The invention provides an attitude and orbit control cabin turnover lifting appliance and a rocket turnover system. The attitude and orbit control cabin turnover lifting appliance comprises transfer frames, lifting rings and a lifting device, the two transfer frames are oppositely arranged on the two shaft ends of an attitude and orbit control cabin, the lifting ring is detachably mounted on the transfer frames, and the lifting device is connected to the lifting rings. During turnover of the attitude and orbit control cabin, only the lifting rings need to be mounted on the transfer frames on the attitude and orbit control cabin, the structure is simple, the cost is low, an extra structure does not need to be added on the attitude and orbit control cabin, and the self weight of the attitudeand orbit control cabin can be effectively reduced.

    本发明提供了一种姿轨控舱翻转吊具及火箭翻转系统,一种姿轨控舱翻转吊具包括:转接框,两个所述转接框相对设置在姿轨控舱的两轴端处;吊环,可拆卸地设置在所述转接框上;起吊装置,连接在所述吊环上。本发明在实现对姿轨控舱的翻转时,仅需要在姿轨控舱上的转接框处安装吊环即可,结构简单,成本低,且不需要在姿轨控舱上增加额外的结构,有效减少了姿轨控舱自身的重量。


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    Title :

    Attitude and orbit control cabin turnover lifting appliance and rocket turnover system


    Additional title:

    姿轨控舱翻转吊具及火箭翻转系统


    Contributors:
    PENG XIAOBO (author) / DONG YANMIN (author) / LI JINMEI (author)

    Publication date :

    2020-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B66C Krane , CRANES



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