General Electric F101: Difference between revisions
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The '''General Electric F101''' is an [[Afterburner|afterburning]] [[turbofan]] [[jet engine]]. It powers the [[Rockwell B-1 Lancer]] [[strategic bomber]] fleet of the [[USAF]]. In full afterburner it produces a thrust of more than {{convert|30000|lb-f|kN|lk=on}}. The F101 was [[GE Aviation|GE]]'s first turbofan with an afterburner.<ref>[http://www.geae.com/engines/military/f101/index.html GE's F101 web page]</ref> |
The '''General Electric F101''' is an [[Afterburner|afterburning]] [[turbofan]] [[jet engine]]. It powers the [[Rockwell B-1 Lancer]] [[strategic bomber]] fleet of the [[USAF]]. In full afterburner it produces a thrust of more than {{convert|30000|lb-f|kN|lk=on}}. The F101 was [[GE Aviation|GE]]'s first turbofan with an afterburner.<ref>[http://www.geae.com/engines/military/f101/index.html GE's F101 web page] {{webarchive|url=https://web.archive.org/web/20110211103843/http://www.geae.com/engines/military/f101/index.html |date=2011-02-11 }}</ref> |
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==Development== |
==Development== |
Revision as of 13:45, 12 October 2017
F101 | |
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A General Electric F101 engine | |
Type | Turbofan |
National origin | United States |
Manufacturer | General Electric |
First run | 1970s |
Major applications | Rockwell B-1 Lancer |
Developed into | General Electric F110 CFM International CFM56 |
The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN). The F101 was GE's first turbofan with an afterburner.[1]
Development
The F101 was developed specifically for the Advanced Manned Strategic Aircraft, which became the B-1A. The F101 powered the four development aircraft from 1970 to 1981. The B-1A was officially cancelled in 1977. However the flight test program continued. General Electric was awarded a contract to further develop the F101-102 engine variant. This turbofan eventually powered the B-1B from 1984, entering service in 1986. The B-1's four F101 engines helped the aircraft win 61 world records for speed, payload and range.
The GE F110 fighter engine is a derivative of the F101, designed using data from the F101-powered variant of the F-16 Fighting Falcon tested in the early 1980s. The F101 also became the basis for the highly successful CFM56 series of civil turbofans.
Applications
Specifications (F101-GE-102)
Data from [2]
General characteristics
- Type: Turbofan
- Length: 181 in (460 cm)
- Diameter: 55 in (140 cm)
- Dry weight: 4,400 lb (1995 kg)
Components
- Compressor: Axial, 2 stage fan, 9 stage high pressure compressor
- Combustors: Annular
- Turbine: 1 stage high pressure turbine, 2 stage low pressure turbine
Performance
- Maximum power output: 17,390 lbf (77.4 kN) (dry thrust), 30,780 lb (136.9 kN) (with afterburner)
- Overall pressure ratio: 26.8:1
- Specific fuel consumption: 0.562 lb/(lbf h) (dry thrust), 2.46 lb/(lbf h) (max thrust)
- Thrust-to-weight ratio: 7.04:1 (afterburner)
See also
Comparable engines
Related lists
References
- ^ GE's F101 web page Archived 2011-02-11 at the Wayback Machine
- ^ Gas Turbine Engines. Aviation Week & Space Technology 2009 Source Book. p. 118.
External links
![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)