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  2. DeltaHawk DH180 - Wikipedia

    en.wikipedia.org/wiki/DeltaHawk_DH180

    The design is a four-cylinder, two-stroke, piston diesel engine, in an inverted-V configuration, with turbocharging and supercharging, mechanical fuel injection, liquid cooling, direct drive. It can run on Jet-A or sustainable aviation fuel. The manufacturer claims that it has "40 percent fewer moving parts than other engines in its category ...

  3. Thielert Centurion - Wikipedia

    en.wikipedia.org/wiki/Thielert_Centurion

    The diesel engine's high compression results in better fuel efficiency and the higher operating rpm of the Centurion allows higher power to be developed from a smaller displacement, in comparison to conventional aircraft piston engines (i.e. engines that require leaded aviation gasoline with a very high octane rating). [citation needed]

  4. Daimler-Benz DB 605 - Wikipedia

    en.wikipedia.org/wiki/Daimler-Benz_DB_605

    In 1944 a series of newer engines was introduced, allowing the engine to run on the 100 octane "C3" fuel and optionally including fittings for various optional power-boosting agent dispensing systems, such as the MW50 methanol-water injection system, and GM-1 nitrous oxide injection system. The DB 605AM, running initially on C3 and MW-50, saw ...

  5. Daimler-Benz DB 600 series - Wikipedia

    en.wikipedia.org/wiki/Daimler-Benz_DB_600_series

    The DB 601 was a development of the DB 600G with direct fuel injection, which produced better fuel economy, and eliminated engine cut-out due to carburettor induced fuel starvation during negative G-loads. [2] The supercharger in the new engine was driven through a stage-less, automatically controlled hydraulic clutch. The supercharger speed ...

  6. Guiberson A-1020 - Wikipedia

    en.wikipedia.org/wiki/Guiberson_A-1020

    Data from Aircraft Diesels: Chapter 3 - The Guiberson Diesel General characteristics Type: 9-cylinder air-cooled radial diesel piston engine Bore: 5.125 in (130.18 mm) Stroke: 5.5 in (139.70 mm) Displacement: 1,021 cu in (16.73 L) Length: 38.6 in (980 mm) including starter Diameter: 47.125 in (1,197.0 mm) Dry weight: 653 lb (296 kg) Designer: F. A. Thaheld Components Valvetrain: two pushrod ...

  7. Lycoming IO-720 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_IO-720

    The Lycoming IO-720 engine is a large displacement, horizontally opposed, eight-cylinder aircraft engine featuring four cylinders per side, manufactured by Lycoming Engines. [ 1 ] There is no carbureted version of the engine, which would have been designated O-720 and therefore the base model is the IO-720.