发明名称 Forward wing canard aircraft - has leading wing mounted in raised position on strut out of line of vision
摘要 <p>The canard aeroplane with the leading wing in from of the fuselage has that wing (1) mounted on a strut (2) extending axially forwards and upwards from the otherwise conventional nose of the aircraft, providing an unobstructed view in all important directions from the cockpit. The leading wing also acts as a control surface. The corresponding vertical surface (3) may be mounted on the wing support strut as an alternative to being embodied in the vertical stabilising surfaces (6, 7) at the after end of the fuselage. The engines are behind the aircraft's CG but are otherwise conventionally arranged in the tail (8) and/or wings (5).</p>
申请公布号 DE2608042(A1) 申请公布日期 1977.09.01
申请号 DE19762608042 申请日期 1976.02.27
申请人 BINDER,HELLMUTH,DIPL.-ING. 发明人 BINDER,HELLMUTH,DIPL.-ING.
分类号 B64C5/04;(IPC1-7):64C5/04 主分类号 B64C5/04
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