The present invention is to provide an aircraft with maximized mobility that can be operated with little power, improves flight stability, and is small in size so that it can fly without restrictions even in complex terrain. To this end, the present invention relates to an aircraft having a wing-shaped fuselage, which comprises: a first fuselage portion whose longitudinal cross-section is shaped like an airfoil and whose upper surface is formed with a concave curved surface along the longitudinal central axis; and a second fuselage portion disposed above the first fuselage portion and having an airfoil-shaped longitudinal section. The first fuselage portion and the second fuselage portion are spaced apart from each other. Accordingly a wing-shaped flying vehicle can be provided.

    본 발명은 날개형상의 동체를 가진 비행체에 관한 것으로, 종단면이 에어포일(airfoil) 형상이며, 상면에는 길이 방향의 중심축을 따라 오목한 만곡면이 형성되는 제1 동체부; 및 상기 제1 동체부의 상부에 배치되고, 종단면이 에어포일 형상인 제2 동체부를 포함하고, 상기 제1 동체부와 상기 제2 동체부는 사이가 이격된 날개형상 비행체를 제공할 수 있다.


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    Titel :

    Multi-Layer Structure Airfoil-Shaped Aircraft


    Weitere Titelangaben:

    날개형상 단면을 갖는 다층구조 비행체


    Beteiligte:
    CHO HYUNG HEE (Autor:in) / NAM JU YEONG (Autor:in) / CHOI SEUNG YEONG (Autor:in) / BAE HYUNG MO (Autor:in) / CHANG IN JOONG (Autor:in) / KIM TAE HYUN (Autor:in) / YUN MA ROO SOL (Autor:in) / LEE YONG HWI (Autor:in)

    Erscheinungsdatum :

    12.10.2023


    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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