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Tantalum oxide-based plasma-sprayed environmental barrier coatings.

机译:基于氧化钽的等离子喷涂环境屏障涂料。

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摘要

Energy efficiency in gas turbine engines is linked to the high temperature capabilities of materials used in the hot section of the engine. To facilitate a significant increase in engine efficiency, tough structural ceramics have been developed that can handle the thermo-mechanical stresses that gas turbine components experience. Unfortunately, the high-temperature, high-pressure, and high-velocity combustion gases in a gas turbine contain water vapor and/or hydrogen which have been shown to volatilize the protective silica layer on silicon-based ceramics. This degradation leads to significant surface recession in ceramic gas turbine components.; In order to maintain their structural integrity, an environmental barrier coating (EBC) could be used to protect ceramics from the harsh gas turbine environment. Due to its coefficient of thermal expansion and phase stability at elevated temperatures, tantalum oxide (Ta2O5) was examined as the base material for an air plasma-sprayed EBC on Si3N 4 ceramics. As-sprayed pure Ta2O5 was comprised of both low-temperature beta-Ta2O5 and high-temperature alpha-Ta 2O5 that was quenched into the structure. Residual stress measurements via X-ray diffraction determined the as-sprayed coating to be in tension and extensive vertical macrocracks were observed in the coating. Heat treatments of the pure coating led to conversion of alpha-Ta2 O5 to beta-Ta2O5, conversion of tensile stresses to compressive, localized buckling of the coating, and significant grain growth which caused microcracking in the coating. The pure coating was found to be an inadequate EBC.; Al2O3 was investigated as a solid solution alloying addition designed to enhance the stability of beta-Ta2O 5, and reduce grain growth by slowing grain boundary diffusion. La 2O3 was investigated as an alloying addition designed to form second phase particles which would reduce grain growth through pinning. Al2O3 was successful at both stabilizing beta-Ta 2O5 and reducing grain growth, though AlTaO4 was found to form in the coatings. La2O3 additions led to the formation of LaTa7O19 which also contributed to grain growth reduction. Residual stresses in the alloyed coatings were generally found to be tensile. Microcracks were not observed in coatings that were alloyed with both Al2O3 and La2O3 with the most promising alloy being Ta2O5 + 1.5 wt.% Al 2O3 + 1.5 wt.% La2O3.
机译:燃气涡轮发动机的能效与发动机高温部分所用材料的高温性能有关。为了促进发动机效率的显着提高,已开发出坚韧的结构陶瓷,可以处理燃气轮机部件遇到的热机械应力。不幸的是,燃气轮机中的高温,高压和高速燃烧气体包含水蒸气和/或氢,业已证明它们会挥发掉硅基陶瓷上的保护性二氧化硅层。这种退化导致陶瓷燃气轮机部件明显的表面凹陷。为了保持其结构完整性,可以使用环境屏障涂层(EBC)保护陶瓷免受恶劣的燃气轮机环境的影响。由于其热膨胀系数和在高温下的相稳定性,因此已研究了氧化钽(Ta2O5)作为在Si3N 4陶瓷上进行空气等离子喷涂EBC的基础材料。喷涂后的纯Ta2O5由低温β-Ta2O5和高温α-Ta2O5组成,后者经过淬火后进入结构。通过X射线衍射的残余应力测量结果确定了喷涂后的涂层处于拉伸状态,并且在涂层中观察到了广泛的垂直大裂纹。纯涂层的热处理导致α-Ta2O5转化为β-Ta2O5,拉伸应力转化为压缩,涂层局部屈曲,以及明显的晶粒长大,导致涂层中的微裂纹。发现纯涂层是不适当的EBC。研究了Al2O3作为固溶合金添加剂,旨在增强β-Ta2O5的稳定性,并通过减缓晶界扩散来降低晶粒长大。对La 2O3进行了合金化添加研究,旨在形成第二相颗粒,该第二相颗粒将通过钉扎减少晶粒的生长。尽管发现涂层中形成了AlTaO4,但Al2O3在稳定β-Ta2O5和减少晶粒长大方面均成功。 La2O3的添加导致形成LaTa7O19,这也有助于减少晶粒长大。通常发现合金涂层中的残余应力为拉伸应力。在与Al2O3和La2O3合金化的涂层中未观察到微裂纹,最有希望的合金是Ta2O5 + 1.5 wt。%Al 2O3 + 1.5 wt。%La2O3。

著录项

  • 作者

    Weyant, Christopher M.;

  • 作者单位

    Northwestern University.;

  • 授予单位 Northwestern University.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2004
  • 页码 198 p.
  • 总页数 198
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;
  • 关键词

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