The main engine air turbine start system, which typically consists of an air turbine starter and starter control valve, is a key contributor to aircraft dispatch reliability. Evolving aircraft propulsion systems have resulted in more aggressive operational environments, thus providing the impetus to improve the design of the start systems to enhance their durability and aid in improving both dispatch reliability and system responsiveness.


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    Titel :

    Design Improvements in Air Turbine Start Systems


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Plevich, C. W. (Autor:in) / Farnsworth, G. A. (Autor:in) / Durnal, K. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1992



    Erscheinungsdatum :

    1992-10-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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