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  2. GE Aerospace - Wikipedia

    en.wikipedia.org/wiki/GE_Aerospace

    General Electric Company, doing business as GE Aerospace, [5] is an American aircraft engine supplier that is headquartered in Evendale, Ohio, outside Cincinnati.It is the legal successor to the original General Electric Company founded in 1892, which split into three separate companies between November 2021 and April 2024, adopting the trade name GE Aerospace after divesting its healthcare ...

  3. 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.

  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 T58 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T58

    The General Electric T58 is an American turboshaft engine developed for helicopter use. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built.

  6. 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

  7. General Electric TF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_TF34

    Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured. The TF34-GE-400A is rated at 9,275 lbf (41.26 kN) static thrust.