The invention discloses a novel multi-rotor tilting wing aircraft which comprises a fuselage, a pair of wings located on the two sides of the fuselage, a tail supporting rod set, a horizontal tail wing and a vertical tail wing, the wings are symmetrically arranged on the two sides of the fuselage in an upper single wing layout mode, and the wings comprise tilting section wings and fixed section wings; the tilting section wings can tilt by 90 degrees perpendicular to the fixed section wings, meanwhile, the front edges of the tilting section wings on the two sides of the fuselage are each provided with two rotor power sets, and a lift rotor set is installed at the tail end of the tail supporting rod set. According to the invention, the structural design of half-wing tilting wings is adopted, the advantages of a helicopter aircraft and a fixed-wing aircraft are effectively combined, vertical take-off and landing and high-efficiency cruising speed can be realized, and the interference problem of impact of lower washing flow of the rotors on the wings is solved; meanwhile, the multi-rotor design is adopted, the flight reliability and stability of the aircraft are effectively improved, and meanwhile stable control over the aircraft is achieved more easily through the tilting lift force rotor power sets.
本发明公开了一种新型多旋翼倾转翼飞行器,包括机身、一对位于机身两侧的机翼、尾撑杆组、水平尾翼、垂直尾翼,机翼呈上单翼布局形式对称设置于机身两侧,机翼包括倾转段机翼和固定段机翼,倾转段机翼可实现垂直于固定段机翼的90度倾转,同时在机身两侧倾转段机翼前缘分别安装两组旋翼动力组,尾撑杆组末端安装一组升力旋翼组。本发明采用半翼倾转翼的结构设计,有效结合直升机飞行器和固定翼飞行器的优点,既可实现垂直起降和较高效的巡航速度,又解决了旋翼下洗流对机翼冲击的干扰问题;同时采用多旋翼设计,在有效提高飞行器飞行的可靠性和稳定性同时,通过倾转升力旋翼动力组更容易实现飞行器的稳定控制。
Novel multi-rotor tilting-wing aircraft
一种新型多旋翼倾转翼飞行器
2024-01-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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