Auxiliary multi-rotor unmanned aerial vehicle flight system

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Auxiliary multi-rotor unmanned aerial vehicle flight system

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HE YUQING / YANG LIYING / TAO BO / CHANG YANCHUN / MA LIXIN / HUANG CHAOXIONG / LI SILIANG

The invention relates to the technical field of multi-rotor unmanned aerial vehicles, in particular to an auxiliary multi-rotor unmanned aerial vehicle flight system. The system comprises a fuselage and four main rotors arranged on the two sides of the fuselage, and further comprises two retractable auxiliary rotors. The two retractable auxiliary rotors are located on the two sides of the fuselage correspondingly and can be retracted and released. When the two retractable auxiliary rotors are unfolded, auxiliary rotors are formed on the two sides of the fuselage. Accommodating cabins are arranged on two sides of the fuselage. The two retractable auxiliary rotors can be accommodated in the two accommodating cabins respectively. The flight speed and steering capability of the unmanned aerial vehicle are improved, the unmanned aerial vehicle flies for a farther distance in a short time and can rapidly and horizontally rotate in situ, and the purpose of improving the application operation capability of the unmanned aerial vehicle is achieved.

本发明涉及多旋翼无人机技术领域，特别涉及一种辅助多旋翼无人机飞行系统。包括机身及设置于机身两侧的四个主旋翼，还包括两个收放式副旋翼；两个收放式副旋翼分别位于机身的两侧，可进行收放；当两个收放式副旋翼展开时，在机身的两侧形成辅助旋翼。机身的两侧设有收容舱；两个收放式副旋翼可分别收纳于两个收容舱内。本发明提高了无人机的飞行速度及转向能力，实现无人机在短时间内飞行更远的距离和能够快速原地水平旋转，达到提高无人机应用作业能力的目标。

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Title :

Auxiliary multi-rotor unmanned aerial vehicle flight system

Additional title:

一种辅助多旋翼无人机飞行系统

Contributors:

HE YUQING (author) / YANG LIYING (author) / TAO BO (author) / CHANG YANCHUN (author) / MA LIXIN (author) / HUANG CHAOXIONG (author) / LI SILIANG (author)

Publication date :

2021-11-16

Type of media :

Patent

Type of material :

Electronic Resource

Language :

Chinese

Classification :

IPC:

B64C AEROPLANES , Flugzeuge