US4864811A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for destroying hazardous organics
Assignee: Individual
•
Filing: 1987-09-21
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Granted: 1989-09-12
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Expires: 2007-09-21
Abstract
Abstract The present invention provides a method for the destruction of hazardous carbonaceous wastes by the plug flow, thermal combustion of said wastes comprising (a) obtaining an intimate admixture of vaporized fuel and air, said admixture containing at least a stoichiometric amount of air, (b) passing said admixture to a plug flow combustion zone, and (c) effecting sustained and essentially complete combustion of said fuel under essentially adiabatic conditions to destroy said wastes and to form a combustion effluent of high thermal energy; said combustion being characterized by said fuel-air admixture having an adiabatic flame temperature such that that actual flame temperature in the combustion zone is greater than about 1350K.
Inventors
- 👤 William C. Pfefferle
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 00:31
CPC Classifications
F; F23; F23G; F23G7/00; F23G7/06; F23G7/07; F02; F02C; F02C3/00; F02C3/20; F23C; F23C13/00; F23G7/061; F23G7/065; F23G2206/00; F23G2206/20; F23G2206/203; F23G2209/00; F23G2209/14; F23G2209/142; F23G2900/00; F23G2900/70; F23G2900/7011; Y; Y02; Y02E; Y02E20/00; Y02E20/12
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
164 words
A method for the destruction of fuels of hazardous carbonaceous wastes by the thermal combustion of said wastes comprising (a) providing a catalytically stabilized plug flow combustion zone having inner flow channels and peripheral outer flow channels, the outer peripheral channels of which are blocked to thermally insulate the inner channels and prevent by-passing of non-combusted waste therethrough; (b) obtaining an intimate admixture of vaporized hazardous carbonaceous wastes and air, said admixture containing at least a stoichiometric amount of air for substantially complete combustion of the wastes; (c) passing said admixture to the insulated plug flow combustion zone; and (d) effecting sustained and essentially complete combustion of said admixture under essentially adiabatic conditions to destroy said hazardous wastes and to form a heated combustion effluent essentially free of said hazardous wastes; said combustion being characterized by said fuel-air admixture having an adiabatic flame temperature such that each inner flow channel has an actual flame temperature in the combustion zone greater than about 1350° K.
Claim 2
Independent Claim
164 words
A method for the destruction of fuels of hazardous carbonaceous wastes by the thermal combustion of said wastes comprising (a) providing a catalytically stabilized plug flow combustion zone having inner flow channels and peripheral outer flow channels, the outer peripheral channels of which are blocked to thermally insulate the inner channels and prevent by-passing of non-combusted waste therethrough; (b) obtaining an intimate admixture of vaporized hazardous carbonaceous wastes and air, said admixture containing at least a stoichiometric amount of air for substantially complete combustion of the wastes; (c) passing said admixture to the insulated plug flow combustion zone; and (d) effecting sustained and essentially complete combustion of said admixture under essentially adiabatic conditions to destroy said hazardous wastes and to form a heated combustion effluent essentially free of said hazardous wastes; said combustion being characterized by said fuel-air admixture having an adiabatic flame temperature such that each inner flow channel has an actual flame temperature in the combustion zone greater than about 1350° K.
Claim 3
Dependent Claim
13 words
The method of claim 1 wherein combustion is stabilized by a combustion catalyst.
Claim 4
Dependent Claim
13 words
The method of claim 2 wherein said catalyst comprises a metal honeycomb structure.
Claim 5
Independent Claim
170 words
The method of operating a gas turbine by the thermal combustion of fuels of carbonaceous wastes comprising the steps of (a) providing a catalytically stabilized plug flow combustion zone having inner flow channels and peripheral outer flow channels, the outer peripheral channels of which are blocked to thermally insulate the inner channels and to prevent by-passing of non-combusted waste therethrough; (b) obtaining an intimate admixture of vaporized carbonaceous wastes and air, said admixture containing at least a stoichiometric amount of air; (c) passing said admixture to the insulated plug flow combustion zone; and (d) effecting sustained and essentially complete combustion of said admixture under essentially adiabatic conditions to destroy said hazardous wastes thereby forming a heated combustion effluent essentially free of said hazardous wastes; said combustion being characterized by said admixture having an adiabatic flame temperature such that each inner flow channel has an actual flame temperature in the combustion zone greater than about; 1350° K. passing said effluent from said combustion zone through a turbine to rotate said turbine.
Claim 6
Independent Claim
170 words
The method of operating a gas turbine by the thermal combustion of fuels of carbonaceous wastes comprising the steps of (a) providing a catalytically stabilized plug flow combustion zone having inner flow channels and peripheral outer flow channels, the outer peripheral channels of which are blocked to thermally insulate the inner channels and to prevent by-passing of non-combusted waste therethrough; (b) obtaining an intimate admixture of vaporized carbonaceous wastes and air, said admixture containing at least a stoichiometric amount of air; (c) passing said admixture to the insulated plug flow combustion zone; and (d) effecting sustained and essentially complete combustion of said admixture under essentially adiabatic conditions to destroy said hazardous wastes thereby forming a heated combustion effluent essentially free of said hazardous wastes; said combustion being characterized by said admixture having an adiabatic flame temperature such that each inner flow channel has an actual flame temperature in the combustion zone greater than about; 1350° K. passing said effluent from said combustion zone through a turbine to rotate said turbine.
Claim 7
Dependent Claim
12 words
The method of claim 4 wherein combustion is stabilized by a catalyst.
Claim 8
Dependent Claim
39 words
The method of claim 5 wherein said catalyst comprises a metal honeycomb and said honeycomb is sealed against by-passing of gases by attaching said catalyst to a metal seal ring and fastening said seal ring to the combustor wall.
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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) | 1992-09-11 | 1993-03-13 | 1993-09-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-09-11 | 1997-03-13 | 1997-09-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-09-11 | 2001-03-13 | 2001-09-12 | $7700.00 | Window Closed / Lapsed |