Combustor and gas turbine
US-2024410584-A1 · Dec 12, 2024 · US
US2016201897A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016201897-A1 |
| Application number | US-201414913056-A |
| Country | US |
| Kind code | A1 |
| Filing date | Aug 19, 2014 |
| Priority date | Aug 20, 2013 |
| Publication date | Jul 14, 2016 |
| Grant date | — |
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Official abstract text for this publication.
In various embodiments, a dual fuel nozzle ( 200 ) for use in a gas 200 turbine engine is provided. The nozzle may be configured to supply and gas and a liquid. The dual fuel nozzle ( 200 ) may include an interior wall ( 217 ). The interior wall ( 217 ) may include a shoulder ( 219 ). The shoulder ( 219 ) may include one or more gas ports ( 216 ). Gas may be discharged through the gas ports ( 216 ) and penetrate a mixing zone.
Opening claim text (preview).
What is claimed is: 1 . A gas turbine fuel nozzle, comprising: a housing, defining a mixing chamber including a transition zone, the housing comprising, an interior wall comprising a shoulder and defining a fuel port in the shoulder, the fuel port configured to conduct a fuel into the mixing chamber, wherein the fuel propagates across a volume of the mixing chamber prior to reaching the transition zone. 2 . The gas turbine fuel nozzle of claim 1 , further comprising a liquid supply. 3 . The gas turbine fuel nozzle of claim 2 , wherein the liquid supply is configured to conduct a liquid to the transition zone. 4 . The gas turbine fuel nozzle of claim 3 , wherein the liquid is at least one of a liquid fuel and water. 5 . The gas turbine fuel nozzle of claim 1 , wherein the shoulder defines a plurality of fuel ports. 6 . The gas turbine fuel nozzle of claim 1 , wherein the fuel port has a diameter of approximately 0.090 inches to approximately 0.110 inches. 7 . The gas turbine fuel nozzle of claim 1 , wherein the fuel propagates away from the interior wall. 8 . A dual fuel nozzle, comprising: a gas supply; an interior wall comprising a shoulder, the shoulder defining a gas port; a housing defining a gas discharge zone configured to receive a gas from the gas port, the gas discharge zone comprising a transition zone; a liquid supply; and a liquid supply channel configured to conduct a liquid into the transition zone. 9 . The dual fuel nozzle of claim 8 , wherein the liquid is a liquid fuel. 10 . The dual fuel nozzle of claim 8 , wherein the liquid is water and is supplied to reduce emissions. 11 . The dual fuel nozzle of claim 8 , wherein the shoulder defines a plurality of gas ports. 12 . The dual fuel nozzle of claim 8 , wherein the gas penetrates a volume of the gas discharge zone. 13 . The dual fuel nozzle of claim 8 , wherein the gas propagates away from the interior way. 14 . The dual fuel nozzle of claim 8 , wherein the gas and the liquid mix in the transition zone. 15 . The dual fuel nozzle of claim 8 , further comprising an air channel configured to conduct air to the transition zone, wherein the air is mixed with the liquid and the gas. 16 . A dual fuel distribution system, comprising: a gas fuel supply; a housing comprising an interior wall defining a shoulder, the shoulder defining a plurality of gas ports, wherein gas from the gas fuel supply is conducted through the plurality of gas ports in a mixing chamber; a liquid supply; and a liquid distribution channel defined in the housing and configured to conduct a liquid from the liquid supply to a transition zone, wherein the transition zone is a portion of the mixing chamber. 17 . The dual fuel distribution system of claim 16 , wherein the gas fuel and the liquid are mixed in the transition zone. 18 . The dual fuel distribution system of claim 16 , wherein the housing further comprises an air supply that is configured to conduct air to the transition zone. 19 . The dual fuel distribution system of claim 16 , wherein the plurality of gas ports is 12 gas ports. 20 . The dual fuel distribution system of claim 16 , wherein the liquid is at least one of water and a liquid fuel.
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