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Rotor Flight Dynamics LFINO : ウィキペディア英語版 | Rotor Flight Dynamics LFINO
The Rotor Flight Dynamics LFINO (''Leap Flight In Normal Operations'' and pronounced by the designers as "ell if I know") is an American experimental autogyro that was designed by Ernie Boyette and Dick DeGraw, with a single prototype produced by their company Rotor Flight Dynamics of Wimauma, Florida. The aircraft was intended as a proof-of-concept for evaluation for police or paramilitary use.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 185. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The LFINO was designed to test out the use of a powered rotor autogyro to allow zero speed take-offs and landings and more efficient forward flight. The design features a single three-bladed main rotor that was built in-house, a two-seats-in side-by-side configuration enclosed bulbous cockpit, tricycle landing gear mounted on stub wings, a triple tail and a single four cylinder liquid-cooled Subaru automotive engine in pusher configuration.〔 The aircraft's frame is made from aluminium and the cabin is of non-structural fiberglass. The aircraft is equipped with a helicopter-style collective pitch control to allow "jump" takeoffs. Take-offs are accomplished by powering the rotor system to 150% cruise rpm and then increasing collective rapidly to jump the aircraft into the air where it can then fly away.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Rotor Flight Dynamics LFINO」の詳細全文を読む
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