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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    Titel :

    Two methods of aircraft skid control


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Collier, G.H. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1958 Landing



    Erscheinungsdatum :

    1958


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    TWO METHODS OF AIRCRAFT SKID CONTROL

    COLLIER, G. H. | SAE Technical Papers | 1958


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