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Thermal properties and calcium-magnesium-alumino-silicate (CMAS) interaction of novel γ-phase ytterbium-doped yttrium disilicate (γ-Y1.5Yb0.5Si2O7) environmental barrier coating material

Zhang, Buhao; Zhang, Hangfeng; Bai, Mingwen; Du, Aochen; Owusu, Ebenezer B.; B. Owusu, Ebenezer B.; Lynam, Alex; Rincon Romero, Acacio; Curry, Nicholas; Hussain, Tanvir

Authors

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BUHAO ZHANG BUHAO.ZHANG@NOTTINGHAM.AC.UK
Research Associate

Hangfeng Zhang

Mingwen Bai

Aochen Du

Ebenezer B. Owusu

Ebenezer B. B. Owusu

Alex Lynam

Nicholas Curry

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TANVIR HUSSAIN TANVIR.HUSSAIN@NOTTINGHAM.AC.UK
Professor of Coatings and Surface Engineering



Abstract

Rare-earth disilicates are promising candidates for thermal and environmental barrier coatings (TEBC) in gas turbines that safeguard SiCf/SiC ceramic matrix composites (CMCs) from thermal degradation and environmental attacks. Here, we report a systematic investigation on novel TEBC material, γ-Y1.5Yb0.5Si2O7. The γ-phase quarter molar ytterbium–doped yttrium disilicate exhibited low thermal conductivity (1.72 W·m−1·K−1 at 1200 °C) and reduced intrinsic thermal expansion (3.17 ± 0.22 × 10−6 K−1 up to 1000 °C), ensuring promisingly effective thermal insulation and minimized thermal stress with CMC substrates. Using density functional theory (DFT), the heat capacity of γ-Y1.5Yb0.5Si2O7 was predicted higher than that of undoped γ-Y2Si2O7. Comparing these predictions to results calculated using the Neumann–Kopp (NK) rule revealed only minor variations. A metastable CMAS interaction byproduct, cyclosilicate phase Ca3RE2(Si3O9)2, was identified based on energy dispersive X-ray spectrometer (EDS) and electron backscatter diffraction (EBSD) techniques, appearing at 1300 °C but disappearing at 1400 °C. The γ-Y1.5Yb0.5Si2O7 exhibited good CMAS resistance on both dense pellets and sprayed coatings, forming a protective apatite (Ca2RE8(SiO4)6O2) interlayer that effectively hindered CMAS infiltration at evaluated temperatures. The relatively higher Y:Yb atomic ratio (> 3) in the apatite grains indicate differential reactivity with molten CMAS and provides crucial insights into the CMAS corrosion mechanism. These findings highlight the potential of γ-Y1.5Yb0.5Si2O7 as a CMC coating material, emphasizing the need for tailored microstructural optimization as a thermal sprayed coating to enhance long-term performance in extreme gas turbine environments.

Citation

Zhang, B., Zhang, H., Bai, M., Du, A., Owusu, E. B., B. Owusu, E. B., Lynam, A., Rincon Romero, A., Curry, N., & Hussain, T. (2024). Thermal properties and calcium-magnesium-alumino-silicate (CMAS) interaction of novel γ-phase ytterbium-doped yttrium disilicate (γ-Y1.5Yb0.5Si2O7) environmental barrier coating material. Advanced Composites and Hybrid Materials, 7(2), Article 64. https://doi.org/10.1007/s42114-024-00879-6

Journal Article Type Article
Acceptance Date Mar 22, 2024
Online Publication Date Apr 1, 2024
Publication Date 2024-04
Deposit Date Apr 1, 2024
Journal Advanced Composites and Hybrid Materials
Print ISSN 2522-0128
Electronic ISSN 2522-0136
Publisher Springer
Peer Reviewed Peer Reviewed
Volume 7
Issue 2
Article Number 64
DOI https://doi.org/10.1007/s42114-024-00879-6
Keywords CMAS resistance, Thermal property, Thermal environmental barrier coatings (TEBC), Density functional theory (DFT), Yttrium ytterbium disilicate
Public URL https://nottingham-repository.worktribe.com/output/33284926
Additional Information Received: 9 October 2023; Revised: 4 March 2024; Accepted: 22 March 2024; First Online: 1 April 2024; : ; : The authors declare no competing interests.