发明名称 |
Hinged panel operation systems and methods |
摘要 |
A hinged panel operation system (10) is provided having a mechanical linkage assembly (90) coupled between a fixed structure (96) and a trailing edge device (36). The mechanical linkage assembly has a first link (118) operatively coupled to the trailing edge device, a second link (130) pivotably connected at a first end to the first link and pivotably connected at a second end to a third link (142), and an eccentric attachment (154) connecting the second link to the third link. The hinged panel operation system further has a hinged panel (162) 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 |
EP2738087(A2) |
申请公布日期 |
2014.06.04 |
申请号 |
EP20130194967 |
申请日期 |
2013.11.28 |
申请人 |
THE BOEING COMPANY |
发明人 |
BEYER, KEVIN W.;SAKURAI, SEIYA;STEPHENSON, MARTIN F. |
分类号 |
B64C9/10;B64C9/20 |
主分类号 |
B64C9/10 |
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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