A vibration damper including a frame having at least a first cavity, a frame first end and a frame second end spaced from the frame first end; a shaft slidably coupled to and extending into the frame where the shaft extends through the first cavity; a first vibration isolator disposed within the first cavity where the shaft extends through the first vibration isolator so as to capture the first vibration isolator within the first cavity where the first vibration isolator interfaces with the frame second end; and a second vibration isolator disposed on the shaft, where the shaft extends through the second vibration isolator so as to capture the second vibration isolator on the shaft where the second vibration isolator interfaces with the frame second end opposite the first vibration isolator, where the first vibration isolator and the second vibration isolator act only in compression.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    VIBRATION DAMPING LINK AND METHOD THEREFORE


    Beteiligte:

    Erscheinungsdatum :

    18.10.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Vibration damping link and method therefore

    LUDIN DOUGLAS R / STAUFFER MATTHEW S | Europäisches Patentamt | 2020

    Freier Zugriff

    VIBRATION DAMPING LINK AND METHOD THEREFOR

    LUDIN DOUGLAS R / STAUFFER MATTHEW S | Europäisches Patentamt | 2021

    Freier Zugriff

    TURBOFAN ENGINE AND CORE LINK THEREFORE

    OLVER BRYAN WILLIAM | Europäisches Patentamt | 2020

    Freier Zugriff

    Turbofan engine and core link therefore

    OLVER BRYAN WILLIAM | Europäisches Patentamt | 2021

    Freier Zugriff

    TURBOFAN ENGINE AND CORE LINK THEREFORE

    OLVER BRYAN WILLIAM | Europäisches Patentamt | 2020

    Freier Zugriff