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1. 发明申请

US20110132704A1 BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE MOTOR FEATURES 有权
标题翻译：制动器执行器总成与线路可更换的电机功能
公开(公告)号：US20110132704A1
公开(公告)日：2011-06-09
申请号：US12732771
申请日：2010-03-26
申请人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer , Allan Blunt
发明人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer , Allan Blunt
IPC分类号： F16D65/18 , B64C25/44
CPC分类号： B60T7/042 , B60T7/085 , B60T13/741 , F16D65/0043 , F16D65/18 , F16D65/28 , F16D2121/24 , F16D2125/40 , F16D2125/48 , F16D2127/06
摘要： An aircraft brake system electromechanical actuator is provided. The actuator is configured with features that allow the electric motor to be a line replaceable unit. One such feature is a foreign-object-damage shield that inhibits dust, debris, and/or other particulate contaminants from entering the electromechanical actuator during electric motor removal and replacement.
摘要翻译：提供飞机制动系统机电致动器。执行器配置有允许电动机成为线路可更换单元的特征。一个这样的特征是异物损坏屏蔽物，其在电动马达移除和更换期间防止灰尘，碎屑和/或其它微粒污染物进入机电致动器。

2. 发明申请

US20130297101A1 AIRCRAFT ELECTRIC BRAKE ACTUATION SYSTEM AND METHOD 有权
标题翻译：飞机电动刹车系统及方法
公开(公告)号：US20130297101A1
公开(公告)日：2013-11-07
申请号：US12693088
申请日：2010-01-25
申请人： Casey Hanlon , James Neil Quitmeyer , Allan Blunt
发明人： Casey Hanlon , James Neil Quitmeyer , Allan Blunt
IPC分类号： B64C25/44
CPC分类号： B64C25/44 , B60T8/1703 , B60T13/741
摘要： A system and method of controlling aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator. An aircraft operational state is determined and an application force that is supplied to the brake pedal is determined When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized.
摘要翻译：一种控制飞机制动器的系统和方法，该系统和方法包括制动踏板和电制动致动器。确定飞行器操作状态并且确定提供给制动踏板的施加力当确定的飞行器操作状态是地面怠速状态并且所确定的施加力大于设定的力大小时，致动器制动器被移动到接合电动制动器致动器并且电动制动致动器被断电。

3. 发明授权

US09440735B2 Aircraft electric brake actuation system and method 有权
标题翻译：飞机电动刹车动作系统及方法
公开(公告)号：US09440735B2
公开(公告)日：2016-09-13
申请号：US12693088
申请日：2010-01-25
申请人： Casey Hanlon , James Neil Quitmeyer , Allan Blunt
发明人： Casey Hanlon , James Neil Quitmeyer , Allan Blunt
IPC分类号： B64C25/44 , B60T8/17 , B60T13/74
CPC分类号： B64C25/44 , B60T8/1703 , B60T13/741
摘要： A system and method of controlling aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator. An aircraft operational state is determined and an application force that is supplied to the brake pedal is determined. When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized.
摘要翻译：一种控制飞机制动器的系统和方法，该系统和方法包括制动踏板和电制动致动器。确定飞行器操作状态并确定提供给制动踏板的施加力。当确定的飞行器操作状态是地面怠速状态并且所确定的施加力大于设定的力大小时，致动器制动器移动以接合电制动致动器，并且电制动致动器被断电。

4. 发明授权

US08919504B2 Brake actuator assembly with line replaceable motor features 有权
标题翻译：具有线路可更换电机功能的制动执行器组件
公开(公告)号：US08919504B2
公开(公告)日：2014-12-30
申请号：US12732771
申请日：2010-03-26
申请人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer , Allan Blunt
发明人： Casey Hanlon , Kellan Geck , James Neil Quitmeyer , Allan Blunt
IPC分类号： B60L7/00 , B60T7/04 , B60T7/08 , B60T13/74 , F16D65/18 , F16D65/28 , F16D65/00 , F16D121/24 , F16D125/40 , F16D125/48 , F16D127/06
CPC分类号： B60T7/042 , B60T7/085 , B60T13/741 , F16D65/0043 , F16D65/18 , F16D65/28 , F16D2121/24 , F16D2125/40 , F16D2125/48 , F16D2127/06
摘要： An aircraft brake system electromechanical actuator is provided. The actuator is configured with features that allow the electric motor to be a line replaceable unit. One such feature is a foreign-object-damage shield that inhibits dust, debris, and/or other particulate contaminants from entering the electromechanical actuator during electric motor removal and replacement.
摘要翻译：提供飞机制动系统机电致动器。执行器配置有允许电动机成为线路可更换单元的特征。一个这样的特征是异物损坏屏蔽物，其在电动马达移除和更换期间防止灰尘，碎屑和/或其它微粒污染物进入机电致动器。

5. 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。

6. 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.

7. 发明授权

US08319384B2 Electromechanical brake actuator motor brake 有权
标题翻译：机电制动执行器马达制动
公开(公告)号：US08319384B2
公开(公告)日：2012-11-27
申请号：US12968521
申请日：2010-12-15
申请人： Casey Hanlon , James Neil Quitmeyer , David M. Eschborn , Carol Lynn Eschborn, legal representative
发明人： Casey Hanlon , James Neil Quitmeyer , David M. Eschborn
IPC分类号： H02K7/10
CPC分类号： F16D65/14 , F16D55/36 , F16D2121/24 , F16D2125/40 , F16D2125/48 , F16D2127/004 , F16D2127/005 , F16D2127/06 , H02K7/102 , H02K7/116 , Y10T29/49826
摘要： In some examples, a system includes a brake rotor, a brake armature configured to engage with the brake rotor to substantially fix a rotational position of the brake rotor relative to the brake armature, and a mechanism mechanically coupled to the brake armature. The brake armature may be configured to rotate in a first rotational direction and a second rotational direction substantially opposite the first rotational direction. The mechanism may be configured to maintain the brake armature in a fixed rotational position when a torque applied to the brake armature in a second rotational direction is less than or equal to a threshold torque value. The mechanism also may be configured to permit rotation of the brake armature in the second rotational direction when torque on the brake armature in the second rotational direction exceeds the threshold torque value.
摘要翻译：在一些示例中，系统包括制动转子，制动电枢，其被配置为与制动转子接合以基本上固定制动转子相对于制动电枢的旋转位置，以及机构地联接到制动电枢。制动衔铁可以构造成在与第一旋转方向大致相反的第一旋转方向和第二旋转方向上旋转。该机构可以被构造成当在第二旋转方向施加到制动电枢的扭矩小于或等于阈值扭矩值时，将制动器衔铁保持在固定的旋转位置。该机构还可以被构造为当制动电枢在第二旋转方向上的转矩超过阈值扭矩值时允许制动电枢沿第二旋转方向旋转。

8. 发明申请

US20120153753A1 ELECTROMECHANICAL BRAKE ACTUATOR MOTOR BRAKE 有权
标题翻译：电动制动器电动机制动器
公开(公告)号：US20120153753A1
公开(公告)日：2012-06-21
申请号：US12968521
申请日：2010-12-15
申请人： Casey Hanlon , James Neil Quitmeyer , David M. Eschborn , Carol Lynn Eschborn
发明人： Casey Hanlon , James Neil Quitmeyer , David M. Eschborn , Carol Lynn Eschborn
IPC分类号： H02K7/102 , B23P11/00 , B60T11/04
CPC分类号： F16D65/14 , F16D55/36 , F16D2121/24 , F16D2125/40 , F16D2125/48 , F16D2127/004 , F16D2127/005 , F16D2127/06 , H02K7/102 , H02K7/116 , Y10T29/49826
摘要： In some examples, a system includes a brake rotor, a brake armature configured to engage with the brake rotor to substantially fix a rotational position of the brake rotor relative to the brake armature, and a mechanism mechanically coupled to the brake armature. The brake armature may be configured to rotate in a first rotational direction and a second rotational direction substantially opposite the first rotational direction. The mechanism may be configured to maintain the brake armature in a fixed rotational position when a torque applied to the brake armature in a second rotational direction is less than or equal to a threshold torque value. The mechanism also may be configured to permit rotation of the brake armature in the second rotational direction when torque on the brake armature in the second rotational direction exceeds the threshold torque value.
摘要翻译：在一些示例中，系统包括制动转子，制动电枢，其被配置为与制动转子接合以基本上固定制动转子相对于制动电枢的旋转位置，以及机构地联接到制动电枢。制动衔铁可以构造成在与第一旋转方向大致相反的第一旋转方向和第二旋转方向上旋转。该机构可以被构造成当在第二旋转方向施加到制动电枢的扭矩小于或等于阈值扭矩值时，将制动器衔铁保持在固定的旋转位置。该机构还可以被构造为当制动电枢在第二旋转方向上的转矩超过阈值扭矩值时允许制动电枢沿第二旋转方向旋转。

9. 发明授权

US07775120B2 Electromechanical actuator test apparatus 失效
标题翻译：机电执行器测试装置
公开(公告)号：US07775120B2
公开(公告)日：2010-08-17
申请号：US12236345
申请日：2008-09-23
申请人： Kevin Eugene Owens , Robert Jay Blome , Dwayne M. Benson , Steven Talbert Forrest , James Neil Quitmeyer , Hugh Scott McDowell
发明人： Kevin Eugene Owens , Robert Jay Blome , Dwayne M. Benson , Steven Talbert Forrest , James Neil Quitmeyer , Hugh Scott McDowell
IPC分类号： G01M19/00
CPC分类号： G01M99/007
摘要： An electromechanical actuator test system includes an inertia simulator, a first load actuator, a second load actuator, and a test system control. The inertia simulator simulates the inertia of at least a portion of a system that is moved by a test actuator. The first load actuator supplies a first load to the inertia simulator to simulate at least one or more dynamic system loads, and the second load actuator supplies a second load to the inertia simulator to simulate at least one or more steady-state system loads. The test system control supplies the first actuator commands and the second actuator commands.
摘要翻译：机电致动器测试系统包括惯性模拟器，第一负载致动器，第二负载致动器和测试系统控制。惯性模拟器模拟由测试致动器移动的系统的至少一部分的惯性。第一负载致动器向惯性模拟器提供第一负载以模拟至少一个或多个动态系统负载，并且第二负载致动器向惯性模拟器提供第二负载以模拟至少一个或多个稳态系统负载。测试系统控制提供第一个执行器命令和第二个致动器命令。

10. 发明申请

US20100072934A1 FAULT-TOLERANT CONTROL SYSTEM 有权
标题翻译：容错控制系统
公开(公告)号：US20100072934A1
公开(公告)日：2010-03-25
申请号：US12236326
申请日：2008-09-23
申请人： Dwayne M. Benson , James Neil Quitmeyer , William Daugherty
发明人： Dwayne M. Benson , James Neil Quitmeyer , William Daugherty
IPC分类号： G05B9/03 , H02P6/16
CPC分类号： G05B9/03 , G05B2219/37297 , G05B2219/42318 , H02P6/16
摘要： A fault-tolerant position feedback filter may be used in an actuation control system to limit the authority of a first position signal, should the first position signal become erroneous, and thereby prevent a postulated runaway condition of an acuator. The filter includes a difference function, a limited integrator, and a summer The difference function is coupled to receive a first position signal and a combined position error signal and is operable to supply a first position error signal representative of a mathematical difference between the first position signal and the combined position signal. The limited integrator is coupled to receive the first position error signal and operable to supply an integrated position error signal that is limited in magnitude to a predetermined limit. The summer is coupled to receive the integrated position error signal and a second position signal and is operable to supply the combined position error signal. The combined position error signal is representative of a mathematical sum of the integrated position error signal and the second position signal.
摘要翻译：如果第一位置信号变得错误，则可以在致动控制系统中使用容错位置反馈滤波器来限制第一位置信号的权限，从而防止推动器的假设失控状态。滤波器包括差分函数，有限积分器和加法器。差分函数被耦合以接收第一位置信号和组合位置误差信号，并且可操作以提供表示第一位置和第二位置之间的数学差的第一位置误差信号信号和组合位置信号。有限积分器被耦合以接收第一位置误差信号并且可操作以将限制在大小上的集成位置误差信号提供给预定极限。加法器耦合以接收积分位置误差信号和第二位置信号，并且可操作以提供组合的位置误差信号。组合位置误差信号表示积分位置误差信号和第二位置信号的数学和。

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