The present invention relates to a joined-wing type unmanned aerial vehicle and, more specifically, to a joined-wing type unmanned aerial vehicle including: a fuselage; main wings formed in both sides of the fuselage and formed into triangular forms toward a rear part of the aerial vehicle; an upper wing with both ends connected to the main wings by connecting boards, arranged in the upper side of the main wings, and forming a joined wing form with the main wings; a propeller formed in the upper wing and generating propulsion; a vertical wing coupled to central parts of top surfaces of the main winds and a central part of the underside of the upper wing; and a rudder formed in a rear part of the vertical wing to be able to rotate and adjusting a direction. According to the present invention, the joined-wing type unmanned aerial vehicle is capable of easily landing in a narrow space, as a lifting force is increased by the forms of the main winds and the upper wind. In addition, an effect of improving flight efficiency and taking-off and landing performance is obtained.

    본 발명은 조인드윙형 무인항공기에 관한 것이다. 더욱 상세하게는, 동체; 상기 동체의 양측에 형성되며, 양 끝단이 상기 동체의 선미 방향을 향하는 삼각형 형태로 이루어지는 메인윙; 양 끝단은 상기 메인윙과 연결대로 연결되며 상기 메인윙의 상부에 배치되어 상기 메인윙과 함께 조인드윙 형태를 이루는 상부윙; 상기 상부윙에 구비되며 추진력을 발생시키는 프로펠러; 상기 메인윙의 상면 중앙부 및 상기 상부윙의 하면 중앙부와 결합되는 수직날개; 및 상기 수직날개의 후미에 회동 가능하게 구비되어 방향을 조절하는 방향타를 포함하는 것을 특징으로 한다. 본 발명에 의하면, 메인윙 및 상부윙의 형상에 의해 양력이 향상되어 좁은 공간에서도 용이하게 착륙할 수 있고, 비행 효율 및 이착륙 성능을 향상시킬 수 있는 효과가 있다.


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    Title :

    JOINED WING TYPE UNMANNED AIRCRAFT


    Additional title:

    조인드윙형 무인항공기


    Contributors:
    LEE HEE WOO (author)

    Publication date :

    2016-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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