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Numerical study on modification of ceramic coatings by high-intensity pulsed ion beam

机译:高强度脉冲离子束改性陶瓷涂层的数值研究

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ZrO2 ceramic coatings, which often call thermal barrier coatings (TBCs), fabricated by electron beam physical vapor deposition (EB-PVD), are widely used in high-temperature environment of aircraft and industry gas-turbine engines, because of the excellent strain tolerance imparted by the columnar structure. However, channels separating the columnar grains in EB-PVD TBCs provide paths for oxygen or other aggressive species from ambient atmosphere into the bond coat, resulting in the premature spallation-failure during high-temperature service. in our previous study, high-intensity pulsed ion beam (HIPIB) technique has been proposed to modify the EB-PVD TBCs, where a melted, densified top layer can be produced as a result of extremely thermal effect induced by the HIPIB irradiation. In this paper, HIPIB melting process is investigated numerically using a physical model based on experimental data, taking into account the surface morphology of HIPIB-melted TBCs to explore the mechanism of interaction between HIPIB and the coatings. Deposition process of the beam energy in TBCs was simulated by Monte Carlo method, and the non-linear equations describing the thermal conducting process were solved numerically based on the deposited energy to obtain the evolution of the temperature field of TBCs. The calculated melting depth of irradiated EB-PVD TBCs is consistent with results obtained in the HIPIB irradiation experiments. (C) 2008 Elsevier Ltd. All rights reserved.
机译:通过电子束物理气相沉积(EB-PVD)制成的ZrO2陶瓷涂层通常称为热障涂层(TBC),由于其出色的应变耐受性而广泛用于飞机和工业燃气轮机发动机的高温环境中由柱状结构赋予。但是,分隔EB-PVD TBC中柱状晶粒的通道为氧气或其他侵蚀性物质从周围大气进入粘结层提供了路径,从而导致在高温工作期间过早散裂失效。在我们先前的研究中,已经提出了高强度脉冲离子束(HIPIB)技术来修饰EB-PVD TBC,其中由于HIPIB辐射引起的极高的热效应,会产生熔化的致密顶层。在本文中,基于实验数据,使用物理模型对HIPIB的熔融过程进行了数值研究,同时考虑了HIPIB熔融的TBC的表面形态,以探索HIPIB与涂层之间相互作用的机理。利用蒙特卡洛方法模拟了TBC中束能量的沉积过程,并基于沉积的能量数值求解了描述导热过程的非线性方程,得到了TBC温度场的演化。辐照的EB-PVD TBC的熔化深度与在HIPIB辐照实验中获得的结果一致。 (C)2008 Elsevier Ltd.保留所有权利。

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