Abstract

The dry lubricated bump-type foil air bearing enables a carrying load capacity due to a pressure build up in a convergent air film. Since the air bearing provides low power dissipation above the lift-off speed and the flexible foil provides an adaptivity against high temperatures, manufacturing errors or rotor growth, the bump-type foil air bearing is in particular suitable for high speed rotating machineries. The corresponding dynamic behavior depends on the operational parameters, the behavior of the flexible foil structure, and in particular on the circumferential clearance. In order to avoid or suppress the critical subsynchronous motion at high rotational speeds, many researchers recommend adding an aerodynamic preload to the bore shape, representing a transition from a circular to a lobed bearing bore shape. In addition to positive effects on the stability, preliminary studies demonstrated degrading effects on the stiffness and damping due to increasing preload values. This observation leads to the assumption, that the preload value meets an optimum with respect to stability, load-capacity, and lift-off speed. With the aim of deriving an appropriate lobe configuration for the design of the bump-type foil air bearing, this work performs comprehensive numerical investigations on the dynamic performance and the stability characteristic as a function of preload and minimum clearance. To this end, this work uses steady-state and transient stability analysis methods to recommend optimal aeroydnamic preload values with respect to the corresponding minimum clearance.

Highlights

  • Among sustainable power units, the hydrogen fuel cell has gained importance, containing a high speed rotating air compressor

  • In order to fully understand the influence of the aerodynamic preload on the dynamic performance and stability, this study covers a wide range of lobed bearing configurations from r p /cm = 0 to r p /cm = 12

  • The present study investigates the influence of the aerodynamic preload and the minimum clearance in a context with the dynamic performance and the stability characteristic of the bump-type foil air bearing

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Summary

Introduction

The hydrogen fuel cell has gained importance, containing a high speed rotating air compressor. Recent conceptual studies use the influence of the aerodynamic preload to adapt the dynamic performance to the existing operational parameters In this context, amongst other authors, Sadri et al [10,11] and Feng et al [12] apply actuation systems on the bearing housing, gradually transfering the bearing bore shape from a circular shape to a lobed shape during the rotor speed-up. Both parameters have an evident influence on the stability of the system, and their stabilizing effects must be considered separately To this end, the following study in particular highlights the stability influence of the preload factor r p and the minimum clearance cm on the bump-type foil air bearing, using a steady-state (linear) and a transient (nonlinear) prediction method. The linear and the transient procedure are compared to show the benefits of the linear stability analysis

Bump-Type Foil Air Bearing Model
Steady-State Analysis
Transient Analysis
Parametric Study
Dynamic Performance
Stability Analysis
Parameter Optimization
Conclusions
Full Text
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