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US4531904A Expired / Lapsed US ⏱️ 0.0 years remaining

Low NOx level combustion method in a radiant tube burner and a burning apparatus used for the method

Assignee: JFE Steel Corp
•
Filing: 1984-11-01
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Granted: 1985-07-30
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Expires: 2004-11-01
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Abstract

Abstract A method of burning a fuel gas in a low NO x level in the exhaust gas is disclosed, wherein a radiant tube burner having concentrically arranged outer air flow nozzle, fuel gas nozzles arranged in a circle and inner air flow nozzle and having a particular structure is used and the fuel gas is burnt under a particularly limited condition.

Inventors

  • 👤 Kuniaki Sato
  • 👤 Shinichiro Muto
  • 👤 Fumiya Yanagishima
  • 👤 Yuji Shimoyama

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 19:02
CPC Classifications
F; F23; F23C; F23C6/00; F23C6/04; F23C6/045; F23D; F23D14/00; F23D14/20; F23D14/22

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 436 words
A low NOx level combustion method in a radiant tube burner, the method comprising flowing an inner air flow in an inner air flow conduit connected to a source of combustion air, and arranged centrally of an annular chamber in the radiant tube, the chamber being provided with a base portion connected to the inner air flow conduit and having a rim portion integrally formed at the peripheral edge thereof, said chamber forming in the radiant tube an annular fuel space bounded by the rim portion and the central inner air flow conduit, flowing a fuel gas flow through a plurality of fuel-gas conduits connected at a first end to a fuel gas source and arranged in a circle in the radiant tube so as to surround the inner air flow conduit, said plurality of fuel-gas conduits opening at a second end open into the base portion of said chamber to form fuel-gas openings, said fuel gas openings communicating with the annular fuel space therethrough, jetting the fuel-gas flow into a primary combustion region adjacent to the rim portion of said chamber and surrounding the inner air flow conduit through said fuel-gas openings arranged in said chamber at the second end of said fuel-gas conduits, the inner air flow conduit extending forwardly and downstream of said chamber in the flowing direction of the fuel gas and along a central axis of the radiant tube, jetting the inner air flow into a secondary combustion region through an open end of the inner air flow conduit, and jetting an outer air flow in communication with the combustion air source and surrounding the fuel gas flow into the primary combustion region through a passage formed between the radiant tube and the rim portion of said chamber, the fuel gas being primarily burnt by the outer air flow and then secondarily burnt by the inner air flow, and further comprising jetting the fuel gas flow by means of 3˜6 fuel gas openings arranged in said chamber, carrying out a primary combustion of the fuel gas by controlling the ratio of the amount of the inner air flow to the total amount of introduced air to 35-80%, and limiting the momentum ratio of the fuel gas flow to the outer air flow to not lower than 0.40, and further carrying out a secondary combustion of the primarily burnt fuel gas by setting the length of the inner air flow conduit such that the secondary combustion is carried out at a time substantially later than the time of the primary combustion, whereby a uniform and smooth two stage combustion is carried out.
Claim 2
Dependent Claim 436 words
A low NOx level combustion method in a radiant tube burner, the method comprising flowing an inner air flow in an inner air flow conduit connected to a source of combustion air, and arranged centrally of an annular chamber in the radiant tube, the chamber being provided with a base portion connected to the inner air flow conduit and having a rim portion integrally formed at the peripheral edge thereof, said chamber forming in the radiant tube an annular fuel space bounded by the rim portion and the central inner air flow conduit, flowing a fuel gas flow through a plurality of fuel-gas conduits connected at a first end to a fuel gas source and arranged in a circle in the radiant tube so as to surround the inner air flow conduit, said plurality of fuel-gas conduits opening at a second end open into the base portion of said chamber to form fuel-gas openings, said fuel gas openings communicating with the annular fuel space therethrough, jetting the fuel-gas flow into a primary combustion region adjacent to the rim portion of said chamber and surrounding the inner air flow conduit through said fuel-gas openings arranged in said chamber at the second end of said fuel-gas conduits, the inner air flow conduit extending forwardly and downstream of said chamber in the flowing direction of the fuel gas and along a central axis of the radiant tube, jetting the inner air flow into a secondary combustion region through an open end of the inner air flow conduit, and jetting an outer air flow in communication with the combustion air source and surrounding the fuel gas flow into the primary combustion region through a passage formed between the radiant tube and the rim portion of said chamber, the fuel gas being primarily burnt by the outer air flow and then secondarily burnt by the inner air flow, and further comprising jetting the fuel gas flow by means of 3˜6 fuel gas openings arranged in said chamber, carrying out a primary combustion of the fuel gas by controlling the ratio of the amount of the inner air flow to the total amount of introduced air to 35-80%, and limiting the momentum ratio of the fuel gas flow to the outer air flow to not lower than 0.40, and further carrying out a secondary combustion of the primarily burnt fuel gas by setting the length of the inner air flow conduit such that the secondary combustion is carried out at a time substantially later than the time of the primary combustion, whereby a uniform and smooth two stage combustion is carried out.
Claim 3
Dependent Claim 72 words
A method according to claim 1, further comprising arranging a retention flange on said rim portion in an upstream side of the outer air flow passage for jetting the outer air flow therethrough, whereby the rate of the outer air flow is adjusted, the outer air flow is made into a steady flow, and the fuel gas is primarily burnt by the jet of the steady flow of the outer air flow.

References Cited (Backward Citations)

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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) 1988-07-29 1989-01-28 1989-07-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-07-29 1993-01-28 1993-07-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-07-29 1997-01-28 1997-07-30 $7700.00 Window Closed / Lapsed

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