A gas turbine engine fuel injector stem includes a single piece of material with a flange, a center body, a gas gallery, and a fluid passage. The flange includes a cylindrical shape, a plurality of mounting holes and a handle hole. The center body extends from a flange cap in the flange axial direct
A gas turbine engine fuel injector stem includes a single piece of material with a flange, a center body, a gas gallery, and a fluid passage. The flange includes a cylindrical shape, a plurality of mounting holes and a handle hole. The center body extends from a flange cap in the flange axial direction. The gas gallery is adjacent the center body and distal to the flange. The gas gallery includes a ring shape oriented transverse to the flange and includes a gallery opening. The fluid passage extends through the flange, center body, and gas gallery and is in flow communication with the gallery opening.
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1. A forged and machined fuel injector stem for a gas turbine engine, the fuel injector stem comprising: a flange defining a plurality of mounting holes and a handle hole, the flange having a cylindrical shape with a base, a flange axis extending perpendicular to the base and defining an axial direc
1. A forged and machined fuel injector stem for a gas turbine engine, the fuel injector stem comprising: a flange defining a plurality of mounting holes and a handle hole, the flange having a cylindrical shape with a base, a flange axis extending perpendicular to the base and defining an axial direction;a center body extending from the base of the flange in the axial direction of the flange, the center body having a solid shape with a rounded rectangle cross-section;a gas gallery connected to the center body distal to the flange, the gas gallery having a hollow cylinder shape with a gas gallery axis oriented crosswise to the flange axis, a hollow portion of the gas gallery hollow cylinder shape defining a gallery opening;a pilot body extending from the center body in a radial direction of the flange, the radial direction of the flange being transverse to the axial direction of the flange, wherein the center body and the pilot body form a t-shaped cross section;a pilot funnel connected to the pilot body, the pilot funnel defining a hollow cylinder shape with a pilot axis, the pilot funnel being offset from the gas gallery along the radial direction of the flange, the pilot axis being aligned with the gas gallery axis, a hollow portion of the pilot funnel hollow cylinder shape defining a pilot opening;a gas main passage extending through the flange, the center body, and the hollow portion of the gas gallery, the gas main passage being in flow communication with the gallery opening;a liquid main passage extending through the flange, the center body, and the hollow portion of the gas gallery, the liquid main passage being in flow communication with the gallery opening and being adjacent to the gas main passage;a gas pilot passage extending through the flange, the pilot body, and the hollow portion of the pilot funnel, the gas pilot passage being in flow communication with the pilot opening; anda liquid pilot passage extending through the flange, the pilot body, and the hollow portion of the pilot funnel, the liquid pilot passage being in flow communication with the pilot opening and being adjacent to the gas pilot passage,wherein the flange, the center body, the gas gallery, the pilot body, and the pilot funnel are forged and machined from a single workpiece. 2. The fuel injector stem of claim 1, further comprising: a pilot boss extending from the flange in a direction opposite the center body, wherein the gas pilot passage and the liquid pilot passage extend into the pilot boss. 3. The fuel injector stem of claim 1, further comprising: an air assist passage extending through the flange, the pilot body, and the hollow portion of the pilot funnel, the air assist passage being in flow communication with the pilot opening and being adjacent to the liquid pilot passage. 4. The fuel injector stem of claim 1, wherein the pilot body includes an elliptical cross-section that rounds into the center body. 5. The fuel injector stem of claim 4, wherein the gas gallery is a hollow circular cylinder and includes a cylindrical surface extending from a front lip to a back lip of the hollow circular cylinder along a direction parallel to the gas gallery axis. 6. The fuel injector stem of claim 1, wherein a thickness of the gas gallery matches and aligns with a thickness of the center body along a direction parallel to the gas gallery axis, and a thickness of the pilot funnel matches and aligns with a thickness of the pilot body along a direction parallel to the pilot axis. 7. A fuel injector comprising the fuel injector stem of claim 1, the fuel injector further comprising: a swirler assembly coupled to the gas gallery and being in flow communication with at least one of the gas main passage, the liquid main passage, the gas pilot passage, and the liquid pilot passage;a barrel coupled to the swirler assembly, the barrel including a barrel end;a fitting coupled to the flange, the fitting being in flow communication with a fluid source and at least one of the gas main passage, the liquid main passage, the gas pilot passage, and the liquid pilot passage; anda handle coupled to the flange at the handle hole. 8. The fuel injector of claim 7, wherein the gas gallery fits around the swirler assembly. 9. The fuel injector stem of claim 1, wherein a thickness of the gas gallery matches and aligns with a thickness of the center body along a direction parallel to the gas gallery axis. 10. The fuel injector stem of claim 1, wherein a thickness of the pilot funnel matches and aligns with a thickness of the pilot body along a direction parallel to the pilot axis. 11. A fuel injector stem for a gas turbine engine, the fuel injector stem comprising: a single piece of material having a flange defining a plurality of mounting holes and a handle hole, the flange including a cylindrical shape with a flange axis extending between a top cap and a bottom cap,a center body extending from the bottom cap of the flange in an axial direction of the flange, the axial direction of the flange extending parallel to the flange axis,a gas gallery adjacent to the center body and distal from the flange, the gas gallery including a ring shape oriented transverse to the flange, the gas gallery defining a gallery opening, anda fluid passage extending through the flange, the center body, and the gas gallery, the fluid passage being in flow communication with the gallery opening,a thickness of the gas gallery matching and aligning with a thickness of the center body along a direction parallel to a longitudinal axis of the gas gallery. 12. The fuel injector stem of claim 11, wherein the fluid passage is a gas main passage, the single piece of material further having a liquid main passage extending through the flange, the center body, and the gas gallery, the liquid main passage being in flow communication with the gallery opening and being adjacent to the gas main passage. 13. The fuel injector stem of claim 11, wherein the center body includes a cuboid shape. 14. The fuel injector stem of claim 13, wherein edges of the cuboid shape of the center body and edges of the ring shape of the gas gallery are rounded. 15. The fuel injector stem of claim 11, wherein the gas gallery is a hollow cylinder and includes a cylindrical surface extending from a front lip to a back lip of the hollow cylinder along a direction parallel to a longitudinal axis of the gas gallery. 16. A fuel injector comprising the fuel injector stem of claim 11, the fuel injector further comprising: a swirler assembly coupled to the gas gallery and being in flow communication with the fluid passage;a barrel coupled to the swirler assembly, the barrel including a barrel end;a fitting coupled to the flange, the fitting being in flow communication with the fluid passage and with a fluid source; anda handle coupled to the flange at the handle hole. 17. The fuel injector of claim 16, wherein the gas gallery fits around the swirler assembly.
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이 특허에 인용된 특허 (8)
Luciano Mei IT; Alessio Miliani IT, Device for connection of a nozzle of a pre-mixing chamber of a gas turbine, to a housing of the pre-mixing chamber.
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