A nonlinear approach based on the method of averaging has been developed to study unstable lateral vibrations of rotors in high-speed turbomachinery. The method makes use of an extended concept of bearing dynamic coefficients, which are defined by applying small perturbations to the dynamic equilibrium positions. The approach has been applied to determine the stability threshold of flexible rotors supported on short and tilting-pad journal bearings, respectively. Stability performance of systems supported on short journal bearings is improved by the presence of mass unbalance. However, for flexible rotors supported on tilting-pad journal bearings, increased unbalance can lead to lower rotordynamic stability margins. This has the significant implication that stability estimates from linear analysis are not always conservative. The present method provides a computationally more efficient way to understand the nonlinear vibration behavior of high-speed turbomachinery.
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January 1996
Research Papers
Nonlinear Analysis of Rotordynamic Instabilities in High-Speed Turbomachinery Available to Purchase
D. S. H. Chan
D. S. H. Chan
Department of Marine Technology, Kværner Engineering A. S., Oslo, Norway
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D. S. H. Chan
Department of Marine Technology, Kværner Engineering A. S., Oslo, Norway
J. Eng. Gas Turbines Power. Jan 1996, 118(1): 122-129 (8 pages)
Published Online: January 1, 1996
Article history
Received:
February 4, 1994
Online:
November 19, 2007
Citation
Chan, D. S. H. (January 1, 1996). "Nonlinear Analysis of Rotordynamic Instabilities in High-Speed Turbomachinery." ASME. J. Eng. Gas Turbines Power. January 1996; 118(1): 122–129. https://doi.org/10.1115/1.2816527
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