A multicopter 1 comprises: a support 10; rotors 20 supported by the support 10; an internal combustion engine 32 supported by the support 10; a generator 47 supported by the support 10 and driven by the internal combustion engine 32 to generate power; electric motors 48 supported by the support 10, supplied with electric power from the generators 47, and configured to drive the rotors 20; and a controller configured to control a flight of an aircraft by individually adjusting a rotational speed of each of the rotors 20. The multicopter 1 also comprises at least one of a plurality of the internal combustion engines 32 or a plurality of the generators 47.


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    Title :

    MULTICOPTER


    Additional title:

    MULTIKOPTER
    MULTICOPTÈRE


    Contributors:

    Publication date :

    2024-01-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / F01P Kühlung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , COOLING OF MACHINES OR ENGINES IN GENERAL / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen



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