This paper reviews those requirements that are common in the design of all gas turbines combustion equipment. Where necessary, a distinction is made between the demands of industrial and aircraft chambers. The problem of designing equipment for long life and low pressure loss, in a size compatible with the overall engine, is discussed in detail, and the application of combustor characteristics and design factors to the demands of new aircraft and industrial turbines are anticipated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Clarke, J. S. (Autor:in) / Jackson, S. R. (Autor:in)

    Kongress:

    SAE World Congress & Exhibition ; 1964



    Erscheinungsdatum :

    1964-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Maintenance Considerations in Aircraft-Derivative Industrial Gas Turbines

    Goodwine, J. K. / Stradley, R. C. | SAE Technical Papers | 1974


    Combustion chambers for open-cycle marine gas turbines

    Darling, R.F. | Engineering Index Backfile | 1949