首页> 外文期刊>Applied Surface Science >Double-ceramic-layer thermal barrier coatings based on La_2(Zr_(0.7)Ce_(0.3))_2O_7/La_2Ce_2O_7 deposited by electron beam-physical vapor deposition
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Double-ceramic-layer thermal barrier coatings based on La_2(Zr_(0.7)Ce_(0.3))_2O_7/La_2Ce_2O_7 deposited by electron beam-physical vapor deposition

机译:电子束-物理气相沉积La_2(Zr_(0.7)Ce_(0.3))_ 2O_7 / La_2Ce_2O_7双层陶瓷隔热涂层

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摘要

Double-ceramic-layer (DCL) thermal barrier coatings (TBCs) of La_2(Zr_(0.7)Ce_(0.3))_2O_7 (LZ7C3) and La_2Ce_2O_7 (LC) were deposited by electron beam-physical vapor deposition (EB-PVD). The composition, interdiffusion, surface and cross-sectional morphologies, cyclic oxidation behavior of DCL coating were studied. Energy dispersive spectroscopy and X-ray diffraction analyses indicate that both LZ7C3 and LC coatings are effectively fabricated by a single LZ7C3 ingot with properly controlling the deposition energy. The chemical compatibility of LC coating and thermally grown oxide (TGO) layer is unstable. LaAlO_3 is formed due to the chemical reaction between LC and Al_2O_3 which is the main composition of TGO layer. Additionally, the thermal cycling behavior of DCL coating is influenced by the interdiffusion of Zr and Ce between LZ7C3 and LC coatings. The failure of DCL coating is a result of the sintering of LZ7C3 coating surface, the chemical incompatibility of LC coating and TGO layer and the abnormal oxidation of bond coat. Since no single material that has been studied so far satisfies all the requirements for high temperature applications, DCL coating is an important development direction of TBCs.
机译:通过电子束物理气相沉积(EB-PVD)沉积La_2(Zr_(0.7)Ce_(0.3))_ 2O_7(LZ7C3)和La_2Ce_2O_7(LC)的双层陶瓷(DCL)隔热涂层(TBC)。研究了DCL涂层的组成,相互扩散,表面和截面形貌,循环氧化行为。能量色散光谱法和X射线衍射分析表明,LZ7C3和LC涂层均由单个LZ7C3铸锭有效地制造,并能适当控制沉积能量。 LC涂层和热生长氧化物(TGO)层的化学相容性不稳定。 LaAlO_3是由于LC和作为TGO层主要成分的Al_2O_3之间的化学反应而形成的。此外,DCL涂层的热循环行为受LZ7C3和LC涂层之间Zr和Ce相互扩散的影响。 DCL涂层的失败是由于LZ7C3涂层表面的烧结,LC涂层和TGO层的化学不相容性以及粘结涂层的异常氧化所致。由于到目前为止,还没有一种材料能够满足高温应用的所有要求,因此DCL涂层是TBC的重要发展方向。

著录项

  • 来源
    《Applied Surface Science》 |2010年第11期|3661-3668|共8页
  • 作者单位

    Beijing Institute of Aeronautical Materials, Department 5, P.O. Box 81-5, Beijing 100095, China State Key Laboratory of Rare Earth Resource Utilization, Changchun Institute of Applied Chemistry, Chinese Academy of Sciences, Changchun 130022, China Graduate School of Chinese Academy of Sciences, Beijing 100039, China;

    rnBeijing Institute of Aeronautical Materials, Department 5, P.O. Box 81-5, Beijing 100095, China;

    rnBeijing Institute of Aeronautical Materials, Department 5, P.O. Box 81-5, Beijing 100095, China;

    rnBeijing Institute of Aeronautical Materials, Department 5, P.O. Box 81-5, Beijing 100095, China;

    rnBeijing Institute of Aeronautical Materials, Department 5, P.O. Box 81-5, Beijing 100095, China;

    rnState Key Laboratory of Rare Earth Resource Utilization, Changchun Institute of Applied Chemistry, Chinese Academy of Sciences, Changchun 130022, China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    thermal barrier coatings; EB-PVD; double-ceramic-layer; La_2(Zr_(0.7)Ce_(0.3))_2O_7; La_2Ce_2O_7; thermal cycling;

    机译:隔热涂层;EB-PVD;双陶瓷层La_2(Zr_(0.7)Ce_(0.3))_ 2O_7;La_2Ce_2O_7;热循环;

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