Correction of procedure for conversion of gas-dynamic characteristics of high-pressure centrifugal сompressor stage in case of frequency change rotor rotation

Authors

  • Aleksandr Dmitriyevich Vanyashov Omsk State Technical University, Omsk, Russia

DOI:

https://doi.org/10.25206/2588-0373-2022-6-2-27-35

Keywords:

centrifugal compressor stage, inlet guide device, axial-radial impeller, gasodynamic performances, whirl of flow

Abstract

The proposed corrected method of conversion of gas-dynamic characteristics of high-pressure stage of turbocharger
operating in the area of high circumferential speeds (conditional Mach numbers > 0,5) to other rotor speeds is given
in the work, taking into account deviation from kinematic and dynamic similarity conditions. The method of combined
control due to creation of swirling of flow in front of impeller and simultaneous change of rotation speed is considered.
Analysis of experimental and theoretical results is done.

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Author Biography

Aleksandr Dmitriyevich Vanyashov, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor of Refrigeration and Compressor Equipment and Technology Department, Omsk State Technical University, Omsk.

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Abstract views: 13

Published

2022-06-21

How to Cite

Vanyashov А. Д. (2022). Correction of procedure for conversion of gas-dynamic characteristics of high-pressure centrifugal сompressor stage in case of frequency change rotor rotation. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 6(2), 27–35. https://doi.org/10.25206/2588-0373-2022-6-2-27-35

Issue

Section

Power and chemical engineering

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