The present invention relates to a drone having a vortex prevention function. According to the present invention, provided is the drone comprising: a base unit; and a rotor unit having a propeller spaced apart as a shaft on the outside of the base unit. An upper cover and a lower cover are respectively coupled to each shaft to surround the shaft, wherein the upper cover is formed with a pointed portion having a sharp cross-sectional shape at the upper end thereof, and the lower cover is formed with a pointed portion having a sharp cross-sectional shape at the lower end thereof, so as to induce the flow of air discharged to the lower side of the rotor unit by the propeller to prevent the occurrence of vortex.

    본 발명은 와류 방지 기능을 갖는 드론에 관한 것으로, 기체부와, 기체부의 외측에 샤프트로서 이격되게 구비되는 프로펠러를 갖는 로터부를 포함하는 드론으로서, 각 샤프트에는 상부커버와 하부커버가 각각 결합되어 샤프트를 감싸도록 구비되되, 상부커버는 그 상단부에 뾰족한 단면 형상을 갖는 첨예부가 형성되고, 하부커버는 그 하단부에 뾰족한 단면 형상을 갖는 첨예부가 형성되어, 프로펠러에 의해 로터부 하방으로 배출되는 공기의 흐름을 유도하여 와류의 발생을 방지하도록 한 드론을 제공한다.


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    Titel :

    Drone having vortex prevention function


    Weitere Titelangaben:

    와류 방지 기능을 갖는 드론


    Beteiligte:
    KIM JI YEON (Autor:in) / PARK HWARK GGYU (Autor:in) / SEO DONG HOON (Autor:in) / KIM MYUNG BUM (Autor:in) / HAN KI NAM (Autor:in)

    Erscheinungsdatum :

    2021-04-06


    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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