Andrews, GE (2015) Ultra Low NOx Gas Turbine Combustion. In: Proceedings of 12th ISAIF. 12th ISAIF International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, 20-23 Jul 2015, Lerica (La Spezia), Italy. ISAIF
Abstract
Contents Introduction Thermal NOx Burning to the lean flammability limit for successful ultra low NOx No combustor film cooling for ultra low NOx Impingement backside cooling Non-thermal NOx dominates in Ultra Low NOx GT Combustion Non-swirling systems – baffle type combustor Axial swirlers Radial swirlers Axial staged or lean/lean low NOx combustors (including reheat burners) Fuel staging within a flame stabiliser for good power turndown Aero Combustors for ultra low Nox Conclusions
Metadata
Item Type: | Proceedings Paper |
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Authors/Creators: |
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Keywords: | NOx; Gas Turbines; Combustor design for low NOx; Thermal NOx |
Dates: |
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Institution: | The University of Leeds |
Academic Units: | The University of Leeds > Faculty of Engineering & Physical Sciences (Leeds) > School of Chemical & Process Engineering (Leeds) |
Depositing User: | Symplectic Publications |
Date Deposited: | 12 Oct 2017 10:22 |
Last Modified: | 12 Oct 2017 15:18 |
Status: | Published |
Publisher: | ISAIF |
Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:109792 |