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The engines were replaced by Pratt & Whitney Canada PW610Fs in 2004 and Eclipse Aviation won the Collier Trophy in February 2006 for the design. A provisional FAA type certification was received on 27 July 2006 and the first delivery occurred on 31 December 2006. The six-seat aircraft has an all-metal airframe with a T-tail and straight wings.
The engine is a single rotor four-stroke, air and liquid-cooled, 294 cc (17.9 cu in) gasoline Wankel engine design, with a mechanical gearbox reduction drive employing a helical gear set with a reduction ratio of 3.225:1. Cooling is predominantly liquid, with forced air cooling for the rotor core. A starter and generator are standard equipment.
This is a cross-country airplane with many exclusive features including carbon fiber construction, pressurized cabin, high strutless wing, and seating for six. The EA-500 was introduced as an alternative version of the EA-400 with the piston engine replaced by a Rolls-Royce Model 250 -B17F/2 turboprop yielding 450 horsepower (340 kW), weighing ...
Source: RMV, Able Experimental Aircraft Engine Co. [6] (Able Experimental Aircraft Engine Co., Altimizer, Hoverhawk ... Air-cooled Anzani engines. Anzani V-2 [31]
It needed to have folding wings and be able to be towed behind, or carried on the back of a 2.5te truck. It was also required to be towed by other aircraft, to extend the aircraft's range. [1] At least eight projects were submitted to meet the requirement for a lighter aircraft, with Aero's design, the Ae 50, considered the best of the proposals.
Like the 500, the 550 is a low-wing, six seat, twin engine jet-powered aircraft. [3] The Eclipse 550 is certified for single-pilot operation. The aircraft was announced at the National Business Aviation Association convention in Las Vegas, Nevada in October 2011. The first example was rolled out in March 2013 and the first customer delivery was ...
Data from Junkers aircraft and engines, 1913-1945, Junkers: an aircraft album General characteristics Length: 7.12 m (23 ft 4 in) Wingspan: 10 m (32 ft 10 in) Height: 2.39 m (7 ft 10 in) Wing area: 13.7 m 2 (147 sq ft) Empty weight: 340 kg (750 lb) Gross weight: 590 kg (1,301 lb) Fuel capacity: 95 L (25 US gal; 21 imp gal) Powerplant: 1 × Armstrong Siddeley Genet II five-cylinder air-cooled ...
ARV Super2 with AE110. Very closely based upon the Norton engine, the MidWest engine developed the design further. The lubrication system became a semi-total-loss system whereby Silkolene 2-stroke oil was directly injected into the inlet tracts and onto the main roller bearings, but the oil that fed the bearings became an oil-mist within the rotor-cooling air, with about 30% [4] of the oil ...
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