Low emissions combustion nozzle for use with a gas turbine...

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

F23R 3/34 (2006.01) F02M 61/18 (2006.01) F23C 7/00 (2006.01) F23D 17/00 (2006.01) F23R 3/36 (2006.01)

Patent

CA 2113082

2113082 9400718 PCTABS00030 An injector nozzle (66, 190) having a central axis (68), said injector nozzle (66, 190) comprising means (179) for passing a pilot fuel through the injector nozzle (66, 190) during operation thereof; means (186) for introducing a supply of pilot air through the injector nozzle (66, 190), said supply of pilot air being mixed with the pilot fuel only after exiting the injector nozzle (66, 190) during operation thereof; means (133) for introducing a primary supply of air through the injector nozzle (66, 190) during operation thereof, said means (133) for introducing the primary supply of air including a main air passage (132) being defined by a portion of the inner surface (90) of the wall (88) and a portion of the shell (126); and means (160) for passing a main source of fuel through the injector nozzle (66, 190) during operation thereof, said means (160) for passing the main source of fuel including a plurality of spoke members (150) disposed within respective ones of the plurality of holes (148) and being partially positioned within the main air passage (132) and having a plurality of passages (156) therein exiting into the main air passage (132).

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