Calculations of the stress state of a two-layer system of a thermal barrier coating are performed depending on the thermal loading mode and the presence or absence of a temperature gradient over the sample cross section during the thermal resistance test. The calculations took into account changes in the state of the structure of the coating ceramic layer and the sublayer. A numerical model of the thermal barrier coating performance is developed depending on the thickness ratio of the ceramic layer and the sublayer.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Regularities of the Heat Resistance Formation of Thermal Barrier Coatings Counting Technological Heredity


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 64 , 4 ; 756-763


    Erscheinungsdatum :

    01.10.2021


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Self-organization and heredity in technological systems subjected to combined influences

    Kheifets, M. L. / Yashcheritsin, P. I. | British Library Online Contents | 1995


    Nucleoproteins and Heredity

    M. V. Turbin | NTIS | 1960


    Thermal Barrier Coatings

    Shih, Tom I-P. / Yang, Vigor / Trice, Rodney et al. | AIAA | 2014



    Thick thermal barrier coatings

    Yonushonis,T.M. / Ng,H.K. / Vovak,R.C. et al. | Kraftfahrwesen | 1991