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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.
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.
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.
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.
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
The General Electric H-Series is a family of turboprop aircraft engines produced by GE BGA Turboprops. The initial H80 is an updated derivative of the Walter M601 , while the H75 and H85 are later derivatives.