According to one embodiment of the present invention, a variable unmanned aerial vehicle includes: an airframe including a driving member; a plurality of first support rods extended to an outer side of the airframe; a plurality of second support rods extended to the outer side of the airframe and provided on the airframe to be swingable; and a plurality of driving parts coupled to each end of the plurality of first support rods and each end of the plurality of second rods to generate rotating force, wherein the plurality of second support rods are arranged in a predetermined direction in accordance with a flight mode. Therefore, the variable unmanned aerial vehicle can have improved power efficiency.

    본 일 실시 예에 따른 가변형 무인 비행체는, 구동부재를 포함하는 기체(airframe); 기체의 외측으로 연장되는 복수의 제1 지지로드; 기체의 외측으로 연장되며 기체에 스윙 가능하게 구비되는 복수의 제2 지지로드; 및 복수의 제1 지지로드 각각의 단부와 복수의 제2 지지로드 각각의 단부에 결합되어 회전력을 발생시키는 복수의 구동부를 포함하되, 복수의 제2 지지로드는 비행 모드에 따라 미리 설정된 방향으로 배치된다.


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    Titel :

    TRANSFORMABLE DRONE AND OPERATION METHOD THEREFOR


    Weitere Titelangaben:

    가변형 무인비행체 및 이를 위한 동작 방법


    Beteiligte:
    MOON MYOUNG GI (Autor:in)

    Erscheinungsdatum :

    2020-12-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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