The invention provides a rocket booster binding and rocket docking device and method.The rocket booster binding comprises a bracket, a supporting plate and a sliding support, pulleys are arranged at the bottom of the sliding support, a lifting mechanism is arranged on the sliding support, the supporting plate is connected to the upper portion of the lifting mechanism, and the supporting plate is adjusted to move in the vertical direction through the lifting mechanism; a bracket is arranged above the supporting plate, a sliding mechanism is arranged between the supporting plate and the bracket, and the bracket is adjusted to move in the horizontal direction through the sliding mechanism; the top of the bracket is an arc-shaped plate, rollers are arranged on the arc-shaped plate, the booster or the rocket core is placed in the bracket, and the booster or the rocket core is adjusted through the rollers to rotate along the axis of the booster or the rocket core. The six-degree-of-freedom adjusting device has the beneficial effects that six-degree-of-freedom adjustment of the booster or the rocket core level in the up-down direction and the left-right direction in the axis direction and the direction perpendicular to the axis can be achieved, and therefore accurate butt joint of rockets is achieved.

    本发明提供了一种火箭助推器捆绑和火箭对接装置及方法,其中,火箭助推器捆绑包括托座、托板和滑动支座,滑动支座底部设有滑轮,滑动支座上面设置升降机构,升降机构上方连接托板,通过升降机构调节托板沿竖直方向运动;托板的上方设置托座,托板和托座之间设置滑动机构,通过滑动机构调节托座沿水平方向运动;托座的顶部为弧形板,弧形板上设置滚轮,助推器或火箭芯级放置在托座内,通过滚轮调节助推器或火箭芯级沿其轴线旋转。本发明的有益效果为:可以实现调节助推器或火箭芯级在其轴线方向、垂直轴线方向的上下和左右方向的六自由度调节,从而实现火箭的准确对接。


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    Title :

    Rocket booster binding and rocket docking device and method


    Additional title:

    一种火箭助推器捆绑和火箭对接装置及方法


    Publication date :

    2024-09-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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