On nonlinear rotor dynamic effects of aerodynamic bearings with simple flexible rotors

被引：16

作者：

Bou-Saïd, Benyebka ^{[1
]}

Grau, G. ^{[2
]}

Iordanoff, I. ^{[3
]}

机构：

[1] Laboratoire de Mécanique des Contacts et des Solides, INSA, 69 621 Villeurbanne Cedex, Bat. Jean D'Alembert 20 Rue Sci.

[2] Microturbo, Toulouse Cedex 2 31 019

[3] ENSAM

来源：

Journal of Engineering for Gas Turbines and Power | 2008年 / 130卷 / 01期

关键词：

Foil bearings; Gas lubrication; Rotor dynamics; Stability;

D O I：

10.1115/1.2747262

中图分类号：

学科分类号：

摘要：

The last decades have experienced a growing enhancement of aeronautical oil free turbomachinery. The classical linear approach of rotor dynamics commonly uses stiffness and damping coefficients to model journal bearings. In the present study, a nonlinear time dependant calculation is used for the dynamic simulation of a rotor mounted with aerodynamic (gas) bearings. A comparison between the two approaches indicates that the dynamic behavior of such bearings can be nonlinear in operating ranges where the rotor eccentricity reaches high values. In that case, the linear approach may lead to incorrect results and the nonlinear approach should be performed for better rotor dynamic prediction. A numerical procedure which analyzes the dynamic behavior of simple flexible rotors taking into account the nonlinear (transient regime) characteristics of aerodynamic bearings is presented. A simple example highlights the needs of nonlinear simulations in order to predict dynamic performance in oil-free turbomachinery. Copyright © 2008 by ASME.

引用

共 42 条

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