The present invention relates to a tilt-prop aircraft. According to the present invention, provided is the tilt-prop aircraft for determining vertical takeoff/landing or forward flight by adjusting a tilt angle of a rotor connected to a blade, comprising: the blade included in the rotor and rotating to generate lift force and thrust force; and a tilt spindle connecting the rotor and the vane and adjusting the tilt angle of the rotor relative to a plane of flight of the tilt prop aircraft. When the tilt angle of the rotor is adjusted, a pitch angle of the blade changes through a power transmitting means mechanically interlocked with the tilt spindle.

    본 발명에 따르면, 날개에 연결된 로터의 틸트각을 조절하여 수직이착륙 또는 전진비행 여부를 결정하는 틸트프롭 항공기(tilt-prop aircraft)에 있어서, 틸트프롭 항공기는, 로터에 포함되고 회전하여 양력 및 추력을 발생시키는 블레이드; 및 상기 로터와 상기 날개를 연결하고 상기 틸트프롭 항공기의 비행 평면에 대한 상기 로터의 틸트각을 조절하는 틸트 중심축;을 포함하고, 상기 로터의 틸트각 조절시, 상기 틸트 중심축과 기계적으로 연동된 동력전달수단을 통해 상기 블레이드의 피치각이 변화하는 틸트프롭 항공기가 제공된다.


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    Titel :

    Tilt-prop aircraft


    Weitere Titelangaben:

    틸트프롭 항공기


    Beteiligte:
    LEE MYEONG KYU (Autor:in) / CHOI SEONG WOOK (Autor:in) / KIM DEOG KWAN (Autor:in)

    Erscheinungsdatum :

    16.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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