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Detection of Precursor Waves Announcing Stall in Two 3-Stage Axial Compressors PUBLIC ACCESS

[+] Author Affiliations
F. Grauer, W. Volgmann, H. Stoff

University of Bochum, Germany

T. Breuer

MTU-München, Germany

Paper No. 98-GT-520, pp. V001T01A125; 8 pages
doi:10.1115/98-GT-520
From:
  • ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 1: Turbomachinery
  • Stockholm, Sweden, June 2–5, 1998
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7862-0
  • Copyright © 1998 by ASME

abstract

Rotating stall and surge limit the operating range of a compressor towards low throughflow and high pressure in the performance map. Usually a safety margin must be observed to prevent the compressor from entering unintentionally aerodynamic instabilities. As the range of highest performance and efficiency lies in the vicinity of the stability limit, efforts concentrate on recognizing imminent onset of unstable operation prior to its occurrence.

The present investigation centers on means of detecting information about onsetting instability from signals of pressure fluctuations in two transonic medium-pressure axial compressors of 3 stages. Fourier-transform-methods as well as artificial neural networks are applied for the data reduction of the time-dependent pressure signals. The methods of investigation presented here detected stall precursors announcing the onset of instability. Some of them seem appropriate to be used in connection with active stall control.

Copyright © 1998 by ASME
Topics: Compressors , Waves
This article is only available in the PDF format.

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