A damper device provided with a first connection member, a second connection member, a resilient member, and a hydraulic system. The hydraulic system includes an outer casing and a rod, the first connection member being fastened in reversible manner to the outer casing, the resilient member being arranged around a projecting portion of the rod, the resilient member comprising at least one resilient means interposed between a first strength member and a second strength member, the first strength member being fastened in reversible manner to the outer casing, the second strength member being constrained to move in translation with the projecting portion, and the connection member being fastened in reversible manner to the projecting portion.


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    Titel :

    DISPOSITIF D'AMORTISSEMENT, ET AERONEF


    Weitere Titelangaben:

    A DAMPER DEVICE AND AN AIRCRAFT
    DÄMPFUNGSVORRICHTUNG UND LUFTFAHRZEUG


    Beteiligte:

    Erscheinungsdatum :

    12.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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