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Effect of TGO Thickness on the Lamellar Interface Cracking in Plasma-Sprayed 8YSZ

机译:TGO厚度对等离子体喷涂8倍的层状界面破裂的影响

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There are a large number of non-bonded interfaces between ceramic lamellas. The non-bonded interfaces are equivalent to precracks in YSZ, which propagate and coalesce during thermal cycling, leading to spallation of YSZ coating. The thickening of thermally grown oxide (TGO) is inevitable during the turbine operation. The finite element analyses (FEA) showed that the residual stress in thermal barrier coating (TBC) increases with growth of TGO thickness. Moreover, the stress distribution in TBC is significantly influenced by TGO thickness. The tensile stress is present at the peaks and compressive stress at the valleys with thin TGO, while the nature of the stresses in the YSZ undulation valley reverses from compression to tension with a thicker TGO. These changes of stress distribution must lead to transformation of cracking tendency and location. In this paper, the gas burners with flame were used to carry out the thermal cyclic test giving a rather homogeneous temperature distribution on the sample surfaces. The influence of TGO thickness on cracking mechanism of TBC system under gradient thermal cycling was examined.
机译:陶瓷薄片之间存在大量的非粘合界面。非粘结界面相当于YSZ中的预粘,其在热循环期间繁殖和聚结,导致YSZ涂层的椎间体。在涡轮机操作期间,热生长的氧化物(TGO)的增厚是不可避免的。有限元分析(FEA)表明,热阻挡涂层(TBC)中的残余应力随TGO厚度的生长而增加。此外,TBC中的应力分布受TGO厚度的显着影响。拉伸应力存在于具有薄TGO的山谷处的峰值和压缩应力,而YSZ波状谷的应力的性质从压力反转到厚度与较厚的TAG。这些压力分布的变化必须导致裂缝倾向和位置的转变。在本文中,使用具有火焰的燃气燃烧器来进行热循环试验,在样品表面上给出相当均匀的温度分布。检测TGA厚度对梯度热循环下TBC系统破裂机理的影响。

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