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International Journal of Turbo & Jet-Engines

Ed. by Sherbaum, Valery / Erenburg, Vladimir


IMPACT FACTOR 2018: 0.863

CiteScore 2018: 0.66

SCImago Journal Rank (SJR) 2018: 0.211
Source Normalized Impact per Paper (SNIP) 2018: 0.625

Online
ISSN
2191-0332
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Volume 32, Issue 1

Issues

Investigation of Blade Angle of an Open Cross-Flow Runner

Yusuke Katayama
  • Corresponding author
  • Department of Mathematics and System Development, Shinshu University, 4-17-1 Wakasato, Nagano 380-8553, Japan
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  • Other articles by this author:
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/ Shouichiro Iio / Salisa Veerapun
  • Department of Mechanical Engineering, Naresuan University, 99 Moo 9 Tambon Tha Pho, Muang, Phitsanulok 65000, Thailand
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  • Other articles by this author:
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/ Tomomi Uchiyama
Published Online: 2015-05-08 | DOI: https://doi.org/10.1515/tjj-2015-0005

Abstract

The aim of this study was to develop a nano-hydraulic turbine utilizing drop structure in irrigation channels or industrial waterways. This study was focused on an open-type cross-flow turbine without any attached equipment for cost reduction and easy maintenance. In this study, the authors used an artificial indoor waterfall as lab model. Test runner which is a simple structure of 20 circular arc-shaped blades sandwiched by two circular plates was used The optimum inlet blade angle and the relationship between the power performance and the flow rate approaching theoretically and experimentally were investigated. As a result, the optimum inlet blade angle due to the flow rate was changed. Additionally, allocation rate of power output in 1st stage and 2nd stage is changed by the blade inlet angle.

Keywords: cross-flow runner; blade angle; power performance; hydraulic turbine; MPS method

About the article

Received: 2015-02-16

Accepted: 2015-02-16

Published Online: 2015-05-08

Published in Print: 2015-04-01


Citation Information: International Journal of Turbo & Jet-Engines, Volume 32, Issue 1, Pages 65–72, ISSN (Online) 2191-0332, ISSN (Print) 0334-0082, DOI: https://doi.org/10.1515/tjj-2015-0005.

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