Publication detail

Damage and Performance Assessment of Protective Coatings on Turbine Blades

POKLUDA, J. KIANICOVÁ, M.

Czech title

Poškození a zhodnocení významu ochranných povlaků na lopatkách turbín

English title

Damage and Performance Assessment of Protective Coatings on Turbine Blades

Type

book chapter

Language

en

Original abstract

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.

Czech abstract

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.

English abstract

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.

Keywords in Czech

Ochranné povlaky; Mechanismy poškozování; Difuse; Termo-mechanická únava

Keywords in English

Protective coatings; Damage mechanisms; Diffussion; Thermo-mechanical fatigue

RIV year

2010

Released

01.10.2010

Publisher

SCIYO

Location

Rijeka

ISBN

978-953-307-146-6

Book

Gas Turbines

Edition number

1

Pages from–to

283–306

Pages count

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",
  month="October",
  pages="283--306",
  publisher="SCIYO",
  address="Rijeka",
  isbn="978-953-307-146-6"
}