无机材料学报

• 研究论文 •    

高熵稀土硅酸盐环境障涂层的界面调控与高温燃气热循环性能

张宇嘉, 吴珂珂, 郭凌翔, 欧鸿康, 张硕, 孙佳   

  1. 西北工业大学 超高温结构复合材料国防科技重点实验室,纤维增强轻质复合材料陕西省重点实验室,西安 710072
  • 收稿日期:2026-05-29 修回日期:2026-09-15
  • 通讯作者: 孙 佳, 研究员. E-mail: j.sun@nwpu.edu.cn
  • 作者简介:张宇嘉(2001-), 男, 博士研究生. E-mail: 1074994320@mail.nwpu.edu.cn
  • 基金资助:
    国防基础科研项目(JCKY2022607C007); 国家重点研发计划(2022YFB3708600)

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)

摘要: 新一代航空发动机热端部件服役环境日益严苛,对C/C复合材料表面环境障涂层的高温相稳定性、界面结合可靠性及热循环寿命提出更高要求。针对高熵稀土硅酸盐涂层与C/C基体间热膨胀失配及界面氧化易导致早期剥落的问题,本工作制备了(Tm0.2Yb0.2Er0.2Lu0.2Ho0.2)2SiO5(简称(5RE0.2)2SiO5)高熵稀土硅酸盐粉体,并结合包埋固渗和超音速大气等离子喷涂技术,分别制备(5RE0.2)2SiO5和(5RE0.2)2SiO5-SiC两种涂层体系,探究SiC黏结层对涂层相结构、界面反应及1400 ℃燃气热循环性能的影响。结果表明,(5RE0.2)2SiO5粉体保持稳定的单斜RE2SiO5固溶体结构,五种稀土元素分布均匀;喷涂后涂层厚度约为(230±5) μm,快速熔融-凝固过程诱导涂层发生部分非晶化并生成质量分数约5.88%的(5RE0.2)2O3相。未引入黏结层的(5RE0.2)2SiO5涂层在1400 ℃热循环6次后大面积剥落,(5RE0.2)2O3含量升至12.01%,其失效主要归因于贯穿裂纹加速氧气与水蒸气向界面扩散,诱发C、Si及SiC氧化,削弱界面结合。相比之下,带有SiC黏结层的(5RE0.2)2SiO5-SiC涂层经100次热循环后仍保持结构完整。SiC黏结层优异的界面调控作用源于其粗糙结构形成的机械咬合,以及热循环中SiC氧化生成的SiO2与(5RE0.2)2SiO5原位反应生成(5RE0.2)2Si2O7过渡相,从而构筑成分连续、热膨胀匹配更优的梯度界面,有效抑制贯穿裂纹扩展和界面氧化损伤。

关键词: 高熵稀土硅酸盐, 环境障涂层, 热喷涂, 燃气热循环, C/C复合材料

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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