Structural requirements for aircraft engine main fuel pumps and controls have been changing and increasing. The influence of these changing conditions on specific component parts, particularly housings and drive train elements, is reviewed. Recommendations are made for detailed specifications changes.


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    Title :

    Structural Requirements for Aircraft Engine Main Fuel Pumps and Controls


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    1968 Automotive Engineering Congress and Exposition ; 1968



    Publication date :

    1968-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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