Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings

In this paper, a finite element model was developed for a turbine blade with thermal barrier coatings to investigate its failure behavior under cyclic thermal loading. Based on temperature and stress fields obtained from finite element simulations, dangerous regions in ceramic coating were determine...

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Main Authors: Yang, Li, Liu, Qixing, Zhou, Yi-Chun, Mao, Weiguo, Lu, Chunsheng
Format: Journal Article
Published: Zhongguo Kexueyuan Jinshu Yanjiusuo 2014
Subjects:
Online Access:http://hdl.handle.net/20.500.11937/17397
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author Yang, Li
Liu, Qixing
Zhou, Yi-Chun
Mao, Weiguo
Lu, Chunsheng
author_facet Yang, Li
Liu, Qixing
Zhou, Yi-Chun
Mao, Weiguo
Lu, Chunsheng
author_sort Yang, Li
building Curtin Institutional Repository
collection Online Access
description In this paper, a finite element model was developed for a turbine blade with thermal barrier coatings to investigate its failure behavior under cyclic thermal loading. Based on temperature and stress fields obtained from finite element simulations, dangerous regions in ceramic coating were determined in terms of the maximum principal stress criterion. The results show that damage preferentially occurs in the chamfer and rabbet of a turbine blade with thermal barrier coatings and its thermal fatigue life decreases with the increase of thermal stress induced by high service temperature.
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format Journal Article
id curtin-20.500.11937-17397
institution Curtin University Malaysia
institution_category Local University
last_indexed 2025-11-14T07:21:13Z
publishDate 2014
publisher Zhongguo Kexueyuan Jinshu Yanjiusuo
recordtype eprints
repository_type Digital Repository
spelling curtin-20.500.11937-173972017-09-13T15:44:15Z Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings Yang, Li Liu, Qixing Zhou, Yi-Chun Mao, Weiguo Lu, Chunsheng Finite element model Thermal fatigue Life prediction Thermal barrier coatings Turbine blade In this paper, a finite element model was developed for a turbine blade with thermal barrier coatings to investigate its failure behavior under cyclic thermal loading. Based on temperature and stress fields obtained from finite element simulations, dangerous regions in ceramic coating were determined in terms of the maximum principal stress criterion. The results show that damage preferentially occurs in the chamfer and rabbet of a turbine blade with thermal barrier coatings and its thermal fatigue life decreases with the increase of thermal stress induced by high service temperature. 2014 Journal Article http://hdl.handle.net/20.500.11937/17397 10.1016/j.jmst.2013.11.005 Zhongguo Kexueyuan Jinshu Yanjiusuo restricted
spellingShingle Finite element model
Thermal fatigue
Life prediction
Thermal barrier coatings
Turbine blade
Yang, Li
Liu, Qixing
Zhou, Yi-Chun
Mao, Weiguo
Lu, Chunsheng
Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title_full Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title_fullStr Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title_full_unstemmed Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title_short Finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
title_sort finite element simulation on thermal fatigue of a turbine blade with thermal barrier coatings
topic Finite element model
Thermal fatigue
Life prediction
Thermal barrier coatings
Turbine blade
url http://hdl.handle.net/20.500.11937/17397