Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine
The combustion process and pollutant emission of an annular combustion chamber for a heavy-duty gas turbine were investigated by numerical method. The realizable k-ε model and finite rate/eddy dissipation model were adopted for calculations of turbulence and combustion. The effects of different swir...
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EDP Sciences
2019-01-01
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doaj-3918bd96e1af48d69a28cf5f130b61092021-03-02T10:16:56ZengEDP SciencesE3S Web of Conferences2267-12422019-01-011180403810.1051/e3sconf/201911804038e3sconf_icaeer18_04038Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas TurbineGao Huanhuan0Fu Zaiguo1Zeng Zhuoxiong2Liu Jiang3Weng Peifen4College of Energy and Mechanical Engineering, Shanghai University of Electric PowerCollege of Energy and Mechanical Engineering, Shanghai University of Electric PowerCollege of Energy and Mechanical Engineering, Shanghai University of Electric PowerCollege of Energy and Mechanical Engineering, Shanghai University of Electric PowerCollege of Energy and Mechanical Engineering, Shanghai University of Electric PowerThe combustion process and pollutant emission of an annular combustion chamber for a heavy-duty gas turbine were investigated by numerical method. The realizable k-ε model and finite rate/eddy dissipation model were adopted for calculations of turbulence and combustion. The effects of different swirling numbers of the double-swirler inlet on the temperature distribution and the thermal NOx formation in the combustion chamber were analyzed. The results show that the change of the swirling number of the outer swirling flow has a greater influence on the generation of the thermal NOx when compared with that of the inner swirling flow. The maximum average temperature of the central cross section of the combustor does not exceed 1760K. The average mass fraction of the generated thermal NOx at the exit decreases with the increasing outer swirling number. When the outer swirling number is less than 0.8, the generation of the thermal NOx is severe at the side wall of the combustion chamber.https://www.e3s-conferences.org/articles/e3sconf/pdf/2019/44/e3sconf_icaeer18_04038.pdf |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Gao Huanhuan Fu Zaiguo Zeng Zhuoxiong Liu Jiang Weng Peifen |
spellingShingle |
Gao Huanhuan Fu Zaiguo Zeng Zhuoxiong Liu Jiang Weng Peifen Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine E3S Web of Conferences |
author_facet |
Gao Huanhuan Fu Zaiguo Zeng Zhuoxiong Liu Jiang Weng Peifen |
author_sort |
Gao Huanhuan |
title |
Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine |
title_short |
Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine |
title_full |
Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine |
title_fullStr |
Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine |
title_full_unstemmed |
Effects of Swirling Strength of the Premixed Gas Flow on Pollutant Emission in a Heavy-Duty Gas Turbine |
title_sort |
effects of swirling strength of the premixed gas flow on pollutant emission in a heavy-duty gas turbine |
publisher |
EDP Sciences |
series |
E3S Web of Conferences |
issn |
2267-1242 |
publishDate |
2019-01-01 |
description |
The combustion process and pollutant emission of an annular combustion chamber for a heavy-duty gas turbine were investigated by numerical method. The realizable k-ε model and finite rate/eddy dissipation model were adopted for calculations of turbulence and combustion. The effects of different swirling numbers of the double-swirler inlet on the temperature distribution and the thermal NOx formation in the combustion chamber were analyzed. The results show that the change of the swirling number of the outer swirling flow has a greater influence on the generation of the thermal NOx when compared with that of the inner swirling flow. The maximum average temperature of the central cross section of the combustor does not exceed 1760K. The average mass fraction of the generated thermal NOx at the exit decreases with the increasing outer swirling number. When the outer swirling number is less than 0.8, the generation of the thermal NOx is severe at the side wall of the combustion chamber. |
url |
https://www.e3s-conferences.org/articles/e3sconf/pdf/2019/44/e3sconf_icaeer18_04038.pdf |
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