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  2. Solar T62 - Wikipedia

    en.wikipedia.org/wiki/Solar_T62

    Turboshaft - 95 hp (71 kW) at 56,700 turbine rpm, for Lockheed Jetstar and Pan American Falcon business Jets at 56,700 turbine rpm, with 1x 8,000 and 1x 8,100 rpm outputs. [1] T62T-32A 150 hp (110 kW) at 61,250 rpm. Military Ground Power Unit (GPU) often used by US Navy and Air Force. T62T-39 T66 A free power turbine version for the US military.

  3. List of turbofan manufacturers - Wikipedia

    en.wikipedia.org/wiki/List_of_turbofan_manufacturers

    Williams International is a manufacturer of small gas turbine engines based in Walled Lake, Michigan, United States. It produces jet engines for cruise missiles and small jet-powered aircraft. They have been producing engines since the 1970s and the range produces between 1000 and 3600 pounds of thrust.

  4. Lycoming Engines - Wikipedia

    en.wikipedia.org/wiki/Lycoming_Engines

    The company has built more than 325,000 piston aircraft engines and powers more than half the world's general aviation fleet, both rotary and fixed wing. [1] Lycoming has been a principal pioneer of turbine engines for medium and large helicopters, and has also produced engines for small jetliners and business jets. [2] [3] [4]

  5. General Electric T64 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T64

    The General Electric T64 is a free-turbine turboshaft engine that was originally developed for use on helicopters, but which was later used on fixed-wing aircraft as well. General Electric introduced the engine in 1964. The original engine design included technical innovations such as corrosion resistant and high-temperature coatings. [1]

  6. General Electric T58 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T58

    a single stage power turbine. which delivers power to the rear of the engine. The hot exhaust stream is diverted sideways, away from the output shaft. the combustor is a straight-through annular design, rather than reverse flow. The main production version of the engine was the T58-GE-10, developing 1,400 hp (1,044 kW). The most powerful ...

  7. 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 ...

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