The present invention relates to a vertical take-off and landing aircraft. The vertical take-off and landing aircraft comprises: a flying body (F), on which a main wing (3) and auxiliary wings (W1, W2) are mounted; a pair of front propulsive bodies (7) mounted on both sides of the flying body (F) to be varied horizontally and vertically; a rear propulsive body (9) mounted at the auxiliary wings (W1, W2) positioned on a rear side of the flying body (F) to be varied horizontally and vertically; a front variable part (11) and a rear variable part (13), which are mounted at the flying body (F) and the auxiliary wings (W1, W2) to vertically or horizontally vary the front propulsive bodies (7) and the rear propulsive body (9); a control part (50) for controlling the front variable part (11) and the rear variable part (13); and a propulsive force correction part (60) correcting a difference between propulsive forces in a case that there is the difference between the propulsive forces when detecting the propulsive forces of the front propulsive bodies (7) and the rear propulsive body (9), thereby allowing the aircraft to stably take off.

    본 발명은 수직 이착륙기에 관한 것이다. 그러한 수직 이착륙기는 주날개(3) 및 보조날개(W1,W2)가 장착된 비행동체(F)와; 비행동체(F)의 양측에 각각 장착되어 수평 및 수직방향으로 가변가능한 한 쌍의 전방 추진체(7)와; 비행동체(F)의 후방에 구비된 보조날개(W1,W2)에 장착되어 수평 및 수직방향으로 가변 가능한 후방 추진체(9)와; 비행동체(F) 및 보조날개(W1,W2)에 장착되어 전방 추진체(7) 및 후방 추진체(9)를 수직 혹은 수평방향으로 가변시키는 전후방 가변부(11,13)와;를 포함한다.


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    Titel :

    Vertical takeoff and landing airplane


    Weitere Titelangaben:

    수직 이착륙기


    Beteiligte:
    HONG SEUNG IL (Autor:in)

    Erscheinungsdatum :

    29.11.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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