US20070207418A1 - Refractory burner tiles having improved emissivity and combustion apparatus employing the same - Google Patents
Refractory burner tiles having improved emissivity and combustion apparatus employing the same Download PDFInfo
- Publication number
- US20070207418A1 US20070207418A1 US11/653,440 US65344007A US2007207418A1 US 20070207418 A1 US20070207418 A1 US 20070207418A1 US 65344007 A US65344007 A US 65344007A US 2007207418 A1 US2007207418 A1 US 2007207418A1
- Authority
- US
- United States
- Prior art keywords
- emissivity
- coating
- combustion apparatus
- burner
- burner tiles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 19
- 239000000463 material Substances 0.000 claims abstract description 28
- 239000011248 coating agent Substances 0.000 claims abstract description 21
- 238000000576 coating method Methods 0.000 claims abstract description 21
- 239000000919 ceramic Substances 0.000 claims abstract description 5
- 239000011247 coating layer Substances 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 claims description 9
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 9
- 238000005524 ceramic coating Methods 0.000 description 5
- 239000000446 fuel Substances 0.000 description 4
- 230000004907 flux Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- -1 e.g. Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 238000009419 refurbishment Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M5/00—Casings; Linings; Walls
- F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
- F23M5/025—Casings; Linings; Walls characterised by the shape of the bricks or blocks used specially adapted for burner openings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/0003—Linings or walls
- F27D1/0006—Linings or walls formed from bricks or layers with a particular composition or specific characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/16—Making or repairing linings ; Increasing the durability of linings; Breaking away linings
- F27D1/1678—Increasing the durability of linings; Means for protecting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D99/00—Subject matter not provided for in other groups of this subclass
- F27D99/0001—Heating elements or systems
- F27D99/0033—Heating elements or systems using burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M2900/00—Special features of, or arrangements for combustion chambers
- F23M2900/05004—Special materials for walls or lining
Definitions
- the present invention relates generally to combustion apparatus such as process heaters, furnaces, boilers, and other fired heating systems.
- the present invention relates to combustion apparatus which include refractory burner tiles provided with improved emissivity characteristics.
- burners function to combust burner fuel and air so as to generate the required heat.
- the efficiency of the burner is very important to operators due to fuel costs and the need to reduce nitrogen oxides (NO x ) in the combustion gases.
- burners designed for combusting fuel with air in a manner resulting in less NO x emissions are commonly referred to as “low NO x ” burners and are well known in the art as evidenced by U.S. Pat. Nos. 6,905,328, 6,499,990 and 6,394,792, the entire content of each being expressly incorporated hereinto by reference.
- combustion apparatus are improved by providing a high emissivity (high-E) coating onto faces of refractory burner tiles.
- high-E high emissivity
- the combustion apparatus which employ the high-E coated burner tiles of the present invention may achieve longer service life, improved flame stability, easier combustion and a more stable flame pattern under a wide range of operating conditions.
- the performance of a combustion apparatus is improved by providing burner tiles therein which include a coating of a high-emissivity (high-E) material.
- the high-E material has an emissivity of greater than about 0.80, usually between about 0.85 to about 0.98. In some embodiments, the high-E material has an emissivity of about 0.92.
- the coating thickness of the high-E material on the burner tile can be between about 0.0005 to about 0.025 inch, preferably between about 0.001 to about 0.002 inch.
- the high-E material is ceramic. Burner tiles comprising a coating layer of the high-emissivity material may therefore be incorporated into a combustion apparatus so as to improve its performance.
- FIGURE is a partial cross-sectional elevational schematic view of a combustion apparatus employing the high-E coated burner tiles of the present invention.
- a high-emissivity (high-E) ceramic coating is applied to surfaces of burner tiles associated with a combustion apparatus so as to provide enhanced combustion. More specifically enhanced combustion of the burner fuel is provided according to the present invention by the higher heat energy (flux) from the high-E ceramic coated surfaces of the burner tiles.
- the emissivity (E) of a material is meant to refer to a unitless number measured on a scale between zero (total energy reflection) and 1.0 (a perfect “black body” capable of total energy absorption and re-radiation).
- a relatively high emissivity (high-E) is meant to refer to coating materials having an emissivity of greater than about 0.80, and usually between about 0.85 to about 0.98, and most preferably between about 0.85 to about 0.95.
- the accompanying drawing FIGURE depicts in schematic fashion a furnace 10 having a burner apparatus 12 operatively attached to the furnace's refractory wall 14 .
- Any suitable burner apparatus may be employed, such as the burner described in U.S. Pat. No. 5,961,312 (the entire content of which is expressly incorporated hereinto by reference.)
- the refractory wall 14 includes a burner tunnel 16 which is defined by burner tiles 18 .
- the burner tiles 18 depicted in the accompanying FIGURE define a generally cylindrical burner tunnel 16 , but other geometric shapes may be employed as desired.
- a square or rectangular burner tunnel 16 may be defined by the refractory tiles 18 .
- the individual burner tiles 18 are constructed of a body of refractory material, e.g., ceramics, conventionally employed for high temperature environments.
- the burner tiles 18 have a coating 20 on the surfaces thereof which is formed from a high-E ceramic material.
- a high-E ceramic coating material may be employed satisfactorily in the practice of the present invention.
- one presently preferred high-E ceramic coating includes CERAK R360/R370 ceramic coating commercially available form Cetek, Ltd. of Brook Park, Ohio, having an emissivity of about 0.92.
- the thickness of the coating 20 on the surfaces of the burner tiles 20 is not critical but will vary in dependence upon the desired resulting thermal flux and/or the particular material forming the coating. Thus, coating thicknesses of from about 0.0005 to about 0.025, usually between about 0.001 inch to about 0.002 inch may be appropriate. Coating densities will typically be greater than about 65%, more specifically 80% or greater, including up to 100%. By “coating density” is meant the amount (wt. %) of the high-E ceramic coating material that is present in the coating 20 .
- the high-E coating material may be applied to the burner tiles 18 in any conventional manner.
- the high-E coating material forming the coating 20 may thus be applied to the surfaces of the burner tiles 18 via any pressurized spray system while the burner tiles are being manufactured or while off-line (i.e., is not at its operational temperatures) during refurbishment.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
- Gas Burners (AREA)
Abstract
Description
- This application is related to and claims domestic priority benefits under 35 USC §119(e) from, U.S. Provisional Patent Application Ser. No. 60/771,480 filed on Feb. 8, 2006, the entire content of the same being expressly incorporated hereinto by reference.
- The present invention relates generally to combustion apparatus such as process heaters, furnaces, boilers, and other fired heating systems. In especially preferred forms, the present invention relates to combustion apparatus which include refractory burner tiles provided with improved emissivity characteristics.
- Many industrial applications require large scale generation of heat from burners for process heaters, boilers or other fired heating systems. In essence, the burners function to combust burner fuel and air so as to generate the required heat. The efficiency of the burner is very important to operators due to fuel costs and the need to reduce nitrogen oxides (NOx) in the combustion gases. In this regard, burners designed for combusting fuel with air in a manner resulting in less NOx emissions are commonly referred to as “low NOx” burners and are well known in the art as evidenced by U.S. Pat. Nos. 6,905,328, 6,499,990 and 6,394,792, the entire content of each being expressly incorporated hereinto by reference.
- According to the present invention, combustion apparatus are improved by providing a high emissivity (high-E) coating onto faces of refractory burner tiles. In such a manner, the combustion apparatus which employ the high-E coated burner tiles of the present invention may achieve longer service life, improved flame stability, easier combustion and a more stable flame pattern under a wide range of operating conditions.
- According to some embodiments, the performance of a combustion apparatus is improved by providing burner tiles therein which include a coating of a high-emissivity (high-E) material. Preferably, the high-E material has an emissivity of greater than about 0.80, usually between about 0.85 to about 0.98. In some embodiments, the high-E material has an emissivity of about 0.92.
- The coating thickness of the high-E material on the burner tile can be between about 0.0005 to about 0.025 inch, preferably between about 0.001 to about 0.002 inch. In especially preferred embodiments, the high-E material is ceramic. Burner tiles comprising a coating layer of the high-emissivity material may therefore be incorporated into a combustion apparatus so as to improve its performance.
- These and other aspects and advantages will become more apparent after careful consideration is given to the following detailed description of the preferred exemplary embodiments thereof.
- Reference will hereinafter be made to the accompanying drawings FIGURE which is a partial cross-sectional elevational schematic view of a combustion apparatus employing the high-E coated burner tiles of the present invention.
- According to the present invention, a high-emissivity (high-E) ceramic coating is applied to surfaces of burner tiles associated with a combustion apparatus so as to provide enhanced combustion. More specifically enhanced combustion of the burner fuel is provided according to the present invention by the higher heat energy (flux) from the high-E ceramic coated surfaces of the burner tiles.
- As used herein, the emissivity (E) of a material is meant to refer to a unitless number measured on a scale between zero (total energy reflection) and 1.0 (a perfect “black body” capable of total energy absorption and re-radiation). According to the present invention, a relatively high emissivity (high-E) is meant to refer to coating materials having an emissivity of greater than about 0.80, and usually between about 0.85 to about 0.98, and most preferably between about 0.85 to about 0.95.
- The accompanying drawing FIGURE depicts in schematic fashion a
furnace 10 having aburner apparatus 12 operatively attached to the furnace'srefractory wall 14. Any suitable burner apparatus may be employed, such as the burner described in U.S. Pat. No. 5,961,312 (the entire content of which is expressly incorporated hereinto by reference.) Therefractory wall 14 includes aburner tunnel 16 which is defined byburner tiles 18. In this regard, theburner tiles 18 depicted in the accompanying FIGURE define a generallycylindrical burner tunnel 16, but other geometric shapes may be employed as desired. For example, a square orrectangular burner tunnel 16 may be defined by therefractory tiles 18. Theindividual burner tiles 18 are constructed of a body of refractory material, e.g., ceramics, conventionally employed for high temperature environments. - Important to the present invention, the
burner tiles 18 have acoating 20 on the surfaces thereof which is formed from a high-E ceramic material. Virtually any commercially available high-E ceramic coating material may be employed satisfactorily in the practice of the present invention. For example, one presently preferred high-E ceramic coating includes CERAK R360/R370 ceramic coating commercially available form Cetek, Ltd. of Brook Park, Ohio, having an emissivity of about 0.92. - The thickness of the
coating 20 on the surfaces of theburner tiles 20 is not critical but will vary in dependence upon the desired resulting thermal flux and/or the particular material forming the coating. Thus, coating thicknesses of from about 0.0005 to about 0.025, usually between about 0.001 inch to about 0.002 inch may be appropriate. Coating densities will typically be greater than about 65%, more specifically 80% or greater, including up to 100%. By “coating density” is meant the amount (wt. %) of the high-E ceramic coating material that is present in thecoating 20. - The high-E coating material may be applied to the
burner tiles 18 in any conventional manner. The high-E coating material forming thecoating 20 may thus be applied to the surfaces of theburner tiles 18 via any pressurized spray system while the burner tiles are being manufactured or while off-line (i.e., is not at its operational temperatures) during refurbishment. - While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Claims (14)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/653,440 US20070207418A1 (en) | 2006-02-09 | 2007-01-16 | Refractory burner tiles having improved emissivity and combustion apparatus employing the same |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US77148006P | 2006-02-09 | 2006-02-09 | |
| US11/653,440 US20070207418A1 (en) | 2006-02-09 | 2007-01-16 | Refractory burner tiles having improved emissivity and combustion apparatus employing the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070207418A1 true US20070207418A1 (en) | 2007-09-06 |
Family
ID=38123952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/653,440 Abandoned US20070207418A1 (en) | 2006-02-09 | 2007-01-16 | Refractory burner tiles having improved emissivity and combustion apparatus employing the same |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20070207418A1 (en) |
| AR (1) | AR059369A1 (en) |
| WO (1) | WO2007091011A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070238058A1 (en) * | 2006-01-27 | 2007-10-11 | Fosbel Intellectual Limited | Longevity and performance improvements to flare tips |
| US20140212823A1 (en) * | 2013-01-25 | 2014-07-31 | Chevron U.S.A. Inc. | Reduction of NOx Emissions From Fired Heaters With Combustion Air Preheaters |
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|---|---|---|---|---|
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| US2207992A (en) * | 1937-06-26 | 1940-07-16 | T E Schundler & Co Inc | Combustion chamber |
| US2628088A (en) * | 1950-05-22 | 1953-02-10 | Kaiser Steel Corp | Refractory product |
| US2781756A (en) * | 1952-04-26 | 1957-02-19 | Kenneth A Kobe | Apparatus for submerged combustion of liquid fuels |
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| US4004789A (en) * | 1975-02-05 | 1977-01-25 | Bethlehem Steel Corporation | Tunnelized burner for panel type furnace |
| US4060379A (en) * | 1975-02-06 | 1977-11-29 | Hague International | Energy conserving process furnace system and components thereof |
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2007
- 2007-01-12 WO PCT/GB2007/000075 patent/WO2007091011A1/en not_active Ceased
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- 2007-02-08 AR ARP070100526A patent/AR059369A1/en unknown
Patent Citations (46)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2007605A (en) * | 1931-01-16 | 1935-07-09 | Globar Corp | Electric furnace |
| US2207992A (en) * | 1937-06-26 | 1940-07-16 | T E Schundler & Co Inc | Combustion chamber |
| US2628088A (en) * | 1950-05-22 | 1953-02-10 | Kaiser Steel Corp | Refractory product |
| US2791977A (en) * | 1950-08-03 | 1957-05-14 | Bernitz Furnace Appliance Comp | Refractory burner rings for furnace walls |
| US2781756A (en) * | 1952-04-26 | 1957-02-19 | Kenneth A Kobe | Apparatus for submerged combustion of liquid fuels |
| US2970829A (en) * | 1954-11-26 | 1961-02-07 | Reynders Charlton | Method of operation of a top-fired open hearth furnace |
| US2849860A (en) * | 1955-10-17 | 1958-09-02 | Norton Co | Rocket motor with recrystallized silicon carbide throat insert |
| US3007512A (en) * | 1955-10-28 | 1961-11-07 | Shell Oil Co | Burner for the burning of regenerator flue gas |
| US3216477A (en) * | 1963-08-08 | 1965-11-09 | Bernard W Devine | Flame safeguard systems and devices |
| US3215098A (en) * | 1963-09-26 | 1965-11-02 | Nat Beryllia Corp | Burner throat |
| US4004789A (en) * | 1975-02-05 | 1977-01-25 | Bethlehem Steel Corporation | Tunnelized burner for panel type furnace |
| US4060379A (en) * | 1975-02-06 | 1977-11-29 | Hague International | Energy conserving process furnace system and components thereof |
| US4072530A (en) * | 1976-06-17 | 1978-02-07 | Fuji Chemical Industries Company | Refractory furnace wall coating |
| US4202148A (en) * | 1978-06-26 | 1980-05-13 | Industrial Insulations, Inc. | Method of making thick-walled refractory fiber modules and the product formed thereby |
| US4363623A (en) * | 1979-02-07 | 1982-12-14 | Heinz Brune | Casings for heat exchangers and burner/recuperator assemblies incorporating such casings |
| US4455319A (en) * | 1982-07-06 | 1984-06-19 | Toastmaster, Inc. | Method of effecting long wavelength radiation cooking |
| US4445444A (en) * | 1982-08-12 | 1984-05-01 | Texaco Inc. | Burner for combusting oxygen-coal mixture |
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| US5356487A (en) * | 1983-07-25 | 1994-10-18 | Quantum Group, Inc. | Thermally amplified and stimulated emission radiator fiber matrix burner |
| US4655044A (en) * | 1983-12-21 | 1987-04-07 | United Technologies Corporation | Coated high temperature combustor liner |
| US5009070A (en) * | 1984-01-13 | 1991-04-23 | Hitachi, Ltd. | Combustion apparatus for gas turbine |
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| US5216981A (en) * | 1991-01-22 | 1993-06-08 | Advanced Fuel Research, Inc. | Coal-fired heating apparatus and method |
| US5220786A (en) * | 1991-03-08 | 1993-06-22 | General Electric Company | Thermally protected venturi for combustor dome |
| US5178921A (en) * | 1991-09-03 | 1993-01-12 | Inland Steel Company | Burner block assembly and material |
| US5383976A (en) * | 1992-06-30 | 1995-01-24 | Jx Crystals, Inc. | Compact DC/AC electric power generator using convective liquid cooled low bandgap thermophotovoltaic cell strings and regenerative hydrocarbon burner |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070238058A1 (en) * | 2006-01-27 | 2007-10-11 | Fosbel Intellectual Limited | Longevity and performance improvements to flare tips |
| US20140212823A1 (en) * | 2013-01-25 | 2014-07-31 | Chevron U.S.A. Inc. | Reduction of NOx Emissions From Fired Heaters With Combustion Air Preheaters |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2007091011A1 (en) | 2007-08-16 |
| AR059369A1 (en) | 2008-03-26 |
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