The invention relates to the technical field of aerospace, in particular to a satellite and rocket separation unlocking device which comprises a main body base, a locking assembly, a connecting assembly and a driving assembly, the main body base is used for being fixed to a carrying tool, and the connecting assembly is used for being connected with a load; the locking assembly and the driving assembly are both installed on the main body base, the driving assembly is used for making contact with the load, and the locking assembly is used for locking the connecting assembly so that the driving assembly can make contact with the connecting assembly. The locking assembly is used for unlocking the connecting assembly so that the driving assembly can drive the connecting assembly to be separated from the locking assembly. The invention aims to provide a satellite and rocket separation unlocking device aiming at at least one technical problem related in the prior art.

    本申请涉及航空航天技术领域,具体而言,涉及一种星箭分离解锁装置,包括主体基座、锁定组件、连接组件和驱动组件,所述主体基座用于固定在运载工具上,所述连接组件用于与载荷连接,所述锁定组件和所述驱动组件均安装于所述主体基座,所述驱动组件用于与所述载荷接触,所述锁定组件用于锁定所述连接组件以使所述驱动组件与所述连接组件接触,且所述锁定组件用于对所述连接组件解锁以使所述驱动组件能够驱动所述连接组件与所述锁定组件分离。本申请的目的在于针对现有技术中所涉及的至少一个技术问题,提供一种星箭分离解锁装置。


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    Title :

    Satellite-rocket separation unlocking device


    Additional title:

    星箭分离解锁装置


    Contributors:
    CHEN YU (author) / GAO ENYU (author) / JIANG XIUPENG (author) / YAN ZHOU (author)

    Publication date :

    2024-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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