Provided are a flap drive device and a rotorcraft blade, and more particularly, a flap drive device using a two-section link mechanism, which may be applied to a rotorcraft blade, and a rotorcraft blade including the same.


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    Titel :

    Flap drive device and blades of rotary-wing aircraft


    Beteiligte:
    SHIN SANG JOON (Autor:in) / EUN WON JONG (Autor:in) / IM BYEONG UK (Autor:in) / LEE CHANG BAE (Autor:in) / SHIN JIN WOOK (Autor:in)

    Erscheinungsdatum :

    06.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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