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contributor authorKoskoletos, Anastasios O.
contributor authorAretakis, Nikolaos
contributor authorAlexiou, Alexios
contributor authorRomesis, Christoforos
contributor authorMathioudakis, Konstantinos
date accessioned2019-02-28T10:57:43Z
date available2019-02-28T10:57:43Z
date copyright11/29/2018 12:00:00 AM
date issued2018
identifier issn0742-4795
identifier othergtp_140_12_121016.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251196
description abstractPropulsion diagnostic method evaluation strategy (ProDiMES) offers an aircraft engine diagnostic benchmark problem where the performance of candidate diagnostic methods is evaluated while a fair comparison can be established. In the present paper, the performance evaluation of a number of gas turbine diagnostic methods using the ProDiMES software is presented. All diagnostic methods presented here were developed at the Laboratory of Thermal Turbomachinery of the National Technical University of Athens (LTT/NTUA). Component, sensor, and actuator fault scenarios that occur in a fleet of deteriorated twin-spool turbofan engines are considered. The performance of each diagnostic method is presented through the evaluation metrics introduced in the ProDiMES software. Remarks about each methods performance as well as the detectability and classification rates of each fault scenario are made.
publisherThe American Society of Mechanical Engineers (ASME)
titleEvaluation of Aircraft Engine Gas Path Diagnostic Methods Through ProDiMES
typeJournal Paper
journal volume140
journal issue12
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4040909
journal fristpage121016
journal lastpage121016-12
treeJournal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 012
contenttypeFulltext


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