Английская Википедия:Brake-specific fuel consumption

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Шаблон:Short description 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

The brake-specific fuel consumption is given by,

<math> \text{BSFC}= \frac{r}{P} </math>

where:

<math> r </math> is the fuel consumption rate in grams per second (g/s)
<math> P </math> is the power produced in watts where <math>P = \tau \omega</math> (W)
<math>\omega</math> is the engine speed in radians per second (rad/s)
<math>\tau</math> is the engine torque in newton metres (N⋅m)

The above values of r, <math>\omega</math>, and <math>\tau</math> 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

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 Шаблон:Convert 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

Файл:Brake specific fuel consumption.svg
BSFC [g/(kW⋅h)] map

Шаблон:Main article 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

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

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
Шаблон:Convert 1989 Rotax 582 gasoline, 2-stroke Aviation, Ultralight, Eurofly Fire Fox Шаблон:Convert[1] 19.3%
Шаблон:Convert 1987 PW206B/B2 turboshaft Helicopter, EC135 Шаблон:Convert[2] 24.4%
Шаблон:Convert 1987 PW207D turboshaft Helicopter, Bell 427 Шаблон:Convert[2] 25.1%
Шаблон:Convert 1981 Arrius 2B1/2B1A-1 turboshaft Helicopter, EC135 Шаблон:Convert[2] 25.6%
Шаблон:Convert 1897 Motor 250/400[3] Diesel, four-stroke Stationary industrial Diesel engine Шаблон:Convert 26.2%
Шаблон:Convert 1960 PT6C-67C turboshaft Helicopter, AW139 Шаблон:Convert[2] 27.5%
Шаблон:Convert 1991 Mazda R26B[4] Wankel, four-rotor Race car, Mazda 787B Шаблон:Convert 28.7%
Шаблон:Convert 1989 MTR390 turboshaft Helicopter, Tiger Шаблон:Convert[2] 29.3%
Шаблон:Convert 1996 Rotax 914 gasoline, turbo Aviation, Light-sport aircraft, WT9 Dynamic Шаблон:Convert[5] 29.7%
Шаблон:Convert 1942 Lycoming O-235-L gasoline Aviation, General aviation, Cessna 152 Шаблон:Convert[6] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Cvt 1973 GE T700 turboshaft Helicopter, AH-1/UH-60/AH-64 Шаблон:Cvt[7] 31.1%
Шаблон:Cvt 1995 PW150 turboprop Airliner, Dash 8-400 Шаблон:Cvt[2] 31.1%
Шаблон:Convert 1984 RTM322-01/9 turboshaft Helicopter, NH90 Шаблон:Convert[2] 32.1%
Шаблон:Convert 1991 GM Saturn I4 engine gasoline Cars, Saturn S-Series Шаблон:Convert[8] 32.8%
Шаблон:Convert 2011 Ford EcoBoost gasoline, turbo Cars, Ford Шаблон:Convert[9] 33.5%
Шаблон:Convert 1961 Lycoming IO-720 gasoline Aviation, General aviation, PAC Fletcher Шаблон:Convert[10] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Cvt 1989 GE T408 turboshaft Helicopter, CH-53K Шаблон:Cvt[7] 33.7%
Шаблон:Convert 1986 Rolls-Royce MT7 gas turbine Hovercraft, SSC Шаблон:Convert[11] 34.7%
Шаблон:Convert 1945 Wright R-3350 Duplex-Cyclone gasoline, turbo-compound Aviation, Commercial aviation; B-29, Constellation, DC-7 Шаблон:Convert[12] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Convert 2003 Toyota 1NZ-FXE gasoline Car, Toyota Prius Шаблон:Convert[13] 36.4%
Шаблон:Convert 2005 Europrop TP400 turboprop Airbus A400M Шаблон:Convert[14] 39.6%
Шаблон:Convert 1931 Junkers Jumo 204 diesel two-stroke, turbo Aviation, Commercial aviation, Junkers Ju 86 Шаблон:Convert[15] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Convert 2002 Rolls-Royce Marine Trent turboshaft Marine propulsion Шаблон:Convert[16] 40.7%
Шаблон:Convert 1949 Napier Nomad Diesel-compound Concept Aircraft engine Шаблон:Convert[17] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Convert 2000 Volkswagen 3.3 V8 TDI Diesel Car, Audi A8 Шаблон:Convert[18] 41.1%
Шаблон:Convert 1940 Deutz DZ 710 Diesel two-stroke Concept Aircraft engine Шаблон:Convert[19] Ошибка выражения: неопознанный символ пунктуации «[»%
Шаблон:Convert 1993 GE LM6000 turboshaft Marine propulsion, Electricity generation Шаблон:Convert[20] 42.1%
Шаблон:Convert 2007 BMW N47 2L Diesel Cars, BMW Шаблон:Convert[21] 42.6%
Шаблон:Convert 1990 Audi 2.5L TDI Diesel Car, Audi 100 Шаблон:Convert[22] 42.6%
Шаблон:Convert 1992 VAG 1.9TDI 66kw Diesel 4-stroke Car, Audi 80, VW Golf/Passat Шаблон:Convert[23] 42.8%
Шаблон:Convert 2017 MAN D2676LF51 Diesel 4-stroke Truck/Bus Шаблон:Convert[24] 44.1%
Шаблон:Convert Scania AB DC16 078A Diesel 4-stroke Electricity generation Шаблон:Convert[25] 44.4%
Шаблон:Convert early 1990s Wärtsilä 6L20 Diesel 4-stroke Marine propulsion Шаблон:Convert[26] 44.5%
Шаблон:Convert 2019 MAN D2676LF78 Diesel 4-stroke Truck/Bus Шаблон:Convert[27] 45.8%
Шаблон:Convert MAN Diesel 6L32/44CR Diesel 4-stroke Marine propulsion, Electricity generation Шаблон:Convert[28] 49%
Шаблон:Convert 2015 Wärtsilä W31 Diesel 4-stroke Marine propulsion, Electricity generation Шаблон:Convert[29] 51.1%
Шаблон:Convert 1998 Wärtsilä-Sulzer RTA96-C Diesel 2-stroke Marine propulsion, Electricity generation Шаблон:Convert[30] 52.7%
Шаблон:Convert MAN Diesel S80ME-C9.4-TII Diesel 2-stroke Marine propulsion, Electricity generation Шаблон:Convert[31] 54.6%
Шаблон:Convert MAN Diesel G95ME-C9 Diesel 2-stroke Marine propulsion Шаблон:Convert[32] 54.6%
Шаблон:Convert 2016 General Electric 9HA Combined cycle gas turbine Electricity generation Шаблон:Convert (eq.) 62.2%[33]
Шаблон:Convert 2021 General Electric 7HA.3 Combined cycle gas turbine Electricity generation (proposed) Шаблон:Convert (eq.) 63.9%[34]

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)[35]
Mode Power fuel flow SFC Energy efficiency
Nominal idle (7%) Шаблон:Convert Шаблон:Convert Шаблон:Convert 6.6%
Approach (30%) Шаблон:Convert Шаблон:Convert Шаблон:Convert Ошибка выражения: неопознанный символ пунктуации «[»%
Max cruise (78%) Шаблон:Convert Шаблон:Convert Шаблон:Convert Ошибка выражения: неопознанный символ пунктуации «[»%
Max climb (80%) Шаблон:Convert Шаблон:Convert Шаблон:Convert Ошибка выражения: неопознанный символ пунктуации «[»%
Max contin. (90%) Шаблон:Convert Шаблон:Convert Шаблон:Convert Ошибка выражения: неопознанный символ пунктуации «[»%
Take-off (100%) Шаблон:Convert Шаблон:Convert Шаблон:Convert Ошибка выражения: неопознанный символ пунктуации «[»%

See also

References

Шаблон:Reflist

Further reading