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公开(公告)号：US20160288903A1
公开(公告)日：2016-10-06
申请号：US15077268
申请日：2016-03-22
申请人： U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
CPC分类号： B64C29/0033 , B64C9/04 , Y02T50/32 , Y02T50/44
摘要： A vehicle includes a wing and a control surface pivotably coupled to the wing and configured to pivot about a range of motion. A propulsor is coupled to the control surface and configured to rotate between a first position associated with a hover flight mode and a second position associated with a forward flight mode. The propulsor is aerodynamically actuated between the first position and the second position due to aerodynamics about the wing. The propulsor may rotate from an initial flight mode, such as a takeoff mode, to a second flight mode, such as a forward flight mode.
摘要翻译： 车辆包括机翼和控制表面，所述机翼和控制表面可枢转地联接到机翼并且被配置为围绕一定范围的运动枢转。 推进器联接到控制表面并且被配置为在与悬停飞行模式相关联的第一位置与与向前飞行模式相关联的第二位置之间旋转。 由于关于机翼的空气动力学，推进器在第一位置和第二位置之间被空气动力学地启动。 推进器可以从初始飞行模式（例如起飞模式）旋转到第二飞行模式，例如前进飞行模式。
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62.发明授权Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement 有权用于飞机机翼的翼片布置和具有这种翼片装置的机翼的飞机公开(公告)号：US09452821B2
公开(公告)日：2016-09-27
申请号：US14280812
申请日：2014-05-19
发明人： Sascha Aljets
摘要： A flap arrangement for a wing of an aircraft includes a base member, at least one first flap, at least one second flap and at least one connecting assembly. The first flap is movably supported on the base member and the second flap is movably supported on the first flap. The connecting assembly is mechanically coupled with the base member and the second flap and is designed to move the second flap relative to the first flap when the first flap is moved relative to the base member. Due to the resulting forced guiding of a second flap relative to a first flap a separate actuator for moving the second flap and linkages extending outside of the shape defining contour of the flap arrangement may substantially be eliminated.
摘要翻译： 用于飞机机翼的翼片装置包括基座构件，至少一个第一翼片，至少一个第二翼片和至少一个连接组件。 第一翼片可移动地支撑在基座构件上，并且第二翼片可移动地支撑在第一翼片上。 所述连接组件与所述基座构件和所述第二翼片机械地联接，并且被设计成当所述第一翼片相对于所述基座构件移动时相对于所述第一翼片移动所述第二翼片。 由于相对于第一挡板导致的第二翼片的强制引导，基本上可以消除用于移动延伸到翼片装置的形状限定轮廓外侧的第二翼片和连杆的单独的致动器。
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公开(公告)号：US09340278B2
公开(公告)日：2016-05-17
申请号：US14275102
申请日：2014-05-12
摘要： A system and method for a controlling an aircraft with flight control surfaces that are controlled both manually and by a computing device is disclosed. The present invention improves overall flight control operation by reducing the mechanical flight control surface components while providing sufficient back-up control capability in the event of either a mechanical or power-related failure. Through the present invention, natural feedback is provided to the operator from the mechanical flight control surface which operates independent of computer-aided flight control surfaces. Further, through the present invention, force input signals received from the pilot are filtered to improve the operation of the computer-aided flight control surfaces.
摘要翻译： 公开了一种用于控制具有由手动控制的飞行控制表面和由计算装置控制的飞行器的系统和方法。 本发明通过减少机械飞行控制表面部件同时在机械或电力相关故障的情况下提供足够的后备控制能力来改进总体飞行控制操作。 通过本发明，自动反馈从机械飞行控制表面提供给操作者，该机械飞行控制表面独立于计算机辅助飞行控制表面操作。 此外，通过本发明，对从飞行员接收的力输入信号进行滤波，以改善计算机辅助飞行控制表面的操作。
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64.发明申请FLAP ARRANGEMENT FOR A WING OF AN AIRCRAFT AND AN AIRCRAFT WITH A WING COMPRISING SUCH A FLAP ARRANGEMENT 有权飞行员飞行员的飞行员安排和包含这种飞行员安排的飞机的飞行员安排公开(公告)号：US20140346282A1
公开(公告)日：2014-11-27
申请号：US14280812
申请日：2014-05-19
发明人： Sascha Aljets
摘要： A flap arrangement for a wing of an aircraft includes a base member, at least one first flap, at least one second flap and at least one connecting assembly. The first flap is movably supported on the base member and the second flap is movably supported on the first flap. The connecting assembly is mechanically coupled with the base member and the second flap and is designed to move the second flap relative to the first flap when the first flap is moved relative to the base member. Due to the resulting forced guiding of a second flap relative to a first flap a separate actuator for moving the second flap and linkages extending outside of the shape defining contour of the flap arrangement may substantially be eliminated.
摘要翻译： 用于飞机机翼的翼片装置包括基座构件，至少一个第一翼片，至少一个第二翼片和至少一个连接组件。 第一翼片可移动地支撑在基座构件上，并且第二翼片可移动地支撑在第一翼片上。 所述连接组件与所述基座构件和所述第二翼片机械地联接，并且被设计成当所述第一翼片相对于所述基座构件移动时相对于所述第一翼片移动所述第二翼片。 由于相对于第一挡板导致的第二翼片的强制引导，基本上可以消除用于移动延伸到翼片装置的形状限定轮廓外侧的第二翼片和连杆的单独的致动器。
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公开(公告)号：US08401716B2
公开(公告)日：2013-03-19
申请号：US11669565
申请日：2007-01-31
IPC分类号： G01C23/00 , G05D1/00 , G05D3/00 , G06F17/00 , G06F7/00 , B64C19/00 , B64C13/00 , B64C3/18 , B64C13/16 , B64C17/00 , B64C9/00 , B64C13/40
CPC分类号： B64C9/04 , B64C9/10 , B64C13/38 , B64C13/503
摘要： A system and method for a controlling an aircraft with flight control surfaces that are controlled both manually and by a computing device is disclosed. The present invention improves overall flight control operation by reducing the mechanical flight control surface components while providing sufficient back-up control capability in the event of either a mechanical or power-related failure. Through the present invention, natural feedback is provided to the operator from the mechanical flight control surface which operates independent of computer-aided flight control surfaces.
摘要翻译： 公开了一种用于控制具有由手动控制的飞行控制表面和由计算装置控制的飞行器的系统和方法。 本发明通过减少机械飞行控制表面部件同时在机械或电力相关故障的情况下提供足够的后备控制能力来改进总体飞行控制操作。 通过本发明，自动反馈从机械飞行控制表面提供给操作者，该机械飞行控制表面独立于计算机辅助飞行控制表面操作。
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公开(公告)号：US08380364B2
公开(公告)日：2013-02-19
申请号：US11383791
申请日：2006-05-17
IPC分类号： G01C23/00 , G05D1/00 , G05D3/00 , G06F7/00 , G06F17/00 , B64C29/00 , B64C3/38 , B64C5/10 , B64C9/00 , B64C13/00 , B64C13/50
CPC分类号： B64C13/04 , B64C9/04 , B64C9/10 , B64C13/38 , B64C13/503
摘要： A system and method for a controlling an aircraft with flight control surfaces that are controlled both manually and by a computing device is disclosed. The present invention improves overall flight control operation by reducing the mechanical flight control surface components while providing sufficient back-up control capability in the event of either a mechanical or power-related failure. Through the present invention, natural feedback is provided to the operator from the mechanical flight control surface which operates independent of computer-aided flight control surfaces.
摘要翻译： 公开了一种用于控制具有由手动控制的飞行控制表面和由计算装置控制的飞行器的系统和方法。 本发明通过减少机械飞行控制表面部件同时在机械或电力相关故障的情况下提供足够的后备控制能力来改进总体飞行控制操作。 通过本发明，自动反馈从机械飞行控制表面提供给操作者，该机械飞行控制表面独立于计算机辅助飞行控制表面操作。
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67.发明授权Actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device 有权基于形状记忆合金的致动器装置和装配有这种致动器装置的翼片组件公开(公告)号：US08348201B2
公开(公告)日：2013-01-08
申请号：US12507677
申请日：2009-07-22
申请人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
发明人： Rosario Pecora , Generoso Iannuzzo , Massimo Riccio , Salvatore Russo , Erika Calvi , Leonardo Lecce , Silvestro Barbarino , Antonio Concilio , Salvatore Ameduri
IPC分类号： B64C3/58
摘要： A wing-flap assembly includes a flap made up of a plurality of flap sections, in which each flap section is connected to the preceding one in a rotatable manner, and one or more actuator devices adapted to control the rotation of the flap sections. Each actuator device includes an extended element made of shape memory alloy and an arch-shaped framework made of elastic material, to which the extended element is fixedly connected under tension. Each end of the extended element is fixed to a respective end of the arch-shaped framework. At least one of the actuator devices is connected at one end to the first of the flap sections, and on the other side it is adapted to be connected to a wing structure.
摘要翻译： 翼片组件包括由多个翼片部分构成的翼片，其中每个翼片部分以可旋转的方式连接到前一个翼片部分，以及适于控制翼片部分的旋转的一个或多个致动器装置。 每个致动器装置包括由形状记忆合金制成的延伸元件和由弹性材料制成的拱形框架，延伸元件在张力下固定连接到该延伸元件。 延伸元件的每个端部固定到拱形框架的相应端部。 致动器装置中的至少一个在一端连接到第一翼片部分，并且另一侧适于连接到机翼结构。
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68.发明申请ADJUSTING MECHANISM FOR KINEMATIC GUIDANCE OF AN ADJUSTABLE BODY DURING ITS ADJUSTMENT ON A SUPPORTING STRUCTURAL COMPONENT, ADJUSTING MECHANISM FOR KINEMATIC ADJUSTMENT OF A HIGH LIFT BODY, AND HIGH LIFT SYSTEM COMPRISING A LIKE ADJUSTING MECHANISM 有权调整机构在调整支持结构部件时调整可调节机构的动力学指标，调整高吊杆机构动态调整机构和包含类似调整机构的高牵引系统公开(公告)号：US20120248257A1
公开(公告)日：2012-10-04
申请号：US13410381
申请日：2012-03-02
申请人： Jochen EICHHORN , Tom DOSTMANN , Bernhard SCHLIPF
发明人： Jochen EICHHORN , Tom DOSTMANN , Bernhard SCHLIPF
摘要： An mechanism for kinematic guidance of a body during its adjustment on a supporting structure. The body is moved between a refracted position and an extended position while performing a movement in a longitudinal direction in combination with a rotary movement. The mechanism includes first and second transmission levers for coupling to the supporting structure, a base connection lever to which these levers are coupled, third and fourth transmission levers coupled to the base connection lever, an adjusting lever coupled to the third and fourth transmission levers for attachment of the adjustable body, to adjust the body by a movement of the adjusting lever, and a coupling lever coupled to the first or second transmission lever and to the third or fourth transmission lever. During a movement of the adjusting lever, the first and second transmission levers each move opposite to the third and fourth transmission levers.
摘要翻译： 一种在支撑结构调整期间身体运动引导的机构。 身体在折射位置和延伸位置之间移动，同时结合旋转运动沿长度方向进行运动。 该机构包括用于联接到支撑结构的第一和第二传动杆，连接这些杠杆的基座连接杆，联接到基座连接杆的第三和第四传动杆，连接到第三和第四传动杆的调节杆， 可调整体的附接，通过调节杆的移动来调节身体，以及联接杆，其联接到第一或第二传动杆和第三或第四传动杆。 在调节杆的移动期间，第一和第二传动杆每个与第三和第四传动杆相对移动。
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公开(公告)号：US08256710B2
公开(公告)日：2012-09-04
申请号：US11855342
申请日：2007-09-14
申请人： Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
发明人： Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
摘要： A trim tab is disclosed for use on an aerodynamic foil that has first and second surfaces which extend between a leading edge and a trailing edge. Structurally, the trim tab includes a tab member that is bounded by slits formed through each surface to extend from the trailing edge toward the leading edge. Also, the tab member is bounded by a slot formed between the slits on the second surface to establish a flange between the slot and the trailing edge. Further, the trim tab includes an actuator that is mounted on the foil between the slot and the leading edge. The actuator includes an actuator arm that is connected to the flange. As a result, extension and retraction of the actuator moves the tab member about a hinge-less tab that is created on the first surface.
摘要翻译： 公开了一种在空气动力学箔上使用的修剪突片，其具有在前缘和后缘之间延伸的第一和第二表面。 在结构上，修剪突片包括突出部件，该突出部件由通过每个表面形成的狭缝限定，以从后缘朝向前缘延伸。 此外，突片构件由形成在第二表面上的狭缝之间的槽限定，以在槽和后缘之间建立凸缘。 此外，修剪片包括安装在插槽和前缘之间的箔上的致动器。 致动器包括连接到凸缘的致动器臂。 结果是，致动器的延伸和缩回使得突片构件围绕在第一表面上形成的无铰链的突片移动。
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公开(公告)号：US20100042271A1
公开(公告)日：2010-02-18
申请号：US12450089
申请日：2008-03-17
申请人： Torsten Holzhausen
发明人： Torsten Holzhausen
摘要： The invention relates to a method for actuating an adjusting drive for adjusting an elevator (12) and an adjusting drive for adjusting a moveable tail (23) provided with the steps: Generation of an elevator command to actuate the elevator adjusting drive; Calculating a moveable tail command (IHC1) for actuating the moveable tail adjusting drive in such a manner that the moveable tail (23) is tracked to the elevator input signal (10); Depending on the adjusting states of the elevator (12) and/or the moveable tail (23) or flight states, retaining the adjusting state of the moveable tail adjusting drive or actuating the moveable tail adjusting drive with a moveable tail command (IHCMD) for changing the adjusting state of the moveable tail (23), during actuation of the elevator adjusting drive with an elevator command for changing the adjusting state of the elevator (23) and in the event of a deviation from the calculated moveable tail command (IHC1) and the commanded moveable tail command (IHCMD), acting upon the elevator command to compensate for retention of the adjusting state of the moveable tail adjusting drive and a control device for carrying out the method.
摘要翻译： 本发明涉及一种致动用于调节电梯（12）的调节驱动器和用于调节可移动尾部（23）的调节驱动器的方法，所述调节驱动装置具有以下步骤：产生升降机命令以启动电梯调节驱动器; 计算用于致动所述可移动尾部调整驱动器的可移动尾部命令（IHC1），使得所述可移动尾部（23）被跟踪到所述电梯输入信号（10）; 根据电梯（12）和/或可移动尾部（23）或飞行状态的调节状态，保持可移动尾部调整驱动器的调节状态或使用可移动尾部调整驱动器致动可移动尾部调整驱动器（IHCMD），以便 在用于改变电梯（23）的调节状态的电梯命令和在偏离计算出的可移动尾部命令（IHC1）的情况下，在电梯调节驱动器致动期间改变可移动尾部（23）的调节状态， 和命令的可移动尾部命令（IHCMD），作用于电梯命令以补偿可动尾部调整驱动器的调节状态的保持和用于执行该方法的控制装置。
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