The invention discloses a fixed-wing aircraft-oriented variant wing with a continuously variable wing shape, which comprises rotary wing systems distributed on two sides of an axis of a fuselage, the rotary wing systems are mounted on the fixed wing of the fuselage, a driving motor is mounted on the fuselage, and the driving motor controls the rotary wing systems to work through a transmission system. According to the variant wing with the continuously variable wing shape for the fixed-wing aircraft, the flight performance of the fixed-wing aircraft can be improved so as to adapt to different flight environments and meet the task requirements of high-speed, low-speed and short-distance take-off and landing, and therefore large-speed-range and full-time maneuvering flight of the aircraft is achieved.
本发明公开了面向固定翼飞机的连续可变翼形的变体机翼,包括分布在机身轴线两侧的转翼系统,转翼系统安装在机身的固定式机翼上,机身上安装有驱动电机,驱动电机通过传动系统控制转翼系统工作。本发明所提供的面向固定翼飞机的连续可变翼形的变体机翼,能提升固定翼飞机的飞行性能,以适应不同的飞行环境,满足高速、低速、短距起降的任务需求,从而实现飞行器的大速域、全时段的机动飞行。
Variable wing of continuous variable wing shape facing fixed wing aircraft
面向固定翼飞机的连续可变翼形的变体机翼
2023-08-29
Patent
Elektronische Ressource
Chinesisch
Wing sweep angle variable mechanism of large variable wing aircraft
Europäisches Patentamt | 2023
|