The appearance of flow instabilities like the blockage severity,impeller cut flaws,pitted cover plate flaws can cause to diminish the efficiency of centrifugal pump(CP),and may result in excessive vibration and noise,...
supported by the National Natural Science Foundation of China(Grant Nos.52079058 and 52209113);the Natural Science Foundation of Jiangsu Province(Grant Nos.BK20230011 and BK20220544);China Postdoctoral Science Foundation(Grant No.2023M731367);Postgraduate Research&Practice Innovation Program of Jiangsu Province(Grant No.KYCX23_3698).
The fluid’s viscosity significantly affects the performance of a centrifugal pump.The entropy production method and leakage are employed to analyze the performance changes under various viscosities by numerical simul...
supported by Science and Technology Project of Quzhou(Grant Nos.2023K256,2023NC08);Zhejiang Provincial Natural Science Foundation of China(Grant No.LZY21E050001);Hunan Province Key Field R&D Plan Project(Grant No.2022GK2068).
In order to obtain the transient characteristics of a low-speed centrifugal pump during the start-up and shutdown stages,dedicated experimental tests were conducted with eight different valve opening conditions.The Pe...
The centrifugal pump is a prevalent power equipment widely used in different engineering patterns,and the impeller blade wrap angle significantly impacts its performance.A numerical investigation was conducted to anal...
supported by the“Pioneer”and“Leading Goose”R&D Program of Zhejiang(Grant No.2022C03170);Science and Technology Project of Quzhou(Grant No.2022K98);Hunan Province Key Field R&D Plan Project(Grant No.2022GK2068).
Centrifugal pumps are widely used in the metallurgy,coal,and building sectors.In order to study the hydraulic characteristics of a closed impeller centrifugal pump during its shutdown in the so-called power frequency ...
supported by the National Science and Technology Major Project, China (No. J2019-V-0016-0111);the Aviation Engine and Gas Turbine Basic Science Center Project, China (No. P2022-B-V-003-001);the Defense Industrial Technology Development Program, China (No. JCKY2022607C002);the AECC Industry University Cooperation Project, China (No. HFZL2022CXY013);the National Natural Science Foundation of China (No. 52372396);the Key R&D Project in Shaanxi Province, China (No. 2021GXLH-01-16)。
This paper aims to tackle the calculation efficiency problem raised in the cavitation-flow simulation of the aviation centrifugal pump due to the fading-away interface resulting from the dissipation of numerics used i...
The authors extend their appreciation to the Researchers Supporting Project number(RSPD2023R698),King Saud University,Riyadh,Saudi Arabia for funding this research work.
A high percentage of failure in pump elements originates from fatigue.This study focuses on the discharge section behavior,made of ductile iron,under dynamic load.An experimental protocol is established to collect the...
supported by the National Natural Science Foundation of China(Grant No.51979126).
Cavitation commonly induces performance deterioration and system vibration in many engineering applications.This paper aims to investigate the effects of air injection on cavitation evolution,pressure pulsation and vi...
supported by the Anhui Province University Discipline(Professional)Top Talent Academic Funding Project(No.gxbjZD2021076);This project is supported by the Key Project of Natural Science Research in Colleges and Universities of Anhui Province(No.KJ2021A1026);This project is supported by the Key Project of Natural Science Foundation of Chaohu University(No.XLZ-201902).
The main structural parameters of the IR100-80-100A type chemical centrifugal pump have been optimized by means of an orthogonal test approach.The centrifugal pump has been modeled using the CFturbo software,and 16 se...
Supported by National Key Research and Development Program of China(Grant No.2022YFC3202901);Natural Science Foundation of China(Grant No.51879121);Jiangsu Provincial Primary Research&Development Plan(Grant No.BE2019009-1);China Scholarship Council(Grant No.202108690020).
Pressure fluctuation due to rotor-stator interaction in turbomachinery is unavoidable,inducing strong vibration in the equipment and shortening its lifecycle.The investigation of optimization methods for an industrial...