본 발명은 수직 비행과 수평 비행이 가능한 천이 비행용 무인 비행체에 관한 것으로서, 구체적으로는 엔진을 이용한 주 추력수단과 탑재수단을 갖는 본체 및 고정익과 각 고정익에 설치되는 보조 추력수단을 갖는 익체로 구성됨에 따라, 중앙의 엔진을 이용한 주 추력장치에 의해 고속으로 장시간 수직, 호버링 또는 수평 천이 비행이 가능하고 외곽의 모터를 이용한 보조 추력장치의 회전비 제어를 통해 수직 또는 수평 천이 비행시 전후좌우의 움직임이 원활하고 안정적으로 이루어지는 천이 비행용 다목적 무인 비행체를 제공하게 된다.

    The present invention relates to an unmanned aerial vehicle for transmission flight and multipurpose capable of performing vertical flight and horizontal flight. In particular, the unmanned aerial vehicle is composed of a main body having a main thrust means and an installation means, and a flying body having a fixed wing and a subsidiary thrust means installed in each fixed wing. By using a main thrust device using a central engine, the unmanned aerial vehicle is able to perform long time vertical, hovering, or horizontal transmission flight at a high speed. By controlling a rotation ratio of a subsidiary thrust device using a motor at the outside, the unmanned aerial vehicle is able to smoothly and stably perform forward, backward, left, and right movements in vertical or horizontal transmission flight.


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    Titel :

    Unmanned Aerial Vehicle for transition flight and multipurpose


    Weitere Titelangaben:

    천이 비행용 다목적 무인 비행체


    Erscheinungsdatum :

    2019-01-30


    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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