# US 10,480,791 B2 · Fuel injector to facilitate reduced NOx emissions in a combustor system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,480,791 B2 - Document ID: US10480791B2 - Status: Granted - Kind: B2 - Application number: 14/447,967 - Filed: 2014-07-31 - Published: 2016-02-04 - Granted: 2019-11-19 - Earliest claimed: 2014-07-31 - Assignees: General Electric Company - Applicants: General Electric Company - Inventors: Krishna Kumar Venkatesan; Joel Meier Haynes; Narendra Digamber Joshi; David James Walker; Junwoo Lim; Sarah Marie Monahan - Web page: https://patentgrep.com/patent/US10480791B2 ## CPC - F23R 3/286: {having fuel-air premixing devices (F23R3/30 takes precedence)} - F23R 3/10: for primary air (F23R3/06, F23R3/045 take precedence) - F23R 3/34: Feeding into different combustion zones - F23R 3/42: characterised by the arrangement or form of the flame tubes or combustion chambers - 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) ## Abstract A fuel injector to reduce NOx emissions in a combustor system. The fuel injector including a housing, at least one oxidizer flow path, extending axially through the fuel injector housing and defining therein one or more oxidizer flow paths for an oxidizer stream and a fuel manifold, extending axially through the fuel injector housing and defining therein one or more fuel flow path. The fuel manifold includes a forward portion and an aft portion including an aft face. A plurality of fuel injector outlets are defined in the aft portion, wherein the plurality of fuel injector outlets are configured to inject a fuel flow along a mid-plane of the fuel injector and away from a downstream wall. The fuel flow exiting the fuel manifold undergoes circumferential and radial mixing upon interaction with the oxidizer stream. Additionally disclosed is a combustor system including the fuel injector. ## Claims ### Claim 1 An annular fuel injection nozzle comprising: a fuel injector housing comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween, the fuel injector housing defined about a center longitudinal axis of the annular fuel injection nozzle; an inner oxidizer flow path, about the center longitudinal axis, having an inner swirler therein; an intermediate oxidizer flow path radially outward of the inner oxidizer flow path, concentric with the center longitudinal axis, having an intermediate swirler therein; an annular fuel manifold radially outward of the intermediate oxidizer flow path, concentric with the center longitudinal axis; and an outer oxidizer flow path radially outward of the annular fuel manifold, concentric with the center longitudinal axis, having an outer swirler therein, wherein an oxidizer stream enters the fuel injector housing through the upstream face of the fuel injector housing, wherein a first portion of the oxidizer stream is diverted to the inner oxidizer flow path and through a centerbody of the fuel injection nozzle via the inner swirler as an inner oxidizer flow stream, wherein a second portion of the oxidizer stream is diverted to the intermediate oxidizer flow path via the intermediate swirler as an intermediate oxidizer flow stream, and wherein a third portion of the oxidizer stream is diverted to the outer oxidizer flow path via the outer swirler as an outer oxidizer flow stream, the annular fuel manifold comprising: a forward portion and an aft portion including an aft face; and a plurality of fuel injector outlets defined in the aft portion, downstream of the inner swirler and the outer swirler, wherein the plurality of fuel injector outlets are configured to inject a fuel flow in a downstream direction along a mid-plane of the annular fuel manifold, wherein the mid-plane is defined as a radial median between an innermost and outermost radius of the annular fuel manifold, and wherein the fuel flow exiting the annular fuel manifold undergoes initial interaction with the intermediate oxidizer stream and the outer oxidizer stream, downstream of the intermediate swirler and the outer swirler, thereby providing a mixed stream, and wherein the mixed stream remains separated from the inner oxidizer stream until the mixed stream undergoes circumferential and radial mixing with the inner oxidizer stream, downstream of the inner swirler and the plurality of fuel injector outlets. ### Claim 2 (depends on 1) The annular fuel injection nozzle-of claim 1, wherein the plurality of fuel injector outlets are configured as a plurality of fuel exit orifices. ### Claim 3 (depends on 1) The annular fuel injection nozzle of claim 1, wherein the plurality of fuel injector outlets are configured as a plurality of fuel exit slots. ### Claim 4 (depends on 1) The annular fuel injection nozzle of claim 1, wherein the plurality of fuel injector outlets are configured circumferentially spaced about the aft portion. ### Claim 5 (depends on 4) The annular fuel injection nozzle of claim 4, wherein the plurality of fuel injector outlets are configured circumferentially spaced about the aft face. ### Claim 6 (depends on 1) The annular fuel injection nozzle of claim 1, wherein the plurality of fuel injector outlets are configured circumferentially spaced about a sidewall defining the aft portion of the annular fuel manifold and circumferentially spaced about the aft face. ### Claim 7 (depends on 1) The annular fuel injection nozzle of claim 1, wherein one or more of the plurality fuel injector outlets include a fuel injector tip to facilitate accelerating the fuel flow through the one or more of the plurality of fuel injector outlets. ### Claim 8 (depends on 1) The annular fuel injection nozzle of claim 1, wherein the inner swirler and outer swirler is a combination of radial swirlers and axial swirlers. ### Claim 9 An annular fuel injection nozzle comprising: a fuel injector housing comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween, the fuel injector housing defined about a center longitudinal axis of the annular fuel injection nozzle; an inner oxidizer flow path, about the center longitudinal axis, having an inner swirler therein; an intermediate oxidizer flow path radially outward of the inner oxidizer flow path, concentric with the center longitudinal axis, having an intermediate swirler therein; an annular fuel manifold radially outward of the intermediate oxidizer flow path, concentric with the center longitudinal axis; and an outer oxidizer flow path radially outward of the annular fuel manifold, concentric with the center longitudinal axis, having an outer swirler therein, wherein an oxidizer stream enters the fuel injector housing through the upstream face of the fuel injector housing, wherein a first portion of the oxidizer stream is diverted to the inner oxidizer flow path and through a centerbody of the fuel injection nozzle via the inner swirler as an inner oxidizer flow stream, wherein a second portion of the oxidizer stream is diverted to the intermediate oxidizer flow path via the intermediate swirler as an intermediate oxidizer flow stream, and wherein a third portion of the oxidizer stream is diverted to the outer oxidizer flow path via the outer swirler as an outer oxidizer flow stream, the annular fuel manifold comprising: a forward portion and an aft portion including an aft face; and a plurality of fuel injector outlets configured downstream of the inner swirler and the outer swirler and circumferentially spaced about at least one of a sidewall defining the aft portion of the annular fuel manifold or downstream of the inner swirler, the intermediate swirler and the outer swirler and circumferentially spaced about an aft face of the aft portion of the annular fuel manifold, wherein the plurality of fuel injector outlets are configured to inject a fuel flow in a downstream direction along a mid-plane of the annular fuel manifold, wherein the mid-plane is defined as a radial median between an innermost and outermost radius of the annular fuel manifold, wherein the fuel flow exiting the annular fuel manifold undergoes initial interaction with the intermediate oxidizer stream and the outer oxidizer stream, downstream of the intermediate swirler and the outer swirler, thereby providing a mixed stream, wherein the mixed stream remains separated from the inner oxidizer stream until the mixed stream undergoes circumferential and radial mixing with the inner oxidizer stream passing through the inner swirler, downstream of the inner swirler and the plurality of fuel injector outlets, and wherein one or more of the plurality of fuel injector outlets comprises a plurality of fuel exit orifices, wherein at least one orifice of the plurality of fuel exit orifices is fitted with a fuel injector tip. ### Claim 10 (depends on 9) The annular fuel injection nozzle of claim 9, wherein the fuel injector tip comprises an additional fuel manifold that operates over a limited power range and is selectively operable such that the additional fuel manifold is switched off during operation beyond the limited power range. ### Claim 11 (depends on 9) The annular fuel injection nozzle of claim 9, wherein the fuel injector tip is configured to facilitate pressure swirl atomization for lower power applications without taking a fuel delivery pressure penalty. ### Claim 12 A combustor assembly comprising: a combustion liner comprising a center longitudinal axis, a forward end and an aft end; and an annular fuel injection nozzle, coupled adjacent to the forward end of the combustion liner, the annular fuel injection nozzle comprising: a fuel injector housing comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween, the fuel injector housing defined about the center longitudinal axis; an inner oxidizer flow path, about the center longitudinal axis, having an inner swirler therein; an intermediate oxidizer flow path radially outward of the inner oxidizer flow path, concentric with the center longitudinal axis, having an intermediate swirler therein; an annular fuel manifold radially outward of the intermediate oxidizer flow path, concentric with the center longitudinal axis; and an outer oxidizer flow path radially outward of the annular fuel manifold, concentric with the center longitudinal axis, having an outer swirler therein, wherein an oxidizer stream enters the fuel injector housing through the upstream face of the fuel injector housing, wherein a first portion of the oxidizer stream is diverted to the inner oxidizer flow path and through a centerbody of the fuel injection nozzle via the inner swirler as an inner oxidizer flow stream, wherein a second portion of the oxidizer stream is diverted to the intermediate oxidizer flow path via the intermediate swirler as an intermediate oxidizer flow stream, and wherein a third portion of the oxidizer stream is diverted to the outer oxidizer flow path via the outer swirler as an outer oxidizer flow stream, the annular fuel manifold comprising: a forward portion and an aft portion including an aft face; and a plurality of fuel injector outlets defined in the aft portion, downstream of the inner swirler and the outer swirler, wherein the plurality of fuel injector outlets are configured to inject a fuel flow in a downstream direction along a mid-plane of the annular fuel manifold, wherein the mid-plane is defined as a radial median between an innermost and outermost radius of the annular fuel manifold, wherein the fuel flow exiting the annular fuel manifold undergoes initial interaction with the intermediate oxidizer stream and the outer oxidizer stream, downstream of the intermediate swirler and the outer swirler, thereby providing a mixed stream, and wherein the mixed stream remains separated from the inner oxidizer stream until the mixed stream undergoes circumferential and radial mixing with the inner oxidizer stream passing through the inner swirler, downstream of the inner swirler and the plurality of fuel injector outlets. ### Claim 13 (depends on 12) The combustor assembly of claim 12, wherein the plurality of fuel injector outlets are configured as at least one of a plurality of fuel exit orifices and a plurality of fuel exit slots. ### Claim 14 (depends on 12) The combustor assembly of claim 12, wherein the plurality of fuel injector outlets are configured circumferentially spaced about at least one of a sidewall defining the aft portion of the annular fuel manifold and the aft face. ### Claim 15 (depends on 12) The combustor assembly of claim 12, wherein one or more of the plurality of fuel injector outlets include a fuel injector tip to facilitate accelerating the fuel flow through the one or more of the plurality of fuel injector outlets. ### Claim 16 A combustor assembly comprising: a combustion liner comprising a center longitudinal axis, a forward end and an aft end: and an annular fuel injection nozzle, coupled adjacent to the forward end of the combustion liner, the annular fuel injection nozzle comprising: a fuel injector housing comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween, the fuel injector housing defined about the center longitudinal axis; an inner oxidizer flow path, about the center longitudinal axis, having an inner swirler therein; an intermediate oxidizer flow path radially outward of the inner oxidizer flow path, concentric with the center longitudinal axis, having an intermediate swirler therein; an annular fuel manifold radially outward of the second oxidizer flow path, concentric with the center longitudinal axis; and an outer oxidizer flow path radially outward of the annular fuel manifold, concentric with the center longitudinal axis, having an outer swirler therein, wherein an oxidizer stream enters the fuel injector housing through the upstream face of the fuel injector housing, wherein a first portion of the oxidizer stream is diverted to the inner oxidizer flow path and through a centerbody of the fuel injection nozzle via the inner swirler as an inner oxidizer flow stream, wherein a second portion of the oxidizer stream is diverted to the Intermediate oxidizer flow path via the intermediate swirler as an intermediate oxidizer flow stream, and wherein a third portion of the oxidizer stream is diverted to the outer oxidizer flow path via the outer swirler as an outer oxidizer flow stream, and the annular fuel manifold comprising: a forward portion and an aft portion including an aft face; and a plurality of fuel injector outlets defined in the aft portion, downstream of the inner swirler and the outer swirler, wherein the plurality of fuel injector outlets are configured to inject a fuel flow in a downstream direction along a mid-plane of the annular fuel manifold, wherein the mid-plane is defined as a radial median between an innermost and outermost radius of the annular fuel manifold, wherein the fuel flow exiting the annular fuel manifold undergoes initial interaction with the intermediate oxidizer stream and the outer oxidizer stream, downstream of the intermediate swirler and the outer swirler, thereby providing a mixed stream, wherein the mixed stream remains separated from the inner oxidizer stream until the mixed stream undergoes circumferential and radial mixing upon interaction with the inner oxidizer stream downstream of the inner swirler and the plurality of fuel injector outlets, and wherein the plurality of fuel injector outlets comprises a plurality of fuel exit orifices, wherein at least one orifice of the plurality of fuel exit orifices is fitted with an injector tip, wherein the injector tip comprises an additional fuel manifold that operates over a limited power range and is selectively operable such that the additional fuel manifold is switched off during operation beyond the limited power range.