CA2827903A1 - Combustion device - Google Patents
Combustion device Download PDFInfo
- Publication number
- CA2827903A1 CA2827903A1 CA2827903A CA2827903A CA2827903A1 CA 2827903 A1 CA2827903 A1 CA 2827903A1 CA 2827903 A CA2827903 A CA 2827903A CA 2827903 A CA2827903 A CA 2827903A CA 2827903 A1 CA2827903 A1 CA 2827903A1
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- Prior art keywords
- burner
- furnace
- air
- combustion
- wind box
- Prior art date
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D1/00—Burners for combustion of pulverulent fuel
- F23D1/005—Burners for combustion of pulverulent fuel burning a mixture of pulverulent fuel delivered as a slurry, i.e. comprising a carrying liquid
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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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D1/00—Burners for combustion of pulverulent fuel
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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
- F23L1/00—Passages or apertures for delivering primary air for combustion
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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
- F23L3/00—Arrangements of valves or dampers before the fire
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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
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- 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
- F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
- F23M9/02—Baffles or deflectors for air or combustion products; Flame shields in air inlets
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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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Abstract
Provided is a boiler having multiple burners (19) arranged on a furnace wall (10) of a furnace (18), each burner (19) comprising: a cylindrical fuel nozzle (3) for injecting a mixture of fuel and carrier gas therefor into the furnace (18); one or more cylindrical air nozzles (8, 11) provided on the outer circumference of the nozzle (3) for injecting combustion air into the furnace; and a wind box (12) for supplying combustion air to the nozzles (8, 11) in common. The wind box (12) is provided with openings (12a, 12b) through which combustion air flows in from a direction perpendicular to the axial direction of the burner (19), and is partitioned by a partition wall (14) to form multiple parallel flow paths for the air flowing in through the openings in a translational manner. Some of the multiple flow paths are connected to an upper part of the combustion air nozzle (8), and the remaining flow paths are connected to a lower part of the nozzle (8). Each of the multiple combustion air flow paths is independently provided with an air momentum deviation damper (15) and an air flow rate adjustment damper (17), such that the direction of the flame of the burner (19) can be changed between upward and downward directions inside the furnace (18) depending on a combustion condition such as a load.
Description
CA 02827903,2013-08-21 DESCRIPTION
COMBUSTION DEVICE
TECHNICAL FIELD
[0001]
The present invention relates to a combustion device such as a pulverized coal burning boiler having a pulverized coal burner.
BACKGROUND ART
COMBUSTION DEVICE
TECHNICAL FIELD
[0001]
The present invention relates to a combustion device such as a pulverized coal burning boiler having a pulverized coal burner.
BACKGROUND ART
[0002]
As a combustion method using a pulverized coal burner of a pulverized coal burning boiler, there is adopted a two-stage combustion method that combusts a fuel in an air insufficient state and then complete burning air is supplied from an after air port in order to reduce an emission rate of a nitride oxide (which will be referred to as NOx hereinafter) in a combustion exhaust gas.
As a combustion method using a pulverized coal burner of a pulverized coal burning boiler, there is adopted a two-stage combustion method that combusts a fuel in an air insufficient state and then complete burning air is supplied from an after air port in order to reduce an emission rate of a nitride oxide (which will be referred to as NOx hereinafter) in a combustion exhaust gas.
[0003]
To further reduce NOx concentration in the exhaust gas at a boiler furnace outlet, the following means can be used.
To further reduce NOx concentration in the exhaust gas at a boiler furnace outlet, the following means can be used.
[0004]
(1) An after-air port is installed to a high position of a furnace, and a detention time of a combustion gas to reach a NOx reduction region between the burner and the after-air port is increased.
CA 02827903,2013-08-21
(1) An after-air port is installed to a high position of a furnace, and a detention time of a combustion gas to reach a NOx reduction region between the burner and the after-air port is increased.
CA 02827903,2013-08-21
[0005]
(2) An excess air ratio (an input air capacity/a theoretical air capacity) is lowered as much as possible, and thermal NOx is reduced beyond those in conventional examples.
(2) An excess air ratio (an input air capacity/a theoretical air capacity) is lowered as much as possible, and thermal NOx is reduced beyond those in conventional examples.
[0006]
However, a complete combustion region shifts to a downstream region (an upper portion of a furnace) according to the technology of (1), a combustion temperature rises as getting closer to the theoretical air capacity according to the technology of (2), and hence an exhaust gas temperature at an outlet of the furnace is increased. Therefore, a steam temperature and a metal temperature on a rear heat transfer surface of the boiler rise, and a possibility of occurrence of tube leak increases in design that a heat transfer surface material, arrangement of the heat transfer surface, and others are unchanged from the conventional examples. Therefore, a design temperature of the rear heat transfer surface must be increased to be higher than those in the conventional examples, and there is a problem that quality of the material must be enhanced in terms of strength and heat resistant properties.
However, a complete combustion region shifts to a downstream region (an upper portion of a furnace) according to the technology of (1), a combustion temperature rises as getting closer to the theoretical air capacity according to the technology of (2), and hence an exhaust gas temperature at an outlet of the furnace is increased. Therefore, a steam temperature and a metal temperature on a rear heat transfer surface of the boiler rise, and a possibility of occurrence of tube leak increases in design that a heat transfer surface material, arrangement of the heat transfer surface, and others are unchanged from the conventional examples. Therefore, a design temperature of the rear heat transfer surface must be increased to be higher than those in the conventional examples, and there is a problem that quality of the material must be enhanced in terms of strength and heat resistant properties.
[0007]
To increase a detention time of the combustion gas to reach the NOx reduction region in the furnace of the after-air port from the burner or to equalize a design temperature of the rear heat transfer surface to a conventional examples while adopting an NOx reduction countermeasure for reducing the air excess ratio (the input air capacity /the theoretical air capacity) %
to be lower than those in the conventional examples, changing a direction of flames of the burner to an upward or downward direction of the furnace in accordance with combustion conditions such as a load can be considered. That is, when a direction of burner flames is set to a downward direction and a detention time of the combustion gas in the NOx reduction region between the burner and the after-air port is increased, the furnace installing position of the after-air port may be the same as that in the conventional example, this position is provided on a lower (upstream) side in the furnace as compared with the conventional examples even if a combustion temperature of the burner flames becomes high, and hence an exhaust gas temperature at the outlet of the furnace can be the same as that in the conventional examples.
To increase a detention time of the combustion gas to reach the NOx reduction region in the furnace of the after-air port from the burner or to equalize a design temperature of the rear heat transfer surface to a conventional examples while adopting an NOx reduction countermeasure for reducing the air excess ratio (the input air capacity /the theoretical air capacity) %
to be lower than those in the conventional examples, changing a direction of flames of the burner to an upward or downward direction of the furnace in accordance with combustion conditions such as a load can be considered. That is, when a direction of burner flames is set to a downward direction and a detention time of the combustion gas in the NOx reduction region between the burner and the after-air port is increased, the furnace installing position of the after-air port may be the same as that in the conventional example, this position is provided on a lower (upstream) side in the furnace as compared with the conventional examples even if a combustion temperature of the burner flames becomes high, and hence an exhaust gas temperature at the outlet of the furnace can be the same as that in the conventional examples.
[0008]
Japanese Unexamined Patent Application Publication No.
2008-121924 discloses a burner having a movable nozzle. When the nozzle is movable in a portion that faces a furnace and has high radiant heat, consideration must be given to damage due to falling of clinkers adhering to the inside of the furnace or securement of movability.
Japanese Unexamined Patent Application Publication No.
2008-121924 discloses a burner having a movable nozzle. When the nozzle is movable in a portion that faces a furnace and has high radiant heat, consideration must be given to damage due to falling of clinkers adhering to the inside of the furnace or securement of movability.
[0009]
Moreover, Japanese Unexamined Patent Application Publication No. 2002-147713 discloses a burner that changes a direction of flames (a combustion region) by deviating an air flow rate in a circumferential direction of a burner.
Incase of the burner provided with a combustion air nozzle having at least two or more air inflow directions, to connect respective combustion air flow paths of a plurality of burners through a duct on outer wall of a furnace and to provide a common wind box, arrangement of the duct is complicated.
PRIOR ART DOCUMENT
PATENT DOCUMENTS
Moreover, Japanese Unexamined Patent Application Publication No. 2002-147713 discloses a burner that changes a direction of flames (a combustion region) by deviating an air flow rate in a circumferential direction of a burner.
Incase of the burner provided with a combustion air nozzle having at least two or more air inflow directions, to connect respective combustion air flow paths of a plurality of burners through a duct on outer wall of a furnace and to provide a common wind box, arrangement of the duct is complicated.
PRIOR ART DOCUMENT
PATENT DOCUMENTS
[0010]
Patent Literature 1: Japanese Unexamined Patent Application Publication No. 2008-121924 Patent Literature 2: Japanese Unexamined Patent Application Publication No. 2002-147713 SUMMARY OF THE INVENTION
PROBLEM TO BE SOLVED BY THE INVENTION
Patent Literature 1: Japanese Unexamined Patent Application Publication No. 2008-121924 Patent Literature 2: Japanese Unexamined Patent Application Publication No. 2002-147713 SUMMARY OF THE INVENTION
PROBLEM TO BE SOLVED BY THE INVENTION
[0011]
As described above, in case of using a burner having a movable nozzle disclosed in Japanese Unexamined Patent Application Publication No. 2008-121924, when the nozzle is movable in the portion that faces the furnace and has large radiant heat, consideration must be given to damage due to falling of clinkers adhering to the inside of the furnace or securement of movability.
As described above, in case of using a burner having a movable nozzle disclosed in Japanese Unexamined Patent Application Publication No. 2008-121924, when the nozzle is movable in the portion that faces the furnace and has large radiant heat, consideration must be given to damage due to falling of clinkers adhering to the inside of the furnace or securement of movability.
[0012]
Additionally, as to the burner provided with the combustion air nozzle having at least two air inflow directions disclosed in Japanese Unexamined Patent Application Publication No. 2002-147713, to connect the respective combustion air flow paths of the plurality of burners through the common dust on the outer wall of the furnace, the arrangement of the duct becomes complicated.
Additionally, as to the burner provided with the combustion air nozzle having at least two air inflow directions disclosed in Japanese Unexamined Patent Application Publication No. 2002-147713, to connect the respective combustion air flow paths of the plurality of burners through the common dust on the outer wall of the furnace, the arrangement of the duct becomes complicated.
[0013]
It is an object of the present invention to provide a combustion device that can change a direction of flames of a burner to upward and downward directions in a furnace in accordance with combustion conditions such as a load and equalize a design temperature of a rear heat transfer surface to that in conventional examples.
MEANS FOR SOLVING PROBLEM
It is an object of the present invention to provide a combustion device that can change a direction of flames of a burner to upward and downward directions in a furnace in accordance with combustion conditions such as a load and equalize a design temperature of a rear heat transfer surface to that in conventional examples.
MEANS FOR SOLVING PROBLEM
[0014]
The above-described object can be achieved by the following solving means.
A first aspect of the present invention provides a combustion device comprising a plurality of burners 19 arranged on a furnace wall 10 of a furnace 18, each burner 19 comprising:
a cylindrical fuel nozzle 3 that injects a mixture of a fuel and a carrier gas therefor into the furnace 18; one or more cylindrical combustion gas nozzles 8, 11 that are provided on the outer circumference of the fuel nozzle 3 and inject a combustion gas into the furnace 18; and a wind box 12 that supplies the combustion gas to the combustion gas nozzles 8, 11, wherein the wind box 12 has a combustion gas inflow opening portion 12a, 12b into which the combustion gas flows from one direction vertical to the axial direction of the burner 19 and is partitioned to form a plurality of parallel flow paths through which the combustion gas flows in from the combustion gas inflow opening portion 12a, 12b, some of the plurality of flow paths are connected to an upper side of the combustion gas nozzles 8, 11, the other flow paths are connected to a lower side of the combustion gas nozzles 8, 11, and first flow rate adjusting means 15 for adjusting a flow rate of the combustion gas is independently provided to each of the plurality of flow paths.
The above-described object can be achieved by the following solving means.
A first aspect of the present invention provides a combustion device comprising a plurality of burners 19 arranged on a furnace wall 10 of a furnace 18, each burner 19 comprising:
a cylindrical fuel nozzle 3 that injects a mixture of a fuel and a carrier gas therefor into the furnace 18; one or more cylindrical combustion gas nozzles 8, 11 that are provided on the outer circumference of the fuel nozzle 3 and inject a combustion gas into the furnace 18; and a wind box 12 that supplies the combustion gas to the combustion gas nozzles 8, 11, wherein the wind box 12 has a combustion gas inflow opening portion 12a, 12b into which the combustion gas flows from one direction vertical to the axial direction of the burner 19 and is partitioned to form a plurality of parallel flow paths through which the combustion gas flows in from the combustion gas inflow opening portion 12a, 12b, some of the plurality of flow paths are connected to an upper side of the combustion gas nozzles 8, 11, the other flow paths are connected to a lower side of the combustion gas nozzles 8, 11, and first flow rate adjusting means 15 for adjusting a flow rate of the combustion gas is independently provided to each of the plurality of flow paths.
[0015]
A second aspect of the present invention provides the combustion device according to the first aspect, wherein one duct 16 through which the combustion gas is supplied to the plurality of wind boxes 12 from the outside of the furnace 18 is installed on the outer side of the furnace wall 10 on which the wind boxes 12 are installed.
A third aspect of the present invention provides the combustion device according to the first or second aspect, wherein the plurality of wind boxes 12 are aligned and installed inside or outside of the one duct 16.
A second aspect of the present invention provides the combustion device according to the first aspect, wherein one duct 16 through which the combustion gas is supplied to the plurality of wind boxes 12 from the outside of the furnace 18 is installed on the outer side of the furnace wall 10 on which the wind boxes 12 are installed.
A third aspect of the present invention provides the combustion device according to the first or second aspect, wherein the plurality of wind boxes 12 are aligned and installed inside or outside of the one duct 16.
[0016]
A fourth aspect of the present invention provides the combustion device according to any one of the first to third aspects, wherein second flow rate adjusting means 17 for adjusting a flow rate of the combustion gas that flows into each burner 19 on the upstream side of the first flow rate adjusting means 15 is provided in each wind box 12.
A fourth aspect of the present invention provides the combustion device according to any one of the first to third aspects, wherein second flow rate adjusting means 17 for adjusting a flow rate of the combustion gas that flows into each burner 19 on the upstream side of the first flow rate adjusting means 15 is provided in each wind box 12.
[0017]
In the combustion device according to the present invention, since the first flow rate adjusting means 15 for adjusting a combustion gas flow rate is provided to each of the plurality of combustion gas nozzles 8 and 11, when an opening degree of the first flow rate adjusting means 15 is adjusted, a momentum of the combustion gas injected into the furnace from the burner 19 can be independently adjusted on each of upper and lower sides. For example, when the first flow rate adjusting means 15 is adjusted to increase an air flow rate injected into the furnace 18 from the combustion gas nozzle 8 or 11 so that a momentum (an air injection flow rate) of the air flow rate from the lower side can be higher than that from the upper side of the burner 19, flames can be deflected to a downward direction. When the flames are deflected to the downward direction, the maximum thermal load region in the furnace 18 shifts to the lower side, thermal absorption of the furnace 18 increases, and an exhaust gas temperature at an outlet of the furnace can be reduced. Further, when the flames are deflected to the lower side of the burner 19 to shift the combustion region of the burner 19 to the lower side, a detention time of the NOx reduction region in the furnace 18 between the burner 19 and the after-airport 24 provided on the furnace wall on the downstream side of the burner 19 becomes longer than that in a case where an injecting direction of flames is parallel, and the NOx concentration in the exhaust gas is reduced to be , , lower than that provided by the conventional technology.
Furthermore, when the second flow rate adjusting means 17 is provided on the upstream side of the first flow rate adjusting means 15, an air capacity supplied to each burner 19 can be adjusted.
EFFECT OF THE INVENTION
In the combustion device according to the present invention, since the first flow rate adjusting means 15 for adjusting a combustion gas flow rate is provided to each of the plurality of combustion gas nozzles 8 and 11, when an opening degree of the first flow rate adjusting means 15 is adjusted, a momentum of the combustion gas injected into the furnace from the burner 19 can be independently adjusted on each of upper and lower sides. For example, when the first flow rate adjusting means 15 is adjusted to increase an air flow rate injected into the furnace 18 from the combustion gas nozzle 8 or 11 so that a momentum (an air injection flow rate) of the air flow rate from the lower side can be higher than that from the upper side of the burner 19, flames can be deflected to a downward direction. When the flames are deflected to the downward direction, the maximum thermal load region in the furnace 18 shifts to the lower side, thermal absorption of the furnace 18 increases, and an exhaust gas temperature at an outlet of the furnace can be reduced. Further, when the flames are deflected to the lower side of the burner 19 to shift the combustion region of the burner 19 to the lower side, a detention time of the NOx reduction region in the furnace 18 between the burner 19 and the after-airport 24 provided on the furnace wall on the downstream side of the burner 19 becomes longer than that in a case where an injecting direction of flames is parallel, and the NOx concentration in the exhaust gas is reduced to be , , lower than that provided by the conventional technology.
Furthermore, when the second flow rate adjusting means 17 is provided on the upstream side of the first flow rate adjusting means 15, an air capacity supplied to each burner 19 can be adjusted.
EFFECT OF THE INVENTION
[0018]
According to the invention of the first aspect, when the momentum of the combustion gas injected into the furnace 18 from the burner 19 is deviated depending on each of the upper and lower sides, the flames can be deflected, and the thermal absorption of the furnace can be controlled. As a result, a temperature controller on the rear heat transfer surface of the furnace 18 can be eliminated. Additionally, in case of modifying an existing combustion device, the NOx reduction technology based on the change in the after-air port installing position and the air excess ratio can be applied without changing a steam temperature and a metal temperature of the rear heat transfer surface in the conventional example. Further, when the flames are deflected toward the lower side in the furnace 18, the combustion region of the burner 19 can be shifted to the lower side, the detention time of the NOx reduction region between the burner 19 and the after-air port 24 can be increased to be longer than that in a case where the injecting direction of the flames is horizontal, and the NOx concentration in the exhaust gas can be reduced as compared with the conventional example.
According to the invention of the second aspect, in addition to the effect of the invention of the first aspect, the combustion gas supplied to the wind box 12 provided on the outer side of one furnace wall surface 10 can be collectively supplied from one duct 16, and the combustion gas supply system for the plurality of burners 19 can have a simple configuration.
According to the invention of the third aspect, in addition to the effect of the invention of the first or second aspect, since the plurality of wind boxes 12 are aligned and installed on the outer side of the furnace wall 10 inside or outside one duct 16, construction of the plurality of wind boxes 12 and the duct 16 can be facilitated.
According to the invention of the fourth aspect, in addition to the effect of the invention of any one of the first to third aspects, the first flow rate adjusting means 15 provided to one wind box 12 can deviate the momentum of the combustion gas on each of the upper and lower sides of the burner
According to the invention of the first aspect, when the momentum of the combustion gas injected into the furnace 18 from the burner 19 is deviated depending on each of the upper and lower sides, the flames can be deflected, and the thermal absorption of the furnace can be controlled. As a result, a temperature controller on the rear heat transfer surface of the furnace 18 can be eliminated. Additionally, in case of modifying an existing combustion device, the NOx reduction technology based on the change in the after-air port installing position and the air excess ratio can be applied without changing a steam temperature and a metal temperature of the rear heat transfer surface in the conventional example. Further, when the flames are deflected toward the lower side in the furnace 18, the combustion region of the burner 19 can be shifted to the lower side, the detention time of the NOx reduction region between the burner 19 and the after-air port 24 can be increased to be longer than that in a case where the injecting direction of the flames is horizontal, and the NOx concentration in the exhaust gas can be reduced as compared with the conventional example.
According to the invention of the second aspect, in addition to the effect of the invention of the first aspect, the combustion gas supplied to the wind box 12 provided on the outer side of one furnace wall surface 10 can be collectively supplied from one duct 16, and the combustion gas supply system for the plurality of burners 19 can have a simple configuration.
According to the invention of the third aspect, in addition to the effect of the invention of the first or second aspect, since the plurality of wind boxes 12 are aligned and installed on the outer side of the furnace wall 10 inside or outside one duct 16, construction of the plurality of wind boxes 12 and the duct 16 can be facilitated.
According to the invention of the fourth aspect, in addition to the effect of the invention of any one of the first to third aspects, the first flow rate adjusting means 15 provided to one wind box 12 can deviate the momentum of the combustion gas on each of the upper and lower sides of the burner
19, and providing the second flow rate adjusting means 17 on the upstream side of the first flow rate adjusting means 15 enables facilitating adjustment of an amount of the combustion gas supplied to each burner 19.
BRIEF DESCRIPTION OF DRAWINGS
[0019]
FIG. 1 is a schematic view showing a pulverized coal boiler system according to the present invention;
FIG. 2 is a cross-sectional view of a pulverized coal burner according to an embodiment of the present invention;
FIG. 3 is a perspective view (FIG. 3 (a) ) of a wind box and a view (FIG. 3 (b) ) showing a wind tunnel test result concerning the wind box according to an embodiment of the present invention;
FIG. 4 shows an example of the wind box in the form of a cross-sectional view (FIG. 4 (a) ) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 4 (b) ) taken along a line B-B in FIG. 2;
FIG. 5 shows an example of the wind box in the form of a cross-sectional view (FIG. 5 (a) ) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 5 (b) ) taken along a line B-B in FIG. 2;
FIG. 6 is a view showing a method for connecting each wind box with a combustion gas carrying duct and supplying combustion air according to an embodiment of the present invention;
FIG. 7 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 8 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 9 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 10 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying ak 02827903 2013-08-21 the combustion air according to an embodiment of the present invention;
FIG. 11 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 12 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 13 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 14 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 15 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 16 shows an example of the wind box in the form of a cross-sectional view (FIG. 16(a)) taken along the line A-A
in FIG. 2 and a cross-sectional view (FIG. 16(b)) taken along a line B-B in FIG. 2;
FIG. 17 shows an example of the wind box in the form of a cross-sectional view (FIG. 17(a)) taken along the line A-A
in FIG. 2 and a cross-sectional view (FIG. 17(b)) taken along a line B-B in FIG. 2;
FIG. 18 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention; and FIG. 19 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention.
BEST MODE(S) FOR CARRYING OUT THE INVENTION
BRIEF DESCRIPTION OF DRAWINGS
[0019]
FIG. 1 is a schematic view showing a pulverized coal boiler system according to the present invention;
FIG. 2 is a cross-sectional view of a pulverized coal burner according to an embodiment of the present invention;
FIG. 3 is a perspective view (FIG. 3 (a) ) of a wind box and a view (FIG. 3 (b) ) showing a wind tunnel test result concerning the wind box according to an embodiment of the present invention;
FIG. 4 shows an example of the wind box in the form of a cross-sectional view (FIG. 4 (a) ) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 4 (b) ) taken along a line B-B in FIG. 2;
FIG. 5 shows an example of the wind box in the form of a cross-sectional view (FIG. 5 (a) ) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 5 (b) ) taken along a line B-B in FIG. 2;
FIG. 6 is a view showing a method for connecting each wind box with a combustion gas carrying duct and supplying combustion air according to an embodiment of the present invention;
FIG. 7 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 8 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 9 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 10 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying ak 02827903 2013-08-21 the combustion air according to an embodiment of the present invention;
FIG. 11 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 12 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 13 shows an example of the wind box in the form of a cross-sectional view taken along the line A-A in FIG. 2;
FIG. 14 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 15 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention;
FIG. 16 shows an example of the wind box in the form of a cross-sectional view (FIG. 16(a)) taken along the line A-A
in FIG. 2 and a cross-sectional view (FIG. 16(b)) taken along a line B-B in FIG. 2;
FIG. 17 shows an example of the wind box in the form of a cross-sectional view (FIG. 17(a)) taken along the line A-A
in FIG. 2 and a cross-sectional view (FIG. 17(b)) taken along a line B-B in FIG. 2;
FIG. 18 is a view showing a method for installing each wind box in the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention; and FIG. 19 is a view showing a method for connecting each wind box with the combustion gas carrying duct and supplying the combustion air according to an embodiment of the present invention.
BEST MODE(S) FOR CARRYING OUT THE INVENTION
[0020]
FIG. 1 shows a pulverized coal boiler system according to the present invention, FIG. 2 is a cross-sectional view of a pulverized coal burner 19 concerning the pulverized coal boiler system in FIG. 1, and FIG. 3 is a perspective view (FIG.
3(a)) of a wind box 12 of the pulverized coal burner 19 and a view (FIG. 3(b)) showing a wind tunnel test result concerning the wind box 12.
It is to be noted that a fuel in the present invention is not restricted to pulverized coal, and a solid fuel pulverized so that it can be carried using an air current can be used without regard to its type or composition. Further, although a description will be given on a situation where air is mainly used as a fuel carrying gas and a combustion gas, the present invention is not necessarily restricted to air alone, and it is possible to adopt any gas that can be used as the fuel carrying gas and the combustion gas for a combustion device such as a boiler, e.g., a combustion exhaust gas or a mixed gas of air or oxygen and the combustion exhaust gas without regard to its type or composition.
FIG. 1 shows a pulverized coal boiler system according to the present invention, FIG. 2 is a cross-sectional view of a pulverized coal burner 19 concerning the pulverized coal boiler system in FIG. 1, and FIG. 3 is a perspective view (FIG.
3(a)) of a wind box 12 of the pulverized coal burner 19 and a view (FIG. 3(b)) showing a wind tunnel test result concerning the wind box 12.
It is to be noted that a fuel in the present invention is not restricted to pulverized coal, and a solid fuel pulverized so that it can be carried using an air current can be used without regard to its type or composition. Further, although a description will be given on a situation where air is mainly used as a fuel carrying gas and a combustion gas, the present invention is not necessarily restricted to air alone, and it is possible to adopt any gas that can be used as the fuel carrying gas and the combustion gas for a combustion device such as a boiler, e.g., a combustion exhaust gas or a mixed gas of air or oxygen and the combustion exhaust gas without regard to its type or composition.
[0021]
In the pulverized coal boiler system shown in FIG. 1, pulverized coal and combustion air are supplied to burners 19 provided on a plurality of stages on a furnace wall 10 of a boiler furnace 18, the pulverized coal is combusted, and a non-illustrated water wall constituting the furnace wall 10 and a heat exchanger such as a non-illustrated superheater provided in the furnace are heated, thereby generating water vapor.
In the pulverized coal boiler system shown in FIG. 1, pulverized coal and combustion air are supplied to burners 19 provided on a plurality of stages on a furnace wall 10 of a boiler furnace 18, the pulverized coal is combusted, and a non-illustrated water wall constituting the furnace wall 10 and a heat exchanger such as a non-illustrated superheater provided in the furnace are heated, thereby generating water vapor.
[0022]
The pulverized coal supplied to each burner 19 is obtained by pulverizing coal in a bunker 20 with use of a mill 21, and the pulverized coal is carried on an air current and supplied to each burner 19 by using a blower 23. Further, the combustion air supplied to each burner 19 and each after-air port 24 is supplied through a duct 16 by a blower 25, and the combustion air is supplied to each pulverized coal burner 19 from each wind box 12 arranged on the outer side of the boiler furnace wall 10.
The pulverized coal supplied to each burner 19 is obtained by pulverizing coal in a bunker 20 with use of a mill 21, and the pulverized coal is carried on an air current and supplied to each burner 19 by using a blower 23. Further, the combustion air supplied to each burner 19 and each after-air port 24 is supplied through a duct 16 by a blower 25, and the combustion air is supplied to each pulverized coal burner 19 from each wind box 12 arranged on the outer side of the boiler furnace wall 10.
[0023]
An oil spraying nozzle 7 is arranged at a central axis of the pulverized coal burner 19, a fuel nozzle 3 through which a gas-particle flow 1 of the pulverized coal and the carrying air is arranged at an outer periphery of the oil spraying nozzle 7, and a secondary air nozzle 8 and a tertiary air nozzle 11 that inject the combustion air 2 are provided at an outer ak 02827903 2013-08-21 periphery of the fuel nozzle 3. As shown in FIG. 2, an outer peripheral wall of the tertiary air nozzle 11 is formed of the wind box 12.
Further, the oil spraying nozzle 7 is used for auxiliary combustion at the time of starting up or low-load combustion of each burner 19. A venturi tube 6 configured to narrow a nozzle inner diameter of the fuel nozzle 3 is arranged on an inner peripheral wall of the fuel nozzle 3, and a pulverized coal concentrator 5 is provided on the outer periphery of the oil spraying nozzle 7 near an outlet portion of the fuel nozzle 3. A flame stabilizer 4 is provided at an end of a partition wall (an outlet portion of each of the nozzles 3 and 8) that partitions the fuel nozzle 3 and the secondary air nozzle 8, and a guide sleeve 13 that directs a fluid toward a diffusing direction from the central axis of the burner 19 is provided at an end of a partition wall (an outlet portion of each of the nozzles 8 and 11) that partitions the secondary air nozzle 8 and the tertiary air nozzle 11.
An oil spraying nozzle 7 is arranged at a central axis of the pulverized coal burner 19, a fuel nozzle 3 through which a gas-particle flow 1 of the pulverized coal and the carrying air is arranged at an outer periphery of the oil spraying nozzle 7, and a secondary air nozzle 8 and a tertiary air nozzle 11 that inject the combustion air 2 are provided at an outer ak 02827903 2013-08-21 periphery of the fuel nozzle 3. As shown in FIG. 2, an outer peripheral wall of the tertiary air nozzle 11 is formed of the wind box 12.
Further, the oil spraying nozzle 7 is used for auxiliary combustion at the time of starting up or low-load combustion of each burner 19. A venturi tube 6 configured to narrow a nozzle inner diameter of the fuel nozzle 3 is arranged on an inner peripheral wall of the fuel nozzle 3, and a pulverized coal concentrator 5 is provided on the outer periphery of the oil spraying nozzle 7 near an outlet portion of the fuel nozzle 3. A flame stabilizer 4 is provided at an end of a partition wall (an outlet portion of each of the nozzles 3 and 8) that partitions the fuel nozzle 3 and the secondary air nozzle 8, and a guide sleeve 13 that directs a fluid toward a diffusing direction from the central axis of the burner 19 is provided at an end of a partition wall (an outlet portion of each of the nozzles 8 and 11) that partitions the secondary air nozzle 8 and the tertiary air nozzle 11.
[0024]
As described above, in this embodiment, each burner 19 is formed of the oil spraying nozzle 7, the fuel nozzle 3, the secondary air nozzle 8, the tertiary air nozzle 11, and the wind box 12 constituting the outer peripheral wall of the tertiary air nozzle 11, and this burner 19 is installed on the furnace wall 10 of the furnace 18.
Although a description will be given with reference to the drawings, the present invention is not restricted to ak 02827903 2013-08-21 structures in the description.
As described above, in this embodiment, each burner 19 is formed of the oil spraying nozzle 7, the fuel nozzle 3, the secondary air nozzle 8, the tertiary air nozzle 11, and the wind box 12 constituting the outer peripheral wall of the tertiary air nozzle 11, and this burner 19 is installed on the furnace wall 10 of the furnace 18.
Although a description will be given with reference to the drawings, the present invention is not restricted to ak 02827903 2013-08-21 structures in the description.
[0025]
FIG. 3(a) shows a perspective view of the wind box 12 of the pulverized coal burner 19 according to this embodiment, and FIG. 4 shows a cross-sectional view (FIG. 4(a)) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 4(b)) taken along a line B-B in FIG. 2. It is to be noted that each dark arrow shown in FIG. 4 and subsequent drawings represents an inflow direction of the combustion air.
FIG. 3(a) shows a perspective view of the wind box 12 of the pulverized coal burner 19 according to this embodiment, and FIG. 4 shows a cross-sectional view (FIG. 4(a)) taken along a line A-A in FIG. 2 and a cross-sectional view (FIG. 4(b)) taken along a line B-B in FIG. 2. It is to be noted that each dark arrow shown in FIG. 4 and subsequent drawings represents an inflow direction of the combustion air.
[0026]
Further, a heavy oil nozzle 7 and the pulverized coal nozzle 3 are not shown in FIG. 4, and the heavy oil nozzle 7 and the pulverized coal nozzle 3 are arranged in a cylindrical through hole of the wind box 12. A furnace wall of the through hole constitutes an outer wall of the secondary air nozzle 8.
Further, a heavy oil nozzle 7 and the pulverized coal nozzle 3 are not shown in FIG. 4, and the heavy oil nozzle 7 and the pulverized coal nozzle 3 are arranged in a cylindrical through hole of the wind box 12. A furnace wall of the through hole constitutes an outer wall of the secondary air nozzle 8.
[0027]
As shown in FIG. 4, the wind box 12 having combustion air inlet openings 12a and 12b provided in a direction vertical to a central axis direction of the pulverized coal burner 19, and the secondary air nozzle 8 is arranged as if it is inserted in the through hole provided in the wind box 12.
As shown in FIG. 4, the wind box 12 having combustion air inlet openings 12a and 12b provided in a direction vertical to a central axis direction of the pulverized coal burner 19, and the secondary air nozzle 8 is arranged as if it is inserted in the through hole provided in the wind box 12.
[0028]
Furthermore, the two combustion air inlet openings 12a and 12b are provided in the wind box 12, a partition plate 14 that partitions the two combustion air inlet openings (combustion gas opening portions) 12a and 12b is provided, and the partition plate 14 is connected to the outer side of a portion that divides the outer wall of the secondary air nozzle 8 constituting the through hole of the wind box 12 into two parts.
Furthermore, the two combustion air inlet openings 12a and 12b are provided in the wind box 12, a partition plate 14 that partitions the two combustion air inlet openings (combustion gas opening portions) 12a and 12b is provided, and the partition plate 14 is connected to the outer side of a portion that divides the outer wall of the secondary air nozzle 8 constituting the through hole of the wind box 12 into two parts.
[0029]
Upper and lower dampers 15a and 15b, each of which has a rotary shaft in a direction cutting across a flow of the combustion air introduced into the wind box and changes an area through which the combustion air flows, are provided near the combustion air inlet openings 12a and 12b in the wind box 12 divided into upper and lower parts by the partition plate 14, and separately adjusting respective rotation angles of the two dampers 15a and 15b enables deviating a momentum of the combustion air injected from the pulverized coal burner 19 depending on each of upper and lower sides in the wind box 12.
Upper and lower dampers 15a and 15b, each of which has a rotary shaft in a direction cutting across a flow of the combustion air introduced into the wind box and changes an area through which the combustion air flows, are provided near the combustion air inlet openings 12a and 12b in the wind box 12 divided into upper and lower parts by the partition plate 14, and separately adjusting respective rotation angles of the two dampers 15a and 15b enables deviating a momentum of the combustion air injected from the pulverized coal burner 19 depending on each of upper and lower sides in the wind box 12.
[0030]
For example, when the upper damper 15a is closed and the lower damper 15b is opened, an injection amount of the combustion air on the lower side of the burner 19 increases, and the momentum of the combustion air on the lower side of the burner 19 increases, whereby flames in the boiler furnace 18 can be deflected to a downward direction.
It is to be noted that, in a state that planes of the dampers 15a and 15b are arranged in a direction parallel to a flow of the combustion air, each of the dampers 15a and 15b is arranged in the wind box 12 to be retracted by a length L1 from the inlet opening portion of the wind box 12.
For example, when the upper damper 15a is closed and the lower damper 15b is opened, an injection amount of the combustion air on the lower side of the burner 19 increases, and the momentum of the combustion air on the lower side of the burner 19 increases, whereby flames in the boiler furnace 18 can be deflected to a downward direction.
It is to be noted that, in a state that planes of the dampers 15a and 15b are arranged in a direction parallel to a flow of the combustion air, each of the dampers 15a and 15b is arranged in the wind box 12 to be retracted by a length L1 from the inlet opening portion of the wind box 12.
[0031]
FIG. 3(b) shows a result of a tertiary air flow path outlet velocity distribution at the time of flame downward deflection realized by conducting a test for deviating a momentum of tertiary air injected from the tertiary air nozzle 11 into the furnace depending on each of the upper and lower sides of the burner 19 based on the wind tunnel test. It was confirmed from this wind tunnel test that the momentum of the combustion air on the lower side of the burner 19 can be increased by adjusting a revolving angle of each of the upper and lower revolving dampers 15a and 15b. In case of deflecting flames into the furnace 18 on the upper side of the burner 19, the upper revolving damper 15a is opened, and the lower revolving damper 15b is closed.
FIG. 3(b) shows a result of a tertiary air flow path outlet velocity distribution at the time of flame downward deflection realized by conducting a test for deviating a momentum of tertiary air injected from the tertiary air nozzle 11 into the furnace depending on each of the upper and lower sides of the burner 19 based on the wind tunnel test. It was confirmed from this wind tunnel test that the momentum of the combustion air on the lower side of the burner 19 can be increased by adjusting a revolving angle of each of the upper and lower revolving dampers 15a and 15b. In case of deflecting flames into the furnace 18 on the upper side of the burner 19, the upper revolving damper 15a is opened, and the lower revolving damper 15b is closed.
[0032]
Since the secondary air nozzle 8 having the guide sleeve 13 at the distal end thereof is provided in the pulverized coal burner 19, the combustion air can be gradually injected. Two upper and lower opening portions 8a are provided at the outer peripheral portion of the secondary air nozzle 8, and it is desirable to provide an air capacity adjusting mechanism such as slide type dampers 9a and 9b that adjust an amount of air supplied into the secondary air nozzle 8 from the opening portions 8a as shown in FIG. 2.
Since the secondary air nozzle 8 having the guide sleeve 13 at the distal end thereof is provided in the pulverized coal burner 19, the combustion air can be gradually injected. Two upper and lower opening portions 8a are provided at the outer peripheral portion of the secondary air nozzle 8, and it is desirable to provide an air capacity adjusting mechanism such as slide type dampers 9a and 9b that adjust an amount of air supplied into the secondary air nozzle 8 from the opening portions 8a as shown in FIG. 2.
[0033]
For example, when the upper revolving damper 15a is closed and the lower revolving damper 15b is opened to increase an injection amount of the combustion air from the lower side of the burner 19, the air can be prevented from flowing into the upper secondary air nozzle 8 and the tertiary air nozzle 11 by fully closing the upper opening portion 8a of the secondary air nozzle 8 with use of the slide type damper 9a, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained in the circumferential direction, thereby keeping flame stabilizing properties.
For example, when the upper revolving damper 15a is closed and the lower revolving damper 15b is opened to increase an injection amount of the combustion air from the lower side of the burner 19, the air can be prevented from flowing into the upper secondary air nozzle 8 and the tertiary air nozzle 11 by fully closing the upper opening portion 8a of the secondary air nozzle 8 with use of the slide type damper 9a, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained in the circumferential direction, thereby keeping flame stabilizing properties.
[0034]
It is to be noted that the momentum of the air injected from the secondary air nozzle 8 into the furnace 18 can be substantially evenly maintained along the circumferential direction of the secondary air nozzle 8 only if the combustion air flows into the secondary nozzle 8 from any position irrespective of whether the upper opening portion 8a of the secondary air nozzle 8 is fully closed by using the slide type damper 9a, but the upper opening portion 8a of the secondary air nozzle 8 must be fully closed by using the slide type damper 9a if softening the deflection of the flames in the furnace 18 toward the lower side is undesirable.
It is to be noted that the momentum of the air injected from the secondary air nozzle 8 into the furnace 18 can be substantially evenly maintained along the circumferential direction of the secondary air nozzle 8 only if the combustion air flows into the secondary nozzle 8 from any position irrespective of whether the upper opening portion 8a of the secondary air nozzle 8 is fully closed by using the slide type damper 9a, but the upper opening portion 8a of the secondary air nozzle 8 must be fully closed by using the slide type damper 9a if softening the deflection of the flames in the furnace 18 toward the lower side is undesirable.
[0035]
A direction of the flames in the furnace 18 can be deflected by just deviating the momentum of the combustion air in each of the upper half portion and the lower half portion in the burner 19 while maintaining flame stabilizing properties by adjusting an inflow amount of the combustion air. When each CA 02827903 2013-,08-21 of the combustion air inlet openings 12a and 12b obtained by dividing the inside of the wind box shown in FIG. 5 into two parts by the partition plate 14 is further divided into two parts and dampers 15aa and 15ab and dampers 15ba and 15bb are provided to the respective combustion air inlet openings 12a and 12b, the momentum of the combustion air is deviated in each of the upper half and the lower half of the burner 19, whereby a direction of flames in the furnace 18 can be deflected.
A direction of the flames in the furnace 18 can be deflected by just deviating the momentum of the combustion air in each of the upper half portion and the lower half portion in the burner 19 while maintaining flame stabilizing properties by adjusting an inflow amount of the combustion air. When each CA 02827903 2013-,08-21 of the combustion air inlet openings 12a and 12b obtained by dividing the inside of the wind box shown in FIG. 5 into two parts by the partition plate 14 is further divided into two parts and dampers 15aa and 15ab and dampers 15ba and 15bb are provided to the respective combustion air inlet openings 12a and 12b, the momentum of the combustion air is deviated in each of the upper half and the lower half of the burner 19, whereby a direction of flames in the furnace 18 can be deflected.
[0036]
In this embodiment, as shown in FIG. 6, the burners 19 each having the wind box 12 are installed on the furnace wall of the boiler furnace 18, and the combustion air is supplied into the burners 19 from the duct 16 provided on the outer side of the furnace wall 10. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 7, the momentum of the combustion air in each of the upper half and the lower half of each burner 19 can be deviated, and a direction of flames in the furnace 18 can be deflected.
In this embodiment, as shown in FIG. 6, the burners 19 each having the wind box 12 are installed on the furnace wall of the boiler furnace 18, and the combustion air is supplied into the burners 19 from the duct 16 provided on the outer side of the furnace wall 10. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 7, the momentum of the combustion air in each of the upper half and the lower half of each burner 19 can be deviated, and a direction of flames in the furnace 18 can be deflected.
[0037]
In this embodiment, as shown in FIG. 8 and FIG. 9, a wind box 12 into which combustion air flows only from the upper side that is vertical to a central axis direction of a burner 19 is provided, and a plurality of partition plate 14 and revolving dampers 15 are provided in the wind box 12 so that the momentum of the combustion air injected into a furnace can be deviated depending on each of upper and lower sides by adjusting the dampers 15.
In this embodiment, as shown in FIG. 8 and FIG. 9, a wind box 12 into which combustion air flows only from the upper side that is vertical to a central axis direction of a burner 19 is provided, and a plurality of partition plate 14 and revolving dampers 15 are provided in the wind box 12 so that the momentum of the combustion air injected into a furnace can be deviated depending on each of upper and lower sides by adjusting the dampers 15.
[0038]
As shown in FIG. 8, in this embodiment, the partition plates 14 are provided so as to divide into three parts the wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19.
Furthermore, the dampers 15a, 15b, and 15b as air capacity adjusters are provided on the upstream side of trifurcated air inflow paths in the wind box 12, respectively. Therefore, air flows into the upper side of the burner 19 from a central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
As shown in FIG. 8, in this embodiment, the partition plates 14 are provided so as to divide into three parts the wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19.
Furthermore, the dampers 15a, 15b, and 15b as air capacity adjusters are provided on the upstream side of trifurcated air inflow paths in the wind box 12, respectively. Therefore, air flows into the upper side of the burner 19 from a central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
[0039]
In an embodiment shown in FIG. 9, two partition plates 14 are provided so as to divide into four parts a wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19. Furthermore, the combustion air inlet opening 12a at a central portion of the wind box 12 is divided into two parts, and dampers 15aa, 15ab, and 15b as air capacity adjusters are provided on the upstream side of respective air inflow paths. Therefore, also when shown in Fig. 9, air flows into the upper side of the burner 19 from an upper central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
In an embodiment shown in FIG. 9, two partition plates 14 are provided so as to divide into four parts a wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19. Furthermore, the combustion air inlet opening 12a at a central portion of the wind box 12 is divided into two parts, and dampers 15aa, 15ab, and 15b as air capacity adjusters are provided on the upstream side of respective air inflow paths. Therefore, also when shown in Fig. 9, air flows into the upper side of the burner 19 from an upper central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
[0040]
In the wind box 12 shown in each of FIG. 8 and FIG. 9, for example, when the damper 15a or the dampers 15aa and 15ab near the combustion air inlet opening 12a at the central portion are closed and the other two dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened, an injection amount of the combustion air in the lower portion of the burner 19 increases, the momentum of the combustion air current flowing toward the lower side of the burner increases, and a direction of flames in a furnace 18 can be changed to a downward direction. A result obtained by conducting a test of deviating the momentum of tertiary air on each of upper and lower sides of the burner 19 based on a wind tunnel test is as shown in FIG. 3.
In the wind box 12 shown in each of FIG. 8 and FIG. 9, for example, when the damper 15a or the dampers 15aa and 15ab near the combustion air inlet opening 12a at the central portion are closed and the other two dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened, an injection amount of the combustion air in the lower portion of the burner 19 increases, the momentum of the combustion air current flowing toward the lower side of the burner increases, and a direction of flames in a furnace 18 can be changed to a downward direction. A result obtained by conducting a test of deviating the momentum of tertiary air on each of upper and lower sides of the burner 19 based on a wind tunnel test is as shown in FIG. 3.
[0041]
As described above, it can be confirmed that the momentum on the lower side of the burner 19 in the furnace 18 can be increased by adjusting an amount of the combustion air flowing into the wind box 12 by using three or four dampers 15.
Performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace.
As described above, it can be confirmed that the momentum on the lower side of the burner 19 in the furnace 18 can be increased by adjusting an amount of the combustion air flowing into the wind box 12 by using three or four dampers 15.
Performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace.
[0042]
A secondary air nozzle 8 having a guide sleeve 13 at an end thereof is provided in the wind box 12 so that the combustion air can be gradually injected. An opening portion 8a is provided in an outer wall of the secondary air nozzle 8, and it is desirable to use an air capacity adjusting mechanism such as slide type dampers 9a and 9b shown in FIG. 2 that can adjust an amount of air supplied into the secondary air nozzle 8 in order to adjust an opening degree of the opening portion 8a.
For example, when the damper 15a near the combustion air inlet opening 12a in the central portion shown in FIG. 8 is closed whilst the two dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened and an injection amount of the combustion air on the lower side in the furnace 18 thereby increases, fully closing the opening portion 8a of the secondary air nozzle 8 provided on the upper side of the wind box 12 with use of the slide type dampers 9a and 9b enables preventing air from flowing into a tertiary air nozzle 11 in the upper portion of the burner 19, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction, whereby flame stabilizing properties can be maintained.
A secondary air nozzle 8 having a guide sleeve 13 at an end thereof is provided in the wind box 12 so that the combustion air can be gradually injected. An opening portion 8a is provided in an outer wall of the secondary air nozzle 8, and it is desirable to use an air capacity adjusting mechanism such as slide type dampers 9a and 9b shown in FIG. 2 that can adjust an amount of air supplied into the secondary air nozzle 8 in order to adjust an opening degree of the opening portion 8a.
For example, when the damper 15a near the combustion air inlet opening 12a in the central portion shown in FIG. 8 is closed whilst the two dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened and an injection amount of the combustion air on the lower side in the furnace 18 thereby increases, fully closing the opening portion 8a of the secondary air nozzle 8 provided on the upper side of the wind box 12 with use of the slide type dampers 9a and 9b enables preventing air from flowing into a tertiary air nozzle 11 in the upper portion of the burner 19, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction, whereby flame stabilizing properties can be maintained.
[0043]
The flames can be deflected by just deviating the momentum of the tertiary air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation. According to these structures and the operating method, even when the combustion air inlet opening 12a in the central portion of the wind box 12 is divided into two portions as shown in FIG. 9 and the dampers 15aa and 15ab are provided near these divided portions, the same effect can be obtained by a damper adjustment method.
The flames can be deflected by just deviating the momentum of the tertiary air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation. According to these structures and the operating method, even when the combustion air inlet opening 12a in the central portion of the wind box 12 is divided into two portions as shown in FIG. 9 and the dampers 15aa and 15ab are provided near these divided portions, the same effect can be obtained by a damper adjustment method.
[0044]
This embodiment provides a configuration that burners 19 each having the wind box 12 are installed on the outer side of the furnace wall 10 of the boiler furnace 18 and the combustion air is put into a duct 16 connected to each wind box 12 from an illustrated inflow direction. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 11, the same operation method can be executed.
This embodiment provides a configuration that burners 19 each having the wind box 12 are installed on the outer side of the furnace wall 10 of the boiler furnace 18 and the combustion air is put into a duct 16 connected to each wind box 12 from an illustrated inflow direction. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 11, the same operation method can be executed.
[0045]
This embodiment shown in FIG. 12 and FIG. 13 has a configuration that a wind box 12 into which combustion air flows only from lower combustion air inlet openings 12a and 12b vertical to a central axis of the burner 19 is provided, the inside of the wind box 12 is partitioned by a plurality of partition plates 14, dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b are provided in respective combustion air nozzles in the wind box 12 partitioned by the partition plates 14, and the momentum of the combustion air injected into a furnace 18 from the burner 19 is deviated depending on each of upper and lower sides of the burner 19 by adjusting opening/closing degrees of the dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b.
This embodiment shown in FIG. 12 and FIG. 13 has a configuration that a wind box 12 into which combustion air flows only from lower combustion air inlet openings 12a and 12b vertical to a central axis of the burner 19 is provided, the inside of the wind box 12 is partitioned by a plurality of partition plates 14, dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b are provided in respective combustion air nozzles in the wind box 12 partitioned by the partition plates 14, and the momentum of the combustion air injected into a furnace 18 from the burner 19 is deviated depending on each of upper and lower sides of the burner 19 by adjusting opening/closing degrees of the dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b.
[0046]
In this embodiment shown in FIG. 12, the partition plates 14 and 14 are provided so as to divide the wind box 12, into which the combustion air flows from only one lower direction which is a direction vertical to the central axis direction of the burner 19, into threeportions. Moreover, dampers 15b, 15a, and 15b as air capacity adjusters are provided on upstream portions of trifurcated air inflow paths 12b, 12a, and 12b of the wind box 12. Therefore, air from a combustion air inlet opening 12a at a central portion of the wind box 12 flows into the lower side of the burner 19, and air flows into the upper side of the burner 19 from the left and right combustion air inlet openings 12b and 12b of the wind box 12.
In this embodiment shown in FIG. 12, the partition plates 14 and 14 are provided so as to divide the wind box 12, into which the combustion air flows from only one lower direction which is a direction vertical to the central axis direction of the burner 19, into threeportions. Moreover, dampers 15b, 15a, and 15b as air capacity adjusters are provided on upstream portions of trifurcated air inflow paths 12b, 12a, and 12b of the wind box 12. Therefore, air from a combustion air inlet opening 12a at a central portion of the wind box 12 flows into the lower side of the burner 19, and air flows into the upper side of the burner 19 from the left and right combustion air inlet openings 12b and 12b of the wind box 12.
[0047]
As described above, for example, when the damper 15a near the combustion air inlet opening 12a in the central portion of the wind box 12 is opened and the dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are closed, an injection amount of the combustion air on the lower side of the burner 19 increases, and the momentum of the combustion air flowing toward the lower side of the burner 19 increases, thereby changing a direction of flames in the furnace 18 to a downward direction. A result obtained by conducting a test of deviating the momentum of tertiary air on each of upper and lower sides based on the wind tunnel test is as shown in FIG. 3.
As described above, for example, when the damper 15a near the combustion air inlet opening 12a in the central portion of the wind box 12 is opened and the dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are closed, an injection amount of the combustion air on the lower side of the burner 19 increases, and the momentum of the combustion air flowing toward the lower side of the burner 19 increases, thereby changing a direction of flames in the furnace 18 to a downward direction. A result obtained by conducting a test of deviating the momentum of tertiary air on each of upper and lower sides based on the wind tunnel test is as shown in FIG. 3.
[0048]
It can be confirmed that the momentum on the lower side of the burner 19 can be increased by adjusting opening/closing degrees of the three dampers 15b, 15a, and 15b, and performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace 18.
It can be confirmed that the momentum on the lower side of the burner 19 can be increased by adjusting opening/closing degrees of the three dampers 15b, 15a, and 15b, and performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace 18.
[0049]
A secondary air nozzle 8 having a guide sleeve 13 is provided in the wind box 12 so that the combustion air can be injected along a spreading direction from an outlet of the burner 19. Further, an opening portion 8a (FIG. 2) is provided in the secondary air nozzle 8, and it is desirable to adjust an air inflow amount from the opening portion 8a by providing a slide type damper 9 shown in FIG. 2. For example, when the damper 15a near the combustion air inlet opening 12a in the central portion of the wind box 12 is closed whilst the dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened and an injection amount of the combustion air in the upper portion of the burner 19 thereby increases, fully closing the opening portion 8a of the secondary air nozzle 8 provided on the lower side of the wind box 12 with use of the slide type damper 9 enables preventing air from flowing into a tertiary air nozzle 11 on the lower side of the burner 19, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction, whereby flame stabilizing properties can be maintained. The flames can be deflected by just adjusting a tertiary air injection amount to deviate the momentum of the air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation.
According to these structures and the operating method, even when the combustion air inlet openings 12b and 12b are provided on both sides of the lower side of the wind box 12, the combustion air inlet opening 12a in the central portion is divided into two portions, and the dampers 15b, 15aa, 15ab, and 15b are provided on the upstream side of the respective air inflow paths as shown in FIG. 13, the same effect can be obtained by adj ustment methods of the dampers 15b, 15aa, 15ab, and 15b.
A secondary air nozzle 8 having a guide sleeve 13 is provided in the wind box 12 so that the combustion air can be injected along a spreading direction from an outlet of the burner 19. Further, an opening portion 8a (FIG. 2) is provided in the secondary air nozzle 8, and it is desirable to adjust an air inflow amount from the opening portion 8a by providing a slide type damper 9 shown in FIG. 2. For example, when the damper 15a near the combustion air inlet opening 12a in the central portion of the wind box 12 is closed whilst the dampers 15b and 15b near the left and right combustion air inlet openings 12b and 12b are opened and an injection amount of the combustion air in the upper portion of the burner 19 thereby increases, fully closing the opening portion 8a of the secondary air nozzle 8 provided on the lower side of the wind box 12 with use of the slide type damper 9 enables preventing air from flowing into a tertiary air nozzle 11 on the lower side of the burner 19, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction, whereby flame stabilizing properties can be maintained. The flames can be deflected by just adjusting a tertiary air injection amount to deviate the momentum of the air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation.
According to these structures and the operating method, even when the combustion air inlet openings 12b and 12b are provided on both sides of the lower side of the wind box 12, the combustion air inlet opening 12a in the central portion is divided into two portions, and the dampers 15b, 15aa, 15ab, and 15b are provided on the upstream side of the respective air inflow paths as shown in FIG. 13, the same effect can be obtained by adj ustment methods of the dampers 15b, 15aa, 15ab, and 15b.
[0050]
This embodiment is characterized in that the burners 19 each having the wind box 12 are installed on the boiler furnace wall 10 as shown in FIG. 14 and the combustion air is supplied into the burners 19 from a duct 16 provided on the outer side of the furnace wall 10. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG.
CA 02827903 2013-,08-21 15, the same operation method can be carried out.
This embodiment is characterized in that the burners 19 each having the wind box 12 are installed on the boiler furnace wall 10 as shown in FIG. 14 and the combustion air is supplied into the burners 19 from a duct 16 provided on the outer side of the furnace wall 10. However, arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19. Further, even if the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG.
CA 02827903 2013-,08-21 15, the same operation method can be carried out.
[0051]
According to this embodiment 3, when flames in the furnace 18 are deflected to the downward direction, the maximum thermal load region in the furnace 18 shifts to the lower side, thermal absorption of the furnace thereby increases, an exhaust gas temperature at an outlet of the furnace 18 can be reduced, a detention time of an NOx reduction region in the furnace 18 between the burner 19 and an after-air port 24 can be increased beyond than that in a case where a combustion region is evenly formed on each of upper and lower sides of the burner 19 by shifting the combustion region of the burner 19 to the lower side, thus providing the pulverized coal burner 19 that can reduce the NOx concentration.
According to this embodiment 3, when flames in the furnace 18 are deflected to the downward direction, the maximum thermal load region in the furnace 18 shifts to the lower side, thermal absorption of the furnace thereby increases, an exhaust gas temperature at an outlet of the furnace 18 can be reduced, a detention time of an NOx reduction region in the furnace 18 between the burner 19 and an after-air port 24 can be increased beyond than that in a case where a combustion region is evenly formed on each of upper and lower sides of the burner 19 by shifting the combustion region of the burner 19 to the lower side, thus providing the pulverized coal burner 19 that can reduce the NOx concentration.
[0052]
This embodiment provides a configuration where a second damper 17 as a supply air capacity adjuster for each burner 19, which is configured to adjust a flow rate of combustion air flowing into each burner 19, is provided on the upstream side of a damper 15 in addition to the configurations of Embodiments 1 to 3.
Since a distribution can appear in a fuel supplied to a plurality of burners 19 arranged on a boiler furnace wall 10, it is desirable to enable adjusting a combustion air flow rate in accordance with each burner 19 so that a combustion air flow CA 02827903 2013-,08-21 rate consistent with a fuel supply amount can be obtained.
Here, although the combustion air flow rate can be adjusted by a first damper 15 alone if its opening degree is adjusted in accordance with each burner 19, when the first damper 15 provided for the purpose of deviating a momentum of the combustion air on each of upper and lower sides of each burner 19 has a function of adjusting the combustion air flow rate consistent with the fuel supply amount, controlling this damper becomes difficult.
Thus, in this embodiment, the first damper 15 and the second damper 17 that share the two different functions are independently provided.
Each of FIG. 16 and FIG. 17 shows a configuration where, in addition to first dampers 15a and 15b configured to deviate an air momentum on each of upper and lower sides of the burner 19 described in Embodiment 1 (FIGS. 4 and 5), second dampers 17a and 17b for adjusting a flow rate of the combustion air flowing into each burner 19 are provided on the upstream side of the first dampers 15a and 15b.
As described above, for example, when the upper first damper 15a in the first dampers 15a and 15b that deviate the momentum of the combustion air depending on each of the upper and lower sides of each burner 19 is closed and the lower first damper 15b is opened, an injection amount of the combustion air on the lower side of the burner 19 increases, and an increase in the momentum of the combustion air flowing toward the lower side of the burner 19 enables deflecting flames in a furnace CA 02827903 2013-,08-21 18 to a downward direction (see FIG. 3(b)).
When the second dampers 17a and 17b are provided on the upstream side of the first dampers 15a and 15b, the flow rate of the combustion air flowing into each burner 19 can be individually adjusted without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
Providing the first dampers 15a and 15b, which are adjusters that deviate the momentum of the combustion air on each of the upper and lower sides of each burner 19 in each wind box 12, on the downstream side of the second dampers 17a and 17b can suffice, and the second dampers 17a and 17b can be arranged at any positions.
Furthermore, as each of the first dampers 15a and 15b and the second dampers 17a and 17b, a member that adjusts an opening area by sliding a plurality of laminated porous plates may be used in place of the illustrated butterfly type damper, and it can have any structure as long as it has a gas flow rate adjusting function.
This embodiment provides a configuration where a second damper 17 as a supply air capacity adjuster for each burner 19, which is configured to adjust a flow rate of combustion air flowing into each burner 19, is provided on the upstream side of a damper 15 in addition to the configurations of Embodiments 1 to 3.
Since a distribution can appear in a fuel supplied to a plurality of burners 19 arranged on a boiler furnace wall 10, it is desirable to enable adjusting a combustion air flow rate in accordance with each burner 19 so that a combustion air flow CA 02827903 2013-,08-21 rate consistent with a fuel supply amount can be obtained.
Here, although the combustion air flow rate can be adjusted by a first damper 15 alone if its opening degree is adjusted in accordance with each burner 19, when the first damper 15 provided for the purpose of deviating a momentum of the combustion air on each of upper and lower sides of each burner 19 has a function of adjusting the combustion air flow rate consistent with the fuel supply amount, controlling this damper becomes difficult.
Thus, in this embodiment, the first damper 15 and the second damper 17 that share the two different functions are independently provided.
Each of FIG. 16 and FIG. 17 shows a configuration where, in addition to first dampers 15a and 15b configured to deviate an air momentum on each of upper and lower sides of the burner 19 described in Embodiment 1 (FIGS. 4 and 5), second dampers 17a and 17b for adjusting a flow rate of the combustion air flowing into each burner 19 are provided on the upstream side of the first dampers 15a and 15b.
As described above, for example, when the upper first damper 15a in the first dampers 15a and 15b that deviate the momentum of the combustion air depending on each of the upper and lower sides of each burner 19 is closed and the lower first damper 15b is opened, an injection amount of the combustion air on the lower side of the burner 19 increases, and an increase in the momentum of the combustion air flowing toward the lower side of the burner 19 enables deflecting flames in a furnace CA 02827903 2013-,08-21 18 to a downward direction (see FIG. 3(b)).
When the second dampers 17a and 17b are provided on the upstream side of the first dampers 15a and 15b, the flow rate of the combustion air flowing into each burner 19 can be individually adjusted without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
Providing the first dampers 15a and 15b, which are adjusters that deviate the momentum of the combustion air on each of the upper and lower sides of each burner 19 in each wind box 12, on the downstream side of the second dampers 17a and 17b can suffice, and the second dampers 17a and 17b can be arranged at any positions.
Furthermore, as each of the first dampers 15a and 15b and the second dampers 17a and 17b, a member that adjusts an opening area by sliding a plurality of laminated porous plates may be used in place of the illustrated butterfly type damper, and it can have any structure as long as it has a gas flow rate adjusting function.
[0053]
In this embodiment, such a secondary air nozzle 8 having the guide sleeve 13 as shown in FIG. 2 is provided in the wind box 12, and the combustion air is injected into the furnace 18 from the outlet of the burner 19 in a spreading manner. The opening portion 8a is provided in the secondary air nozzle 8, and it is desirable to provide the slide type damper 9 that can adjust an air capacity flowing into the secondary air nozzle =
8.
For example, when the upper first damper 15a in the wind box 12 shown in FIG. 16 is closed and the lower first damper 15b in the same is opened to increase an injection amount of the combustion air on the lower side of the burner 19, the combustion air can be prevented from flowing into the tertiary air nozzle 11 on the upper side in the wind box 12 by fully closing the opening portion 8a of the secondary air nozzle 8 provided on the upper side in the wind box 12 with use of the slide type damper 9a, and the momentum of the combustion air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction of the burner 19, thereby holding the flame stabilizing properties.
When the first dampers 15a and 15b and the slide type damper 9a are operated and the momentum of the tertiary air on each of the upper and lower sides of the burner 19 is deviated while maintaining the flame stabilizing properties of the burner 19, flames in the furnace 18 can be deflected.
In this embodiment, such a secondary air nozzle 8 having the guide sleeve 13 as shown in FIG. 2 is provided in the wind box 12, and the combustion air is injected into the furnace 18 from the outlet of the burner 19 in a spreading manner. The opening portion 8a is provided in the secondary air nozzle 8, and it is desirable to provide the slide type damper 9 that can adjust an air capacity flowing into the secondary air nozzle =
8.
For example, when the upper first damper 15a in the wind box 12 shown in FIG. 16 is closed and the lower first damper 15b in the same is opened to increase an injection amount of the combustion air on the lower side of the burner 19, the combustion air can be prevented from flowing into the tertiary air nozzle 11 on the upper side in the wind box 12 by fully closing the opening portion 8a of the secondary air nozzle 8 provided on the upper side in the wind box 12 with use of the slide type damper 9a, and the momentum of the combustion air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction of the burner 19, thereby holding the flame stabilizing properties.
When the first dampers 15a and 15b and the slide type damper 9a are operated and the momentum of the tertiary air on each of the upper and lower sides of the burner 19 is deviated while maintaining the flame stabilizing properties of the burner 19, flames in the furnace 18 can be deflected.
[0054]
According to these structures and the operating method, the damper adjustment method for dividing each of the combustion air inlet openings 12a and 12b in the wind box 12 into two parts and providing the first dampers 15aa, 15ab, 15ba, and 15bb and the second dampers 17aa, 17ab, 17ba, and 17bb to the respective combustion air inlet openings 12a and 12b as shown in FIG. 17 enables individually adjusting the flow rate of the combustion air flowing into each burner 19 without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
According to these structures and the operating method, the damper adjustment method for dividing each of the combustion air inlet openings 12a and 12b in the wind box 12 into two parts and providing the first dampers 15aa, 15ab, 15ba, and 15bb and the second dampers 17aa, 17ab, 17ba, and 17bb to the respective combustion air inlet openings 12a and 12b as shown in FIG. 17 enables individually adjusting the flow rate of the combustion air flowing into each burner 19 without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
[0055]
In this embodiment, as shown in FIG. 18, the burners 19 each having the wind box 12 are arranged in the duct 16. An air capacity of each of the plurality of burners 19 arranged on the furnace wall 10 along the horizontal direction in line can be adjusted by providing the second dampers 17 (17a, 17b and 17aa, 17ab; and 17ba, 17bb) shown in FIG. 16 and FIG. 17 in each wind box 12.
Moreover, as shown in FIG. 19, the burners 19 each having the wind box 12 shown in FIG. 16 and FIG. 17 may be installed on the outer side of the furnace wall 10 of the boiler so that the combustion air from the outside of the furnace 18 can be supplied into the burners 19 each having the wind box 12 through the duct 16.
INDUSTRIAL APPLICABILITY
In this embodiment, as shown in FIG. 18, the burners 19 each having the wind box 12 are arranged in the duct 16. An air capacity of each of the plurality of burners 19 arranged on the furnace wall 10 along the horizontal direction in line can be adjusted by providing the second dampers 17 (17a, 17b and 17aa, 17ab; and 17ba, 17bb) shown in FIG. 16 and FIG. 17 in each wind box 12.
Moreover, as shown in FIG. 19, the burners 19 each having the wind box 12 shown in FIG. 16 and FIG. 17 may be installed on the outer side of the furnace wall 10 of the boiler so that the combustion air from the outside of the furnace 18 can be supplied into the burners 19 each having the wind box 12 through the duct 16.
INDUSTRIAL APPLICABILITY
[0056]
According to the present invention, when the flame deflection and heat absorption control function and the combustion gas flow rate adjustment function for each burner 19 are additionally provided, the industrial applicability can be further enhanced.
DESCRIPTION OF THE REFERENCE NUMERALS
According to the present invention, when the flame deflection and heat absorption control function and the combustion gas flow rate adjustment function for each burner 19 are additionally provided, the industrial applicability can be further enhanced.
DESCRIPTION OF THE REFERENCE NUMERALS
[0057]
1 gas-particle flow 2 combustion air 3 fuel nozzle 4 flame stabilizer pulverized coal concentrator 6 venturi tube 7 heavy oil nozzle 8 secondary air nozzle 9 slide type damper boiler furnace wall 11 tertiary air nozzle 12 wind box 13 guide sleeve 14 partition wall (15a, 15aa, 15ab, 15b, 15ba, 15bb) damper (first flow rate adjusting means) 16 duct 17 (17a, 17aa, 17ab, 17b, 17ba, 17bb) damper (second flow rate adjusting means) 18 boiler furnace 19 burner bunker 21 mill 23 blower 24 after-air port blower
1 gas-particle flow 2 combustion air 3 fuel nozzle 4 flame stabilizer pulverized coal concentrator 6 venturi tube 7 heavy oil nozzle 8 secondary air nozzle 9 slide type damper boiler furnace wall 11 tertiary air nozzle 12 wind box 13 guide sleeve 14 partition wall (15a, 15aa, 15ab, 15b, 15ba, 15bb) damper (first flow rate adjusting means) 16 duct 17 (17a, 17aa, 17ab, 17b, 17ba, 17bb) damper (second flow rate adjusting means) 18 boiler furnace 19 burner bunker 21 mill 23 blower 24 after-air port blower
Claims (4)
1. A combustion device comprising a plurality of burners arranged on a furnace wall of a furnace, each burner comprising:
a cylindrical fuel nozzle that injects a mixture of a fuel and a carrier gas therefor into the furnace; one or more cylindrical combustion gas nozzles that are provided on the outer circumference of the fuel nozzle and inject a combustion gas into the furnace; and a wind box that supplies the combustion gas to the combustion gas nozzles, wherein the wind box has a combustion gas inflow opening portion into which the combustion gas flows from one direction vertical to the axial direction of the burner and is partitioned to form a plurality of parallel flow paths through which the combustion gas flows in from the combustion gas inflow opening portion, some of the plurality of flow paths are connected to an upper side of the combustion gas nozzles, the other flow paths are connected to a lower side of the combustion gas nozzles, and first flow rate adjusting means for adjusting a flow rate of the combustion gas is independently provided to each of the plurality of flow paths.
a cylindrical fuel nozzle that injects a mixture of a fuel and a carrier gas therefor into the furnace; one or more cylindrical combustion gas nozzles that are provided on the outer circumference of the fuel nozzle and inject a combustion gas into the furnace; and a wind box that supplies the combustion gas to the combustion gas nozzles, wherein the wind box has a combustion gas inflow opening portion into which the combustion gas flows from one direction vertical to the axial direction of the burner and is partitioned to form a plurality of parallel flow paths through which the combustion gas flows in from the combustion gas inflow opening portion, some of the plurality of flow paths are connected to an upper side of the combustion gas nozzles, the other flow paths are connected to a lower side of the combustion gas nozzles, and first flow rate adjusting means for adjusting a flow rate of the combustion gas is independently provided to each of the plurality of flow paths.
2. The combustion device according to claim 1, wherein one duct through which the combustion gas is supplied to the plurality of wind boxes from the outside of the furnace is installed on the outer side of the furnace wall on which the wind boxes are installed.
3. The combustion device according to claim 1 or claim 2, wherein the plurality of wind boxes are aligned and installed inside or outside the one duct.
4. The combustion device according to any one of claims 1 to 3, wherein second flow rate adjusting means for adjusting a flow rate of the combustion gas that flows into each burner on the upstream side of the first flow rate adjusting means is provided in each wind box.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/JP2011/000976 WO2012114370A1 (en) | 2011-02-22 | 2011-02-22 | Combustion device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2827903A1 true CA2827903A1 (en) | 2012-08-30 |
| CA2827903C CA2827903C (en) | 2016-07-12 |
Family
ID=46720199
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2827903A Active CA2827903C (en) | 2011-02-22 | 2011-02-22 | Combustion device |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US20130340659A1 (en) |
| EP (1) | EP2679899B1 (en) |
| JP (1) | JP5743115B2 (en) |
| KR (1) | KR101582729B1 (en) |
| AU (1) | AU2011360560B2 (en) |
| CA (1) | CA2827903C (en) |
| PL (1) | PL2679899T3 (en) |
| WO (1) | WO2012114370A1 (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10375901B2 (en) | 2014-12-09 | 2019-08-13 | Mtd Products Inc | Blower/vacuum |
| CN105202568B (en) * | 2015-10-14 | 2017-05-10 | 北京高能时代环境技术股份有限公司 | Secondary air device of domestic waste grate furnace |
| CN108087867A (en) * | 2018-01-11 | 2018-05-29 | 西安热工研究院有限公司 | It is a kind of to be used to balance underload nitrogen oxides and the low nitrogen burning system and method for carbonated drink parameter |
| CN109185872B (en) * | 2018-10-17 | 2023-09-19 | 烟台龙源电力技术股份有限公司 | Secondary air system of boiler |
| CN109185871B (en) * | 2018-10-17 | 2023-09-15 | 烟台龙源电力技术股份有限公司 | Secondary air system of boiler |
| JP7141574B1 (en) * | 2021-08-10 | 2022-09-26 | コロナ株式会社 | Blower burner device |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS543924A (en) * | 1977-06-09 | 1979-01-12 | Kobe Steel Ltd | Combustion method and system for small nitrogen oxide production |
| US4551090A (en) * | 1980-08-25 | 1985-11-05 | L. & C. Steinmuller Gmbh | Burner |
| JPS61101226U (en) * | 1984-12-04 | 1986-06-27 | ||
| JPH0729335B2 (en) * | 1989-04-24 | 1995-04-05 | キタノ製作株式会社 | Molding method and mold for handle such as toothbrush |
| JP3054420B2 (en) * | 1989-05-26 | 2000-06-19 | 株式会社東芝 | Gas turbine combustor |
| JPH0543924A (en) * | 1991-08-15 | 1993-02-23 | Kobe Steel Ltd | Secondary combustion blow-refining method |
| JPH0735302A (en) * | 1993-07-22 | 1995-02-07 | Ishikawajima Harima Heavy Ind Co Ltd | Method for warming always mill of coal fired boiler |
| JPH09101015A (en) * | 1995-10-03 | 1997-04-15 | Babcock Hitachi Kk | Combustion device and adhered slag removing device thereof |
| JPH09133345A (en) * | 1995-11-06 | 1997-05-20 | Mitsubishi Heavy Ind Ltd | Burner |
| JP3009370B2 (en) * | 1997-03-07 | 2000-02-14 | 株式会社日立製作所 | Pulverized coal burner, pulverized coal boiler and pulverized coal combustion method |
| JP4301422B2 (en) * | 2000-11-07 | 2009-07-22 | バブコック日立株式会社 | Combustion burner, combustion apparatus equipped with the burner, and combustion method using the burner |
| US6699031B2 (en) * | 2001-01-11 | 2004-03-02 | Praxair Technology, Inc. | NOx reduction in combustion with concentrated coal streams and oxygen injection |
| JP2003254510A (en) * | 2002-02-28 | 2003-09-10 | Babcock Hitachi Kk | Combustor and wind box |
| JP4898393B2 (en) | 2006-11-09 | 2012-03-14 | 三菱重工業株式会社 | Burner structure |
| JP4969464B2 (en) * | 2008-01-08 | 2012-07-04 | 三菱重工業株式会社 | Burner structure |
| BRPI0911632A2 (en) * | 2008-04-10 | 2015-10-13 | Babcock Hitachi Kabushiku Kaisha | solid fuel burner combustion apparatus using solid fuel burner and method for operating combustion apparatus |
| JP5344897B2 (en) * | 2008-12-12 | 2013-11-20 | 三菱重工業株式会社 | Swirl combustion boiler |
| JP2010249362A (en) * | 2009-04-13 | 2010-11-04 | Ihi Corp | Burner |
| JP2011033287A (en) * | 2009-08-04 | 2011-02-17 | Mitsubishi Heavy Ind Ltd | Pulverized coal burner |
| US20130291770A1 (en) * | 2011-01-21 | 2013-11-07 | Babcock-Hitachi Kabushiki Kaisha | Solid fuel burner and combustion device using same |
-
2011
- 2011-02-22 KR KR1020137024829A patent/KR101582729B1/en active IP Right Grant
- 2011-02-22 US US13/981,485 patent/US20130340659A1/en not_active Abandoned
- 2011-02-22 EP EP11859242.7A patent/EP2679899B1/en active Active
- 2011-02-22 AU AU2011360560A patent/AU2011360560B2/en active Active
- 2011-02-22 JP JP2013500663A patent/JP5743115B2/en active Active
- 2011-02-22 PL PL11859242T patent/PL2679899T3/en unknown
- 2011-02-22 CA CA2827903A patent/CA2827903C/en active Active
- 2011-02-22 WO PCT/JP2011/000976 patent/WO2012114370A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| KR101582729B1 (en) | 2016-01-05 |
| CA2827903C (en) | 2016-07-12 |
| EP2679899A4 (en) | 2018-01-24 |
| JP5743115B2 (en) | 2015-07-01 |
| AU2011360560B2 (en) | 2015-11-05 |
| EP2679899A1 (en) | 2014-01-01 |
| JPWO2012114370A1 (en) | 2014-07-07 |
| KR20140008407A (en) | 2014-01-21 |
| US20130340659A1 (en) | 2013-12-26 |
| EP2679899B1 (en) | 2021-04-07 |
| WO2012114370A1 (en) | 2012-08-30 |
| PL2679899T3 (en) | 2021-07-05 |
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Effective date: 20151023 |