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  2. Allison T56 variants - Wikipedia

    en.wikipedia.org/wiki/Allison_T56_variants

    A T56 on a mobile test unit at MCAS Futenma, 1982 T56-A-1 (Series I) A 1,600 lb weight (730 kg) engine delivering 3,460 shp (2,580 kW) and 725 lbf (329 kgf; 3.22 kN) residual jet thrust, which is equal to 3,750 equivalent shp (2,800 kW); single-shaft 14-stage axial flow compressor, cannular combustion chamber with 6-cylindrical through-flow combustion liners, 4-stage axial flow turbine; 13,800 ...

  3. CFM International CFM56 - Wikipedia

    en.wikipedia.org/wiki/CFM_International_CFM56

    Once restored, the life limited parts must be replaced after: 20,000 cycles for the hot section ($0.5m), 25,000 for the axial compressor, and 30,000 for the fan and booster ($0.5m-$0.7m) for a recent CFM56. The whole engine parts cost more than $3m, $3.5 to $4m with the shop work-hours, around $150 per cycle. [43]

  4. Pratt & Whitney F135 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_F135

    The Pratt & Whitney F135 is an afterburning turbofan developed for the Lockheed Martin F-35 Lightning II, a single-engine strike fighter.It has two variants; a Conventional Take-Off and Landing variant used in the F-35A and F-35C, and a two-cycle Short Take-Off Vertical Landing variant used in the F-35B that includes a forward lift fan. [1]

  5. Aircraft engine - Wikipedia

    en.wikipedia.org/wiki/Aircraft_engine

    Though the fan creates thrust like a propeller, the surrounding duct frees it from many of the restrictions that limit propeller performance. This operation is a more efficient way to provide thrust than simply using the jet nozzle alone, and turbofans are more efficient than propellers in the transsonic range of aircraft speeds and can operate ...

  6. Allison Engine Company - Wikipedia

    en.wikipedia.org/wiki/Allison_Engine_Company

    In 1995, Allison tested a prototype lift fan for the Joint Strike Fighter Program [6] and a LiftFan nozzle was tested in 1997 at NASA's Lewis facility. [7] By 1997, a complete prototype had been demonstrated [ 8 ] by the Rolls-Royce owned but American-controlled Allison Advanced Development Company.

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