Multi-locking arm quick folding mechanism, unmanned aerial vehicle arm and unmanned aerial vehicle
By using a multi-locking rapid folding mechanism for the boom, and by utilizing the rotational connection between the first and second folding components and the synergistic effect of the locking components, the problem of cumbersome locking and wobbling in the mid-section folding structure of the UAV boom is solved, thereby improving stability and reliability.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- NANCHANG SANRUI INTELLIGENT TECH CO LTD
- Filing Date
- 2026-05-28
- Publication Date
- 2026-07-17
AI Technical Summary
The existing mid-section folding structure of drone arms has problems such as cumbersome locking methods, locking gaps causing swaying that affects flight stability, and insufficient locking force.
The arm quick-folding mechanism employs multiple locking mechanisms. Through the rotational connection of the first and second folding components, combined with the synergistic effect of the first and second locking components, it achieves automatic locking and circumferential limiting, providing progressive locking force and radial preload, thus avoiding additional manual operation.
It simplifies the folding and unfolding operation of the arms, improves flight stability and locking reliability, reduces arm sway, and enhances the stability and reliability of locking performance.
Smart Images
Figure CN122402831A_ABST