A core-shell thermal barrier coating with strong resistance to molten silicate attack and fracture

Date published

2025-04-15

Free to read from

2025-03-10

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Publisher

Elsevier

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Article

ISSN

1359-6454

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Citation

Li Z, Brewster G, Isern L, et al., (2025) A core-shell thermal barrier coating with strong resistance to molten silicate attack and fracture. Acta Materialia, Volume 288, April 2025, Article number 120870

Abstract

We report a new thermal barrier coating (TBC) with strong resistance to calcia–magnesia–alumina–silicate (CMAS) attack and fracture. The design is based on a core-shell microstructure where each building block of the TBC comprises a tough yttria stabilised zirconia (YSZ) core and a CMAS-resistant shell. To demonstrate the feasibility of the design, we select alumina, an established CMAS-resistant ceramic, as the shell material and manufacture core-shell TBCs by first synthesising “YSZ core-alumina shell” powder using the sol-gel method and then thermally spraying the powder to form core-shell TBCs. Microstructural characterisations confirm that a core-shell coating structure is successfully manufactured. However, the melting and mixing of alumina and YSZ in thermal spray result in the formation of a microstructure composed of alumina-alloyed zirconia grains and intergranular alumina, with the overall alumina concentration increasing from the core to the shell. The CMAS penetration depth through the core-shell TBC is over an order of magnitude lower than that through the benchmark YSZ TBC, which is attributed to the multiscale protection of the core-shell microstructure against CMAS infiltration through cracks and grain boundaries. The core-shell TBC has a similar stiffness to the YSZ TBC but exhibits a lower erosion rate and higher fracture toughness, indicating enhanced fracture resistance without compromising strain tolerance. The improved fracture resistance of the core-shell TBC is attributed to its less defective intersplat structure and greater ferroelastic toughening strain. Compared to the YSZ TBC, the core-shell TBC shows lower stiffness and nearly identical fracture toughness after annealing.

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Github

Keywords

40 Engineering, 4016 Materials Engineering, 4017 Mechanical Engineering, Materials, 4016 Materials engineering, 4017 Mechanical engineering, 5104 Condensed matter physics, Core-shell, TBC, CMAS, Fracture

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Attribution 4.0 International

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Funder/s

Ying Chen would like to thank the funding support from Innovate UK (project number: 10040292) and the Henry Royce Institute for advanced materials through the Industrial Collaboration Programme (EP/X527257/1). Part of this work was supported by the new lecturer start-up grant awarded to Ying Chen by the Department of Materials at the University of Manchester. Ping Xiao acknowledges support from the Royal Academy of Engineering and Rolls-Royce for the appointment of Rolls-Royce/Royal Academy of Engineering Research Chair in Advanced Coating Technology. This work was supported by the Henry Royce Institute for Advanced Materials through the Researcher and Student Access Scheme, funded through EPSRC grants EP/R00661X/1, EP/S019367/1, EP/P025021/1 and EP/P025498/1. The authors would like to acknowledge the support of Mr Arturo Vara Herrera (Cranfield University) in the erosion experiments.