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    SUPPORT ASSEMBLY
    1.
    发明申请
    SUPPORT ASSEMBLY 有权
    支持大会

    公开(公告)号：US20140158822A1

    公开(公告)日：2014-06-12

    申请号：US14101791

    申请日：2013-12-10

    Applicant: AIRBUS OPERATIONS LIMITED

    Inventor： Anthony LANGLEY ,  Simon KING

    IPC: B64C13/28

    CPC classification number: B64C9/02 ,  B64C9/16 ,  B64C9/22 ,  Y02T50/44

    Abstract: An assembly to support a wing leading or trailing edge device during deployment and retraction of the device includes a fixed support member attachable to the support structure of an aircraft wing, an intermediate link arm having one end pivotally mounted for rotation relative to the support member about a first axis and, a primary link arm having a first end pivotally mounted to the opposite end of the intermediate link arm for rotation relative to the intermediate link arm about a second axis. A second end of the primary link arm is for attachment to the device via a bearing element so that the device can move relative to the primary link arm in any direction when the intermediate and primary link arms rotate about the first and second axes, respectively, during deployment or retraction of the device from the aircraft wing.

    Abstract translation: 在装置的展开和缩回期间支撑机翼前缘或后缘装置的组件包括可附接到飞行器机翼的支撑结构的固定支撑构件，中间连杆臂，其一端枢转地安装成相对于支撑构件旋转约 第一轴线和主连杆臂，其具有枢转地安装到中间连杆臂的相对端的第一端，用于相对于中间连杆臂围绕第二轴线旋转。 主连杆臂的第二端用于经由轴承元件附接到装置，使得当中间和主连杆臂分别围绕第一和第二轴线旋转时，该装置可以在任何方向上相对于主连杆臂移动， 在从飞机机翼部署或撤回设备时。

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