在转速空载条件下运行的混流式水轮机转轮入口处的流量测量值

Araz Rezavand Hesari, Anthony Munoz, Maxime Coulaud, S. Houde, Yvan Maciel
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摘要

对于混流式水轮机来说,空转是最不利的运行条件之一,其特点是转轮上的压力和应变波动很大。要减缓这些波动,就必须全面了解和描述产生波动的流动现象。本文介绍了使用高速立体和内窥镜粒子图像测速仪对无速度无负荷条件下运行的混流式水轮机转轮模型入口处的流动情况进行的实验研究。测量是在一个径向-方位平面内进行的,该平面覆盖了无叶片空间和叶片间通道的大片区域。这项研究标志着首次在流道中测量该工作点的临界流动现象。对瞬时速度场和平均速度场以及其他统计数据进行了分析。研究结果证实了空转速度下流动的随机性,同时也强调了其他研究中观察到的流动的一般结构。吸入侧的高速波动与延伸至无形空间的回流以及由回流偶尔产生的循环区有关。这两种现象经常出现,但随机波动。此外,在叶片的压力侧还会间歇性地形成另外两个环流区。叶片前缘附近出现比环流区更小的涡流与逆流强度相关。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Measured Flow at the Inlet of a Francis Turbine Runner Operating in Speed No-load Condition
For Francis turbines, speed-no-load represents one of the most detrimental operating conditions, marked by significant pressure and strain fluctuations on the runner. Mitigating these fluctuations necessitates a comprehensive understanding and characterization of the flow phenomena responsible for their generation. This paper presents an experimental investigation of the flow at the inlet of a Francis turbine runner model operating in speed-no-load condition using high-speed stereoscopic and endoscopic particle image velocimetry. The measurements are made in a radial-azimuthal plane that covers the vaneless space and a large region in the interblade channel. This study marks the first-time measurement of critical flow phenomena at this operating point, performed in the runner. Instantaneous and average velocity fields are analyzed, along with other statistical data. The results confirm the stochastic nature of the flow at speed-no-load but also highlight the general structure of the flow observed in other studies. The high velocity fluctuations on the suction side are associated with a backflow extending into the vaneless space and a circulation zone occasionally generated by this backflow. Both phenomena are frequently present, but fluctuate stochastically. Additionally, two other circulation zones intermittently form on the pressure side of the blades. The presence of vortices, smaller than the circulation zones, near the blade's leading edge correlates with the backflow intensity.
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