一种可变形翼发融合环形机翼和电动垂直起降飞行器
By using a deformable wing-engine fusion annular wing design, the problems of low aerodynamic efficiency and insufficient safety in eVTOL design are solved, achieving efficient airflow utilization and structural strength enhancement of the wing, thereby improving the overall performance and stability of the aircraft.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- UNIV OF SCI & TECH BEIJING
- Filing Date
- 2025-03-03
- Publication Date
- 2026-07-17
AI Technical Summary
Existing electric vertical takeoff and landing (eVTOL) aircraft designs suffer from low aerodynamic efficiency, high requirements for takeoff and landing sites, low lift-to-thrust conversion efficiency, and insufficient safety, which limits their application in urban environments.
It adopts a deformable wing-engine fusion annular wing design, including a canard, curved side wings and a rear wing, which are connected into an annular wing through a rotating structure and integrated with a ducted fan to achieve airflow optimization and thrust vector adjustment. Combined with linkage mechanism and flap control, it optimizes airflow distribution and adjusts wing state.
It improves the service life and reliability of the wings, enhances structural strength and compactness, reduces production costs and failure probability, improves aerodynamic performance and flight stability, and increases the efficiency of vertical takeoff and landing and horizontal flight as well as fuel efficiency.
Smart Images
Figure CN119975775B_ABST