发明名称 HINGED PANEL OPERATION SYSTEMS AND METHODS
摘要 A hinged panel operation system is provided having a mechanical linkage assembly coupled between a fixed structure and a trailing edge device. The mechanical linkage assembly has a first link operatively coupled to the trailing edge device, a second link pivotably connected at a first end to the first link and pivotably connected at a second end to a third link, and an eccentric attachment connecting the second link to the third link. The hinged panel operation system further has a hinged panel positioned forward of the trailing edge device and being operatively coupled to the mechanical linkage assembly. The hinged panel is movable by the mechanical linkage assembly between a stowed position and a drooped position. The mechanical linkage assembly provides a load path to the hinged panel.
申请公布号 CA2826502(A1) 申请公布日期 2014.05.29
申请号 CA20132826502 申请日期 2013.09.04
申请人 THE BOEING COMPANY 发明人 BEYER, KEVIN W;SAKURAI, SEIYA;STEPHENSON, MARTIN F.
分类号 B64C13/28;B64C3/50;F16C11/04;F16H21/12 主分类号 B64C13/28
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