发明名称 Aircraft emergency letdown system
摘要 An aircraft letdown system is deployable in the event of power failure or mechanical failure over inhospitable terrain or in the event of environmental conditions which preclude VFR or IFR landings. A parachute system, which is attached to the aircraft at a point in approximate vertical alignment with the aircraft center of gravity, is selectively energized by the pilot when it becomes apparent that a safe normal landing cannot be made. On energization, the parachute canopy and the shroud lines are repositioned from the place of storage to a location external to the aircraft and deployed in the conventional manner. To alleviate the shock of landing to the passengers and cargo, a specially constructed impact absorbing landing gear is extended and the occupants are further protected from the landing shock through impact absorbing seats.
申请公布号 US4108402(A) 申请公布日期 1978.08.22
申请号 US19770758960 申请日期 1977.01.13
申请人 BOWEN, ELEANOR J. 发明人 BOWEN, ARTHUR D.
分类号 B64D17/80;(IPC1-7):B64D17/62 主分类号 B64D17/80
代理机构 代理人
主权项
地址
您可能感兴趣的专利