The invention belongs to the field of aviation flight, and particularly relates to a tilt wing vertical take-off and landing aircraft and a control method thereof. According to the invention, vertical take-off and landing and cruising functions of the aircraft are realized by tilting part of the main wings with a structure as simple, efficient and safe as possible. The unmanned aerial vehicle comprises a fuselage, empennages and an undercarriage, the fuselage is fixedly connected with the empennages, the undercarriage is fixedly connected with the fuselage, the empennages comprise a vertical empennage and a horizontal empennage, the unmanned aerial vehicle further comprises tilting wings, the tilting wings are rotatably connected with the fuselage, and the unmanned aerial vehicle is mainly characterized in that double engines are arranged on main wings on the two sides. And the power system has no variable pitch. Control moments of pitching, rolling and directions are obtained through a control surface of a rear flow field of the engine.

    本发明属于航空飞行领域,特别涉及一种倾转翼垂直起降飞行器及其控制方法。本发明实现飞行器通过倾转部分主翼,以尽可能简单、高效、安全的结构,实现垂直起降和巡航功能。本发明包括机身、尾翼和起落架,所述机身和尾翼固定连接,所述起落架固定连接机身,所述尾翼包括垂直尾翼和水平尾翼,还包括倾转翼,所述倾转机翼与机身可转动连接,其主要特点是双发动机,置于两侧主翼。动力系统无变距。通过发动机后流场舵面,获得俯仰、滚转及方向的控制力矩。


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    Title :

    Tilting-rotor vertical take-off and landing aircraft and control method thereof


    Additional title:

    一种倾转翼垂直起降飞行器及其控制方法


    Contributors:
    YIN JIANMING (author) / SHEN TAO (author) / YIN ZHENJIE (author)

    Publication date :

    2023-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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