Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2

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Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2. / Mesquita-Guimarães, Joana; Garcia, Eugenio; Osendi, Maria Isabel et al.
in: Composites / B, Jahrgang 61.2014, Nr. May, 29.01.2014, S. 199-205.

Publikationen: Beitrag in FachzeitschriftArtikelForschung(peer-reviewed)

Vancouver

Mesquita-Guimarães J, Garcia E, Osendi MI, Sevecek O, Bermejo R. Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2. Composites / B. 2014 Jan 29;61.2014(May):199-205. Epub 2014 Jan 29. doi: 10.1016/j.compositesb.2013.11.012

Author

Mesquita-Guimarães, Joana ; Garcia, Eugenio ; Osendi, Maria Isabel et al. / Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2. in: Composites / B. 2014 ; Jahrgang 61.2014, Nr. May. S. 199-205.

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@article{a868b7befd854436883fecce5af4b4a8,
title = "Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2",
abstract = "Environmental barrier coatings (EBCs) are proposed as an option to reduce the high temperature water vapour corrosion in gas turbines ceramic components made of Si3N4 or SiC/SiCf, which are projected to achieve further energy efficient gas turbines. These coating are commonly designed as multilayer systems firmly attached to the ceramic substrate with the aim of retarding or avoiding its degradation after exposure to environmental conditions close to those in gas turbines. Therefore, to fulfil this function crack formation/propagation in the coatings must be controlled. In present work, three types of environmental barrier coatings fabricated by air plasma spray and containing a Si layer attached to SiC substrate plus 2 to 5 layers of different mullite/Y2O3 stabilized–ZrO2 mixtures are examined. To determine the level of residual stresses in the as-sprayed coating/substrate systems a three dimensional finite element model is developed and also tested for same coatings but aged under, high temperature and rich water vapour atmosphere. The model calculates the zones of maximum tensile stresses in the coatings which agree with experimental observation identifying the type, number and location of cracks. This model could be extended to similar EBC systems, and more importantly, could be use as a powerful designing tool for these complex structures.",
author = "Joana Mesquita-Guimar{\~a}es and Eugenio Garcia and Osendi, {Maria Isabel} and Oldrich Sevecek and Raul Bermejo",
year = "2014",
month = jan,
day = "29",
doi = "10.1016/j.compositesb.2013.11.012",
language = "English",
volume = "61.2014",
pages = "199--205",
journal = "Composites / B",
issn = "1879-1069",
publisher = "Elsevier",
number = "May",

}

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TY - JOUR

T1 - Effect of aging on the onset of cracks due to redistribution of residual stresses in functionally graded environmental barrier coatings of mullite/ZrO2

AU - Mesquita-Guimarães, Joana

AU - Garcia, Eugenio

AU - Osendi, Maria Isabel

AU - Sevecek, Oldrich

AU - Bermejo, Raul

PY - 2014/1/29

Y1 - 2014/1/29

N2 - Environmental barrier coatings (EBCs) are proposed as an option to reduce the high temperature water vapour corrosion in gas turbines ceramic components made of Si3N4 or SiC/SiCf, which are projected to achieve further energy efficient gas turbines. These coating are commonly designed as multilayer systems firmly attached to the ceramic substrate with the aim of retarding or avoiding its degradation after exposure to environmental conditions close to those in gas turbines. Therefore, to fulfil this function crack formation/propagation in the coatings must be controlled. In present work, three types of environmental barrier coatings fabricated by air plasma spray and containing a Si layer attached to SiC substrate plus 2 to 5 layers of different mullite/Y2O3 stabilized–ZrO2 mixtures are examined. To determine the level of residual stresses in the as-sprayed coating/substrate systems a three dimensional finite element model is developed and also tested for same coatings but aged under, high temperature and rich water vapour atmosphere. The model calculates the zones of maximum tensile stresses in the coatings which agree with experimental observation identifying the type, number and location of cracks. This model could be extended to similar EBC systems, and more importantly, could be use as a powerful designing tool for these complex structures.

AB - Environmental barrier coatings (EBCs) are proposed as an option to reduce the high temperature water vapour corrosion in gas turbines ceramic components made of Si3N4 or SiC/SiCf, which are projected to achieve further energy efficient gas turbines. These coating are commonly designed as multilayer systems firmly attached to the ceramic substrate with the aim of retarding or avoiding its degradation after exposure to environmental conditions close to those in gas turbines. Therefore, to fulfil this function crack formation/propagation in the coatings must be controlled. In present work, three types of environmental barrier coatings fabricated by air plasma spray and containing a Si layer attached to SiC substrate plus 2 to 5 layers of different mullite/Y2O3 stabilized–ZrO2 mixtures are examined. To determine the level of residual stresses in the as-sprayed coating/substrate systems a three dimensional finite element model is developed and also tested for same coatings but aged under, high temperature and rich water vapour atmosphere. The model calculates the zones of maximum tensile stresses in the coatings which agree with experimental observation identifying the type, number and location of cracks. This model could be extended to similar EBC systems, and more importantly, could be use as a powerful designing tool for these complex structures.

U2 - 10.1016/j.compositesb.2013.11.012

DO - 10.1016/j.compositesb.2013.11.012

M3 - Article

VL - 61.2014

SP - 199

EP - 205

JO - Composites / B

JF - Composites / B

SN - 1879-1069

IS - May

ER -