The invention discloses a foldable composite wing type vertical take-off and landing aerocar, which belongs to the technical field of aerocars and comprises a car body, a vertical motion control system, a forward power control system and a flight attitude control system. The vertical motion power systems are telescopically and symmetrically mounted on the two sides of the vehicle body, and the forward power system is mounted at the tail of the vehicle body and used for generating forward thrust; the flight attitude control systems are installed on the tail portion and the two sides of the middle of the vehicle body respectively, and the flight attitude control systems installed on the two sides of the middle of the vehicle body are retractable. The hovercar can take off and land flexibly like a rotor wing type hovercar and can also have high speed and long endurance like a fixed wing type hovercar, and the wings and the rotor wings can be contracted and folded to save space.
本发明公开了一种可折叠的复合翼式垂直起降飞行汽车,属于飞行汽车技术领域,本发明的飞行汽车包括车体、垂直运动控制系统、前进动力控制系统、飞行姿态控制系统;所述垂直运动动力系统可伸缩的对称安装于车体两侧,所述前进动力系统安装于车体尾部用于产生向前推力;所述飞行姿态控制系统分别安装于车体的尾部和中部两侧,安装于车体中部两侧的飞行姿态控制系统可收缩。本发明的飞行汽车既可以像旋翼式飞行汽车一样灵活起降,又可以像固定翼式飞行汽车一样拥有高速和长航时,还可以将机翼和旋翼全部收缩折叠以节省空间。
Foldable composite wing type vertical take-off and landing hovercar
一种可折叠的复合翼式垂直起降飞行汽车
2023-07-18
Patent
Elektronische Ressource
Chinesisch