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contributor authorHartmann, Ulrich
contributor authorHennecke, Christoph
contributor authorDinkelacker, Friedrich
contributor authorSeume, Joerg R.
date accessioned2017-11-25T07:15:41Z
date available2017-11-25T07:15:41Z
date copyright2016/27/9
date issued2017
identifier issn0742-4795
identifier othergtp_139_03_031504.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233627
description abstractA significant challenge in improving the regeneration process of jet engines is the reduction of engine down-time during inspection. As such, early defect detection without engine disassembly will speed up the regeneration process. Defects in the engines hot-gas path (HGP) influence the density distribution of the flow and lead to irregularities in the density distribution of the exhaust jet which can be detected with the optical background-oriented Schlieren (BOS) method in a tomographic setup. The present paper proposes a combination of tomographic BOS measurements and supervised learning algorithms to develop a methodology for an automatic defect detection system. In the first step, the methodology is tested by analyzing the exhaust jet of a swirl burner array with a nonuniform fuel-supply of single burners with tomographic BOS measurements. The measurements are used to implement a support vector machine (SVM) pattern recognition algorithm. It is shown that the reconstruction quality of tomographic BOS measurements is high enough to be combined with pattern recognition algorithms. The results strengthen the hypothesis that it is possible to automatically detect defects in jet engines with tomographic BOS measurements and pattern recognition algorithms.
publisherThe American Society of Mechanical Engineers (ASME)
titleAutomatic Detection of Defects in a Swirl Burner Array Through an Exhaust Jet Pattern Analysis
typeJournal Paper
journal volume139
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4034449
journal fristpage31504
journal lastpage031504-8
treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 003
contenttypeFulltext


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