System for reducing combustion dynamics by varying fuel flow axial distances
US-9255711-B2 · Feb 9, 2016 · US
US9347668B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9347668-B2 |
| Application number | US-201313797896-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 12, 2013 |
| Priority date | Mar 12, 2013 |
| Publication date | May 24, 2016 |
| Grant date | May 24, 2016 |
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A system includes an end cover for a multi-tube fuel nozzle. The end cover includes a first side, a second side disposed opposite the first side, a plurality of fuel injectors disposed on the first side, and at least one pre-orifice disposed within a passage within the end cover between the first and second sides. The pre-orifice is configured to be removed through the end cover from the second side.
Opening claim text (preview).
The invention claimed is: 1. A system comprising: an end cover of a multi-tube fuel nozzle, wherein the end cover comprises: a first side; a second side disposed opposite the first side; a plurality of fuel injectors disposed on the first side; a pre-orifice cavity extending through the end cover from the first side to the second side; and at least one pre-orifice conduit disposed within the pre-orifice cavity, wherein the at least one pre-orifice conduit comprises: a longitudinal wall having a first end portion and a second end portion, the first end portion disposed to the second side within the end cover and the second end portion extends through and beyond the first side, a plurality of apertures disposed on the longitudinal wall of the at least one pre-orifice conduit on the second end portion to deliver fuel to a fuel plenum, and wherein the at least one pre-orifice conduit is configured to be removed through the end cover from the second side. 2. The system of claim 1 , comprising a cover different from the end cover, the cover is disposed on the second side of the end cover over the pre-orifice cavity to enclose the at least one pre-orifice conduit within the end cover. 3. The system of claim 1 , wherein the pre-orifice conduit is breech-loaded through the second side into the end cover. 4. The system of claim 1 , wherein the end cover comprises the fuel plenum disposed within the end cover between the first and second sides, the second end portion of the at least one pre-orifice conduit is disposed within the fuel plenum, and the fuel plenum is in fluid communication with at least two or more fuel injectors of the plurality of fuel injectors. 5. The system of claim 1 , wherein the system comprises a gas turbine engine, a combustor, the multi-tube fuel nozzle, or a combination thereof, having the end cover. 6. The system of claim 2 , wherein the cover is configured to be removed to enable removal of the at least one pre orifice conduit through the end cover from the second side. 7. A system comprising: an end cover of a combustor for a gas turbine engine, wherein the end cover comprises: a first side; a second side disposed opposite the first side, wherein the first side is configured to reach a higher temperature relative to the second side during operation of the gas turbine engine; a plurality of pre-orifice cavities extending through the end cover from the first side to the second side; and a plurality of pre-orifice conduits disposed within respective said pre-orifice cavities within the end cover between the first and second sides, wherein each of the plurality of said pre-orifice conduits comprises: a respective longitudinal wall, wherein each of the respective longitudinal wall having a respective first end portion and a respective second end portion, a plurality of apertures disposed on each of the respective second end portion to deliver fuel to a fuel plenum, and wherein the each of the plurality of said pre-orifice conduits is configured to be removed through the end cover from the second side; and a plurality of covers, wherein each cover is different from the end cover and is disposed on the second side of the end cover over one of the respective pre-orifice cavities to enclose a respective pre-orifice conduit of the each of the plurality of said pre-orifice conduits within the end cover. 8. The system of claim 7 , wherein each of the cover is configured to be removed to enable removal of the respective pre-orifice conduit through the end cover from the second side. 9. The system of claim 7 , wherein the end cover comprises a plurality of fuel injectors disposed on the first side. 10. The system of claim 7 , wherein the each of the plurality of said pre-orifice conduits is breech-loaded through the second side into the end cover. 11. The system of claim 9 , wherein the end cover comprises a plurality of fuel plenums disposed within the end cover between the first and second sides, and each of the fuel plenum of the plurality of fuel plenums is in fluid communication with at least one or more fuel injectors of the plurality of fuel injectors. 12. The system of claim 11 , wherein a portion of a portion of the each of the plurality of said pre-orifice conduits extends into a respective fuel plenum of the plurality of fuel plenums. 13. The system of claim 12 , wherein the each of the plurality of said pre-orifice conduits is configured to provide fuel to the respective fuel plenum of the plurality of fuel plenums via a plurality of apertures disposed on the longitudinal wall of the respective pre-orifice conduit.
Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title
having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title
Repairing or maintaining combustion chamber liners or subparts · CPC title
Fluidic or fluid actuated device making · CPC title
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