The invention discloses aninstallation and separation mechanism for a booster. One end of an aircraft body is fixedly connected with a ball socket, the other end of the aircraft body is fixedly connected with a suspended beam, a connector fixed to the front end of the booster abuts against the interior of the ball socket, and a rear support is fixed to the rear end of the booster; the lower part of one end of the suspended beam is clamped on the rear support; a rotating shaft connected with the middle of the hook is arranged in the middle of the suspended beam; the hook can freely rotate around the rotating shaft; the lower part of one end of the hook is clamped in a groove formed in the rear support; the same bayonet lock is embedded into the other end of the suspendedbeam and the other end of the hook; the hook and the suspendedbeam are simultaneously clamped through the bayonet lock; meanwhile, the bayonet lock is provided with the steel wire rope connected with the ground fixing end, the bayonet lock is pulled out through the steel wire rope, the booster is separated from the aircraft through the hook, the structure is simple and reliable, the booster is effectively separated from the aircraft, initiating explosive devices are not needed, repeated use can be achieved, and therefore the use cost of the booster is reduced, and the assembly difficulty of the booster is reduced.

    一种用于助推器的安装与分离机构,其中,飞行器本体一端与球窝固定连接,飞行器本体另一端与挂梁固定连接,固定在助推器前端的接头顶入球窝中,后支架固定在助推器后端;挂梁一端下方卡在后支架上,挂梁中部设置有用于连接挂钩中部的转轴,使得挂钩能够绕转轴自由转动,挂钩一端下方卡在后支架上设置的凹槽内,且在挂梁另一端、挂钩另一端嵌入有同一块卡销,通过卡销同时卡住挂钩与挂梁,同时在卡销上设置有与地面固定端连接的钢丝绳,通过钢丝绳将卡销拉出,由挂钩实现助推器与飞行器分离,结构简单可靠,有效实现推器与飞行器分离,无需使用火工品,可多次重复使用,从而降低助推器的使用成本,减小其装配难度。


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    Title :

    Installation and separation mechanism for booster


    Additional title:

    一种用于助推器的安装与分离机构


    Contributors:
    YAO PANPAN (author) / LI YULIANG (author) / DENG JIN (author) / FU JUNXING (author) / JIANG YUTAO (author) / WU HUAQING (author) / HAO GUIZHEN (author) / ZHENG JIAN (author) / DONG HAOWEI (author) / ZHAO YUKUN (author)

    Publication date :

    2020-10-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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