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THE EFFECT OF TIP LEAKAGE VORTEX ON CAVITATION PERFORMANCE IN AXIAL HYDRO TURBINE

机译:尖端泄漏涡旋对轴向水轮机空化性能的影响

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From viewpoint of greenhouse gas emission reduction, recently utilization of renewable energy becomes the focus of attention. Among several renewable energy systems, hydro power generation can supply the most stable energy and Torishima has already supplied an axial micro hydro turbine [1]. In general, the low cost system is needed in the case of micro hydro turbine. And one solution is to apply a fixed blade and constant rotation speed type. However the operating range will be narrow because of a cavitation problem. As is well known, there are some kinds of cavitations in the hydro machinery and they cause adverse effects such as vibration, excessive noise, decreasing efficiency and affecting turbine life [2]. Furthermore, these effects are more serious at partial and/or overload condition, so that turbine allowable operating range is limited by them. Therefore, the purpose of this study is to improve the cavitation performance in wider range for satisfying this requirement. In this paper, we focused on the influence of tip leakage vortex cavitation; one of the important phenomena for cavitation performance improvement as described in the references [3-5]. We tried to clarify the influence by both experimental and numerical investigation on the cavitation performance. In CFD (Computational Fluid Dynamics) analysis, tip clearance was applied for whole circumference model of runner and the full cavitation model [6] was used for the unsteady cavitation analysis. The calculation domain included guide vane was used to consider the effect of unsteady interference between runner and guide vane. In the CFD result, the tip leakage vortex cavitation was identified by void ratio and helicity [7] to analyze vortex structure with detail.
机译:从温室气体排放的观点来看,最近利用可再生能源成为关注的焦点。在几种可再生能源系统中,水力发电可以提供最稳定的能源,并且托里黎菲已经提供了轴向微水涡轮机[1]。通常,在微水力涡轮机的情况下需要低成本系统。一个解决方案是施加固定刀片和恒定的转速型。然而,由于空化问题,工作范围将是狭窄的。众所周知,水电机械中有一些空化物,它们会导致振动,过度噪音,降低效率和影响涡轮机寿命的不利影响[2]。此外,这些效果在部分和/或过载状态下更严重,因此涡轮机允许的操作范围受到它们的限制。因此,本研究的目的是改善更广泛的空化性能,以满足这一要求。在本文中,我们专注于尖端泄漏涡旋空心的影响;如参考文献[3-5]所述的空化性能改善的重要现象之一。我们试图通过对空化性能的实验和数值调查来阐明影响。在CFD(计算流体动力学)分析中,施加尖端间隙用于跑步者的整个圆周模型,全空化模型[6]用于不稳定的空化分析。计算域包括导向叶片用于考虑转轮与导向叶片之间不稳定干扰的效果。在CFD结果中,通过空隙率和螺旋度鉴定尖端泄漏涡流空化,并详细识别涡旋结构。

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