The invention provides a multi-rotor type aircraft. The multi-rotor type aircraft comprises a main rotor and a plurality of secondary rotors, wherein the main rotor is driven by a fuel engine, and is arranged at the lower end or the upper end of the center position of the engine body of the fuel engine; the plurality of secondary rotors are distributed on the periphery of the engine body; the secondary rotors are driven by motors respectively. The multi-rotor aircraft has the advantages of high carrying capacity and long voyage time.


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    Title :

    Multi-rotor type aircraft


    Contributors:
    NI HUI (author)

    Publication date :

    2015-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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