Automatic Detection of Defects in a Swirl Burner Array Through an Exhaust Jet Pattern Analysis
Author:
Hartmann Ulrich1, Hennecke Christoph2, Dinkelacker Friedrich2, Seume Joerg R.3
Affiliation:
1. Institute of Turbomachinery and Fluid Dynamics, Leibniz Universität Hannover, Hannover 30167, Lower Saxony, Germany e-mail: 2. Institute of Technical Combustion, Leibniz Universität Hannover, Hannover 30167, Lower Saxony, Germany 3. Institute of Turbomachinery and Fluid Dynamics, Leibniz Universität Hannover, Hannover 30167, Lower Saxony, Germany
Abstract
A 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.
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference24 articles.
1. Impact of Defects and Damage in Aircraft Engines on the Exhaust Jet,2013 2. Richard, H., Raffel, M., Rein, M., Kompenhans, J., and Meier, G. E. A., 2000, “Demonstration of the Applicability of a Background Oriented Schlieren (BOS) Method,” 10th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, July 10–13, pp. 145–156.10.1007/978-3-662-08263-8_9 3. The Application of Background Oriented Schlieren Method to Aircraft Wake Vortex Investigations,2013 4. Schröder, A., Geisler, R., Schanz, D., Agocs, J., Pallek, D., Schroll, M., Klinner, J., Beversdorff, M., Voges, M., and Willert, C., 2014, “Application of Image Based Measurement Techniques for the Investigation of Aeroengine Performance on a Commercial Aircraft in Ground Operation,” 17th International Symposium on Applications of Laser Techniques to Mechanics, Lisbon, Portugal, July 7–10.http://elib.dlr.de/89806/1/FullPaper_242_SchroederSchroll.pdf 5. Adamczuk, R. R., Hartmann, U., and Seume, J., 2013, “Experimental Demonstration of Analyzing an Engine's Exhaust Jet With the Background-Oriented Schlieren Method,” AIAA Paper No. AIAA 2013-2488.10.2514/6.2013-2488
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