The invention discloses a miniature aircraft air ejection mechanism with a variable ejection angle. The ejection mechanism is designed according to the characteristics of miniaturization and light weight of a miniature aircraft, and ejection release of a plurality of miniature aircraft targets is achieved based on a small and medium-sized aircraft carrier platform by means of a cylinder type ejection device. According to the device, a suspension type structure is adopted to fix the ejection cylinder on the aerial carrier platform hanging frame, so that the ejection angle of the micro aircraft can be adjusted, it can be guaranteed that the micro aircraft cannot fall off from the ejection cylinder in the transportation process, and the ejection angle of the micro aircraft can be adjusted in the release process; therefore, the ejected micro aircraft obtains the initial speed in the specific direction.
本发明公开了一种可变弹射角度的微型飞行器空中弹射机构。该弹射机构针对微型飞行器小型化、轻量化的特点设计,借助筒式弹射装置,基于中小型飞行器载机平台实现多个微型飞行器目标的弹射释放。装置采用悬吊式结构将弹射筒固定在载机平台挂架上实现微型飞行器弹射角度可调,既能够保证微型飞行器运输过程不会从弹射筒中脱落,又能实现微型飞行器释放过程弹射角度可调,从而使被弹射出去的微型飞行器获得特定方向的初速度。
Miniature aircraft air ejection mechanism with variable ejection angle
一种可变弹射角度的微型飞行器空中弹射机构
2024-05-24
Patent
Electronic Resource
Chinese
IPC: | B64U |
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