A parametric study into the effect of variability in clearance shape and bump foil stiffness distribution in foil-air bearings

Ibrahim Ghalayini, Philip Bonello

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Abstract

The linearised force coefficients method (LFCM) has traditionally been used to study the stability and compute the Campbell diagrams of rotor/foil-air bearing (FAB) systems, despite reported disagreement with low-amplitude dynamics of the nonlinear system. In this paper, a new approach for extracting the Campbell diagram from the Jacobian matrix of the nonlinear state-space model that simultaneously couples the rotor, air film and foil structure domains is used for the first time in a parametric study into the effect of variability in clearance shape and bump foil stiffness distribution in foil-air bearings. The results provide guidelines for improved foil-air bearing design that raises the onset of instability speed.
Original languageEnglish
Title of host publicationVIRM 12: Vibrations in Rotating Machinery conference
ISBN (Electronic)9781003132639
DOIs
Publication statusPublished - 22 Oct 2020
EventVibrations in Rotating Machinery conference - Online
Duration: 14 Oct 202015 Oct 2020

Conference

ConferenceVibrations in Rotating Machinery conference
Abbreviated titleVIRM 12
CityOnline
Period14/10/2015/10/20

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