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31. 发明授权

US08382044B2 High-lift system on the wing of an aircraft, and method for its operation 有权
标题翻译：飞机机翼上的高升力系统及其操作方法
公开(公告)号：US08382044B2
公开(公告)日：2013-02-26
申请号：US12514379
申请日：2007-11-12
申请人： Torsten Holzhausen
发明人： Torsten Holzhausen
IPC分类号： B64C3/58
CPC分类号： B64C9/22 , B64C9/24 , B64C2009/143 , Y02T50/32
摘要： A high-lift system on the wing of an aircraft and a method for its operation are described. High-lift flaps (2) which are arranged on the wing (1) are extended from a retracted position in order to increase the lift, and a slot (3) through which flow passes from the lower face to the upper face of the wing (1) is opened (advanced slat/flap-gap control). According to the invention, the slot (3) through which flow passes is opened independently of the position of the high-lift flap (2). This makes it possible to selectively achieve a better maximum coefficient of lift (CL) or a better lift-to-drag ratio with less noise being produced.
摘要翻译：描述了飞机机翼上的高升力系统及其操作方法。布置在翼（1）上的高升降翼（2）从缩回位置延伸以增加升力，以及从所述翼的下表面到所述翼的上表面通过的槽（3）（1）打开（高级板条/翼片间隙控制）。根据本发明，流过的槽（3）独立于高升降挡板（2）的位置打开。这使得可以选择性地实现更好的最大提升系数（CL）或更好的提升到阻力比，同时产生更少的噪声。

32. 发明申请

US20120234983A1 CONTROL SURFACE ASSEMBLY 有权
标题翻译：控制面组件
公开(公告)号：US20120234983A1
公开(公告)日：2012-09-20
申请号：US13513219
申请日：2010-12-06
申请人： Eric Wildman
发明人： Eric Wildman
IPC分类号： B64C9/20 , B64C13/26 , B64C13/28 , B23P19/00
CPC分类号： B64C13/28 , B64C9/20 , B64C9/323 , B64C2009/143 , Y10T29/49815
摘要： An aerodynamic control surface assembly comprising: an aerodynamic control surface (4); an actuator (10) for controlling deployment of the control surface; and a locking mechanism (30) moveable from a locked to an unlocked position. When the locking mechanism is set to the locked position, the actuator is operatively coupled to the control surface and the control surface can move in dependently of the actuator when the locking mechanism is set to the unlocked position. Such an assembly may be used in an aircraft to prevent clashing between a deployed flap (16) and a drooped spoiler (4) in the event of an actuator control systems failure.
摘要翻译：一种空气动力学控制表面组件，包括：空气动力学控制表面（4）; 用于控制所述控制表面的展开的致动器（10）; 以及可从锁定位置移动到解锁位置的锁定机构（30）。当锁定机构设置在锁定位置时，致动器可操作地联接到控制表面，并且当锁定机构被设置到解锁位置时，控制表面可以依靠致动器移动。在发动机控制系统故障的情况下，这种组件可用于飞行器中以防止展开的挡板（16）和下垂的扰流器（4）之间的冲突。

33. 发明申请

US20120104180A1 KRUEGER 有权
公开(公告)号：US20120104180A1
公开(公告)日：2012-05-03
申请号：US13279642
申请日：2011-10-24
申请人： James BROWN , Edmund KAY
发明人： James BROWN , Edmund KAY
IPC分类号： B64C3/50 , B64D45/00
CPC分类号： B64C9/24 , B64C2009/143 , Y02T50/44
摘要： A Krueger, or leading edge flap, deployable from a lower aerodynamic surface of an aircraft main wing element so as to form a slot between the Krueger and the main wing element when deployed, the deployed Krueger having a leading edge, a trailing edge and upper and lower aerodynamic surfaces extending between the leading edge and the trailing edge, and a flow deflector which provides an effectively divergent flap profile thickness in the downstream direction at or adjacent the Krueger trailing edge so as to direct airflow away from the lower aerodynamic surface of the deployed Krueger towards an upper aerodynamic surface of the main wing element. Also, aircraft wing assembly including a main wing element and the Krueger.
摘要翻译： Krueger或前缘翼片可从飞机主翼元件的下部空气动力学表面展开，以便在部署时在Krueger和主翼元件之间形成槽，部署的Krueger具有前缘，后缘和上部以及在前缘和后缘之间延伸的下部空气动力学表面，以及导流器，其在Krueger后缘处或邻近Krueger后缘处沿下游方向提供有效发散的翼片轮廓厚度，以便将气流从空气动力学表面将Krueger部署到主翼元件的上部空气动力学表面。此外，飞机机翼组件包括主翼元件和Krueger。

34. 发明授权

US08006941B2 System for reducing aerodynamic noise at a supplementary wing of an aircraft 有权
标题翻译：用于降低飞机辅助翼面空气动力学噪音的系统
公开(公告)号：US08006941B2
公开(公告)日：2011-08-30
申请号：US12829831
申请日：2010-07-02
申请人： Thomas Lorkowski , Boris Grohmann
发明人： Thomas Lorkowski , Boris Grohmann
IPC分类号： B64C3/50
CPC分类号： B64C3/50 , B64C9/14 , B64C2009/143
摘要： A system for reducing aerodynamic noise of a supplementary wing of an aircraft is provided. The supplementary wing is hinged to a main wing and is extendable when a gap region between the main wing and the supplementary wing is opened. The system includes a separating surface which can be moved into the gap region when the supplementary wing is extended and which extends at least partially along a separation flow line between a vortex flow region and a gap flow for the air flowing in the gap region. The separating surface is an n-stable surface which through an actuator device can be moved between at least one of the stable states and at least one additional state.
摘要翻译：提供了一种降低飞机辅助翼的气动噪声的系统。辅助机翼铰接到主翼，当主翼和辅助翼之间的间隙打开时，可以延伸。该系统包括分离表面，当分离表面延伸时，该分离表面可以移动到间隙区域中，并且至少部分地沿涡流流动区域和在间隙区域中流动的空气的间隙流之间的分离流线延伸。分离表面是通过致动器装置可以在至少一个稳定状态和至少一个附加状态之间移动的n稳定表面。

35. 发明授权

US07744034B2 Translating flap drive door 有权
标题翻译：翻译挡板驱动门
公开(公告)号：US07744034B2
公开(公告)日：2010-06-29
申请号：US11829780
申请日：2007-07-27
申请人： Ray F. Coughlin
发明人： Ray F. Coughlin
IPC分类号： B64C1/14
CPC分类号： B64C9/16 , B64C2009/143 , Y02T50/32
摘要： In one embodiment, an apparatus is provided for covering and uncovering a flap opening in an aircraft. The apparatus comprises a door member, a torque tube roller member, at least one roller member, and a biasing member. The door member may be adapted to cover and uncover a flap opening. The torque tube roller member may be attached with the door member, and may be adapted to be pushed by a torque tube member attached with a flap of an aircraft. The door member may be adapted to be driven from a closed position covering a flap opening into an open position uncovering a flap opening. The roller member may be attached with the door member and may be adapted to follow at least one track member. The biasing member may be attached with the door member for biasing the door member towards a closed position covering a flap opening.
摘要翻译：在一个实施例中，提供了一种用于覆盖和露出飞行器中的翼片开口的装置。该装置包括门构件，扭矩管辊构件，至少一个辊构件和偏置构件。门构件可以适于覆盖和露出翼片开口。扭矩管辊构件可以与门构件一起安装，并且可以适于被附接有飞行器的翼片的扭矩管构件推动。门构件可以适于从覆盖翼片开口的关闭位置驱动到暴露翼片开口的打开位置。辊构件可以与门构件相连，并且可以适于跟随至少一个轨道构件。偏置构件可以与门构件附接，用于将门构件偏压到覆盖翼片开口的关闭位置。

36. 发明申请

US20070114329A1 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：US20070114329A1
公开(公告)日：2007-05-24
申请号：US11284247
申请日：2005-11-21
申请人： Douglas Lacy , Kevin Beyer , Stephen Brown , Paul Dees , Neal Huynh , Jan Kordel , Clayton Prow , Seiya Sakurai
发明人： Douglas Lacy , Kevin Beyer , Stephen Brown , Paul Dees , Neal Huynh , Jan Kordel , Clayton Prow , Seiya Sakurai
IPC分类号： B64C39/06
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。

37. 发明授权

US2668027A Airplane flap and ground contact control means therefor 失效
标题翻译：飞机挡板和接地控制装置
公开(公告)号：US2668027A
公开(公告)日：1954-02-02
申请号：US4350348
申请日：1948-08-10
申请人： BURNELLI VINCENT J
发明人： BURNELLI VINCENT J
IPC分类号： B64C21/02
CPC分类号： B64C21/02 , B64C2009/143 , B64C2230/06 , B64C2230/20 , Y02T50/166

38. 发明授权

US2556326A Airplane flap with slot controller 失效
标题翻译：带狭槽控制器的飞机挡板
公开(公告)号：US2556326A
公开(公告)日：1951-06-12
申请号：US58730245
申请日：1945-04-09
申请人： GRANT CHARLES H
发明人： GRANT CHARLES H
IPC分类号： B64C9/16
CPC分类号： B64C9/16 , B64C2009/143

39. 发明授权

US2381678A Airplane wing 失效
公开(公告)号：US2381678A
公开(公告)日：1945-08-07
申请号：US43031742
申请日：1942-02-11
申请人： MAXWELL FRANK R
发明人： MAXWELL FRANK R
IPC分类号： B64C9/22 , B64C21/02
CPC分类号： B64C9/22 , B64C21/02 , B64C2009/143 , B64C2230/06 , B64C2230/20 , Y02T50/166

40. 发明授权

US2321837A Airplane and control device therefor 失效
标题翻译：飞机及其控制装置
公开(公告)号：US2321837A
公开(公告)日：1943-06-15
申请号：US36534740
申请日：1940-11-12
申请人： MAKWELL FRANK R
发明人： MAKWELL FRANK R
IPC分类号： B64C9/22 , B64C21/02
CPC分类号： B64C9/22 , B64C21/02 , B64C2009/143 , B64C2230/06 , B64C2230/20 , Y02T50/166

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