Cavitation flow and blade loading characteristic in impeller tip region of axial flow pump

被引:0
作者
Zhang, Desheng [1 ]
Pan, Dazhi [1 ]
Shi, Weidong [1 ]
Shao, Peipei [1 ]
Wang, Haiyu [1 ]
Li, Tongtong [1 ]
机构
[1] Research Center of Fluid Machinery Engineering and Technology, Jiangsu University
来源
Huagong Xuebao/CIESC Journal | 2014年 / 65卷 / 02期
关键词
Axial-flow pump; Blade loading; Cavitation; High speed photograph; Numerical simulation;
D O I
10.3969/j.issn.0438-1157.2014.02.019
中图分类号
学科分类号
摘要
In order to take into account the local density of gas-liquid mixing area in cavitation flow field in impeller tip region of axial flow pump, the turbulent viscosity term in SST k-ω turbulence mode was corrected. NPSH curves, cavitation characteristic and blade loading were analyzed based on full cavitation model with simulation and experimental methods. The investigation results show that the modified SST k-ω turbulence model and cavitation model can predict the cavitation flow field with gas-liquid two-phase flow in the impeller tip region, and the relative error of the critical cavitation number between experimental and predicted values is 7.79% under design conditions, which is satisfactory for the computational accuracy. The high speed phohography experiments show that the cavitation inception is induced by blowing cavitation, clearance attached cavitation and tip leakage vortex cavitation, and the cavitation region continually spreads with the decrease of cavitation number. The break of cavitation bubble cluster occurs at the aft of the blade, and the position of bubble break moves toward the middle of the blade span. The angular interval between (13° and +13° is the main region of the suction side with low pressure. Within the 3% area attached to the blade tip clearance, the pressure gradually decreases with the increase of radius coefficient r*, decreasing the blade surface loading. Near the tip clearance, the blade loading decreases more obviously. © All Rights Reserved.
引用
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页码:501 / 507
页数:6
相关论文
共 19 条
[1]  
Guan X., Axial Flow Pump and Mixed Flow Pump, (2009)
[2]  
Lakshminarayana B., Fluid Dynamics and Heat Transfer of Turbomachinery, (1996)
[3]  
Furukawa M., Inoue M., Saiki K., Yamada K., The role of tip leakage vortex breakdown in compressor rotor aerodynamics, Turbomach, 121, pp. 469-480, (1999)
[4]  
Gerolymos G.A., Vallet I., Tip-clearance and secondary flows in a transonic compressor rotor, Turbomach, 121, pp. 751-762, (1999)
[5]  
Gourdain N., Leboeuf F., Unsteady simulation of an axial compressor stage with casing and blade passive treatments, Turbomach, 131, (2009)
[6]  
Shi W., Zhang H., Chen B., Et al., Numerical simulation of internal flow field in axial-flow pump with different blade tip clearance sizes, Drainage and Irrigation Machinery, 28, 5, pp. 374-377, (2010)
[7]  
Liang K., Zhang K., Xu L., Analysis of the flow trough the blade tip clearances of axial pump by CFD, J. Huazhong Univ. of Sci&Tech: Nature Science Edition., 32, 9, pp. 36-38, (2004)
[8]  
Zhang D., Shi W., Zhang H., Numerical simulation of flow field characteristics in tip clearance region of axial-flow impeller, Transactions of the Chinese Society for Agricultural Machinery, 43, 3, pp. 73-77, (2012)
[9]  
Kohei O., Yoichiro M., Kdnjiro K., Numerical analysis for unsteady cavitating flow in pump inducer, Fifth International Symposiun on Cavitation, 11, pp. 1-4, (2003)
[10]  
Murayama M., Wang M., Moin P., Et al., Vortex dynamics and low-pressure fluctuations in the tip-clearance flow, ASME Journal of Fluids Engineering, 129, 8, pp. 1002-1014, (1997)