The invention relates to a foldable unmanned aerial vehicle ejection device which comprises a storage box, a supporting mechanism and an ejection mechanism, the storage box comprises a cover body part and a box body part, the cover body part and the box body part are rotationally connected, the supporting mechanism comprises a supporting plate and a supporting rod, the box body part is provided with a storage groove, the supporting plate is rotationally connected to the box body part and located in the storage groove, and the ejection mechanism is located in the storage groove. The supporting rod is rotationally connected to the supporting plate, the ejection mechanism comprises an ejection rail and an ejection assembly, when the ejection device is erected, one free end of the ejection rail is in abutting fit with the supporting rod, the other free end of the ejection rail is in abutting fit with the cover body part, and the ejection assembly is used for driving the fixed-wing unmanned aerial vehicle to slide along the ejection rail; the supporting mechanism is used for supporting one end of the ejection track. The ejection device has the effect of shortening the erection time of the ejection device.
本申请涉及一种可折叠式无人机弹射装置,其包括收纳箱、支撑机构以及弹射机构,收纳箱包括盖体部和箱体部,盖体部和箱体部转动连接,支撑机构包括支撑板和支撑杆,箱体部开设有收纳槽,支撑板转动连接于箱体部并位于收纳槽,支撑杆转动连接于支撑板,弹射机构包括弹射轨道和弹射组件,弹射装置架设时,弹射轨道一自由端与支撑杆抵接配合,弹射轨道另一自由端与盖体部抵接配合,弹射组件用于带动固定翼无人机沿弹射轨道滑移,支撑机构用于支撑弹射轨道的一端。本申请具有减少弹射装置架设时间的效果。
Foldable unmanned aerial vehicle ejection device
一种可折叠式无人机弹射装置
2024-01-16
Patent
Electronic Resource
Chinese
IPC: | B64U |
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