Dual fuel nozzle system and apparatus

US2016201897A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016201897-A1
Application numberUS-201414913056-A
CountryUS
Kind codeA1
Filing dateAug 19, 2014
Priority dateAug 20, 2013
Publication dateJul 14, 2016
Grant date

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

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.

First claim

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.

Assignees

Inventors

Classifications

  • Nozzles · CPC title

  • F23C1/08Primary

    liquid and gaseous fuel · CPC title

  • F23R3/36Primary

    Supply of different fuels · CPC title

  • having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

  • Pulverising gas flow impinging on fuel from pre-filming surface, e.g. lip atomizers · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2016201897A1 cover?
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 (…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F23C1/08. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jul 14 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).