Comparative Heat-Resistance Investigation of Protective Coatings

Since modern gas turbine engines operate under changing temperature load conditions, one of the important characteristics of the protective coatings on turbine blades is their high resistance to the appearance and development of cracks under mechanical and thermal loads. The effective internal heat...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Russian metallurgy Metally 2023-12, Vol.2023 (12), p.1942-1946
Hauptverfasser:	Zorichev, A. V., Pashchenko, G. T., Parfenovskaya, O. A., Samoilenko, V. M., Golovneva, T. I.
Format:	Artikel
Sprache:	eng
Schlagworte:	Chemical composition Chemistry and Materials Science Cracks Fatigue cracks Fatigue failure Fracture mechanics Gas turbine engines Hardening and Coating Technologies Heat resistance High resistance High temperature Materials Science Metallic Materials Phase composition Protective coatings Surface layers System effectiveness Temperature Temperature dependence Thermal analysis Thermal cycling Thermal fatigue Thermal resistance Thermal stress Turbine blades
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!