Basic difference of systems is that in Skid Warning brakes are controlled by pilot, while Automatic Anti-Skid releases brake pressure automatically by means of hydraulic valve; with either system, d-c generator, driven by wheel, senses changes in wheel rotation; by connecting generator through electrical circuitry, deviation of wheel from normal deceleration is sensed; sequence of operations; detailed circuitry of systems using same sensing, power, and locked wheel prevention circuits.


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    Title :

    Two methods of aircraft skid control


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1958 Landing



    Publication date :

    1958


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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