The invention discloses a multi-rotor manned vehicle, comprising man-carried cabin, lifting rotor, equipment bin and steering rudder; the upper part of the said man-carried cabin is provided with a window, the bottom edge is provided with a landing gear or taxiing wheels, the outer wall is provided with a cabin door, the outer wall of both sides or the top is provided with a side-push rotor separately, and the back end of the said side-push rotor is provided with a first power device to drive the said side-push rotor; the said lifting rotors are provided of a quantity of at least two, which are arranged side-by-side in parallel around or on both sides of the said man-carried cabin, and the lower end of each said lifting rotor is respectively provided with a second power device to drive the said lifting rotor; the said equipment bin is arranged at the bottom of the said man-carried cabin, in which a power source is provided for the operation of the said first power device and the second power device; the said steering rudder is arranged at the rear or top of the said man-carried cabin. The flight, take-off and landing of the invention is similar to the unmanned aerial vehicle, having the advantages of small and flexible, low altitude and low speed, vertical lifting, economic and practical.


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    Titel :

    Multi-rotor manned aircraft


    Beteiligte:
    YE SHUWU (Autor:in)

    Erscheinungsdatum :

    21.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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