1673-159X

CN 51-1686/N

低比转速离心泵驼峰稳定性及其影响因素研究

Research on Hump Stability of Low Specific Speed Centrifugal Pump and Its Influencing Factors

  • 摘要: 为了提高低比转速离心泵的效率,一般会将叶轮叶片出口角加大一些,但会引起H-Q曲线有驼峰,导致泵在小流量区运行不稳定。本文以国内某水泵厂生产的比转速为47的单级单吸式离心泵为研究对象,采用正交试验法选择叶轮出口边斜切比、出口角度、叶轮轴线倾斜角度、叶片包角、叶片进口边位置5个因素,每个因素采用4个水平,一共16个叶轮设计方案;针对每个方案进行数值模拟,得到其外特性曲线;利用极差分析法研究5个因素对特性曲线形状以及泵额定工况下扬程、效率的影响,得到影响特性曲线稳定性的因素主次顺序依次为叶片进口边位置、叶轮出口边斜切、叶轮轴线倾斜角度、出口角度、叶片包角;利用分析得到的结果得出叶轮的优化组合方案,对该方案进行数值模拟验证。结果表明:优化方案的H-Q曲线稳定且泵的扬程和效率分别提升2.2%和1.4%;从优化前后的叶轮流场中分析消除驼峰的机理,得到驼峰工况区内叶轮进口处的能量损失占据主导,进口边位置的前移减小进口处的能量损失,同时叶轮出口边斜切与轴面倾斜使叶轮出口处相对速度变化减小,“射流–尾迹”现象减弱甚至消失,损失大幅减小。

     

    Abstract: In order to improve the efficiency of low specific speed centrifugal pumps, the outlet angle of impeller blades is generally increased, but this will cause hump of the H-Q curve, resulting in unstable operation of the pump in the small flow area. The single-stage single suction centrifugal pump with specific speed of 47 produced by a domestic pump factory is taken as the research object, the orthogonal test method is adopted to select five factors, namely, the impeller outlet oblique cutting ratio, the outlet angle, the impeller axis oblique angle, the blade wrap angle and the blade inlet edge position. Each factor adopts four levels, and this results in a total of 16 impeller design schemes. Each scheme was carried out numerical simulation to obtain the external characteristic curve of it. The influence of five factors on the shape of the characteristic curve and the head, efficiency and shaft power of the pump under rated working conditions was studied by range analysis method. The primary and secondary order of factors affecting the stability of the characteristic curve was found to be the blade inlet edge position, the impeller outlet edge chamfer, the impeller axis inclination angle, the outlet angle and the blade wrap angle. Based on the analysis results, the optimal combination scheme of the impeller was obtained, and the scheme was numerically simulated and tested. The results show that the H-Q curve of the optimized scheme is stable and the pump efficiency is increased by 1.4%. The reason for improving the stability is observed from the impeller rotation field before and after optimization, i.e. secondary flow area is generated at the outlet of the impeller rear cover plate to obtain higher lift. The relative velocity gradient at the impeller outlet decreases, and the "Jet wake" phenomenon weakened or even disappears with loss significantly .

     

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