一种无人机缓冲起落架及缓冲方法
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- CHINA JILIANG UNIV
- Filing Date
- 2024-05-29
- Publication Date
- 2026-07-17
AI Technical Summary
The existing drone landing gear structure is relatively simple, mainly relying on spring components for support and cushioning. This causes airflow disturbances when the rotating fan blades shorten the distance to the ground during drone landing, affecting landing stability.
Design a buffer landing gear for unmanned aerial vehicles (UAVs), including a support frame, blade shaft, braking structure, drive structure, and landing gear. It utilizes friction braking and elastic element support, and through the cooperation of connecting rods, spring plates, and compression frames, it reduces the impact of airflow disturbance and improves landing stability.
By using friction braking and elastic support, the impact of airflow disturbance on UAV landing is reduced, landing stability is improved, drive equipment is saved, wear is reduced, and the structural functionality of the landing gear is enhanced.
Smart Images
Figure CN118387339B_ABST