利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

23 条记录 (耗时 0.023 秒)

    ACTUATION ASSEMBLY
    1.
    发明申请
    ACTUATION ASSEMBLY 失效
    执行装配

    公开(公告)号：US20120181372A1

    公开(公告)日：2012-07-19

    申请号：US12252175

    申请日：2008-10-15

    申请人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    发明人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    IPC分类号： F42B15/01 ,  F15B15/18 ,  F15B15/02

    CPC分类号： F42B10/663 ,  F42B10/665 ,  Y10T74/18568

    摘要： An actuation assembly is provided. The actuation assembly includes a casing, a plurality of linear actuators coupled to the casing, each of the linear actuators having first and second components and being configured to move the second component thereof relative to the first component thereof along a respective first axis, and a plurality of translational member sets, each being coupled to the second component of a respective one of the linear actuators and the casing and being configured such that when the second component of the respective linear actuator moves along the respective first axis, a selected portion of the translational member set moves substantially along a respective second axis.

    摘要翻译： 提供致动组件。 致动组件包括壳体，联接到壳体的多个线性致动器，每个线性致动器具有第一和第二部件，并且构造成沿相应的第一轴线相对于其第一部件移动其第二部件，并且 多个平移构件组，每个平行构件组联接到线性致动器和壳体中的相应一个的第二部件，并且构造成使得当相应的线性致动器的第二部件沿着相应的第一轴线移动时，所选择的部分 平移构件组基本上沿相应的第二轴线移动。

    DUAL DRIVE ELECTROMECHANICAL ACTUATOR WITH CENTER OUTPUT
    3.
    发明申请
    DUAL DRIVE ELECTROMECHANICAL ACTUATOR WITH CENTER OUTPUT 失效
    双驱动电动执行器，带中央输出

    公开(公告)号：US20100072842A1

    公开(公告)日：2010-03-25

    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

    IPC分类号： H02K7/06 ,  F16H25/20

    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) are provided that 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： 提供了机电致动器（EMA），其包括设置在两个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

    Actuation assembly
    4.
    发明授权
    Actuation assembly 失效
    启动装配

    公开(公告)号：US08338768B2

    公开(公告)日：2012-12-25

    申请号：US12252175

    申请日：2008-10-15

    申请人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    发明人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    IPC分类号： F42B10/66 ,  F42B10/00 ,  F16H27/02

    CPC分类号： F42B10/663 ,  F42B10/665 ,  Y10T74/18568

    摘要： An actuation assembly is provided. The actuation assembly includes a casing, a plurality of linear actuators coupled to the casing, each of the linear actuators having first and second components and being configured to move the second component thereof relative to the first component thereof along a respective first axis, and a plurality of translational member sets, each being coupled to the second component of a respective one of the linear actuators and the casing and being configured such that when the second component of the respective linear actuator moves along the respective first axis, a selected portion of the translational member set moves substantially along a respective second axis.

    摘要翻译： 提供致动组件。 致动组件包括壳体，联接到壳体的多个线性致动器，每个线性致动器具有第一和第二部件，并且构造成沿相应的第一轴线相对于其第一部件移动其第二部件，并且 多个平移构件组，每个平行构件组联接到线性致动器和壳体中的相应一个的第二部件，并且构造成使得当相应的线性致动器的第二部件沿着相应的第一轴线移动时，所选择的部分 平移构件组基本上沿相应的第二轴线移动。

    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。