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1. 发明申请

US20090072083A1 Actuation system with redundant motor actuators 审中-公开
标题翻译：具有冗余电机执行器的驱动系统
公开(公告)号：US20090072083A1
公开(公告)日：2009-03-19
申请号：US11445876
申请日：2006-06-02
申请人： Casey Hanlon , Calvin C. Potter , Paul T. Wingett , John T. Morris
发明人： Casey Hanlon , Calvin C. Potter , Paul T. Wingett , John T. Morris
IPC分类号： B64C9/00 , H02K16/00
CPC分类号： H02K21/24 , B64C13/505 , H02K16/00 , H02K2213/06
摘要： A multi-redundant motor may be used to implement a relatively small, lightweight redundant actuator assembly package. The motor is implemented as a brushless DC motor and includes N-number of stators and M-number of rotors. Each stator has a plurality of independent stator coils disposed thereon, and N is an integer greater than two. Each permanent magnet rotor is disposed between, and is spaced axially apart from, two of the stators. Each rotor has a plurality of magnetic dipoles disposed thereon, and M is an integer equal to (N−1).
摘要翻译：可以使用多冗余电动机来实现相对较小，重量轻的冗余致动器组件封装。电动机实现为无刷直流电动机，包括N个定子和M个转子。每个定子具有设置在其上的多个独立的定子线圈，并且N是大于2的整数。每个永磁转子设置在两个定子之间，并且与两个定子轴向分开。每个转子具有多个设置在其上的磁偶极子，M是等于（N-1）的整数。

2. 发明申请

US20100275710A1 Ballscrew with an integral high-efficiency thrust bearing 失效
标题翻译：滚珠丝杠带有一体的高效推力轴承
公开(公告)号：US20100275710A1
公开(公告)日：2010-11-04
申请号：US11545971
申请日：2006-10-10
申请人： Paul T. Wingett , Calvin C. Potter , Brent L. Bristol , Casey Hanlon , Kellan Geck , Louie T. Gaines
发明人： Paul T. Wingett , Calvin C. Potter , Brent L. Bristol , Casey Hanlon , Kellan Geck , Louie T. Gaines
IPC分类号： F16H25/22
CPC分类号： F16H25/20 , F16C19/08 , F16C33/581 , F16C43/06 , F16H25/2204 , F16H2025/2081 , Y10S384/906 , Y10T74/18576 , Y10T74/19744 , Y10T74/19749
摘要： A linear actuator includes a thrust bearing that is integral to the actuation member. The actuator includes a translation member and an actuation member. The actuation member is responsive to a drive force to rotate. The translation member is configured to translate in response to actuation member. The thrust bearing is coupled to the actuation member and includes an inner race, an outer race, and a plurality of balls. The thrust bearing is configured as a zero lead ballscrew, with the inner race integrally formed on the actuation member, and the plurality of balls disposed between the inner and outer races.
摘要翻译：线性致动器包括与致动构件成一体的止推轴承。致动器包括平移构件和致动构件。致动构件响应于驱动力旋转。翻译构件被配置为响应于致动构件而平移。推力轴承联接到致动构件并且包括内座圈，外座圈和多个球。推力轴承构造为零引线滚珠丝杠，内圈整体形成在致动构件上，并且多个球设置在内圈和外圈之间。

3. 发明申请

US20090045979A1 TWO-DIMENSIONAL POSITION SENSING SYSTEM 有权
标题翻译：二维位置传感系统
公开(公告)号：US20090045979A1
公开(公告)日：2009-02-19
申请号：US11839907
申请日：2007-08-16
申请人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett , James I. Kern
发明人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett , James I. Kern
IPC分类号： G01S13/00
CPC分类号： G06F3/016 , G06F3/0338 , G06F2203/015
摘要： A position sensing system includes a plurality of two-axis anisotropic magneto-resistive (AMR) sensors to determine the position of a user interface. A magnetic member is coupled to the user interface, which is movable to a position along a random path. The plurality of two-axis AMR sensors is arranged in a two-dimensional sensor array that is spaced apart from the magnetic member. A signal processor circuit is operable to sense the electrical resistance values of each two-axis AMR sensor, to determine the position of the user interface from the resistance values, and to supply position feedback data representative of the determined position.
摘要翻译：位置感测系统包括多个两轴各向异性磁阻（AMR）传感器，以确定用户界面的位置。磁性构件耦合到用户界面，用户界面可移动到沿着随机路径的位置。多个两轴AMR传感器布置在与磁性构件间隔开的二维传感器阵列中。信号处理器电路可操作以感测每个两轴AMR传感器的电阻值，以根据电阻值确定用户界面的位置，并提供表示确定位置的位置反馈数据。

4. 发明申请

US20080297120A1 ELECTRONICALLY REDUNDANT SPACECRAFT POWER AND ATTITUDE CONTROL SYSTEM 审中-公开
标题翻译：电子冗余功率和姿态控制系统
公开(公告)号：US20080297120A1
公开(公告)日：2008-12-04
申请号：US11637290
申请日：2006-12-12
申请人： Calvin C. Potter , David Corcino , Paul T. Wingett , Casey Hanlon
发明人： Calvin C. Potter , David Corcino , Paul T. Wingett , Casey Hanlon
IPC分类号： H02K7/02
CPC分类号： B64G1/426 , H02K7/025 , Y02E60/16
摘要： An energy storage flywheel system for a spacecraft is implemented with an electronically redundant power and attitude control system. In particular, the system includes a plurality of flywheels, and a multi-channel processing module and a multi-channel power control module associated with each flywheel. Each multi-channel processing module includes a plurality of controllers that may be operated in either an active or a standby mode, and each multi-channel power control module includes a plurality of power control circuits that may also be operated in either an active or standby mode.
摘要翻译：用于航天器的储能飞轮系统由电子冗余电源和姿态控制系统来实现。特别地，该系统包括多个飞轮，以及与每个飞轮相关联的多通道处理模块和多通道功率控制模块。每个多通道处理模块包括可以在主动或待机模式下操作的多个控制器，并且每个多通道功率控制模块包括多个功率控制电路，其也可以在主动或备用模式。

5. 发明申请

US20080087133A1 Fully redundant spacecraft power and attitude control system 失效
标题翻译：完全冗余的航天器动力和姿态控制系统
公开(公告)号：US20080087133A1
公开(公告)日：2008-04-17
申请号：US11580664
申请日：2006-10-13
申请人： Calvin C. Potter , David Corcino , Paul T. Wingett , Casey Hanlon
发明人： Calvin C. Potter , David Corcino , Paul T. Wingett , Casey Hanlon
IPC分类号： H02K7/02
CPC分类号： H02K7/025 , B64G1/283 , B64G1/286 , B64G1/426 , B64G1/428 , B64G1/44 , F16C32/0442 , F16C32/0451 , F16C2326/47 , F16C2361/55 , F16F15/3156 , H02K7/09 , H02K11/048 , H02K16/00 , Y02E60/16 , Y10T74/2117
摘要： An energy storage flywheel system for a spacecraft is implemented with a fully redundant rotating group and gimbal actuator. In particular, the gimbal actuator, motor/generator, primary bearings, and secondary bearing actuator are each implemented with a pair of redundant coils or motors.
摘要翻译：用于航天器的储能飞轮系统由完全冗余的旋转组和万向传动器执行。特别地，万向运动器，电动机/发电机，主轴承和次级轴承致动器各自由一对冗余线圈或电动机实现。

6. 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。

7. 发明申请

US20100071496A1 ACTIVE CONTROL STICK ASSEMBLY 有权
标题翻译：主动控制组件
公开(公告)号：US20100071496A1
公开(公告)日：2010-03-25
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 , G05G9/00
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。

8. 发明授权

US07607611B2 Flight control surface actuation system with redundantly configured and lockable actuator assemblies 有权
标题翻译：飞行控制表面致动系统，具有冗余配置和可锁定的执行器组件
公开(公告)号：US07607611B2
公开(公告)日：2009-10-27
申请号：US11192625
申请日：2005-07-28
申请人： Paul T. Wingett , Calvin C. Potter , Casey Hanlon , Dwayne M. Benson
发明人： Paul T. Wingett , Calvin C. Potter , Casey Hanlon , Dwayne M. Benson
IPC分类号： B64C13/14
CPC分类号： B64C13/42 , B64C13/00
摘要： A flight control surface actuator assembly includes a pair of flight control surface actuators and a pivot arm. One of the flight control surface actuators is coupled to a flight control surface and a static airframe structure, the other flight control surface actuator is coupled to the flight control surface and the pivot arm. The pivot arm coupled to the static airframe structure and is configured to pivot relative to the second flight control surface actuator and the static airframe structure.
摘要翻译：飞行控制表面致动器组件包括一对飞行控制表面致动器和枢转臂。飞行控制表面致动器中的一个联接到飞行控制表面和静态机身结构，另一个飞行控制表面致动器联接到飞行控制表面和枢转臂。枢转臂联接到静态机身结构并且构造成相对于第二飞行控制表面致动器和静止机身结构枢转。

9. 发明授权

US08080966B2 Motor control architecture for simultaneously controlling multiple motors 有权
标题翻译：同时控制多台电机的电机控制架构
公开(公告)号：US08080966B2
公开(公告)日：2011-12-20
申请号：US12167762
申请日：2008-07-03
申请人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett
发明人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett
IPC分类号： G05B11/32 , G05B19/19
CPC分类号： G05B19/0421 , B64C13/50
摘要： A motor control architecture is provided that simultaneously controls multiple motors. The motor control system includes memory, a plurality of motor control processors, and a communication controller. The motor control processors are each responsive to control signals supplied from the communication controller to selectively retrieve system commands and motor positions from the memory, to generate motor commands, and to supply the generated motor commands to the memory. The communication controller selectively receives system commands and transmits the received system commands to the memory, selectively supplies the command signals to selected ones of the motor control processors, selectively receives motor positions from a plurality of motors, selectively transmits motor positions to the memory, selectively retrieves generated motor commands supplied to the memory, and selectively transmits the retrieved motor commands.
摘要翻译：提供了同时控制多个电机的电机控制架构。电动机控制系统包括存储器，多个电动机控制处理器和通信控制器。电动机控制处理器各自响应于从通信控制器提供的控制信号，以选择性地从存储器检索系统命令和电动机位置，以产生电动机命令，并将生成的电动机命令提供给存储器。通信控制器选择性地接收系统命令并将接收到的系统命令发送到存储器，选择性地将命令信号提供给电动机控制处理器中的选定的一个，选择性地从多个电动机接收电动机位置，选择性地将电动机位置传送到存储器检索提供给存储器的生成的电动机命令，并且选择性地发送所检索的电动机命令。

10. 发明授权

US07852183B2 Power drive unit electromagnetic latch 失效
标题翻译：电源驱动单元电磁锁
公开(公告)号：US07852183B2
公开(公告)日：2010-12-14
申请号：US11433118
申请日：2006-05-12
申请人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett
发明人： Calvin C. Potter , Casey Hanlon , Paul T. Wingett
IPC分类号： H01F7/14 , H02K7/10 , H02K49/00 , H02P15/00
CPC分类号： H02K7/106 , H02K7/06 , H02K49/106
摘要： A no-back device for a power drive unit is configured such that, during operation of the power drive unit, the no-back device does not supply magnetic or frictional force against power drive unit rotation. The no-back device is implemented either redundantly or no-redundantly, and includes a latch rotor and an electromagnet. In both embodiments, the latch rotor is coupled to the power drive unit to rotate therewith, and the electromagnet is coupled to receive a flow of current and, upon receipt thereof, generates a magnetic field force that opposes rotation of the latch rotor. In the redundant embodiment, the no-back device further includes one or more permanent magnets, and the magnetic field generated by the electromagnet selectively opposes or aids the magnetic field supplied by the permanent magnet(s).
摘要翻译：用于动力驱动单元的无背装置被配置为使得在动力驱动单元的操作期间，无返回装置不向动力驱动单元旋转提供磁力或摩擦力。无背装置被冗余或不冗余地实现，并且包括闩锁转子和电磁体。在两个实施例中，闩锁转子联接到动力驱动单元以与其一起旋转，并且电磁体被联接以接收电流，并且在其接收时产生与闩锁转子的旋转相对的磁场力。在冗余实施例中，无背装置还包括一个或多个永磁体，并且由电磁体产生的磁场选择性地与由永磁体提供的磁场相反或有助于其提供的磁场。

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