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RESEARCH PAPERS: Gas Turbines: Structures and Dynamics

Characterization of Laws of Friction in the Context of Engine Blade Dynamics

[+] Author and Article Information
A. V. Srinivasan

Worcester Polytechnic Institute, Department of Mechanical Engineering, 100 Institute Road, Worcester, MA 01609-2282

D. M. McFarland

Department of Mechanical Engineering, University of Connecticut, Storrs, CT 06269-3139

J. Eng. Gas Turbines Power 120(4), 759-765 (Oct 01, 1998) (7 pages) doi:10.1115/1.2818464 History: Received February 06, 1998; Online November 19, 2007

Abstract

Experience has shown that energy dissipation due to rubbing at interfaces of engine blade shrouds provides damping of bladed disk assemblies. An accurate estimate of such damping has been a subject of study for more that a decade. The most difficult parameter that influences its accurate calculation pertains to an appropriate definition of the laws of friction that relate the rubbing motion with the forces induced. This paper develops an analysis that leads to a mathematical relationship between the forces of friction damping at a vibrating interface and the corresponding relative motion. The analysis permits calculation of forces at the interface if the displacements are known or vice. The equations are cast in terms of relative motion between mating shrouds so that degenerate cases of fully locked and freely slipping can be calculated. Examples are given showing simulation results obtained using discrete structural models. Extension of the analysis to the case of a full assembly is discussed.

Copyright © 1998 by The American Society of Mechanical Engineers
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