基于伽马过渡模型的离心泵旋转失速特性研究

Changliang Ye, Wanru Huang, Hongyeyu Yan, Yuan Zheng, K. Kan, B. V. van Esch
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引用次数: 0

摘要

离心泵的旋转失速现象与叶片边界层的演变密切相关。为了准确预测边界层的特征,本研究利用伽马(γ)过渡模型研究了离心泵叶轮的旋转失速现象。通过将数值模拟的结论与试验结果进行比较,证实了数值模拟的准确性。在考虑过渡特性的计算中,叶轮内部低压区域的分布相对不连续,而压力分布则较为均匀。然而,在不考虑过渡的计算中,相邻流道的低压区域呈现出相互连接的趋势,导致压力分布更加多变,出口处的压力轮廓更加接近平行。通过动态模态分解方法获得了离心泵叶轮旋转失速的动态特性,包括失速涡的频率、结构和动态演化过程。通过模态重构发现,叶轮的旋转会导致失速涡发生周期性波动。失速涡并非静止不动,而是与叶片的旋转同步运动。在不同的时间点,滞流漩涡呈现周期性变化。在叶片吸入口,失速涡最初出现。随后,多个涡流结构导致通道堵塞。经过一段时间的发展,多余的漩涡结构合并成一个典型的 "8 "字形漩涡结构,并向出口移动。最后,出口失速漩涡消失,新的漩涡结构在叶片吸入面的入口处产生。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on rotating stall characteristics of centrifugal pumps based on gamma transition model
The phenomenon of rotating stall in centrifugal pumps is closely associated with the evolution of the blade boundary layer. Aiming to accurately predict the characteristics of the boundary layer, this study investigates the phenomenon of rotating stall in centrifugal pump impellers using the gamma (γ) transition model. The accuracy of the numerical simulation was confirmed by comparing its conclusions with the results of the testing. In calculations considering transition characteristics, the distribution of low-pressure areas inside the impeller is relatively discontinuous, while the pressure distribution is more uniform. However, in calculations without considering transition, the low-pressure regions in neighboring flow channels exhibit a tendency to be interconnected, resulting in a more variable pressure distribution, and the pressure contour at the outlet is closer to parallel. The dynamic characteristics of the centrifugal pump impeller rotating stall were obtained through the dynamic mode decomposition method, including the frequency, structure, and dynamic evolution process of the stall vortex. Through modal reconstruction, it was discovered that the impeller's rotation causes the stall vortex to undergo periodic fluctuations. The stall vortex is not stationary but moves synchronously with the rotation of the blades. At different time points, the stall vortex exhibits periodic changes. At the blade suction entrance, the stall vortex initially appears. Subsequently, multiple vortex structures resulted in channel blockage. After a period of development, the excess vortex structures merge to generate a typical “8” shaped vortex structure and move toward the exit. Finally, the exit stall vortex disappears, and a new vortex structure is generated at the inlet of the blade suction surface.
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