Active and passive combustion stabilization for burners for highly and rapidly varying fuel gas compositions

US12072097B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12072097-B2
Application numberUS-202117451932-A
CountryUS
Kind codeB2
Filing dateOct 22, 2021
Priority dateMar 29, 2021
Publication dateAug 27, 2024
Grant dateAug 27, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A burner apparatus and process are described. The burner apparatus includes an inlet chamber in communication with a combustion chamber. A primary conduit delivers fuel gas to the combustion chamber. Each of a plurality of primary tips is located in the throat of the burner tile. Each of a plurality of cavities is disposed on a downstream wall of the burner tile and stabilize the flame. The primary tips have an end port and a lateral port. A secondary conduit provides fuel gas to a plurality of secondary tips. In a passive control mode, the fuel gas to the primary tips and secondary tips is a mixed gas comprising flue gas and fuel gas. In an active mode, valves are provided to proportion the amount of fuel gas fed to the primary tips and the amount of flue gas provided to the secondary tips.

First claim

Opening claim text (preview).

The invention claimed is: 1. A burner comprising: a plenum; a burner tile configured to provide combustion air from the plenum through the burner tile to a combustion zone, the burner tile having an upstream portion, a throat, and a downstream portion, the downstream portion having a wall and a plurality of cavities disposed on the wall; and at least one primary conduit having a plurality of primary tips configured to inject a fuel stream comprising fuel gas into the combustion zone, wherein each of the primary tips comprising a plurality of ports, wherein each of the plurality of cavities has a different diameter and is disposed at a different distance relative to the throat of the burner tile. 2. The burner of claim 1 , further comprising at least one secondary conduit having a plurality of secondary tips configured to inject a second portion of a second fuel stream downstream of the primary tips. 3. The burner of claim 2 , wherein the secondary tips are disposed radially outward with respect to the primary tips and wherein the secondary tips are disposed along an outer wall of the burner tile. 4. The burner of claim 2 , wherein each secondary tip comprises a lateral port and an end port, wherein the lateral port of each secondary tip is disposed on a side of the secondary tip and is angled toward an outer wall of the burner tile, and wherein the end port of each secondary tip is disposed at a distal end of the secondary tip and is angled toward the outer wall of the burner tile. 5. The burner of claim 4 , wherein the at least one primary conduit comprises a plurality of further secondary tips and wherein the at least one secondary conduit comprises a plurality of further primary tips. 6. The burner of claim 1 , wherein the wall of the burner tile is an inner wall that comprises a curved shoulder and a planar portion, and wherein each of the plurality of cavities is disposed on the planar portion. 7. The burner of claim 6 , wherein each primary tip comprises a lateral port and an end port, wherein the lateral port is disposed on a side of the primary tip and is angled toward the inner wall of the burner tile. 8. The burner of claim 7 , wherein each end port is disposed at a distal end of the primary tip and is angled toward the wall of the burner tile. 9. The burner of claim 1 , wherein the burner tile has an annular cross section and each of the plurality of cavities is defined by a curved cross section. 10. A burner comprising: a plenum; a burner tile arranged such that combustion air from the plenum flows from the plenum through the burner tile to a combustion zone, the burner tile having an upstream portion, a throat, and a downstream portion, the downstream portion having wall, and the burner tile further comprising a plurality of cavities disposed on the wall; at least one primary conduit having a plurality of primary tips configured to inject a first fuel stream comprising fuel gas into the combustion zone; at least one secondary conduit having a plurality of secondary tips configured to inject a second fuel stream; at least one sensor configured to sense one or more aspects of the combustion zone; a valve in fluid communication with the primary conduit and the secondary conduit; and a controller that receives inputs from the at least one sensor, wherein the controller is configured to operate the valve to control the one or more aspects of the combustion zone, wherein the valve is a three-way control valve configured to control a proportion of first fuel stream flow in the at least one primary conduit and a proportion of second fuel stream flow in the at least one secondary conduit. 11. The burner of claim 10 , wherein the second fuel stream is injected downstream relative to the first fuel stream. 12. The burner of claim 10 , wherein the wall of the burner tile is an inner wall. 13. The burner of claim 10 , wherein the at least one sensor is one of a camera, a pressure sensor, a thermocouple, a flame detector, a calorimeter, or a chromatograph. 14. The burner of claim 10 , wherein the at least one primary conduit comprises a plurality of further primary tips and wherein the at least one secondary conduit comprises a plurality of further secondary tips. 15. The burner of claim 14 , wherein the valve is a three-way control valve configured to control a proportion of the first fuel stream flow in the at least one conduit and a proportion of the second fuel stream flow in the at least one secondary conduit, and further comprising a further control valve configured to control a proportion of the first fuel stream flow in the plurality of further secondary tips and a proportion of the second fuel stream flow in the plurality of further primary tips. 16. The burner of claim 10 , wherein the burner tile has an annular cross section and each of the plurality of cavities is defined by a curved wall. 17. A burner comprising: a plenum; a burner tile configured to provide combustion air from the plenum through the burner tile to a combustion zone, the burner tile having an upstream portion, a throat, and a downstream portion, the downstream portion having a wall and a plurality of cavities disposed on the wall; and at least one primary conduit having a plurality of primary tips configured to inject a fuel stream comprising fuel gas into the combustion zone, wherein each of the primary tips comprising a plurality of ports, wherein the wall of the burner tile is an inner wall that comprises a curved shoulder and a planar portion, and wherein each of the plurality of cavities is disposed on the planar portion, wherein each primary tip comprises a lateral port and an end port, wherein the lateral port is disposed on a side of the primary tip and is angled toward the inner wall of the burner tile.

Assignees

Inventors

Classifications

  • with different fuels in stages · CPC title

  • with fuel supply in stages · CPC title

  • using electronic means · CPC title

  • using devices responsive to thermal changes or to thermal expansion of a medium · CPC title

  • F23N1/002Primary

    using electronic means (F23N1/04 - F23N1/10 take precedence) · CPC title

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Frequently asked questions

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What does patent US12072097B2 cover?
A burner apparatus and process are described. The burner apparatus includes an inlet chamber in communication with a combustion chamber. A primary conduit delivers fuel gas to the combustion chamber. Each of a plurality of primary tips is located in the throat of the burner tile. Each of a plurality of cavities is disposed on a downstream wall of the burner tile and stabilize the flame. The pri…
Who is the assignee on this patent?
Honeywell Int Inc
What technology area does this patent fall under?
Primary CPC classification F23N1/002. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 27 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 6 related publications on this page (citations in our corpus or others sharing the same primary CPC).