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US4104017A Expired / Lapsed US ⏱️ 0.0 years remaining

Metallic non-premixed gas-burner with counter-rotation of gases

Assignee: Engie SA
•
Filing: 1977-03-30
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Granted: 1978-08-01
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Expires: 1997-03-30
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Abstract

Abstract The metallic gas-burner of the invention comprises a central fire-tube constituting a mixing and combustion chamber into which is admitted a fuel-gas and a gaseous combustion agent from an annular air-box surrounding the fire-tube. The fuel-gas is supplied at a low pressure into the rear of the fire-tube and the gaseous combustion agent is distributed at a low pressure into the fire-tube, in the form of at least three main flows from the rear to the front of the tube, the second and third flows being provided in counter-rotation relationship.

Inventors

  • 👤 Jean-Marie Georges Fernand Alin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 14:41
CPC Classifications
F; F23; F23D; F23D14/00; F23D14/20; F23D14/22; F23D14/24

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 250 words
A metallic gas-burner with high-velocity gas outflow allowing a high temperature of the burnt gases to be obtained, of the type comprising a central fire-tube comprising a rear portion closed by a rear wall, and a front portion on both sides of a medial transverse plane, said fire-tube constituting a mixing and combustion chamber into which is admitted, on the one hand, a fuel-gas and, on the other hand a gaseous combustion agent usually air, from an annular space constituting an air box provided between the outer wall of the said fire-tube and an external tube surrounding it, the said burner being provided at its front end portion with a front plate closing the said air-box, wherein the fuel gas is supplied at a low pressure, e.g. on the order of a few tens of millibars, into the rear of the fire-tube by a fuel-gas intake and the gaseous combustion agent is distributed at a low pressure into the said fire-tube in the form of at least essentially three main flows from the rear to the front of the said tube, the intake of the first flow being provided in a transverse plane close to the rear wall of the said fire-tube, the intakes of the second and third flows being provided in counter-rotation relationship with respect to one another, the second flow being fed into the rear portion of the fire-tube and the said third flow being fed into its front portion beyond the said medial transverse plane respectively.
Claim 2
Dependent Claim 250 words
A metallic gas-burner with high-velocity gas outflow allowing a high temperature of the burnt gases to be obtained, of the type comprising a central fire-tube comprising a rear portion closed by a rear wall, and a front portion on both sides of a medial transverse plane, said fire-tube constituting a mixing and combustion chamber into which is admitted, on the one hand, a fuel-gas and, on the other hand a gaseous combustion agent usually air, from an annular space constituting an air box provided between the outer wall of the said fire-tube and an external tube surrounding it, the said burner being provided at its front end portion with a front plate closing the said air-box, wherein the fuel gas is supplied at a low pressure, e.g. on the order of a few tens of millibars, into the rear of the fire-tube by a fuel-gas intake and the gaseous combustion agent is distributed at a low pressure into the said fire-tube in the form of at least essentially three main flows from the rear to the front of the said tube, the intake of the first flow being provided in a transverse plane close to the rear wall of the said fire-tube, the intakes of the second and third flows being provided in counter-rotation relationship with respect to one another, the second flow being fed into the rear portion of the fire-tube and the said third flow being fed into its front portion beyond the said medial transverse plane respectively.
Claim 3
Dependent Claim 42 words
A burner according to claim 1, wherein the gyratory moments of the said second and third flows of gaseous combustion agent in counter-rotation relationship with respect to one another are such that there subsists a partial residual rotation of the fuel mixture.
Claim 4
Dependent Claim 40 words
A burner according to claim 1, wherein a fourth annular intake of gaseous combustion agent into the fire-tube is ensured at the front end of the burner, in substantially counter-flow relationship to the flow of the gases in the fire-tube.
Claim 5
Dependent Claim 34 words
A burner according to claim 2, wherein the flow rate of the said second flow of gaseous combustion agent is lower than the flow rate of the said third flow of gaseous combustion agent.
Claim 6
Dependent Claim 36 words
A burner according to claim 4, wherein the flow rate of the said second flow of gaseous combustion agent is substantially equal to half the flow rate of the said third flow of gaseous combustion agent.
Claim 7
Dependent Claim 46 words
A burner according to claim 3, wherein the said fourth, annular intake of gaseous combustion agent takes place from the air-box through a gap provided between a ring interval with the said front plate of the said burner and the front end portion of the fire-tube.
Claim 8
Dependent Claim 50 words
A burner according to claim 1, wherein, in a manner known per se, the said front plate of the burner is provided with a part extending beyond the said fire-tube so as to ensure a constriction of the outlet section and to increase the outflow velocity of the burnt gases.
Claim 9
Dependent Claim 27 words
A burner according to claim 1, wherein the said first flow of gaseous combustion agent close to the rear wall of the said fire-tube is distributed radially.
Claim 10
Dependent Claim 34 words
A burner according to claim 1; wherein, the intake of fuel-gas takes place at the rear end of the fire tube, rearward of the various flows of gaseous combustion agent admitted into the burner.
Claim 11
Dependent Claim 39 words
A burner according to claim 9, wherein the intake of fuel-gas into the rear of the fire-tube takes place in a transverse plane of the said fire-tube, e.g. radially, a little rearward of the first gaseous combustion agent intake.
Claim 12
Dependent Claim 71 words
A burner according to claim 1, wherein the intake of the first flow of gaseous combustion agent takes place through a great number of small openings, the intake of the second gaseous combustion agent takes place through a small number of large openings, and the intake of the third flow of gaseous combustion agent takes place through large openings greater in number than the intake openings for the said second flow.
Claim 13
Dependent Claim 46 words
A burner according to claim 11, wherein the total section of the said small intake openings for the said first flow of gaseous combustion agent is of the same order of magnitude as the total section of the large intake openings for the said second flow.

References Cited (Backward Citations)

US3273623A Cited
US3951584A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-07-31 1982-01-30 1982-08-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-07-31 1986-01-30 1986-08-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-07-31 1990-01-30 1990-08-01 $7700.00 Window Closed / Lapsed

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