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RESEARCH PAPERS

Influence of Impeller Shroud Forces on Turbopump Rotor Dynamics

[+] Author and Article Information
J. P. Williams

Rockwell Space Operations Company, 600 Gemini, R20-B, Houston, TX 77058

D. W. Childs

Department of Mechanical Engineering, Texas A&M University, College Station, TX 77843

J. Vib. Acoust 113(4), 508-515 (Oct 01, 1991) (8 pages) doi:10.1115/1.2930215 History: Received February 01, 1990; Online June 17, 2008

Abstract

The shrouded-impeller leakage path forces calculated by Childs (1987) have been analyzed to answer two questions. First, because of certain characteristics of the results of Childs, the forces could not be modeled with traditional approaches. Therefore, an approach has been devised to include the forces in conventional rotordynamic analyses. The forces were approximated by traditional stiffness, damping and inertia coefficients with the addition of whirl-frequency-dependent direct and cross-coupled stiffness terms. The forces were found to be well-modeled with this approach. Finally, the effect these forces had on a simple rotor-bearing system was analyzed, and, therefore, they, in addition to seal forces, were applied to a Jeffcott rotor. The traditional methods of dynamic system analysis were modified to incorporate the impeller forces and yielded results for the eigenproblem, frequency response, critical speed, transient response, and an iterative technique for finding the frequency of free vibration as well as system stability. All results lead to the conclusion that the forces have little influence on natural frequency but can have appreciable effects on system stability. Specifically, at higher values of fluid swirl at the leakage path entrance, relative stability is reduced. The only unexpected response characteristics that occurred are attributed to the nonlinearity of the model.

Copyright © 1991 by The American Society of Mechanical Engineers
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