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Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering

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Optimization of centrifugal compressor stages

https://doi.org/10.25206/2588-0373-2023-7-4-33-39

Abstract

The article describes а hydraulic efficiency increase in the centrifugal compressor stage using automatic optimization algorithms. The optimization criterion is the polytropic efficiency of the intermediate compressor stage. The sequence of stages of the optimization process in the Fine/Design3D software module of the Numeca software package is presented. The creating process a solid model of the compression stage is shown. The performance curves of the developed stage after optimization of the shape of the rotor and stator elements are also presented.

About the Authors

E. V. Dubinin
NIIturbokompressor JSC
Russian Federation

DUBININ Evgeniy Vladimirovich, Chief of Bureau

Kazan, Sibirsky Trakt str., 40, 420029



B. F. Idiyatullin
NIIturbokompressor JSC
Russian Federation

IDIYATULLIN Bulat Fanisovich, 2nd Category Engineer for Calculations and Modes

Kazan, Sibirsky Trakt str., 40, 420029



N. G. Khasanov
NIIturbokompressor JSC
Russian Federation

KHASANOV Nariman Gayazovich, Candidate of Technical Sciences, Senior Researcher

Kazan, Sibirsky Trakt str., 40, 420029



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For citations:


Dubinin E.V., Idiyatullin B.F., Khasanov N.G. Optimization of centrifugal compressor stages. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2023;7(4):33-39. (In Russ.) https://doi.org/10.25206/2588-0373-2023-7-4-33-39

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ISSN 2588-0373 (Print)
ISSN 2587-764X (Online)