The present invention relates to a discoid drone, and according to the present invention, the discoid drone comprises: a top body having a plurality of first through portions; a bottom body disposed on a lower portion of the top body, having a plurality of second through portions formed on positions corresponding to the first through portions, and coupled to the top body to form a space therein; a damper portion formed to surround an outer circumferential surface of the top and bottom bodies and absorbing vibration of the same; an air tunnel portion disposed between the first through portion and the second through portion; a propeller portion disposed inside the air tunnel portion; a power supply portion fixed to the top body and providing power to the propeller portion; and a control portion fixed to the bottom body and controlling the propeller portion. The present invention intends to provide a discoid drone which minimizes occurrence of gas impacts and safety accidents at the time of collision and has improved flight efficiency by applying an air tunnel structure.

    본 발명은 원반형 무인항공기에 관한 것으로, 본 발명에 따르면, 복수의 제1 관통부가 형성된 상단 바디, 상단 바디의 하부에 배치되며 제1 관통부와 대응되는 위치에 복수의 제2 관통부가 형성되며, 상단 바디와 결합되어 내부에 공간을 형성하도록 하는 하단 바디, 상단 및 하단 바디의 외주면을 감싸도록 형성되며, 상단 및 하단 바디의 진동을 흡수하는 댐퍼부, 제1 관통부와 제2 관통부 사이에 배치되는 에어터널부, 에어터널부 내측에 배치되는 프로펠러부, 상단 바디에 고정되며, 플로펠러부에 동력을 제공하는 전원부 및 하단 바디에 고정되며, 프로펠러부를 제어하는 제어부를 포함하는 원반형 무인항공기에 관한 것이다.


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    Titel :

    DISK SHAPED DRONE


    Weitere Titelangaben:

    원반형 무인항공기


    Beteiligte:
    HA TAE HOON (Autor:in)

    Erscheinungsdatum :

    29.05.2017


    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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