A method and apparatus for reducing a vibratory response in a structure using a tuning object. A selected mass may be identified for the tuning object. A plurality of channels may be formed in a workpiece having a mass greater than the selected mass to form the tuning object having the selected mass. The tuning object may be bonded to the structure using an adhesive bond to reduce the vibratory response of the structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Apparatus and method for tuning a vibratory response of a rotor blade


    Beteiligte:

    Erscheinungsdatum :

    02.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



    Apparatus and method for tuning a vibratory response of a rotor blade

    GILL FRANK JOSEPH III / FAY RUSSELL EDDY | Europäisches Patentamt | 2019

    Freier Zugriff




    Investigation of Rotor Vibratory Loads of a UH-60A Individual Blade Control System

    Yeo, Hyeonsoo / Jain, Rohit / Jayaraman, Buvana | British Library Conference Proceedings | 2015