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    ELECTROMECHANICAL BRAKE ACTUATOR MOTOR BRAKE
    1.
    发明申请
    ELECTROMECHANICAL BRAKE ACTUATOR MOTOR BRAKE 有权
    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。

    Electromechanical brake actuator motor brake
    2.
    发明授权
    Electromechanical brake actuator motor brake 有权
    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。

    AIRCRAFT ELECTRIC BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE ACTUATOR BRAKE
    5.
    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。

    AIRCRAFT ELECTRIC BRAKE ACTUATION SYSTEM AND METHOD
    6.
    发明申请
    AIRCRAFT ELECTRIC BRAKE ACTUATION SYSTEM AND METHOD 有权
    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。

    Aircraft electric brake actuation system and method
    7.
    发明授权
    Aircraft electric brake actuation system and method 有权
    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。

    REDUNDANT ELECTROMECHANICAL ACTUATOR FOR CONTROL SURFACES
    9.
    发明申请
    REDUNDANT ELECTROMECHANICAL ACTUATOR FOR CONTROL SURFACES 有权
    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。

    HIGH ACCURACY, ZERO BACKLASH ROTARY-TO-LINEAR ELECTROMECHANICAL ACTUATOR
    10.
    发明申请
    HIGH ACCURACY, ZERO BACKLASH ROTARY-TO-LINEAR ELECTROMECHANICAL ACTUATOR 失效
    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。