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US5267850A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel jet burner

Assignee: Praxair Technology Inc
•
Filing: 1992-06-04
•
Granted: 1993-12-07
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Expires: 2012-06-04
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Abstract

Abstract A burner system and combustion method for high temperature applications employing a high velocity central fuel stream and a low velocity annular coaxial oxidant stream to carry out stable steady combustion in an expanding combusting stream within a cavity stably attached to the fuel nozzle so as to prevent combustion zone furnace gases from entering the cavity.

Inventors

  • 👤 Hisashi Kobayashi
  • 👤 Arthur W. Francis, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 20:14
CPC Classifications
F; F23; F23D; F23D14/00; F23D14/20; F23D14/22; C; C03; C03B; C03B5/00; C03B5/16; C03B5/235; C03B5/2353; F23D14/32; F23D2900/00; F23D2900/00006; Y; Y02; Y02P; Y02P40/00; Y02P40/50

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 167 words
A combustion method for carrying out high temperature combustion comprising: (A) providing a substantially cylindrical cavity having an opening with a diameter D communicating with a combustion zone containing furnace gases; (B) injecting a fuel stream through a nozzle into the cavity at a point recessed from the opening at a high velocity not less than 200 feet per second, said recess having a length L such that L/D is at least 1.0 but not more than 4.0; (C) injecting oxidant having an oxygen concentration of at least 30 percent into the cavity in an annular stream coaxially with the fuel stream at a low velocity not more than 100 feet per second; (D) establishing a stable flame attached to the nozzle while combusting fuel and oxidant in an expanding stream within the cavity and passing the combusting stream into the combustion zone to produce furnace gases; and (E) maintaining furnace gases outside the cavity and entraining furnace gases into the combusting stream within the combustion zone.
Claim 2
Dependent Claim 167 words
A combustion method for carrying out high temperature combustion comprising: (A) providing a substantially cylindrical cavity having an opening with a diameter D communicating with a combustion zone containing furnace gases; (B) injecting a fuel stream through a nozzle into the cavity at a point recessed from the opening at a high velocity not less than 200 feet per second, said recess having a length L such that L/D is at least 1.0 but not more than 4.0; (C) injecting oxidant having an oxygen concentration of at least 30 percent into the cavity in an annular stream coaxially with the fuel stream at a low velocity not more than 100 feet per second; (D) establishing a stable flame attached to the nozzle while combusting fuel and oxidant in an expanding stream within the cavity and passing the combusting stream into the combustion zone to produce furnace gases; and (E) maintaining furnace gases outside the cavity and entraining furnace gases into the combusting stream within the combustion zone.
Claim 3
Dependent Claim 10 words
The method of claim 1 wherein the fuel comprises methane.
Claim 4
Dependent Claim 17 words
The method of claim 1 wherein the oxidant has an oxygen concentration of at least 90 percent.
Claim 5
Dependent Claim 12 words
The method of claim 1 wherein the oxidant is technically pure oxygen.
Claim 6
Dependent Claim 32 words
The method of claim 1 wherein the oxidant is injected into the cavity at a point further recessed from the opening than is the point where fuel is injected into the cavity.

References Cited (Backward Citations)

US2138998A Cited
US4797087A Cited
US4690635A Cited
US4986748A Cited
US5100313A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1996-12-06 1997-06-07 1997-12-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2000-12-06 2001-06-07 2001-12-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2004-12-06 2005-06-07 2005-12-07 $7700.00 Window Closed / Lapsed

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