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DC Field | Value | Language |
---|---|---|
dc.contributor.author | Matthew O.T. Cole | en_US |
dc.contributor.author | Chakkapong Chamroon | en_US |
dc.contributor.author | Prinya Ngamprapasom | en_US |
dc.date.accessioned | 2018-09-04T04:45:25Z | - |
dc.date.available | 2018-09-04T04:45:25Z | - |
dc.date.issued | 2010-12-01 | en_US |
dc.identifier.other | 2-s2.0-82055161073 | en_US |
dc.identifier.other | 10.1115/GT2010-23246 | en_US |
dc.identifier.uri | https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=82055161073&origin=inward | en_US |
dc.identifier.uri | http://cmuir.cmu.ac.th/jspui/handle/6653943832/50770 | - |
dc.description.abstract | Synchronous 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.subject | Engineering | en_US |
dc.title | Force feedback control for active stabilization of synchronous whirl orbits in rotor systems with non-linear stiffness elements | en_US |
dc.type | Conference Proceeding | en_US |
article.title.sourcetitle | Proceedings of the ASME Turbo Expo | en_US |
article.volume | 6 | en_US |
article.stream.affiliations | Chiang Mai University | en_US |
Appears in Collections: | CMUL: Journal Articles |
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