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  2. Mistral Engines - Wikipedia

    en.wikipedia.org/wiki/Mistral_Engines

    Mistral Engines SA was a Swiss developer and manufacturer of wankel rotary aviation light aircraft, helicopter and unmanned military vehicle engines. [1] Its headquarters was in Geneva, Switzerland [ 2 ] and was majority owned by DEA General Aviation, a Chinese company based in Guangdong .

  3. List of Allis-Chalmers engines - Wikipedia

    en.wikipedia.org/wiki/List_of_Allis-Chalmers_engines

    In a later reversal of this practice, the Engine Division eventually served as a third-party supplier to other makers of farm and industrial machinery, most notably Cockshutt and LeRoi. Allis-Chalmers (and Buda) produced heavy-duty engine designs that were built to handle a variety of fuel types (generally gasoline , diesel fuel , or liquefied ...

  4. Tumansky R-29 - Wikipedia

    en.wikipedia.org/wiki/Tumansky_R-29

    The Tumansky R-29 is a Soviet turbojet aircraft engine that was developed in the early 1970s. [1] It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.

  5. Jacobs R-755 - Wikipedia

    en.wikipedia.org/wiki/Jacobs_R-755

    300 hp variant. R-755A3 Similar to A1 but with Scintilla magnetoes. R-755B1 De-rated version of the R-755A to drive a fixed pitch airscrew. [2] R-755B2 De-rated version of the R-755A to drive a variable or controllable pitch airscrew. [2] R-755E Up-rated engine with reduction gearing. [2] R-755EH Developed to power the Jacobs Type 104 Gyrodyne. [2]

  6. Pratt & Whitney Canada PW500 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW500

    The engines, designated PW535E1, are rated at 3,478 lbf (15.47 kN)/ [4] Unveiled at the May 2023 EBACE show, the FADEC-controlled PW545D is developed for the Cessna 560XL Ascend variant, to be rated at 4,200 lbf (19 kN) and optimized for improved fuel burn and longer time between overhauls (TBO) up to 6,000 hours. [ 2 ]

  7. Tumansky R-25 - Wikipedia

    en.wikipedia.org/wiki/Tumansky_R-25

    The Tumansky R-25 was designed as a replacement for the Tumansky R-13 in MiG-21 fighters. The R-25 is a two-spool axial-flow turbojet with a new compressor with increased overall pressure ratio and airflow, variable two-stage afterburner, and greater use of titanium.

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