A shock damper is disclosed. The shock damper may have a shear control apparatus through which a shear-thickening fluid may flow. In this manner, the shock damper may compress at different rates for different applied impulse forces, in response to the changing viscosity of the shear-thickening fluid.


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    Titel :

    LANDING GEAR SYSTEMS HAVING SHEAR-THICKENING AND SHEAR-THINNING FLUID RESPONSES


    Beteiligte:
    SMITH KENNETH D (Autor:in) / MANES ENRICO (Autor:in)

    Erscheinungsdatum :

    2016-08-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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