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RESEARCH PAPERS: Vibration and Sound

Evaluation of Aerodynamic Instability Mechanisms for Centrifugal Compressors—Part II: Advanced Analysis

[+] Author and Article Information
R. G. Kirk

Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

J. Vib., Acoust., Stress, and Reliab 110(2), 207-212 (Apr 01, 1988) (6 pages) doi:10.1115/1.3269500 History: Received October 30, 1987; Online November 23, 2009

Abstract

The results of advanced analysis for labyrinth seal dynamic characteristics are compared to current methods of calculating aerodynamic excitation and to test rig data published in the literature to date. The results of a shop full load test are presented and compared to predicted stability parameters. Results of the labyrinth analysis of the full-load test compressor are presented. Conclusions and recommendations are given for high pressure compressor rotor dynamics analysis with design guidelines for evaluation of new or proposed compressor designs.

Copyright © 1988 by ASME
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