Provided is a vibration control system for a compound helicopter with a rotor and a fixed wing. The fixed wing includes a movable flap that is mounted on a rear edge of the fixed wing. The vibration control system periodically moves the movable flap so as to periodically change lift of the fixed wing such that vibration aerodynamically generated by the fixed wing is in anti-phase with vibration caused by rotation of the rotor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vibration control system for compound helicopter


    Beteiligte:
    KOBAYASHI WATARU (Autor:in) / HAYASHI HIROTAKA (Autor:in) / NAKAMURA MIZUKI (Autor:in) / SASAKI MASAFUMI (Autor:in) / TANABE YASUTADA (Autor:in) / KOBIKI NOBORU (Autor:in) / SUGAWARA HIDEAKI (Autor:in)

    Erscheinungsdatum :

    28.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    VIBRATION CONTROL SYSTEM FOR COMPOUND HELICOPTER

    KOBAYASHI WATARU / HAYASHI HIROTAKA / NAKAMURA MIZUKI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    VIBRATION CONTROL SYSTEM FOR COMPOUND HELICOPTER

    KOBAYASHI WATARU / HAYASHI HIROTAKA / NAKAMURA MIZUKI et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    VIBRATION INHIBITION SYSTEM IN COMPOUND HELICOPTER

    KOBAYASHI KO / HAYASHI HIROTAKA / NAKAMURA MIZUKI et al. | Europäisches Patentamt | 2021

    Freier Zugriff


    COMPOUND HELICOPTER

    KIMURA KEITA / TANABE YASUTADA / SUGAWARA HIDEAKI | Europäisches Patentamt | 2024

    Freier Zugriff