dc.contributor.author | Aretakis, N | en |
dc.contributor.author | Roumeliotis, I | en |
dc.contributor.author | Mathioudakis, K | en |
dc.date.accessioned | 2014-03-01T02:52:44Z | |
dc.date.available | 2014-03-01T02:52:44Z | |
dc.date.issued | 2010 | en |
dc.identifier.uri | https://dspace.lib.ntua.gr/xmlui/handle/123456789/36028 | |
dc.relation.uri | http://www.scopus.com/inward/record.url?eid=2-s2.0-82055190160&partnerID=40&md5=532fe213fdae1f868ebd340a885dacff | en |
dc.subject.other | 1-D models | en |
dc.subject.other | Component faults | en |
dc.subject.other | Component model | en |
dc.subject.other | Compressor performance | en |
dc.subject.other | Current performance | en |
dc.subject.other | Diagnostic engines | en |
dc.subject.other | Diagnostic methods | en |
dc.subject.other | Empirical knowledge | en |
dc.subject.other | Engine components | en |
dc.subject.other | Engine models | en |
dc.subject.other | Fault identifications | en |
dc.subject.other | Gas path components | en |
dc.subject.other | Measurement data | en |
dc.subject.other | Multistage compressor | en |
dc.subject.other | Performance Model | en |
dc.subject.other | Stage stacking | en |
dc.subject.other | Compressors | en |
dc.subject.other | Electric fault currents | en |
dc.subject.other | Machine design | en |
dc.subject.other | Marine engines | en |
dc.title | Performance model ""zooming"" for in-depth component fault diagnosis | en |
heal.type | conferenceItem | en |
heal.publicationDate | 2010 | en |
heal.abstract | A method giving the possibility for a more detailed gas path component fault diagnosis, by exploiting the ""zooming"" feature of current performance modelling techniques, is presented. A diagnostic engine performance model is the main tool that points to the faulty engine component. A diagnostic component model is then used to identify the fault. The method is demonstrated on the case of compressor faults. A 1-D model based on the ""stage stacking"" approach is used to ""zoom"" into the compressors, supporting a 0-D engine model. A first level diagnosis determines the deviation of overall compressor performance parameters, while ""zooming"" calculations allow a localization of the faulty stages of a multistage compressor. The possibility to derive more detailed information with no additional measurement data is established, by incorporation of empirical knowledge on the type of faults that are usually encountered in practice. Although the approach is based on known individual diagnostic methods, it is demonstrated that the integrated formulation provides not only higher effectiveness but also additional fault identification capabilities. Copyright © 2010 by ASME. | en |
heal.journalName | Proceedings of the ASME Turbo Expo | en |
dc.identifier.volume | 3 | en |
dc.identifier.spage | 307 | en |
dc.identifier.epage | 317 | en |
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