The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types

Addressing the cavitation prevention requirements for a longer service life of the high-speed centrifugal pump in the temperature control system of aerospace, the effect of blade inlet width on cavitation performance is studied on the premise of consistency of impeller outlet diameter D2, impeller o...

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Main Authors: Wen-xiong Chao, Bao-lu Shi, Hui Ruan, Wei Dong
Format: Article
Language:English
Published: Frontiers Media S.A. 2022-07-01
Series:Frontiers in Energy Research
Subjects:
Online Access:https://www.frontiersin.org/articles/10.3389/fenrg.2022.811690/full
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author Wen-xiong Chao
Wen-xiong Chao
Bao-lu Shi
Hui Ruan
Hui Ruan
Wei Dong
author_facet Wen-xiong Chao
Wen-xiong Chao
Bao-lu Shi
Hui Ruan
Hui Ruan
Wei Dong
author_sort Wen-xiong Chao
collection DOAJ
description Addressing the cavitation prevention requirements for a longer service life of the high-speed centrifugal pump in the temperature control system of aerospace, the effect of blade inlet width on cavitation performance is studied on the premise of consistency of impeller outlet diameter D2, impeller outlet width b2, volute inlet diameter D3, pump interface and other structural parameters. Therefore, the corrected coefficient k1 of blade inlet exclusion coefficient is introduced; four groups of centrifugal impellers with inlets of different geometric structures blades are put forward. To begin with, based on the D# pump performance test and Pumplinx simulation, the cavitation performance of high-speed pump with four different groups of impellers is studied under five working conditions of negative inlet pressure (Pj=(−20, −30, −40, −50, −60)kPa) on the premise that energy characteristics agree well with cavitation performance. According to the results, when Pj drops from −50 kPa to −60 kPa, the cavitation perform changes the most significantly. This indicates that the method of twisting the centrifugal impeller of the suspended forward-extended blade shows a significant effect in preventing cavitation performance under such working conditions of high speed and negative pressure. Its application in aerospace power systems can effectively reduce the impact of low pressure in the system and significantly improve the cavitation performance.
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spelling doaj.art-04676c982a7b46878e1e0de4f87ace932022-12-22T03:38:17ZengFrontiers Media S.A.Frontiers in Energy Research2296-598X2022-07-011010.3389/fenrg.2022.811690811690The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller TypesWen-xiong Chao0Wen-xiong Chao1Bao-lu Shi2Hui Ruan3Hui Ruan4Wei Dong5Xi’an Aeronautical University, Shaanxi, ChinaNational Joint Engineering Research Center of Special Pump System Technology, Shaanxi, ChinaAstronaut Center of China, Shaanxi, ChinaXi’an Aeronautical University, Shaanxi, ChinaNational Joint Engineering Research Center of Special Pump System Technology, Shaanxi, ChinaNorthwest A&F University, Shaanxi, ChinaAddressing the cavitation prevention requirements for a longer service life of the high-speed centrifugal pump in the temperature control system of aerospace, the effect of blade inlet width on cavitation performance is studied on the premise of consistency of impeller outlet diameter D2, impeller outlet width b2, volute inlet diameter D3, pump interface and other structural parameters. Therefore, the corrected coefficient k1 of blade inlet exclusion coefficient is introduced; four groups of centrifugal impellers with inlets of different geometric structures blades are put forward. To begin with, based on the D# pump performance test and Pumplinx simulation, the cavitation performance of high-speed pump with four different groups of impellers is studied under five working conditions of negative inlet pressure (Pj=(−20, −30, −40, −50, −60)kPa) on the premise that energy characteristics agree well with cavitation performance. According to the results, when Pj drops from −50 kPa to −60 kPa, the cavitation perform changes the most significantly. This indicates that the method of twisting the centrifugal impeller of the suspended forward-extended blade shows a significant effect in preventing cavitation performance under such working conditions of high speed and negative pressure. Its application in aerospace power systems can effectively reduce the impact of low pressure in the system and significantly improve the cavitation performance.https://www.frontiersin.org/articles/10.3389/fenrg.2022.811690/fullimpeller typetwisted overhung forward-extendedhigh-speed centrifugal pumpcavitationethylene glycol aqueous solutionnumerical simulation CLC number: TH137
spellingShingle Wen-xiong Chao
Wen-xiong Chao
Bao-lu Shi
Hui Ruan
Hui Ruan
Wei Dong
The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
Frontiers in Energy Research
impeller type
twisted overhung forward-extended
high-speed centrifugal pump
cavitation
ethylene glycol aqueous solution
numerical simulation CLC number: TH137
title The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
title_full The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
title_fullStr The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
title_full_unstemmed The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
title_short The Cavitation Characteristics of High Speed Centrifugal Pumps With Different Impeller Types
title_sort cavitation characteristics of high speed centrifugal pumps with different impeller types
topic impeller type
twisted overhung forward-extended
high-speed centrifugal pump
cavitation
ethylene glycol aqueous solution
numerical simulation CLC number: TH137
url https://www.frontiersin.org/articles/10.3389/fenrg.2022.811690/full
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