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Residual stresses and phase transformations in Ytterbium silicate environmental barrier coatings.

机译:硅酸Y环境隔离涂层中的残余应力和相变。

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摘要

Due to their high melting temperature, low density, and good thermomechanical stability, silicon-based ceramics (SiC, Si3N4) are some of the most promising materials systems for high temperature structural applications in gas turbine engines. However, their silica surface layer reacts with water vapor contained in combustion environments. The resulting hydroxide layer volatilizes, leading to component recession. Environmental barrier coatings (EBCs) have been developed to shield the substrate from degradation. Next generation coatings for silicon-based ceramics based on ytterbium silicates have shown a promising combination of very low and good thermomechanical properties. The focus of this thesis is threefold: In the first part, phase transformations in plasma sprayed ytterbium silicates were investigated. Plasma sprayed materials are known to contain large amounts of amorphous material. Phase changes during the conversion from amorphous to crystalline materials were investigated as they have been known to lead to failure in many coatings. The second part of this work focused on measuring residual stresses in multilayer EBCs using synchrotron X-ray diffraction (XRD). Strains were resolved spatially, with probe sizes as small as 20 um. Stresses were calculated using mechanical properties of ytterbium silicates, determined with in-situ loading and heating experiments. In-situ and ex-situ heating experiments allowed for the study of changes in stress states that occur in these EBC materials during heating and cooling cycles. Lastly, the interaction of ytterbium silicates with low-melting environmental calcium-magnesium-aluminosilicate (CMAS) glasses was studied. Synchrotron XRD was used to study the influence of CMAS on the stress state in the coating, X-ray computed tomography was used to provide 3D images of coatings, and EDS and TEM analysis were used to study the interactions at the CMAS/ytterbium silicate interface in detail.
机译:硅基陶瓷(SiC,Si3N4)由于具有高熔化温度,低密度和良好的热机械稳定性,因此是燃气涡轮发动机高温结构应用中最有希望的材料系统。但是,它们的二氧化硅表面层会与燃烧环境中包含的水蒸气发生反应。所得的氢氧化物层挥发,导致部件退缩。已经开发了环境屏障涂层(EBC),以保护基材免受降解。基于硅酸y的硅基陶瓷的下一代涂料已显示出非常低和良好的热机械性能的良好组合。本文的研究重点包括三个方面:第一部分,研究了等离子喷涂硅酸y的相变。已知等离子喷涂材料包含大量无定形材料。研究了从无定形到结晶材料转化过程中的相变,因为已知它们会导致许多涂层失效。这项工作的第二部分着重于使用同步加速器X射线衍射(XRD)测量多层EBC中的残余应力。菌株在空间上得到解析,探针尺寸小至20 um。使用硅酸的机械性能计算应力,并通过原位加载和加热实验确定。原位和异位加热实验允许研究这些EBC材料在加热和冷却周期中发生的应力状态变化。最后,研究了硅酸与低熔点环境钙镁铝硅酸盐(CMAS)玻璃的相互作用。使用Synchrotron XRD研究CMAS对涂层应力状态的影响,使用X射线计算机断层扫描提供涂层的3D图像,使用EDS和TEM分析研究CMAS /硅酸silicate界面的相互作用详细。

著录项

  • 作者

    Stolzenburg, Fabian.;

  • 作者单位

    Northwestern University.;

  • 授予单位 Northwestern University.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 202 p.
  • 总页数 202
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:41:23

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