This paper examines some of the background that has led to the requirements for a lightweight universal fuel control for aircraft gas turbine engines. One design solution for this type of fuel control is reviewed with regard to function, adaptability, maintenance, and cost.


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    Title :

    A Lightweight Universal Fuel Control for Aircraft Turbine Engines


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Lightweight universal fuel control for aircraft turbine engines

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