A linkage assembly configured for use on a rotor blade having a first section and a second section, the second section being configured to rotate about a blade fold axis between an aligned position and a rotated position relative to the first section is provided. The linkage assembly includes a bracket having a first portion rotatably coupled to the first section about the blade fold axis and a second portion mounted to the second section. A spacer assembly is positioned between the bracket and an adjacent wall of the second section. The overall thickness of the spacer assembly is adjustable to control a distance between the second section and the bracket to adjust the rotated position.


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    Titel :

    SYSTEM FOR SHIMMING BLADE FOLD ANGLE ABOUT AN AXIS OF ROTATION


    Beteiligte:
    KIRCHEN ADRIAL (Autor:in) / CRIM JONATHON (Autor:in) / CAPELLE STEVEN M (Autor:in) / POULIN STEPHEN V (Autor:in)

    Erscheinungsdatum :

    2017-08-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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