This paper describes a procedure suitable for field implementation that allows identification of synchronous bearing support parameters (force coefficients) from recorded rotor responses to imbalance. The experimental validation is conducted on a test rotor supported on two dissimilar bearing supports, both mechanically complex, each comprising a hydrodynamic film bearing in series with a squeeze film damper and elastic support structure. The identification procedure requires a minimum of two different imbalance distributions for identification of force coefficients from the two bearing supports. Presently, the test rotor responses show minimal cross-coupling effects, as also predicted by analysis, and the identification procedure disregards cross-coupled force coefficients thereby reducing its sensitivity to small variations in the measured response. The procedure renders satisfactory force coefficients in the speed range between 1500 and , enclosing the rotor-bearing system first critical speed. The identified direct force coefficients are in accordance with those derived from the impact load excitations presented in a companion paper.
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January 2007
Technical Papers
Field Methods for Identification of Bearing Support Parameters—Part II: Identification From Rotor Dynamic Response due to Imbalances
Luis San Andrés
Luis San Andrés
Mast-Childs Tribology Professor
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Oscar C. De Santiago
Luis San Andrés
Mast-Childs Tribology Professor
J. Eng. Gas Turbines Power. Jan 2007, 129(1): 213-219 (7 pages)
Published Online: March 1, 2003
Article history
Received:
October 1, 2002
Revised:
March 1, 2003
Citation
De Santiago, O. C., and San Andrés, L. (March 1, 2003). "Field Methods for Identification of Bearing Support Parameters—Part II: Identification From Rotor Dynamic Response due to Imbalances." ASME. J. Eng. Gas Turbines Power. January 2007; 129(1): 213–219. https://doi.org/10.1115/1.2227034
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