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Journal of Advanced Ceramics 2021, 10(6): 1389-1397 https://doi.org/10.1007/s40145-021-0514-x
Research Article | Open Access | Issue | Published: 27 October 2021

Reaction products of Sm2Zr2O7 with calcium-magnesium-aluminum-silicate (CMAS) and their evolution

Show Author's Information Yinghua WANGa,b,  Zhuang MAa,b,  Ling LIUa,b( ),  Yanbo LIUa,b
School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
National Key Laboratory of Science and Technology on Materials under Shock and Impact, Beijing 100081, China
Keywords:
corrosion, Sm2Zr2O7 ceramic, calcium-magnesium-aluminum-silicate (CMAS), reaction product
Cite this article:
WANG Y, MA Z, LIU L, et al. Reaction products of Sm2Zr2O7 with calcium-magnesium-aluminum-silicate (CMAS) and their evolution. Journal of Advanced Ceramics, 2021, 10(6): 1389-1397. https://doi.org/10.1007/s40145-021-0514-x
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Abstract Full text About this article

During flight, many silicates (sand, dust, debris, fly ash, etc.) are ingested by an engine. They melt at high operating temperatures on the surface of thermal barrier coatings (TBCs) to form calcium-magnesium-aluminum-silicate (CMAS) amorphous settling. CMAS corrodes TBCs and causes many problems, such as composition segregation, degradation, cracking, and disbanding. As a new generation of TBC candidate materials, rare-earth zirconates (such as Sm2Zr2O7) have good CMAS resistance properties. The reaction products of Sm2Zr2O7 and CMAS and their subsequent changes were studied by the reaction of Sm2Zr2O7 and excess CMAS at 1350 ℃. After 1 h of reaction, Sm2Zr2O7 powders were not completely corroded. The reaction products were Sm-apatite and c-ZrO2 solid solution. After 4 h of reaction, all Sm2Zr2O7 powders were completely corroded. After 24 h of reaction, Sm-apatite disappeared, and the c-ZrO2 solid solution remained.


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Reaction products of Sm2Zr2O7 with calcium-magnesium-aluminum-silicate (CMAS) and their evolution

Show Author's information Yinghua WANGa,b, Zhuang MAa,b, Ling LIUa,b( ), Yanbo LIUa,b
School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
National Key Laboratory of Science and Technology on Materials under Shock and Impact, Beijing 100081, China

Abstract

During flight, many silicates (sand, dust, debris, fly ash, etc.) are ingested by an engine. They melt at high operating temperatures on the surface of thermal barrier coatings (TBCs) to form calcium-magnesium-aluminum-silicate (CMAS) amorphous settling. CMAS corrodes TBCs and causes many problems, such as composition segregation, degradation, cracking, and disbanding. As a new generation of TBC candidate materials, rare-earth zirconates (such as Sm2Zr2O7) have good CMAS resistance properties. The reaction products of Sm2Zr2O7 and CMAS and their subsequent changes were studied by the reaction of Sm2Zr2O7 and excess CMAS at 1350 ℃. After 1 h of reaction, Sm2Zr2O7 powders were not completely corroded. The reaction products were Sm-apatite and c-ZrO2 solid solution. After 4 h of reaction, all Sm2Zr2O7 powders were completely corroded. After 24 h of reaction, Sm-apatite disappeared, and the c-ZrO2 solid solution remained.

Keywords: corrosion, Sm2Zr2O7 ceramic, calcium-magnesium-aluminum-silicate (CMAS), reaction product

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Publication history

Received: 01 March 2021
Revised: 26 June 2021
Accepted: 06 July 2021
Published: 27 October 2021
Issue date: December 2021

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© The Author(s) 2021

Acknowledgements

This work was financially supported by the National Natural Science Foundation of China (No. 5177020526).

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