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1. 发明授权

US5033695A Aileron counterbalance mount bracket 失效
标题翻译：副翼平衡支架
公开(公告)号：US5033695A
公开(公告)日：1991-07-23
申请号：US469032
申请日：1990-01-23
申请人： Paul L. Foshee , Holley L. Foshee
发明人： Paul L. Foshee , Holley L. Foshee
IPC分类号： B64C9/30
CPC分类号： B64C9/30
摘要： A counterbalance mount bracket for mounting aileron counterbalances on the ailerons of selected aircraft, which counterbalance mount bracket includes an aileron attachment plate having a wing hinge flange adapted to mount on the wing hinge of the aircraft, an aileron hinge flange adapted to mount on the aircraft aileron hinge and a gusset plate for attaching the aileron counterbalance to the counterbalance mount bracket and facilitating pivoting of the aileron counterbalance with the aileron. In a preferred embodiment the counterbalance tubing attached to the counterbalance spade in the aileron counterbalance is welded to the gusset plate, which gusset plate is, in turn, welded to the wing hinge flange of the aileron attachment plate.
摘要翻译：一种用于将副翼平衡安装在所选飞机的副翼上的平衡安装支架，该平衡安装支架包括副翼连接板，该副翼安装板具有适于安装在飞行器的翼铰链上的翼铰链凸缘，适于安装在飞机上的副翼铰链凸缘副翼铰链和用于将副翼平衡板附接到平衡安装支架的角撑板，并且有助于副翼平衡与副翼的枢转。在优选实施例中，连接在副翼平衡板上的平衡板上的平衡管被焊接到角撑板上，该角撑板又被焊接到副翼连接板的翼铰链凸缘上。

2. 发明申请

US20190233136A1 Optical Systems and Methods for Aircraft Flight Control Rigging 审中-公开
公开(公告)号：US20190233136A1
公开(公告)日：2019-08-01
申请号：US15884734
申请日：2018-01-31
申请人： The Boeing Company
发明人： Scott Charles Farner , Joseph Edward Dale Sharp , Randall Wade Dickson
IPC分类号： B64F5/10 , G01S17/06 , B64C9/02 , B64F5/60 , B64C5/10 , B64C9/30 , B64C9/00 , B64C9/14
CPC分类号： B64F5/10 , B64C5/10 , B64C9/02 , B64C9/14 , B64C9/30 , B64C2009/005 , B64F5/60 , G01S17/06
摘要： Systems and methods for aircraft flight control rigging are described. An example system includes a first set of laser rangefinders to measure, for each laser rangefinder of the first set, a distance from the laser rangefinder to a respective target location on a fixed surface of an aircraft, and a second set of laser rangefinders to measure, for each laser rangefinder of the second set, a distance to a respective target location on a control surface of the aircraft. The example system also includes a processor to (i) receive signals indicative of the distance measured by each rangefinder and (ii) generate a first plot line graphic of the measured distances of each of the rangefinders of the first set to its respective target location and a second plot line graphic of the measured distances of each of the laser rangefinders of the second set to its respective target location.

3. 发明申请

US20180319481A1 Aircraft Spade Apparatus 审中-公开
公开(公告)号：US20180319481A1
公开(公告)日：2018-11-08
申请号：US15972363
申请日：2018-05-07
申请人： Reed Chuda , Warren Cilliars
发明人： Reed Chuda , Warren Cilliars
IPC分类号： B64C9/30
CPC分类号： B64C9/30 , B64C2009/005
摘要： An aileron counterbalance or aircraft spade apparatus disposed to afford optimal drag force, which particularly enhances the capability of an aircraft to spin, turn and dive more quickly and efficiently in aircraft races. The aircraft spade apparatus includes a rectangular shape and which exhibits a greater surface area and higher drag force characteristics.

4. 发明授权

US08128039B2 Aerodynamic surface assembly for aircraft 有权
标题翻译：飞机气动表面装配
公开(公告)号：US08128039B2
公开(公告)日：2012-03-06
申请号：US12413959
申请日：2009-03-30
申请人： Bertrand Soucheleau
发明人： Bertrand Soucheleau
IPC分类号： B64D3/50
CPC分类号： B64C9/30 , B64C9/10
摘要： Disclosed is a set of aerodynamic surfaces for an aircraft. There is included in the set a fixed aerodynamic surface delimited by two external walls which, at the rear, converge toward one another. A mobile flap extends the external walls, forming a mobile trailing-edge. An actuator is positioned so as to cause the mobile flap to rotate. A vane runs in the overall direction of the span of the fixed aerodynamic surface, and rotates with the flap.
摘要翻译：公开了一组飞机的空气动力学表面。在该组中包括由两个外壁限定的固定的空气动力学表面，其在后部相互收敛。移动挡板延伸外壁，形成移动后缘。致动器被定位成使得移动挡板旋转。叶片在固定空气动力学表面的跨度的整个方向上运行，并与挡板一起旋转。

5. 发明授权

US2859925A Automatic balancing arrangement for aircraft control 失效
标题翻译：飞机控制自动平衡装置
公开(公告)号：US2859925A
公开(公告)日：1958-11-11
申请号：US45604754
申请日：1954-09-14
申请人： JULES GERIN JACQUES JEAN-MARIE
发明人： JULES GERIN JACQUES JEAN-MARIE
IPC分类号： B64C9/30
CPC分类号： B64C9/30

6. 发明申请

US20160016653A1 AIRCRAFT COMPONENT ROTARY DEVICE 有权
标题翻译：飞机组件旋转装置
公开(公告)号：US20160016653A1
公开(公告)日：2016-01-21
申请号：US14486443
申请日：2014-09-15
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： Victor Barger
IPC分类号： B64C9/30 , F16H57/00 , F16H13/04 , F16D59/00 , B64C13/28
CPC分类号： B64C9/30 , B64C9/16 , B64C9/22 , B64C13/28 , F16D43/206 , F16D43/218 , F16D59/00 , F16D65/18 , F16D2125/36 , F16H13/04 , F16H57/0006
摘要： A rotary device assembly is provided and includes an input shaft coupled to a torque generating device, an output shaft and a rotary device disposed to transmit first torque from the input shaft to the output shaft and configured with no-back capability to prevent second torque applied to the output shaft from being transmitted to the input shaft in an event the second torque deceeds a torque-limiting threshold and the no-back capability and torsional lock-up capability to prevent an overload of the torque generating device in an event the second torque exceeds the torque-limiting threshold.
摘要翻译：提供了一种旋转装置组件，其包括联接到转矩产生装置的输入轴，输出轴和旋转装置，其被设置为将第一扭矩从输入轴传递到输出轴，并且被配置为具有不反转能力以防止施加第二扭矩在第二扭矩变为扭矩限制阈值和无返回能力和扭转锁定能力的情况下，输出轴传递到输入轴，以防止在第二扭矩的情况下扭矩产生装置的过载超过扭矩限制阈值。

7. 发明申请

US20090250558A1 AERODYNAMIC SURFACE ASSEMBLY FOR AIRCRAFT 有权
标题翻译：航空器的航空表面装配
公开(公告)号：US20090250558A1
公开(公告)日：2009-10-08
申请号：US12413959
申请日：2009-03-30
申请人： Bertrand SOUCHELEAU
发明人： Bertrand SOUCHELEAU
IPC分类号： B64C9/00
CPC分类号： B64C9/30 , B64C9/10
摘要： Set of aerodynamic surfaces for an aircraft.According to the invention, inside the rear part of the fixed aerodynamic surface on which a mobile flap is mounted, there is a vane that rotates as one with the flap and is able to generate an antagonistic moment that opposes the hinge moment of said flap.
摘要翻译：一套飞机的空气动力学表面。根据本发明，在其上安装有活动翼片的固定空气动力学表面的后部内部存在叶片，其与翼片一体旋转，并且能够产生与所述翼片的铰链力矩相对的对抗力矩。

8. 发明授权

US2980367A Linked inertial balance for tab 失效
标题翻译：标签的连接惯性平衡
公开(公告)号：US2980367A
公开(公告)日：1961-04-18
申请号：US81972159
申请日：1959-06-11
申请人： LOCKHEED AIRCRAFT CORP
发明人： FORD JOHNSTON J , EVERETT POSTEL EDWARD
IPC分类号： B64C9/30
CPC分类号： B64C9/30

9. 发明授权

US2630988A Aerodynamic balance control 失效
标题翻译：气动平衡控制
公开(公告)号：US2630988A
公开(公告)日：1953-03-10
申请号：US14534650
申请日：1950-02-21
申请人： NORTH AMERICAN AVIATION INC
发明人： PRIBIL RICHARD F , MYERS DALE D , SCHREIBER RALPH B
IPC分类号： B64C9/30
CPC分类号： B64C9/30

10. 发明授权

US2081957A Dynamic balance of control surfaces 失效
标题翻译：控制面动态平衡
公开(公告)号：US2081957A
公开(公告)日：1937-06-01
申请号：US68779533
申请日：1933-09-01
申请人： ALFRED ROCHE JEAN
发明人： ALFRED ROCHE JEAN
IPC分类号： B64C9/30
CPC分类号： B64C9/30 , Y02T50/44

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