The invention discloses an ejection releasing and recycling mechanism capable of being repeatedly unlocked and locked for tethered satellites and a working method of the ejection releasing and recycling mechanism, and belongs to the field of tethered satellite releasing and recycling. The separation ejection butt joint assembly comprises an ejection sleeve, a locking mechanism and a child star connecting piece, the ejection sleeve is in two-section type internal and external sliding connection, and initial kinetic energy is provided for a child star through a compression spring; the locking mechanism is installed in the ejection sleeve, one end of the child star connecting piece is connected with the child star, and the other end of the child star connecting piece is in sliding fit with the locking mechanism to complete locking/unlocking action of the child star. The mechanism does not need an additional control assembly to control unlocking and locking of the mechanism, the complexity of the mechanism can be effectively reduced, and the overall reliability of the mechanism is improved.
本发明公开了一种用于绳系卫星可重复解锁锁止的弹射释放回收机构及其工作方法,属于绳系卫星释放和回收领域,本发明包括分离弹射对接组、子星;所述分离弹射对接组件包括弹射套筒、锁止机构、子星连接件,所述弹射套筒为两段式内外滑动连接,通过压缩弹簧为子星提供初始动能;所述锁止机构安装于在弹射套筒内部,所述子星连接件一端与子星连接,另一端与锁止机构滑动配合完成子星的锁止/解锁动作。本发明机构无需额外的控制组件来控制机构解锁锁止,能够有效降低机构复杂程度,提升机构整体可靠性。
Ejection release recovery mechanism capable of being repeatedly unlocked and locked and used for tethered satellite and working method of ejection release recovery mechanism
一种用于绳系卫星可重复解锁锁止的弹射释放回收机构及其工作方法
04.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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