首页> 外文期刊>Renewable energy >Pressure fluctuation and flow instability in S-shaped region of a reversible pump-turbine
【24h】

Pressure fluctuation and flow instability in S-shaped region of a reversible pump-turbine

机译:可逆泵汽轮机S形区域的压力波动和流量不稳定性

获取原文
获取原文并翻译 | 示例
       

摘要

To understand the pressure fluctuations occurring in S-shaped region of the pump-turbine and their relationships with rotor-stator interaction, rotating stall and vortex rope, the numerical and experimental studies of a reversible pump-turbine were conducted under turbine, runaway, turbine brake, small flow rate and reverse pump operating modes. The experimental results show that pressure fluctuations under turbine mode were most affected by the guide vane opening. This effect was weaker under turbine brake mode and weaker still under reverse pump mode. At a guide vane opening of 19 mm, the maximum fluctuation peak in the vaneless space is 5.7 times, 6.9 times and 2.0 times greater than that in the spiral casing inlet, draft tube cone and draft tube elbow, respectively. Unsteady simulation results for the whole flow passage of the pump-turbine show that asymmetric flow occurred in the runner under turbine, runaway and turbine brake operating modes. Meanwhile, an obvious rotating stall vortex with a frequency of 0.65fn was generated in turbine brake mode, resulting in relatively large pressure fluctuations in the vaneless space. At the small flow rate, flow separation in the vaneless space became very obvious, while that in the runner weakened, resulting in decreased pressure fluctuations in the vaneless space. Under reverse pump mode, pressure fluctuations in the vaneless space were relatively small because of obvious symmetrical flow separation in the runner. Pressure fluctuations in the draft tube were mainly attributed to the combined actions of rotating stall and vortex rope phenomena. What's more, the fluctuation amplitudes at the rotating stall frequency of 0.65fn and the vortex rope frequencies of 0.30fn and 0.17fn were relatively large. (C) 2020 Elsevier Ltd. All rights reserved.
机译:为了了解泵涡轮机的S形区域的压力波动及其与转子 - 定子相互作用,旋转档位和涡旋绳索的关系,可逆泵涡轮机的数值和实验研究在涡轮机,失控,涡轮机下进行制动器,小型流速和反向泵操作模式。实验结果表明,涡轮机模式下的压力波动受到导向叶片开口的影响。在涡轮机制动模式下,这种效果较弱,较弱仍然在反向泵模式下。在19毫米的导向叶片开口,无差距空间中的最大波动峰值为5.7倍,比螺旋套管入口,草稿管锥和管弯管中的最大波动峰值为5.7倍,6.9倍和2.0倍。泵涡轮机整体流动通道的不稳定模拟结果表明,在涡轮机,失控和涡轮机制动器操作模式下的流动器中发生不对称流量。同时,在涡轮机制动模式下产生具有0.65fn频率的明显旋转失速涡流,导致无差距空间中的压力波动相对大。在小的流速下,无差距空间中的流动分离变得非常明显,而在转轮中的削弱,导致无形的空间中的压力波动下降。在逆向泵模式下,由于跑步者在倒车器中的明显对称流动分离是相对较小的无差距空间的压力波动。草稿管中的压力波动主要归因于旋转档位和涡旋绳现象的组合作用。更重要的是,旋转失速频率的波动幅度为0.65fn,涡旋绳频为0.30fn和0.17fn的涡流频率相对较大。 (c)2020 elestvier有限公司保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号