The invention provides a three-rotor rotorcraft which comprises a rotorcraft body, the rotorcraft body comprises a middle section, a head and a tail, the head and the tail are connected with the middle section, the left side and the right side of the middle section are rotationally connected with first rotors, and the tail is rotationally connected with a second rotor. The two first rotor wings are arranged in an axial symmetry mode, and the second rotor wing can rotate leftwards or rightwards by 180 degrees relative to the tail. The three-rotor rotorcraft does not need a runway, can ascend and descend on a slope, and is high in propulsive force, large in portable weight and good in stability.

    本发明提供一种三旋旋翼机,包括:机体,机体包括中间段以及连接中间段的头部和尾部,中间段的左、右两侧均旋转连接有第一旋翼,尾部旋转连接有第二旋翼。两个第一旋翼呈轴对称设置,且第二旋翼可以相对所述尾部向左或向右进行180°的旋转。本发明的三旋旋翼机无需跑道,可于斜面升降,推进力强,可携带重量大,且稳定性好。


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    Title :

    Three-rotor aircraft


    Additional title:

    一种三旋翼机


    Contributors:
    WU YOULI (author)

    Publication date :

    2023-04-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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