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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    Title :

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


    Contributors:

    Publication date :

    2016-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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