Evaluation of the Residual Stress Evolution in Thermal Barrier Coating System Using the In Situ Curvature of a Three-Layered Specimen
Thermal barrier coatings (TBCs) are used to protect the hot sections of gas turbines and jet engines. A typical TBC system consists of a substrate, bond coat, and a TBC top coat (TC). To develop a high-performance TBC, it is essential to accurately evaluate the residual stress evolution during the t...
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Published in | Journal of thermal spray technology Vol. 30; no. 5; pp. 1183 - 1198 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
New York
Springer US
01.06.2021
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Subjects | |
Online Access | Get full text |
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Summary: | Thermal barrier coatings (TBCs) are used to protect the hot sections of gas turbines and jet engines. A typical TBC system consists of a substrate, bond coat, and a TBC top coat (TC). To develop a high-performance TBC, it is essential to accurately evaluate the residual stress evolution during the thermal spray process (deposition and post-deposition cooling) of TBCs. In this study, a simple analytical block model of three-layered system using the in situ curvature change caused by the misfit strain of each layer was proposed to investigate the residual stress evolution of a TBC system. In the model, the deposition stress and final residual stress were evaluated from the change in the curvature. Subsequently, the thermal stress during post-deposition cooling was indirectly evaluated by subtracting the deposition stress from the final residual stress. The accuracy of the average through-thickness stress of the deposition process, cooling process, and final state evaluated by the proposed analytical block model was verified by the finite element analysis block model and analytical progressively deposited model. Finally, the proposed model was applied to an atmospheric plasma-sprayed TBC system, and the practicability of the model was experimentally demonstrated. |
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ISSN: | 1059-9630 1544-1016 |
DOI: | 10.1007/s11666-021-01221-y |