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1. 发明授权

US08998135B1 Translating equipment rack system 有权
标题翻译：翻译设备机架系统
公开(公告)号：US08998135B1
公开(公告)日：2015-04-07
申请号：US13102265
申请日：2011-05-06
申请人： Andrew John Bayliss , Stephen T. Brown , Perry Nicholas Rea , Kevin Matthew Retz
发明人： Andrew John Bayliss , Stephen T. Brown , Perry Nicholas Rea , Kevin Matthew Retz
IPC分类号： B64C1/22 , B64C3/14
CPC分类号： B64C1/22 , B64C1/1446 , B64C3/141 , B64D43/00 , B64D47/00 , H05K7/1411 , H05K7/18 , Y10T292/0802 , Y10T292/0807
摘要： An apparatus and method comprising a rack and a translation mechanism. The rack may be configured to hold components. The rack may comprise movable rack segments that are movable independently of each other. The translation mechanism may be configured to move a portion of the movable rack segments relative to another portion of the movable rack segments inside a platform such that internal access to at least a portion of the components is provided inside the platform.
摘要翻译：一种包括机架和平移机构的装置和方法。机架可能被配置为保持组件。机架可以包括可彼此独立移动的可移动齿条段。平移机构可以被配置为使可移动齿条段的一部分相对于可移动齿条段的另一部分移动到平台内，使得至少部分组件的内部通路设置在平台内。

2. 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。

3. 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。

4. 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.

5. 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。

10. 发明授权

US07575194B2 Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures 有权
标题翻译：用于将复合构件和其他结构构件连接在飞机机翼箱和其他结构中的装置和方法
公开(公告)号：US07575194B2
公开(公告)日：2009-08-18
申请号：US11607333
申请日：2006-11-30
申请人： Stephen T. Brown , Max U. Kismarton
发明人： Stephen T. Brown , Max U. Kismarton
IPC分类号： B64C3/18 , B64C1/06
CPC分类号： B64C1/26
摘要： Apparatuses and methods for joining composite members and other structural members in aircraft wings and other structures. An aircraft wing box structure configured in accordance with one embodiment of the invention includes a first composite member having a first surface portion positioned at an angel relative to a second surface portion of a second composite member. The wing box structure of this embodiment further includes at least one metallic joining member having an upstanding leg portion extending from a base portion. The base portion of the joining member is bonded to the first surface portion of the first composite member with a first portion of adhesive, and the upstanding leg portion of the metallic joining member is bonded to the second surface portion of the second composite member with a second portion of adhesive.
摘要翻译：用于在飞机机翼和其他结构中连接复合构件和其他结构构件的装置和方法。根据本发明的一个实施例构造的飞行器翼盒结构包括第一复合构件，其具有相对于第二复合构件的第二表面部分成一角度定位的第一表面部分。本实施例的翼盒结构还包括至少一个金属接合构件，其具有从基部延伸的直立的腿部。接合构件的基部用第一粘合剂部分粘合到第一复合构件的第一表面部分，并且金属接合构件的直立腿部分与第二复合构件的第二表面部分接合粘合剂的第二部分。

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