中国航空学报(英文版)2024,Vol.37Issue(6) :410-424.DOI:10.1016/j.cja.2024.03.035

Thermal oxidation description methodology of thermal barrier coatings on gas turbine blades considering service characteristics

Qiannan TAO Yanrong WANG Dasheng WEI Shun YANG
中国航空学报(英文版)2024,Vol.37Issue(6) :410-424.DOI:10.1016/j.cja.2024.03.035

Thermal oxidation description methodology of thermal barrier coatings on gas turbine blades considering service characteristics

Qiannan TAO 1Yanrong WANG 2Dasheng WEI 2Shun YANG1
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作者信息

  • 1. School of Energy and Power Engineering,Beihang University,Beijing 100191,China
  • 2. School of Energy and Power Engineering,Beihang University,Beijing 100191,China;Jiangxi Research Institute of Beihang University,Nanchang 330096,China
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Abstract

Predicting the thickness of Thermally Grown Oxide(TGO)and the residual stresses induced by TGO growth in the Thermal Barrier Coatings(TBCs)is significant work in analyzing the failure of TBCs.In practical applications,the operating temperature,oxygen partial pressure,aluminium content in TBCs,and porosity of the topcoat affect the oxidation rate.Therefore,a novel oxidation rate model is proposed to describe the effect of such factors.The parameters in the proposed model were fitted with isothermal degradation test data from prior literature.Then,a method for calculating the residual stress in a disk-shaped specimen was developed based on the oxidized growth strain model and the oxidized model.Finally,a variable-temperature oxidation experiment was performed to validate the new oxidation model.The average error between the pre-dicted and experimental thicknesses is approximately 10%,and the average error between the resid-ual stresses is 30%.Under the variable-temperature condition,the error between the predicted thickness and the average experimental thickness is 3.9%.

Key words

Thermal barrier coatings/Oxidation/Gas turbine/Residual stresses/Sintering

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基金项目

National Science and Technology Major Project,China(J2019-Ⅳ-0006-0074)

National Natural Science Foundation of China(12202030)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量2
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