In situ identification strategy of thermoacoustic stability in annular combustors

In annular combustion systems, thermoacoustic eigenmodes can manifest as standing waves, traveling waves or some form in between. Which dynamic solution appears in a combustor depends on details, regarding the flow field and (unintentional) breaking of the cylindrical symmetry of the annular combust...

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Main Authors: Driek Rouwenhorst, Jakob Hermann, Wolfgang Polifke
Format: Article
Language:English
Published: SAGE Publishing 2018-12-01
Series:International Journal of Spray and Combustion Dynamics
Online Access:https://doi.org/10.1177/1756827718799043
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spelling doaj-f2e873f96d614aa1a36de6e84b81e6a12020-11-25T03:01:07ZengSAGE PublishingInternational Journal of Spray and Combustion Dynamics1756-82771756-82852018-12-011010.1177/1756827718799043In situ identification strategy of thermoacoustic stability in annular combustorsDriek Rouwenhorst0Jakob Hermann1Wolfgang Polifke2IfTA GmbH, Gröbenzell, GermanyIfTA GmbH, Gröbenzell, GermanyProfessur für Thermofluiddynamik, Technical University of Munich, Garching, GermanyIn annular combustion systems, thermoacoustic eigenmodes can manifest as standing waves, traveling waves or some form in between. Which dynamic solution appears in a combustor depends on details, regarding the flow field and (unintentional) breaking of the cylindrical symmetry of the annular combustion system. When these details are unknown, the specific behavior cannot be predicted from the characteristics of a single burner. Due to the (nearly) degenerate nature of the acoustic solution, annular eigenmodes come in pairs with practically the same eigenfrequency. In order to identify the thermoacoustic modes, conventional analysis of a spectral peak from a measurement does not suffice, because the peak is a superposition of the two eigenmodes. A method has been proposed to identify the two eigenmodes of given azimuthal mode order from multiple simultaneous measurements around the circumference of the combustion system. Using output-only identification on the acoustic signals, it is possible to estimate the individual mode shapes, frequencies and growth rates of the co-existing eigenmode pair. In this work, the strategy is applied to experimental data from an annular combustor. A split in the growth rate pair is observed during stable operation, depending on the equivalence ratio and flame-to-flame distance. It shows that in situ identification of annular thermoacoustics can reveal subtle dynamic effects, which is useful for testing and online monitoring of annular combustors. The moment when instability occurs can be foreseen under prevailing conditions, with simultaneous identification of the azimuthal mode structure.https://doi.org/10.1177/1756827718799043
collection DOAJ
language English
format Article
sources DOAJ
author Driek Rouwenhorst
Jakob Hermann
Wolfgang Polifke
spellingShingle Driek Rouwenhorst
Jakob Hermann
Wolfgang Polifke
In situ identification strategy of thermoacoustic stability in annular combustors
International Journal of Spray and Combustion Dynamics
author_facet Driek Rouwenhorst
Jakob Hermann
Wolfgang Polifke
author_sort Driek Rouwenhorst
title In situ identification strategy of thermoacoustic stability in annular combustors
title_short In situ identification strategy of thermoacoustic stability in annular combustors
title_full In situ identification strategy of thermoacoustic stability in annular combustors
title_fullStr In situ identification strategy of thermoacoustic stability in annular combustors
title_full_unstemmed In situ identification strategy of thermoacoustic stability in annular combustors
title_sort in situ identification strategy of thermoacoustic stability in annular combustors
publisher SAGE Publishing
series International Journal of Spray and Combustion Dynamics
issn 1756-8277
1756-8285
publishDate 2018-12-01
description In annular combustion systems, thermoacoustic eigenmodes can manifest as standing waves, traveling waves or some form in between. Which dynamic solution appears in a combustor depends on details, regarding the flow field and (unintentional) breaking of the cylindrical symmetry of the annular combustion system. When these details are unknown, the specific behavior cannot be predicted from the characteristics of a single burner. Due to the (nearly) degenerate nature of the acoustic solution, annular eigenmodes come in pairs with practically the same eigenfrequency. In order to identify the thermoacoustic modes, conventional analysis of a spectral peak from a measurement does not suffice, because the peak is a superposition of the two eigenmodes. A method has been proposed to identify the two eigenmodes of given azimuthal mode order from multiple simultaneous measurements around the circumference of the combustion system. Using output-only identification on the acoustic signals, it is possible to estimate the individual mode shapes, frequencies and growth rates of the co-existing eigenmode pair. In this work, the strategy is applied to experimental data from an annular combustor. A split in the growth rate pair is observed during stable operation, depending on the equivalence ratio and flame-to-flame distance. It shows that in situ identification of annular thermoacoustics can reveal subtle dynamic effects, which is useful for testing and online monitoring of annular combustors. The moment when instability occurs can be foreseen under prevailing conditions, with simultaneous identification of the azimuthal mode structure.
url https://doi.org/10.1177/1756827718799043
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