The multi-rotor type unmanned aerial vehicle includes: a main body including the battery module and the control module; a plurality of frames connected to a side surface of the main body and extending therefrom; a first motor connected to a distal end of each of the frames; and a drive unit connected to the first motor, wherein the drive unit includes a rotary frame and a stationary frame each having a circular shape and connected to each other in the form of a gyroscope, a second motor supported at the center of the rotatable frame, and a propeller connected to the second motor, and a vector of thrust generated by rotation of the propeller is variable according to rotation of the first and second motors.


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    Title :

    MULTIROTOR TYPE UNMANNED AERIAL VEHICLE AVAILABLE FOR ADJUSTING DIRECTION OF THRUST


    Contributors:
    AHN HYO SUNG (author) / CHOI YOUNG CHEOL (author) / KANG SUNG MO (author) / SON JI HWAN (author) / LEE BYUNG HUN (author) / KO GWI HAN (author)

    Publication date :

    2016-11-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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