A centrifugal compressor requires a wide operating range as well as a high efficiency. At high pressure ratios, the impeller discharge velocity becomes transonic and effective pressure recovery in a vaned or vaneless diffuser is necessary. At high pressure ratios, a vaned diffuser is used as it has high pressure recovery, but may have a narrow operating range. At low flow, diffuser stall may trigger surge. At high flow, choking in the throat of the vanes may limit the maximum flow rate. A low solidity diffuser allows a good pressure recovery because it has vanes to guide the flow and a wide operating range as there is no geometrical throat to limit the maximum flow. In experimental studies at a pressure ratio around 4:1, the author has replaced vaned diffusers with a range of low solidity diffusers to try to broaden the operating range. The test results showed that the low solidity diffuser also chokes. In this paper, a virtual throat is defined and its existence is confirmed by flow visualization and pressure measurements. A method to select low solidity diffusers is proposed based on test data and the fundamental nature of the flow. The extension of the proposed method to the selection of a vaneless diffuser is examined and a design approach for a vaneless diffuser system to minimize surge flow rate without limiting the attainable maximum flow rate is proposed.
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April 2019
Research-Article
A Study on Matching Between Centrifugal Compressor Impeller and Low Solidity Diffuser and Its Extension to Vaneless Diffuser
Hideaki Tamaki
Hideaki Tamaki
Corporate Research & Development,
IHI Corporation,
1, Shin-Nakahara-Cho,
Isogo-Ku 235-8501, Yokohama, Japan
e-mail: hideaki_tamaki@ihi.co.jp
IHI Corporation,
1, Shin-Nakahara-Cho,
Isogo-Ku 235-8501, Yokohama, Japan
e-mail: hideaki_tamaki@ihi.co.jp
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Hideaki Tamaki
Corporate Research & Development,
IHI Corporation,
1, Shin-Nakahara-Cho,
Isogo-Ku 235-8501, Yokohama, Japan
e-mail: hideaki_tamaki@ihi.co.jp
IHI Corporation,
1, Shin-Nakahara-Cho,
Isogo-Ku 235-8501, Yokohama, Japan
e-mail: hideaki_tamaki@ihi.co.jp
Manuscript received June 24, 2018; final manuscript received July 4, 2018; published online December 5, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Apr 2019, 141(4): 041026 (16 pages)
Published Online: December 5, 2018
Article history
Received:
June 24, 2018
Revised:
July 4, 2018
Citation
Tamaki, H. (December 5, 2018). "A Study on Matching Between Centrifugal Compressor Impeller and Low Solidity Diffuser and Its Extension to Vaneless Diffuser." ASME. J. Eng. Gas Turbines Power. April 2019; 141(4): 041026. https://doi.org/10.1115/1.4041003
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