The invention provides a quick unlocking and separating mechanism for a docking satellite, a mechanism body can be connected with a to-be-connected first assembly and a to-be-connected second assembly, and the mechanism body comprises a base body part and an unlocking part configured on the base body part; the unlocking part can enable the to-be-connected second assembly to be connected with/separated from the to-be-connected first assembly under the locking/unlocking condition; the base body part comprises a base unit and an elastic unit arranged on the base unit; under the condition that the to-be-connected second assembly is connected with the to-be-connected first assembly, the elastic unit is in a compressed state; the unlocking part comprises a fixed unit and a movable unit, the fixed unit is used for connecting the base body part, the bottom of the movable unit can be movably connected to the fixed unit, and the top can be connected to the second unit; the movable unit can be connected to the fixed unit in an electromagnetic mode. According to the method, the difficulty of separation operation of the docking satellite is simplified, the efficiency is improved, the cost is controlled, and the method has certain practical significance.
本发明提供一种对接卫星的快速解锁分离机构,机构本体能够连接待连接第一组件和待连接第二组件,机构本体包括基体部分以及配置于基体部分的解锁部分;解锁部分能够在锁紧/解锁的情形下,使待连接第二组件连接/脱离于待连接第一组件;基体部分包括基座单元以及配置于基座单元的弹性单元;在待连接第二组件连接待连接第一组件的情形下,弹性单元处于压缩状态;解锁部分包括固定单元和活动单元,固定单元用于连接基体部分,活动单元的底部能够活动连接于固定单元、顶部能够连接于第二单元;活动单元能够通过电磁的方式连接于固定单元。本发明简化了对接卫星的分离作业的难度,提升了效率,且控制了成本,具有一定的实用意义。
Quick unlocking and separating mechanism for docking satellites
一种对接卫星的快速解锁分离机构
2024-06-11
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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