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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Main Authors: Gao Huanhuan, Fu Zaiguo, Zeng Zhuoxiong, Liu Jiang, Weng Peifen
Format: Article
Language:English
Published: EDP Sciences 2019-01-01
Series:E3S Web of Conferences
Online Access:https://www.e3s-conferences.org/articles/e3sconf/pdf/2019/44/e3sconf_icaeer18_04038.pdf
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spelling 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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