According to one embodiment of the present invention, provided is a vane system for a flight vehicle. The present invention comprises: a duct unit disposed in a flight vehicle; a propeller unit disposed in the duct unit; and a wind control unit disposed in an aperture of an upper portion and a lower portion of the duct unit. The wind control unit can have a plurality of vane structures, which are disposed to be rotated to change the direction of air flowing into the duct unit.

    본 발명의 실시 예에 따른 비행체용 베인 시스템은 비행체에 구비되는 덕트부, 상기 덕트부에 구비되는 프로펠러부 및, 상기 덕트부의 상부와 하부의 개구에 구비되는 풍향조절부를 포함하고, 상기 풍향조절부는, 상기 덕트부로 유입되는 공기의 진행 방향을 변경시키도록 회전 가능하게 배치된 복수의 베인구조체를 포함할 수 있다.


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    Titel :

    Vane system for aircraft


    Weitere Titelangaben:

    비행체용 베인 시스템


    Beteiligte:
    LEE SEOUNG HAN (Autor:in) / HUH SEOK HAENG (Autor:in) / KIM HYO TAE (Autor:in) / SEOL JIN WOON (Autor:in)

    Erscheinungsdatum :

    05.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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