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Continuum and kinetic simulations of the neutral gas flow in an industrial physical vapor deposition reactor

机译:工业物理气相沉积反应器中中性气流的连续和动力学模拟

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Magnetron sputtering used for physical vapor deposition processes often requires gas pressureswell below1 Pa. Under these conditions the gas flow in the reactor is usually determined by a Knudsen number of about one, i.e., a transition regime between the hydrodynamic and the rarefied gas regime. In the first, the gas flow is well described by the Navier-Stokes equations, while in the second a kinetic approach via the Boltzmann equation is necessary. In this paper the neutral gas flow of argon and molecular nitrogen gas inside an industrial scale plasma reactor was simulated using both a fluid model and a fully kinetic Direct Simulation Monte Carlo model. By comparing bothmodel results the validity of the fluidmodelwas checked. Although in bothmodels a Maxwell- Boltzmann energy distribution of the neutral particles is the natural outcome, the results of the gas flow differ significantly. The fluid model description breaks down, due to the inappropriate assumption of a fluid continuum. This is due to exclusion of non-local effects in the multi dimensional velocity space, as well as invalid gas/wall interactions. Only the kinetic model is able to provide an accurate physical description of the gas flow in the transition regime. Our analysis is completed with a brief investigation of different definitions of the local Knudsen number.We conclude that the most decisive parameter-the spatial length scale L-has to be very careful chosen in order to obtain a reasonable estimate of the gas flow regime.
机译:用于物理气相沉积工艺的磁控溅射通常要求气体压力远低于1 Pa。在这些条件下,反应器中的气体流量通常由约1的克努森数确定,即流体力学和稀有气体之间的过渡态。首先,用Navier-Stokes方程很好地描述了气流,而在第二步中,需要通过Boltzmann方程进行动力学处理。本文使用流体模型和全动力学直接模拟蒙特卡洛模型对工业规模等离子体反应器内的氩气和分子氮气的中性气流进行了模拟。通过比较两个模型结果,检查了流体模型的有效性。尽管在这两个模型中,中性粒子的Maxwell-Boltzmann能量分布都是自然的结果,但是气流的结果却有很大差异。由于对流体连续性的不适当假设,流体模型描述失败了。这是由于排除了多维速度空间中的非局部效应以及无效的气体/壁相互作用。只有动力学模型才能提供过渡状态下气流的准确物理描述。我们的分析是通过对局部Knudsen数的不同定义进行的简短调查而完成的。我们得出结论,最关键的参数-空间长度标度L-必须谨慎选择,以便获得合理的气体流态估计。

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