Journal of Inorganic Materials

   

Interfacial Regulation and High-temperature Combustion-gas Thermal-cycling Performance of High-entropy Rare-earth Silicate Environmental Barrier Coatings

ZHANG Yujia, WU Keke, GUO Lingxiang, OU Hongkang, ZHANG Shuo, SUN Jia   

  1. State Key Laboratory of Ultra High Temperature Composite Materials, Shaanxi Key Laboratory of Fiber Reinforced Light Composite Materials, Northwestern Polytechnical University, Xi’an 710072, China
  • Received:2026-05-29 Revised:2026-09-15
  • Contact: SUN Jia, professor. E-mail: j.sun@nwpu.edu.cn
  • About author:ZHANG Yujia (2001-), male, PhD candidate. E-mail: 1074994320@mail.nwpu.edu.cn
  • Supported by:
    National Defense Basic Scientific Research Program of China (JCKY2022607C007); National Key R&D Program of China(2022YFB3708600)

Abstract: Environmental barrier coatings (EBCs) for C/C-based hot-section components must retain phase stability and interfacial integrity under severe thermal cycling. However, thermal-expansion mismatch and interfacial oxidation can lead to premature spallation of high-entropy rare-earth silicate coatings. Here, (Tm0.2Yb0.2Er0.2Lu0.2Ho0.2)2SiO5, denoted as (5RE0.2)2SiO5, powder was synthesized, and (5RE0.2)2SiO5 and (5RE0.2)2SiO5-SiC coating systems were fabricated by combining pack cementation with supersonic atmospheric plasma spraying. The synthesized powder formed a stable monoclinic (5RE0.2)2SiO5-type solid solution with a homogeneous distribution of the five rare-earth elements. The approximately (230 ± 5) μm-thick sprayed coating was partially amorphized and contained 5.88%(in mass) (5RE0.2)2SiO5 owing to rapid melting and solidification. Without the SiC bond coat, the coating spalled extensively after only six burner-rig thermal cycles at 1400 °C, accompanied by an increase in the (5RE0.2)2O3 content to 12.01%. Through-thickness cracks accelerated the transport of oxygen and steam to the interface, promoting the oxidation of C, Si and SiC and weakening interfacial bonding. By contrast, the SiC-bonded coating remained macroscopically intact after 100 cycles. The rough SiC surface provided mechanical interlocking, while oxidation-derived SiO2 reacted in situ with (5RE0.2)2SiO5 to form a (5RE0.2)2Si2O7 transition phase. The resulting compositionally graded reaction zone improved thermal-expansion compatibility near the SiC interface and suppressed crack penetration and interfacial oxidation, thereby markedly extending the thermal-cycling lifetime.

Key words: high-entropy rare-earth silicate, environmental barrier coating, thermal spraying, combustion-gas thermal cycling, C/C composites

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