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).

Calculation edit

The brake-specific fuel consumption is given by,

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

Relation to efficiency edit

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)

Operating values and as a cycle average statistic edit

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)

Engine design and class edit

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 for shaft engines edit

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.

kWHPYearEngineTypeApplicationlb/(hp⋅h)g/(kW⋅h)Efficiency
48641989Rotax 582gasoline, 2-strokeAviation, Ultralight, Eurofly Fire Fox0.699425[1]19.3%
3214311987PW206B/B2turboshaftHelicopter, EC1350.553336[2]24.4%
4275721987PW207DturboshaftHelicopter, Bell 4270.537327[2]25.1%
5006701981Arrius 2B1/2B1A-1turboshaftHelicopter, EC1350.526320[2]25.6%
13.117.81897Motor 250/400[3]Diesel, four-strokeStationary industrial Diesel engine0.53332426.2%
8201,1001960PT6C-67CturboshaftHelicopter, AW1390.490298[2]27.5%
5156911991Mazda R26B[4]Wankel, four-rotorRace car, Mazda 787B0.47028628.7%
9581,2851989MTR390turboshaftHelicopter, Tiger0.460280[2]29.3%
84.5113.31996Rotax 914gasoline, turboAviation, Light-sport aircraft, WT9 Dynamic0.454276[5]29.7%
881181942Lycoming O-235-LgasolineAviation, General aviation, Cessna 1520.452275[6]29.8%
4566121988Honda RA168Egasoline, turboRace car, McLaren MP4/40.447272[7]31.6%
1,7702,3801973GE T700turboshaftHelicopter, AH-1/UH-60/AH-640.433263[8]31.1%
3,7815,0711995PW150turbopropAirliner, Dash 8-4000.433263[2]31.1%
1,7992,4121984RTM322-01/9turboshaftHelicopter, NH900.420255[2]32.1%
63841991GM Saturn I4 enginegasolineCars, Saturn S-Series0.411250[9]32.8%
1502002011Ford EcoBoostgasoline, turboCars, Ford0.403245[10]33.5%
3004001961Lycoming IO-720gasolineAviation, General aviation, PAC Fletcher0.4243[11]34.2%
5,6007,5001989GE T408turboshaftHelicopter, CH-53K0.4240[8]33.7%
7,0009,4001986Rolls-Royce MT7gas turbineHovercraft, SSC0.3998243.2[12]34.7%
2,0002,7001945Wright R-3350 Duplex-Cyclonegasoline, turbo-compoundAviation, Commercial aviation; B-29, Constellation, DC-70.380231[13]35.5%
57762003Toyota 1NZ-FXEgasolineCar, Toyota Prius0.370225[14]36.4%
8,25111,0652005Europrop TP400turbopropAirbus A400M0.350213[15]39.6%
5507401931Junkers Jumo 204diesel two-stroke, turboAviation, Commercial aviation, Junkers Ju 860.347211[16]40%
36,00048,0002002Rolls-Royce Marine TrentturboshaftMarine propulsion0.340207[17]40.7%
2,3403,1401949Napier NomadDiesel-compoundConcept Aircraft engine0.340207[18]40.7%
1652212000Volkswagen 3.3 V8 TDIDieselCar, Audi A80.337205[19]41.1%
2,0132,6991940Deutz DZ 710Diesel two-strokeConcept Aircraft engine0.330201[20]41.9%
42,42856,8971993GE LM6000turboshaftMarine propulsion, Electricity generation0.329200.1[21]42.1%
1301702007BMW N47 2LDieselCars, BMW0.326198[22]42.6%
881181990Audi 2.5L TDIDieselCar, Audi 1000.326198[23]42.6%
66891992VAG 1.9TDI 66kwDiesel 4-strokeCar, Audi 80, VW Golf/Passat0.324197[24]42.8%
3684932017MAN D2676LF51Diesel 4-strokeTruck/Bus0.314191[25]44.1%
620830Scania AB DC16 078ADiesel 4-strokeElectricity generation0.312190[26]44.4%
1,2001,600early 1990sWärtsilä 6L20Diesel 4-strokeMarine propulsion0.311189.4[27]44.5%
3755032019MAN D2676LF78Diesel 4-strokeTruck/Bus0.302184[28]45.8%
3,6004,800MAN Diesel 6L32/44CRDiesel 4-strokeMarine propulsion, Electricity generation0.283172[29]49%
4,2005,6002015Wärtsilä W31Diesel 4-strokeMarine propulsion, Electricity generation0.271165[30]51.1%
34,32046,0201998Wärtsilä-Sulzer RTA96-CDiesel 2-strokeMarine propulsion, Electricity generation0.263160[31]52.7%
27,06036,290MAN Diesel S80ME-C9.4-TIIDiesel 2-strokeMarine propulsion, Electricity generation0.254154.5[32]54.6%
34,35046,060MAN Diesel G95ME-C9Diesel 2-strokeMarine propulsion0.254154.5[33]54.6%
605,000811,0002016General Electric 9HACombined cycle gas turbineElectricity generation0.223135.5 (eq.)62.2%[34]
640,000860,0002021General Electric 7HA.3Combined cycle gas turbineElectricity generation (proposed)0.217131.9 (eq.)63.9%[35]

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)[36]
ModePowerfuel flowSFCEnergy 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 edit

References edit

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Further reading edit