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Optimization of Draft Tube Structure for the Pilot-Scale Airlift Reactors

机译:中试空运反应堆尾水管结构的优化

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The effects of draft tube structure on the performance of pilot-scale Internal Loop Airlift Reactors (IL-ALRs) were investigated by Computational Fluid Dynamic (CFD) simulations and experiments. The Euler-Euler two fluid model and the κ-ε turbulence model were adopted in the CFD model to predict the influence of draft-tube structure on the key flow parameters including gas holdup, gas distribution and liquid circulation velocity. A good agreement was obtained between the CFD predictions and experimental measurements. In present study, perforation was applied to the expanding section of the draft tube, and numerical results show the optimized structure can enhance the gas-liquid separation, promote the oriented liquid circulation, increase the superficial gas velocity and maximize the productivity. Further optimization was conducted on the perforated design based on the CFD simulation.
机译:通过计算流体动力学(CFD)仿真和实验研究了引流管结构对中试规模内环空运反应堆(IL-ALR)性能的影响。在CFD模型中采用Euler-Euler两种流体模型和κ-ε湍流模型来预测尾水管结构对关键流量参数(包括气体滞留率,气体分布和液体循环速度)的影响。 CFD预测和实验测量之间获得了很好的一致性。在目前的研究中,对引流管的扩展段进行了穿孔,数值结果表明,优化的结构可以增强气液分离,促进定向的液体循环,增加表观气速,并最大化生产率。基于CFD仿真,对穿孔设计进行了进一步优化。

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