Improvements of an existing pneumatic-fluidic antiskid system leading to operating efficiencies above 85% and installation concepts for a full system test on the T-43A aircraft are described. A fluidic locked wheel and touchdown protection circuit is proposed. Initial design of the integrated fluidic circuit and the modification of the antiskid valve in accordance with a detailed system specification are shown.


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    Titel :

    Improved Pneumatic-Fluidic Antiskid System and Preliminary System Integration Study


    Beteiligte:
    H. H. Straub (Autor:in) / R. H. Lichtenwalter (Autor:in) / N. S. Attri (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    104 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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