According to embodiments of the present invention, provided is a tilt-prop aircraft, which includes: a main body part; a wing part coupled to the main body part and having an installation hole part; a pair of tilt parts which are rotationally coupled to both side end portions of the wing part and in which a first propeller is installed; a second propeller spaced apart from the tilt parts to be arranged in the installation hole part; and a cover part installed on the wing part and opening and closing the installation hole part. Therefore, the tilt-prop aircraft can decrease drag when flying in a cruising mode.

    본 발명의 실시예들에 따르면, 본체부; 상기 본체부에 결합되고, 설치홀부가 형성되는 날개부; 상기 날개부의 양 측단부에 회전가능하게 결합되고, 제1프로펠러가 설치되는 한 쌍의 틸트부; 상기 틸트부와 이격 배치되어 상기 설치홀부의 내측에 배치되는 제2프로펠러; 상기 날개부에 설치되며, 상기 설치홀부를 개폐하는 커버부;를 포함하는, 틸트프롭 항공기를 제공한다.


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    Titel :

    Tilt-prop aircraft


    Weitere Titelangaben:

    틸트프롭 항공기


    Beteiligte:
    LEE YUNG GYO (Autor:in) / CHOI SEONG WOOK (Autor:in) / HWANG CHANG JEON (Autor:in)

    Erscheinungsdatum :

    15.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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