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7. 发明申请

US20090146017A1 Aircraft Trailing Edge Devices, Including Devices With Non-Parallel Motion Paths, and Associated Methods 有权
标题翻译：飞机后端设备，包括具有非并行运动路径的设备以及相关方法
公开(公告)号：US20090146017A1
公开(公告)日：2009-06-11
申请号：US12264831
申请日：2008-11-04
申请人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
发明人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
IPC分类号： B64C3/50 , B64C13/00 , B64C3/18
CPC分类号： B64C9/16 , B64C2009/143
摘要： Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods are disclosed. A device in accordance with one embodiment includes a wing and an inboard trailing edge 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. An outboard trailing edge 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 that is non-parallel to the first motion path. An intermediate trailing edge device can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path 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.
摘要翻译：公开了包括具有非平行运动路径的装置和相关方法的飞行器后缘装置。根据一个实施例的装置包括机翼和内侧后缘装置，其联接到机翼并且可沿着第一运动路径在第一收起位置和第一展开位置之间相对于机翼移动。外侧后缘装置可以联接到内侧后缘装置的翼外侧，并且可以沿着不平行于第一运动路径的第二运动路径相对于机翼移动。中间后缘装置可以联接在内侧和后侧后缘装置之间，并且可以沿着不平行于第一和第二运动路径的第三运动路径移动。每个后缘装置可以在移动到它们各自的展开位置时相对于机翼打开间隙。

8. 发明授权

US07475854B2 Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods 有权
标题翻译：飞机后缘装置，包括具有非平行运动路径的装置，以及相关方法
公开(公告)号：US07475854B2
公开(公告)日：2009-01-13
申请号：US11284247
申请日：2005-11-21
申请人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
发明人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
IPC分类号： B64C3/50
CPC分类号： B64C9/16 , B64C2009/143
摘要： Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods are disclosed. A device in accordance with one embodiment includes a wing and an inboard trailing edge 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. An outboard trailing edge 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 that is non-parallel to the first motion path. An intermediate trailing edge device can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path 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.
摘要翻译：公开了包括具有非平行运动路径的装置和相关方法的飞行器后缘装置。根据一个实施例的装置包括机翼和内侧后缘装置，其联接到机翼并且可沿着第一运动路径在第一收起位置和第一展开位置之间相对于机翼移动。外侧后缘装置可以联接到内侧后缘装置的翼外侧，并且可以沿着不平行于第一运动路径的第二运动路径相对于机翼移动。中间后缘装置可以联接在内侧和后侧后缘装置之间，并且可以沿着不平行于第一和第二运动路径的第三运动路径移动。每个后缘装置可以在移动到它们各自的展开位置时相对于机翼打开间隙。

9. 发明授权

US4429844A Variable camber aircraft wing tip 失效
公开(公告)号：US4429844A
公开(公告)日：1984-02-07
申请号：US451216
申请日：1982-09-29
申请人： Stephen T. Brown , Frank D. Statkus
发明人： Stephen T. Brown , Frank D. Statkus
IPC分类号： B64C3/48
CPC分类号： B64C3/48
摘要： A variable wing tip (18) for securing to a variable camber leading edge portion (12) of an aircraft wing (10). The wing tip has a normal fore and aft camber in an upper position and is adapted to have an increased camber curvature in a deflected down position. In the down position, the wing tip has a compound curvature, is shortened in the fore and aft direction ad is generally thickened in depth in a substantial portion of the wing tip. By operation of an actuator (96) in the leading edge (21), a multiple of generally parallel scissor plates (30,32) are pivoted apart. The plates extend in an inboard outboard direction and are spaced in the fore and aft direction. The scissor plates are pairs of upper and lower plates with respect to the upper and lower surface of the wing tip, the upper plates (30) being adapted to be pivotally secured inboard to a complementary outer portion of the wing leading edge to secure the upper portion of the wing tip thereto, and the lower plates (32) being pivotally and slidably secured inboard within the wing tip and being adapted to be secured to a complementary outer portion of the wing leading edge to secure the lower portion of the wing tip thereto. Each respective pair of upper and lower plates are pivotally secured together outboard (40) adjacent and outboard leading edge (42) of the wing tip. Respective upper and lower plates are adapted to be pivoted apart inwardly of and on the outboard pivots (40) when the camber is increased in the down position so as to increase the depth of and shorten the fore and aft direction of the wing tip. An elastomer (84) is bonded to the plates, permitting the plates to be pivoted apart. An elastomeric wing tip configuration (88), is secured to the wing leading edge and to a forwardly facing edge of the wing. The elastomeric configuration has the normal camber of the wing tip in the upper position and the increased camber and compound curvature of the wing tip in the deflected position. It forms continuous surfaces in the varied camber positions with the wing.

10. 发明授权

US07744040B2 Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods 有权
标题翻译：飞机后缘装置，包括具有非平行运动路径的装置，以及相关方法
公开(公告)号：US07744040B2
公开(公告)日：2010-06-29
申请号：US12264831
申请日：2008-11-04
申请人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
发明人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
IPC分类号： B64C3/50
CPC分类号： B64C9/16 , B64C2009/143
摘要： Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods are disclosed. A device in accordance with one embodiment includes a wing and an inboard trailing edge 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. An outboard trailing edge 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 that is non-parallel to the first motion path. An intermediate trailing edge device can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path 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.
摘要翻译：公开了包括具有非平行运动路径的装置和相关方法的飞行器后缘装置。根据一个实施例的装置包括机翼和内侧后缘装置，其联接到机翼并且可沿着第一运动路径在第一收起位置和第一展开位置之间相对于机翼移动。外侧后缘装置可以联接到内侧后缘装置的翼外侧，并且可以沿着不平行于第一运动路径的第二运动路径相对于机翼移动。中间后缘装置可以联接在内侧和后侧后缘装置之间，并且可以沿着不平行于第一和第二运动路径的第三运动路径移动。每个后缘装置可以在移动到它们各自的展开位置时相对于机翼打开间隙。

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