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A numerical approach to reduction of NO sub(x) emission from swirl premix burner in a gas turbine combustor

NO sub(x) reduction in EV burners with double cone is investigated numerically by evaluation of the mixing characteristics with the parameter of modified unmixedness and NO sub(x) emission. Modified unmixedness of fuel and air evaluated at the burner exit shows strong correlation with NO sub(x) emis...

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Published in:Applied thermal engineering 2013-09, Vol.59 (1-2), p.454-463
Main Authors: Cho, CH, Baek, G M, Sohn, CH, Cho, J H, Kim, H S
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Language:English
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Baek, G M
Sohn, CH
Cho, J H
Kim, H S
description NO sub(x) reduction in EV burners with double cone is investigated numerically by evaluation of the mixing characteristics with the parameter of modified unmixedness and NO sub(x) emission. Modified unmixedness of fuel and air evaluated at the burner exit shows strong correlation with NO sub(x) emission from a model combustor. Several design changes from a baseline burner have been made to enhance uniform mixing of fuel and air for the purpose of NO sub(x) reduction. Flow and combustion fields in the combustors with the eight modified burners resulting from design changes are simulated and NO sub(x) emissions are calculated. With a burner re-designed for lance injection, where some part of fuel is injected through the top holes of the burner, unmixedness inside the burner has been reduced, i.e., mixing uniformity improved significantly. The numerical data have been compared with available experimental data and the experimental and the numerical results showed appreciable NO sub(x) reduction with several design changes. Another method suggested to reduce NO sub(x) emission is to increase time for mixing of fuel and air through the increase in an interval between fuel holes. The decrease in modified unmixedness is followed by the reduction in NO sub(x) emission. This strong correlation between unmixedness and NO sub(x) emission verifies that NO sub(x) reduction can be attained by mixing enhancement of fuel and air inside the burner.
doi_str_mv 10.1016/j.applthermaleng.2013.06.004
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Modified unmixedness of fuel and air evaluated at the burner exit shows strong correlation with NO sub(x) emission from a model combustor. Several design changes from a baseline burner have been made to enhance uniform mixing of fuel and air for the purpose of NO sub(x) reduction. Flow and combustion fields in the combustors with the eight modified burners resulting from design changes are simulated and NO sub(x) emissions are calculated. With a burner re-designed for lance injection, where some part of fuel is injected through the top holes of the burner, unmixedness inside the burner has been reduced, i.e., mixing uniformity improved significantly. The numerical data have been compared with available experimental data and the experimental and the numerical results showed appreciable NO sub(x) reduction with several design changes. Another method suggested to reduce NO sub(x) emission is to increase time for mixing of fuel and air through the increase in an interval between fuel holes. The decrease in modified unmixedness is followed by the reduction in NO sub(x) emission. 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Another method suggested to reduce NO sub(x) emission is to increase time for mixing of fuel and air through the increase in an interval between fuel holes. The decrease in modified unmixedness is followed by the reduction in NO sub(x) emission. 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subjects Combustion
Correlation
Emission analysis
Emissions control
Fuels
Mathematical models
Reduction
Variability
title A numerical approach to reduction of NO sub(x) emission from swirl premix burner in a gas turbine combustor
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