详细信息
翼型轴流桨推力系数实验及CFD模拟
Experimental study and CFD simulation for thrust coefficient of hydrofoil impellers
文献类型:期刊文献
中文题名:翼型轴流桨推力系数实验及CFD模拟
英文题名:Experimental study and CFD simulation for thrust coefficient of hydrofoil impellers
作者:雷建奇[1];祝贺[1];陈剑佩[1];吴高杰[1]
机构:[1]华东理工大学化学工程联合国家重点实验室,上海200237
年份:2010
卷号:29
期号:3
起止页码:430
中文期刊名:化工进展
外文期刊名:Chemical Industry and Engineering Progress
收录:CSTPCD;;Scopus;北大核心:【北大核心2008】;CSCD:【CSCD2011_2012】;
语种:中文
中文关键词:翼型轴流桨;推力系数;计算流体力学;轴向速度;功率准数
外文关键词:hydrofoil impellers thrust coefficient CFD(computational fluid dynamics) axial velocity power number
摘要:对几种不同型式轴流桨的推力系数进行了实验及CFD模拟研究。结果表明:四宽叶翼型桨A的推力系数最大,三窄叶翼型桨D推力系数最小;模拟结果与实验结果有很好的吻合;四宽叶翼型桨A较其它几种轴流桨形成的全釜大循环更为彻底,没有发生分区现象;四宽叶翼型桨A在叶端线上的最大轴向速度远大于其它4种桨;四宽叶翼型桨A最大轴向速度随着r/R的增大而逐渐减小且逐渐向釜底方向移动。在水体系中的实验结果表明:当通气量Qg为1.1vvm,P/V≥1.5kW/m3时,四宽叶翼型桨A-透平桨组合的传质系数较双层透平桨组合高约9.6%。
The thrust coefficient of different hydrofoil impellers was experimentally studied and simulated with CFD.Results showed that the thrust coefficient of four-broad-blade hydrofoil A is the largest,and that of three-narrow-blade hydrofoil D is the smallest.The simulation results are in good agreement with experiment.Compared with other axial impellers,four-broad-blade hydrofoil A produces a fully developed circulation.The maximum axial velocity of four-broad-blade hydrofoil A is the biggest in these impellers at the vertical line of blade tip.The maximum axial velocity of four-broad-blade hydrofoil A gradually declines with the increase of r/R,and moves toward the bottom of the tank.Experimental results in water system indicated that the mass transfer coefficient(kLa)of four-broad-blade hydrofoil A-Rushton turbine(HF-A -RT)is 9.6% higher than that of Rushton turbine-Rushton turbine(RT-RT)when gas aerated rate is 1.1 vvm and the power consumption per volume(P/V)is not less than 1.5 kW/m3.
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