The invention discloses a vertical take-off and landing fixed-wing aircraft which comprises a fuselage, four rotor wing modules, a control system, a cabin and a power system, an H-shaped wing layout is formed through the four rotor wing modules, vertical take-off is achieved through power generated by the four rotor wing modules during take-off, a runway is not needed, the requirement for the use environment is low, a control system adjusts the rotating speed power of each rotor wing module after being in the air to realize the conversion of the flight attitude, the fuselage is gradually tilted until the level flight state of the fixed wings is achieved, tilting mechanisms do not need to be mounted on the rotor wings, the structure is simple, the reliability is high, and the safety is good. The seat in the cabin can rotate adaptively according to the adjustment of the flight attitude, so that the passenger can keep a horizontal sitting attitude all the time, physiological discomfort caused by the change of the sitting attitude is avoided, and the riding comfort is improved.
本发明公开了一种垂直起降的固定翼飞行器,包括机身、四个旋翼模组、控制系统、座舱和动力系统,通过四个旋翼模组形成H型的机翼布局,起飞时通过四个旋翼模组产生的动力垂直起飞,无需跑道,使用环境要求低,凌空后控制系统调整各个旋翼模组转速功率来实现飞行姿态的转换,逐渐倾转机身直至达到固定翼的平飞状态,旋翼上无需安装倾转机构,结构简单,可靠性高,安全性好。并且座舱内的座椅可以根据飞行姿态的调整自适应转动,使乘员一直保持水平正坐姿态,避免坐姿改变导致的生理不适,提高乘坐舒适度。
Vertical take-off and landing fixed wing aircraft
垂直起降的固定翼飞行器
2022-01-04
Patent
Elektronische Ressource
Chinesisch