REINFORCED ELECTROMECHANICAL ACTUATOR HOUSING
    1.
    发明申请
    REINFORCED ELECTROMECHANICAL ACTUATOR HOUSING 有权
    加强电动执行器外壳

    公开(公告)号:US20140375179A1

    公开(公告)日:2014-12-25

    申请号:US13922590

    申请日:2013-06-20

    IPC分类号: H02K5/04 B21J5/00

    摘要: An electromechanical actuator housing assembly comprising a reinforcement ring is disclosed herein. The design of the electromechanical actuator housing assembly may be directed to improving load measurement accuracy. The design of the electromechanical actuator housing assembly may be directed to reducing housing deflections. A method of manufacture of an EMA housing assembly is also disclosed herein. This method may include an electromechanical actuator housing assembly having a reinforcement ring.

    摘要翻译: 本文公开了一种包括增强环的机电致动器壳体组件。 机电致动器壳体组件的设计可以用于改善负载测量精度。 机电致动器壳体组件的设计可以用于减小壳体偏转。 本文还公开了一种制造EMA外壳组件的方法。 该方法可以包括具有加强环的机电致动器壳体组件。

    BALL SCREW ASSEMBLY FOR AIRCRAFT BRAKE
    5.
    发明申请
    BALL SCREW ASSEMBLY FOR AIRCRAFT BRAKE 有权
    用于飞机制动器的螺栓组件

    公开(公告)号:US20160123445A1

    公开(公告)日:2016-05-05

    申请号:US14528816

    申请日:2014-10-30

    IPC分类号: F16H25/22 F16D65/16

    摘要: A mechanical linear actuator in an aircraft brake may include a ball nut, a ball screw, and an actuator drive unit housing. The ball screw may rotate to drive the ball nut axially. The ball screw and the actuator drive unit housing may form a series of annular raceways. The ball screw may have a first window corresponding to a first raceway and a second window corresponding to a second raceway. Balls may be inserted into the first raceway through the first window and into the second raceway through the second window.

    摘要翻译: 飞行器制动器中的机械线性致动器可以包括滚珠螺母,滚珠丝杠和致动器驱动单元壳体。 滚珠丝杠可以旋转以轴向驱动滚珠螺母。 滚珠丝杠和致动器驱动单元壳体可以形成一系列环形滚道。 滚珠丝杠可以具有对应于第一滚道的第一窗口和对应于第二滚道的第二窗口。 球可以通过第一窗口插入第一滚道并通过第二窗口进入第二滚道。

    AIRCRAFT BRAKE PUCK ASSEMBLY
    6.
    发明申请
    AIRCRAFT BRAKE PUCK ASSEMBLY 有权
    航空器制动委员会大会

    公开(公告)号:US20160122009A1

    公开(公告)日:2016-05-05

    申请号:US14531648

    申请日:2014-11-03

    IPC分类号: B64C25/44 F16D65/18

    摘要: An electro-mechanical actuator in an aircraft brake may include a ball nut piston, and endcap coupled to the ball nut piston, a retaining ring coupled to the endcap, and a puck secured within the endcap. The puck may be permanently retained within the retaining ring. The retaining ring may be a split ring which is installed around a base of the puck. The puck may be inserted within a single-piece retaining ring, and the retaining ring may be bent over a base of the puck.

    摘要翻译: 飞行器制动器中的机电致动器可以包括滚珠螺母活塞和联接到滚珠螺母活塞的端盖,联接到端盖的保持环和固定在端盖内的圆盘。 圆盘可以永久地保持在固定环内。 保持环可以是围绕圆盘的基部安装的开口环。 圆盘可以插入单片保持环中,并且保持环可以在圆盘的基部上弯曲。