The rocket engine turnover mechanism comprises supporting columns, a fixing frame, rotating shafts, shifting blocks and a driving device, the supporting columns are symmetrically arranged at the two opposite ends of the fixing frame, the fixing frame is used for fixing a rocket engine, the rotating shafts are arranged on the side faces, close to the supporting columns, of the fixing frame, and the rotating shafts abut against the supporting columns; the fixing frame can rotate around the rotating shaft, the driving device is fixedly installed on one supporting column, a shifting block is arranged on the side, close to the driving device, of the fixing frame, and the driving device is selectively in transmission connection with the shifting block and can drive the fixing frame to rotate around the rotating shaft. According to the turnover mechanism, the fixing frame can be conveniently detached and adjusted, and therefore the turnover mechanism can be suitable for turnover operation of engines of different models.

    本发明提出了一种火箭发动机翻转机构,包括:支撑柱、固定框架、旋转轴、拨块和驱动装置,支撑柱对称设置在固定框架相对的两端,固定框架用于固定火箭发动机,固定框架靠近支撑柱的侧面均设置有旋转轴,旋转轴抵接在支撑柱上,固定框架可绕旋转轴转动,驱动装置固定安装在其中一个支撑柱上,固定框架靠近驱动装置的一侧设有拨块,驱动装置选择性地与拨块传动连接并可驱动固定框架绕旋转轴转动。本发明提供了一种便于对固定框架进行拆卸和调整的翻转机构,从而可以适用于不同型号的发动机的翻转操作。


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    Titel :

    Rocket engine turnover mechanism


    Weitere Titelangaben:

    一种火箭发动机翻转机构


    Beteiligte:
    XU YE (Autor:in) / GAO ZHIQIANG (Autor:in) / WAN JIANWU (Autor:in) / TU KEHENG (Autor:in) / BAI JUNSONG (Autor:in)

    Erscheinungsdatum :

    2022-05-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last



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