One embodiment of the present invention may provide a pneumatically propelled drone, comprising: a mainframe in which a control unit, a power unit, and a communication unit for operating a drone are arranged; at least two arms that are foldably connected to a lower part of the main frame and each has a rotor formed at its end; and a cover unit that is formed on an upper part of the main frame and can obtain propulsion through air pressure applied from the lower part of the main frame, thereby capable of increasing convenience in moving and storing the drone and reducing take-off time.

    본 발명의 일실시 형태는, 드론의 작동을 위한 제어부, 전원부, 및 통신부가 배치되는 메인프레임과, 상기 메인프레임의 하부방향으로 접이가능하도록 연결되며, 각각 단부에 로터가 형성되는 적어도 2개의 암(Arm), 및 상기 메인프레임의 상부에 형성되며, 메인프레임 하부로부터 가해지는 공기압을 통해 추진력을 얻을 수 있는 덮개부을 포함하는 공압 추진 드론을 제공할 수 있다.


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    Titel :

    AIR PROPELLED DRONE


    Weitere Titelangaben:

    공압 추진 드론


    Beteiligte:
    KIM YEON SU (Autor:in) / RYU TAE HYEON (Autor:in) / LEE SEUNG MIN (Autor:in) / JANG YOUNG SUK (Autor:in) / KIM HYEONG JUNG (Autor:in)

    Erscheinungsdatum :

    18.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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