发明名称 Aircraft ejection seat with adjustable headrest
摘要 An aircraft ejection seat includes a frame and a headrest. The vertical position of the seat is adjusted by a pair of motor driven lead screws that cooperate with threaded barrel nuts attached to the seat frame. The upper end of one of these motor driven lead screws drives a slip coupling driving a splined shaft. The splined shaft then drives a gearbox mounted to the seat frame. The gearbox in turn drives an upper lead screw, which acts on an upper barrel nut to move the headrest up and down relative to the seat frame. The upper lead screw is driven in the opposite direction from the lower lead screws. Consequently, as the seat moves up to accommodate a shorter pilot, the headrest moves down to accommodate the shorter torso of the shorter pilot.
申请公布号 US7500639(B2) 申请公布日期 2009.03.10
申请号 US20060445879 申请日期 2006.06.02
申请人 GOODRICH CORPORATION 发明人 MASTROLIA BRAD
分类号 B64D25/02 主分类号 B64D25/02
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