The fixed-wing vertical take-off and landing aircraft comprises a fuselage, wings and cabin doors, the wings are arranged on the two sides of the fuselage respectively, the fixed-wing vertical take-off and landing aircraft further comprises four sets of rotor wing modules and a mounting frame, and each rotor wing module comprises a power column and a propeller; the mounting frame is fixed at the tail part of the fuselage and comprises four empennages, and a group of rotor modules are arranged on each empennage; the two empennages extend towards the upper side of the fuselage, and the empennages are opened upwards and arranged in a V shape; the other two rotor wing modules extend towards the lower side of the fuselage, and the empennage opens downwards and is arranged in a V shape; the upwards-opened empennages and the downwards-opened empennages are symmetrically distributed on the upper side and the lower side of the fuselage. The four rotor wing modules form a fuselage layout which is symmetrical along the upper side and the lower side of the fuselage, a runway is not needed, the flight attitude conversion is realized through adjustment of a control system after the aerial state until the level flight state is achieved, and the unmanned aerial vehicle is simple in structure, high in reliability and good in safety.
一种固定翼垂直起降飞行器,包括机身、机翼和舱门,机身的两侧分别设置有一个机翼,还包括四组旋翼模组和安装架,各个所述的旋翼模组均包括动力柱和螺旋桨;安装架固定在机身的尾部,包括四件尾翼,每件尾翼上设置一组旋翼模组;两件尾翼朝向机身上侧延伸,尾翼向上张开呈V型设置;另两件旋翼模组朝向机身下侧延伸,尾翼向下张开呈V型设置;向上张开的尾翼和向下张开的尾翼呈形成机身上侧和下侧对称分布。本发明通过四个旋翼模组形成沿机身上侧和下侧对称的机身布局,无需跑道,凌空后控制系统调整来实现飞行姿态的转换,直至达到平飞状态,其结构简单,可靠性高,安全性好。
Fixed-wing vertical take-off and landing aircraft
固定翼垂直起降飞行器
2022-07-22
Patent
Electronic Resource
Chinese