无机材料学报 ›› 2019, Vol. 34 ›› Issue (4): 394-400.DOI: 10.15541/jim20180276

• 研究论文 • 上一篇    下一篇

单相双稀土改性SrZrO3热障涂层的热物理性能

马伯乐1,2,马文1,2(),黄威1,2,白玉1,2,贾瑞灵1,2,董红英2,3   

  1. 1. 内蒙古工业大学 材料科学与工程学院, 呼和浩特 010051
    2. 内蒙古自治区薄膜与涂层重点实验室, 呼和浩特 010051
    3. 内蒙古工业大学 化工学院, 呼和浩特 010051
  • 收稿日期:2018-06-22 修回日期:2018-08-29 出版日期:2019-04-20 网络出版日期:2019-04-15
  • 作者简介:马伯乐(1993-), 男, 硕士研究生. E-mail:995375781@qq.com
  • 基金资助:
    国家自然科学基金(51462026);国家自然科学基金(51672136);内蒙古自然科学基金(2017MS0503)

Thermophysical Property of Single-phase Strontium Zirconate Co-doped with Double Rare-earth Oxides as a Thermal Barrier Coating Material

Bo-Le MA1,2,Wen MA1,2(),Wei HUANG1,2,Yu BAI1,2,Rui-Ling JIA1,2,Hong-Ying DONG2,3   

  1. 1. School of Materials Science and Engineering, Inner Mongolia University of Technology, Hohhot 010051, China
    2. Inner Mongolia Key Laboratory of Thin Film and Coatings Technology, Hohhot 010051, China
    3. School of Chemical Engineering, Inner Mongolia University of Technology, Hohhot 010051, China
  • Received:2018-06-22 Revised:2018-08-29 Published:2019-04-20 Online:2019-04-15
  • Supported by:
    National Natural Science Foundation of China(51462026);National Natural Science Foundation of China(51672136);Natural Science Foundation of Inner Mongolia(2017MS0503)

摘要:

由于SrO和ZrO2的蒸气压不同, 造成等离子喷涂SrZrO3涂层组分偏离原始粉末化学计量比, 从而导致制备态涂层中出现第二相ZrO2。为了获得高相稳定性的单相涂层, 实验采用固相合成法合成并经过喷雾造粒制备了双稀土改性Sr过量SrZrO3(Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05)热喷涂粉末, 采用大气等离子喷涂方法制备了相应的涂层, 研究了单相双稀土改性SrZrO3热障涂层的热物理性能及其热循环寿命。研究结果表明, 制备态Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05涂层中无第二相产生, 1600 ℃热处理360 h后Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05保持单相SrZrO3结构, 高温相稳定性良好。Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05涂层的烧结系数为7.27×10 -6 s -1, 热处理360 h后该涂层的热膨胀系数为(9.0~11.0)×10 -6 K -1 (200~1400 ℃), 热导率为2.83 W/(m?K) (1000 ℃)。Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05/YSZ双层涂层的火焰循环次数为1000次, 失效区域主要发生在Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05陶瓷层内。在喷涂粉末中增加SrO的含量能够弥补在大气等离子喷涂过程中Sr元素过量挥发的问题, 成功制备了单相双稀土改性Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05热障涂层。双稀土掺杂能够明显提高涂层的热膨胀系数, 且单相双稀土改性Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05涂层的抗烧结性能明显优于SrZrO3涂层, 但单相Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05涂层热导率比含有第二相的SrZrO3涂层高。

关键词: 热障涂层, SrZrO3, 热膨胀, 热导率

Abstract:

Due to the different vapor pressures between SrO and ZrO2, composition of air plasma sprayed (APS) SrZrO3 coating deviates from stoichiometric SrZrO3, resulting in formation of second phase ZrO2 in the as-sprayed SrZrO3 coating. To obtain single-phase coating with high phase stability, the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 powder with excess Sr was synthesized by solid state reaction and spray drying, followed by air plasma spray to obtain the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating. Thermo-physical properties and thermal cycling behavior of the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating were investigated. Experimental results showed that the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating had no second phase and showed a good high-temperature phase stability after heat- treatment at 1600 ℃ for 360 h. The sintering rate of the as-sprayed Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating was 7.27×10 -6 s -1. Thermal expansion coefficients (TECs) and thermal conductivity of the coating after heat-treatment at 1600 ℃ for 360 h were (9.0-11.0)×10 -6 K -1 (200-1400 ℃) and 2.83 W/(m?K) (1000 ℃), respectively. Thermal cycling lifetime of the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05/YSZ double ceramic layer coating was 1000 cycles, due to failure occurring in the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating. Moreover, singe-phase Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating with SrZrO3 structure could be prepared by adding excess SrO in the feedstock, which showed higher TEC by co-dopping with Yb2O3 and Gd2O3 and sintering resistance than did the SrZrO3 coating. However, the thermal conductivity of the Sr1.1(Zr0.9Yb0.05Gd0.05)O3.05 coating is higher than that of the SrZrO3 coating because of the absence of the second phase.

Key words: thermal barrier coating, SrZrO3, thermal expansion, thermal conductivity

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