The present invention relates to an aircraft having a wing-rotor and, more specifically, to an aircraft having a wing-rotor, wherein the angle of attack of the root and the angle of attack of the tip of a rotary wing to which the cross-sectional structure of an aircraft wing is applied are different from each other. The aircraft having a wing-rotor can have the maximum lift coefficient according to the rotation radius by using a wing-rotor that the lift generation principle of an aircraft wing and the rotor rotation of a helicopter are combined, thereby providing greater lift even at lower RPMs than rotary wings of traditional helicopters or gyrocopters, enabling vertical takeoff and landing of the aircraft, suppressing the generation of torque reaction due to rotation by adopting a structure rotating by a propulsion motor attached to the tip of the wing-rotor, and enabling the application to heavyweight and large-sized airframes due to weight lightening.

    본 발명은 윙-로터를 구비한 비행체에 관한 것으로, 보다 상세하게는, 항공기 날개의 단면구조가 적용된 회전 날개의 뿌리 쪽 받음각과 끝 쪽 받음각을 서로 상이하게 구성한 방식으로서, 항공기 날개의 양력발생 원리와 헬리콥터의 로터 회전을 결합한 윙-로터를 이용하여 회전 반경에 따라 최대양력계수를 가질 수 있게 하여 기존 헬리콥터나 자이로콥터의 회전 날개 대비 저 RPM으로 회전하여도 큰 양력을 제공하고 나아가 비행체의 수직 이, 착륙을 가능하게 하며, 윙-로터 끝단에 달린 추진모터에 의해 회전하는 구조를 채택해 회전에 따른 반작용 토크(Torque reaction) 발생을 억제하고, 경량화를 통해 보다 고중량 대형기체에 적용하기에 유리하도록 개발된 윙-로터를 구비한 비행체에 관한 것이다.


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    Titel :

    - Flying object with Wing-Rotor


    Weitere Titelangaben:

    윙-로터를 구비한 비행체


    Beteiligte:
    LEE BONG SEUB (Autor:in) / HONG CHOL GI (Autor:in)

    Erscheinungsdatum :

    2023-06-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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