The invention discloses an inclined strut type floating self-adaptive spray pipe capturing tool, and relates to the technical field of space flight and aviation. The problem that after a satellite is captured by an existing jet pipe capturing tool, connection between a conical rod and an engine jet pipe is not stable is solved. A locking supporting section shell and a posture adjusting positioning section shell are connected through a constant velocity universal joint, a locking module is installed in the locking supporting section shell, a driving module, a positioning module and a posture adjusting module are arranged in the posture adjusting positioning section shell, one end of the driving module is fixedly connected with the tail end of the locking supporting section shell, and the other end of the driving module is fixedly connected with the positioning module. The other end of the driving module is connected with one end of the positioning module, the other end of the positioning module is rotationally connected with one end of the posture adjusting module, and the other end of the posture adjusting module is connected to the inner wall of the posture adjusting and positioning section shell; one end of the despinning module is connected with the tail end of the posture adjusting and positioning section shell, the other end of the despinning module is fixedly connected with one end of the electrical module, and the other end of the electrical module is fixedly connected with one end of the quick-change interface. The method is mainly used for capturing the space satellites.

    一种斜撑式浮动自适应喷管抓捕工具,涉及航天航空技术领域。为了解决现有的喷管抓捕工具在抓捕到卫星后,锥杆与发动机喷管存在连接不稳定的问题。本发明中锁紧支撑段外壳与调姿定位段外壳通过等速万向节进行连接,锁紧模块安装在锁紧支撑段外壳内,驱动模块、定位模块和调姿模块设置在调姿定位段外壳内,驱动模块的一端与锁紧支撑段外壳的尾端固连,驱动模块的另一端与定位模块的一端连接,定位模块的另一端与调姿模块的一端转动连接,调姿模块的另一端连接在调姿定位段外壳的内壁上;消旋模块的一端与调姿定位段外壳的尾端连接,消旋模块的另一端与电气模块的一端固连,电气模块的另一端与快换接口的一端与固连。本发明主要用于抓捕空间卫星。


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    Title :

    Inclined strut type floating self-adaptive spray pipe capturing tool


    Additional title:

    一种斜撑式浮动自适应喷管抓捕工具


    Contributors:
    LI XUEAI (author) / SUN KUI (author) / CAO BAOSHI (author) / LIU HONG (author)

    Publication date :

    2022-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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