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。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Three-rotor aircraft


    Weitere Titelangaben:

    一种三旋翼机


    Beteiligte:
    WU YOULI (Autor:in)

    Erscheinungsdatum :

    21.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Single-engine three-rotor aircraft

    WANG ZHICHENG / MA WEI | Europäisches Patentamt | 2021

    Freier Zugriff

    Three-rotor aircraft and control method thereof

    LI ZEBO / LI XIANBANG / LI BOWEN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    ROTOR AIRCRAFT

    SUGAKI KIYOKAZU | Europäisches Patentamt | 2020

    Freier Zugriff

    Rotor aircraft

    YOSHIMURA KENSUKE / TAJIRI KEISUKE / FUKUROSE TAKESHI | Europäisches Patentamt | 2024

    Freier Zugriff

    Three-rotor vertical take-off and landing aircraft

    WANG SENLIN | Europäisches Patentamt | 2024

    Freier Zugriff