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Application of Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor PUBLIC ACCESS

[+] Author Affiliations
H. Hayami

Kyushu University, Kasuga, Japan

Y. Senoo

Miura Company, Ltd., Matsuyama, Japan

K. Utsunomiya

Mitsubishi Kasei, Ltd., Yokohama, Japan

Paper No. 89-GT-66, pp. V001T01A037; 6 pages
doi:10.1115/89-GT-66
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7913-9
  • Copyright © 1989 by ASME

abstract

Low-solidity circular cascades, conformally transformed from high-stagger linear cascades of double-circular-arc vanes with solidity 0.69, were used as a part of the diffuser system of a transonic centrifugal compressor. Performance test results were compared with data of the same compressor with a vaneless diffuser. Good compressor performance, a wider flow range as well as a higher pressure ratio and a higher efficiency, superior to those with a vaneless diffuser, where the flow range was limited by choke of the impeller, were demonstrated. The test circular cascade diffusers demonstrated a good pressure recovery over a wide range of flow angles, even when the inflow Mach number to the cascade was over unity.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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