A rotor for a rotorcraft, the rotor having a plurality of lift assemblies, together with a flapping abutment mechanism for each lift assembly. Each abutment mechanism has a projection secured to a lift assembly with an abutment end provided with an inner face and an outer face, and at least one pivotally-mounted lever extending longitudinally from a flyweight to a hook. The hook is provided with two walls in elevation and a bottom wall forming a periphery that defines the groove, a first wall in elevation having an upper bearing zone for blocking the inner face and a second wall in elevation including a lower bearing zone for blocking the outer face.


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    Titel :

    ROTOR POUR GIRAVION COMPORTANT UN MECANISME DE BUTEE EN BATTEMENT, ET GIRAVION


    Beteiligte:
    MASSAL FABIEN (Autor:in) / EBERHARD ALAIN (Autor:in)

    Erscheinungsdatum :

    29.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotor pour giravion comportant un mécanisme de butée en battement, et giravion

    MASSAL FABIEN / EBERHARD ALAIN | Europäisches Patentamt | 2016

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    ROTOR POUR GIRAVION COMPORTANT UN MECANISME DE BUTEE EN BATTEMENT, ET GIRAVION

    MASSAL FABIEN | Europäisches Patentamt | 2015

    Freier Zugriff

    Rotor pour giravion comportant un mécanisme de butée en battement, et giravion

    MASSAL FABIEN | Europäisches Patentamt | 2015

    Freier Zugriff