A hydro-elastic damper comprising at least one elastic assembly comprising an elastic member between two strength members. The elastic assembly including a compression chamber. The hydro-elastic damper includes a damping assembly provided with an expansion chamber that is defined in a transverse direction by an end wall and by a piston. The compression chamber is hydraulically connected to the expansion chamber by three hydraulic connections comprising respectively: a duct; at least one first passage with an overpressure valve; and at least one second passage with a check valve.


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    Title :

    AMORTISSEUR HYDRO-ELASTIQUE, ET AERONEF


    Additional title:

    HYDRO-ELASTIC SHOCK ABSORBER, AND AIRCRAFT
    HYDROELASTISCHER STOSSDÄMPFER, UND LUFTFAHRZEUG


    Contributors:

    Publication date :

    2020-10-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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