The high-altitude unlocking mechanism comprises a main gear frame and gear sets arranged on the two sides of the main gear frame, third open holes are formed in the two sides of the upper portion of the main gear frame, second open holes are formed in the positions, on the lower sides of the third open holes, of the main gear frame, and first open holes are formed in the positions, on the lower sides of the second open holes, of the gear frame. A pulley is arranged on the lower side of the main gear frame, and a separation lug piece is arranged on the upper side of the main gear frame. According to the high-altitude unlocking mechanism, the pulley is driven by the rope, the pin shaft is driven by the pulley, so that the gear is driven to rotate, the opposite lead screw is separated, unlocking in the high-altitude state is achieved, and the high-altitude unlocking mechanism is high in economical efficiency, high in reliability and high in efficiency of releasing rope constraint in the high-altitude state.
本发明公开了一种高空解锁机构,包括主齿轮架和设置于主齿轮架两侧的齿轮组,所述主齿轮架上部两侧设置有第三开孔,所述第三开孔下侧于主齿轮架上设置有第二开孔,所述第二开孔下侧于齿轮架上设置有第一开孔,所述主齿轮架下侧设置有滑轮,所述主齿轮架上侧设置有分离耳片。本发明采用上述的一种高空解锁机构,通过绳索驱动滑轮,滑轮驱动销轴,从而带动齿轮转动,使对向丝杆分离,实现了高空状态下的解锁,且该机构的经济性高、可靠性高,实现高空状态下解除绳索约束的效率高。
High-altitude unlocking mechanism
一种高空解锁机构
25.08.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft |
Europäisches Patentamt | 2025
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