Please use this identifier to cite or link to this item: http://cmuir.cmu.ac.th/jspui/handle/6653943832/50770
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dc.contributor.authorMatthew O.T. Coleen_US
dc.contributor.authorChakkapong Chamroonen_US
dc.contributor.authorPrinya Ngamprapasomen_US
dc.date.accessioned2018-09-04T04:45:25Z-
dc.date.available2018-09-04T04:45:25Z-
dc.date.issued2010-12-01en_US
dc.identifier.other2-s2.0-82055161073en_US
dc.identifier.other10.1115/GT2010-23246en_US
dc.identifier.urihttps://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=82055161073&origin=inwarden_US
dc.identifier.urihttp://cmuir.cmu.ac.th/jspui/handle/6653943832/50770-
dc.description.abstractSynchronous vibration in rotor systems having bearings, seals or other elements with non-linear stiffness characteristics is prone to amplitude jump when operating close to critical speeds as there may be two or more possible whirl responses for a given unbalance condition. This paper describes research on the use of active control methods for eliminating this potentially undesirable behavior. A control scheme based on direct feedback of rotor-stator interaction forces is considered. Modelbased conditions for stability of low amplitude whirl, derived using Lyapunov's direct method, are used as a basis for synthesizing controller gains. Subsidiary requirements for existence of a static feedback control law that can achieve stabilization are also explained. An experimental validation is undertaken on a flexible rotor test rig where non-linear rotorstator contact interaction can occur across a small radial clearance in one transverse plane. A single radial active magnetic bearing is used to apply control forces in a separate transverse plane. The experiments confirm the conditions under which static feedback of the measured interaction force can prevent degenerate whirl responses so that the low amplitude contact-free orbit is the only possible steady-state response. The gain synthesis method leads to controllers that are physically realizable and can eliminate amplitude jump over a range of running speeds. Copyright © 2010 by ASME.en_US
dc.subjectEngineeringen_US
dc.titleForce feedback control for active stabilization of synchronous whirl orbits in rotor systems with non-linear stiffness elementsen_US
dc.typeConference Proceedingen_US
article.title.sourcetitleProceedings of the ASME Turbo Expoen_US
article.volume6en_US
article.stream.affiliationsChiang Mai Universityen_US
Appears in Collections:CMUL: Journal Articles

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