Hydrogen Fast Fill Modeling and Optimization of Cylinders Lined With Phase Change Material

M. Liszka, A. Fridlyand, A. Jayaraman, Michael Bonnema, C. Sishtla
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Abstract

This work is a continuation of a previous study (IMECE2019-11449) which sought to explore the feasibility and means of successfully modeling the hydrogen fast filling process of cylinders lined with phase change material (PCM) entirely in CFD software. The first focus of this work was to address the simplistic approach of how the liner temperature was modelled in the previous study. Previously, the entire liner was assigned a single temperature which was obtained and updated through the lumped heat capacity method. This meant that the hotter gas at the end of the cylinder opposite the inlet was in contact with a liner at a temperature lower than could realistically be expected. This was remedied by splitting the liner into four sections. Two sections were used for the curved portions at each end of the cylinder, and the straight wall section was split into two. Each section had its temperature independently calculated through the lumped heat capacity method. A temperature difference on the order of a ten degrees Celsius was observed between the different sections of the liner prior to latent heating beginning. The mass averaged temperature of the hydrogen inside the cylinder obtained with the sectioned wall case matched that obtained with the single wall temperature almost exactly, less than a degree difference. Despite the unexpected findings of the average hydrogen temperature not changing much when the wall is split into sections, this approach was still taken with all the cases completed in this study. The liner could be split into a greater amount of sections than four, but this was considered unnecessary due to the findings regarding the overall hydrogen temperature. Four sections were considered adequate and used to model the temperature gradient along the wall or liner. The effect of gravity on the filling process was also explored based on the orientation of the cylinder. This required completing three-dimensional simulations to accurately simulate buoyancy driven flow in horizontally mounted cylinders. All the simulations were completed with ANSYS Fluent 2019 R1 without the use of additional software to handle the heat transfer involving the PCM. All simulations were completed with the coupled pressure-based solver and K-Omega SST turbulence model. The gas properties were obtained from tables generated from NIST properties (REFPROP) available within ANSYS Fluent to limit the amount of error in the accumulated mass within the cylinder due to inaccurate gas properties. The initial conditions for the gas and liner temperatures were 25°C and 100 bar for the gas pressure. A constant mass flow rate of 0.02174 kg/s at a temperature 0°C were used as the initial conditions for the inlet hydrogen gas.
相变材料内衬气瓶快速充氢建模与优化
这项工作是先前研究(IMECE2019-11449)的延续,该研究旨在探索完全在CFD软件中成功模拟相变材料(PCM)内衬气瓶的氢气快速充注过程的可行性和方法。这项工作的第一个重点是解决在以前的研究中如何模拟衬垫温度的简单方法。以前,整个内衬被指定一个单一的温度,该温度是通过集总热容法获得和更新的。这意味着,在入口对面的气缸末端,较热的气体在低于实际预期的温度下与衬套接触。解决这一问题的方法是将尾管分成四段。圆柱体两端的弯曲部分采用两段,直壁部分分成两段。通过集总热容法独立计算各截面的温度。在潜热开始之前,在衬垫的不同部分之间观察到十摄氏度的温差。用分壁箱得到的筒体内氢气的质量平均温度与用单壁箱得到的质量平均温度几乎完全吻合,相差不到一度。尽管意外地发现,当壁面被分成几段时,平均氢气温度没有太大变化,但本研究中完成的所有案例仍然采用了这种方法。内衬可以被分成比四个更多的部分,但考虑到总体氢气温度,这被认为是不必要的。四个截面被认为是足够的,用来模拟沿壁或衬管的温度梯度。根据筒体的方向,探讨了重力对充填过程的影响。这需要完成三维模拟,以准确地模拟水平安装的圆柱体中浮力驱动的流动。所有模拟均使用ANSYS Fluent 2019 R1完成,无需使用额外的软件来处理涉及PCM的传热。所有模拟均使用基于压力的求解器和K-Omega海温湍流模型完成。气体特性是从ANSYS Fluent中可用的NIST特性(REFPROP)生成的表格中获得的,以限制由于不准确的气体特性而导致的圆柱体内累积质量的误差量。气体和衬管温度的初始条件为25℃,气体压力为100 bar。在0℃温度下,以0.02174 kg/s的恒定质量流量作为氢气进口的初始条件。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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