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A fuel nozzle for a turbine engine includes a primary fuel passageway for supplying fuel to a plurality of radially extending fuel injectors arranged around the exterior of the fuel nozzle. A secondary fuel passageway couples an upstream end of the primary fuel passageway to a downstream end of the

A fuel nozzle for a turbine engine includes a primary fuel passageway for supplying fuel to a plurality of radially extending fuel injectors arranged around the exterior of the fuel nozzle. A secondary fuel passageway couples an upstream end of the primary fuel passageway to a downstream end of the primary fuel passageway. The secondary fuel passageway acts as a resonator tube to help reduce oscillations in the fuel flowing through the primary fuel passageway.

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1. A fuel nozzle for a turbine engine, comprising: an exterior wall;a plurality of radially extending fuel injectors formed on the exterior wall and extending outward away from the exterior wall, where at least one fuel delivery port is formed on each fuel injector;a generally annular shaped primary

1. A fuel nozzle for a turbine engine, comprising: an exterior wall;a plurality of radially extending fuel injectors formed on the exterior wall and extending outward away from the exterior wall, where at least one fuel delivery port is formed on each fuel injector;a generally annular shaped primary fuel passageway formed inside the exterior wall and configured to deliver fuel to the fuel injectors; anda secondary fuel passageway located closer to a central longitudinal axis of the fuel nozzle than the primary fuel passageway, wherein the secondary fuel passageway receives fuel from a first portion of the primary fuel passageway and delivers fuel back into a second portion of the primary fuel passageway at a location that is downstream from the first portion and upstream of the radially extending fuel injectors. 2. The fuel nozzle of claim 1, wherein the secondary fuel passageway is also generally annular shaped. 3. The fuel nozzle of claim 2, wherein the primary fuel passageway and the secondary fuel passageway are concentric. 4. The fuel nozzle of claim 3, wherein a plurality of radially extending connection passageways connect the primary fuel passageway and the secondary fuel passageway. 5. The fuel nozzle of claim 4, wherein a set of inlet connection passageways connect the first portion of the primary fuel passageway to an upstream end of the secondary fuel passageway, and wherein a set of outlet connection passageways connect the second portion of the primary fuel passageway to a downstream end of the secondary fuel passageway. 6. The fuel nozzle of claim 4, wherein a set of inlet connection passageways connect the first portion of the primary fuel passageway to an upstream end of the secondary fuel passageway, and wherein a set of outlet connection passageways connect the second portion of the primary fuel passageway to an interim position along a length of the secondary fuel passageway. 7. The fuel nozzle of claim 6, wherein a downstream end of the secondary fuel passageway is closed off. 8. The fuel nozzle of claim 4, wherein a set of inlet connection passageways connect the first portion of the primary fuel passageway to an interim position along a length of the secondary fuel passageway, and wherein a set of outlet connection passageways connect the second portion of the primary fuel passageway to a downstream end of the secondary fuel passageway. 9. The fuel nozzle of claim 8, wherein an upstream end of the secondary fuel passageway is closed off. 10. A fuel nozzle for a turbine engine, comprising: an exterior wall;a plurality of radially extending fuel injectors formed on the exterior wall and extending outward away from the exterior wall, where at least one fuel delivery port is formed on each fuel injector;a plurality of primary fuel passageways that extend down a length of the nozzle, wherein the primary fuel passageways are positioned along an inner side of the exterior wall, and wherein the primary fuel passageways deliver fuel to the fuel injectors; anda plurality of secondary fuel passageways, wherein each secondary fuel passageway is located closer to a central longitudinal axis of the fuel nozzle than the primary fuel passageways, and wherein each secondary fuel passageway receives fuel from a first portion of a corresponding primary fuel passageway and delivers fuel back into a second portion of its corresponding primary fuel passageway at a location that is downstream from the first portion and upstream of the radially extending fuel injectors. 11. The fuel nozzle of claim 10, wherein a single primary fuel passageway delivers fuel to a plurality of fuel injectors. 12. The fuel nozzle of claim 10, wherein the exterior wall forms the outer wall of the primary fuel passageways. 13. The fuel nozzle of claim 12, wherein an inner wall of each primary fuel passageway also forms the outer wall of a corresponding secondary fuel passageway. 14. The fuel nozzle of claim 13, wherein openings in the inner wall of each primary fuel passageway connect the primary fuel passageway to its corresponding secondary fuel passageway. 15. The fuel nozzle of claim 13, wherein an upstream opening in the inner wall of each primary fuel passageway allows fuel from the first portion of the primary fuel passageway to flow into the corresponding secondary fuel passageway, and wherein a downstream opening in the inner wall of each primary fuel passageway allows fuel in the corresponding secondary fuel passageway to flow into the second portion of the primary fuel passageway. 16. A method of forming a fuel nozzle for a turbine engine, comprising: forming a plurality of radially extending fuel injectors that extend outward from an exterior wall, where at least one fuel delivery port is formed on each fuel injector;forming at least one primary fuel passageway along an inner side of the exterior wall, wherein the at least one primary fuel passageway delivers fuel to at least one of the fuel injectors; andforming at least one secondary fuel passageway on a portion of the fuel nozzle that is located closer to a central longitudinal axis of the fuel nozzle than a corresponding primary fuel passageway, wherein each at least one secondary fuel passageway receives fuel from a first portion of a corresponding primary fuel passageway and delivers fuel back into a second portion of the corresponding primary fuel passageway at a location that is downstream from the first portion and upstream of the radially extending fuel injectors. 17. The method of claim 16, further comprising forming a plurality of connecting passageways that couple each at least one primary fuel passageway to a corresponding secondary fuel passageway. 18. The method of claim 17, wherein the connecting passageways are formed such that an upstream connecting passageway couples an upstream portion of each primary fuel passageway to a first portion of a corresponding secondary fuel passageway, and such that a downstream connecting passageway couples a downstream portion of each primary fuel passageway to a second portion of the corresponding secondary fuel passageway. 19. The method of claim 16, wherein the forming steps result in an inner wall of each primary fuel passageway forming an outer wall of a corresponding secondary fuel passageway. 20. The method of claim 19, further comprising forming apertures in the inner wall of each primary fuel passageway to couple the primary fuel passageway to upstream and downstream ends of the corresponding secondary fuel passageways.