The invention discloses a flying net catapulting device capable of adjusting a launching angle, a plurality of launching cylinders of the flying net catapulting device are distributed at the top of a base along the circumferential direction of the base, the outer sides of the bottom ends of the launching cylinders are hinged to the base through hinges, and the inner sides of the bottom ends are connected with an angle adjusting mechanism; the angle adjusting mechanism can be movably installed on the base relative to the base and used for adjusting the inclination angle of the launching cylinders; a mass block, a pre-compression spring and a spring base are mounted in a cavity of each launching cylinder; each mass block compresses the corresponding pre-compression spring to the top of the corresponding spring base; one end of each lock pin penetrates through the corresponding launching cylinder and then matches the corresponding mass block in an inserted mode, and the lock pin is used for locking the mass block in the corresponding launching cylinder; a trigger mechanism is connected with each lock pin and used for pulling the lock pin to be separated from the corresponding mass block, so that the mass block is ejected out of the corresponding launching cylinder under the elastic force action of the corresponding pre-compression spring to achieve catapulting trigger of a flying net. The flying net catapulting device can adjust the launching angle according to the distance between a mother satellite and a target to achieve the optimal capturing effect.

    本发明公开了一种可调节发射角度的飞网弹射装置,该飞网弹射装置的多个发射筒沿底座的周向分布于底座的顶部,发射筒的底端外侧通过铰链铰接于底座,底端内侧与角度调节机构连接;角度调节机构能够相对底座移动地安装于底座,用于调节发射筒的倾斜角度;每个发射筒的腔体内均安装有质量块、预压缩弹簧以及弹簧底座;质量块将预压缩弹簧压缩于弹簧底座的顶部;锁销的一端穿过发射筒后与质量块插接配合,用于将质量块锁定于发射筒内;触发机构与锁销相连,用于牵拉锁销脱离质量块,使质量块在预压缩弹簧的弹力作用下弹射出发射筒实现飞网弹射触发。上述飞网弹射装置能够根据母星与目标的距离调节发射角度达到最优捕获效果。


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    Title :

    Flying net catapulting device capable of adjusting launching angle


    Additional title:

    一种可调节发射角度的飞网弹射装置


    Contributors:
    SHAN MINGHE (author) / SHI LINGLING (author) / FU HUANG'AN (author)

    Publication date :

    2021-08-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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