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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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