Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES

Relying on a closed test rig of a high-power intercooling centrifugal compressor for compressed air energy storage (CAES), this study measured the static pressure and static temperature at different radii on the static wall of the impeller backside cavity (IBC) under variable rotating speeds. Simult...

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Main Authors: Zhihua Lin, Zhitao Zuo, Wei Li, Jianting Sun, Xin Zhou, Haisheng Chen, Xuezhi Zhou
Format: Article
Language:English
Published: MDPI AG 2022-01-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/15/2/420
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author Zhihua Lin
Zhitao Zuo
Wei Li
Jianting Sun
Xin Zhou
Haisheng Chen
Xuezhi Zhou
author_facet Zhihua Lin
Zhitao Zuo
Wei Li
Jianting Sun
Xin Zhou
Haisheng Chen
Xuezhi Zhou
author_sort Zhihua Lin
collection DOAJ
description Relying on a closed test rig of a high-power intercooling centrifugal compressor for compressed air energy storage (CAES), this study measured the static pressure and static temperature at different radii on the static wall of the impeller backside cavity (IBC) under variable rotating speeds. Simultaneously, the coupled computations of all mainstream domains with IBC or not were used for comparative analysis of the aerodynamic performances of the compressor and the internal flow field in IBC. The results show that IBC has a significant impact on coupling characteristics including pressure ratio, efficiency, torque, shaft power, and axial thrust of the centrifugal compressor. The gradients of radial static pressure and static temperature in IBC both increase with the decrease of mainstream flow or the increase of rotating speed, whose distributions are different under variable rotating speeds due to the change of the aerodynamic parameters of mainstream.
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spelling doaj.art-a0ab60b684cb42e780ee69981bab72b02023-11-23T13:35:48ZengMDPI AGEnergies1996-10732022-01-0115242010.3390/en15020420Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAESZhihua Lin0Zhitao Zuo1Wei Li2Jianting Sun3Xin Zhou4Haisheng Chen5Xuezhi Zhou6Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaNational Energy Large Scale Physical Energy Storage Technologies R&D Center of Bijie High-Tech Industrial Development Zone, Bijie 551712, ChinaRelying on a closed test rig of a high-power intercooling centrifugal compressor for compressed air energy storage (CAES), this study measured the static pressure and static temperature at different radii on the static wall of the impeller backside cavity (IBC) under variable rotating speeds. Simultaneously, the coupled computations of all mainstream domains with IBC or not were used for comparative analysis of the aerodynamic performances of the compressor and the internal flow field in IBC. The results show that IBC has a significant impact on coupling characteristics including pressure ratio, efficiency, torque, shaft power, and axial thrust of the centrifugal compressor. The gradients of radial static pressure and static temperature in IBC both increase with the decrease of mainstream flow or the increase of rotating speed, whose distributions are different under variable rotating speeds due to the change of the aerodynamic parameters of mainstream.https://www.mdpi.com/1996-1073/15/2/420centrifugal compressorimpeller backside cavityvariable rotating speedscoupling characteristics
spellingShingle Zhihua Lin
Zhitao Zuo
Wei Li
Jianting Sun
Xin Zhou
Haisheng Chen
Xuezhi Zhou
Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
Energies
centrifugal compressor
impeller backside cavity
variable rotating speeds
coupling characteristics
title Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
title_full Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
title_fullStr Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
title_full_unstemmed Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
title_short Experimental and Numerical Analysis of the Impeller Backside Cavity in a Centrifugal Compressor for CAES
title_sort experimental and numerical analysis of the impeller backside cavity in a centrifugal compressor for caes
topic centrifugal compressor
impeller backside cavity
variable rotating speeds
coupling characteristics
url https://www.mdpi.com/1996-1073/15/2/420
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