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Curtiss-Wright X-19 : ウィキペディア英語版 | Curtiss-Wright X-19
The Curtiss-Wright X-19 was an American experimental VTOL tiltrotor airplane of the early 1960s. ==Design and development== In March 1960 the Curtiss-Wright Corporation developed the X-100, a prototype for a new, vertical takeoff transport aircraft. The X-100 had a single turboshaft engine, which propelled two tilting-rotors, while at the tail swivelling nozzles used the engine's exhaust gases to give additional control for hovering or slow flight. From the X-100 Curtiss-Wright developed the larger X-200, of which the United States Air Force ordered two prototypes designated the X-19A. The X-19 had high-mounted tandem wings. Each wing mounted a propeller that could be rotated through 90 degrees allowing the aircraft to take off and land like a helicopter. The propellers were driven by twin Avco Lycoming T55-L-5 turboshaft engines mounted in the fuselage.〔Apostolo 1984, p. 63.〕
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「Curtiss-Wright X-19」の詳細全文を読む
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