Experimental investigations of ion current in liquid-fuelled gas turbine combustors

This work covers investigations of the static and dynamic behaviour of a confined, co-swirled and liquid-fuelled airblast injection system. The focus lies on the application of ion current sensors for the qualitative measurement of the heat release rate or for flame monitoring purposes in complex te...

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Main Authors: J Christopher Wollgarten, Nikolaos Zarzalis, Fabio Turrini, Antonio Peschiulli
Format: Article
Language:English
Published: SAGE Publishing 2017-09-01
Series:International Journal of Spray and Combustion Dynamics
Online Access:https://doi.org/10.1177/1756827716688477
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spelling doaj-46d3e175323a40d6ab66e615476275f52020-11-25T03:44:02ZengSAGE PublishingInternational Journal of Spray and Combustion Dynamics1756-82771756-82852017-09-01910.1177/1756827716688477Experimental investigations of ion current in liquid-fuelled gas turbine combustorsJ Christopher WollgartenNikolaos ZarzalisFabio TurriniAntonio PeschiulliThis work covers investigations of the static and dynamic behaviour of a confined, co-swirled and liquid-fuelled airblast injection system. The focus lies on the application of ion current sensors for the qualitative measurement of the heat release rate or for flame monitoring purposes in complex technical combustion processes. The ion current sensor is to operate in a feedback control loop in order to react on combustion dynamics in real time. The first part of the work analyses experimental data, which were obtained with different techniques, e.g. dynamic pressure, chemiluminescence, fine-wire thermocouples and ion current. The results show that the thermo-acoustic instability and the precessing vortex core generate an interaction mode. The frequency of this interaction mode is the difference of the other two modes. This has not yet been observed for partially premixed and liquid-fuelled injection systems before and also was not detected by the chemiluminescence of the flame. The ion current measurement technique is able to detect the helical mode of the precessing vortex core as well as the interaction frequency, leading to the conclusion that the chemical reactions are influenced by this helical structure. Contour maps of the frequencies reveal this influence in the outer shear layer. The second part of the study focused on the ion current probe as a method to predict static combustion instabilities, such as lean blowout. According to the results, the ion current is a fast responding method to detect lean blowout, provided that the detector is mounted at a suitable position. Measurements at different positions in the flame were compared with phase-locked chemiluminescence measurements. Precursors in the ion current signal for lean-blowout prediction were found using a statistical approach, which is based on ion peak distance. The precursor events allow for the use of this approach with a feedback control loop in future applications.https://doi.org/10.1177/1756827716688477
collection DOAJ
language English
format Article
sources DOAJ
author J Christopher Wollgarten
Nikolaos Zarzalis
Fabio Turrini
Antonio Peschiulli
spellingShingle J Christopher Wollgarten
Nikolaos Zarzalis
Fabio Turrini
Antonio Peschiulli
Experimental investigations of ion current in liquid-fuelled gas turbine combustors
International Journal of Spray and Combustion Dynamics
author_facet J Christopher Wollgarten
Nikolaos Zarzalis
Fabio Turrini
Antonio Peschiulli
author_sort J Christopher Wollgarten
title Experimental investigations of ion current in liquid-fuelled gas turbine combustors
title_short Experimental investigations of ion current in liquid-fuelled gas turbine combustors
title_full Experimental investigations of ion current in liquid-fuelled gas turbine combustors
title_fullStr Experimental investigations of ion current in liquid-fuelled gas turbine combustors
title_full_unstemmed Experimental investigations of ion current in liquid-fuelled gas turbine combustors
title_sort experimental investigations of ion current in liquid-fuelled gas turbine combustors
publisher SAGE Publishing
series International Journal of Spray and Combustion Dynamics
issn 1756-8277
1756-8285
publishDate 2017-09-01
description This work covers investigations of the static and dynamic behaviour of a confined, co-swirled and liquid-fuelled airblast injection system. The focus lies on the application of ion current sensors for the qualitative measurement of the heat release rate or for flame monitoring purposes in complex technical combustion processes. The ion current sensor is to operate in a feedback control loop in order to react on combustion dynamics in real time. The first part of the work analyses experimental data, which were obtained with different techniques, e.g. dynamic pressure, chemiluminescence, fine-wire thermocouples and ion current. The results show that the thermo-acoustic instability and the precessing vortex core generate an interaction mode. The frequency of this interaction mode is the difference of the other two modes. This has not yet been observed for partially premixed and liquid-fuelled injection systems before and also was not detected by the chemiluminescence of the flame. The ion current measurement technique is able to detect the helical mode of the precessing vortex core as well as the interaction frequency, leading to the conclusion that the chemical reactions are influenced by this helical structure. Contour maps of the frequencies reveal this influence in the outer shear layer. The second part of the study focused on the ion current probe as a method to predict static combustion instabilities, such as lean blowout. According to the results, the ion current is a fast responding method to detect lean blowout, provided that the detector is mounted at a suitable position. Measurements at different positions in the flame were compared with phase-locked chemiluminescence measurements. Precursors in the ion current signal for lean-blowout prediction were found using a statistical approach, which is based on ion peak distance. The precursor events allow for the use of this approach with a feedback control loop in future applications.
url https://doi.org/10.1177/1756827716688477
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