According to one embodiment, an aerial vehicle having a wing of which a gradient is controlled comprises: a body; a thrust unit connected to the body and having a propeller and a rotational shaft; and the wing disposed on both sides of the body and spaced from the thrust unit. The wing pitching-rotated based on a horizontal shaft of the body, and an angle between the rotational shaft and the wing of the thrust unit can be varied by pitching rotation of the wing.

    일 실시예에 따른 기울기가 조절되는 날개를 가지는 비행체는 몸체, 상기 몸체와 연결되고 프로펠러 및 회전 축을 가지는 추력부, 및 상기 몸체의 양 측에 각각 배치되고 상기 추력부와 이격되게 배치되는 날개를 포함할 수 있다. 상기 날개의 받음각이 조절되도록, 상기 날개는 상기 몸체의 좌우 방향 축을 기준으로 피칭 회전되며, 상기 날개의 피칭 회전에 의해 상기 추력부의 상기 회전 축 및 상기 날개 사이의 각도가 가변 될 수 있다.


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    Titel :

    AERIAL VEHICLE HAVING AIRFOIL TO CONTROL SLOPE


    Weitere Titelangaben:

    기울기 제어 날개를 가지는 비행체


    Beteiligte:
    PARK YOUNG MIN (Autor:in)

    Erscheinungsdatum :

    2017-11-06


    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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