US5634784A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Catalytic method
Assignee: Precision Combustion Inc
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Filing: 1994-04-14
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Granted: 1997-06-03
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Expires: 2014-04-14
Abstract
Abstract Gas phase combustion producing lower emissions in gas turbines is stabilized in a lean pre-mixed combustor, by flow of the fuel/air mixture through a catalyst which is heated by contact with recirculated, partially reacted combustion gases.
Inventors
- 👤 William C. Pfefferle
- 👤 E. Jack Sweet
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 06:22
CPC Classifications
F; F01; F01N; F01N3/00; F01N3/08; F01N3/10; F01N3/18; F01N3/24; F01N3/26; F01N3/28; F01N3/2882; F23; F23C; F23C13/00; F23C9/00; F23C9/006; F23R; F23R3/00; F23R3/40; F01N2250/00; F01N2250/04; F01N3/30; F02; F02B; F02B1/00; F02B1/02; F02B1/04; F23C2900/00; F23C2900/13002
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
100 words
A method for efficient combustion of fuel-air admixtures having an adiabatic flame temperature below 2000° Kelvin which comprises: a. reacting fuel with air in the presence of an oxidation catalyst disposed within a fuel burner, b. passing additional fuel and air into said burner, c. mixing said reacted fuel and air with said additional fuel and air, d. aerodynamically stabilizing combustion of the mixture of reacted fuel and air with the additional fuel and air; e. recirculating hot combustion products into contact with said catalyst to maintain said catalyst at a temperature effective for reaction of the fuel and air.
Claim 2
Independent Claim
100 words
A method for efficient combustion of fuel-air admixtures having an adiabatic flame temperature below 2000° Kelvin which comprises: a. reacting fuel with air in the presence of an oxidation catalyst disposed within a fuel burner, b. passing additional fuel and air into said burner, c. mixing said reacted fuel and air with said additional fuel and air, d. aerodynamically stabilizing combustion of the mixture of reacted fuel and air with the additional fuel and air; e. recirculating hot combustion products into contact with said catalyst to maintain said catalyst at a temperature effective for reaction of the fuel and air.
Claim 3
Dependent Claim
19 words
The method of claim 1 wherein passing the additional fuel and air is through vanes of a flow swirler.
Claim 4
Dependent Claim
20 words
The method of claim 1 wherein said catalyst comprises a metal of group VIII of the periodic table of elements.
Claim 5
Dependent Claim
13 words
The method of claim 1 wherein said aerodynamic stabilization is achieved using swirlers.
Claim 6
Dependent Claim
15 words
The method of claim 1 wherein said aerodynamic stabilization is achieved with a flow dump.
Claim 7
Dependent Claim
12 words
The method of claim 1 wherein said reacted fuel is a hydrocarbon.
Claim 8
Dependent Claim
162 words
A burner for clean combustion of fuels comprising: a. a tubular housing defining a tube lumen having an open first end and an open second end; b. aerodynamic combustion stabilization means mounted in the tube lumen between the first and the second end, said means having flow passages for passage of fuel and air in admixture; c. an oxidation catalyst within a passage of said aerodynamic means for combustion of fuel and air mixtures so as to provide reaction gases for admixture with additional fuel and additional air; d. means to provide a fuel-air mixture to said catalyst for combustion; e. a zone between the catalyst and the second open end of the lumen, for mixing the reaction gases and the additional fuel and the additional air and for recirculating the reaction gases mixed with additional fuel and additional air to the oxidation catalyst for further combustion; and f. means of delivering the additional fuel and the additional air to said zone.
Claim 9
Dependent Claim
162 words
A burner for clean combustion of fuels comprising: a. a tubular housing defining a tube lumen having an open first end and an open second end; b. aerodynamic combustion stabilization means mounted in the tube lumen between the first and the second end, said means having flow passages for passage of fuel and air in admixture; c. an oxidation catalyst within a passage of said aerodynamic means for combustion of fuel and air mixtures so as to provide reaction gases for admixture with additional fuel and additional air; d. means to provide a fuel-air mixture to said catalyst for combustion; e. a zone between the catalyst and the second open end of the lumen, for mixing the reaction gases and the additional fuel and the additional air and for recirculating the reaction gases mixed with additional fuel and additional air to the oxidation catalyst for further combustion; and f. means of delivering the additional fuel and the additional air to said zone.
Claim 10
Dependent Claim
13 words
The burner of claim 7 further comprising means to electrically heat said catalyst.
Claim 11
Dependent Claim
14 words
The burner of claim 7 wherein said aerodynamic stabilization means is a dump combustor.
Claim 12
Dependent Claim
22 words
The burner of claim 9 wherein said aerodynamic means comprises a swirler having vanes and flow passages formed by the swirler vanes.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2000-06-02 | 2000-12-02 | 2001-06-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2004-06-02 | 2004-12-02 | 2005-06-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2008-06-02 | 2008-12-02 | 2009-06-03 | $7700.00 | Window Closed / Lapsed |