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  2. Honeywell HTS900 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_HTS900

    Developed from. Lycoming LTS101. The Honeywell HTS900 is an American turboshaft engine produced by Honeywell Aerospace. A growth version of the LTS101 which it is designed to replace, [1] the HTS900 is in the 1,000 shp (745 kW) class. At the October 2018 NBAA convention, it was shown with two 200 kW (270 hp) electric generators for hybrid ...

  3. Honeywell auxiliary power unit - Wikipedia

    en.wikipedia.org/wiki/Honeywell_auxiliary_power_unit

    Honeywell auxiliary power unit. Honeywell auxiliary power units are a series of gas turbine auxiliary power units (APU) made by Honeywell Aerospace. Honeywell started manufacturing APUs in the early 1950s and since then they can be found on many aircraft. [1] Over the years Honeywell have produced more than 95,000 APUs and more than 36,000 are ...

  4. Honeywell HTF7000 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_HTF7000

    Honeywell HTF7000. The Honeywell HTF7000 is a turbofan engine produced by Honeywell Aerospace. Rated in the 6,540–7,624 lbf (29.09–33.91 kN) range, the HTF7000 is used on the Bombardier Challenger 300 /350, Gulfstream G280, Embraer Legacy 500 /450 and the Cessna Citation Longitude. Its architecture could be extended for a range of 8,000 to ...

  5. Improved Turbine Engine Program - Wikipedia

    en.wikipedia.org/wiki/Improved_Turbine_Engine...

    The Improved Turbine Engine Program (ITEP), formerly the Advanced Affordable Turbine Engine (AATE) program, is a United States Army project to develop a General Electric T700 replacement for the UH-60 Black Hawk and AH-64 Apache, improving fuel consumption, power, durability and cost. Honeywell and Pratt & Whitney formed the ATEC joint venture ...

  6. Garrett TFE731 - Wikipedia

    en.wikipedia.org/wiki/Garrett_TFE731

    Honeywell/ITEC F124/F125. The Garrett TFE731 (now Honeywell TFE731) is a family of geared turbofan engines commonly used on business jet aircraft. Garrett AiResearch originally designed and built the engine, which due to mergers was later produced by AlliedSignal and now Honeywell Aerospace. Since the engine was introduced in 1972, over 11,000 ...

  7. Turbo generator - Wikipedia

    en.wikipedia.org/wiki/Turbo_generator

    The rotor of a turbo generator is a non-salient pole type usually with two poles. [5] The normal speed of a turbo generator is 1500 or 3000 rpm with four or two poles at 50 Hz (1800 or 3600 rpm with four or two poles at 60 Hz). The rotating parts of a turbo generator are subjected to high mechanical stresses because of the high operation speed.