1990
DOI: 10.1080/10402009008981979
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Measurement and Calculation of the Dynamic Operating Characteristics of the Five Shoe, Tilting Pad Journal Bearing

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Cited by 43 publications
(25 citation statements)
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“…Brockwell et al [32] reported additional results for the same rig, bearing and identification method for rotational speeds of 900rpm, 1800rpm, 2700rpm, and 3600rpm. Horizontal stiffness and damping values at 3600rpm were not reported due to a resonance in the test rig frame.…”
Section: Sinusoidal Excitation Without Comprehensivementioning
confidence: 89%
See 1 more Smart Citation
“…Brockwell et al [32] reported additional results for the same rig, bearing and identification method for rotational speeds of 900rpm, 1800rpm, 2700rpm, and 3600rpm. Horizontal stiffness and damping values at 3600rpm were not reported due to a resonance in the test rig frame.…”
Section: Sinusoidal Excitation Without Comprehensivementioning
confidence: 89%
“…The rotor was run below the first critical speed and was supported in two cylindrical test bearings. The advantage is that sinusoidal excitation can be applied at any excitation frequency up to the exciter limits, although some experiments have been limited to synchronous excitation [30][31][32][33].…”
Section: Sinusoidal Excitationmentioning
confidence: 99%
“…Stiffness coefficients had about an order of magnitude less uncertainty than the damping coefficients. The method is applicable to rigs in which steady state sinusoidal loads are used to excite a journal bearing on a rigid rotor (1)-(4), (7), (9)-( l l ) , (17), (18).…”
Section: Experimental Rigmentioning
confidence: 99%
“…Then, the bearing stiffness and damping coefficients are readily estimated by measuring the instantaneous force (magnitude and phase) at the precise instant of time when the displacements (x,y) or velocities (ẋ,ẏ) of the bearing housing are exactly zero. Brockwell, et al (7) use this method for identification of stiffness and damping force coefficients of a five-pad, tilting pad journal bearing with satisfactory results for small orbital motions.…”
Section: Introductionmentioning
confidence: 96%