Sangam: A Confluence of Knowledge Streams

Performance-based fault diagnosis of a gas turbine engine using an integrated support vector machine and artificial neural network method

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dc.creator Fentaye, Amare
dc.creator Ul-Haq Gilani, Syed Ihtsham
dc.creator Baheta, Aklilu Tesfamichael
dc.creator Li, Yi-Guang
dc.date 2018-12-05T14:58:59Z
dc.date 2018-12-05T14:58:59Z
dc.date 2018-11-18
dc.date.accessioned 2022-05-25T16:40:22Z
dc.date.available 2022-05-25T16:40:22Z
dc.identifier AD Fentaye, SI Ul-Haq Gilani, AT Baheta and YG Li. Performance-based fault diagnosis of a gas turbine engine using an integrated support vector machine and artificial neural network method. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, Volume 233, Issue 6, 2019, pp.786-802
dc.identifier 0957-6509
dc.identifier https://doi.org/10.1177/0957650918812510
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/13697
dc.identifier.uri http://localhost:8080/xmlui/handle/CUHPOERS/182549
dc.description An effective and reliable gas path diagnostic method that could be used to detect, isolate, and identify gas turbine degradations is crucial in a gas turbine condition-based maintenance. In this paper, we proposed a new combined technique of artificial neural network and support vector machine for a two-shaft industrial gas turbine engine gas path diagnostics. To this end, an autoassociative neural network is used as a preprocessor to minimize noise and generate necessary features, a nested support vector machine to classify gas path faults, and a multilayer perceptron to assess the magnitude of the faults. The necessary data to train and test the method are obtained from a performance model of the case engine under steady-state operating conditions. The test results indicate that the proposed method can diagnose both single- and multiple-component faults successfully and shows a clear advantage over some other methods in terms of multiple fault diagnosis. Moreover, 5-8 sets of measurements have been used to assess the prediction accuracy, and only a 2.3% difference was observed. This result indicates that the proposed method can be used for multiple fault diagnosis of gas turbines with limited measurements.
dc.language en
dc.publisher SAGE
dc.rights Attribution-NonCommercial 4.0 International
dc.rights http://creativecommons.org/licenses/by-nc/4.0/
dc.subject Sensor
dc.subject gas turbine
dc.subject artificial neural network
dc.subject support vector machine
dc.subject gas path diagnostics
dc.title Performance-based fault diagnosis of a gas turbine engine using an integrated support vector machine and artificial neural network method
dc.type Article


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