초록 ▼

The present application thus describes a method of manufacture for a late lean injection system in a combustor of a combustion turbine engine. The method may include the steps of: a) identifying a desired position within the flow assembly for a late lean injector, wherein the late lean injector comp

The present application thus describes a method of manufacture for a late lean injection system in a combustor of a combustion turbine engine. The method may include the steps of: a) identifying a desired position within the flow assembly for a late lean injector, wherein the late lean injector comprises a late lean nozzle and a transfer tube; b) corresponding to the desired position for the late lean injector, identifying an injection point on the inner radial wall and a late lean nozzle position on the outer radial wall; c) positioning the inner radial wall and the outer radial wall in an unassembled position; d) while in the unassembled position, forming a hole through the inner radial wall at the injection point and slideably engaging the transfer tube within the hole; e) installing the late lean nozzle in the outer radial wall at the late lean nozzle position; f) positioning the inner radial wall and the outer radial wall in an assembled position; and g) connecting the transfer tube to the late lean nozzle.

대표청구항 ▼

1. A method of manufacture for a late lean injection system in a combustor of a combustion turbine engine, wherein the combustor includes a flow assembly that includes an inner radial wall, which defines a primary combustion chamber downstream of a primary fuel nozzle, and an outer radial wall, whic

1. A method of manufacture for a late lean injection system in a combustor of a combustion turbine engine, wherein the combustor includes a flow assembly that includes an inner radial wall, which defines a primary combustion chamber downstream of a primary fuel nozzle, and an outer radial wall, which surrounds the inner radial wall forming a flow annulus therebetween, the method including the steps of: a) identifying a desired position within the flow assembly for a late lean injector in the combustor, wherein the late lean injector comprises a late lean nozzle and a transfer tube;b) corresponding to the desired position for the late lean injector, identifying an injection point on the inner radial wall and a late lean nozzle position on the outer radial wall;c) positioning the inner radial wall and the outer radial wall in an unassembled position;d) while the inner radial wall and the outer radial wall are in the unassembled position, forming a hole through the inner radial wall at the injection point and slideably engaging the transfer tube within the hole;e) installing the late lean nozzle in the outer radial wall at the late lean nozzle position;f) positioning the inner radial wall and the outer radial wall in an assembled position; andg) connecting the transfer tube to the late lean nozzle. 2. The method according to claim 1, wherein the flow assembly comprises a liner/flow sleeve assembly, the inner radial wall comprises a liner, and the outer radial wall comprises a flow sleeve. 3. The method according to claim 1, wherein the flow assembly comprises a transition piece/impingement sleeve assembly, the inner radial wall comprises a transition piece, and the outer radial wall comprises an impingement sleeve. 4. The method according to claim 2, wherein forming the hole through the liner includes installing a boss within the hole, wherein the transfer tube slideably engages a hollow passageway defined by the boss. 5. The method according to claim 2, further comprising repeating certain of the steps a) through g) so that at least three late lean injectors are installed within the liner/flow sleeve assembly. 6. The method according to claim 2, wherein: step a) includes identifying desired positions within the liner/flow sleeve assembly for at least three late lean injectors, wherein each of the late lean injectors comprise the late lean nozzle and the transfer tube;step b) includes: corresponding to the desired locations for the late lean injectors, identifying the injection points on the liner and the late lean nozzle positions on the flow sleeve for each of the late lean injectors;step c) includes: positioning the liner and the flow sleeve in the unassembled position;step d) includes: while the liner and the flow sleeve are in the unassembled position, forming holes through the liner at the injection points and slideably engaging each of the transfer tubes within one of the holes;step e) includes: installing the late lean nozzles in the flow sleeve at the late lean nozzle positions;step f) includes: positioning the liner and flow sleeve in the assembled position; andstep g) includes connecting each of the transfer tubes to the corresponding late lean nozzle. 7. The method according to claim 6, wherein the step of identifying desired positions for the at least three late lean injectors is based upon the late lean injectors supporting the liner relative to the flow sleeve in a desired configuration. 8. The method according to claim 7, wherein the desired positions for the at least three late lean injectors comprises spaced angular positions about an approximate constant axial position within the liner/flow sleeve assembly. 9. The method according to claim 8, wherein the flow sleeve and the liner each comprises a circular cross-sectional shape; and wherein the desired configuration at which the liner is supported relative to the flow sleeve comprises an approximate concentric configuration. 10. The method according to claim 2, wherein the unassembled position comprises one in which the liner is outside of the flow sleeve; and wherein the assembled position comprises one in which the liner is inside of the flow sleeve and positioned similar to how the liner will be once the liner/flow sleeve assembly is assembled. 11. The method according to claim 6, wherein the unassembled position comprises one in which the liner is outside of the flow sleeve; and wherein the assembled position comprises one in which the liner is inside of the flow sleeve and positioned such that each of the transfer tubes aligns with a corresponding late lean nozzle. 12. The method according to claim 2, further comprising the step of forming a fuel passageway through flow sleeve; wherein the fuel passageway extends from a forward position to the late lean nozzle position; and wherein the late lean injection system comprises a system for injecting a mixture of fuel and air within the aft end of the primary combustion chamber defined by the liner. 13. The method according to claim 12, wherein the step of forming the fuel passageway comprises drilling. 14. The method according to claim 2, further comprising the steps of: sliding the transfer tube into a first position before the liner and the flow sleeve are positioned in the assembled position, the first position comprising one in which at least most of the transfer tube juts from an inner surface of the liner;sliding the transfer tube into a second position before connecting the transfer tube to the late lean nozzle, the second position comprising one in which at least most of the transfer tube juts from an outer surface of the liner. 15. The method according to claim 4, further comprising the steps of: welding the boss to the liner;welding the late lean nozzle to the flow sleeve; andconnecting the fuel passageway to the late lean nozzle. 16. The method according to claim 12, further comprising the step of installing the liner/flow sleeve assembly in the combustor once the liner/flow sleeve assembly is assembled. 17. The method according to claim 16, wherein installing the liner/flow sleeve assembly comprises rigidly attaching an aft end of the liner to a transition piece and rigidly attaching a forward end of the liner to a primary fuel nozzle assembly. 18. The method according to claim 16, further comprising the steps of: pressure testing the late lean injection system before installing the liner/flow sleeve assembly in the combustor; andinspecting the late lean injection system before installing the liner/flow sleeve assembly in the combustor. 19. The method according to claim 18, wherein the pressure testing comprises: pressure testing the connection between the transfer tube and the late lean nozzle for leaks; andpressure testing the connection between the fuel passageway and the late lean nozzle. 20. The method according to claim 16, wherein the combustor comprises a used combustor. 21. The method according to claim 2, wherein the flow annulus is configured to carry a supply of compressed air toward a forward end of the combustor; wherein the liner comprises an inner radial wall of the flow annulus and the flow sleeve comprises an outer radial wall of the flow annulus; andwherein the desired position at which the liner is supported relative to the flow sleeve comprises one in which the distance between the inner radial wall and the outer radial wall of the flow annulus conform to predetermined dimensional criteria. 22. The method according to claim 4, wherein the step of slideably engaging the transfer tube within the boss includes sliding the transfer tube into the boss from a position outside of the liner until the transfer tube projects into the interior of the liner; further comprising the step of rigidly connecting a stop to the portion of the transfer tube projecting into the interior of the liner;wherein, upon slidably withdrawing the transfer tube from the boss, the stop is configured to arrest further withdrawal once the transfer tube projects from the exterior surface of the liner a desired length. 23. The method according to claim 22, wherein the desired length that the transfer tube projects from the exterior surface of the liner coincides with a desired spatial relation between the liner and the flow sleeve in the liner/flow sleeve assembly; and wherein the stop comprises a rigid section of enlargement that is larger than the hollow passageway defined by the boss; andwherein the section of enlargement is configured to contact the boss such that further withdrawal of the transfer tube from the liner is arrested. 24. The method according to claim 4, wherein: the transfer tube comprises flow directing structure that defines a fluid passageway; wherein, at a first end, the flow directing structure includes an inlet and, about the inlet, attachment means, the attachment means configured to rigidly connect the transfer tube to the late lean nozzle; and, at a second end, the flow directing structure includes an outlet; andthe late lean nozzle comprises a cylindrical configuration that defines a hollow passageway through the flow sleeve; wherein a plurality of fuel outlets are formed on an inner surface of the cylindrical configuration, the fuel outlets being configured to fluidly communicate with the fuel passageway such that fuel flowing therethrough is injected into the hollow passageway from the fuel outlets; and wherein the late lean nozzle includes attachment means for rigidly attaching the late lean nozzle to the transfer tube.