一种飞行器的旋转折叠机翼和飞行器
By using a rotating folding wing design and a motor-driven cam mechanism and limit mechanism, the wing can be quickly deployed and locked, solving the problem of complex wing deployment mechanisms in existing technologies and improving the stability and reliability of the aircraft.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- AVIC XIAN AIRCRAFT IND GRP CO LTD
- Filing Date
- 2025-05-30
- Publication Date
- 2026-07-17
AI Technical Summary
In existing technologies, wing deployment mechanisms are complex, making it difficult to quickly and reliably fold, deploy, and lock the wings, which affects the maneuverability and stability of the aircraft.
The design features a rotating folding wing. A cam mechanism and a limiting mechanism driven by a motor enable the wing to unfold and lock quickly. The locking mechanism is achieved by the combined action of a limiting hook and a baffle after a set angle is reached. The combination of a pull rod and a compression spring ensures that the wing is fixed in the folded state.
It enables rapid deployment and locking of wings, simplifies mechanism design, reduces weight, is suitable for small aircraft, meets the folding, deployment and locking requirements under small space conditions, and improves the stability and reliability of aircraft.
Smart Images
Figure CN120482341B_ABST