发明名称 Aircraft exit door locking system
摘要 An aircraft exit door locking system in which an exit door is automatically locked depending on three dissimilar inputs to a logic system. The inputs are provided from acceleration, pressure, and motion sensors and are utilized in a manner whereby any two can determine whether the lock in the passenger cabin exit door will be energized or deenergized.
申请公布号 US4915326(A) 申请公布日期 1990.04.10
申请号 US19890387387 申请日期 1989.07.31
申请人 THE BOEING COMPANY 发明人 PLUDE, LEO W.
分类号 B64C1/14;E05B47/00;E05B47/06 主分类号 B64C1/14
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