A multi-rotor unmanned aerial vehicle comprises: a vehicle main body which has a flying control part for controlling the flying of the multi-rotor unmanned aerial vehicle; first rotor parts which are connected to the vehicle main body according to the flying direction of the vehicle main body; and second rotor parts which are connected to the vehicle main body to be arranged between the first rotor parts, wherein the distance from the center of the vehicle main body to the rotation center of the first rotor parts is longer than the distance from the center of the vehicle main body to the rotation center of the second rotor parts, thereby increasing the flight duration thereof and improving the response ability to disturbance.

    본 발명에 따른 다중회전익 무인비행체는, 다중회전익 무인비행체의 비행을 제어하는 비행제어부를 구비하는 비행본체; 상기 비행본체의 비행방향을 따라 상기 비행본체에 연결된 제1로터부; 및 상기 제1로터부의 사이에 배치되도록 상기 비행본체에 연결된 제2로터부;를 포함하며, 상기 비행본체의 중심에서부터 상기 제1로터부의 회전중심까지의 거리는 상기 비행본체의 중심에서부터 상기 제2로터부의 회전중심까지의 거리 보다 길게 형성됨으로써, 체공시간을 늘이고 외란 대응력을 높일 수 있다.


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    Titel :

    MULTI ROTOR UNMANNED AERIAL VEHICLE


    Weitere Titelangaben:

    다중회전익 무인비행체


    Beteiligte:

    Erscheinungsdatum :

    31.08.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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