The invention provides a satellite-borne rotating wheel type multiple separation device which comprises an ejection device (1), a drive locking mechanism (2), a wheel type rotating disc (3), an impactor (4) and a satellite body (5), and the ejection device (1) provides thrust when the impactor (4) is separated; and the locking mechanism (2) is driven to rotate, replace and limit the impactor (4). When the impactor is launched, the impactor is pushed away through the magnetic force of the ejection device (1); when the impactor is replaced, the next impactor is rotated to the impact opening through the driving motor (21), limiting and locking are carried out through matched use of the locking spring component (22) and a limiting device on the supporting structure (31), and launching preparation of the second impactor is completed. The requirement for continuous launching of multiple impactors is met, and multiple times of separated launching of the impactors in a short time are achieved. Meanwhile, the rotating wheel type separating device can be arranged as an independent module and carried on different detectors, and has certain universality.

    本发明提供了一种星载转轮式多次分离装置,包括弹射装置(1)、驱动锁定机构(2)、轮式转盘(3)、撞击器(4)和星本体(5),弹射装置(1)为撞击器(4)分离时提供推力;驱动锁定机构(2)进行撞击器(4)旋转更换及限位。发射撞击器时通过弹射装置(1)的磁力将撞击器推离;更换撞击器时,通过驱动电机(21)将下一个撞击器旋转到撞击口处,并通过锁定弹簧部件(22)与支撑结构(31)上的限位装置配合使用进行限位锁定,完成第二发撞击器的发射准备。本发明满足多个撞击器连续发射的需求,实现短时间内多次撞击器的分离发射。同时,该转轮式分离装置可设为独立的模块,搭载在不同的探测器上,具备一定的通用性。


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    Title :

    Satellite-borne rotating wheel type multi-separation device


    Additional title:

    星载转轮式多次分离装置


    Contributors:
    GENG ZHIQING (author) / ZHAO LIN (author) / XIA GUOJUN (author) / PENG YUMING (author) / LU XI (author) / WANG WEI (author)

    Publication date :

    2023-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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