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On thermal mismatch and thermal gradients and the failure of thermal barrier coatings.

机译:关于热失配和热梯度以及热障涂层的失效。

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摘要

Thermal barrier coatings (TBCs) are widely used in the hot sections of gas turbine engines to protect the underlying structure from the damaging high temperatures. Unfortunately, premature failures prevent the design engineers from taking full advantage of the coatings. The lack of understanding of the failures is due to the complex nature of the coating, which consists of three major layers: (i) a metallic bond coat deposited on the superalloy, (ii) a ceramic top coat deposited on the bond coat, and (iii) a thermally grown oxide (TGO) that forms between the bond coat and top coat as the coating is exposed to elevated temperatures. This work investigates one dominate mode of failures seen in TBCs, "morphological instabilities", in an effort to better understand the failures, potentially leading to improvement of the reliability of the coatings.; The development of morphological instability (sometimes referred to as "ratcheting") occurs in TBCs subjected to cyclic loading and is characterized by an amplitude growth of initial small imperfections in the TGO. In particular, we are interested in how thermo-mechanically induced stresses in the coating, along with eigen-strains such as phase transformations, influence the development of the instabilities.; Based on experimental observations (conducted by our collaborators), numerical models are developed, spanning a range of properties to establish criteria for morphological instabilities. A key feature of the numerical models is to accurately capture the oxidation mechanisms of the TGO formation. Material changes in a Pt-modified aluminide bond coat, such as martensitic transformation and the change from beta- to gamma'-grains, are also important to incorporate. In addition, thermo-mechanical testing of systems containing NiCoCrAlY bond coats resulted in the development of morphological instabilities depending on the combination of thermal gradient over the structure. Thus, it is important to correctly simulate thermal gradients over the coating if gradients were present in the experiments.; The key results from the numerical simulations show that when the thermal mismatch is large enough to cause overall yielding in the bond coat, the thermal expansion of the substrate (superalloy) will govern the system response. It is furthermore seen that eigen-strain introduced by phase transformations may enhance or suppress the instability growth, depending on the class of phase transformation. Lastly, the numerical simulations capture the morphological instabilities seen in the experimental investigations of the NiCoCrAlY In this case, the morphological instabilities develop during thermal cycling with a thermal gradient over the cylinder wall, whereas the surface remains smooth for thermal cyclic conditions without a gradient. If an axial force is applied, the morphological instabilities become aligned with the axial direction.
机译:隔热涂层(TBC)广泛用于燃气涡轮发动机的高温区域,以保护基础结构免受高温破坏。不幸的是,过早的故障使设计工程师无法充分利用涂层。对失败的理解不足是由于涂层的复杂性,它由三个主要层组成:(i)沉积在高温合金上的金属粘结层,(ii)沉积在粘结层上的陶瓷面涂层,以及(iii)当涂层暴露于高温下时,在粘合涂层和面涂层之间形成的热生长氧化物(TGO)。这项工作研究了在TBC中看到的一种主要的失效模式,即“形态不稳定性”,目的是为了更好地理解这些失效,从而潜在地改善涂层的可靠性。形态不稳定性的发展(有时称为“棘齿”)发生在承受循环载荷的TBC中,其特征是TGO中初始小缺陷的幅度增长。特别是,我们对涂层中热机械感应的应力以及诸如相变之类的本征应变如何影响不稳定性的发展感兴趣。根据实验观察结果(由我们的合作者进行),开发了数值模型,涵盖了一系列特性,以建立形态不稳定的标准。数值模型的关键特征是准确捕获TGO形成的氧化机理。结合Pt改性的铝化物键合涂层的材料变化,例如马氏体相变以及从β-晶粒到γ'晶粒的变化,也很重要。此外,对包含NiCoCrAlY粘结涂层的系统进行热机械测试会导致结构不稳定性的发展,具体取决于结构上热梯度的组合。因此,如果实验中存在梯度,则正确模拟涂层上的热梯度非常重要。数值模拟的关键结果表明,当热失配足够大以致导致粘结涂层的整体屈服时,基材(超合金)的热膨胀将决定系统的响应。此外还可以看出,取决于相变的类型,相变引入的本征应变可以增强或抑制不稳定性的增长。最后,数值模拟捕获了在NiCoCrAlY的实验研究中看到的形态不稳定性。在这种情况下,形态不稳定性在热循环过程中随着汽缸壁上的温度梯度而发展,而表面在没有梯度的热循环条件下仍保持光滑。如果施加轴向力,形态不稳定性变得与轴向方向对准。

著录项

  • 作者

    Shi, Jun.;

  • 作者单位

    University of Delaware.;

  • 授予单位 University of Delaware.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 123 p.
  • 总页数 123
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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