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Title: Method of reducing NOx emissions in a gas turbine engine

Patent ·
OSTI ID:6344471

A method is described for reducing NO[sub x] emissions and for eliminating stress cracking in combustion components caused by combustion in a gas turbine comprising the steps of: (a) providing a fuel nozzle body having a nozzle arranged to provide a fuel passageway, a combustion passageway and a water passageway, the water passageway located substantially centrally along a longitudinal axis of the nozzle, the combustion air passageway lying radially outwardly of the water passageway, and the fuel passageway lying adjacent and radially outwardly of the combustion air passageway; (b) injecting fuel through said fuel passageway and into a combustion chamber of a gas turbine as a first conical spray; (c) injecting water through said water passageway in said nozzle assembly coincident with said longitudinal axis into said combustion chamber as a second, finely atomized conical spray located radially inwardly of said first conical spray so as to avoid direct water impingement on hot metal surfaces within said combustion chamber; and (d) injecting combustion air through said air passageway in said nozzle assembly into said combustion chambers as a third conical spray located radially between said first and said second conical sprays, wherein the fuel, water and combustion air are mixed upon discharge from said fuel nozzle body in said combustion chamber.

Assignee:
General Electric Co., Schenectady, NY (United States)
Patent Number(s):
US 5228283; A
Application Number:
PPN: US 7-517349
OSTI ID:
6344471
Resource Relation:
Patent File Date: 1 May 1990
Country of Publication:
United States
Language:
English