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  2. Total-loss oiling system - Wikipedia

    en.wikipedia.org/wiki/Total-loss_oiling_system

    These engines were designed to have a total-loss lubrication system, with the motor oil held in a separate tank from the fuel in the vehicle, and not pre-mixed with it as with two-cycle engines, but mixed within the engine instead while running. Castor oil was often used because it lubricates well at the high temperatures found in air-cooled ...

  3. Oil pump (internal combustion engine) - Wikipedia

    en.wikipedia.org/wiki/Oil_pump_(internal...

    [c] These are supplementary pumps and do not replace the main, mechanical, oil pump. Electric pump as a main engine pump again will require big electric motors and it may be simply cheaper to drive directly from the engine. For e.g. BMW S65 engine's oil pump delivers ca. 45 LPM (Litres Per Minute) of oil at 5.5 bar pressure. [5]

  4. List of aircraft engines - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_engines

    Source: RMV [1]. Advanced Engine Design Spitfire 1 Cylinder; Advanced Engine Design Spitfire 2 Cylinder; Advanced Engine Design Spitfire 3 Cylinder; Advanced Engine Design Spitfire 4 Cylinder

  5. Rotax 912 - Wikipedia

    en.wikipedia.org/wiki/Rotax_912

    The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.

  6. Rotax 914 - Wikipedia

    en.wikipedia.org/wiki/Rotax_914

    The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads.It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.

  7. Aircraft fuel system - Wikipedia

    en.wikipedia.org/wiki/Aircraft_fuel_system

    Adding tanks and engines increases the complexity of the fuel system and its management. Additional features found in multi-engine aircraft are: Each wing tank often has its own electric boost fuel pump, and each engine has its own mechanical pump, replicating the fuel system described above for the single engine.

  8. Wankel engine - Wikipedia

    en.wikipedia.org/wiki/Wankel_engine

    UEL UAV-741 Wankel engine for a UAV. The Wankel engine is well-suited for devices in which a human operator is close to the engine, e.g., hand-held devices such as chainsaws. [191] The excellent starting behavior and low mass make the Wankel engine also a good powerplant for portable fire pumps and portable power generators. [192]

  9. AAI RQ-7 Shadow - Wikipedia

    en.wikipedia.org/wiki/AAI_RQ-7_Shadow

    Other improvements in the program will include an electronic fuel injection engine and fuel system to replace the AR741-1101's carburetted engine. The most visible improvement to the system will be a wider wing of 20 feet (6.1 m) in span which is designed to increase fuel capacity and allow for mission endurance of almost 9 hours.

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