The invention discloses a side opening type multi-sonde carrying and separating device which comprises a main shell, a locking releaser, a movable shell and an ejection assembly. More than two openings are formed in the outer circumferential surface of the main shell, and the movable shells correspond to the openings one to one; the rear end of each movable shell is hinged with the rear end of the opening; when the carrying and separating device is in a carrying state, the locking releaser locks the front ends of all the movable shells; when the carrying separation device is in a separation state, the locking releaser unlocks the front ends of the more than one movable shell; the front end of the movable shell is separated from the main shell under the action of the elastic piece, and an included angle is formed between the movable shell and the main shell; the ejection assemblies are fixedly connected to the inner side of the movable shell in a one-to-one correspondence mode, and the ejection direction of the sonde faces the front end of the movable shell. More than two sondes can be carried at the same time, the detection efficiency is improved, and the rocket launching cost is reduced; and a side opening mode is adopted, so that the sonde does not generate space interference with other parts when being separated.
本发明公开了一种侧开式多探空仪搭载分离装置,包括:主壳体、锁定释放器、活动壳体和弹射组件;主壳体的外圆周面设置有两个以上开口,活动壳体与开口一一对应设置;每个活动壳体的后端与开口的后端铰接;搭载分离装置处于搭载状态时,锁定释放器对所有活动壳体的前端进行锁定;搭载分离装置处于分离状态时,锁定释放器对一个以上活动壳体的前端进行解锁;活动壳体的前端在弹性件的作用下与主壳体分离,活动壳体与主壳体形成夹角;弹射组件一一对应固定连接在活动壳体内侧,探空仪的弹射方向朝向活动壳体的前端;本发明能够同时搭载两枚以上探空仪,提高探测效率,降低火箭发射成本;且采用侧开方式,探空仪分离时不会与其他部件发生空间干涉。
Side opening type multi-sonde carrying and separating device
一种侧开式多探空仪搭载分离装置
06.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Sonde emitter structure based on unmanned aerial vehicle carrying
Europäisches Patentamt | 2021
|IuD Bahn | 1996
|