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Hovey Delta Bird : ウィキペディア英語版 | Hovey Delta Bird
The Hovey Delta Bird is an American ultralight aircraft that was designed by Bob Hovey in 1982 and supplied as plans for amateur construction.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-12 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Design and development== The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a biplane wing configuration, a single-seat, open cockpit, conventional landing gear and a single engine in tractor configuration.〔 The aircraft is made from pop-riveted and gusseted aluminum tubing, with the wings and tail surfaces covered in doped aircraft fabric covering. Its biplane wing has a top span of , a bottom span of , employs cabane struts and one set of interplane struts. The controls are conventional three-axis, with full-span ailerons on the top wing. The landing gear is bungee suspended and includes main wheel brakes and tailwheel steering. Common engines used include the Cuyuna 430R in the Delta Bird and the Kawasaki 440 in the Delta Hawk.〔
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「Hovey Delta Bird」の詳細全文を読む
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