Requirements of universal fuel-filled aircraft control, adaptable to commercial use; basic design considerations to consider embrace control functions, environment, maintainability, adaptability, and cost; control is divided into computer, governing, and fuel metering; design areas are examined taking type 2039 fuel control, developed by Woodward Governor Co, as example.


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    Titel :

    Lightweight universal fuel control for aircraft turbine engines


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Leeson, P.J. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Fuel systems



    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A Lightweight Universal Fuel Control for Aircraft Turbine Engines

    Leeson, Plato J. | SAE Technical Papers | 1964


    Control of aircraft turbine engines

    Ravagli, A. / Noel, P. | Engineering Index Backfile | 1968


    Lightweight aircraft turbine protection

    DELUCA, J. / FENTON, B. / PETRIE, S. et al. | AIAA | 1993


    Aircraft gas turbine engines

    Engineering Index Backfile | 1948