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POKLUDA, J.; KIANICOVÁ, M.
Originální název
Damage and Performance Assessment of Protective Coatings on Turbine Blades
Anglický název
Druh
Kapitola, resp. kapitoly v odborné knize
Originální abstrakt
Protective coatings on blades serve as physical barriers between the underlying substrate and the outer environment. This article presents an overview of damage mechanisms leading to failure of all basic types of coatings (diffusion, overlay and thermal barrier) on turbine blades of aircraft engines during service. Although a special emphasize is devoted to destructive effects of thermo-mechanical fatigue and overheating, the severe effects of hot corrosion, oxidation and erosion effects are also described. Most important material and design parameters of coatings are highlighted with respect to an optimum protection from damage caused by aggressive environment and thermo-mechanical loading. For this purpose, many recent results of advanced numerical models based on fracture mechanics are taken into account.
Anglický abstrakt
Klíčová slova
Protective coatings; Damage mechanisms; Diffussion; Thermo-mechanical fatigue
Klíčová slova v angličtině
Autoři
Rok RIV
2013
Vydáno
01.10.2010
Nakladatel
SCIYO
Místo
Rijeka
ISBN
978-953-307-146-6
Kniha
Gas Turbines
Edice
1
Strany od
283
Strany do
306
Strany počet
24
BibTex
@inbook{BUT98965, author="Jaroslav {Pokluda} and Marta {Kianicová}", title="Damage and Performance Assessment of Protective Coatings on Turbine Blades", booktitle="Gas Turbines", year="2010", publisher="SCIYO", address="Rijeka", series="1", edition="1", pages="283--306", isbn="978-953-307-146-6" }