发明名称 Dual lost motion mechanism for an aircraft door
摘要 A pair of four-bar linkages employing lost motion incorporated into an aircraft door construction which simultaneously are operable by a main door handle so that the output crank of each linkage has a dwell which is sequenced such that the operation of the associated latches and door hinges are properly timed and sequenced for opening and closing of the door.
申请公布号 US4180943(A) 申请公布日期 1980.01.01
申请号 US19780942879 申请日期 1978.09.15
申请人 MCDONNELL DOUGLAS CORP 发明人 BLACKMORE, DAVID M;SMITH, HUGH D
分类号 B64C1/14;E05C9/06;(IPC1-7):E05F11/54 主分类号 B64C1/14
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