The invention discloses a novel vertical take-off and landing fixed-wing aircraft. The aircraft comprises a fuselage; the left main wing and the right main wing are symmetrically arranged in the middle of the fuselage; the empennage is arranged on the tail part of the fuselage; the left lift force driving mechanism and the right lift force driving mechanism are mounted on the left main wing and the right main wing, are connected with an aircraft control system and are used for providing lift force and thrust force for the aircraft; the aircraft further comprises a telescopic balance lift force adjusting mechanism which is installed on the tail portion of the aircraft body and connected with an aircraft control system, and when the aircraft enters a take-off and landing mode, the telescopic balance lift force adjusting mechanism extends outwards from the tail end of the aircraft body. The telescopic balance lift force adjusting mechanism is used for providing lift force for the aircraft in the take-off and landing process and adjusting the balance stability of the aircraft in the take-off and landing process, and when the aircraft enters the level flight mode, the telescopic balance lift force adjusting mechanism retracts into the tail of the aircraft body. The influence on the aerodynamic configuration of the airplane is avoided, the aerodynamic configuration of the airplane is simplified, meanwhile, the resistance of the airplane is reduced, and the attractiveness is better.
本发明公开的一种新型垂直起降固定翼飞机,包括:机身;对称设置在所述机身的中部的左、右主机翼;设置在所述机身的尾部上的尾翼;以及安装在所述左、右主机翼上且与飞机控制系统连接的用于为飞机提供升力和推力的左、右升力驱动机构;还包括安装在所述机身的尾部上且与飞机控制系统连接的可伸缩式平衡升力调节机构,当飞机进入起降模式时,所述可伸缩式平衡升力调节机构从所述机身的尾端内向外伸出,用于为飞机在起降过程中提供升力和调整飞机在起降过程中的平衡稳定性,当飞机进入平飞模式时,所述可伸缩式平衡升力调节机构回缩至所述机身的尾部内。本发明避免对飞机气动外形的影响,有利于飞机精简气动外形,同时也减少飞机阻力,美观性更佳。
Novel vertical take-off and landing fixed-wing aircraft
一种新型垂直起降固定翼飞机
2022-03-18
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |