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Thermal Fatigue Damage Evaluation of EB-PVD TBC Specimens: Its Potential and Problems

机译:EB-PVD TBC样品的热疲劳损伤评估:潜力和问题

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Thermal fatigue damage evolution behavior in thermal barrier coatings (TBCs) was studied, by employing the originally designed two dimensional ring-shape TBC specimen. The TBC specimen consisted of Ni-based superalloy IN738LC substrate, bond coat, and 8 wt.% Y_2O_3-stabilized ZrO_2 (YSZ) top coat. The top coat was fabricated by electron-beam physical vapor deposition (EB-PVD) method with 250 micron-meters in thickness. Three kinds of MCrAlY bond coat alloys were specified as an experimental variable. Through the work, special attention was paid not only to the failure life of TBC specimen, but also to the underlying failure mechanisms. Some problems have been also pointed out, on feeding back these experimental findings to engineering applications.
机译:通过使用最初设计的二维环形TBC样品,研究了热障涂层(TBC)中的热疲劳损伤演化行为。 TBC样品由Ni基高温合金IN738LC基底,粘结涂层和8 wt%的Y_2O_3稳定的ZrO_2(YSZ)面涂层组成。通过电子束物理气相沉积(EB-PVD)方法制造面涂层,其厚度为250微米。指定了三种MCrAlY粘结涂层合金作为实验变量。通过这项工作,不仅要特别注意TBC标本的失效寿命,还要特别注意其潜在的失效机理。在将这些实验结果反馈给工程应用时,还指出了一些问题。

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