Dependency on Runner Geometry for Reversible-Pump Turbine Characteristics in Turbine Mode of Operation

Author:

Olimstad Grunde1,Nielsen Torbjørn2,Børresen Bjarne3

Affiliation:

1. e-mail:

2. e-mail:  Department of Energy and Process Engineering, Norwegian University of Science and Technology, Alfred Getz Vei 4, Trondheim 7491, Norway

3. Energi Norge, Næringslivets Hus, Middelthunsgate 27, Oslo 0307, Norway e-mail:

Abstract

Characteristics of a reversible-pump turbine have been measured with five different leading edge profiles in turbine mode. These profiles varied the inlet blade angle and the radius of curvature. Further geometry parameters have been investigated through numerical simulations. The pump turbine tested has much steeper flow-speed characteristics than a comparable Francis turbine. The most obvious geometry difference is the inlet part of the runner blades, where the blade angle for the pump turbine is much smaller than for the Francis turbine. Two different blade angles have been tested on a physical model and computational fluid dynamics (CFD) simulations have been performed on four different angles. Both methods show that a smaller blade angle gives less steep characteristics in turbine mode, whereas the measured s-shape in turbine brake- and turbine pumping mode gets more exaggerated. Long-radius leading edges result in less steep characteristics. The unstable pump turbine characteristics are in the literature shown to be a result of vortex formation in the runner and guide vane channels. A leading edge with longer curvature radius moves the formation of vortices towards higher speed of rotation.

Publisher

ASME International

Subject

Mechanical Engineering

Reference14 articles.

1. Pejovic, S., Krsmanovic, L., Jemcov, R., and Crnkovic, P., 1976, “Unstable Operation of High-Head Reversible Pump-Turbines,” 8th IAHR Symposium on Hydraulic Machinery and Cavitation, Leningrad, USSR, pp. 283–295.

2. Dörfler, P. K., Engineer, A. J., Pendse, R. N., Huvet, P., and Brahme, M. V., 1998, “Stable Operation Achieved on a Single-Stage Reversible Pump-Turbine Showing Instability at No-Load,” 19th IAHR Symposium on Hydraulic Machinery and Cavitation, Singapore.

3. Stabilisierung der Kennlinien einer Pumpenturbine im Bereich zwischen Turbinen-Teillast und Rückwärtspumpenbetrieb;Voith Forschung und Konstruktion,1982

4. Energy-Saving, Shock-Free Throttling With the Aid of a Reverse Running Centrifugal Pump;KSB Technische Berichte, Frankenthal,1988

5. Martin, C. S., 1986, “Stability of Pump-Turbines During Transient Operations,” 5th International Conference on Pressure Surges, BHRA, Hanover, Germany.

Cited by 56 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3