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Koopman, Johannes and Hassa, Christoph (2004) Numerical Design of an Axially Staged Low Emission Gas Turbine Combustor. In: Proceedings: Trends in Numerical and Physical Modelling of Turbulent Processes in Gasturbine Combustors, 2, pp. 119-124. 2nd (International) SBF568-WORKSHOP : Trends on Numerical and Physical Modelling of Turbulent Processes in Gas Turbine Combustors, Heidelberg, April 1, 2 - 2004.
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Official URL: Johannes.Koopman@dlr.de
Abstract
Fuel staging between pilot- and main burner can reduce the pollutant emissions significantely when the main zone is designed for low emissions. The use of a low emission combustion concept for the pilot zone has the potential of diminishing the production of pollutants. The emphasis in this contribution is placed upon the mixing process of the Rich-Quench-Lean pilot combustor, being the key to low NOx production. A numerical study of the mixing process of the non reacting strongly swirling pilot burner flow with secondary and cooling flow has been performed. An optimized geometry of the mixing zone was established.
| Item URL in elib: | https://elib.dlr.de/1294/ | ||||||||||||
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| Document Type: | Conference or Workshop Item (Paper) | ||||||||||||
| Additional Information: | LIDO-Berichtsjahr=2005, | ||||||||||||
| Title: | Numerical Design of an Axially Staged Low Emission Gas Turbine Combustor | ||||||||||||
| Authors: |
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| Date: | 2004 | ||||||||||||
| Journal or Publication Title: | Proceedings: Trends in Numerical and Physical Modelling of Turbulent Processes in Gasturbine Combustors | ||||||||||||
| Open Access: | No | ||||||||||||
| Gold Open Access: | No | ||||||||||||
| In SCOPUS: | No | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Volume: | 2 | ||||||||||||
| Page Range: | pp. 119-124 | ||||||||||||
| Editors: |
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| Series Name: | International Workshop: SFB568 | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | Gas Turbine, Low Emission, Combustion, Numerical, staged combustor | ||||||||||||
| Event Title: | 2nd (International) SBF568-WORKSHOP : Trends on Numerical and Physical Modelling of Turbulent Processes in Gas Turbine Combustors, Heidelberg, April 1, 2 - 2004 | ||||||||||||
| Organizer: | Ercoftac und DGLR | ||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||
| HGF - Program Themes: | Propulsion Systems (old) | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L ER - Engine Research | ||||||||||||
| DLR - Research theme (Project): | L - Combustion Chamber Technologies (old) | ||||||||||||
| Location: | Köln-Porz | ||||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology | ||||||||||||
| Deposited By: | DLR-Beauftragter, elib | ||||||||||||
| Deposited On: | 16 Sep 2005 | ||||||||||||
| Last Modified: | 06 Jan 2010 13:34 |
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