The invention discloses a partially fixed wing type wing-engine co-rotating vertical take-off and landing aircraft which comprises an aircraft fuselage and a front wing and a rear wing which are arranged on the aircraft fuselage, each of the front wing and the rear wing comprises a fixed wing connected with the aircraft fuselage, and tilting wings are hinged to the ends, away from the aircraft fuselage, of the fixed wings. The rotating axes of the tilting wings horizontally extend inwards and are perpendicular to the axis of the aircraft fuselage, propellers rotating along with the tilting wings are arranged on the tilting wings, geometrically, one ends of rotating shafts of the propellers are arranged on the tilting wings, the other ends of the rotating shafts extend in the advancing or rising direction of the aircraft fuselage, and negative included angles are formed between the rotating shafts and the plane where the tilting wings are located. Lift force is generated by completely depending on vertical suspension of the engine in the hovering state, lift force is generated by completely depending on the wings in the flat flying state, and the two are combined in the transition state, so that the aircraft flies in the most reasonable working mechanism when the tilting wings are at any tilting angle.
本发明公开的一种部分固定翼式翼发共转的可垂直起降飞行器,包括飞行器机身及设置在飞行器机身上的前翼和后翼,前翼和后翼均包括与飞行器机身相连接的固定翼,固定翼远离飞行器机身的端部铰接有倾转翼,倾转翼的转动轴线水平向内延伸并垂直于飞行器机身轴线,各倾转翼上均设有随其转动的螺旋桨,在几何上,螺旋桨的旋转轴一端设置在倾转翼上,另一端沿飞行器机身前进或升高的方向延伸,且旋转轴与倾转翼所在平面形成负夹角,在悬停态完全依靠发动机的垂直悬吊产生升力,在平飞态完全依靠机翼产生升力,在转换过渡态将二者结合,使得倾转翼在任意倾转角下飞行器均以最合理的工作机制飞行。
Partially fixed wing type wing-generator co-rotating vertical take-off and landing aircraft
一种部分固定翼式翼发共转的可垂直起降飞行器
2024-01-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |