본 발명은 외곽체부를 구비한 비행체에 관한 것이다. 본 발명의 실시예에 따르면, 본체부와 그 외측을 둘러싸는 링 형상을 이루는 외곽체부가 연결 프레임부를 통해 결합되고, 본체부의 외측과 외곽체부의 내측이 이루는 링 형상의 사이 공간에 복수의 모터 구동형 공기 유동 수단이 대칭적으로 배치되어, 프로펠러의 노출에 따른 안전 사고의 위험성을 감소시키고 외곽체부를 이용한 다양한 부가 기능을 제공하도록 구성된 외곽체부를 구비한 비행체가 개시된다.

    The present invention relates to an aircraft provided with an outer body part. According to an embodiment of the present invention, a main body part and an outer body part forming a ring shape surrounding the outside of the main body part are coupled through a connection frame part, and a plurality of motor-driven air flow means are symmetrically arranged in a ring-shaped space between the outer side of the main body part and the inner side of the outer body part so that risk of accidents due to propeller exposure can be reduced and various additional functions using the outer body part can be provided.


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    Titel :

    Aircraft with outer body


    Weitere Titelangaben:

    외곽체부를 구비한 비행체


    Erscheinungsdatum :

    30.08.2023


    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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