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Thermal Shock Resistance of APS 8YSZ Thermal Barrier Coatings on Titanium Alloy

机译:钛合金上APS 8YSZ热障涂层的抗热震性

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Thermal barrier coatings (TBCs) with a typical 8YSZ ceramic top coat and CoNiCrAlY bond coat were deposited on titanium alloy substrate (Ti-6Al-4V in wt.%) by air plasma spraying. Thermal insulation and thermal shock resistance of the TBCs at different temperatures as well as their failure behavior were investigated. The results showed that the test temperature had a significant effect on thermal shock life of the TBCs. Failure of the TBCs systems was caused by the formation of crack, bond coat oxidation and elemental diffusion. The vertical cracks induced by thermal shock cycles were probably responsible for the enhancement in thermal shock resistance of the TBCs. Furthermore, elemental diffusion had a great effect on the acceleration of the TBCs failure. The TBCs could provide a good thermal protection for the titanium alloy substrate.
机译:通过空气等离子喷涂将具有典型的8YSZ陶瓷面涂层和CoNiCrAlY粘结涂层的热障涂层(TBC)沉积在钛合金基材(Ti-6Al-4V的重量百分比)上。研究了TBC在不同温度下的隔热性和抗热震性及其破坏行为。结果表明,测试温度对TBC的热冲击寿命有显着影响。 TBCs系统的故障是由裂纹的形成,粘结层的氧化和元素的扩散引起的。由热冲击循环引起的垂直裂纹可能是TBC的抗热冲击性增强的原因。此外,元素扩散对TBC破坏的加速有很大影响。 TBC可以为钛合金基底提供良好的热保护。

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