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  2. Allison T40 - Wikipedia

    en.wikipedia.org/wiki/Allison_T40

    The engine cowlings on this Hiller X-18 have not been fully installed, so the dual turbine units are visible. The first aircraft to fly with the T40 was the Convair XP5Y-1 patrol aircraft prototype. As flying boat patrol aircraft became redundant, the US Navy changed the role of the aircraft from Anti-Submarine Warfare to Transport.

  3. Avco-Lycoming AGT1500 - Wikipedia

    en.wikipedia.org/wiki/Avco-Lycoming_AGT1500

    The engine weighs approximately 2,500 lb (1,100 kg) and occupies a volume of 40 cu ft (1.1 m 3), measuring 63 in × 40 in × 28 in (1,600 mm × 1,020 mm × 710 mm). [4] The engine can use a variety of fuels, including jet fuel, gasoline, diesel and marine diesel. [2] The engine is a three-shaft machine composed of five sub-modules: [4]

  4. IAE V2500 - Wikipedia

    en.wikipedia.org/wiki/IAE_V2500

    The engine's name is a combination of the Roman numeral V, symbolizing the five original members of the International Aero Engines consortium, which was formed in 1983 to produce the V2500 engine. The 2500 represents the 25,000- pound-force (110 kN) produced by the original engine model, the V2500-A1.

  5. Pratt & Whitney Canada PW600 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW600

    The 2,500 lbf (11 kN) thrust PW625F demonstrator engine was first run on 31 October 2001. [1] It flew in late 2002. [2] In 2002, the PW610F was selected for the Eclipse 500 twinjet, replacing the EJ22 as Williams was unable to reach sufficient reliability. The 950 lbf (4.2 kN) thrust engine was certified by Transport Canada on 27 July 2006. [3]

  6. GE Honda HF120 - Wikipedia

    en.wikipedia.org/wiki/GE_Honda_HF120

    The engine has a wide-chord swept fan, two-stage low-pressure compressor and counter rotating high-pressure compressor based on a titanium impeller, for a 2,050 lbf (9.1 kN) takeoff thrust. [5] The HF120 engine's components interact with greater efficiency by incorporating 3D aerodynamic design, and its effusion-cooled combustor design emits ...

  7. Klimov VK-2500 - Wikipedia

    en.wikipedia.org/wiki/Klimov_VK-2500

    Rated at 2,500 shp (1,864 kW) take-off power. Powers Mi-28NM. [2] VK-2500M Next generation derivative of VK-2500 under development by Klimov, with planned reduced fuel burn and weight. Rated at 2,600 shp (1,939 kW) for take-off and 2,200 shp (1,641 kW) continuous power. Deliveries planned by 2023. [4] TV3-117VMA-SB3 Ukrainian designation for VK ...

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