The crack behavior and delamination mechanisms of air plasma sprayed thermal barrier coatings under ultrasonic plasma jet at 1600 °C

In this contribution, the performance and delamination mechanisms of air plasma sprayed (APS) yttria stabilized zirconia thermal barrier coatings (YSZ TBCs) under high intensity heat flux at 1600 °C was investigated. The plasma jet was adopted as the heat source with a combination of high temperatur...

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Published inJournal of the European Ceramic Society Vol. 43; no. 9; pp. 4136 - 4145
Main Authors Cai, Huangyue, Shan, Xiao, Lu, Jie, Luo, Lirong, Cai, Zhenwei, Wang, Weize, Zhang, Xiancheng, Zhao, Xiaofeng
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.08.2023
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Online AccessGet full text
ISSN0955-2219
1873-619X
DOI10.1016/j.jeurceramsoc.2023.03.005

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Abstract In this contribution, the performance and delamination mechanisms of air plasma sprayed (APS) yttria stabilized zirconia thermal barrier coatings (YSZ TBCs) under high intensity heat flux at 1600 °C was investigated. The plasma jet was adopted as the heat source with a combination of high temperature and high-speed jet-stream erosion. It was found that the YSZ topcoat would exfoliate when the vertical crack connected to the interior (interfacial/shear) cracks to form a free edge, which turned the mixed-mode buckle delamination into a mode I cracking. The thermo-mechanical analysis indicated that energy release rate associated with the transient cooling was the driving force for the interfacial cracks, while the vertical cracks were developed by the tensile stress during cooldown. The findings obtained in this study implied that the YSZ TBCs can be used for the thermal protection of combustor in ramjet engines.
AbstractList In this contribution, the performance and delamination mechanisms of air plasma sprayed (APS) yttria stabilized zirconia thermal barrier coatings (YSZ TBCs) under high intensity heat flux at 1600 °C was investigated. The plasma jet was adopted as the heat source with a combination of high temperature and high-speed jet-stream erosion. It was found that the YSZ topcoat would exfoliate when the vertical crack connected to the interior (interfacial/shear) cracks to form a free edge, which turned the mixed-mode buckle delamination into a mode I cracking. The thermo-mechanical analysis indicated that energy release rate associated with the transient cooling was the driving force for the interfacial cracks, while the vertical cracks were developed by the tensile stress during cooldown. The findings obtained in this study implied that the YSZ TBCs can be used for the thermal protection of combustor in ramjet engines.
Author Lu, Jie
Zhang, Xiancheng
Zhao, Xiaofeng
Luo, Lirong
Shan, Xiao
Wang, Weize
Cai, Huangyue
Cai, Zhenwei
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Thermal barrier coatings
Delamination mechanism
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Snippet In this contribution, the performance and delamination mechanisms of air plasma sprayed (APS) yttria stabilized zirconia thermal barrier coatings (YSZ TBCs)...
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elsevier
SourceType Enrichment Source
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Publisher
StartPage 4136
SubjectTerms Delamination mechanism
Plasma jet erosion
Thermal barrier coatings
Thermal transient
Title The crack behavior and delamination mechanisms of air plasma sprayed thermal barrier coatings under ultrasonic plasma jet at 1600 °C
URI https://dx.doi.org/10.1016/j.jeurceramsoc.2023.03.005
Volume 43
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