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Enhanced fault localization using probabilistic fusion with gas path analysis algorithms

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dc.contributor.author Kyriazis, A en
dc.contributor.author Mathioudakis, K en
dc.date.accessioned 2014-03-01T01:30:21Z
dc.date.available 2014-03-01T01:30:21Z
dc.date.issued 2009 en
dc.identifier.issn 0742-4795 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/19559
dc.subject Fault Localization en
dc.subject Path Analysis en
dc.subject.classification Engineering, Mechanical en
dc.subject.other Component performance deviation en
dc.subject.other Diagnostic problem en
dc.subject.other Engine components en
dc.subject.other Fault identifications en
dc.subject.other Fault localization en
dc.subject.other Fault probabilities en
dc.subject.other Gas path en
dc.subject.other Gas path analysis en
dc.subject.other Two-stage process en
dc.subject.other Regression analysis en
dc.subject.other Algorithms en
dc.title Enhanced fault localization using probabilistic fusion with gas path analysis algorithms en
heal.type journalArticle en
heal.identifier.primary 10.1115/1.3078793 en
heal.identifier.secondary http://dx.doi.org/10.1115/1.3078793 en
heal.identifier.secondary 051601 en
heal.language English en
heal.publicationDate 2009 en
heal.abstract A method for gas turbine fault identification from gas path data, in situations with a limited number of measurements, is presented. The method consists of a two stage process: (a) localization of the component or group of components with a fault and (b) fault identification by determining the precise location and magnitude of component performance deviations. The paper focuses on methods that allow improved localization of the faulty components. Gas path analysis (GPA) algorithms are applied to diagnostic sets comprising different combinations of engine components. The results are used to derive fault probabilities, which are then fused to derive a conclusion as to the location of a fault. Once the set of possible faulty components is determined, a well defined diagnostic problem is formulated and the faulty parameters are determined by means of a suitable algorithm. It is demonstrated that the method has an improved effectiveness when compared with previous GPA based methods. [DOI: 10.1115/1.3078793] en
heal.publisher ASME-AMER SOC MECHANICAL ENG en
heal.journalName Journal of Engineering for Gas Turbines and Power en
dc.identifier.doi 10.1115/1.3078793 en
dc.identifier.isi ISI:000266967200003 en
dc.identifier.volume 131 en
dc.identifier.issue 5 en


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