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1. 发明授权

US07093424B2 Thrust reverser system electro-mechanical brake manual release mechanism 失效
标题翻译：推力倒车系统机电制动手动释放机构
公开(公告)号：US07093424B2
公开(公告)日：2006-08-22
申请号：US10925700
申请日：2004-08-24
申请人： Casey Hanlon , Donald J. Christensen , Kevin K. Chakkera
发明人： Casey Hanlon , Donald J. Christensen , Kevin K. Chakkera
IPC分类号： F02K1/70 , F02K1/76
CPC分类号： F02K1/766 , F16D2121/22 , F16D2125/38 , F16D2127/04
摘要： A manual release mechanism for a thrust reverser actuation system electromechanical brake includes a first release plate, a second release plate, at least two balls, and a handle. The first and second release plates each have grooves formed therein that have a cam surface located at a predetermined angle. The release plates face one another such that the grooves in each plate are substantially aligned, and the balls are each positioned in the aligned grooves. The first release plate is configured to rotate, and the second release plate is configured to translate. The handle is coupled to the first release plate to allow manual rotation thereof. In response to rotation of the first release plate, the second release plate will translate and disengage the electromechanical brake.
摘要翻译：用于推力反向器致动系统机电制动器的手动释放机构包括第一释放板，第二释放板，至少两个球和手柄。第一和第二释放板各自具有形成在其中的凹槽，其具有位于预定角度的凸轮表面。释放板彼此面对，使得每个板中的凹槽基本上对准，并且球各自定位在对准的凹槽中。第一释放板构造成旋转，并且第二释放板被配置成平移。手柄联接到第一释放板以允许其手动旋转。响应于第一释放板的旋转，第二释放板将使机电制动器平移和脱离。

2. 发明申请

US20080105790A1 RUDDER PEDAL ASSEMBLY INCLUDING NON-PARALLEL SLIDE RAILS 失效
标题翻译： RUDDER PEDAL ASSEMBLY包括非平行滑轨
公开(公告)号：US20080105790A1
公开(公告)日：2008-05-08
申请号：US11688701
申请日：2007-03-20
申请人： Donald J. Christensen , Casey Hanlon
发明人： Donald J. Christensen , Casey Hanlon
IPC分类号： B64C19/02
CPC分类号： G05G1/46 , B64C13/06 , B64C13/08 , G05G1/34 , G05G1/36 , G05G1/40 , G05G1/506 , G05G5/03
摘要： A rudder pedal assembly exhibits sufficient ergonomic feel for a pilot, and is relatively small in overall size. The rudder pedal assembly includes a plurality of rails disposed non-parallel to each other within a common plane, and a rudder pedal. The rudder pedal is movably coupled to the plurality of rails and is configured to receive an input force in at least a first direction and a second direction. The rudder pedal is further configured, in response to the input force, to move along a path constrained by the plurality of rails in at least the first direction and the second direction, respectively, and within the common plane.
摘要翻译：方向舵踏板组件对飞行员表现出足够的人体工程学感觉，并且整体尺寸相对较小。方向舵踏板组件包括在公共平面内彼此不平行设置的多个轨道和方向舵踏板。方向舵踏板可移动地联接到多个轨道并且构造成在至少第一方向和第二方向上接收输入力。方向舵踏板进一步配置为响应于输入力，在至少第一方向和第二方向以及公共平面内沿着由多个轨道约束的路径移动。

3. 发明授权

US07726611B2 Active rudder pedal mechanism with foreign object strike tolerance and articulating brake 失效
标题翻译：主动方向舵踏板机构具有异物撞击公差和铰接制动
公开(公告)号：US07726611B2
公开(公告)日：2010-06-01
申请号：US11585771
申请日：2006-10-23
申请人： Donald J. Christensen , Casey Hanlon
发明人： Donald J. Christensen , Casey Hanlon
IPC分类号： B64C19/02
CPC分类号： B64C13/04
摘要： A rudder pedal mechanism is configured with foreign object strike tolerance and/or with an articulating brake. The foreign object strike tolerance is implemented via a force transfer mechanism that is responsive to an input force supplied to the rudder pedal. The force transfer mechanism is configured to supply a transfer force to a rudder position command unit when the input force is supplied in a first direction, and to not supply the transfer force to the rudder position command unit when the input force is supplied in the second direction and exceeds at least a predetermined force magnitude. The articulating brake is implemented via a brake rod assembly that is rotationally coupled to the rudder pedal, and includes a first rod that is rotationally coupled to the rudder pedal, and a second rod that surrounds at least a portion of the first rod.
摘要翻译：方向舵踏板机构配置有异物撞击公差和/或铰接式制动器。异物撞击公差通过力传递机构实现，该力传递机构响应于供给舵踏板的输入力。力传递机构被配置为当在第一方向上提供输入力时向舵位置指令单元提供传递力，并且当输入力在第二方向被提供时，不向舵位置指令单元提供传递力方向并且至少超过预定的力量级。铰接制动器通过一个制动杆组件来实现，该制动杆组件旋转地联接到舵脚上，并且包括旋转地联接到舵踏板的第一杆和围绕第一杆的至少一部分的第二杆。

4. 发明授权

US07690604B2 Rudder pedal assembly including non-parallel slide rails 失效
标题翻译：方向舵踏板总成包括非平行滑轨
公开(公告)号：US07690604B2
公开(公告)日：2010-04-06
申请号：US11688701
申请日：2007-03-20
申请人： Donald J. Christensen , Casey Hanlon
发明人： Donald J. Christensen , Casey Hanlon
IPC分类号： B64C19/02
CPC分类号： G05G1/46 , B64C13/06 , B64C13/08 , G05G1/34 , G05G1/36 , G05G1/40 , G05G1/506 , G05G5/03
摘要： A rudder pedal assembly exhibits sufficient ergonomic feel for a pilot, and is relatively small in overall size. The rudder pedal assembly includes a plurality of rails disposed non-parallel to each other within a common plane, and a rudder pedal. The rudder pedal is movably coupled to the plurality of rails and is configured to receive an input force in at least a first direction and a second direction. The rudder pedal is further configured, in response to the input force, to move along a path constrained by the plurality of rails in at least the first direction and the second direction, respectively, and within the common plane.
摘要翻译：方向舵踏板组件对飞行员表现出足够的人体工程学感觉，并且整体尺寸相对较小。方向舵踏板组件包括在公共平面内彼此不平行设置的多个轨道和方向舵踏板。方向舵踏板可移动地联接到多个轨道并且构造成在至少第一方向和第二方向上接收输入力。方向舵踏板进一步配置为响应于输入力，在至少第一方向和第二方向以及公共平面内沿着由多个轨道约束的路径移动。

5. 发明申请

US20080023591A1 Active rudder pedal mechanism with foreign object strike tolerance and articulating brake 失效
标题翻译：主动方向舵踏板机构具有异物撞击公差和铰接制动
公开(公告)号：US20080023591A1
公开(公告)日：2008-01-31
申请号：US11585771
申请日：2006-10-23
申请人： Donald J. Christensen , Casey Hanlon
发明人： Donald J. Christensen , Casey Hanlon
IPC分类号： B64C19/02
CPC分类号： B64C13/04
摘要： A rudder pedal mechanism is configured with foreign object strike tolerance and/or with an articulating brake. The foreign object strike tolerance is implemented via a force transfer mechanism that is responsive to an input force supplied to the rudder pedal. The force transfer mechanism is configured to supply a transfer force to a rudder position command unit when the input force is supplied in a first direction, and to not supply the transfer force to the rudder position command unit when the input force is supplied in the second direction and exceeds at least a predetermined force magnitude. The articulating brake is implemented via a brake rod assembly that is rotationally coupled to the rudder pedal, and includes a first rod that is rotationally coupled to the rudder pedal, and a second rod that surrounds at least a portion of the first rod.
摘要翻译：方向舵踏板机构配置有异物撞击公差和/或铰接式制动器。异物撞击公差通过力传递机构实现，该力传递机构响应于供给舵踏板的输入力。力传递机构被配置为当在第一方向上提供输入力时向舵位置指令单元提供传递力，并且当输入力在第二方向被提供时，不向舵位置指令单元提供传递力方向并且至少超过预定的力量级。铰接制动器通过一个制动杆组件来实现，该制动杆组件旋转地联接到舵脚上，并且包括旋转地联接到舵踏板的第一杆和围绕第一杆的至少一部分的第二杆。

6. 发明授权

US06974107B2 Thrust reverser system actuator having an integral torque limiter 有权
标题翻译：具有整体扭矩限制器的推力反向器系统致动器
公开(公告)号：US06974107B2
公开(公告)日：2005-12-13
申请号：US10465413
申请日：2003-06-18
申请人： Donald J. Christensen , Casey Hanlon , Douglas T. Hopper , Andrew Johnson , Robert D. Kortum
发明人： Donald J. Christensen , Casey Hanlon , Douglas T. Hopper , Andrew Johnson , Robert D. Kortum
IPC分类号： F02K1/76 , F16H25/20 , F16H57/02
CPC分类号： F02K1/763 , F05D2270/114 , F16H25/2021 , F16H48/12 , F16H2025/2075 , Y10T74/19005
摘要： A thrust reverser system actuator assembly is provided that includes a torque limiter to limit the number of torque that may be applied to the actuator assembly. The actuator assembly includes an actuator and a torque limiter assembly. The actuator is adapted to receive a drive force and is configured, in response to receipt of the drive force, to move between a stowed position and a deployed position. The torque limiter assembly is coupled to an end of the actuator and is configured to limit torque applied to the actuator assembly upon a torque magnitude being reached in at least the actuator.
摘要翻译：提供了一种推力反向器系统致动器组件，其包括扭矩限制器以限制可施加到致动器组件的扭矩的数量。致动器组件包括致动器和扭矩限制器组件。致动器适于接受驱动力，并且响应于接收到的驱动力而构造为在收起位置和展开位置之间移动。扭矩限制器组件联接到致动器的端部，并且被构造成在至少在致动器中达到转矩幅度时限制施加到致动器组件的扭矩。

7. 发明授权

US09815438B2 Aircraft electric brake actuator assembly with line replaceable actuator brake 有权
公开(公告)号：US09815438B2
公开(公告)日：2017-11-14
申请号：US12704971
申请日：2010-02-12
申请人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer
发明人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer
IPC分类号： F16D55/02 , B60T7/04 , B60T8/00 , B60T13/74 , F16D65/18 , F16D125/40 , F16D125/48 , F16D127/06
CPC分类号： B60T7/042 , B60T8/00 , B60T13/746 , F16D65/18 , F16D2125/40 , F16D2125/48 , F16D2127/06
摘要： An aircraft electric brake actuator assembly includes an actuator housing, a motor housing, an actuator, an electric motor, and an actuator brake. The actuator housing is configured to be mounted on an aircraft landing gear. The motor housing is coupled to the actuator housing and is removable therefrom. The motor housing is also accessible when the actuator housing is mounted on an aircraft. The electric motor is disposed within the motor housing and is coupled to the actuator. The actuator brake is disposed within the motor housing and is removably coupled to the motor.

8. 发明授权

US08742711B2 Active feedback user interface system and gimbal assembly therefor 失效
标题翻译：主动反馈用户界面系统和万向节组件
公开(公告)号：US08742711B2
公开(公告)日：2014-06-03
申请号：US13240933
申请日：2011-09-22
申请人： Casey Hanlon , Donald Jeffrey Christensen
发明人： Casey Hanlon , Donald Jeffrey Christensen
IPC分类号： G05G9/047
CPC分类号： B64C13/04 , B64C13/10 , B64C13/48 , B64C13/50 , G05G2009/04718 , G05G2009/04766 , Y10T74/20201
摘要： An active user interface system includes a gimbal assembly that is configured as a dual-input/single-output differential mechanism. The differential mechanism implements a speed reduction from the inputs of the differential mechanism to the output of the differential mechanism. Speed reduction enables the maximum drive torque that is supplied to the user interface about one rotational axis to be greater than the maximum drive torque that is supplied to the user interface about another, perpendicular axis.
摘要翻译：主动用户界面系统包括被配置为双输入/单输出差分机构的万向节组件。差速机构实现了从差速机构的输入到差速机构的输出的减速。减速使得能够将围绕一个旋转轴提供给用户界面的最大驱动扭矩大于相对于另一个垂直轴提供给用户界面的最大驱动转矩。

9. 发明授权

US08201467B2 Dual drive electromechanical actuator with center output 失效
标题翻译：双驱动机电执行器，带中心输出
公开(公告)号：US08201467B2
公开(公告)日：2012-06-19
申请号：US12237978
申请日：2008-09-25
申请人： Andrew T. Johnson , Casey Hanlon , Kellan Geck
发明人： Andrew T. Johnson , Casey Hanlon , Kellan Geck
IPC分类号： F16H27/02 , F16H29/02
CPC分类号： H02K16/00 , F16H25/20 , F16H2025/2059 , H02K7/06 , Y10T74/1625 , Y10T74/1633 , Y10T74/18568 , Y10T74/18608 , Y10T74/18624
摘要： Electromechanical actuators (EMAs) include an output disposed at a location that is axially central between two EM devices. The EMAs include either one or two motors and an output mechanism. The motors are adapted to be energized and are operable, upon being energized, to either generate torques about a first axis or drive forces along a first axis. The output mechanism is responsive to the torques or forces to translate along a second axis that is perpendicular to the first axis.
摘要翻译：机电致动器（EMA）包括设置在两个EM装置之间轴向中心的位置处的输出。 EMA包括一个或两个电机和输出机构。电动机适于被激励，并且在通电时可操作地产生围绕第一轴线的扭矩或沿着第一轴线的驱动力。输出机构响应扭矩或力沿垂直于第一轴线的第二轴平移。

10. 发明授权

US08056432B2 Active control stick assembly 有权
标题翻译：主动控制杆组件
公开(公告)号：US08056432B2
公开(公告)日：2011-11-15
申请号：US12234262
申请日：2008-09-19
申请人： Casey Hanlon , Calvin C. Potter , Paul T. Wingett
发明人： Casey Hanlon , Calvin C. Potter , Paul T. Wingett
IPC分类号： G05G9/047
CPC分类号： G05G9/047 , G05G5/05 , Y10T74/20201
摘要： An active control stick assembly is provided. In one embodiment, the active control stick assembly includes a housing assembly, and a control stick support body mounted within the housing assembly for rotation about two substantially orthogonal and co-planar rotational axes. A control stick is fixedly coupled to the control stick support body and rotatable along therewith from a null position to a plurality of control positions. A first spring element is coupled between the housing assembly and the control stick support body and passively biases the control stick toward the null position.
摘要翻译：提供主动控制杆组件。在一个实施例中，主动控制杆组件包括壳体组件和安装在壳体组件内的控制棒支撑体，用于围绕两个基本正交和共面的旋转轴线旋转。控制杆固定地联接到控制棒支撑体并且随之从零位置转动到多个控制位置。第一弹簧元件联接在壳体组件和控制棒支撑体之间，并且被动地将控制杆偏压到空位置。

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