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Data from OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582 General characteristics Type: two-stroke air-cooled aeroengine Bore: 67.5 mm (2.66 in) Stroke: 61 mm (2.4 in) Displacement: 426.5 cc (26.64 cu in) Dry weight: 26.8 kg (59 lb) (dry, no exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: regular autofuel Oil system: premixed in the fuel ...
The aircraft replaces the Spyder's two-stroke engine with a Yuneec Power Drive 20 20 kW (27 hp) electric motor and two 28 lb (13 kg) Lithium polymer battery packs which provide a 40-minute endurance. The aircraft is intended to be developed into a commercially available kit and forecast to be available for under US$25,000. [7] [8] [9]
The larger engines, some 2000cc and all 2400cc, are based on the Volkswagen Wasserboxer engine. The most powerful versions of the 2400cc engines have water cooled cylinder heads as well as electronic fuel injection and electronic ignition. Limbach also makes two-stroke engines for UAV as well as uncertified versions of a few four-stroke engines ...
The L275E is a twin cylinder horizontally-opposed two-stroke, air-cooled, direct-drive petrol engine design, based upon the Volkswagen air-cooled engine.It employs a single magneto ignition, two carburettors, is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 for synthetic oil and produces 15 kW (20 hp) at 7200 rpm.
It features a single main rotor and tail rotor, a single-seat enclosed cockpit with a windshield, skid landing gear and a two-cylinder, air-cooled, two stroke 64 hp (48 kW) MZ 202 engine. [1] The aircraft fuselage is made from composites and metal tubing. Its two-bladed rotor has a diameter of 5.95 m (19.5 ft) and a chord of 17 cm (6.7 in).
It is equipped with a recoil starter system or optionally electric start and a 2.5 or 2.8:1 belt reduction drive. [1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 22 hp (16 kW) at 6600 rpm, the G-25 competed in the early 1980s ultralight powerplant market against the similar Rotax 277. Production of the ...
The L550E is an air-cooled horizontally-opposed 550cc four-cylinder two-stroke petrol engine developing 37 kW (50 hp) at 7500 rpm which can drive a propeller either directly or geared. It employs a single magneto ignition, four carburettors , and is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 ...
Powerplant: 1 × McCulloch Model 4318AX 4-cylinder air-cooled 2-stroke horizontally-opposed piston engine, 72 hp (54 kW) Main rotor diameter: 20 ft 0 in (6.10 m) Main rotor area: 314.2 sq ft (29.19 m 2) Blade section: Bensen G2; Propellers: 2-bladed Aero Prop Model BA 48-A2fixed-pitch pusher propeller, 4 ft 0 in (1.22 m) diameter; Performance
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