Cost reduction in aircraft turbine engines may be obtained through performance reductions that are acceptable for ranges that are considerably shorter than the range for which current and costly engines were developed. Cost reduction in the fuel control for these cost engines must be achieved without significant performance reduction. This paper describes a fuel control approach that appears to meet this requirement and reviews the work that has been performed on it over the past few years.


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    Titel :

    A Simplified Fuel Control Approach for Low-Cost Aircraft Gas Turbines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Gold, Harold (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1973



    Erscheinungsdatum :

    01.02.1973




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch