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Optimizing automated gas turbine fault detection using statistical pattern recognition

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dc.contributor.author Loukis, E en
dc.contributor.author Mathioudakis, K en
dc.contributor.author Papailiou, K en
dc.date.accessioned 2014-03-01T01:10:04Z
dc.date.available 2014-03-01T01:10:04Z
dc.date.issued 1994 en
dc.identifier.issn 0742-4795 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/11304
dc.subject Fault Detection en
dc.subject Gas Turbine en
dc.subject Statistical Pattern Recognition en
dc.subject.classification Engineering, Mechanical en
dc.subject.other Automation en
dc.subject.other Compressors en
dc.subject.other Decision theory en
dc.subject.other Failure analysis en
dc.subject.other Identification (control systems) en
dc.subject.other Optimization en
dc.subject.other Pattern recognition en
dc.subject.other Statistical methods en
dc.subject.other Turbomachine blades en
dc.subject.other Decision making en
dc.subject.other Discriminants en
dc.subject.other Fault diagnosis en
dc.subject.other Gas turbines en
dc.title Optimizing automated gas turbine fault detection using statistical pattern recognition en
heal.type journalArticle en
heal.identifier.primary 10.1115/1.2906787 en
heal.identifier.secondary http://dx.doi.org/10.1115/1.2906787 en
heal.language English en
heal.publicationDate 1994 en
heal.abstract A method enabling the automated diagnosis of gas turbine compressor blade faults, based on the principles of statistical pattern recognition, is initially presented. The decision making is based on the derivation of spectral patterns from dynamic measurement data and then the calculation of discriminants with respect to reference spectral patterns of the faults while it takes into account their statistical properties. A method of optimizing the selection of discriminants using dynamic measurement data is also presented. A few scalar discriminants are derived, in such a way that the maximum available discrimination potential is exploited. In this way the success rate of automated decision making is further improved, while the need for intuitive discriminant selection is eliminated. The effectiveness of the proposed methods is demonstrated by application to data coming from an industrial gas turbine while extension to other aspects of fault diagnosis is discussed. en
heal.publisher ASME-AMER SOC MECHANICAL ENG en
heal.journalName Journal of Engineering for Gas Turbines and Power en
dc.identifier.doi 10.1115/1.2906787 en
dc.identifier.isi ISI:A1994MV01500023 en
dc.identifier.volume 116 en
dc.identifier.issue 1 en
dc.identifier.spage 165 en
dc.identifier.epage 171 en


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