Aircraft landing gear loader
    2.
    发明申请
    Aircraft landing gear loader 审中-公开
    飞机起落架装载机

    公开(公告)号:US20070110552A1

    公开(公告)日:2007-05-17

    申请号:US11274036

    申请日:2005-11-15

    CPC classification number: B66F7/22 B64F5/50 B66F7/14

    Abstract: An apparatus for loading the main landing gear (“MLG”) of a large aircraft includes a support frame having symmetrical side portions disposed on opposite sides of a sagittal plane of the MLG. A pair of opposing slide mechanisms are coupled to opposite sides of the MLG and supported on a corresponding side of the support frame for translation of the MLG in the sagittal plane. Two pairs of laterally opposing vertical jacks are mounted on opposite sides of the support frame, and respective opposite ends of the slide mechanisms are rotatably coupled to corresponding output ends of the jacks, such that raising or lowering the output ends of the jacks in one opposing pair relative to the output ends of the other pair results in rotation of the MLG in the sagittal plane. A drive mechanism on the support frame enables translation and rotation of the MLG in a horizontal plane.

    Abstract translation: 用于装载大型飞行器的主起落架(“MLG”)的装置包括:支撑框架,其具有设置在MLG的矢状平面的相对侧上的对称侧部。 一对相对的滑动机构联接到MLG的相对侧并且支撑在支撑框架的相应侧上,用于在矢状平面中翻译MLG。 两对横向相对的垂直千斤顶安装在支撑框架的相对侧上,并且滑动机构的相应的相对端可旋转地联接到千斤顶的相应的输出端,使得在一个相对的位置上升或降低千斤顶的输出端 相对于另一对的输出端的对导致MLG在矢状面中的旋转。 支撑框架上的驱动机构使得MLG能够在水平面中平移和旋转。

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