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Transient Response of Rotor on Rolling Element Bearings with Clearance

 

David P. Fleming                                                Brian T. Murphy

NASA Glenn Research Center                                                RMA, Inc.

Cleveland, OH 44135, USA                                                      7701 Baja Cove

David.P.Fleming@nasa.gov                                                    Austin, TX 78759, USA

                                                                                                      bmurphy@xlrotor.com 

 

J. V. Poplawski                                                   Jerzy T. Sawicki

J. V. Poplawski and Associates                                              Cleveland State University

Bethlehem, PA 18018, USA                                                     Cleveland, OH 44115, USA.

Jvpoplawski@aol.com                                              j.sawicki@csuohio.edu

 

Published:  May 2007

Abstract


Internal clearance in rolling element bearings is usually present to allow for radial and axial growth of the rotor-bearing system and to accommodate bearing fit-up. The presence of this clearance also introduces a "dead band" into the load-deflection behavior of the bearing. Previous studies demonstrated that the presence of dead band clearance might have a significant effect on synchronous rotor response. In this work, the authors investigate transient response of a rotor supported on rolling element bearings with internal clearance. In addition, the stiffness of the bearings varies nonlinearly with bearing deflection and with speed. Bearing properties were accurately calculated with a state of the art rolling bearing analysis code. The subsequent rotordynamics analysis shows that for rapid acceleration rates the maximum response amplitude may be less than predicted by steady-state analysis. The presence of clearance may shift the critical speed location to lower speed values. The rotor vibration response exhibits subharmonic components which are more prominent with bearing clearance.

Full Text (PDF)

Introduction


Response of all but very flexible rotors depends strongly on bearing properties. When bearings are nonlinear, accurate rotor response calculations require use of bearing properties for the precise conditions encountered, rather than average properties. While fluid film bearings are often reasonably linear for small deflections (although there is usually a strong speed dependence), rolling-element bearings have a much less linear force-displacement relationship. Two aspects of rolling element bearings contribute further to nonlinearity. First, the bearings are often fabricated with internal clearance, or deadband. For example, in a 25 mm bore deep-groove ball bearing, the internal radial clearance (IRC) is typically between 4 and 13 μm. (For rotordynamic purposes it is most convenient to use bearing radial clearance as is done herein. However, bearing engineers more typically use internal diametral clearance (IDC), which is twice the internal radial clearance). Second, at speed, centrifugal forces move the rolling elements outward, increasing the clearance between the inner race and the rolling elements.

The rotordynamic software XLRotor was used to perform all numerical integrations. XLRotor was selected because it enables the use of user-defined routines for nonlinear elements. For this study, a Microsoft Excel Visual Basic Macro was written which computes the bearing reaction force as a function of both speed and deflection via a curve fit of the COBRA data.  For transient analysis, XLRotor provides several different numerical integration schemes, all of which are implicit and unconditionally stable. These types of integration schemes permit efficient integration of the full unreduced system of differential equations.

Fig 1: Sketch of Rotor

Fig 2: Critical Speed map

Fig 3: The Rotor response over a speed range from 10000 rpm to 80000 rpm for these values of internal radial clearance and four acceleration rates with the rotor axis vertical (i.e., no gravity load on the bearings)



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