This paper presents a theoretical model of corrugated foil strip (bump foil) deformation in compliant foil bearings and dampers. The friction forces between bump foils and the housing or the top foil, local interaction forces, variable load distributions, and bump geometries are taken into consideration. Following the trend of earlier published experimental data, the bumps near the fixed end have a much higher predicted stiffness (lower deflection) than those near the free end. Higher friction coefficients tend to increase stiffness and may pin down bumps near the fixed end. An increase in the friction coefficient between the top foil and the bump is a more effective method of achieving both Coulomb damping and higher stiffness. In addition to bump geometry, the load distribution profile greatly influences bump stiffness. A follow-up paper will present the experimental verification and discuss the comparison between theoretical and experimental results.
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April 1992
Research Papers
Compliant Foil Bearing Structural Stiffness Analysis: Part I—Theoretical Model Including Strip and Variable Bump Foil Geometry
C.-P. Roger Ku,
C.-P. Roger Ku
Advanced Technology Department, Mechanical Technology Incorporated, Latham, New York 12110
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H. Heshmat
H. Heshmat
Advanced Technology Department, Mechanical Technology Incorporated, Latham, New York 12110
Search for other works by this author on:
C.-P. Roger Ku
Advanced Technology Department, Mechanical Technology Incorporated, Latham, New York 12110
H. Heshmat
Advanced Technology Department, Mechanical Technology Incorporated, Latham, New York 12110
J. Tribol. Apr 1992, 114(2): 394-400 (7 pages)
Published Online: April 1, 1992
Article history
Received:
January 30, 1991
Revised:
July 1, 1991
Online:
June 5, 2008
Citation
Ku, C. R., and Heshmat, H. (April 1, 1992). "Compliant Foil Bearing Structural Stiffness Analysis: Part I—Theoretical Model Including Strip and Variable Bump Foil Geometry." ASME. J. Tribol. April 1992; 114(2): 394–400. https://doi.org/10.1115/1.2920898
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