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词条 CFE CFE738
释义

  1. Design and development

  2. Applications

  3. Specifications

  4. See also

  5. References

  6. External links

name= CFE738image=caption=
}}{{Infobox Aircraft Engine
type= Turbofannational origin = United Statesmanufacturer= CFE Companyfirst run= 1990major applications= Dassault Falcon 2000number built =program cost =unit cost =developed from = General Electric GE27developed into =variants with their own articles =
}}

The CFE738 is a small turbofan engine aimed at the business/commuter jet market manufactured by the CFE Company, and is used on the Dassault Falcon 2000.

Design and development

The success of the GE27/GLC38 gas generator development of the 1980s led to the formation of the CFE Company by GE and the Garrett Engine Division of Allied Signal (now Honeywell) in 1987.

The CFE738 is a two-shaft design, consisting of a single stage bypass fan connected via one shaft to a 3-stage low-pressure (LP) turbine at the rear of the engine; with a six-stage combination low-pressure/high-pressure (LP/HP) axial/centrifugal compressor (five axial stages and one centrifugal stage) driven by a two-stage HP turbine, between the fan and the LP turbine, on the other shaft. There is an axial combustion chamber between the compressor stages and the HP turbine. A mixer is built in to the jetpipe to mix cold bypass air with the hot exhaust gases. The engine has an overall pressure ratio of 35:1, which is extremely high for an engine with a centrifugal compressor. Other cycle parameters are a bypass ratio of 5.3 and airflow of 240 lb/s (108.9 kg/s). The take-off thrust is 5,600 lbf (24.9 kN), flat-rated to ISA +15°C (30°C, 86°F).

The engine was first run in 1990 and first flown on a Boeing 727 testbed on 31 August 1992.[1] It was certified by the American Federal Aviation Authority on 17 December 1993.

Applications

  • Dassault Falcon 2000

Specifications

{{jetspecs
|ref=
|type=Turbofan
|length=68.3 in
|diameter=35.50 in (Fan)
|weight=1,214 lb (Basic) Dry Weight: 1,325 lb
|compressor=Fan/Compressor Stages: 1/5+1C
|combustion=
|turbine=High-Pressure Turbine/Low-Pressure Turbine Stages: 2/3
|fueltype=
|oilsystem=
|power=
|thrust=Max. Thrust (Sea Level Static): 26.3 kN (5,918 lbf), Cruise Net Thrust (Mach 0.8, 40000 ft, ISA): 1310 lbf
|compression= ~30:1, Bypass Ratio: 5.3
|aircon= 240 lb/s
|turbinetemp=
|fuelcon=
|specfuelcon=(Sea Level Static): 0.369 lb/(h lbf), (Mach 0.8, 40000 ft, ISA): 0.645 lb/(h lbf)
|power/weight=
|thrust/weight=
}}

See also

{{Aircontent
|related=
  • General Electric GE27/GE38

|similar engines=
|lists=
  • List of aircraft engines

|see also=
}}

References

1. ^{{cite magazine|magazine=Aviation World|publisher=Air-Britain|title=Turbojet Engines - The High Bypass Turbofans Part 2|date=2004|page=132|issn=1742 996X}}
  • {{cite book |last= Gunston |first= Bill |title= World Encyclopedia of Aero Engines, 5th Edition |year= 2006 |publisher= Sutton Publishing Limited |location= Phoenix Mill, Gloucestershire, England, UK |isbn= 0-7509-4479-X |page= }}
  • {{cite book|last= Leyes II |first= Richard A. |author2=William A. Fleming |title= The History of North American Small Gas Turbine Aircraft Engines |publisher= Smithsonian Institution |location= Washington, DC |date= 1999 |pages= |chapter= |isbn= 1-56347-332-1 |url= }}

External links

  • General Electric CFE738 page
{{Joint development aeroengines}}{{USAF gas turbine engines}}

2 : High-bypass turbofan engines|Turbofan engines 1990–1999

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