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Hiller X-18 : ウィキペディア英語版
Hiller X-18


The Hiller X-18 was an experimental cargo transport aircraft designed to be the first testbed for tiltwing and VSTOL (vertical/short takeoff and landing) technology.
==Development==

Design work started in 1955 by Stanley Hiller Jr and Hiller Aircraft Corporation received a manufacturing contract and funding from the U.S. Air Force to build the only X-18 ever produced, serialled ''57-3078''.〔http://www.joebaugher.com/usaf_serials/1957.html〕
To speed up construction and conserve money the plane was constructed from scavenged parts including a Chase YC-122C Avitruc fuselage, ''49-2883'',〔http://www.joebaugher.com/usaf_serials/1957.html〕 and the turboprops came from the Lockheed XFV-1 and Convair XFY-1 Pogo experimental fighter programs. The tri-bladed contra-rotating propellers were a giant 16 ft (4.8 m) across. The Westinghouse turbojet engine had its exhaust diverted upwards and downwards at the tail to give the plane pitch control at low speeds. Hiller nicknamed their X-18 the Propelloplane for public relations purposes.〔("Hiller's Tiltwing Transport if Largest VTOL Transport." )''Popular Mechanics'', March 1959, p. 107.〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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