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  2. Aircraft fuel system - Wikipedia

    en.wikipedia.org/wiki/Aircraft_fuel_system

    Single-engine light aircraft fuel tanks are usually in the wings, but some aircraft have a small "header tank" between the normal fuel tank and the engine, to facilitate reliable fuel flow to the engine. On many small or very old single-engine header tanks (and even main tanks) are often mounted above and/or immediately behind the engine.

  3. AIDC AT-3 - Wikipedia

    en.wikipedia.org/wiki/AIDC_AT-3

    There's a rarely used small bomb bay feature in the aircraft, now mostly holding an auxiliary fuel tank. AT-3 has two Honeywell / Garrett TFE731-2-2L non-afterburning turbofan engines, producing a total thrust of 3178 kg (31.1 kN; 7000 lb).

  4. Carden–Baynes Auxiliary - Wikipedia

    en.wikipedia.org/wiki/Carden–Baynes_Auxiliary

    A small fuel tank was fixed above the crankcase, at the top of the engine. [1] [3] Carden also designed the engine mounting that enabled the engine and its propeller to be swung out of its housing and into action. The engine was hung to the top of the pylon bulkhead, just ahead of the trailing edge, on a diagonally cross-braced pair of tubes ...

  5. Aircraft fuel tank - Wikipedia

    en.wikipedia.org/wiki/Aircraft_fuel_tank

    Drop tanks, external tanks, wing tanks, pylon tanks or belly tanks are all terms used to describe auxiliary externally mounted fuel tanks. Drop tanks are generally expendable and often jettisonable. External tanks are commonplace on modern military aircraft and occasionally found in civilian ones, although the latter are less likely to be ...

  6. Bensen B-8 - Wikipedia

    en.wikipedia.org/wiki/Bensen_B-8

    Fuel capacity: 6 US gal (5.0 imp gal; 22.7 L) or 9.7 US gal (8.1 imp gal; 36.7 L) in a combined seat/fuel tank, with provision for an auxiliary tank for ferrying Powerplant: 1 × McCulloch Model 4318AX 4-cylinder air-cooled 2-stroke horizontally-opposed piston engine, 72 hp (54 kW)

  7. Auxiliary power unit - Wikipedia

    en.wikipedia.org/wiki/Auxiliary_power_unit

    The first German jet engines built during the Second World War used a mechanical APU starting system designed by the German engineer Norbert Riedel.It consisted of a 10 horsepower (7.5 kW) two-stroke flat engine, which for the Junkers Jumo 004 design was hidden in the intake diverter, essentially functioning as a pioneering example of an auxiliary power unit for starting a jet engine.

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