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Article

Experimental and Simulation Studies on Thermal Shock of Multilayer Thermal Barrier Coatings with an Intermediate Transition Layer at 1500 °C

1
Key Laboratory of Pressure System and Safety, Ministry of Education, East China University of Science and Technology, Shanghai 200237, China
2
Shanghai Institute of Aircraft Mechanics and Control, Shanghai 200092, China
*
Authors to whom correspondence should be addressed.
These authors contributed equally to this work.
Coatings 2024, 14(12), 1614; https://doi.org/10.3390/coatings14121614
Submission received: 14 November 2024 / Revised: 19 December 2024 / Accepted: 21 December 2024 / Published: 23 December 2024

Abstract

Strain tolerance is a crucial factor affecting the thermal life of coatings, and a higher strain tolerance can effectively alleviate the thermal stresses on coatings during thermal shock. To improve the strain tolerance, the coating structure was optimized by introducing an intermediate transition layer in this study. The intermediate transition layer material was prepared using a 1:1 volume ratio mixture of 6–8 wt. % Yttria-stabilized zirconia (YSZ) and NiCrAlY powders in the experiments. The coating structure consisted of an Al2O3-GdAlO3 (AGAP) anti-erosion layer, a YSZ layer, an intermediate transition layer, and a bonding layer from top to bottom. After thermal shock experiments at 1500 °C, the coatings with the addition of the intermediate transition layer exhibited different failure modes, with the crack location shifting from between the YSZ and the bonding layer to within the intermediate transition layer, compared to the coatings without the intermediate transition layer. Finite element simulation analysis showed that the intermediate transition layer effectively increased the strain tolerance of the coating and significantly reduced the thermal stress. Furthermore, incorporating an embedded micron agglomerated particle-based (EMAP) thermal barrier coating structure into the intermediate transition layer effectively alleviated thermal stresses and enhanced the coating’s thermal insulation performance.
Keywords: thermal barrier coatings; multilayer; thermal shock; finite element analysis thermal barrier coatings; multilayer; thermal shock; finite element analysis

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MDPI and ACS Style

Liu, P.; Yang, S.; Li, K.; Wang, W.; Liu, Y.; Yang, T. Experimental and Simulation Studies on Thermal Shock of Multilayer Thermal Barrier Coatings with an Intermediate Transition Layer at 1500 °C. Coatings 2024, 14, 1614. https://doi.org/10.3390/coatings14121614

AMA Style

Liu P, Yang S, Li K, Wang W, Liu Y, Yang T. Experimental and Simulation Studies on Thermal Shock of Multilayer Thermal Barrier Coatings with an Intermediate Transition Layer at 1500 °C. Coatings. 2024; 14(12):1614. https://doi.org/10.3390/coatings14121614

Chicago/Turabian Style

Liu, Pengpeng, Shilong Yang, Kaibin Li, Weize Wang, Yangguang Liu, and Ting Yang. 2024. "Experimental and Simulation Studies on Thermal Shock of Multilayer Thermal Barrier Coatings with an Intermediate Transition Layer at 1500 °C" Coatings 14, no. 12: 1614. https://doi.org/10.3390/coatings14121614

APA Style

Liu, P., Yang, S., Li, K., Wang, W., Liu, Y., & Yang, T. (2024). Experimental and Simulation Studies on Thermal Shock of Multilayer Thermal Barrier Coatings with an Intermediate Transition Layer at 1500 °C. Coatings, 14(12), 1614. https://doi.org/10.3390/coatings14121614

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