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81. 发明申请

US20110148666A1 USER INTERFACE PASSIVE HAPTIC FEEDBACK SYSTEM 审中-公开
标题翻译：用户界面被动式HAPTIC反馈系统
公开(公告)号：US20110148666A1
公开(公告)日：2011-06-23
申请号：US11696589
申请日：2007-04-04
申请人： Casey Hanlon , Douglas C. Smith , Todd Kuhar
发明人： Casey Hanlon , Douglas C. Smith , Todd Kuhar
IPC分类号： H04B3/36 , G01C23/00
CPC分类号： B64C13/0421 , B64C13/0425 , G05G5/03 , G05G2009/04718
摘要： A user interface system includes a user interface and a plurality of torsion bars. The user interface is configured to rotate, from a null position, about two perpendicular rotational axes. The plurality of torsion bars are coupled to the user interface and include two or more torsion bars disposed along a first one of the rotational axes and two or more torsion bars disposed along a second one of the rotational axes. Each torsion bar is configured to selectively supply a feedback force to the user interface that opposes the rotational direction and that varies as a function of the control position and the rotational direction. The system provides for the setting and adjustment of a preload force to the user interface, for retaining the set preload force, for passively returning the user interface to its null position, and for preventing each passive mechanism from introducing additional force into adjacent vectors.
摘要翻译：用户界面系统包括用户界面和多个扭杆。用户界面被配置为从零位置旋转大约两个垂直的旋转轴。多个扭力杆联接到用户界面，并且包括沿着旋转轴线中的第一个设置的两个或多个扭力杆和沿第二个旋转轴线设置的两个或更多个扭力杆。每个扭杆被配置成选择性地向用户界面提供与旋转方向相对的反馈力，并且其作为控制位置和旋转方向的函数而变化。该系统提供对用户界面的预载力的设置和调节，用于保持设定的预载力，将用户界面被动地返回到其零位置，并且用于防止每个被动机构将附加的力引入相邻的向量。

82. 发明授权

US07866230B2 Apparatus for releasably securing a rotatable object in a predetermined position 有权
标题翻译：用于将可旋转物体可释放地固定在预定位置的装置
公开(公告)号：US07866230B2
公开(公告)日：2011-01-11
申请号：US12016552
申请日：2008-01-18
申请人： Justin A. Tanner , Todd Langston , David Tornquist , Casey Hanlon , James I. Kern
发明人： Justin A. Tanner , Todd Langston , David Tornquist , Casey Hanlon , James I. Kern
IPC分类号： G05G5/06 , H01F7/20
CPC分类号： G05G5/06 , G05G1/04 , G05G5/05 , Y10T74/1412 , Y10T74/20636
摘要： An apparatus is provided for biasing a shaft toward, and releasably securing it in, a predetermined position. The apparatus comprises a magnetic assembly coupled to the shaft for releasably securing the shaft in a predetermined position, a first member coupled to and extending from the shaft for rotating the shaft from the predetermined position, and a spring assembly coupled to the shaft for securing the shaft in the predetermined position.
摘要翻译：提供一种用于将轴偏压并将其可释放地固定在预定位置的装置。该装置包括耦合到轴的磁性组件，用于将轴可释放地固定在预定位置，联接到轴并从轴延伸以使轴从预定位置旋转的第一构件和联接到轴的弹簧组件，用于固定轴在预定位置。

83. 发明授权

US07701161B2 Motor balanced active user interface assembly 失效
标题翻译：电机平衡主动用户界面组件
公开(公告)号：US07701161B2
公开(公告)日：2010-04-20
申请号：US11676845
申请日：2007-02-20
申请人： Casey Hanlon , James I. Kern , Douglas C. Smith , David Cowling
发明人： Casey Hanlon , James I. Kern , Douglas C. Smith , David Cowling
IPC分类号： G05B13/00
CPC分类号： B64C13/04 , B64C13/46 , G05G2009/04766 , Y10T74/20012
摘要： An active user interface assembly includes a user interface, and one or more feedback motors coupled to the user interface. The one or more feedback motors, when energized, supply a feedback force to the user interface that opposes user interface movement. One of the feedback motors is disposed such that its center of gravity is located at a position relative to the user interface to mass balance the user interface when it is in the null position. The configurations allow for the center of gravity of a feedback motor to be positioned in a manner that alleviates the need for counterbalance weights.
摘要翻译：活动用户界面组件包括用户界面和耦合到用户界面的一个或多个反馈电机。一个或多个反馈电机通电时，向用户界面提供反对用户界面移动的反馈力。反馈电动机中的一个被布置成使得其重心位于相对于用户界面的位置，以在用户界面处于零位置时大量平衡。该配置允许反馈电动机的重心定位成减轻对平衡重量的需要。

84. 发明授权

US07658349B2 Pilot flight control stick haptic feedback system and method 失效
标题翻译：飞行员控制杆触觉反馈系统及方法
公开(公告)号：US07658349B2
公开(公告)日：2010-02-09
申请号：US11739479
申请日：2007-04-24
申请人： Stephen G. Abel , Casey Hanlon
发明人： Stephen G. Abel , Casey Hanlon
IPC分类号： B64C13/46
CPC分类号： B64C13/10 , B64C13/503
摘要： A pilot flight control stick haptic feedback system includes a pilot user interface, a position sensor, a pilot motor, and a control circuit. The pilot user interface is movable to a position at a movement rate. The position sensor senses the position of the pilot user interface and supplies a pilot user interface position signal. The pilot motor is coupled to the pilot user interface, and receives pilot motor feedback signals. The pilot motor, in response to the pilot motor feedback signals, supplies feedback force to the pilot user interface. The control circuit determines one or more of the pilot user interface position, movement rate, aircraft control surface slew rate capacity, aircraft control surface load rate capacity, and aerodynamic stall risk and, based on at least a subset of these determinations, supplies pilot motor feedback signals to the pilot motor.
摘要翻译：飞行员控制杆触觉反馈系统包括飞行员用户界面，位置传感器，先导电机和控制电路。飞行员用户界面可移动到移动速度的位置。位置传感器感测导频用户界面的位置，并提供导频用户界面位置信号。先导电机耦合到导频用户接口，并接收导频电机反馈信号。先导电机响应于先导电机反馈信号，向飞行员用户界面提供反馈力。控制电路确定导频用户接口位置，移动速率，飞机控制面压摆率容量，飞机控制面载荷率容量和气动失速风险中的一个或多个，并且至少基于这些确定的子集，提供导向马达反馈信号到先导电机。

85. 发明申请

US20100025539A1 ACTIVE CONTROL STICK ASSEMBLY INCLUDING TRACTION DRIVE 有权
标题翻译：主动控制组件包括跟踪驱动
公开(公告)号：US20100025539A1
公开(公告)日：2010-02-04
申请号：US12182839
申请日：2008-07-30
申请人： Casey Hanlon , Dave Eschborn
发明人： Casey Hanlon , Dave Eschborn
IPC分类号： B64C13/46 , G05G1/08 , F16H57/08
CPC分类号： B64C13/04 , B64C13/10 , B64C13/46 , G05G9/047 , G05G2009/04718 , G05G2009/04766 , Y10T74/20498
摘要： An active control stick assembly is provided. In one embodiment, the active control stick assembly includes a housing assembly, a control stick coupled to the assembly housing for rotation about at least a first rotational axis, a first artificial force feel (AFF) motor disposed in the housing assembly, and a first traction drive mechanically coupling the first AFF motor to the control stick. A controller is operatively coupled to the first AFF motor. The controller is configured to selectively activate the first AFF motor to supply a torque through the first traction drive and acting on the control stick about the first rotational axis.
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，耦合到组件壳体的控制杆，用于围绕至少第一旋转轴线旋转，设置在壳体组件中的第一人造力感觉（AFF）电动机，以及第一牵引驱动器将第一AFF马达机械地联接到控制杆。控制器可操作地耦合到第一AFF电动机。控制器被配置为选择性地激活第一AFF电动机以通过第一牵引驱动器提供扭矩并且围绕第一旋转轴线作用在控制杆上。

86. 发明申请

US20090102413A1 ELECTROMECHANICAL FLIGHT CONTROL SYSTEM AND METHOD FOR ROTORCRAFT 有权
标题翻译：电动飞行控制系统和旋转方法
公开(公告)号：US20090102413A1
公开(公告)日：2009-04-23
申请号：US11876456
申请日：2007-10-22
申请人： Casey Hanlon , James I. Kern
发明人： Casey Hanlon , James I. Kern
IPC分类号： H02P6/00
CPC分类号： B64C27/08 , B64C27/605 , B64C27/68 , H02K7/083 , H02K41/031 , H02K2213/12
摘要： Flight control systems and methods for rotorcraft are provided. The flight control system includes a user input device and a motor in operable communication with the user input device. The motor includes a plurality of winding sets and an armature coupled to the plurality of winding sets. The armature includes multiple magnets. The winding sets and the armature are configured such that when one or more of the plurality of winding sets are selectively energized, the armature moves relative to the one or more of the plurality of winding sets.
摘要翻译：提供旋翼飞行器的飞行控制系统和方法。飞行控制系统包括用户输入装置和与用户输入装置可操作地通信的马达。电动机包括多个绕组和耦合到多个绕组的电枢。电枢包括多个磁体。绕组和电枢被构造成使得当多个绕组中的一个或多个被选择性地通电时，电枢相对于多个绕组中的一个或多个绕组移动。

87. 发明申请

US20090039205A1 AIRCRAFT FLIGHT CONTROL USER INTERFACE LINKAGE SYSTEM 失效
标题翻译：飞机飞行控制用户界面连接系统
公开(公告)号：US20090039205A1
公开(公告)日：2009-02-12
申请号：US11835089
申请日：2007-08-07
申请人： Casey Hanlon , Dean R. Wilkens , Pablo Bandera , Toren S. Davis
发明人： Casey Hanlon , Dean R. Wilkens , Pablo Bandera , Toren S. Davis
IPC分类号： B64C13/04
CPC分类号： B64C13/12 , Y02T50/44
摘要： A user interface linkage system includes first and second user interfaces that are linked by a single hydraulic circuit. The system is configured to provide compensation for relatively slow changes in hydraulic fluid pressure due, for example, to temperature variations. The system is also configured to allow the user interfaces to be selectively unlinked from each other.
摘要翻译：用户界面联动系统包括由单个液压回路链接的第一和第二用户界面。该系统被配置为为由于例如温度变化引起的液压流体压力的相对较慢的变化提供补偿。该系统还被配置为允许用户接口被选择性地彼此链接。

88. 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。

89. 发明申请

US20060255207A1 Flight control surface actuation system with redundantly configured actuator assemblies 审中-公开
标题翻译：具有冗余配置的执行器组件的飞行控制表面致动系统
公开(公告)号：US20060255207A1
公开(公告)日：2006-11-16
申请号：US11193059
申请日：2005-07-28
申请人： Paul Wingett , Calvin Potter , Casey Hanlon , Dwayne Benson
发明人： Paul Wingett , Calvin Potter , Casey Hanlon , Dwayne Benson
IPC分类号： B64C13/00
CPC分类号： B64C13/00 , B64C13/341 , B64C13/504 , B64C13/505
摘要： A flight control surface actuator assembly includes a plurality of flight control surface actuators, and a pivot arm. Each flight control surface actuator is adapted to couple to a flight control surface, and each is further adapted to receive a drive force and is operable, upon receipt thereof, to move between at least an extended position and a retracted position. The pivot arm is rotationally coupled to, and is configured to pivot relative to, each of the flight control surface actuators, the pivot arm is also adapted to be rotationally coupled to, and configured to pivot relative to, a static airframe structure.
摘要翻译：飞行控制表面致动器组件包括多个飞行控制表面致动器和枢转臂。每个飞行控制表面致动器适于联接到飞行控制表面，并且每个飞行控制表面致动器进一步适于接收驱动力，并且在其接收时可操作以在至少延伸位置和缩回位置之间移动。枢转臂旋转地联接到每个飞行控制表面致动器并被构造成相对于每个飞行控制表面致动器枢转，枢转臂还适于旋转地联接到静止的机身结构并且被构造成相对于静止的机身结构枢转。

90. 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。

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