direct Injection". SAE Technical Paper Series. Vol. 1. Society of Automotive Engineers. doi:10.4271/900648.
  23. ^ "DC16 078A" (PDF). Scania AB.
  24. ^ "Wärtsilä 20 product guide" (PDF). Wärtsilä. 14 February 2017.
  25. ^ (PDF). Man Diesel. 2015. Archived from the original (PDF) on 2016-04-17.
  26. ^ "The new Wärtsilä 31 engine". Wärtsilä Technical Journal. 20 October 2015.
  27. ^ (PDF). Wärtsilä. 2004. Archived from the original (PDF) on December 26, 2005.
  28. ^ "MAN B&W S80ME-C9.4-TII Project Guide" (PDF). Man Diesel. May 2014.
  29. ^ "MAN B&W G95ME-C9.2-TII Project Guide" (PDF). Man Diesel. May 2014. p. 16.
  30. ^ Tomas Kellner (17 Jun 2016). "Here's Why The Latest Guinness World Record Will Keep France Lit Up Long After Soccer Fans Leave" (Press release). General Electric.
  31. ^ "GE Unveils New H-Class Gas Turbine—and Already Has a First Order". October 2, 2019.
  32. ^ (PDF). Avions de Transport Regional. June 2001. p. PW127F engine gaseous emissions. Archived from the original (PDF) on 2016-08-08.

Further reading

  • HowStuffWorks: How Car Engines Work
  • Reciprocating Engines at infoplease
  • US Centennial of Flight Commission
  • Effect of EGR on the exhaust gas temperature and exhaust opacity in compression ignition engines
  • Heywood J B 1988 Pollutant formation and control. Internal combustion engine fundamentals Int. edn (New York: Mc-Graw Hill) pp 572–577
  • Exemplary maps for commercial car engines collected by ecomodder forum users

brake, specific, fuel, consumption, bsfc, measure, fuel, efficiency, prime, mover, that, burns, fuel, produces, rotational, shaft, power, typically, used, comparing, efficiency, internal, combustion, engines, with, shaft, output, rate, fuel, consumption, divid. Brake specific fuel consumption BSFC is a measure of the fuel efficiency of any prime mover that burns fuel and produces rotational or shaft power It is typically used for comparing the efficiency of internal combustion engines with a shaft output It is the rate of fuel consumption divided by the power produced In traditional units it measures fuel consumption in pounds per hour divided by the brake horsepower lb hp h in SI units this corresponds to the inverse of the units of specific energy kg J s2 m2 It may also be thought of as power specific fuel consumption for this reason BSFC allows the fuel efficiency of different engines to be directly compared The term brake here as in brake horsepower refers to a historical method of measuring torque see Prony brake Contents 1 The BSFC calculation in metric units 2 The relationship between BSFC numbers and efficiency 3 The use of BSFC numbers as operating values and as a cycle average statistic 4 The significance of BSFC numbers for engine design and class 5 Examples of values of BSFC for shaft engines 6 See also 7 References 8 Further readingThe BSFC calculation in metric units EditTo calculate BSFC use the formula B S F C r P displaystyle BSFC frac r P where r displaystyle r is the fuel consumption rate in grams per second g s P displaystyle P is the power produced in watts where P t w displaystyle P tau omega W w displaystyle omega is the engine speed in radians per second rad s t displaystyle tau is the engine torque in newton metres N m dd The above values of r w displaystyle omega and t displaystyle tau may be readily measured by instrumentation with an engine mounted in a test stand and a load applied to the running engine The resulting units of BSFC are grams per joule g J Commonly BSFC is expressed in units of grams per kilowatt hour g kW h The conversion factor is as follows BSFC g kW h BSFC g J 3 6 106 The conversion between metric and imperial units is BSFC g kW h BSFC lb hp h 608 277 BSFC lb hp h BSFC g kW h 0 001644The relationship between BSFC numbers and efficiency EditTo calculate the actual efficiency of an engine requires the energy density of the fuel being used Different fuels have different energy densities defined by the fuel s heating value The lower heating value LHV is used for internal combustion engine efficiency calculations because the heat at temperatures below 150 C 300 F cannot be put to use Some examples of lower heating values for vehicle fuels are Certification gasoline 18 640 BTU lb 0 01204 kW h g Regular gasoline 18 917 BTU lb 0 0122222 kW h g Diesel fuel 18 500 BTU lb 0 0119531 kW h g dd Thus a diesel engine s efficiency 1 BSFC 0 0119531 and a gasoline engine s efficiency 1 BSFC 0 0122225 The use of BSFC numbers as operating values and as a cycle average statistic Edit BSFC g kW h map Main article Consumption map Any engine will have different BSFC values at different speeds and loads For example a reciprocating engine achieves maximum efficiency when the intake air is unthrottled and the engine is running near its peak torque The efficiency often reported for a particular engine however is not its maximum efficiency but a fuel economy cycle statistical average For example the cycle average value of BSFC for a gasoline engine is 322 g kW h translating to an efficiency of 25 1 322 0 0122225 0 2540 Actual efficiency can be lower or higher than the engine s average due to varying operating conditions In the case of a production gasoline engine the most efficient BSFC is approximately 225 g kW h which is equivalent to a thermodynamic efficiency of 36 An iso BSFC map fuel island plot of a diesel engine is shown The sweet spot at 206 BSFC has 40 6 efficiency The x axis is rpm y axis is BMEP in bar bmep is proportional to torque The significance of BSFC numbers for engine design and class EditBSFC numbers change a lot for different engine designs and compression ratio and power rating Engines of different classes like diesels and gasoline engines will have very different BSFC numbers ranging from less than 200 g kW h diesel at low speed and high torque to more than 1 000 g kW h turboprop at low power level Examples of values of BSFC for shaft engines EditThe following table takes values as an example for the specific fuel consumption of several types of engines For specific engines values can and often do differ from the table values shown below Energy efficiency is based on a lower heating value of 42 7 MJ kg 84 3 g kW h for diesel fuel and jet fuel 43 9 MJ kg 82 g kW h for gasoline kW hp Year Engine Type Application lb hp h g kW h efficiency48 64 1989 Rotax 582 gasoline 2 stroke Aviation Ultralight Eurofly Fire Fox 0 699 425 1 19 3 321 431 1987 PW206B B2 turboshaft Helicopter EC135 0 553 336 2 24 4 427 572 1987 PW207D turboshaft Helicopter Bell 427 0 537 327 2 25 1 500 670 1981 Arrius 2B1 2B1A 1 turboshaft Helicopter EC135 0 526 320 2 25 6 13 1 17 8 1897 Motor 250 400 3 Diesel four stroke Stationary industrial Diesel engine 0 533 324 26 2 820 1 100 1960 PT6C 67C turboshaft Helicopter AW139 0 490 298 2 27 5 515 691 1991 Mazda R26B 4 Wankel four rotor Race car Mazda 787B 0 470 286 28 7 958 1 285 1989 MTR390 turboshaft Helicopter Tiger 0 460 280 2 29 3 84 5 113 3 1996 Rotax 914 gasoline turbo Aviation Light sport aircraft WT9 Dynamic 0 454 276 5 29 7 88 118 1942 Lycoming O 235 L gasoline Aviation General aviation Cessna 152 0 452 275 6 29 8 1 770 2 380 1973 GE T700 turboshaft Helicopter AH 1 UH 60 AH 64 0 433 263 7 31 1 3 781 5 071 1995 PW150 turboprop Airliner Dash 8 400 0 433 263 2 31 1 1 799 2 412 1984 RTM322 01 9 turboshaft Helicopter NH90 0 420 255 2 32 1 63 84 1991 GM Saturn I4 engine gasoline Cars Saturn S Series 0 411 250 8 32 8 150 200 2011 Ford EcoBoost gasoline turbo Cars Ford 0 403 245 9 33 5 300 400 1961 Lycoming IO 720 gasoline Aviation General aviation PAC Fletcher 0 4 243 10 34 2 5 600 7 500 1989 GE T408 turboshaft Helicopter CH 53K 0 4 240 7 33 7 7 000 9 400 1986 Rolls Royce MT7 gas turbine Hovercraft SSC 0 3998 243 2 11 34 7 2 000 2 700 1945 Wright R 3350 Duplex Cyclone gasoline turbo compound Aviation Commercial aviation B 29 Constellation DC 7 0 380 231 12 35 5 57 76 2003 Toyota 1NZ FXE gasoline Car Toyota Prius 0 370 225 13 36 4 8 251 11 065 2005 Europrop TP400 turboprop Airbus A400M 0 350 213 14 39 6 550 740 1931 Junkers Jumo 204 diesel two stroke turbo Aviation Commercial aviation Junkers Ju 86 0 347 211 15 40 36 000 48 000 2002 Rolls Royce Marine Trent turboshaft Marine propulsion 0 340 207 16 40 7 2 340 3 140 1949 Napier Nomad Diesel compound Concept Aircraft engine 0 340 207 17 40 7 165 221 2000 Volkswagen 3 3 V8 TDI Diesel Car Audi A8 0 337 205 18 41 1 2 013 2 699 1940 Deutz DZ 710 Diesel two stroke Concept Aircraft engine 0 330 201 19 41 9 42 428 56 897 1993 GE LM6000 turboshaft Marine propulsion Electricity generation 0 329 200 1 20 42 1 130 170 2007 BMW N47 2L Diesel Cars BMW 0 326 198 21 42 6 88 118 1990 Audi 2 5L TDI Diesel Car Audi 100 0 326 198 22 42 6 620 830 Scania AB DC16 078A Diesel 4 stroke Electricity generation 0 312 190 23 44 4 1 200 1 600 early 1990s Wartsila 6L20 Diesel 4 stroke Marine propulsion 0 311 189 4 24 44 5 3 600 4 800 MAN Diesel 6L32 44CR Diesel 4 stroke Marine propulsion Electricity generation 0 283 172 25 49 4 200 5 600 2015 Wartsila W31 Diesel 4 stroke Marine propulsion Electricity generation 0 271 165 26 51 1 34 320 46 020 1998 Wartsila Sulzer RTA96 C Diesel 2 stroke Marine propulsion Electricity generation 0 263 160 27 52 7 27 060 36 290 MAN Diesel S80ME C9 4 TII Diesel 2 stroke Marine propulsion Electricity generation 0 254 154 5 28 54 6 34 350 46 060 MAN Diesel G95ME C9 Diesel 2 stroke Marine propulsion 0 254 154 5 29 54 6 605 000 811 000 2016 General Electric 9HA Combined cycle gas turbine Electricity generation 0 223 135 5 eq 62 2 30 640 000 860 000 2021 General Electric 7HA 3 Combined cycle gas turbine Electricity generation proposed 0 217 131 9 eq 63 9 31 Turboprop efficiency is only good at high power SFC increases dramatically for approach at low power 30 Pmax and especially at idle 7 Pmax 2 050 kW Pratt amp Whitney Canada PW127 turboprop 1996 32 Mode Power fuel flow SFC Energy efficiencyNominal idle 7 192 hp 143 kW 3 06 kg min 405 lb h 1 282 g kW h 2 108 lb hp h 6 6 Approach 30 825 hp 615 kW 5 15 kg min 681 lb h 502 g kW h 0 825 lb hp h 16 8 Max cruise 78 2 132 hp 1 590 kW 8 28 kg min 1 095 lb h 312 g kW h 0 513 lb hp h 27 Max climb 80 2 192 hp 1 635 kW 8 38 kg min 1 108 lb h 308 g kW h 0 506 lb hp h 27 4 Max contin 90 2 475 hp 1 846 kW 9 22 kg min 1 220 lb h 300 g kW h 0 493 lb hp h 28 1 Take off 100 2 750 hp 2 050 kW 9 9 kg min 1 310 lb h 290 g kW h 0 477 lb hp h 29 1 See also EditFuel economy in automobiles Energy efficient driving Fuel management systems Marine fuel management Thrust specific fuel consumptionReferences Edit Operator Manual for 447 503 582 PDF Rotax Sep 2010 Archived from the original PDF on 2017 07 22 Retrieved 2018 06 08 a b c d e f g Gas Turbine Engines PDF Aviation Week January 2008 Gunter Mau Handbuch Dieselmotoren im Kraftwerks und Schiffsbetrieb Vieweg Springer Braunschweig Wiesbaden 1984 ISBN 978 3 528 14889 8 p 7 Shimizu Ritsuharu Tadokoro Tomoo Nakanishi Toru Funamoto Junichi 1992 02 01 Mazda 4 Rotor Rotary Engine for the Le Mans 24 Hour Endurance Race SAE International p 4 doi 10 4271 920309 ISSN 0148 7191 Operator Manual for 914 series PDF Rotax Apr 2010 Archived from the original PDF on 2017 06 11 Retrieved 2018 06 08 O 235 and O 290 Operator s Manual PDF Lycoming Jan 2007 p 3 8 version L a b Peter deBock September 18 2019 GE turbines and small engines overview PDF ARPA e INTEGRATE meeting Global Research General Electric Michael Soroka March 26 2014 Are Airplane Engines Inefficient Advanced Gasoline Turbocharged Direct Injection GTDI Engine Development PDF Ford Research and Advanced Engineering May 13 2011 IO 720 Operator s Manual PDF Lycoming October 2006 p 3 8 MT7 Brochure PDF Rolls Royce 2012 Archived from the original PDF on 2017 04 20 Retrieved 2018 07 09 Kimble D McCutcheon 27 October 2014 Wright R 3350 Cyclone 18 PDF Archived from the original PDF on 1 August 2016 Muta Koichiro Yamazaki Makoto Tokieda Junji 8 March 2004 Development of New Generation Hybrid System THS II Drastic Improvement of Power Performance and Fuel Economy SAE Technical Paper Series Vol 1 Society of Automotive Engineers doi 10 4271 2004 01 0064 Kaiser Sascha Donnerhack Stefan Lundbladh Anders Seitz Arne 27 29 July 2015 A composite cycle engine concept with hecto pressure ratio AIAA SAE ASEE Joint Propulsion Conference 51st ed doi 10 2514 6 2015 4028 inter action association 1987 Marine Trent Civil Engineering Handbook 19 Mar 2015 Napier Nomad Flight 30 April 1954 The new Audi A8 3 3 TDI quattro Top TDI for the luxury class Press release Audi AG July 10 2000 Jane s Fighting Aircraft of World War II London UK Bracken Books 1989 LM6000 Marine Gas Turbine PDF General Electric 2016 Archived from the original PDF on 2016 11 19 BMW 2 0d N47 in French Auto innovations June 2007 Stock Dieter Bauder Richard 1 February 1990 The New Audi 5 Cylinder Turbo Diesel Engine The First Passenger Car Diesel Engine with Second Generation Direct Injection SAE Technical Paper Series Vol 1 Society of Automotive Engineers doi 10 4271 900648 DC16 078A PDF Scania AB Wartsila 20 product guide PDF Wartsila 14 February 2017 Four Stroke Propulsion Engines PDF Man Diesel 2015 Archived from the original PDF on 2016 04 17 The new Wartsila 31 engine Wartsila Technical Journal 20 October 2015 RTA C Technology Review PDF Wartsila 2004 Archived from the original PDF on December 26 2005 MAN B amp W S80ME C9 4 TII Project Guide PDF Man Diesel May 2014 MAN B amp W G95ME C9 2 TII Project Guide PDF Man Diesel May 2014 p 16 Tomas Kellner 17 Jun 2016 Here s Why The Latest Guinness World Record Will Keep France Lit Up Long After Soccer Fans Leave Press release General Electric GE Unveils New H Class Gas Turbine and Already Has a First Order October 2 2019 ATR The Optimum Choice for a Friendly Environment PDF Avions de Transport Regional June 2001 p PW127F engine gaseous emissions Archived from the original PDF on 2016 08 08 Further reading EditReciprocating engine types HowStuffWorks How Car Engines Work Reciprocating Engines at infoplease Piston Engines US Centennial of Flight Commission Effect of EGR on the exhaust gas temperature and exhaust opacity in compression ignition engines Heywood J B 1988 Pollutant formation and control Internal combustion engine fundamentals Int edn New York Mc Graw Hill pp 572 577 Well to Wheel Studies Heating Values and the Energy Conservation Principle Exemplary maps for commercial car engines collected by ecomodder forum users Retrieved from https en wikipedia org w index php title Brake specific fuel consumption amp oldid 1128550062, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.