CA2653890C - Method and apparatus for staged combustion of air and fuel - Google Patents
Method and apparatus for staged combustion of air and fuel Download PDFInfo
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- CA2653890C CA2653890C CA2653890A CA2653890A CA2653890C CA 2653890 C CA2653890 C CA 2653890C CA 2653890 A CA2653890 A CA 2653890A CA 2653890 A CA2653890 A CA 2653890A CA 2653890 C CA2653890 C CA 2653890C
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- duct
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- air
- burner
- flow
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
- F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
- F23C6/047—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure with fuel supply in stages
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L9/00—Passages or apertures for delivering secondary air for completing combustion of fuel
- F23L9/02—Passages or apertures for delivering secondary air for completing combustion of fuel by discharging the air above the fire
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N1/00—Regulating fuel supply
- F23N1/02—Regulating fuel supply conjointly with air supply
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2201/00—Staged combustion
- F23C2201/10—Furnace staging
- F23C2201/101—Furnace staging in vertical direction, e.g. alternating lean and rich zones
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2201/00—Staged combustion
- F23C2201/20—Burner staging
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2209/00—Safety arrangements
- F23D2209/20—Flame lift-off / stability
Abstract
A method for operating a fuel-fired furnace including at least one burner is provided.
The method includes channeling a first fluid flow to the at least one burner at a first predetermined velocity, and channeling a second fluid flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner. The second predetermined velocity is different than the first predetermined velocity.
The method includes channeling a first fluid flow to the at least one burner at a first predetermined velocity, and channeling a second fluid flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner. The second predetermined velocity is different than the first predetermined velocity.
Description
METHOD AND APPARATUS FOR STAGED COMBUSTION OF AIR AND
FUEL
BACKGROUND OF THE INVENTION
This invention relates generally to combustion devices and, more particularly, to a multi-function burner for use with combustion devices.
During a typical combustion process within a furnace or boiler, for example, a flow of combustion gas, or flue gas, is produced. Known combustion gases contain combustion products including, but not limited to, carbon, fly ash, carbon dioxide, carbon monoxide, water, hydrogen, nitrogen, sulfur, chlorine, and/or mercury generated as a result of combusting solid and/or liquid fuels.
At least some known furnaces use air/fuel staged combustion, such as a three-stage combustion, to facilitate reducing the production of at least some of the combustion products, such as nitrogen oxide (NOx). A three-stage combustion process includes combusting fuel and air in a first stage, introducing fuel into the combustion gases in a second stage, and then introducing air into the combustion gases in a third stage. In the second stage, fuel is injected, without combustion air, to form a sub-stoichiometric, or fuel-rich, zone. During the second stage, at least some of the fuels combust to produce hydrocarbon fragments that react with NOx that may have been produced in the first stage. As such, the NOx may be reduced to atmospheric nitrogen in the second stage. In the third stage, air is injected to consume the carbon monoxide and unburnt hydrocarbons exiting the second stage. Although such air/fuel staging may achieve relatively high NOx reduction, the use of injectors that are dedicated to either air injection or fuel/air combustion may limit the operation of the furnace and may limit the flexibility in staging air and/or fuel.
BRIEF DESCRIPTION OF THE INVENTION
In one aspect, a method for operating a fuel-fired furnace including at least one burner is provided. The method includes channeling a first fluid flow to the at least one burner at a first predetermined velocity, and channeling a second fluid flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner. The second predetermined velocity is different than the first predetermined velocity.
In another aspect a burner for use with a fuel-fired furnace is provided. The burner includes a first duct configured to channel a fuel flow into the furnace, and a second duct substantially concentrically-aligned with and extending through the first duct.
The second duct is configured to channel a first fluid flow into the furnace, wherein the first fluid flow is a non-fuel flow.
In a still further aspect a fuel-fired furnace coupled to a fuel source and an air source is provided. The furnace includes a combustion zone defined within the furnace, and a plurality of burners coupled within the combustion zone. At least one of the plurality of burners includes a first duct coupled to the fuel source via a first flow regulation device. The furnace also includes a second duct extending through the first duct, wherein the second duct is coupled to the air source via a second flow regulation device. The first flow regulation device and the second flow regulation device are selectively operable based on an operation of the furnace.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a schematic view of an exemplary power plant system.
Figure 2 is a schematic view of an exemplary burner that may be used with the power plant system shown in Figure 1.
Figure 3 is a schematic view of an alternative burner that may be used with the power plant system shown in Figure 1.
DETAILED DESCRIPTION OF THE INVENTION
Figure 1 is a schematic view of an exemplary power plant system 10. In the exemplary embodiment, system 10 is supplied with fuel 12 in the form of coal.
Alternatively, fuel 12 may be any other suitable fuel, such as, but not limited to, oil, natural gas, biomass, waste, or any other fossil or renewable fuel. In the exemplary
FUEL
BACKGROUND OF THE INVENTION
This invention relates generally to combustion devices and, more particularly, to a multi-function burner for use with combustion devices.
During a typical combustion process within a furnace or boiler, for example, a flow of combustion gas, or flue gas, is produced. Known combustion gases contain combustion products including, but not limited to, carbon, fly ash, carbon dioxide, carbon monoxide, water, hydrogen, nitrogen, sulfur, chlorine, and/or mercury generated as a result of combusting solid and/or liquid fuels.
At least some known furnaces use air/fuel staged combustion, such as a three-stage combustion, to facilitate reducing the production of at least some of the combustion products, such as nitrogen oxide (NOx). A three-stage combustion process includes combusting fuel and air in a first stage, introducing fuel into the combustion gases in a second stage, and then introducing air into the combustion gases in a third stage. In the second stage, fuel is injected, without combustion air, to form a sub-stoichiometric, or fuel-rich, zone. During the second stage, at least some of the fuels combust to produce hydrocarbon fragments that react with NOx that may have been produced in the first stage. As such, the NOx may be reduced to atmospheric nitrogen in the second stage. In the third stage, air is injected to consume the carbon monoxide and unburnt hydrocarbons exiting the second stage. Although such air/fuel staging may achieve relatively high NOx reduction, the use of injectors that are dedicated to either air injection or fuel/air combustion may limit the operation of the furnace and may limit the flexibility in staging air and/or fuel.
BRIEF DESCRIPTION OF THE INVENTION
In one aspect, a method for operating a fuel-fired furnace including at least one burner is provided. The method includes channeling a first fluid flow to the at least one burner at a first predetermined velocity, and channeling a second fluid flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner. The second predetermined velocity is different than the first predetermined velocity.
In another aspect a burner for use with a fuel-fired furnace is provided. The burner includes a first duct configured to channel a fuel flow into the furnace, and a second duct substantially concentrically-aligned with and extending through the first duct.
The second duct is configured to channel a first fluid flow into the furnace, wherein the first fluid flow is a non-fuel flow.
In a still further aspect a fuel-fired furnace coupled to a fuel source and an air source is provided. The furnace includes a combustion zone defined within the furnace, and a plurality of burners coupled within the combustion zone. At least one of the plurality of burners includes a first duct coupled to the fuel source via a first flow regulation device. The furnace also includes a second duct extending through the first duct, wherein the second duct is coupled to the air source via a second flow regulation device. The first flow regulation device and the second flow regulation device are selectively operable based on an operation of the furnace.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a schematic view of an exemplary power plant system.
Figure 2 is a schematic view of an exemplary burner that may be used with the power plant system shown in Figure 1.
Figure 3 is a schematic view of an alternative burner that may be used with the power plant system shown in Figure 1.
DETAILED DESCRIPTION OF THE INVENTION
Figure 1 is a schematic view of an exemplary power plant system 10. In the exemplary embodiment, system 10 is supplied with fuel 12 in the form of coal.
Alternatively, fuel 12 may be any other suitable fuel, such as, but not limited to, oil, natural gas, biomass, waste, or any other fossil or renewable fuel. In the exemplary
2 embodiment, fuel 12 is supplied to system 10 from a main fuel source 14 to a boiler or a furnace 16. More specifically, in the exemplary embodiment, system 10 includes a fuel-fired furnace 16 that includes a combustion zone 18 and heat exchangers 20.
More specifically, combustion zone 18 includes a primary combustion zone 22, a reburning zone 24, and a burnout zone 26. Alternatively, combustion zone 18 may not include reburning zone 24 and/or burnout zone 26, in which case, furnace 16 is a "straight fire" furnace (not shown). Fuel 12 enters system 10 through fuel sources 14 and 28, as described in more detail below, and air 30 enters system 10 through an air source 32. Alternatively, fuel 12 may enter system 10 from other than fuel sources 14 and 28. The fuel/air mixture is ignited in primary combustion zone 22 to create combustion gas 34.
In the exemplary embodiment, fuel 12 and air 30 are supplied to primary combustion zone 22 through one or more main injectors and/or burners 36. In the exemplary embodiment, burners 36 are low-NOx burners. Main burners 36 receive a predetermined amount of fuel 12 from fuel source 14 and a predetermined quantity of air 30 from air source 32. Burners 36 may be tangentially arranged in each corner of furnace 16, wall-fired, or have any other suitable arrangement that enables furnace 16 to function as described herein. In the exemplary embodiment, burners 36 are oriented within furnace 16 such that a plurality of rows 38 of burners 36 are defined.
Although only one burner 36 is illustrated in each row 38, each row 38 may include a plurality of burners 36.
In the exemplary embodiment, at least one burner 36 is a multi-function burner 100.
Alternatively, combustion zone 18 may include a row 38 and/or array (not shown) of multi-function burners 100. Moreover, although multi-function burner 100 is shown as being in the row 38 that is the most downstream, multi-function burner may be included anywhere within combustion zone 18 that enables system 10 to function as described herein. In the exemplary embodiment, multi-function burner 100 either burns the fuel/air mixture 12 and 30 or injects air 30 into combustion zone 18.
Moreover, in the exemplary embodiment, multi-function burner 100 is coupled in flow communication with main fuel source 14 and air source 32. At least one fuel flow regulation device 40 is coupled between multi-function burner 100 and main fuel
More specifically, combustion zone 18 includes a primary combustion zone 22, a reburning zone 24, and a burnout zone 26. Alternatively, combustion zone 18 may not include reburning zone 24 and/or burnout zone 26, in which case, furnace 16 is a "straight fire" furnace (not shown). Fuel 12 enters system 10 through fuel sources 14 and 28, as described in more detail below, and air 30 enters system 10 through an air source 32. Alternatively, fuel 12 may enter system 10 from other than fuel sources 14 and 28. The fuel/air mixture is ignited in primary combustion zone 22 to create combustion gas 34.
In the exemplary embodiment, fuel 12 and air 30 are supplied to primary combustion zone 22 through one or more main injectors and/or burners 36. In the exemplary embodiment, burners 36 are low-NOx burners. Main burners 36 receive a predetermined amount of fuel 12 from fuel source 14 and a predetermined quantity of air 30 from air source 32. Burners 36 may be tangentially arranged in each corner of furnace 16, wall-fired, or have any other suitable arrangement that enables furnace 16 to function as described herein. In the exemplary embodiment, burners 36 are oriented within furnace 16 such that a plurality of rows 38 of burners 36 are defined.
Although only one burner 36 is illustrated in each row 38, each row 38 may include a plurality of burners 36.
In the exemplary embodiment, at least one burner 36 is a multi-function burner 100.
Alternatively, combustion zone 18 may include a row 38 and/or array (not shown) of multi-function burners 100. Moreover, although multi-function burner 100 is shown as being in the row 38 that is the most downstream, multi-function burner may be included anywhere within combustion zone 18 that enables system 10 to function as described herein. In the exemplary embodiment, multi-function burner 100 either burns the fuel/air mixture 12 and 30 or injects air 30 into combustion zone 18.
Moreover, in the exemplary embodiment, multi-function burner 100 is coupled in flow communication with main fuel source 14 and air source 32. At least one fuel flow regulation device 40 is coupled between multi-function burner 100 and main fuel
3 source 14, and at least one air flow regulation device 42 is coupled between multi-function burner 100 and air source 32. In the exemplary embodiment, an air velocity control device 44 is coupled between multi-function burner 100 and air source 32 to facilitate controlling the velocity of at least a portion of the air 30 discharged through multi-function burner 100. Furthermore, in the exemplary embodiment, air flow regulation device 42 is coupled upstream from velocity control device 44 such that regulation device 42 controls an amount of air 30 entering velocity control device 44.
In the exemplary embodiment, an intermediate air zone 46 is defined proximate multi-function burner 100 within primary combustion zone 22. Alternatively, intermediate air zone 46 may be defined downstream from, and/or upstream from, primary combustion zone 22. In the exemplary embodiment, intermediate air zone 46 is an air staging zone when multi-function burner 100 is used for air injection, and intermediate air zone 46 forms a portion of primary combustion zone 22 when multi-function burner 100 is used similarly to burners 36.
Combustion gases 34 flow from primary combustion zone 22 and/or intermediate air zone 46 towards reburning zone 24. In reburning zone 24, a predetermined amount of reburn fuel 48 is injected through a reburn fuel inlet 50. Reburn fuel 48 is supplied to inlet 50 from a reburn fuel source 28. Although reburn fuel 48 and fuel 12 are shown as originating at a different sources 14 and 28, reburn fuel 48 may be supplied from the same source (not shown) as fuel 12. In one embodiment reburn fuel 48 is a different type of fuel than fuel 12. For example, fuel 12 entering from main fuel source 14 may be, but is not limited to being, pulverized coal, and reburn fuel 48 entering from reburn fuel source 28 may be natural gas. Alternatively, any suitable combination of fuel 12 and/or 48 that enables system 10 to function as described herein may be injected into furnace 16. In the exemplary embodiment, the amount of reburn fuel 48 injected is based on achieving a desired stoichiometric ratio within reburning zone 24. More specifically, in the exemplary embodiment, an amount of reburn fuel 48 is injected to create a fuel-rich environment in reburning zone 24.
Combustion gases 34 flow from reburning zone 24 into burnout zone 26. In the exemplary embodiment, overfire air 52 is injected into burnout zone 26 through an
In the exemplary embodiment, an intermediate air zone 46 is defined proximate multi-function burner 100 within primary combustion zone 22. Alternatively, intermediate air zone 46 may be defined downstream from, and/or upstream from, primary combustion zone 22. In the exemplary embodiment, intermediate air zone 46 is an air staging zone when multi-function burner 100 is used for air injection, and intermediate air zone 46 forms a portion of primary combustion zone 22 when multi-function burner 100 is used similarly to burners 36.
Combustion gases 34 flow from primary combustion zone 22 and/or intermediate air zone 46 towards reburning zone 24. In reburning zone 24, a predetermined amount of reburn fuel 48 is injected through a reburn fuel inlet 50. Reburn fuel 48 is supplied to inlet 50 from a reburn fuel source 28. Although reburn fuel 48 and fuel 12 are shown as originating at a different sources 14 and 28, reburn fuel 48 may be supplied from the same source (not shown) as fuel 12. In one embodiment reburn fuel 48 is a different type of fuel than fuel 12. For example, fuel 12 entering from main fuel source 14 may be, but is not limited to being, pulverized coal, and reburn fuel 48 entering from reburn fuel source 28 may be natural gas. Alternatively, any suitable combination of fuel 12 and/or 48 that enables system 10 to function as described herein may be injected into furnace 16. In the exemplary embodiment, the amount of reburn fuel 48 injected is based on achieving a desired stoichiometric ratio within reburning zone 24. More specifically, in the exemplary embodiment, an amount of reburn fuel 48 is injected to create a fuel-rich environment in reburning zone 24.
Combustion gases 34 flow from reburning zone 24 into burnout zone 26. In the exemplary embodiment, overfire air 52 is injected into burnout zone 26 through an
4 overtire air inlet 54, and a predetermined quantity of overfire air 52 is injected into burnout zone 26. In the exemplary embodiment, overfire air inlet 54 is in flow communication with air source 32 via an overfire air regulation device 56.
Alternatively, overtire air 52 may be supplied to system 10 through a source (not shown) that is separate from air source 32. The quantity of overfire air 52 supplied is selected based on achieving a desired stoichiometric ratio within burnout zone 26.
More specifically, in the exemplary embodiment, the quantity of overfire air supplied is selected to facilitate completing combustion of fuel 12 and reburn fuel 48, which facilitates reducing pollutants in combustion gas 34, such as, but not limited to, nitrogen oxides, NON, and/or carbon monoxide, CO.
In the exemplary embodiment, flue gases 58 exit combustion zone 18 and enter heat exchangers 20. Heat exchangers 20 transfer heat from flue gas 58 to a fluid (not shown) in a known manner. More specifically, the heat transfer heats the fluid, such as, for example, heating water to generate steam. The heated fluid, for example, the steam, is used to generate power, typically by known power generation methods and systems (not shown), such as, for example, a steam turbine (not shown).
Alternatively, heat exchangers 20 transfer heat from flue gas 58 to a fuel cell (not shown) used to generate power. Power may be supplied to a power grid (not shown) or any other suitable power outlet.
In the exemplary embodiment, system 10 includes a control system 60 that is operatively coupled at least to a main air regulation device 62, main fuel source 14, reburn fuel source 28, overfire air regulation device 56, air velocity control device 44, air flow regulation device 42, and fuel flow regulation device 40. Control system 60 facilitates controlling sources 14 and 28 and devices 40, 42, 44, 56, and 62 to adjust the stoichiometric ratios within combustion zone 18 by activating and/or deactivating air and fuel flows from sources 14 and 28 and/or through devices 40, 42, 44, 56, and 62. More specifically, main air regulation device 62 is used to regulate the air 30 entering burners 36, multi-function burner 100, and/or overfire air inlet 54, main fuel source 14 is used to enable fuel 12 to enter system 10, reburn fuel source 28 is used to enable reburn fuel 48 to enter system 10, overfire air regulation device 56 regulates the amount of overtire air 52 entering system 10 from air source 32 through overfire inlet 54, air flow regulation device 42 and air velocity control device 44 each regulate the amount and/or velocity of air 30 entering system 10 through multi-function burner 100, and fuel flow regulation device 40 is used to enable fuel 12 to enter system 10 through multi-function burner 100.
During operation of system 10, fuel 12, air 30, reburn fuel 48, and/or overfire air 52 are injected and combusted in combustion zone 18 to form flue gases 58 that flow from combustion zone 18 through heat exchangers 20. More specifically, in the exemplary embodiment, control system 60 controls air and fuel entering combustion zone 18 to form flue gases 58. Furthermore, in the exemplary embodiment, control system 60 causes multi-function burner 100 either to inject air 30 into combustion zone 18, or to burn fuel 12 and air 30 in primary combustion zone 22. More specifically, in the exemplary embodiment, when multi-function burner 100 is used to burn fuel 12 and air 30, control system 60 causes fuel flow regulation device 40 to inject fuel 12 into combustion zone 18 through multi-function burner 100, causes main air regulation device 62 to inject air 30 into combustion zone 18 through multi-function burner 100, and causes air flow regulation device 42 to prevent air 30 from being injected into combustion zone 18 through multi-function burner 100. As such, fuel 12 and air 30 are entering combustion zone 18 through multi-function burner 100 from fuel flow regulation device 40 and main air regulation device 62, respectively, to facilitate the combustion of fuel 12 in air 30.
Furthermore, in the exemplary embodiment, when multi-function burner 100 is used to inject air 30, control system 60 controls fuel flow regulation device 40 to prevent fuel 12 from entering combustion zone 18 through multi-function burner 100, controls main air regulation device 62 to inject air 30 into combustion zone 18 through multi-function burner 100 at a first velocity VI, and controls air flow regulation device 42 and air velocity control device 44 to inject air 30 into combustion zone 18 through multi-function burner 100 at a second velocity V2. In the exemplary embodiment, velocity V2 is higher than velocity VI. As such, air 30 enters combustion zone through multi-function burner 100 from air flow regulation device 42 and main air regulation device 62 such that a first portion 202 (shown in Figures 2 and 3) of air 30 is at velocity V1 and a second portion 204 (shown in Figures 2 and 3) of air 30 is at velocity V2. In another embodiment, air 30 entering through air flow regulation device 42 is not accelerated through air velocity control device 44, such that air 30 entering combustion zone 18 through multi-function burner 100 is supplied from air flow regulation device 42 and main air regulation device 62 at substantially the same velocity.
Control system 60 further controls the stoichiometric ratio within combustion zone 18. For example, when multi-function burner 100 is used to inject air 30, main fuel source 14 and/or main air regulation device 62 are controlled such that a first stoichiometric ratio SRIA within primary combustion zone 22 is fuel rich, air velocity control device 44 and air flow regulation device 42 are controlled such that a second stoichiometric ratio SR2A within intermediate air zone 46 is less fuel rich than stoichiometric ratio SIZIA, reburn fuel source 28 is controlled such that a third stoichiometric ratio SR3A within reburning zone 24 is more fuel rich than stoichiometric ratio SR2A, and overfire air regulation device 56 is controlled such that a forth stoichiometric ratio Situ, within burnout zone 26 is approximately an ideal stoichiometric ratio. Alternatively, stoichiometric ratios SR1A, SR2A, SR3A, and/or SR4A may have any values and/or relative values that enable system 10 to function as described herein.
In another example, when multi-function burner 100 is used to combust fuel 12 and air 30, and when multi-function burner 100 is considered to be within the primary combustion zone 22 such that intermediate air zone 46 is not implemented, main fuel source 14, fuel flow regulation device 40, and main air regulation device 62 are controlled to ensure that a first stoichiometric ratio SR13 within primary combustion zone 22 is fuel lean, reburn fuel source 28 is controlled to ensure that a third stoichiometric ratio SR38 within reburning zone 24 is fuel rich, and overfire air regulation device 56 is controlled to ensure that a forth stoichiometric ratio within burnout zone 26 is approximately an ideal stoichiometric ratio.
Alternatively, stoichiometric ratios SRIB, SR3B, and/or SR48 may have any values and/or relative values that enable system 10 to function as described herein.
In the exemplary embodiment, flue gases 58 exiting combustion zone 18 enter heat exchangers 20 to transfer heat to fluid for use in generating power. Within primary combustion zone 22, fuel products not entrained in combustion gas 34 may be solids (not shown) and may be discharged from furnace 16 as waste (not shown).
Figure 2 is a schematic view of an exemplary multi-function burner 200 that may be used as burner 100 within system 10 (shown in Figure 1). In the exemplary embodiment, burner 200 has a substantially circular cross-sectional shape (not shown). Alternatively, burner 200 may have any suitable cross-sectional shape that enables burner 200 to function as described herein.
In the exemplary embodiment, multi-function burner 200 includes a first duct 206, a second duct 208, a third duct 210, and a fourth duct 212 that are each substantially concentrically aligned with a centerline 214 of the burner 200. More specifically, first duct 206 is the radially outermost of the ducts 206, 208, 210, and 212 such that a radially outer surface 216 of first duct 206 defines the outer surface of burner 200.
Furthermore, in the exemplary embodiment, first duct 206 includes a convergent and substantially conical section 218, a substantially cylindrical section 220, and a divergent and substantially conical section 222. Second duct 208, in the exemplary embodiment, is spaced radially inward from first duct 206 such that a first passageway 224 is defined between first and second ducts 206 and 208.
Moreover, second duct 208 includes a substantially cylindrical section 226 and a divergent and substantially conical section 228.
In the exemplary embodiment, third duct 210 is spaced radially inward from second duct 208 such that a second passageway 230 is defined between second and third ducts 208 and 210. Furthermore, in the exemplary embodiment, third duct 210 is substantially cylindrical and includes an annular flame regulation device 232, such as a flame holder, that creates a recirculation zone 234. Fourth duct 212, in the exemplary embodiment, defines a center passageway 236 that has a diameter DI
and that is radially spaced inward from third duct 210 such that a third passageway 238 is defined between third and fourth ducts 210 and 212. In the exemplary embodiment, fourth duct 212 is substantially cylindrical including having conical and/or cylindrical shapes, ducts 206, 208, 210, and 212 may each have any suitable configuration or shape that enables burner 200 to function as described herein.
First and second ducts 206 and 208, in the exemplary embodiment, are each coupled in flow communication with a common plenum 240, which is coupled in flow communication with air source 32 via main air regulation device 62.
Alternatively, first and second ducts 206 and 208 are each coupled separately in flow communication independently with air source 32 such that first and second ducts 206 and 208 do not share a common plenum 240. In the exemplary embodiment, first and second ducts 206 and 208 are oriented such that air 30 may be injected into common plenum 240, through first passageway 224 and/or second passageway 230, and into primary combustion zone 22 (shown in Figure 1) and/or intermediate air zone 46 (shown in Figure 1). In one embodiment, first passageway 224 and/or second passageway 230 may induce a swirl flow pattern (not shown) to air 30 injected through first passageway 224 and/or second passageway 230.
Furthermore, third duct 210, in the exemplary embodiment, is coupled in flow communication with fuel source 14 via fuel flow regulation device 40. In the exemplary embodiment, third duct 210 is oriented such that fuel 12 may be injected through third passageway 238 and into primary combustion zone 22, when burner is used to combust fuel 12 and air 30. Moreover, fourth duct 212, in the exemplary embodiment, is coupled in flow communication with air source 32 via air flow regulation device 42 and air velocity control device 44. In the exemplary embodiment, fourth duct 212 is oriented such that air 30 may be injected through center passageway 236 and into intermediate air zone 46 at a predetermined velocity, when burner 200 is used to inject air 30.
During a first operation of multi-function burner 200, burner 200 is used to burn fuel 12 and air 30. Control system 60 controls fuel flow regulation device 40 to enable fuel 12 to enter combustion zone 18 through third passageway 238, controls main air regulation device 62 to inject air 30 into combustion zone 18 through first passageway 224 and/or second passageway 230, and controls air flow regulation device 42 to prevent air 30 from being injected into combustion zone 18 through center passageway 236.
During a second operation of multi-function burner 200, burner 200 is used to inject air 30. Control system 60 controls fuel flow regulation device 40 to prevent fuel 12 from entering combustion zone 18 through third passageway 238, controls main air flow regulation device to inject air 30 into combustion zone 18 through first passageway 224 and/or second passageway 230 at first velocity VI, and controls air flow regulation device 42 and air velocity control device 44 to inject air 30 into combustion zone 18 through center passageway 236 at second velocity V2, which is higher than velocity VI. As such, the first portion 202 of air 30 is injected at velocity VI and the second portion 204 of air 30 is injected at velocity V2. In another embodiment, air 30 entering through center passageway 236 does not experience a velocity change through air velocity control device 44, and air 30 entering combustion zone 18 through center, first, and/or second passageways 236, 224, and/or 230, respectively, enters from air flow regulation device 42 and main air regulation device 62 at substantially the same velocity.
Figure 3 is a schematic view of an alternative exemplary multi-function burner that may be used as burner 100 within system 10. Burner 300 is substantially similar to burner 200, as described above, with the exception that burner 300 includes a fifth duct 302 that is substantially concentrically aligned with and is spaced radially inward from fourth duct 212. More specifically, in the exemplary embodiment, fifth duct 302 is substantially cylindrical and defines a center passageway 304 having a diameter D2 that is smaller than diameter Di (shown in Figure 2). Alternatively, diameter D2 may be substantially equal to, or larger than, diameter DI. Fifth duct 302 is spaced radially inward from fourth duct 212 such that a fourth passageway 306 is defined between fourth and fifth ducts 212 and 302. In the exemplary embodiment, fifth duct 302 is coupled in flow communication with air source 32 via air flow regulation device 42 and air velocity control device 44. As such, fifth duct 302 is oriented such that air 30 may be injected through center passageway 304 into intermediate air zone 46 (shown in Figure 1) at a predetermined velocity, when burner 300 is used to inject air 30.
During the first or second operation of burner 300, control system 60 controls air flow regulation device 42 and air velocity control device 44 to either prevent, or to enable air 30 to be injected into combustion zone 18 through center passageway 304 at second velocity V2, as described above. Accordingly, only an insignificant amount of air 30 is injected through fourth passageway 306, during either operation of multi-function burner 300.
The above-described methods and apparatuses facilitate increasing the effectiveness and flexibility of staging air and/or fuel within a furnace, as compared to furnaces that do not include multi-function burners. More specifically, the multi-function burners described herein facilitate providing low-NOx burner performance and/or providing optimal air injection that increases the effective air/gas mixing upstream of the reburn zone as compared to furnaces that do not include multi-function burners. As such, the above-described burners facilitate increasing the operational flexibility of the furnace and optimizing intermediate stage air/gas mixing in a multi-stage reburn application.
Furthermore, the above-described burners facilitate reducing burnout residence time requirements, while improving gas emissions control, as compared to a single-function burner operating in a cooling mode. For example, NOx control is facilitated to be improved, as compared to a single-function burner operating in a cooling mode, by enabling both near and far field air/gas mixing when the above-described burner is operating in an air-injection mode. More specifically, the higher velocity air injected through the multi-function burner penetrates the far-field within the furnace to facilitate substantially homogenous mixing among air, fuel, and combustion gases before the mixture of gases enters subsequence staging zones. By more efficiently reducing the variance in the gas stoichiometric ratio flowing into the reburn zone, the above-described burner facilitates reducing burnout residence time requirements and reducing NOx, carbon-in-ash, and CO, as compared to furnaces that do not include multi-function burners.
Moreover, by utilizing the above-described fifth duct, the diameter of a center passageway of a burner may be reduced to facilitate reducing the amount of air required to achieve a suitably high air velocity for far-field penetration, as compared to burners having a larger center passageway diameter. As such, retrofitting a furnace with the above-described multi-function burners is facilitated to be simplified.
Furthermore, the above-described burner includes a passageway for swirled or non-swirled lower velocity air, which facilitates cooling the burner and penetrating the near-field of the furnace.
Exemplary embodiments of a method and apparatus for combusting fuel and air within a combustion device are described above in detail. The method and apparatus _ are not limited to the specific embodiments described herein, but rather, components of the method and apparatus may be utilized independently and separately from other components described herein. For example, the multi-function burner may also be used in combination with other emission control systems and methods, and is not limited to practice with only the fuel-fired power plant as described herein.
Rather, the present invention can be implemented and utilized in connection with many other staged fuel and air combustion applications.
While there have been described herein what are considered to be preferred and exemplary embodiments of the present invention, other modifications of these embodiments falling within the scope of the invention described herein shall be apparent to those skilled in the art.
Alternatively, overtire air 52 may be supplied to system 10 through a source (not shown) that is separate from air source 32. The quantity of overfire air 52 supplied is selected based on achieving a desired stoichiometric ratio within burnout zone 26.
More specifically, in the exemplary embodiment, the quantity of overfire air supplied is selected to facilitate completing combustion of fuel 12 and reburn fuel 48, which facilitates reducing pollutants in combustion gas 34, such as, but not limited to, nitrogen oxides, NON, and/or carbon monoxide, CO.
In the exemplary embodiment, flue gases 58 exit combustion zone 18 and enter heat exchangers 20. Heat exchangers 20 transfer heat from flue gas 58 to a fluid (not shown) in a known manner. More specifically, the heat transfer heats the fluid, such as, for example, heating water to generate steam. The heated fluid, for example, the steam, is used to generate power, typically by known power generation methods and systems (not shown), such as, for example, a steam turbine (not shown).
Alternatively, heat exchangers 20 transfer heat from flue gas 58 to a fuel cell (not shown) used to generate power. Power may be supplied to a power grid (not shown) or any other suitable power outlet.
In the exemplary embodiment, system 10 includes a control system 60 that is operatively coupled at least to a main air regulation device 62, main fuel source 14, reburn fuel source 28, overfire air regulation device 56, air velocity control device 44, air flow regulation device 42, and fuel flow regulation device 40. Control system 60 facilitates controlling sources 14 and 28 and devices 40, 42, 44, 56, and 62 to adjust the stoichiometric ratios within combustion zone 18 by activating and/or deactivating air and fuel flows from sources 14 and 28 and/or through devices 40, 42, 44, 56, and 62. More specifically, main air regulation device 62 is used to regulate the air 30 entering burners 36, multi-function burner 100, and/or overfire air inlet 54, main fuel source 14 is used to enable fuel 12 to enter system 10, reburn fuel source 28 is used to enable reburn fuel 48 to enter system 10, overfire air regulation device 56 regulates the amount of overtire air 52 entering system 10 from air source 32 through overfire inlet 54, air flow regulation device 42 and air velocity control device 44 each regulate the amount and/or velocity of air 30 entering system 10 through multi-function burner 100, and fuel flow regulation device 40 is used to enable fuel 12 to enter system 10 through multi-function burner 100.
During operation of system 10, fuel 12, air 30, reburn fuel 48, and/or overfire air 52 are injected and combusted in combustion zone 18 to form flue gases 58 that flow from combustion zone 18 through heat exchangers 20. More specifically, in the exemplary embodiment, control system 60 controls air and fuel entering combustion zone 18 to form flue gases 58. Furthermore, in the exemplary embodiment, control system 60 causes multi-function burner 100 either to inject air 30 into combustion zone 18, or to burn fuel 12 and air 30 in primary combustion zone 22. More specifically, in the exemplary embodiment, when multi-function burner 100 is used to burn fuel 12 and air 30, control system 60 causes fuel flow regulation device 40 to inject fuel 12 into combustion zone 18 through multi-function burner 100, causes main air regulation device 62 to inject air 30 into combustion zone 18 through multi-function burner 100, and causes air flow regulation device 42 to prevent air 30 from being injected into combustion zone 18 through multi-function burner 100. As such, fuel 12 and air 30 are entering combustion zone 18 through multi-function burner 100 from fuel flow regulation device 40 and main air regulation device 62, respectively, to facilitate the combustion of fuel 12 in air 30.
Furthermore, in the exemplary embodiment, when multi-function burner 100 is used to inject air 30, control system 60 controls fuel flow regulation device 40 to prevent fuel 12 from entering combustion zone 18 through multi-function burner 100, controls main air regulation device 62 to inject air 30 into combustion zone 18 through multi-function burner 100 at a first velocity VI, and controls air flow regulation device 42 and air velocity control device 44 to inject air 30 into combustion zone 18 through multi-function burner 100 at a second velocity V2. In the exemplary embodiment, velocity V2 is higher than velocity VI. As such, air 30 enters combustion zone through multi-function burner 100 from air flow regulation device 42 and main air regulation device 62 such that a first portion 202 (shown in Figures 2 and 3) of air 30 is at velocity V1 and a second portion 204 (shown in Figures 2 and 3) of air 30 is at velocity V2. In another embodiment, air 30 entering through air flow regulation device 42 is not accelerated through air velocity control device 44, such that air 30 entering combustion zone 18 through multi-function burner 100 is supplied from air flow regulation device 42 and main air regulation device 62 at substantially the same velocity.
Control system 60 further controls the stoichiometric ratio within combustion zone 18. For example, when multi-function burner 100 is used to inject air 30, main fuel source 14 and/or main air regulation device 62 are controlled such that a first stoichiometric ratio SRIA within primary combustion zone 22 is fuel rich, air velocity control device 44 and air flow regulation device 42 are controlled such that a second stoichiometric ratio SR2A within intermediate air zone 46 is less fuel rich than stoichiometric ratio SIZIA, reburn fuel source 28 is controlled such that a third stoichiometric ratio SR3A within reburning zone 24 is more fuel rich than stoichiometric ratio SR2A, and overfire air regulation device 56 is controlled such that a forth stoichiometric ratio Situ, within burnout zone 26 is approximately an ideal stoichiometric ratio. Alternatively, stoichiometric ratios SR1A, SR2A, SR3A, and/or SR4A may have any values and/or relative values that enable system 10 to function as described herein.
In another example, when multi-function burner 100 is used to combust fuel 12 and air 30, and when multi-function burner 100 is considered to be within the primary combustion zone 22 such that intermediate air zone 46 is not implemented, main fuel source 14, fuel flow regulation device 40, and main air regulation device 62 are controlled to ensure that a first stoichiometric ratio SR13 within primary combustion zone 22 is fuel lean, reburn fuel source 28 is controlled to ensure that a third stoichiometric ratio SR38 within reburning zone 24 is fuel rich, and overfire air regulation device 56 is controlled to ensure that a forth stoichiometric ratio within burnout zone 26 is approximately an ideal stoichiometric ratio.
Alternatively, stoichiometric ratios SRIB, SR3B, and/or SR48 may have any values and/or relative values that enable system 10 to function as described herein.
In the exemplary embodiment, flue gases 58 exiting combustion zone 18 enter heat exchangers 20 to transfer heat to fluid for use in generating power. Within primary combustion zone 22, fuel products not entrained in combustion gas 34 may be solids (not shown) and may be discharged from furnace 16 as waste (not shown).
Figure 2 is a schematic view of an exemplary multi-function burner 200 that may be used as burner 100 within system 10 (shown in Figure 1). In the exemplary embodiment, burner 200 has a substantially circular cross-sectional shape (not shown). Alternatively, burner 200 may have any suitable cross-sectional shape that enables burner 200 to function as described herein.
In the exemplary embodiment, multi-function burner 200 includes a first duct 206, a second duct 208, a third duct 210, and a fourth duct 212 that are each substantially concentrically aligned with a centerline 214 of the burner 200. More specifically, first duct 206 is the radially outermost of the ducts 206, 208, 210, and 212 such that a radially outer surface 216 of first duct 206 defines the outer surface of burner 200.
Furthermore, in the exemplary embodiment, first duct 206 includes a convergent and substantially conical section 218, a substantially cylindrical section 220, and a divergent and substantially conical section 222. Second duct 208, in the exemplary embodiment, is spaced radially inward from first duct 206 such that a first passageway 224 is defined between first and second ducts 206 and 208.
Moreover, second duct 208 includes a substantially cylindrical section 226 and a divergent and substantially conical section 228.
In the exemplary embodiment, third duct 210 is spaced radially inward from second duct 208 such that a second passageway 230 is defined between second and third ducts 208 and 210. Furthermore, in the exemplary embodiment, third duct 210 is substantially cylindrical and includes an annular flame regulation device 232, such as a flame holder, that creates a recirculation zone 234. Fourth duct 212, in the exemplary embodiment, defines a center passageway 236 that has a diameter DI
and that is radially spaced inward from third duct 210 such that a third passageway 238 is defined between third and fourth ducts 210 and 212. In the exemplary embodiment, fourth duct 212 is substantially cylindrical including having conical and/or cylindrical shapes, ducts 206, 208, 210, and 212 may each have any suitable configuration or shape that enables burner 200 to function as described herein.
First and second ducts 206 and 208, in the exemplary embodiment, are each coupled in flow communication with a common plenum 240, which is coupled in flow communication with air source 32 via main air regulation device 62.
Alternatively, first and second ducts 206 and 208 are each coupled separately in flow communication independently with air source 32 such that first and second ducts 206 and 208 do not share a common plenum 240. In the exemplary embodiment, first and second ducts 206 and 208 are oriented such that air 30 may be injected into common plenum 240, through first passageway 224 and/or second passageway 230, and into primary combustion zone 22 (shown in Figure 1) and/or intermediate air zone 46 (shown in Figure 1). In one embodiment, first passageway 224 and/or second passageway 230 may induce a swirl flow pattern (not shown) to air 30 injected through first passageway 224 and/or second passageway 230.
Furthermore, third duct 210, in the exemplary embodiment, is coupled in flow communication with fuel source 14 via fuel flow regulation device 40. In the exemplary embodiment, third duct 210 is oriented such that fuel 12 may be injected through third passageway 238 and into primary combustion zone 22, when burner is used to combust fuel 12 and air 30. Moreover, fourth duct 212, in the exemplary embodiment, is coupled in flow communication with air source 32 via air flow regulation device 42 and air velocity control device 44. In the exemplary embodiment, fourth duct 212 is oriented such that air 30 may be injected through center passageway 236 and into intermediate air zone 46 at a predetermined velocity, when burner 200 is used to inject air 30.
During a first operation of multi-function burner 200, burner 200 is used to burn fuel 12 and air 30. Control system 60 controls fuel flow regulation device 40 to enable fuel 12 to enter combustion zone 18 through third passageway 238, controls main air regulation device 62 to inject air 30 into combustion zone 18 through first passageway 224 and/or second passageway 230, and controls air flow regulation device 42 to prevent air 30 from being injected into combustion zone 18 through center passageway 236.
During a second operation of multi-function burner 200, burner 200 is used to inject air 30. Control system 60 controls fuel flow regulation device 40 to prevent fuel 12 from entering combustion zone 18 through third passageway 238, controls main air flow regulation device to inject air 30 into combustion zone 18 through first passageway 224 and/or second passageway 230 at first velocity VI, and controls air flow regulation device 42 and air velocity control device 44 to inject air 30 into combustion zone 18 through center passageway 236 at second velocity V2, which is higher than velocity VI. As such, the first portion 202 of air 30 is injected at velocity VI and the second portion 204 of air 30 is injected at velocity V2. In another embodiment, air 30 entering through center passageway 236 does not experience a velocity change through air velocity control device 44, and air 30 entering combustion zone 18 through center, first, and/or second passageways 236, 224, and/or 230, respectively, enters from air flow regulation device 42 and main air regulation device 62 at substantially the same velocity.
Figure 3 is a schematic view of an alternative exemplary multi-function burner that may be used as burner 100 within system 10. Burner 300 is substantially similar to burner 200, as described above, with the exception that burner 300 includes a fifth duct 302 that is substantially concentrically aligned with and is spaced radially inward from fourth duct 212. More specifically, in the exemplary embodiment, fifth duct 302 is substantially cylindrical and defines a center passageway 304 having a diameter D2 that is smaller than diameter Di (shown in Figure 2). Alternatively, diameter D2 may be substantially equal to, or larger than, diameter DI. Fifth duct 302 is spaced radially inward from fourth duct 212 such that a fourth passageway 306 is defined between fourth and fifth ducts 212 and 302. In the exemplary embodiment, fifth duct 302 is coupled in flow communication with air source 32 via air flow regulation device 42 and air velocity control device 44. As such, fifth duct 302 is oriented such that air 30 may be injected through center passageway 304 into intermediate air zone 46 (shown in Figure 1) at a predetermined velocity, when burner 300 is used to inject air 30.
During the first or second operation of burner 300, control system 60 controls air flow regulation device 42 and air velocity control device 44 to either prevent, or to enable air 30 to be injected into combustion zone 18 through center passageway 304 at second velocity V2, as described above. Accordingly, only an insignificant amount of air 30 is injected through fourth passageway 306, during either operation of multi-function burner 300.
The above-described methods and apparatuses facilitate increasing the effectiveness and flexibility of staging air and/or fuel within a furnace, as compared to furnaces that do not include multi-function burners. More specifically, the multi-function burners described herein facilitate providing low-NOx burner performance and/or providing optimal air injection that increases the effective air/gas mixing upstream of the reburn zone as compared to furnaces that do not include multi-function burners. As such, the above-described burners facilitate increasing the operational flexibility of the furnace and optimizing intermediate stage air/gas mixing in a multi-stage reburn application.
Furthermore, the above-described burners facilitate reducing burnout residence time requirements, while improving gas emissions control, as compared to a single-function burner operating in a cooling mode. For example, NOx control is facilitated to be improved, as compared to a single-function burner operating in a cooling mode, by enabling both near and far field air/gas mixing when the above-described burner is operating in an air-injection mode. More specifically, the higher velocity air injected through the multi-function burner penetrates the far-field within the furnace to facilitate substantially homogenous mixing among air, fuel, and combustion gases before the mixture of gases enters subsequence staging zones. By more efficiently reducing the variance in the gas stoichiometric ratio flowing into the reburn zone, the above-described burner facilitates reducing burnout residence time requirements and reducing NOx, carbon-in-ash, and CO, as compared to furnaces that do not include multi-function burners.
Moreover, by utilizing the above-described fifth duct, the diameter of a center passageway of a burner may be reduced to facilitate reducing the amount of air required to achieve a suitably high air velocity for far-field penetration, as compared to burners having a larger center passageway diameter. As such, retrofitting a furnace with the above-described multi-function burners is facilitated to be simplified.
Furthermore, the above-described burner includes a passageway for swirled or non-swirled lower velocity air, which facilitates cooling the burner and penetrating the near-field of the furnace.
Exemplary embodiments of a method and apparatus for combusting fuel and air within a combustion device are described above in detail. The method and apparatus _ are not limited to the specific embodiments described herein, but rather, components of the method and apparatus may be utilized independently and separately from other components described herein. For example, the multi-function burner may also be used in combination with other emission control systems and methods, and is not limited to practice with only the fuel-fired power plant as described herein.
Rather, the present invention can be implemented and utilized in connection with many other staged fuel and air combustion applications.
While there have been described herein what are considered to be preferred and exemplary embodiments of the present invention, other modifications of these embodiments falling within the scope of the invention described herein shall be apparent to those skilled in the art.
Claims (16)
1. A method for operating a fuel-fired furnace including at least one burner, said method comprising:
mixing a far field and a near field substantially homogeneously by:
channeling a first air flow to the at least one burner at a first predetermined velocity;
channeling a second air flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner, wherein the second predetermined velocity is different than the first predetermined velocity, and wherein during the first mode of operation, fuel is substantially prevented from being channeled through the at least one burner; and creating a recirculation zone by channeling a fuel flow through a flame regulation device to the at least one burner during a second mode of operation, wherein during the second mode of operation, the second air flow is substantially prevented from being channeled through the at least one burner.
mixing a far field and a near field substantially homogeneously by:
channeling a first air flow to the at least one burner at a first predetermined velocity;
channeling a second air flow to the at least one burner at a second predetermined velocity during a first mode of operation of the at least one burner, wherein the second predetermined velocity is different than the first predetermined velocity, and wherein during the first mode of operation, fuel is substantially prevented from being channeled through the at least one burner; and creating a recirculation zone by channeling a fuel flow through a flame regulation device to the at least one burner during a second mode of operation, wherein during the second mode of operation, the second air flow is substantially prevented from being channeled through the at least one burner.
2. A method in accordance with claim 1 wherein:
channeling a second air flow to the at least one burner further comprises channeling the second air flow through a first duct; and channeling a fuel flow to the at least one burner further comprises channeling the fuel flow through a second duct that is substantially concentrically-aligned with and radially outward from the first duct.
channeling a second air flow to the at least one burner further comprises channeling the second air flow through a first duct; and channeling a fuel flow to the at least one burner further comprises channeling the fuel flow through a second duct that is substantially concentrically-aligned with and radially outward from the first duct.
3. A method in accordance with claim 1 wherein:
channeling a first air flow to the at least one burner further comprises channeling the first air flow through a first passageway defined through the at least one burner; and channeling a second air flow to the at least one burner further comprises channeling the second air flow through a second passageway defined through the at least one burner.
channeling a first air flow to the at least one burner further comprises channeling the first air flow through a first passageway defined through the at least one burner; and channeling a second air flow to the at least one burner further comprises channeling the second air flow through a second passageway defined through the at least one burner.
4. A method in accordance with claim 3 wherein channeling the first air flow through a first passageway and channeling the second air flow through a second passageway further comprises channeling the first and second air flows through substantially concentrically-aligned first and second passageways.
5. A method in accordance with claim 1 wherein channeling a first air flow to the at least one burner further comprises channeling the first air flow to a burner at a downstream end of a combustion zone within the fuel-fired furnace.
6. A burner for use with a fuel-fired furnace, said burner comprising:
a first duct configured to channel a fuel flow into the furnace, said first duct comprises a flame regulation device coupled to a downstream end of said first duct;
a second duct substantially concentrically-aligned with and extending through said first duct, said second duct configured to channel a first air flow into the furnace, at a first predetermined velocity when the fuel flow is substantially prevented from flowing into the furnace through said first duct; and at least one third duct substantially concentrically-aligned with said first duct, said at least one third duct radially outward from said first duct and configured to channel a second air flow into the furnace at a second predetermined velocity that is different than the first predetermined velocity, wherein the first and second air flows facilitate substantially homogeneous mixing of a far field and a near field.
a first duct configured to channel a fuel flow into the furnace, said first duct comprises a flame regulation device coupled to a downstream end of said first duct;
a second duct substantially concentrically-aligned with and extending through said first duct, said second duct configured to channel a first air flow into the furnace, at a first predetermined velocity when the fuel flow is substantially prevented from flowing into the furnace through said first duct; and at least one third duct substantially concentrically-aligned with said first duct, said at least one third duct radially outward from said first duct and configured to channel a second air flow into the furnace at a second predetermined velocity that is different than the first predetermined velocity, wherein the first and second air flows facilitate substantially homogeneous mixing of a far field and a near field.
7. A burner in accordance with claim 6 wherein the fuel flow is a flow of air including fuel particulates entrained therein.
8. A burner in accordance with claim 6 wherein the second predetermined velocity is slower than the first predetermined velocity.
9. A burner in accordance with claim 6 further comprising an annular wall extending circumferentially between said first duct and said third duct.
10. A burner in accordance with claim 6 further comprising a fourth duct coupled between said second duct and said first duct.
11. A fuel-fired furnace coupled to a fuel source and an air source, said furnace comprising:
a combustion zone defined within said furnace;
a first flow regulation device coupled to the fuel source and selectively operable based on an operation of said furnace;
a second flow regulation device coupled to the air source and selectively operable based on an operation of said furnace; and a plurality of burners coupled within said combustion zone, at least one of said plurality of burners comprising:
a first duct coupled to the fuel source via said first flow regulation device, said first duct comprises a flame regulation device coupled to a downstream end of said first duct, said first duct configured to channel a fuel flow into said furnace;
a second duct extending through said first duct, said second duct coupled to the air source via said second flow regulation device and configured to channel a first air flow into said furnace at a first predetermined velocity when the fuel flow is substantially prevented from being channeled through said first duct by said first flow regulation device;
a third flow regulation device coupled to the air source and selectively operable based on an operation of said furnace; and at least one third duct substantially concentrically-aligned with and radially outward from said first duct, said at least one third duct coupled to the air source via said third flow regulation device and configured to channel a second air flow into said furnace at a second predetermined velocity that is different than the first predetermined velocity, wherein the first and second air flows facilitate substantially homogeneous mixing of a far field and a near field.
a combustion zone defined within said furnace;
a first flow regulation device coupled to the fuel source and selectively operable based on an operation of said furnace;
a second flow regulation device coupled to the air source and selectively operable based on an operation of said furnace; and a plurality of burners coupled within said combustion zone, at least one of said plurality of burners comprising:
a first duct coupled to the fuel source via said first flow regulation device, said first duct comprises a flame regulation device coupled to a downstream end of said first duct, said first duct configured to channel a fuel flow into said furnace;
a second duct extending through said first duct, said second duct coupled to the air source via said second flow regulation device and configured to channel a first air flow into said furnace at a first predetermined velocity when the fuel flow is substantially prevented from being channeled through said first duct by said first flow regulation device;
a third flow regulation device coupled to the air source and selectively operable based on an operation of said furnace; and at least one third duct substantially concentrically-aligned with and radially outward from said first duct, said at least one third duct coupled to the air source via said third flow regulation device and configured to channel a second air flow into said furnace at a second predetermined velocity that is different than the first predetermined velocity, wherein the first and second air flows facilitate substantially homogeneous mixing of a far field and a near field.
12. A fuel-fired furnace in accordance with claim 11 further comprises a fuel injector coupled downstream from said combustion zone.
13. A fuel-fired furnace in accordance with claim 11 further comprising an air injector coupled downstream from said combustion zone.
14. A fuel-fired furnace in accordance with claim 11 further comprising a velocity regulation device coupled in flow communication with said second duct and the air source.
15. A fuel-fired furnace in accordance with claim 11 wherein said at least one burner further comprises a fourth duct coupled between said second duct and said first duct.
16. A fuel-fired furnace in accordance with claim 11 further comprising a control system operatively coupled to said first flow regulation device, said second flow regulation device, said third flow regulation device, said control system configured to:
channel the second air flow to said third duct at the second predetermined velocity;
channel the first air flow to said second duct at the second predetermined velocity during a first mode of operation of said furnace, the first mode of operation substantially preventing the fuel flow from being channeled through said first duct;
discontinue the first air flow to said second duct during a second mode of operation of said furnace; and channel the fuel flow to said first duct during the second mode of operation, the second mode of operation substantially preventing the first air flow from being channeled through said second duct.
channel the second air flow to said third duct at the second predetermined velocity;
channel the first air flow to said second duct at the second predetermined velocity during a first mode of operation of said furnace, the first mode of operation substantially preventing the fuel flow from being channeled through said first duct;
discontinue the first air flow to said second duct during a second mode of operation of said furnace; and channel the fuel flow to said first duct during the second mode of operation, the second mode of operation substantially preventing the first air flow from being channeled through said second duct.
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| US12/036,772 | 2008-02-25 | ||
| US12/036,772 US7775791B2 (en) | 2008-02-25 | 2008-02-25 | Method and apparatus for staged combustion of air and fuel |
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| CA2653890C true CA2653890C (en) | 2016-06-07 |
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| CA (1) | CA2653890C (en) |
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-
2008
- 2008-02-25 US US12/036,772 patent/US7775791B2/en not_active Expired - Fee Related
-
2009
- 2009-02-12 CA CA2653890A patent/CA2653890C/en not_active Expired - Fee Related
- 2009-02-12 GB GB0902241.9A patent/GB2457565B/en not_active Expired - Fee Related
- 2009-02-23 DE DE102009003521A patent/DE102009003521A1/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CA2653890A1 (en) | 2009-08-25 |
| DE102009003521A1 (en) | 2009-08-27 |
| GB0902241D0 (en) | 2009-03-25 |
| US7775791B2 (en) | 2010-08-17 |
| US20090214989A1 (en) | 2009-08-27 |
| GB2457565B (en) | 2012-10-03 |
| GB2457565A (en) | 2009-08-26 |
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