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  2. JLT Motors Ecoyota - Wikipedia

    en.wikipedia.org/wiki/JLT_Motors_Ecoyota

    The engine is a three-cylinder, in-line, four-stroke, 998 cc (60.9 cu in) displacement, liquid-cooled, automotive-conversion petrol engine design, with a poly V belt reduction drive with a reduction ratio of 2.41:1. It employs electronic ignition and has a compression ratio of 10.5:1. [1]

  3. Bailey B200 - Wikipedia

    en.wikipedia.org/wiki/Bailey_B200

    The B200 was designed specifically as a more fuel efficient and quieter replacement for small two-stroke engines that are typically used on this class of aircraft. The B200 has a displacement of 200 cc (12.2 cu in), includes standard electric starting and capacitor discharge ignition.

  4. Hexadyne P60 - Wikipedia

    en.wikipedia.org/wiki/Hexadyne_P60

    The engine is a twin cylinder four-stroke, horizontally-opposed, 800 cc (48.8 cu in), air-cooled, gasoline engine design, with a mechanical gearbox spur gear reduction drive with a reduction ratio of 2.5:1. It employs electronic ignition and produces 60 hp (45 kW) continuous at 5750 rpm. The engine management system is a six-sensor computer and ...

  5. Jabiru 2200 - Wikipedia

    en.wikipedia.org/wiki/Jabiru_2200

    The engine generates up to 60 kW (80 bhp) at 3,300 rpm. [2] In Europe the engine competes with the Rotax 912, another flat four four-stroke engine, but one that has water-cooled cylinder heads and a geared reduction drive to the propeller. Jabiru Aircraft began as a builder of small two-seater aircraft in Bundaberg, Australia. [3]

  6. KFM 112M - Wikipedia

    en.wikipedia.org/wiki/KFM_112M

    The KFM 112M is a four-cylinder, four-stroke, dual ignition, horizontally opposed aircraft engine designed for ultralight aircraft and motor gliders. [1]The engine was designed and produced by the KFM (Komet Flight Motor) Aircraft Motors Division of Italian American Motor Engineering of Italy as a follow-on engine to their KFM 107 series and has been out of production since 1990.

  7. HKS 700E - Wikipedia

    en.wikipedia.org/wiki/HKS_700e

    Data from Cliche & HKS General characteristics Type: Two cylinder, four-stroke aircraft engine Bore: 85 mm (3.3 in) Stroke: 60 mm (2.4 in) Displacement: 680 cc (41.49 cu in) Dry weight: 55 kg (121 lb) equipped with electrical system, electric starter, carburetors, gearbox, exhaust system, oil tank and cooler Components Valvetrain: two intake and two exhaust valves per cylinder Fuel type ...

  8. Verner JCV 360 - Wikipedia

    en.wikipedia.org/wiki/Verner_JCV_360

    The engine is a twin cylinder, 360 cc (22.0 cu in), horizontally-opposed four-stroke, liquid-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratio of 2.76:1. It employs a single electronic ignition and produces 35 hp (26 kW) at 7800 rpm.

  9. Eggenfellner E6 - Wikipedia

    en.wikipedia.org/wiki/Eggenfellner_E6

    Based on Subaru automotive engines, the E6 series are all six cylinder, four-stroke, horizontally-opposed, liquid-cooled, gasoline engine designs, with mechanical gearbox reduction drives with a reduction ratio of 2.02:1. They employ electronic ignition and produce up to 250 hp (186 kW) at 6000 rpm. [1] [2]