According to the present invention, a vertical take-off and landing unmanned aerial vehicle includes: a fuselage unit; a wing unit provided on both sides of the fuselage unit; a rotor unit provided on the wing unit; an opening and closing unit opening and closing an upper portion and a lower portion of the rotor unit; a tilt rotor unit provided on the back of the fuselage unit and rotationally provided thereon; and a control unit provided on the fuselage unit and controlling take-off, landing and flight based on a control signal received in a wireless manner. According to the present invention, the vertical take-off and landing unmanned aerial vehicle is capable of vertical take-off and landing, is possible to minimize air resistance during horizontal glide, and is possible to rapidly reduce speed when an emergency situation is generated during the horizontal glide.

    본 발명에 따른 수직이착륙 무인항공기는 동체부, 상기 동체부의 양측에 마련된 날개부, 날개부에 구비되는 로터부, 로터부의 상부 및 하부를 개폐시키는 개폐부, 동체부의 후미에 배치되고 회전 가능하게 구비되는 틸트 로터부 및 동체부에 배치되어, 무선으로 수신되는 제어 신호에 기초하여 이착륙 및 비행을 제어하는 제어부를 포함한다. 본 발명에 따른 수직이착륙 무인항공기에 의하면 수직 이착륙이 가능하고, 수평 활공 중에는 공기 저항을 최소화할 수 있으며, 수평 활공 중 긴급 상황이 생긴 경우 속도를 급속히 저감시킬 수 있게 된다.


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    Title :

    VERTICAL TAKEOFF AND LANDING UNMANNED AERIAL VEHICLE


    Additional title:

    수직이착륙 무인항공기


    Contributors:
    CHONG WOO SUK (author) / KIM JE NAM (author) / KIM JAE JUN (author) / JO JONG HYUN (author) / LEE JUN HO (author)

    Publication date :

    2019-12-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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