The invention discloses a multi-layer multi-rotor aircraft. The multi-layer multi-rotor aircraft comprises a plurality of layers of rotor components which are arranged at different heights of a central axis of the multi-layer multi-rotor aircraft, wherein the rotor component in each layer comprises two rotors; the two rotors are separated by an angle of 180 DEG in a circumferential direction of the central axis; and in each rotor of the multi-layer multi-rotor aircraft, the rotation directions of the two adjacent rotors in the circumferential direction of the central axis are reverse to each other. Due to the adoption of a big rotor blade, the multi-layer multi-rotor aircraft disclosed by the invention has the advantages of small structure and compact layout and is also advantaged in that the power area of the rotors is increased and the power and load of the aircraft are also increased.


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    Titel :

    Multi-layer multi-rotor aircraft


    Beteiligte:
    LIU ZHIYUAN (Autor:in)

    Erscheinungsdatum :

    2016-01-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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