The invention relates to a satellite-rocket separation device with separation guiding and a satellite-rocket separation method.The satellite-rocket separation device with separation guiding comprises a pin puller, a lock seat, a lock cylinder barrel, a separation spring, an unlocking push rod, a spring sleeve, a lock body, a lock block, a lock cylinder spring and a limiting rod, the lock seat is provided with an assembly cavity, and the pin puller is arranged on the side wall of the assembly cavity; the lock cylinder barrel is installed at the upper end of the assembly cavity and is coaxial with the assembly cavity, the spring sleeve coaxially sleeves the unlocking push rod, the lower end of the spring sleeve is connected with the lower end of the unlocking push rod, the unlocking push rod coaxially sleeves the interior of the lower end of the lock cylinder barrel, and the spring sleeve sleeves the exterior of the lower end of the lock cylinder barrel; the lower end of the separation spring is connected with the lower end of the assembly cavity, and the upper end of the separation spring is connected with the upper end of the spring sleeve; the pin puller can stretch out and draw back in the radial direction of the assembly cavity to achieve locking or unlocking of the spring sleeve. The lock body is installed in the lock cylinder barrel in a matched mode and can stretch out of the upper end of the lock cylinder barrel, and a satellite connecting rod is arranged at the upper end of the lock body.
本发明涉及一种带分离导向的星箭分离装置及星箭分离方法,带分离导向的星箭分离装置包括拔销器、锁座、锁芯筒、分离弹簧、解锁推杆、弹簧套筒、锁体、锁块、锁芯弹簧和限位杆,锁座具有装配腔体,装配腔体的侧壁设有拔销器;锁芯筒安装在装配腔体上端且与装配腔体同轴布置,弹簧套筒同轴套设在解锁推杆外且弹簧套筒下端与解锁推杆下端连接,解锁推杆同轴套设在锁芯筒下端内部,弹簧套筒套设在锁芯筒的下端外部;分离弹簧套设在弹簧套筒外侧,分离弹簧下端与装配腔体下端连接,分离弹簧上端与弹簧套筒上端连接;拔销器能沿装配腔体径向伸缩实现对弹簧套筒的锁定或解锁;锁体适配安装在锁芯筒内且能从锁芯筒上端伸出,锁体上端设有卫星连接杆。
Satellite-rocket separation device with separation guiding function and satellite-rocket separation method
一种带分离导向的星箭分离装置及星箭分离方法
2024-11-15
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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