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contributor authorBruno Schuermans
contributor authorFelix Guethe
contributor authorWolfgang Mohr
date accessioned2017-05-09T00:37:34Z
date available2017-05-09T00:37:34Z
date copyrightAugust, 2010
date issued2010
identifier issn1528-8919
identifier otherJETPEZ-27125#081501_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143121
description abstractThis paper deals with a novel approach for measuring thermoacoustic transfer functions. These transfer functions are essential to predict the acoustic behavior of gas turbine combustion systems. Thermoacoustic prediction has become an essential step in the development process of low NOx combustion systems. The proposed method is particularly useful in harsh environments. It makes use of simultaneous measurement of the chemiluminescence of different species in order to obtain the heat release fluctuations via inverse method. Generally, the heat release fluctuation has two contributions: one due to equivalence ratio fluctuations, and the other due to modulations of mass flow of mixture entering the reaction zone. Because the chemiluminescence of one single species depends differently on the two contributions, it is not possible to quantitatively estimate the heat based on this information. Measurement of the transfer matrix based on a purely acoustic method provides quantitative results, independent of the nature of the interaction mechanism. However, this method is difficult to apply in industrial full-scale experiments. The method developed in this work uses the chemiluminescence time traces of several species. After calibration, an overdetermined inverse method is used to calculate the two heat release contributions from the time traces. The optical method proposed here has the advantage that it does not only provide quantitative heat release fluctuations but it also quantifies the underlying physical mechanisms that cause the heat release fluctuations: It shows what part of the heat release is caused by equivalence ratio fluctuations and what part by flame front dynamics. The method was tested on a full scale swirl-stabilized gas turbine burner. Comparison with a purely acoustic method validated the concept.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptical Transfer Function Measurements for Technically Premixed Flames
typeJournal Paper
journal volume132
journal issue8
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3124663
journal fristpage81501
identifier eissn0742-4795
keywordsAcoustics
keywordsTransfer functions
keywordsFluctuations (Physics)
keywordsFlames
keywordsFlow (Dynamics)
keywordsHeat
keywordsMixtures
keywordsMeasurement
keywordsCombustion AND Mechanisms
treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 008
contenttypeFulltext


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