Foldable rotor unmanned aerial vehicle and ejection device thereof
Foldable rotor unmanned aerial vehicle and ejection device thereof
- Neue Suche nach: LU YING
- Neue Suche nach: DENG BAOSONG
- Neue Suche nach: YAO WEN
- Neue Suche nach: ZHU HAI
- Neue Suche nach: GUI JIANJUN
- Neue Suche nach: ZHOU JIEXIN
- Neue Suche nach: LU YING
- Neue Suche nach: DENG BAOSONG
- Neue Suche nach: YAO WEN
- Neue Suche nach: ZHU HAI
- Neue Suche nach: GUI JIANJUN
- Neue Suche nach: ZHOU JIEXIN
The invention relates to the technical field of unmanned aerial vehicles, in particular to a foldable rotor unmanned aerial vehicle and an ejection device thereof. The multiple vehicle arms and the multiple foot stools are arranged on the side walls of the first end and the second end of the vehicle body, and the multiple vehicle arms, the multiple foot stools and the vehicle body are of a hinged connection structure. In addition, the machine body, the machine arms and the foot stands are all installed in an inner shell of the ejection device, and an ejection unit used for ejection is further arranged between the machine body and the inner shell. In actual use, the foldable rotor unmanned aerial vehicle can quickly switch a folding state into a flying state for aerial operation through the ejection effect of the ejection device according to the field use condition. By the adoption of the structural design, the foldable rotor unmanned aerial vehicle can be rapidly switched between the folding state and the flying state, the launching speed of the foldable rotor unmanned aerial vehicle is greatly increased in cooperation with the ejection function of the ejection device, and the preparation time before launching is shortened to the maximum extent.
本申请涉及无人机技术领域，尤其涉及一种可折叠旋翼无人机及其弹射装置。将多个机臂与多个脚架均设置在机身第一端和第二端的侧壁上，并且多个机臂与多个脚架和机身之间为铰接相连的结构。此外，机身连同机臂以及脚架均安装在弹射装置的内壳中，机身与内壳之间还设置有用于进行弹射的弹射单元。在实际使用时，该可折叠旋翼无人机可以根据现场的使用情况，通过弹射装置的弹射作用，迅速将折叠状态切换为飞行状态进行空中作业。采用上述结构设计，可以使得可折叠旋翼无人机能够迅速进行折叠状态与飞行状态之间的切换，并配合弹射装置的弹射功能，极大的提高了可折叠旋翼无人机的发射速度，并最大程度的减少了发射前的准备时间。
Dokumentinformationen
Foldable rotor unmanned aerial vehicle and ejection device thereof
可折叠旋翼无人机及其弹射装置
2024-04-16
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64U |
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