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Thermophysical properties and CMAS corrosion resistance of a novel high-entropy RE monosilicate as T/EBC materials

  • Qungong He
  • , Qiongyuan Zhang
  • , Chao Wang*
  • , Yu Huang
  • , Bing He
  • , Haiyang Wang
  • , Yusheng Wu*
  • *Corresponding author for this work
  • State Key Laboratory of Clean and Efficient Turbomachinery Power Equipment
  • LTD
  • Shenyang University of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

High-entropy design is an attractive strategy to improve the comprehensive performances of RE2SiO5 as next-generation thermal/environmental barrier coating (T/EBC) materials for protecting SiC-based ceramic composites (SiC-CMCs) in the hot section of gas turbine engines. Herein, we designed a novel high-entropy RE monosilicate ((6RE1/6)2SiO5) by co-doping the Sc, Yb, Tm, Er, Y, and Dy elements to synergistically improve thermophysical properties and molten calcium–magnesium–alumina–silicate (CMAS) corrosion resistance. The results revealed that as-prepared (6RE1/6)2SiO5 had an ultra-low thermal conductivity (1.22–1.74 W·m−1·K−1), and a matched coefficient of thermal expansion ((4.57–5.05) × 10−6 K−1) with SiC-CMCs in the testing temperature range. Moreover, it showed an excellent ability against CMAS corrosion at 1300°C and 1500°C. The thicknesses of reaction product layer were about 44 and 102 µm after CMAS corrosion at 1300°C for 48 h and 1500°C for 24 h, respectively. All of the above results identify that as-prepared (6RE1/6)2SiO5 will be a suitable candidate as next-generation T/EBC for protecting SiC-CMCs.

Original languageEnglish
Article numbere15147
JournalInternational Journal of Applied Ceramic Technology
Volume22
Issue number4
DOIs
StatePublished - 1 Jul 2025
Externally publishedYes

Keywords

  • CMAS corrosion resistance
  • high-entropy RE monosilicate
  • microstructure
  • thermophysical properties

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