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Microstructure and thermal cyclic performance of laser-glazed plasma-sprayed ceria-yttria-stabilized zirconia thermal barrier coatings

机译:激光玻璃等离子体喷涂氧化铈-氧化钇稳定的氧化锆热障涂层的组织和热循环性能

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In this study, substrates of Hastelloy-X superalloy coupons were first sprayed with a Ni-22Cr-10Al-1Y bond coat and then with a ceria-yttria-stabilized zirconia (CYSZ) top coat by air plasma spraying (APS). After that, the plasma-sprayed ceria-yttria-stabilized zirconia thermal barrier coatings (TBCs) were glazed using a pulsed CO2 laser. The effects of laser-glazing on the microstructure and cyclic oxidation behavior of the coatings were evaluated. The microstructures of both the as-processed and the tested TBCs were investigated by using optic microscopy (OM), scanning electron microscopy (SEM) and electron probe microanalysis (EPMA). The phases of the coatings were measured with X-ray diffractometry (XRD). An investigation of microstructure revealed that both plasma-sprayed and laser-glazed top coatings consisted of nonequibrium tetragonal (T) phase, cubic (C) phase and minor amount of Ce0.75Zr0.25O2 phase. Minor amount of monoclinic (M) phase found in plasma-sprayed coatings disappeared after laser-glazing. The phase analysis of tested top coat indicated that the mole% of tetragonal (T) phase decreased and that of Ce0.75Zr0.25O2 phase increased after thermal cycling for both sprayed and glazed samples. It was also found that the monoclinic phase in the plasma-sprayed sample disappeared after thermal cycling. Results showed that laser-glazing did not have a substantial effect on reducing the oxidation rate of the bond coat. Cyclic test results showed that the life times of the plasma-sprayed TBCs were enhanced about twofold by laser-glazing for initial spallation life. With regard to 50% spallation life, the laser-glazed samples exhibited about a half lifetime improvement relative to the plasma-sprayed samples. Failure of the TBCs was initiated within the top coat near the bond coat valley region and propagated mainly within the top coat and the out-growth oxide near the top coat-bond coat interface. Segmented cracks produced by laser-glazing improved the strain accommodation ability of top coat and could be identified as the major enhancement mechanism for TBC life extension.
机译:在这项研究中,Hastelloy-X超级合金试样的基材首先通过空气等离子体喷涂(APS)喷涂Ni-22Cr-10Al-1Y键合涂层,然后喷涂氧化铈-氧化钇稳定的氧化锆(CYSZ)面涂层。之后,使用脉冲CO2激光对等离子喷涂的氧化铈-氧化钇稳定的氧化锆隔热层(TBC)进行上光。评估了激光抛光对涂层的微观结构和循环氧化行为的影响。通过使用光学显微镜(OM),扫描电子显微镜(SEM)和电子探针显微分析(EPMA)研究了已加工和已测试的TBC的微观结构。用X射线衍射仪(XRD)测量涂层的相。微观结构研究表明,等离子喷涂和激光釉面涂层均由非平衡四方(T)相,立方(C)相和少量的Ce0.75Zr0.25O2相组成。等离子喷涂涂层中发现的少量单斜相(M)在激光上光后消失了。对喷涂和上釉的样品进行热循环后,测试的面漆的相分析表明四方(T)相的摩尔%降低,而Ce0.75Zr0.25O2相的摩尔%提高。还发现等离子喷涂样品中的单斜晶相在热循环后消失了。结果表明,激光玻璃对降低粘结涂层的氧化速率没有实质性影响。循环测试结果表明,通过激光玻璃化,等离子喷涂的TBC的寿命延长了两倍,达到了最初的剥落寿命。关于50%的散裂寿命,相对于等离子喷涂的样品,激光玻璃化的样品表现出约半衰期的改善。 TBC的失效是在粘结涂层谷部附近的面漆内引发的,并且主要在面漆和面漆与胶层界面附近的外生氧化物内传播。激光玻璃产生的分段裂纹改善了面漆的应变适应能力,可以被认为是TBC寿命延长的主要增强机制。

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