Abstract Influence of the free air temperature during aircraft takeoff and engine operating time upon the cyclic life of an aircraft GTE turbine disk made from the heat-resistance deformable nickel-base alloy is analyzed and the variation of engine operating parameters in the process of service is taken into account.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Variation of aircraft GTE turbine disks cyclic life depending on operational factors


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2011-06-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Life prediction methodology for aircraft gas turbine engine disks

    MAHORTER, R. / LONDON, G. / FOWLER, S. et al. | AIAA | 1985




    Designing Film-Cooled Turbine Disks

    Wagner, William R. | NTRS | 1988


    Development and Characterization of Overspeed and Cyclic Behavior of Dual Grain Structure Turbine Disks

    Green, K. A. / Helmink, R. C. | British Library Conference Proceedings | 2007