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Radial compressor fault identification using dynamic measurement data

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dc.contributor.author Aretakis, N en
dc.contributor.author Mathioudakis, K en
dc.date.accessioned 2014-03-01T02:48:26Z
dc.date.available 2014-03-01T02:48:26Z
dc.date.issued 1996 en
dc.identifier.issn 04021215 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/33807
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-17344394527&partnerID=40&md5=a1bb099e0be675d5e5cf4a5b4aea085f en
dc.subject.other Casing vibration en
dc.subject.other Fault identification en
dc.subject.other Fault signatures en
dc.subject.other Impeller fouling en
dc.subject.other Impeller tip clearance en
dc.subject.other Inlet obstruction en
dc.subject.other Mechanical alterations en
dc.subject.other Radial compressors en
dc.subject.other Sound emission en
dc.subject.other Vaned diffuser en
dc.subject.other Acoustic emissions en
dc.subject.other Acoustic variables measurement en
dc.subject.other Diffusers (fluid) en
dc.subject.other Error detection en
dc.subject.other Failure analysis en
dc.subject.other Monitoring en
dc.subject.other Performance en
dc.subject.other Pressure measurement en
dc.subject.other Rotors en
dc.subject.other Vibration measurement en
dc.subject.other Compressors en
dc.title Radial compressor fault identification using dynamic measurement data en
heal.type conferenceItem en
heal.publicationDate 1996 en
heal.abstract The exploitation of different unsteady quantity measurements for identifying mechanical alterations on a radial compressor with a vaned diffuser is examined in this paper. Measurements of sound emission, casing vibration and unsteady inner wall pressure are performed. The mechanical alterations considered have been chosen in order to reproduce or simulate faults in the compressor. They include the insertion of an inlet obstruction, an obstruction in a diffuser passage, variation of impeller tip clearance, and impeller fouling. Processing these measurement data leads to the derivation of fault signatures which can be utilized for identifying them. The suitability of measuring each of the above physical quantities is discussed with respect to their sensitivity to particular faults. The dependence of the fault signatures on operating point is also examined. It's demonstrated that minor faults which do not affect compressor operation and are not detectable by performance monitoring, can possibly be detected by the proposed methodology. en
heal.journalName American Society of Mechanical Engineers (Paper) en


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