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  2. General Electric Catalyst - Wikipedia

    en.wikipedia.org/wiki/General_Electric_Catalyst

    The General Electric Catalyst (formerly Advanced Turboprop, or ATP) is a turboprop engine by GE Aerospace.It was announced on 16 November 2015 and will power the Beechcraft Denali, it first ran on December 22, 2017, and should be certified in 2024.

  3. General Electric GE90 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_GE90

    The General Electric GE90 is a family of high-bypass turbofan aircraft engines built by GE Aerospace for the Boeing 777, with thrust ratings from 81,000 to 115,000 pounds-force (360 to 510 kilonewtons).

  4. General Electric T64 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T64

    The engine features a high overall pressure ratio, yielding a low specific fuel consumption for its time. [2] Although the compressor is all-axial, like the earlier General Electric T58 , the power turbine shaft is coaxial with the HP shaft and delivers power to the front of the engine, not rearwards.

  5. General Electric T700 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T700

    The T700-GE-700 is rated at 1,622 shp (1,210 kW) intermediate power. The T700-GE-700 was followed by improved and uprated Army engine variants for the UH-60 Black Hawk and the AH-64 Apache helicopters, as well as marinized naval engine variants for the SH-60 Seahawk derivative of the Black Hawk, the SH-2G Seasprite, and the Bell AH-1W Supercobra.

  6. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN ) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg).

  7. General Electric F110 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F110

    The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace (formerly GE Aviation). It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well.

  8. General Electric GE38 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_GE38

    T408-GE-400 (GE38-1B) Boeing NCH-47D Chinook (flying testbed) [16] Sikorsky CH-53K King Stallion; CFE CFE738 Turbofan variant of the T407-GE-400, used on the Dassault Falcon CPX38 Proposed turboprop engine variant of the GE38-1B [17] GE38-3 An 8,000 shp (6,000 kW) class derivative engine under consideration by the U.S. military in 2006 [18] GE38-B5

  9. General Electric F414 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F414

    The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound (98 kN) thrust class produced by GE Aerospace (formerly GE Aviation). The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet.