The invention discloses a composite wing system and a hovercar. The technical problem that in the prior art, a folding mechanism of a hovercar is complex is solved. The composite wing system is used for the aircraft and comprises a wing assembly and a rotor assembly, the wing assembly comprises a wing folding mechanism and two wings, each wing comprises a wing surface and a four-bar mechanism, and the wing folding mechanism is in force transmission connection with the four-bar mechanism; the rotor wing assembly comprises a machine arm and a paddle assembly, the machine arm is rotationally installed on one connecting rod of the four-connecting-rod mechanism, and the machine arm and the connecting rod are arranged at an angle; wherein the two sets of wings are driven by the wing folding mechanism to rotate to be parallel to or perpendicular to the aircraft, and one connecting rod of the four-connecting-rod mechanism is driven by the wing folding mechanism to be parallel to or perpendicular to the wings. The two sets of wings can be driven to rotate to be parallel to or perpendicular to the aircraft through the wing folding mechanism, and the wings and the arms can be folded through one set of wing folding mechanism, so that the mass of the aircraft is reduced.
本申请公开了一种复合翼系统及飞行汽车,解决现有技术中飞行汽车折叠机构复杂的技术问题。复合翼系统用于飞行器,包括机翼组件和旋翼组件,机翼组件包括机翼折叠机构和两个机翼,机翼包括机翼面和四连杆机构,机翼折叠机构与四连杆机构传力连接;旋翼组件包括机臂和桨叶组件,机臂转动安装于四连杆机构的其中一根连杆上,且与连杆呈角度设置;其中,两组机翼在机翼折叠机构的驱动下转动至与飞行器平行或垂直,且四连杆机构的其中一根连杆在机翼折叠机构的驱动下至与机翼平行或垂直。通过机翼折叠机构可以驱动两组机翼转动至与与飞行器平行或垂直,通过一组机翼折叠结构,可以实现机翼和机臂的折叠,从而减少了飞行器的质量。
Composite wing system and hovercar
一种复合翼系统及飞行汽车
2023-11-03
Patent
Electronic Resource
Chinese
Foldable composite wing type vertical take-off and landing hovercar
European Patent Office | 2023
|