专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

51. 发明授权

US08219909B2 Human-machine interface with integrated position sensors and passive haptic feedback devices 有权
标题翻译：具有集成位置传感器和被动触觉反馈装置的人机界面
公开(公告)号：US08219909B2
公开(公告)日：2012-07-10
申请号：US12359946
申请日：2009-01-26
申请人： Casey Hanlon , Cal Potter , Paul Wingett
发明人： Casey Hanlon , Cal Potter , Paul Wingett
IPC分类号： G06F3/00
CPC分类号： B64C13/10 , B64C27/56 , G05G9/047 , G05G2009/04766 , H03K17/967 , Y10T74/20201
摘要： A system and method for determining the input force supplied to a user interface by a user is provided. A passive feedback mechanism is coupled to the user interface, and a change in position of the passive feedback mechanism is sensed. The input force supplied by the user to the user interface is then calculated from the sensed change in position.
摘要翻译：提供了一种用于确定由用户提供给用户界面的输入力的系统和方法。无源反馈机构耦合到用户界面，并且感测到被动反馈机构的位置变化。然后，根据感测到的位置变化计算由用户提供给用户界面的输入力。

52. 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。

53. 发明授权

US08033509B2 Load optimized redundant flight control surface actuation system and method 有权
标题翻译：负载优化冗余飞行控制表面驱动系统和方法
公开(公告)号：US08033509B2
公开(公告)日：2011-10-11
申请号：US11711295
申请日：2007-02-27
申请人： Larry J. Yount , Casey Hanlon , Andrew T. Johnson , Joseph Jackson
发明人： Larry J. Yount , Casey Hanlon , Andrew T. Johnson , Joseph Jackson
IPC分类号： B64C13/40 , B64C13/42 , B64C13/50
CPC分类号： B64C13/42 , Y02T50/44
摘要： An aircraft flight surface control system and method simultaneously provides the benefits of both an active/active system architecture and in active/standby system architecture. The system is preferably implemented using hydraulic actuator assemblies and electromechanical actuator assemblies coupled to the same flight control surface. During normal system operations the electromechanical actuator assemblies are energized to supply a relatively minimal force to associated flight control surfaces. In effect, the electromechanical actuators, although energized, may be pulled along by the associated hydraulic actuator assemblies, until needed. Thus, the electromechanical actuator assemblies are controlled in a manner that closely resembles the active/standby architecture.
摘要翻译：飞机飞行面控制系统和方法同时提供主动/主动系统架构和主动/待机系统架构的优点。该系统优选地使用联接到相同飞行控制表面的液压致动器组件和机电致动器组件来实现。在正常的系统操作期间，机电致动器组件被通电以向相关的飞行控制表面提供相对最小的力。实际上，机电致动器虽然通电，但可以通过相关联的液压致动器组件被拉动，直到需要。因此，机电致动器组件以与主动/待机架构非常相似的方式被控制。

54. 发明申请

US20110198163A1 AIRCRAFT ELECTRIC BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE ACTUATOR BRAKE 有权
标题翻译：航空电动制动器组件与线路可更换执行器制动器
公开(公告)号：US20110198163A1
公开(公告)日：2011-08-18
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
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.
摘要翻译：飞行器电动制动器致动器组件包括致动器壳体，马达壳体，致动器，电动马达和致动器制动器。致动器壳体构造成安装在飞机起落架上。马达壳体联接到致动器壳体并且可从其移除。当执行器外壳安装在飞机上时，马达外壳也可以接近。电动机设置在电动机壳体内并联接到致动器。致动器制动器设置在马达壳体内并且可拆卸地联接到马达。

55. 发明申请

US20110177896A1 REDUNDANT ELECTROMECHANICAL ACTUATOR FOR CONTROL SURFACES 有权
标题翻译：用于控制表面的冗余电动执行器
公开(公告)号：US20110177896A1
公开(公告)日：2011-07-21
申请号：US12362189
申请日：2009-01-29
申请人： Casey Hanlon , David M. Eschborn
发明人： Casey Hanlon , David M. Eschborn
IPC分类号： F16H7/04
CPC分类号： B63B1/28
摘要： A redundant electromechanical actuator is provided that includes first and second electric motors, a common output shaft, first and second drive cable drums, first and second driven cable drums, a first cable, and a second cable. The first and second electric motors are each adapted to be controllably energized to supply a drive torque. The common output shaft is coupled to receive the drive torque supplied from one or both of the motors. The first and second drive cable drums are coupled to the common output shaft to receive the drive torque from one or both of the motors. The first and second driven cable drums are each configured, upon being driven, to rotate. The first cable is coupled between the first drive cable drum and the first driven cable drum, and the second cable is coupled between the second drive cable drum and the second driven cable drum.
摘要翻译：提供了一种冗余机电致动器，其包括第一和第二电动机，公共输出轴，第一和第二驱动电缆卷筒，第一和第二驱动电缆卷筒，第一电缆和第二电缆。第一和第二电动机各自适于被可控制地通电以提供驱动扭矩。公共输出轴被联接以接收从一个或两个电动机提供的驱动力矩。第一和第二驱动电缆卷筒联接到公共输出轴以接收来自一个或两个电动机的驱动扭矩。第一和第二驱动的电缆卷筒在被驱动时都被配置成旋转。第一电缆耦合在第一驱动电缆鼓和第一从动电缆鼓之间，第二电缆耦合在第二驱动电缆鼓和第二从动电缆鼓之间。

56. 发明申请

US20110031424A1 HIGH ACCURACY, ZERO BACKLASH ROTARY-TO-LINEAR ELECTROMECHANICAL ACTUATOR 失效
标题翻译：高精度，零回程旋转线性电动执行器
公开(公告)号：US20110031424A1
公开(公告)日：2011-02-10
申请号：US12535511
申请日：2009-08-04
申请人： Casey Hanlon , Steve Abel , David M. Eschborn , Doug Kortum , Don Christensen
发明人： Casey Hanlon , Steve Abel , David M. Eschborn , Doug Kortum , Don Christensen
IPC分类号： F16K31/02 , H02K7/10 , H02K7/116 , G05B1/06 , H02P6/16
CPC分类号： H02K7/06 , F16K31/047 , H02K7/116
摘要： An electromechanical actuator is provided for converting rotary action into linear action, and includes an electric motor, a cable yoke, an output shaft, and a pair of cables. The electric motor is adapted to be selectively energized and is configured, upon being energized to generate a drive torque. The cable yoke is coupled to receive the drive torque and is configured, upon receipt thereof, to rotate about a rotational axis. The output shaft is coupled to receive a drive force and is configured, upon receipt thereof, to translate along a linear axis that is disposed at least substantially perpendicular to the rotational axis. Each cable is wound, in pretension, on a portion of the cable yoke and around a portion of the output shaft. The pair of cables is configured, upon rotation of the cable yoke, to supply the drive force to the output shaft.
摘要翻译：提供了一种机电致动器，用于将旋转动作转换为线性动作，并且包括电动机，电缆轭，输出轴和一对电缆。电动机适于被选择性地通电，并且在通电时被构造以产生驱动转矩。电缆轭被联接以接收驱动扭矩，并且在其接收时被配置为围绕旋转轴线旋转。输出轴被联接以接收驱动力，并且在接收到驱动力时构造成沿着至少基本上垂直于旋转轴线设置的线性轴线平移。每个电缆在预紧中缠绕在电缆轭架的一部分上并围绕输出轴的一部分。一对电缆在电缆轭架旋转时被配置成将驱动力提供给输出轴。

57. 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。

58. 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。

59. 发明申请

US20100084517A1 ELECTROMECHANICAL ACTUATION SYSTEM AND METHOD 有权
标题翻译：电动执行系统及方法
公开(公告)号：US20100084517A1
公开(公告)日：2010-04-08
申请号：US12247930
申请日：2008-10-08
申请人： Dwayne M. Benson , Casey Hanlon , Dean Wilkens
发明人： Dwayne M. Benson , Casey Hanlon , Dean Wilkens
IPC分类号： B64C13/50 , H02K41/02
CPC分类号： B64C27/605
摘要： Electromechanical actuation systems and methods are provided. The electromechanical actuation system includes first, second, and third linear actuators having respective first, second, and third ranges of motion and an output member coupled to the first, second, and third linear actuators such that a position of a selected portion of the output member is based on actuation of the first, second, and third linear actuators.
摘要翻译：提供了机电致动系统和方法。机电致动系统包括具有相应的第一，第二和第三运动范围的第一，第二和第三线性致动器，以及耦合到第一，第二和第三线性致动器的输出构件，使得输出的选定部分的位置构件基于第一，第二和第三线性致动器的致动。

60. 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。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式