Author:
Hong Enyu,Ban Haibo,Qi Mingxu
Abstract
Abstract
The paper presents a design optimization method for a type of centrifugal compressor’s vaned diffuser with using a one-dimensional (1D) mathematical model to determine the best throat area ratio of the impeller to the diffuser. The research aims to verify of the 1D throat area mathematical model and to study the influence of vaned diffuser structure on the impeller-diffuser matching and the stage performance. The results of CFD analysis and experiments have proved that 1D throat area model can predict the throat area ratio of the impeller to the vaned diffuser accurately for the same choking mass flow at the required rotating speed. After optimization, the compressor performances and the matching between impeller and vane diffuser are considerably improved as well. The results and conclusions indicate that quick geometry modification of vaned diffusers can achieve excellent performance optimization and provide the theoretical basis for the selection of variable vaned diffusers.
Subject
General Physics and Astronomy
Reference11 articles.
1. Experimental Performance of a 16.1 Centimetre Tip Diameter Centrifugal Compressor Designed for a 6: 1 Pressure Ratio;Klassen
2. The Experimental Study of Matching Between Centrifugal Compressor Impeller And Diffuser;Tamaki;J. Turbomach.,1999
3. The Matching of a Vaned Diffuser With a Radial Compressor Impeller and Its Effect on the Stage Performance;Casey;J. Journal of Turbomachinery,2014
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献