The present invention relates to a drone taxi, comprising: a main body; a left wing frame protruding outwardly on the left side of the main body; a left boom provided at an end of the left wing frame and having a longitudinal length toward the front and back sides; a left wing protruding outwardly on the left boom; a right wing frame protruding outwardly on the right side of the main body; a right boom provided at an end of the right wing frame and having a longitudinal length toward the front and back sides; a right wing protruding outwardly on the right boom; and a plurality of thrust units provided on each of the left boom and the right boom and capable of generating thrust in the forward direction and the vertical direction of the main body.

    본 발명은 본체; 상기 본체의 좌측에 외측으로 돌출된 좌측날개프레임; 상기 좌측날개프레임 끝단에 구비되며, 정면측과 배면측으로 장축 길이를 갖는 좌측붐; 상기 좌측붐 외측으로 돌출된 좌측날개; 상기 본체의 우측에 외측으로 돌출된 우측날개프레임; 상기 우측날개프레임 끝단에 구비되며, 정면측과 배면측으로 장축 길이를 갖는 우측붐; 상기 우측붐 외측으로 돌출된 우측날개; 및 상기 좌측붐과 우측붐 각각에 구비되며, 본체의 전진 방향과 수직 방향으로 각각 추력 발생이 가능하도록 다수 개 구비되는 추력부;를 포함하여 구성되는 것을 기술적 특징으로 한다.


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    Titel :

    ELECTRIC VERTICAL TAKE-OFF AND LANDING DRONE


    Weitere Titelangaben:

    드론 택시


    Beteiligte:
    HEEWOO LEE (Autor:in) / YOU JAE MYEONG (Autor:in)

    Erscheinungsdatum :

    08.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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