Title of article
Performance Enhancement of Centrifugal Compressor with Addition of Splitter Blade Close to Pressure Surface
Author/Authors
Malik, A College of Power and Energy Engineering - Harbin Engineering University, Harbin, China , Zheng, Q College of Power and Energy Engineering - Harbin Engineering University, Harbin, China , Zaidi, A. A College of Power and Energy Engineering - Harbin Engineering University, Harbin, China , Fawzy, H College of Power and Energy Engineering - Harbin Engineering University, Harbin, China
Pages
10
From page
919
To page
928
Abstract
This paper exemplified a way to increase pressure ratio and improve efficiency with addition of multi splitters
in centrifugal impeller with a vaneless diffuser. DDA 404-III back swept impeller of centrifugal compressor,
studied through experiment is modified with the addition of splitters blades and a sample impeller is designed
and analyzed with big splitter close to pressure surface and small splitter close to suction surface. Keeping all
flow conditions and impeller definitions, same as experimentally validated impeller, in order to investigate
effects of the location of the splitters between two main blades. It was observed that total pressure ratio is
increased from 4.1 to 4.5 with 2 % increase in efficiency with big splitter close to pressure surface of main
blade and small splitter close to suction surface of main blade. It was observed that relative Mach number
reduces at inlet of modified impeller.
Keywords
Centrifugal Compressor , DDA 404-III Impeller , Multi splitter blades , Numerical simulation
Journal title
Astroparticle Physics
Serial Year
2018
Record number
2466907
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