发明授权
US08038103B2 Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
有权
飞机后缘装置，包括具有向前定位的铰链线的装置以及相关联的方法
- 专利标题： Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
- 专利标题（中）： 飞机后缘装置，包括具有向前定位的铰链线的装置以及相关联的方法
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申请号： US12497493申请日： 2009-07-02
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公开(公告)号： US08038103B2公开(公告)日： 2011-10-18
- 发明人: Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
- 申请人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
- 申请人地址： US IL Chicago
- 专利权人： The Boeing Company
- 当前专利权人： The Boeing Company
- 当前专利权人地址： US IL Chicago
- 代理机构： Perkins Coie LLP
- 主分类号： B64C9/18
- IPC分类号： B64C9/18
摘要：
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.