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Rotortec Cloud Dancer II : ウィキペディア英語版
Rotortec Cloud Dancer II

The Rotortec Cloud Dancer II is a German autogyro, designed by Jochen Steinbeck and produced by Rotortec of Görisried, Allgäu. The aircraft was first shown at AERO Friedrichshafen in 2009 and is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 186. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The Cloud Dancer II features a single four-bladed main rotor, a two-seats in side-by-side configuration enclosed cockpit, tricycle landing gear with wheel pants and a twin cylinder, air-cooled, four-stroke, turbocharged Rotortec MPE engine that was developed in-house and is mounted in pusher configuration. It drives a three-bladed composite propeller though a planetary reduction drive.〔
The aircraft fuselage and the three vertical surface tail are made from aluminum and Kevlar composites. Its diameter rotor has a chord of and is equipped with a micro-processor controlled hydraulic pre-rotator. The prototype aircraft mounted a three-bladed main rotor, but this was changed to a four-bladed unit during development. The four-bladed rotor provides improved vibration levels, but at the cost of requiring larger space for storage. An electronic touchscreen instrument panel is standard equipment. The aircraft has an empty weight of and a gross weight of , giving a useful load of . The fuel tanks hold , giving a full fuel payload of .〔



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