发明名称 |
AIRCRAFT TRAILING EDGE DEVICES, INCLUDING DEVICES WITH NON-PARALLEL MOTION PATHS, AND ASSOCIATED METHODS |
摘要 |
Aircraft trailing edge devices (230) , including devices with non-parallel motion paths (241, 242, 243) , and associated methods are disclosed. A device in accordance with one embodiment includes a wing (220) and an inboard trailing edge (231) device coupled to the wing and movable relative to the wing between a first stowed position and a first deployed position along a first motion path (241) . An outboard trailing edge (232) device can be coupled to the wing outboard of the inboard trailing edge device, and can be movable relative to the wing along a second motion path (242) that is non-parallel to the first motion path. An intermediate trailing edge device (260) can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path (243) that is non-parallel to both the first and second motion paths. Each of the trailing edge devices can open a gap relative to the wing when moved to their respective deployed positions.
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申请公布号 |
CA2628662(C) |
申请公布日期 |
2011.02.22 |
申请号 |
CA20062628662 |
申请日期 |
2006.11.20 |
申请人 |
THE BOEING COMPANY |
发明人 |
LACY, DOUGLAS S.;BEYER, KEVIN W.;BROWN, STEPHEN T.;DEES, PAUL W.;HUYNH, NEAL V.;KORDEL, JAN A.;PROW, CLAYTON A.;SAKURAI, SEIYA |
分类号 |
B64C9/16 |
主分类号 |
B64C9/16 |
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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