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


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural requirements for aircraft engine main fuel pumps and controls


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1968 Fuel systems



    Publication date :

    1968


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Structural Requirements for Aircraft Engine Main Fuel Pumps and Controls

    Eckert, Arthur F. J. | SAE Technical Papers | 1968


    Fuel requirements of the gasoline aircraft-engine

    Heron, S.A. | Engineering Index Backfile | 1930


    Fuel Requirements of the Gasoline Aircraft-Engine

    Heron, S. D. | SAE Technical Papers | 1930


    AIR DENSITY CONTROLS FOR FUEL INJECTION PUMPS

    HUMBER, JOHN | SAE Technical Papers | 1956


    General fuel requirements for commercial aircraft gas turbine engine

    Dougherty, F.G. / Hardin, M.C. | Engineering Index Backfile | 1956