Five-degree-of-freedom (5-DOF) characterization of the stability of a gas-lubricated conical bearing of the spiral-groove design is presented for bearing numbers up to 500. Critical points in stability analysis are identified in impedance contour plots separately for axial, cylindrical, and conical modes. The stability thresholds with respect to each mode are graphed as functions of the bearing number. For axial and cylindrical modes, the threshold parameter is the rotor mass. For the conical mode, the threshold parameter is an equivalent mass that is dependent on both transverse and polar radii of gyration of the rotor. An application example illustrates a rational procedure to specify nominal bearing clearance and its allowable tolerance range.
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April 2007
Technical Papers
Stability Characteristics of a Rigid Rotor Supported by a Gas-Lubricated Spiral-Groove Conical Bearing
Coda H. T. Pan,
CPan208663@aol.com
Coda H. T. Pan
Global Technology
, Millbury, MA 01525-3361
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Daejong Kim
Daejong Kim
Mechanical Engineering,
djkim@tamu.edu
Texas A&M University
, College Station, TX 77843-3123
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Coda H. T. Pan
Daejong Kim
J. Tribol. Apr 2007, 129(2): 375-383 (9 pages)
Published Online: January 9, 2007
Article history
Received:
May 4, 2006
Revised:
January 9, 2007
Citation
Pan, C. H. T., and Kim, D. (January 9, 2007). "Stability Characteristics of a Rigid Rotor Supported by a Gas-Lubricated Spiral-Groove Conical Bearing." ASME. J. Tribol. April 2007; 129(2): 375–383. https://doi.org/10.1115/1.2647443
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