# US 10,309,653 B2 · Bundled tube fuel nozzle with internal cooling > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,309,653 B2 - Document ID: US10309653B2 - Status: Granted - Kind: B2 - Application number: 15/060,688 - Filed: 2016-03-04 - Published: 2017-09-07 - Granted: 2019-06-04 - Earliest claimed: 2016-03-04 - Assignees: General Electric Company - Applicants: General Electric Company - Inventors: Patrick Benedict Melton; David William Cihlar; Timothy James Purcell - Web page: https://patentgrep.com/patent/US10309653B2 ## CPC - F23R 3/283: {Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances} - F23D 14/02: Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone - F23D 14/64: with injectors - F23R 3/005: {Combined with pressure or heat exchangers} - F23R 3/08: between annular flame tube sections, e.g. flame tubes with telescopic sections - F23R 3/286: {having fuel-air premixing devices (F23R3/30 takes precedence)} - F23R: GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (fluidised bed combustion apparatus specially adapted for operation at superatmospheric pressures F23C10/16) - F23D: BURNERS ## Abstract A bundled tube fuel nozzle includes a forward plate, a first intermediate plate and an outer sleeve defining a fuel plenum, a second intermediate plate axially spaced from the first intermediate plate where the first intermediate plate, the second intermediate plate and the outer sleeve define a purge air plenum, an aft plate axially spaced from the second intermediate plate where the second intermediate plate, the aft plate and the outer sleeve define a cooling air plenum and an annular wall that extends from the second intermediate plate to the aft plate. The annular wall defines a cooling flow channel within the bundled tube fuel nozzle. A plurality of apertures is defined proximate to a cool side of the aft plate and provide for fluid communication between the cooling flow channel and the cooling air plenum. ## Claims ### Claim 1 A bundled tube fuel nozzle comprising: a forward plate, a first intermediate plate, and an outer sleeve defining a fuel plenum therebetween; a second intermediate plate axially spaced from the first intermediate plate, wherein the first intermediate plate, the second intermediate plate, and the outer sleeve define a purge air plenum therebetween; an aft plate axially spaced from the second intermediate plate, wherein the second intermediate plate, the aft plate, and the outer sleeve define a cooling air plenum therebetween; a plurality of tubes that extends through the forward plate, the fuel plenum, the first intermediate plate, the purge air plenum, the second intermediate plate, the cooling air plenum, and the aft plate, each tube of the plurality of tubes having a longitudinal tube axis; an annular wall that extends from the second intermediate plate to the aft plate, the annular wall being surrounded by the plurality of tubes and defining a cooling flow channel, the cooling flow channel having a longitudinal channel axis that is non-coaxial with the longitudinal tube axis of each tube of the plurality of tubes; and a plurality of apertures defined proximate to a cool side of the aft plate, wherein the plurality of apertures provides for fluid communication between the cooling flow channel and the cooling air plenum. ### Claim 2 (depends on 1) The bundled tube fuel nozzle as in claim 1, wherein the apertures of the plurality of apertures are circumferentially spaced along the annular wall. ### Claim 3 (depends on 1) The bundled tube fuel nozzle as in claim 1, wherein one or more of the apertures of the plurality of apertures includes an outlet oriented towards the cool side of the aft plate. ### Claim 4 (depends on 1) The bundled tube fuel nozzle as in claim 1, wherein the outer sleeve defines an inlet port, wherein the inlet port provides for fluid communication into the purge air plenum. ### Claim 5 (depends on 1) The bundled tube fuel nozzle as in claim 1, wherein the outer sleeve defines one or more exhaust ports, wherein the one or more exhaust ports provide for fluid communication out of the cooling air plenum. ### Claim 6 (depends on 5) The bundled tube fuel nozzle as in claim 5, wherein at least one of the one or more exhaust ports is defined along an inner band portion of the outer sleeve. ### Claim 7 (depends on 5) The bundled tube fuel nozzle as in claim 5, wherein at least one of the one or more exhaust ports is defined along an outer band portion of the outer sleeve. ### Claim 8 A combustor comprising: an end cover coupled to an outer casing; a bundled tube fuel nozzle disposed within the outer casing and coupled to the end cover via one or more fluid conduits, wherein the bundled tube fuel nozzle comprises: a forward plate, a first intermediate plate, and an outer sleeve defining a fuel plenum therebetween, wherein the fuel plenum is in fluid communication with at least one fluid conduit of the one or more fluid conduits; a second intermediate plate axially spaced from the first intermediate plate, wherein the first intermediate plate, the second intermediate plate, and the outer sleeve define a purge air plenum therebetween; an aft plate axially spaced from the second intermediate plate, wherein the second intermediate plate, the aft plate, and the outer sleeve define a cooling air plenum therebetween, and wherein the outer sleeve defines one or more exhaust ports, the one or more exhaust ports providing fluid communication out of the cooling air plenum; a plurality of tubes that extends through the forward plate, the fuel plenum, the first intermediate plate, the purge air plenum, the second intermediate plate, the cooling air plenum, and the aft plate; an annular wall that extends from the second intermediate plate to the aft plate, the annular wall defining a cooling flow channel; and a plurality of apertures defined proximate to a cool side of the aft plate, wherein the plurality of apertures provides for fluid communication between the cooling flow channel and the cooling air plenum. ### Claim 9 (depends on 8) The combustor as in claim 8, wherein the apertures of the plurality of apertures are circumferentially spaced along the annular wall. ### Claim 10 (depends on 8) The combustor as in claim 8, wherein one or more of the apertures of the plurality of apertures includes an outlet oriented towards the cool side of the aft plate. ### Claim 11 (depends on 8) The combustor as in claim 8, wherein the outer sleeve defines an inlet port, wherein the inlet port provides for fluid communication into the purge air plenum. ### Claim 12 (depends on 8) The combustor as in claim 8, further comprising a center fuel nozzle coupled to the end cover, wherein the bundled tube fuel nozzle extends circumferentially around at least a portion of the center fuel nozzle. ### Claim 13 (depends on 8) The combustor as in claim 8, wherein at least one of the one or more exhaust ports is defined along an inner band portion of the outer sleeve. ### Claim 14 (depends on 8) The combustor as in claim 8, wherein at least one of the one or more exhaust ports is defined along an outer band portion of the outer sleeve. ### Claim 15 A combustor comprising: an end cover coupled to an outer casing; a plurality of bundled tube fuel nozzle assemblies disposed within the outer casing and annularly arranged about a center fuel nozzle of the combustor, wherein each bundled tube fuel nozzle assembly is coupled to the end cover, via at least one fluid conduit, and comprises: a forward plate, a first intermediate plate, and an outer sleeve defining a fuel plenum therebetween, wherein the fuel plenum is in fluid communication with the at least one fluid conduit; a second intermediate plate axially spaced from the first intermediate plate, wherein the first intermediate plate, the second intermediate plate, and the outer sleeve define a purge air plenum therebetween and wherein the second intermediate plate defines an opening therethrough; an aft plate axially spaced from the second intermediate plate, wherein the second intermediate plate, the aft plate, and the outer sleeve define a cooling air plenum therebetween; a plurality of tubes that extends through the forward plate, the fuel plenum, the first intermediate plate, the purge air plenum, the second intermediate plate, the cooling air plenum, and the aft plate, the plurality of tubes being disposed around the opening; an annular wall that extends from the opening in the second intermediate plate to the aft plate, the annular wall defining a cooling flow channel separate and independent from the plurality of tubes; and a plurality of apertures defined proximate to a cool side of the aft plate, wherein the plurality of apertures provides for fluid communication between the cooling flow channel and the cooling air plenum. ### Claim 16 (depends on 15) The combustor as in claim 15, wherein the apertures of the plurality of apertures are circumferentially spaced along the annular wall. ### Claim 17 (depends on 15) The combustor as in claim 15, wherein one or more of the apertures of the plurality of apertures includes an outlet oriented towards the cool side of the aft plate. ### Claim 18 (depends on 15) The combustor as in claim 15, wherein the outer sleeve defines an inlet port, wherein the inlet port provides for fluid communication into the purge air plenum. ### Claim 19 (depends on 15) The combustor as in claim 15, wherein the outer sleeve defines one or more exhaust ports that provide for fluid communication out of the cooling air plenum.