RESEARCH PAPERS: Vibration and Sound

Rotor Stability of High Pressure Multistage Centrifugal Compressors

[+] Author and Article Information
H. R. Wyssmann

Sulzer-Escher Wyss Ltd., Zurich, Switzerland

J. Vib., Acoust., Stress, and Reliab 110(2), 185-192 (Apr 01, 1988) (8 pages) doi:10.1115/1.3269497 History: Received August 12, 1987; Online November 23, 2009


A major factor influencing rotor stability of multistage high pressure centrifugal turbocompressors are the forces caused by the fluid-rotor interaction in the interstage and balance piston gas seals. An example of a fully 3-D labyrinth flow solution shows that using time averaged Navier-Stokes solutions are still excessive in computer time and hence cannot be used for practical applications. The paper gives a theory based on a two-volume bulk flow model for the prediction of the rotor-dynamic coefficients used for rotor stability calculation by complex eigenvalue analysis. Comparisons of predicted coefficients with measurements carried out on a high pressure compressor and on labyrinth seal test stands are given. The theoretically predicted phenomenon that labyrinth damping is retained even at zero inlet swirl of the leakage flow is confirmed. An example of a stability analysis of a high pressure natural gas compressor is given, where the stability margin increases with fluid pressure, i.e., density, provided seal swirl is controlled.

Copyright © 1988 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In