The major technological developments which have made possible the trend towards higher temperatures in modern aircraft gas turbine engines are discussed. The relative importance of manufacturing processes, material developments, cooling techniques, analytical design procedures, rupture and cyclic life considerations, and aerodynamic and mechanical design improvements are discussed along with illustrative examples and technical data.The need for a balanced design approach is stressed, and examples are given where trade-offs can be made. It is noted that the advances in aircraft engines during the last 10 years have been based on the evolution of sound engineering principles, extensive component and engine development, and careful consideration of the operational requirements rather than a tremendous breakthrough or revolutionary concept in any one area.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    High Temperature Turbine Design Considerations


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Suciu, S. N. (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1971



    Erscheinungsdatum :

    01.02.1971




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    High Temperature Turbine Design Considerations

    Suciu, S.N. | Emerald Group Publishing | 1970




    DESIGN CONSIDERATIONS FOR A HELICOPTER GAS TURBINE POWERPLANT

    KOETTING, J. L. | SAE Technical Papers | 1953