Systems and methods for combustor emissions control

The present application thus provides a gas turbine engine system (100). The gas turbine engine system (100) may include a gas turbine engine (110), a nitrogen oxides reduction system (200) in communication with a flow of combustion gases (160) downstream from the gas turbine engine (110), and a nit...

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Bibliographische Detailangaben
1. Verfasser:	HOSKIN, ROBERT FRANK
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS FLUES GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTIONRESIDUES WEAPONS
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Beschreibung
Zusammenfassung:	The present application thus provides a gas turbine engine system (100). The gas turbine engine system (100) may include a gas turbine engine (110), a nitrogen oxides reduction system (200) in communication with a flow of combustion gases (160) downstream from the gas turbine engine (110), and a nitrogen oxides controller (300) to control the ratio of nitrogen dioxide to nitrogen oxides in the flow of combustion gases (160) entering the nitrogen oxides reduction system (200).