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US4863371A Expired / Lapsed US ⏱️ 0.0 years remaining

Low NOx high efficiency combustion process

Assignee: Praxair Technology Inc
•
Filing: 1988-06-03
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Granted: 1989-09-05
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Expires: 2008-06-03
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Abstract

Abstract A process to combust fuel and oxidant at high efficiency and with low NO x generation even when the fuel has non-uniform characteristics and the oxidant is pure oxygen, wherein fuel and oxidant are first combusted within a high velocity oxidant-rich jet, fuel is mixed with combustion products in a recirculation zone and the mixture is aspirated into the oxidant-rich jet and combusted in a diffuse secondary flame at the periphery of the oxidant-rich jet.

Inventors

  • 👤 Min-Da Ho

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 20:34
CPC Classifications
F; F23; F23C; F23C9/00; F23C9/006; F23C1/00; F23G; F23G5/00; F23G5/08; F23G5/12; F23L; F23L7/00; F23L7/007; F23C2202/00; F23C2202/40; Y; Y02; Y02E; Y02E20/00; Y02E20/34

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 126 words
A process for combusting fuel and oxidant at high efficiency with low NO x generation comprising: (A) injecting into a combustion zone fuel and oxidant in an oxidant-rich jet at a velocity sufficient to create a reduced pressure and consequently a strong recirculation zone within the combustion zone proximate the oxidant-rich jet; (B) combusting fuel and oxidant within the oxidant-rich jet to produce combustion products in a jet diluted with oxidant; (C) introducing fuel into the recirculation zone and mixing fuel and combustion products within the recirculation zone; (D) aspirating the mixture of fuel and combustion products into the oxidant rich jet; and (E) combusting the resulting diluted mixture in a diffuse secondary flame at the periphery of the oxidant-rich jet to produce further combustion products.
Claim 2
Dependent Claim 126 words
A process for combusting fuel and oxidant at high efficiency with low NO x generation comprising: (A) injecting into a combustion zone fuel and oxidant in an oxidant-rich jet at a velocity sufficient to create a reduced pressure and consequently a strong recirculation zone within the combustion zone proximate the oxidant-rich jet; (B) combusting fuel and oxidant within the oxidant-rich jet to produce combustion products in a jet diluted with oxidant; (C) introducing fuel into the recirculation zone and mixing fuel and combustion products within the recirculation zone; (D) aspirating the mixture of fuel and combustion products into the oxidant rich jet; and (E) combusting the resulting diluted mixture in a diffuse secondary flame at the periphery of the oxidant-rich jet to produce further combustion products.
Claim 3
Dependent Claim 15 words
The process of claim 1 wherein the oxidant comprises at least 30 volume percent oxygen.
Claim 4
Dependent Claim 11 words
The process of claim 1 wherein the oxidant is pure oxygen.
Claim 5
Dependent Claim 39 words
The process of claim 1 wherein the oxidant-rich jet contains oxygen in an amount within the range of from 300 to 2000 percent of the stoichiometric amount of oxygen necessary to completely combust the fuel in the oxidant-rich jet.
Claim 6
Dependent Claim 19 words
The process of claim 1 wherein the velocity of the oxidant-rich jet is at least 150 feet per second.
Claim 7
Dependent Claim 19 words
The process of claim 1 wherein the fuel and oxidant are injected into the combustion zone as a mixture.
Claim 8
Dependent Claim 17 words
The process of claim 1 wherein the fuel and oxidant are injected into the combustion zone separately.
Claim 9
Dependent Claim 44 words
The process of claim 7 wherein one of the fuel and oxidant is injected into the combustion zone as a central stream and the other of the fuel and oxidant is injected into the combustion zone as an annular stream around the central stream.
Claim 10
Dependent Claim 25 words
The process of claim 1 wherein the fuel introduced into the recirculation zone is fuel volatized from liquid and/or solid material within the combustion zone.
Claim 11
Dependent Claim 29 words
The process of claim 1 wherein the fuel introduced into the recirculation zone is fuel introduced into the combustion zone as a stream separate from the oxidant rich jet.
Claim 12
Dependent Claim 30 words
The process of claim 10 wherein said stream additionally contains oxygen in an amount up to 60 percent of the oxygen necessary to completely combust the fuel within said stream.
Claim 13
Dependent Claim 41 words
The process of claim 1 wherein the fuel introduced into the recirculation zone is both fuel volatized from liquid and/or solid material within the combustion zone and fuel introduced into the combustion zone as a stream separate from the oxidant-rich jet.
Claim 14
Dependent Claim 35 words
The process of claim 1 wherein the mass of the fuel and combustion products within the recirculation zone exceeds the mass of the oxidant- rich jet by a factor of at least 4 to 1.

References Cited (Backward Citations)

US4297093A Cited
US4378205A Cited
US4541796A Cited
US4408982A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-09-04 1993-03-06 1993-09-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-09-04 1997-03-06 1997-09-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-09-04 2001-03-06 2001-09-05 $7700.00 Window Closed / Lapsed

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