The invention relates to the technical field of quad-rotor unmanned aerial vehicles, in particular to a quad-rotor unmanned aerial vehicle with foldable soft wing auxiliary flight mechanisms. The quad-rotor unmanned aerial vehicle comprises a vehicle body and four main rotors arranged on the two sides of the vehicle body, and further comprises two folding soft wing mechanisms. The two folding softwing mechanisms are arranged on the two sides of the vehicle body correspondingly; and when the two folding soft wing mechanisms are unfolded, auxiliary wings are formed on the two sides of the vehicle body. Contraction cavities are formed in the two sides of the vehicle body; and the two folding soft wing mechanisms are contained in the contraction cavities in the two sides of the vehicle body correspondingly. The flight distance of the unmanned aerial vehicle is increased, the endurance time is prolonged, and the purpose of improving the application and operation capacity of the unmanned aerial vehicle is achieved.
本发明涉及四旋翼无人机技术领域,特别涉及一种具备折叠式软翼辅助飞行机构的四旋翼无人机。包括机身及设置于机身两侧的四个主旋翼,还包括两个折叠式软翼机构;两个折叠式软翼机构分别设置于机身的两侧;当两个折叠式软翼机构展开时,在机身的两侧形成辅助机翼。机身的两侧设有收缩腔;两个折叠式软翼机构分别容置于机身两侧的收缩腔内。本发明提高了无人机的飞行距离,延长了续航时间,达到提高无人机应用作业能力的目的。
Quad-rotor unmanned aerial vehicle with foldable soft wing auxiliary flight mechanisms
一种具备折叠式软翼辅助飞行机构的四旋翼无人机
2021-01-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Quad-rotor unmanned aerial vehicle with foldable wing auxiliary flight mechanisms
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