The invention discloses a multi-mode conversion micro-miniature unmanned aerial vehicle which comprises a fuselage, deformable wings, a wing flapping system, a main shaft, a main shaft rotation control system and an empennage. The main shaft is vertically installed at the gravity center position of the fuselage through the main shaft rotation control system, and the deformable wings are distributed on the two sides of the top end of the main shaft and flap up and down through the wing flapping system. The empennage is mounted at the tail of the fuselage; when the deformable wings on the two sides are of a central symmetry structure, a flapping rotor wing mode is formed, and the main shaft rotates under the control of the main shaft rotation control system; the deformable wings are in an axial symmetry structure to form a flapping wing mode after being deformed, and the main shaft stops rotating under the control of the main shaft rotation control system. According to the invention, vertical take-off and landing, spot hovering and rapid take-off can be realized.
本发明公开了一种多模式转换微小型无人机,包括机身、可变形机翼、机翼扑动系统、主轴、主轴旋转控制系统及尾翼;主轴通过主轴旋转控制系统竖直安装在机身重心位置,可变形机翼分布于主轴顶端两侧且通过机翼扑动系统上下扑动;所述尾翼安装在机身尾部;两侧的可变形机翼呈中心对称结构时形成扑旋翼模式,主轴在主轴旋转控制系统的控制下转动;可变形机翼变形后呈轴对称结构形成扑翼模式,主轴在主轴旋转控制系统的控制下停止转动。本发明能够实现垂直起降、定点悬停、快速起飞。
Multi-mode conversion micro-miniature unmanned aerial vehicle
一种多模式转换微小型无人机
2021-08-06
Patent
Electronic Resource
Chinese
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