一种具有滑翔功能的仿生飞行器扭转扑翼结构
The twisting flapping wing structure driven by a dual-axis motor enables the gliding function of flapping-wing aircraft, solving the problems of complex wing structures and inability to glide in existing technologies. It has a compact structure and low energy consumption, and is suitable for a variety of flying organisms.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- XIHUA UNIV
- Filing Date
- 2023-10-30
- Publication Date
- 2026-07-17
AI Technical Summary
The wing structure of existing flapping-wing aircraft fails to achieve ideal flapping and twisting, resulting in the aircraft's inability to glide, and the structure is complex and heavy.
The twisting flapping wing structure is driven by a dual-axis motor. The dual-axis motor drives the first short shaft to rotate, and combined with the swinging and twisting mechanism, the wing flap can swing up and down and twist. The gliding angle is controlled by a clutch and a brake. The structure is compact and requires only two rods and one power source.
It achieves the gliding function of flapping-wing aircraft, has a compact structure, reduces weight and energy consumption, is suitable for the design of various flying organisms, and has high social and economic promotion value.
Smart Images
Figure CN117446236B_ABST