无机材料学报 ›› 2026, Vol. 41 ›› Issue (7): 923-929.DOI: 10.15541/jim20250452

• 研究论文 • 上一篇    下一篇

Al表面改性Si-HfO2/YbDS/GYYZO热/环境障涂层的抗CMAS腐蚀性能

商森1,2(), 姜林文1(), 董浩2, 戴睿2, 吴健2, 卓学士2, 张军贵2, 张小锋2()   

  1. 1 宁波大学 材料科学与化学工程学院, 宁波 315000
    2 广东省科学院 新材料研究所, 现代材料表面工程技术国家工程实验室, 广东省现代表面工程技术重点实验室, 广州 510650
  • 收稿日期:2025-11-09 修回日期:2026-01-19 出版日期:2026-02-05 网络出版日期:2026-02-05
  • 通讯作者: 姜林文, 副教授. E-mail: jianglinwen@nbu.edu.cn;
    张小锋, 正高级工程师. E-mail: zxf200808@126.com
  • 作者简介:商 森(2000-), 男, 硕士研究生. E-mail:2356800464@qq.com
  • 基金资助:
    四川省科技计划(2025ZDZX0003)

CMAS Corrosion Resistance of Al-modified Si-HfO2/YbDS/GYYZO Thermal/Environmental Barrier Coating

SHANG Sen1,2(), JIANG Linwen1(), DONG Hao2, DAI Rui2, WU Jian2, ZHUO Xueshi2, ZHANG Jungui2, ZHANG Xiaofeng2()   

  1. 1 College of Materials Science and Chemical Engineering, Ningbo University, Ningbo 315000, China
    2 Guangdong Provincial Key Laboratory of Modern Surface Engineering Technology, National Engineering Laboratory for Modern Materials Surface Engineering Technology, Institute of New Materials, Guangdong Academy of Sciences, Guangzhou 510650, China
  • Received:2025-11-09 Revised:2026-01-19 Published:2026-02-05 Online:2026-02-05
  • Contact: JIANG Linwen, associate professor. E-mail: jianglinwen@nbu.edu.cn;
    ZHANG Xiaofeng, professor. E-mail: zxf200808@126.com
  • About author:SHANG Sen (2000-), male, Master candidate. E-mail: 2356800464@qq.com
  • Supported by:
    Sichuan Science and Technology Program(2025ZDZX0003)

摘要:

随着航空发动机热端部件服役温度的提升, 钙镁铝硅酸盐(CMAS)腐蚀已成为热/环境障涂层(T/EBCs)失效的关键因素。新型Gd2O3-Yb2O3-Y2O3共稳ZrO2 (GYYZO)陶瓷因其优异的热物理性能而颇具应用前景, 但在1500 ℃极端高温下, 其抗CMAS腐蚀性能仍需进一步提高。本研究采用表面镀铝+真空热处理方法对等离子喷涂-物理气相沉积(Plasma spray-physical vapor deposition, PS-PVD)制备的Si-HfO2/Yb2Si2O7/GYYZO涂层体系进行表面改性。首先, 对PS-PVD制备的涂层进行1300 ℃退火处理, 愈合微裂纹; 随后, 利用直流脉冲磁控溅射技术在GYYZO层表面沉积厚度为3~4 μm的铝薄膜; 最后, 通过真空热处理(400 ℃/2.5 h + 660 ℃/2 h + 808 ℃/1.5 h + 980 ℃/1 h)使铝层转化为致密的Al2O3阻挡层。系统研究了改性前后涂层在1500 ℃下的CMAS腐蚀演变行为及失效机理。结果表明, 在1500 ℃下, CMAS熔体通过晶界快速渗透至未改性GYYZO涂层内部, 诱使Yb2Si2O7层产生“起泡”损伤及大量裂纹, 最终导致涂层加速失效。与之相比, 经铝改性技术处理后的GYYZO涂层, 得益于表面原位生成的致密Al2O3阻挡层, 可有效抑制CMAS的晶界渗透, 从而延缓腐蚀动力学进程。在腐蚀1 h后, 改性涂层仍能保持结构完整性。

关键词: 热/环境障涂层, CMAS腐蚀, 铝改性, GYYZO

Abstract:

The rising service temperature of aero-engine hot-section components makes calcium magnesium aluminum silicate (CMAS) corrosion a key failure mechanism for thermal/environmental barrier coatings (T/EBCs). The novel Gd2O3-Yb2O3-Y2O3 co-stabilized ZrO2 (GYYZO) ceramic is promising due to its good thermophysical properties. However, its CMAS corrosion resistance at 1500 ℃ needs improvement. In this work, a PS-PVD- fabricated Si-HfO2/Yb2Si2O7/GYYZO coating system was enhanced via Al deposition and vacuum heat treatment. Firstly, the as-sprayed coating was annealed at 1300 ℃ to heal microcracks. Subsequently, a 3-4 μm thick aluminum film was deposited on the GYYZO layer surface via direct current pulsed magnetron sputtering. Finally, vacuum heat treatment (400 ℃/2.5 h + 660 ℃/2 h + 808 ℃/1.5 h + 980 ℃/1 h) was conducted to promote the formation of a dense Al2O3 barrier layer. A comparative study at 1500 ℃ revealed that CMAS rapidly penetrated the unmodified GYYZO coating along grain boundaries, causing blistering and cracking in the Yb2Si2O7 layer and accelerating failure. Conversely, the Al-modified GYYZO coating formed a dense Al2O3 barrier in situ, effectively suppressing CMAS penetration and slowing corrosion kinetics, thus maintaining structural integrity after 1 h.

Key words: thermal/environmental barrier coating, CMAS corrosion, aluminum modification, GYYZO

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