An unmanned aerial vehicle comprising a center hub; a plurality of wings securable to the center hub; and one or more propeller systems located on each wing of the plurality of wings. The unmanned aerial vehicle further including one or more actuator systems, wherein each of the one or more propeller systems is independently associated with one actuator system of the one or more actuator systems. Wherein the unmanned aerial vehicle system is operatively configured to be operated in a variety of flight modes.


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    Title :

    VORTEX DRONE


    Contributors:

    Publication date :

    2024-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U



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