Apparatus and method for mixing fuel in a gas turbine nozzle
A nozzle includes a fuel plenum and an air plenum downstream of the fuel plenum. A primary fuel channel includes an inlet in fluid communication with the fuel plenum and a primary air port in fluid communication with the air plenum. Secondary fuel channels radially outward of the primary fuel channel include a secondary fuel port in fluid communication with the fuel plenum. A shroud circumferentially surrounds the secondary fuel channels. A method for mixing fuel and air in a nozzle prior to combustion includes flowing fuel to a fuel plenum and flowing air to an air plenum downstream of the fuel plenum. The method further includes injecting fuel from the fuel plenum through a primary fuel passage, injecting fuel from the fuel plenum through secondary fuel passages, and injecting air from the air plenum through the primary fuel passage.
1. A fuel nozzle, comprising:
a top divider plate extending radially across a diameter of an annular shroud;
a middle divider plate axially spaced from the top divider plate and circumscribed within the shroud, wherein the top divider plate, the middle divider plate and the outer shroud at least partially define a fuel plenum;
a bottom divider plate axially spaced from the middle divider plate, wherein the bottom divider plate, the middle divider plate and the shroud at least partially define an air plenum;
a plurality of primary fuel channels which extend axially through the air plenum from the middle divider plate at least partially through the bottom divider plate, each primary fuel channel having an inlet in fluid communication with the fuel plenum; and
a plurality of secondary fuel channels arranged in an annular array around the plurality of primary fuel channels, wherein the secondary fuel channels comprises a plurality of tubes which extend through the top divider plate, the fuel plenum and the bottom divider plate.
2. The fuel nozzle as in claim 1 , wherein the inlet of each primary fuel passage is axially spaced from the top divider plate.
3. The fuel nozzle as in claim 1 , wherein the primary fuel passages comprise a plurality of parallel tubes in fluid communication with the inlets, wherein each tube defines a passage through the air plenum and out of an exit of the fuel nozzle.
4. The fuel nozzle as in claim 1 , wherein each primary fuel channel includes a primary air port, the primary air port being in fluid communication with the air plenum.
5. The fuel nozzle as in claim 1 , wherein the at least one primary fuel channel is axially aligned with a centerline of the fuel nozzle.
6. The fuel nozzle as in claim 1 , wherein each of the plurality of secondary fuel channels includes a secondary fuel port in fluid communication with the fuel plenum.
7. The fuel nozzle as in claim 1 , wherein the shroud defines an air port in fluid communication with the air plenum.
8. The fuel nozzle as in claim 1 , wherein the top divider plate extends radially and circumferentially across a diameter of the shroud, the middle divider plate extends radially and circumferentially across the diameter of the shroud and the bottom divider plate extends radially and circumferentially across the diameter of the shroud downstream from the middle divider plate.
9. The fuel nozzle as in claim 1 , further comprising a fluid conduit coaxially aligned with an opening defined by the top divider plate, wherein the fluid conduit is in fluid. communication with the fuel plenum.