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In its standard configuration, the aircraft is a true double-delta with no horizontal stabilizer; however, a small T-tail is an option for trimming variants with higher-power engines. Since the mid-1960s, designer John Dyke has sold full construction plans and three-view drawings for the aircraft to homebuilders and is still selling them today.
Engine designers had always been aware of the many limitations of the rotary engine, so when static style engines became more reliable and gave better specific weights and fuel consumption, the days of the rotary engine were numbered. Rotary engines had a fundamentally inefficient total-loss oiling system. In order to reach the whole engine ...
[3] [4] The engine retained the Clerget’s signature offset epicyclical cam gears with separate pushrods for the intake and exhaust. In common with many other late war rotary engines, the new engine had two spark plugs per cylinder. [4] The engine was initially known as the A.R.1 for "Admiralty Rotary", but later called the BR.1 ("Bentley ...
Later models of the motorcycle dispensed with the pedals, and the engine was lowered to improve the centre of gravity. No known models of the engine exist but a similar Redrup 1912 rotary aircraft engine is in the Museum of Science and Industry in Manchester, and Redrup Radial, later engines designed and built by Redrup, are still in existence. [4]
The Le Rhône 9C is a nine-cylinder rotary aircraft engine produced in France by Société des Moteurs Le Rhône / Gnome et Rhône. Also known as the Le Rhône 80 hp in a reference to its nominal power rating, the engine was fitted to many military aircraft types during the First World War. Le Rhône 9C engines were also produced under license ...
It was shown at the Paris Aero Salon held in December 1908 and was first flown in 1909. It was the world's first [1] aviation rotary engine produced in quantity. Its introduction revolutionized the aviation industry [3] and it was used by many early aircraft. It produced 37 kW (50 hp) from its 8 L (490 cu in) engine capacity. [4]
The Bentley B.R.2 was a nine-cylinder British rotary aircraft engine developed during the First World War by the motor car engine designer W. O. Bentley from his earlier Bentley BR.1. The BR.2 was built in small numbers during the war, its main use being by the Royal Air Force in the early 1920s. [1]
A variety of engine types have been used, including 50 to 80 hp (37 to 60 kW) Volkswagen air-cooled engines, the 80 hp (60 kW) Rotax 912UL and the 85 hp (63 kW) Jabiru 2200. [1] [2] The aircraft is built from plans, although some parts are available as well. [2] Additionally Aircraft Spruce & Specialty offer materials kits for the design. [3]