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Evolution of Lamellar Interface Cracks during Isothermal Cyclic Test of Plasma-Sprayed 8YSZ coating with a columnar structured YSZ interlayer

机译:等离子喷涂8苏斯涂层等温循环试验过程中裂纹裂缝的演变,用柱状结构性ysz中间层

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The failure of plasma-sprayed thermal barrier coatings (TBC) usually occurs through spalling of ceramic coating. The cracking of YSZ coating parallel to the interface between the bond coat and YSZ during thermal cycling of TBC is primary cause to lead to spalling YSZ coating. With plasma-sprayed YSZ coating with substantial non-bonded lamellar interfaces which are regarded as precracks uniformly distributed in the coating, although it is known that the fracture toughness is proportional to lamellar bonding ratio, it was still not well known how the cracking along lamellar interface occurs during thermal cycles and its relation to failure of coating. Moreover, there was no data which directly relate the cracks in the coating to the lamellar bonding. In this study, the cracks in YSZ coatings were examined after YSZ coatings were subjected to different isothermal cycles till failure of TBC to examine how the cracking is associated to the thermal cycles and failure of TBCs.
机译:等离子体喷涂的热阻挡涂层(TBC)的失效通常通过陶瓷涂层剥落来进行。在TBC热循环期间平行于粘合涂层和YSZ之间的界面的ysz涂层的破裂是主要的原因,以导致剥落的YSZ涂层。具有等离子体喷涂的YSZ涂层,其具有基本的非粘合层状界面,其被认为是均匀分布在涂层中的预粘性的预粘性,但是已知断裂韧性与层状粘合率成比例,仍然没有众所周知的是沿层状裂缝的开裂界面在热循环期间发生及其与涂层失效的关系。此外,没有任何数据,其直接将涂层中的裂缝与层状粘合剂相关联。在这项研究中,在将YSZ涂层进行不同的等温循环后检查YSZ涂层的裂缝直至TBC失效,以检查裂缝如何与TBC的热循环相关。

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