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Twin-cylinder in-line, two stroke, aircraft engine with dual or optionally a single Bing 34mm slide carburetor. Produces 55 hp (41 kW) at 6200 rpm and has a factory rated TBO of 1000 hours. The 2703 has been largely supplanted in production by the Hirth 3202 , but in 2009 was still available as a special order from the factory.
The reduction drive system available is the G-50 gearbox, with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1. [ 1 ] The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil, or optionally 100:1 oil injection.
It is equipped with a recoil starter system or optionally electric start and a 2.1 or 2.6:1 belt reduction drive. [1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 45 hp (34 kW) at 5800 rpm, the G-50 competed in the early 1980s ultralight powerplant market against the similar Rotax 447. Production of the ...
Data from Cliche General characteristics Type: Twin cylinder, two-stroke, aircraft engine Displacement: 383 cc (23.4 cu in) Dry weight: 70 lb (31.8 kg) Components Valvetrain: piston-ported Fuel system: 1 X Bing carburetor Fuel type: unleaded 93 octane auto fuel Oil system: 50:1 fuel/oil premix Cooling system: fan forced air Reduction gear: optional gearbox Performance Power output: 30 hp (22 ...
Data from Recreational Power Engineering General characteristics Type: Twin cylinder, two-stroke, aircraft engine Bore: 72 mm (2.8 in) Stroke: 64 mm (2.5 in) Displacement: 521 cc (31.8 cu in) Length: 247 mm (9.7 in) Width: 570 mm (22.4 in) Height: 338 mm (13.3 in) Dry weight: 84 lb (38.1 kg) including reduction unit, full exhaust system and electric start Components Valvetrain: piston-ported ...
Animation of a two-stroke engine. A two-stroke (or two-stroke cycle) engine is a type of internal combustion engine that completes a power cycle with two strokes of the piston (one up and one down movement) in one revolution of the crankshaft in contrast to a four-stroke engine which requires four strokes of the piston in two crankshaft revolutions to complete a power cycle.
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Data from ROTAX 377 UL Data Sheet General characteristics Type: two-stroke air-cooled aeroengine Bore: 62 mm (2.44 in) Stroke: 61 mm (2.40 in) Displacement: 368.3 cc (22.48 cu in) Dry weight: 38.4 kg (84.6 lb) (complete including reduction drive and exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: premium unleaded autofuel Oil system ...