通气降载增稳结构、圆柱体飞行器及降载增稳方法
By setting up exhaust bays and sliding microstructure groups on the surface of the aircraft to form a stable air film, the problem of attitude instability of high-speed aircraft during underwater launch was solved, the rapid construction and stability of the air film was achieved, and the attitude stability and load reduction effect were improved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- PEKING UNIV
- Filing Date
- 2026-05-20
- Publication Date
- 2026-07-17
AI Technical Summary
When high-speed aircraft are launched underwater, the porous exhaust technology has difficulty in quickly building and maintaining a stable air film in extreme environments, resulting in attitude instability and affecting the aircraft's load reduction and stabilization effect.
The structure employs a ventilation-based load reduction and stabilization system, which includes an exhaust compartment and a sliding microstructure group. Gas is discharged through exhaust vents to form bubbles, which expand and merge in the grid gaps to form an air film. The superhydrophobic coating and sliding microstructure are used to control the bubble migration path, thereby achieving rapid construction and stability of the air film.
It improves the attitude stability of the aircraft, reduces the peak hydrodynamic load, and enhances the motion stability of the aircraft during underwater launch.
Smart Images
Figure CN122232859B_ABST