The present invention relates to an unmanned aerial vehicle system having a multi-rotor type rotary wing. The unmanned aerial vehicle system having a multi-rotor type rotary wing includes a first unmanned aerial vehicle, at least one second unmanned aerial vehicle, and a bridge that connects the first unmanned aerial vehicle and the at least one second unmanned aerial vehicle to be separable from each other, wherein the at least one second unmanned aerial vehicle is moveable by the first unmanned aerial vehicle in a state where the at least one second unmanned aerial vehicle is coupled to the first unmanned aerial vehicle by the bridge without being driven, and the at least one second unmanned aerial vehicle is separable from the first unmanned aerial vehicle which is in flight.


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    Titel :

    UNMANNED AERIAL VEHICLE SYSTEM HAVING MULTI-ROTOR TYPE ROTARY WING


    Beteiligte:
    LEE TAIKJIN (Autor:in) / NAM SUK WOO (Autor:in) / YOON CHANG WON (Autor:in) / PARK HYUN SEO (Autor:in) / JHON YOUNG MIN (Autor:in) / LEE SEOK (Autor:in) / CHOI MIN-JUN (Autor:in)

    Erscheinungsdatum :

    2017-12-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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