This paper presents the effect of preload, as one of the design parameters, on nonlinear dynamic behavior of a rigid rotor supported by gas-lubricated noncircular journal bearings. A finite element method has been employed to solve the Reynolds equation in static and dynamical states and the dynamical equations are solved using the Runge-Kutta method. To analyze the behavior of the rotor center in horizontal and vertical directions under different operating conditions, dynamic trajectory, power spectra, Poincare maps, and bifurcation diagrams are used. Results of this study reveal how the complex dynamic behavior of two types of noncircular bearing systems comprising periodic, KT-periodic, and quasi-periodic responses of the rotor center varies with changes in preload value.
NomenclaturēC Conventional radial clearance (m) C m Minor clearance when rotor and bearing geometric centers are coincident (m) D Rotor diameter (m) F X 0 ,F Y 0 Components of the fluid film force on the rotor in the steady state (N) F X ,F Y Components of the fluid film force on the rotor in the dynamical state (N) W 0 Static load (N) h Film thickness (m) L Bearing length (m) m r Rotor mass (Kg) N i Shape function n e Number of nodes in an element n f Number of nodes in fluid domain P * Absolute gas pressure (N/m 2 ) P Partial gas pressure (N/m 2 ) P a Ambient pressure (N/m 2 ) R Rotor radius (m) t Time (s) U Peripheral speed of the rotor in dynamical state (m/s) X,Ȳ Cartesian axes with origin at the bearing geometric center (m) X j 0 ,Ȳ j 0 Coordinates of the rotor center in steady state (m) X j ,Ȳ j Coordinates of the rotor center in dynamical state (m) 232 R. Rashidi et al.