US5228283A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of reducing nox emissions in a gas turbine engine
Assignee: General Electric Co
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Filing: 1990-05-01
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Granted: 1993-07-20
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Expires: 2010-05-01
Abstract
Abstract A breech loaded fuel nozzle cartridge assembly is provided for use with a fuel nozzle capable of use with gaseous or distillate fuels. The cartridge assembly includes an elongated water delivery pipe having an interior through passageway extending from a rearward open end to a forward open end. A mounting coupling is fixed to the exterior of the pipe adjacent its rearward end for use in mounting the cartridge assembly within the rearward end of a fuel nozzle body. The forward end of the cartridge pipe is provided with an interior water swirler and an exterior distillate fuel swirler, while the forward end of the fuel nozzle body is provided with an air swirler so that at the fuel nozzle tip, an outer conical air spray, an intermediate distillate or gaseous fuel spray and an inner conical water spray combine to provide a homogenous mixture at the point of combustion.
Inventors
- 👤 Michael B. Sciocchetti
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 23:05
CPC Classifications
F; F23; F23R; F23R3/00; F23D; F23D17/00; F23D17/002; F02; F02C; F02C3/00; F02C3/20; F02C3/30; F23L; F23L7/00; F23L7/002
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
210 words
A method for reducing NOx emissions and for eliminating stress cracking in combustion components caused by combustion in a gas turbine comprising the steps of: (a) providing a fuel nozzle body having a nozzle assembly arranged to provide a fuel passageway, a combustion air passageway and a water passageway, the water passageway located substantially centrally along a longitudinal axis of the nozzle, the combustion air passageway lying radially outwardly of the water passageway, and the fuel passageway lying adjacent and radially outwardly of the combustion air passageway; (b) injecting fuel through said fuel passageway and into a combustion chamber of a gas turbine as a first conical spray; (c) injecting water through said water passageway in said nozzle assembly coincident with said longitudinal axis into said combustion chamber as a second, finely atomized conical spray located radially inwardly of said first conical spray so as to avoid direct water impingement on hot metal surfaces within said combustion chamber; and (d) injecting combustion air through said air passageway in said nozzle assembly into said combustion chamber as a third conical spray located radially between said first and said second conical sprays, wherein the fuel, water and combustion air are mixed upon discharge from said fuel nozzle body in said combustion chamber.
Claim 2
Independent Claim
210 words
A method for reducing NOx emissions and for eliminating stress cracking in combustion components caused by combustion in a gas turbine comprising the steps of: (a) providing a fuel nozzle body having a nozzle assembly arranged to provide a fuel passageway, a combustion air passageway and a water passageway, the water passageway located substantially centrally along a longitudinal axis of the nozzle, the combustion air passageway lying radially outwardly of the water passageway, and the fuel passageway lying adjacent and radially outwardly of the combustion air passageway; (b) injecting fuel through said fuel passageway and into a combustion chamber of a gas turbine as a first conical spray; (c) injecting water through said water passageway in said nozzle assembly coincident with said longitudinal axis into said combustion chamber as a second, finely atomized conical spray located radially inwardly of said first conical spray so as to avoid direct water impingement on hot metal surfaces within said combustion chamber; and (d) injecting combustion air through said air passageway in said nozzle assembly into said combustion chamber as a third conical spray located radially between said first and said second conical sprays, wherein the fuel, water and combustion air are mixed upon discharge from said fuel nozzle body in said combustion chamber.
Claim 3
Dependent Claim
12 words
The method according to claim 1 wherein said fuel is gaseous fuel.
Claim 4
Dependent Claim
34 words
The method of claim 2 and including providing a distillage fuel passageway in said nozzle assembly radially between said water passageway and said air passageway, and optionally injecting said distillate fuel into said combustion.
Claim 5
Dependent Claim
18 words
The method of claim 3 wherein said distillage fuel is swirled prior to discharge into said combustion chamber.
Claim 6
Dependent Claim
37 words
The method according to claim 1 wherein step (c) is carried out by loading a water feed cartridge into a rearward end of said fuel nozzle body to establish said center water passageway in said nozzle body.
Claim 7
Dependent Claim
36 words
The method according to claim 5 wherein step (b) is further carried out by locating a discharge orifice of said water feed cartridge axially adjacent and concentric with a discharge orifice of said fuel nozzle body.
Claim 8
Dependent Claim
18 words
The method of claim 1 wherein said combustion air is swirled prior to discharge into said combustion chamber.
Claim 9
Dependent Claim
18 words
The method of claim 1 wherein said gaseous fuel is swirled prior to discharge into said combustion chamber.
Claim 10
Dependent Claim
17 words
The method of claim 1 wherein said water is swirled prior to discharge into said combustion chamber.
Claim 11
Independent Claim
101 words
A method for reducing NOx emissions generated by combustion in a gas turbine engine comprising the steps of: a) introducing three discrete conical sprays of water, gaseous fuel and combustion air from a fuel nozzle into a combustion chamber wherein said water spray is radially innermost of said three discrete conical sprays of water, fuel and combustion air sprays and wherein said gaseous fuel spray is radially outermost of said three discrete sprays of water, fuel and combustion air; and b) mixing said water, fuel and combustion air to provide a homogeneous mixture in a combustion zone of the combustion chamber.
Claim 12
Independent Claim
101 words
A method for reducing NOx emissions generated by combustion in a gas turbine engine comprising the steps of: a) introducing three discrete conical sprays of water, gaseous fuel and combustion air from a fuel nozzle into a combustion chamber wherein said water spray is radially innermost of said three discrete conical sprays of water, fuel and combustion air sprays and wherein said gaseous fuel spray is radially outermost of said three discrete sprays of water, fuel and combustion air; and b) mixing said water, fuel and combustion air to provide a homogeneous mixture in a combustion zone of the combustion chamber.
Claim 13
Dependent Claim
21 words
The method of claim 10 wherein said water, fuel and air are each swirled prior to introduction into said combustion chamber.
Claim 14
Dependent Claim
37 words
The method of claim 10 and including the step of providing a distillate fuel passageway for optionally injecting distillage fuel as a fourth conical spray which is radially between said water spray and said combustion air spray.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1996-07-19 | 1997-01-18 | 1997-07-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2000-07-19 | 2001-01-18 | 2001-07-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2004-07-19 | 2005-01-18 | 2005-07-20 | $7700.00 | Window Closed / Lapsed |