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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
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。
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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。
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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
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。
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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。
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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.
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6.发明申请AIRCRAFT ELECTRIC BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE ACTUATOR BRAKE 有权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。
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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
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。
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公开(公告)号：US20120153753A1
公开(公告)日：2012-06-21
申请号：US12968521
申请日：2010-12-15
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。
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公开(公告)号：US08742711B2
公开(公告)日：2014-06-03
申请号：US13240933
申请日：2011-09-22
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。
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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
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。
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