WO2016158081A1 - 燃焼バーナ及びこれを備えたボイラ - Google Patents
燃焼バーナ及びこれを備えたボイラ Download PDFInfo
- Publication number
- WO2016158081A1 WO2016158081A1 PCT/JP2016/055008 JP2016055008W WO2016158081A1 WO 2016158081 A1 WO2016158081 A1 WO 2016158081A1 JP 2016055008 W JP2016055008 W JP 2016055008W WO 2016158081 A1 WO2016158081 A1 WO 2016158081A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- combustion burner
- nozzle
- fuel
- fuel gas
- combustion
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 307
- 239000002737 fuel gas Substances 0.000 claims abstract description 178
- 239000000446 fuel Substances 0.000 claims abstract description 149
- 238000005192 partition Methods 0.000 claims abstract description 53
- 239000003381 stabilizer Substances 0.000 claims abstract description 9
- 238000011144 upstream manufacturing Methods 0.000 claims description 36
- 239000000567 combustion gas Substances 0.000 claims description 13
- 230000007423 decrease Effects 0.000 claims description 8
- 238000007664 blowing Methods 0.000 claims description 7
- 239000000203 mixture Substances 0.000 abstract description 16
- 239000003245 coal Substances 0.000 description 45
- 239000007789 gas Substances 0.000 description 17
- 230000002093 peripheral effect Effects 0.000 description 12
- 229910052760 oxygen Inorganic materials 0.000 description 11
- 239000001301 oxygen Substances 0.000 description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical group [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 9
- 239000004449 solid propellant Substances 0.000 description 9
- 230000004048 modification Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 238000013459 approach Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010298 pulverizing process Methods 0.000 description 4
- 230000009467 reduction Effects 0.000 description 4
- 239000002028 Biomass Substances 0.000 description 3
- 238000009841 combustion method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 238000000638 solvent extraction Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 238000006477 desulfuration reaction Methods 0.000 description 1
- 230000023556 desulfurization Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 239000012717 electrostatic precipitator Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000002006 petroleum coke Substances 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D1/00—Burners for combustion of pulverulent fuel
- F23D1/04—Burners producing cylindrical flames without centrifugal action
-
- 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
- F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
- F23C5/08—Disposition of burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
- F22B9/00—Steam boilers of fire-tube type, i.e. the flue gas from a combustion chamber outside the boiler body flowing through tubes built-in in the boiler body
-
- 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
- F23C99/00—Subject-matter not provided for in other groups of this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D1/00—Burners for combustion of pulverulent fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2201/00—Burners adapted for particulate solid or pulverulent fuels
- F23D2201/10—Nozzle tips
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2201/00—Burners adapted for particulate solid or pulverulent fuels
- F23D2201/20—Fuel flow guiding devices
Definitions
- the present invention relates to a combustion burner applied to a boiler for generating steam for power generation or factory use, and a boiler equipped with the combustion burner.
- a conventional pulverized coal fired boiler has a furnace having a hollow shape and installed in the vertical direction, and a plurality of combustion burners are disposed on the furnace wall along the circumferential direction, and a plurality of combustion burners are provided in the vertical direction. It is arranged over the steps.
- This combustion burner is supplied with a mixture of pulverized coal (fuel) obtained by pulverizing coal and primary air (air), and also supplied with high-temperature combustion burner air (Coal secondary air).
- a flame is formed by blowing air for the combustion burner into the furnace, and combustion is possible in the furnace.
- the furnace has a flue connected to the upper part, and a heat exchanger such as a superheater, a reheater, and a economizer for recovering the heat of the exhaust gas is provided in the flue. Heat exchange is performed between the exhaust gas generated by the combustion and water, and steam can be generated.
- a heat exchanger such as a superheater, a reheater, and a economizer for recovering the heat of the exhaust gas is provided in the flue. Heat exchange is performed between the exhaust gas generated by the combustion and water, and steam can be generated.
- Patent Document 1 As a combustion burner of such a pulverized coal fired boiler, for example, there is one described in Patent Document 1 below.
- a fuel nozzle that injects a fuel gas mixed with solid fuel and primary air
- a combustion burner air nozzle that injects combustion burner air from the outer periphery of the fuel nozzle
- an opening of the fuel nozzle A combustion burner with a flame holder arranged is described.
- the flame holder for a combustion burner described in Patent Document 1 has a structure that substantially crosses the opening of the fuel nozzle and has a split shape that branches the fuel gas in the flow direction of the fuel gas, and the fuel nozzle and the combustion burner.
- the air nozzle has a structure for injecting the fuel gas and the combustion burner air as a straight flow, and a plurality of flame stabilizers are connected to each other, and the intersection is a central region of the opening of the fuel nozzle. It is placed in the position.
- the combustion burner like the device described in Patent Document 1, provides a flame holder inside the combustion nozzle, thereby realizing internal ignition of fuel gas in which solid fuel and air are mixed to reduce the amount of NOx generated. Can be possible.
- the combustion burner described in Patent Document 1 has a problem that a large amount of NOx is generated because the fuel gas and the combustion burner air are ignited (so-called external ignition) to form a high-temperature high-oxygen region.
- a flame holder is provided inside the combustion nozzle as in Patent Document 1, in the case of a solid fuel such as pulverized coal, the combustion speed is slower than that of a gas fuel, and there is a risk that a flame will blow out. Therefore, stable ignition with a flame holder becomes relatively difficult. Therefore, it is desirable to obtain stable ignition by lowering the flow rate of the fuel gas to approach the combustion speed.
- the present invention solves the above-described problems, and lowers the flow rate of the fuel gas in which fuel and air are mixed so as to approach the combustion speed, thereby realizing stable ignition and reducing the amount of NOx generated. It aims at providing a combustion burner and a boiler provided with the same.
- a combustion burner for achieving the above object is provided with a fuel nozzle capable of injecting a fuel gas mixed with fuel and air, and an axial center side in the vicinity of the tip of the fuel nozzle. At least one flame stabilizer, and a partition member that partitions an inner flow path in which the flame stabilizer is disposed and an outer flow path outside the inner flow path in the fuel nozzle, and the partition member The flow path cross-sectional area of the partitioned inner flow path expands in the fuel gas flow direction.
- a partition member is provided in the fuel nozzle to partition the inner flow path in which the flame stabilizer is disposed and the outer flow path outside the inner flow path, and the flow path cross-sectional area of the inner flow path is determined by the partition member. Since the expansion is made in the flow direction, the flow rate of the fuel gas in the inner flow path can be reduced. Thereby, since the blow-off of the flame can be suppressed by bringing the flow rate of the fuel gas close to the combustion speed, more stable flame holding becomes possible. Therefore, by strengthening the internal flame holding which is held on the inner side which is the central axis side of the combustion burner, a high temperature and high oxygen region which can occur on the outer peripheral side of the fuel nozzle can be suppressed, and NOx can be reduced.
- the partition member is a cylindrical member.
- the inner channel and the outer channel are partitioned by the cylindrical member.
- the cross-sectional shape orthogonal to the fuel gas flow of the cylindrical member is arbitrary, but for example, a polygon such as a quadrangle, a circle, an ellipse, or an oval is used.
- the partition member has two plate-like bodies extending with a space therebetween with the flame holder interposed therebetween, and each of the plate-like bodies is a fuel. It is connected with respect to the wall surface which divides the outer periphery of a nozzle.
- the partition member has two plate-like bodies, and these plate-like bodies are connected to the wall surface defining the outer periphery of the fuel nozzle. As a result, an inner flow path surrounded by the two plate-like bodies and the wall surface of the fuel nozzle is formed.
- the combustion burner according to one aspect of the present invention includes a combustion burner air nozzle for supplying air from the outside of the fuel nozzle, and the flow path cross-sectional area of the outer flow path partitioned by the partition member is a fuel gas. It decreases in the flow direction.
- the outer flow path typically means a flow path between the partition member and the inner wall of the fuel nozzle (in some cases, the inner wall of the combustion burner air nozzle also serves as the inner wall of the fuel nozzle). To do.
- the partition member has an inclination angle that is an angle formed with a direction parallel to the flow direction of the fuel gas as it goes toward the front end side. It is characterized by being smaller than the part.
- the inclination angle formed by the direction parallel to the flow direction of the fuel gas becomes smaller with respect to the upstream end portion in the flow direction of the fuel gas as it goes to the front end side. Therefore, the flow rate of the fuel gas can be effectively reduced.
- the inner wall surface of the partition member is provided with a guide surface that is inclined toward the axial center side of the fuel nozzle as it goes in the fuel gas flow direction.
- the fuel gas that has flowed along the inner wall surface of the partition member is removed. It can be directed to the mind side, and internal ignition can be further strengthened.
- the area of the surface surrounded by the outer surface of the combustion burner air nozzle is larger than the upstream end of the fuel gas in the flow direction. It is characterized by being smaller.
- the combustion burner according to an aspect of the present invention further includes a guide member that is disposed upstream of the partition member of the fuel nozzle and guides the fuel gas flowing through the fuel nozzle to the axial center side. It is said. Accordingly, the guide member can move the solid fuel flowing through the fuel nozzle to the axial center side of the nozzle, and can supply a fuel gas with a high concentration of the solid fuel into the cylindrical member. Can be high.
- the combustion burner according to one aspect of the present invention further includes a secondary air nozzle capable of blowing air from the outside of the combustion burner air nozzle, and the secondary air nozzle has a tip on the axial center side.
- the secondary air flowing in the secondary air nozzle is discharged away in a direction leading away from the air blown by the combustion burner air nozzle. It is characterized by that. Therefore, the combustion burner air can be sucked away from the axis by the secondary air nozzle, and ignition at the boundary between the combustion burner air and the fuel gas can be suppressed.
- the flame holder is provided with two first flame holding members that are parallel to each other in the vertical direction along the horizontal direction and in the horizontal direction along the vertical direction. It is characterized by a structure in which two second flame holding members that are parallel to each other with a predetermined gap are arranged to intersect each other.
- the flame holder is provided on the upstream side of the fuel gas flow, on the upstream side of the fuel gas flow, and on the downstream side of the fuel gas with respect to the upstream side of the flame holding member. And a provided downstream flame holding member.
- the cross-sectional area of the flow passage narrowed by the flame-holding member occupying can be made as small as possible. Thereby, the acceleration of the fuel gas flowing through the inner flow path can be suppressed, and the internal ignition can be enhanced by bringing the flow rate of the fuel gas flowing through the inner flow path close to the combustion speed.
- the combustion burner according to one aspect of the present invention is characterized in that the flame holder has a widened portion on the downstream side in the fuel gas flow direction.
- a boiler according to an aspect of the present invention includes a furnace, the above-described combustion burner installed for the furnace, and a heat exchanger that exchanges heat with the combustion gas from the combustion burner on the downstream side of the furnace. And.
- the flow passage cross-sectional area of the inner flow passage is expanded in the fuel gas flow direction by the partition member, the flow velocity of the fuel gas flowing through the inner flow passage is reduced, and the flow velocity of the combustion gas is made closer to the combustion speed.
- Stable ignition in the flame holder can be realized by suppressing the blow-off of the flame. Thereby, the internal flame holding which holds the flame inside the combustion burner is strengthened, and the reduction by the combustion under the oxygen shortage is effectively performed, so that NOx can be reduced.
- FIG. 1 is a longitudinal sectional view illustrating a combustion burner of Example 1.
- FIG. It is a schematic block diagram showing the pulverized coal burning boiler to which the combustion burner of Example 1 was applied.
- 1 is a plan view showing a combustion burner in a pulverized coal burning boiler of Example 1.
- FIG. It is sectional drawing showing the combustion burner which concerns on Example 2 of this invention.
- FIG. 6 is a cross-sectional view showing a modification of Example 2. It is sectional drawing showing the combustion burner which concerns on Example 3 of this invention. It is sectional drawing showing the combustion burner which concerns on Example 4 of this invention. It is sectional drawing showing the combustion burner which concerns on Example 5 of this invention.
- FIG. 6 is a front view of a combustion burner according to Embodiment 5.
- FIG. It is a front view of the combustion burner of a modification. It is sectional drawing which planarly viewed the fuel nozzle of the combustion burner which concerns on Example 6 of this invention.
- 10 is a front view of a combustion nozzle of Example 6.
- FIG. 10 is a cross-sectional view of a fuel nozzle of a circular combustion burner as a modification of Example 6 when viewed from above.
- It is sectional drawing which planarly viewed the fuel nozzle of Example 7 of this invention.
- It is a front view of the fuel nozzle of FIG. It is a sectional side view of the fuel nozzle of FIG.
- FIG. 1 is a front view showing a combustion burner according to a first embodiment of the present invention
- FIG. 2 is a longitudinal sectional view showing the combustion burner of the first embodiment
- FIG. 3 is a fine powder to which the combustion burner of the first embodiment is applied.
- FIG. 4 is a schematic configuration diagram showing a charcoal-fired boiler
- FIG. 4 is a plan view showing a combustion burner in the pulverized coal-fired boiler of the first embodiment.
- the pulverized coal fired boiler to which the combustion burner of Example 1 is applied can use the pulverized coal obtained by pulverizing coal as a solid fuel, burn the pulverized coal with the combustion burner, and recover the heat generated by the combustion. Boiler.
- the pulverized coal burning boiler 10 is a conventional boiler, and includes a furnace 11, a combustion device 12, and a flue 13.
- the furnace 11 has a rectangular hollow shape and is installed along the vertical direction.
- a combustion device 12 is provided at the lower part of the furnace wall constituting the furnace 11.
- the combustion apparatus 12 has a plurality of combustion burners 21, 22, 23, 24, and 25 attached to the furnace wall.
- the combustion burners 21, 22, 23, 24, and 25 are arranged as four sets at equal intervals along the circumferential direction, and 5 sets along the vertical direction. Five stages are arranged.
- Each combustion burner 21, 22, 23, 24, 25 is connected to a pulverized coal machine (mill) 31, 32, 33, 34, 35 via a pulverized coal supply pipe 26, 27, 28, 29, 30. ing.
- the pulverized coal machines 31, 32, 33, 34, and 35 are supported in a housing so that the pulverization table can be driven to rotate with a rotation axis along the vertical direction, and face the upper side of the pulverization table.
- a plurality of crushing rollers are configured to be rotatably supported in conjunction with the rotation of the crushing table.
- the pulverized coal pulverized to a predetermined size and classified by carrier air (air) is supplied to the pulverized coal supply pipes 26, 27, 28. , 29, 30 are supplied to the combustion burners 21, 22, 23, 24, 25.
- the furnace 11 is provided with a wind box 36 at the mounting position of each combustion burner 21, 22, 23, 24, 25, and one end portion of an air duct 37 is connected to the wind box 36, and this air A blower 38 is attached to the duct 37 at the other end. Further, the furnace 11 is provided with an additional air nozzle 39 above the mounting position of each combustion burner 21, 22, 23, 24, 25. A branched air duct 40 branched from the air duct 37 to the additional air nozzle 39. The ends of are connected. Accordingly, the combustion air (combustion burner air (fuel gas combustion air), secondary air) sent by the blower 38 is supplied from the air duct 37 to the wind box 36, and each combustion burner 21 is supplied from the wind box 36. , 22, 23, 24, 25, and combustion air (additional air) sent by the blower 38 can be supplied from the branch air duct 40 to the additional air nozzle 39.
- combustion air combustion burner air (fuel gas combustion air), secondary air
- each combustion burner 21, 22, 23, 24, 25 can inject a pulverized fuel mixture (fuel gas) obtained by mixing pulverized coal and air into the furnace 11 and burn it. Burner air and secondary air can be blown into the furnace 11, and a flame can be formed by igniting the pulverized fuel mixture with an ignition torch (not shown).
- each combustion burner 21, 22, 23, 24, 25 injects oil fuel into the furnace 11 to form a flame.
- the air for combustion burners is supplied from this oil burning burner at the time of normal operation.
- the furnace 11 has a flue 13 connected to the upper portion thereof, and superheaters (super heaters) 41 and 42 which are heat exchangers for recovering heat of exhaust gas as a convection heat transfer section are connected to the flue 13.
- superheaters (super heaters) 41 and 42 which are heat exchangers for recovering heat of exhaust gas as a convection heat transfer section are connected to the flue 13.
- Heaters 43, 44 and economizers 45, 46, 47 are provided, and heat exchange is performed between the exhaust gas generated by combustion in the furnace 11 and water.
- the flue 13 is connected to an exhaust gas pipe 48 through which exhaust gas subjected to heat exchange is discharged downstream.
- This exhaust gas pipe 48 is provided with an air heater 49 between the air duct 37 and performs heat exchange between the air flowing through the air duct 37 and the exhaust gas flowing through the exhaust gas pipe 48, and the combustion burners 21, 22, 23, The temperature of the combustion air supplied to 24 and 25 can be raised.
- the exhaust gas pipe 48 is provided with a denitration device, an electrostatic precipitator, an induction blower, and a desulfurization device, and a chimney is provided at the downstream end.
- the generated pulverized coal together with the conveying air passes through the pulverized coal supply pipes 26, 27, 28, 29, and 30 and the combustion burners 21, 22, 23, 24, 25.
- the heated combustion air is supplied from the air duct 37 to the combustion burners 21, 22, 23, 24, and 25 through the wind box 36, and is supplied from the branch air duct 40 to the additional air nozzle 39.
- the combustion burners 21, 22, 23, 24, and 25 blow the pulverized fuel mixture mixed with the pulverized coal and the carrier air into the furnace 11 and blow the combustion air into the furnace 11 and ignite at this time. Can form a flame.
- the additional air nozzle 39 can perform combustion control by blowing additional air into the furnace 11.
- the pulverized fuel mixture and the combustion air are burned to generate a flame.
- the combustion gas exhaust gas
- the combustion burners 21, 22, 23, 24, and 25 are combusted by injecting pulverized coal mixture and combustion air (combustion burner air / secondary air) into the combustion region in the furnace 11 and igniting at this time.
- a flame swirl is formed in the region. This flame swirl rises while swirling and reaches the reduction region.
- the additional air nozzle 39 blows additional air above the reduction region in the furnace 11.
- the interior is maintained in a reducing atmosphere by setting the air supply amount to be less than the theoretical air amount with respect to the pulverized coal supply amount.
- the NOx generated by the combustion of the pulverized coal is reduced in the furnace 11, and then additional air (additional air) is supplied to complete the oxidation combustion of the pulverized coal, and the amount of NOx generated by the combustion of the pulverized coal is reduced. Reduced.
- the exhaust gas that has passed through the economizers 45, 46, and 47 of the flue 13 is subjected to removal of harmful substances such as NOx by a catalyst in a denitration device (not shown) in the exhaust gas pipe 48, and the particulate matter is collected by an electric dust collector. Is removed, and after the sulfur content is removed by the desulfurizer, it is discharged from the chimney into the atmosphere.
- combustion apparatus 12 since each combustion burner 21, 22, 23, 24, 25 which comprises this combustion apparatus 12 has comprised the substantially the same structure, it is located in the uppermost stage. Only the combustion burner 21 will be described.
- the combustion burner 21 includes combustion burners 21 a, 21 b, 21 c, and 21 d provided on four wall surfaces in the furnace 11.
- Each combustion burner 21a, 21b, 21c, 21d is connected to each branch pipe 26a, 26b, 26c, 26d branched from the pulverized coal supply pipe 26, and each branch pipe 37a, 37b, 37c branched from the air duct 37. , 37d are connected.
- each combustion burner 21a, 21b, 21c, 21d on each wall surface of the furnace 11 blows into the furnace 11 a pulverized fuel mixture in which pulverized coal and carrier air are mixed, and the pulverized fuel mixture Blow combustion air to the outside. Then, by igniting the pulverized fuel mixture from each combustion burner 21a, 21b, 21c, 21d, four flames F1, F2, F3, F4 can be formed, and this flame F1, F2, F3, F4. Is a flame swirl flow swirling counterclockwise as viewed from above the furnace 11 (in FIG. 4).
- the fuel nozzle 51 In the combustion burner 21 (21a, 21b, 21c, 21d) configured as described above, as shown in FIGS. 1 and 2, the fuel nozzle 51, the combustion burner air nozzle 52, and the secondary air from the center side. A nozzle 53 and a flame holder 54 and a cylindrical member (partition member) 55 are provided. As shown by an arrow 202, the fuel nozzle 51 is capable of injecting a fuel gas (fine fuel mixture, air) obtained by mixing pulverized coal (solid fuel) and carrier air (air, primary air). .
- a fuel gas fine fuel mixture, air
- Combustion burner air nozzle (combustion air nozzle) 52 is disposed outside fuel nozzle 51, and, as indicated by arrow 204, combustion air (for combustion burner) is disposed on the outer peripheral side of the fuel gas injected from fuel nozzle 51. Air, fuel gas combustion air, and Coal secondary air).
- the secondary air nozzle 53 is located outside the combustion burner air nozzle 52 and above the combustion burner air nozzle 52 in the vertical direction, outside the combustion burner air nozzle 52, and at the combustion burner air nozzle 52. It is arranged at a position on the lower side in the vertical direction. In this case, the vertical direction includes a direction shifted by a minute angle with respect to the vertical direction.
- the secondary air nozzle 53 is not disposed outside the combustion burner air nozzle 52 and at a position adjacent in the horizontal direction.
- the secondary air nozzle 53 can blow secondary air (AUX) into the outer peripheral side of the combustion burner air injected from the combustion burner air nozzle 52 as indicated by an arrow 206.
- the secondary air nozzle 53 may be disposed outside the combustion burner air nozzle 52 and at a position adjacent in the horizontal direction. Further, the secondary air nozzle 53 may be disposed outside the combustion burner air nozzle 52 and at a position adjacent in the horizontal direction, and not disposed at a position adjacent in the vertical direction.
- the secondary air nozzle 53 may be provided on the entire outer periphery of the combustion burner air nozzle 52.
- the secondary air nozzle 53 may be capable of adjusting the ejection amount of the secondary air by providing a damper opening adjustment mechanism or the like.
- the fuel nozzle 51, the combustion burner air nozzle 52, and the secondary air nozzle 53 of the combustion burner 21 are connected to the burner angle adjustment unit 80 and the burner angle adjustment unit 80 in a slidable state. 82.
- the burner angle adjustment unit 80 is the tip of the fuel nozzle 51 of the combustion burner 21, the combustion burner air nozzle 52, and the secondary air nozzle 53, and is movable in the direction set with respect to the pipe line unit 82. It is supported by.
- the direction in which the burner angle adjustment unit 80 is movable is not particularly limited, and may be movable in the axial direction (vertical direction) of the furnace 11 or may be movable in the cross-sectional direction (horizontal direction) of the furnace 11.
- the combustion burner 21 adjusts the direction in which the pulverized fuel mixture in which the pulverized coal and the carrier air are mixed is adjusted by adjusting the direction of the burner angle adjusting unit 80.
- the pipe section 82 is connected to the burner angle adjusting section 80, and pipe lines corresponding to the fuel nozzle 51, the combustion burner air nozzle 52, and the secondary air nozzle 53 are formed, and the burner angle adjusting section is formed.
- a fuel gas obtained by mixing pulverized coal and air, combustion burner air, and secondary air are supplied to each part of 80.
- the pipe line part 82 has a long tubular structure.
- the fuel nozzle 51 has a straight pipe at the tip side, that is, the part corresponding to the burner angle adjusting unit 80, and has a cross-sectional (opening) area (channel cross-sectional area) orthogonal to the direction in which the pulverized fuel mixture is blown. It becomes constant.
- the combustion burner air nozzle 52 has a shape in which a tip side portion, that is, a portion corresponding to the burner angle adjusting unit 80 is narrowed toward the tip, and a cross section (opening) perpendicular to the direction in which the pulverized fuel mixture is blown. ) Area (channel cross-sectional area) decreases toward the tip.
- the combustion burner air nozzle 52 has a shape in which the area of the surface surrounded by the outer surface becomes smaller with respect to the upstream end portion in the fuel gas flow direction toward the tip.
- the secondary air nozzle 53 has a shape in which a portion on the tip side, that is, a portion corresponding to the burner angle adjusting unit 80 is narrowed toward the tip, and a cross section (opening) orthogonal to the direction in which the pulverized fuel mixture is blown. Area (channel cross-sectional area) becomes smaller toward the tip.
- the shapes of the openings of the fuel nozzle 51 and the combustion burner air nozzle 52 are not limited to a square, and may be a rectangle. In this case, the corner may have a curved shape.
- the strength of the nozzle can be improved. Furthermore, it is good also as a cylinder.
- the flame holder 54 is disposed in the fuel nozzle 51 at the downstream side in the fuel gas blowing direction and at the axial center side, thereby functioning for ignition of the fuel gas and flame holding. is there.
- This flame holder 54 is a so-called so-called “flame shape” in which first flame holding members 61 and 62 along the horizontal direction and second flame holding members 63 and 64 along the vertical direction (vertical direction) are arranged in a cross shape. It has a double cross split structure.
- Each first flame holding member 61, 62 has a flat portion 61a, 62a having a flat plate shape and a front end portion (downstream end portion in the fuel gas flow direction) of the flat portions 61a, 62a.
- the widened portions 61b and 62b are provided with widened portions 61b and 62b which are integrally provided.
- the widened portions 61b and 62b have an isosceles triangular cross section, the width increases toward the downstream side in the fuel gas flow direction, and the front end is a plane perpendicular to the fuel gas flow direction.
- the widened portions 61b and 62b are not limited to the isosceles triangular cross section, and may be any split shape that separates the flow of the fuel gas and forms a recirculation region on the downstream side. It may be Y-shaped.
- the second flame holding members 63 and 64 have the same structure.
- the fuel nozzle 51 and the combustion nozzle air nozzle 52 have a long tubular structure, the fuel nozzle 51 has a rectangular opening 51a, and the combustion burner air nozzle 52 has a rectangular ring shape. Since the opening 52a is provided, the fuel nozzle 51 and the combustion burner air nozzle 52 have a double tube structure.
- a secondary air nozzle 53 is arranged as a double pipe structure outside the fuel nozzle 51 and the combustion burner air nozzle 52, and has a rectangular ring-shaped opening 53a.
- the opening 52a of the combustion burner air nozzle 52 is disposed outside the opening 51a of the fuel nozzle 51, and the opening of the secondary air nozzle 53 is disposed outside the opening 52a of the combustion burner air nozzle 52.
- 53a is disposed.
- the secondary air nozzle 53 may be a secondary air nozzle by arranging a plurality of nozzles separately on the outer peripheral side of the combustion burner air nozzle 52 without being arranged as a double pipe structure.
- nozzles 51, 52, 53 are arranged with openings 51a, 52a, 53a aligned on the same plane.
- the flame holder 54 is supported by a plate material (not shown) from the inner wall surface of the fuel nozzle 51 or the upstream side of the flow path through which the fuel gas flows.
- the fuel nozzle 51 has a plurality of flame holding members 61, 62, 63, 64 as a flame holder 54 arranged in a double split structure therein, so that the fuel gas flow path is divided into nine. Will be.
- the widened portions 61b and 62b whose widths are widened at the front end portions are located, and the widened portions 61b and 62b have the front end surfaces aligned on the same plane as the opening 51a.
- the cylinder member 55 that reduces the flow velocity of the fuel gas flowing in the axial center side of the fuel gas flowing in the fuel nozzle 51 is the inside of the fuel nozzle 51, more precisely, the fuel This position includes the tip of the nozzle 51 and is disposed at a portion corresponding to the burner angle adjustment unit 80.
- the cylindrical member 55 By the cylindrical member 55, the inner flow path in which the flame holder 54 is disposed and the outer flow path outside the inner flow path are partitioned.
- the cylindrical member 55 has an inner flow path surrounded by the cylindrical member 55 as it goes from the upstream side to the downstream side in the flow direction of the fuel gas, that is, toward the opening at the tip.
- the cross-sectional area of the flow path is large.
- the cylinder member 55 is a square cylinder having a square cross section, and is disposed inside the fuel nozzle 51.
- the cylindrical member 55 is disposed between the plate member 65 disposed between the flame holding member 61 and the upper wall surface of the combustion burner air nozzle 52, and between the flame holding member 62 and the lower wall surface of the combustion burner air nozzle 52.
- a plate member 66 disposed between the flame holding member 63 and the side wall surface of the combustion burner air nozzle 52; and between the flame holding member 64 and the side wall surface of the combustion burner air nozzle 52.
- a plate member 68 disposed on the surface.
- the cylindrical member 55 is joined to the respective ends of the plate members 65, 66, 67, 68 in a cross section perpendicular to the fuel gas flow direction to form a square cylinder.
- the cylindrical member 55 encloses a part of the flame holder 54 on the axial center side of the fuel nozzle 51, in this embodiment, a portion that forms a quadrangle with the flame holding members 61, 62, 63, 64.
- the plate members 65, 66, 67, and 68 have upstream end portions in the fuel gas flow direction upstream from the flame holder 54, and downstream end portions in the fuel gas flow direction. The same position as the downstream end of the vessel 54.
- the cylindrical member 55 has plate members 65, 66, 67, 68 as fuel nozzles as they go from upstream to downstream in the fuel gas flow direction, that is, toward the opening at the tip (opening for fuel gas injection). Inclined in a direction away from the axis 51. Further, the plate members 65, 66, 67 and 68 are joined to the flame holding members 61, 62, 63 and 64 at positions where they overlap with the flame holding members 61, 62, 63 and 64. Thereby, the flame-holding members 61, 62, 63, 64 penetrate the plate members 65, 66, 67, 68 at the overlapping positions.
- the cylindrical member 55 has a shape in which the inner area surrounded by the cylindrical member 55 becomes larger toward the opening at the tip in the fuel gas flow direction.
- the cylindrical member 55 has an area A1 of the area A2. Smaller than.
- the fuel gas in which pulverized coal and air are mixed is blown into the furnace from the opening 51 a of the fuel nozzle 51, and the combustion burner air is outside the combustion burner air nozzle 52.
- the air is blown into the furnace through the opening 52a, and the secondary air is blown into the furnace through the opening 53a of the secondary air nozzle 53 on the outside thereof.
- the fuel gas is blown into both the inner flow path and the outer flow path partitioned by the cylindrical member 55.
- the combustion gas blown into the inside of the cylindrical member 55 is branched and ignited by the flame holder 54 at the opening 51a of the fuel nozzle 51, and burns to become combustion gas.
- the combustion gas blown to the outside of the cylindrical member 55 is burned by the flame ignited by the flame holder 54. Moreover, combustion of fuel gas is accelerated
- the flame holder 54 has a split shape, the fuel gas is branched by the flame holder 54 at the opening 51 a of the fuel nozzle 51. At this time, the flame holder 54 is moved to the fuel nozzle 51. In the central region of the opening 51a, ignition and flame holding of the fuel gas are performed in this central region. Thereby, the internal flame holding of the combustion flame (flame holding in the central region of the opening 51a of the fuel nozzle 51) is realized.
- the outer peripheral portion of the combustion flame becomes low temperature, and oxygen is consumed from the inside of the flame, resulting in low oxygen.
- the temperature of the outer peripheral part of the combustion flame under a high oxygen atmosphere can be lowered, and the amount of NOx generated in the outer peripheral part of the combustion flame is reduced.
- the combustion burner 21 employs a structure that holds the internal flame, it is preferable that the fuel gas and the combustion air (combustion burner air and secondary air) are supplied as a straight flow. That is, the fuel nozzle 51, the combustion burner air nozzle 52, and the secondary air nozzle 53 have a structure for supplying the fuel gas, the combustion burner air, and the secondary air as a straight flow in the burner axial direction without swirling. Is preferred. Since this fuel gas, combustion burner air, and secondary air are injected as a straight flow to form a combustion flame, gas circulation in the combustion flame is suppressed in the configuration in which the combustion flame is held inside. As a result, the outer periphery of the combustion flame is maintained at a low temperature, and the amount of NOx generated by mixing with the combustion burner air is reduced.
- the flow rate of the fuel gas flowing through the inner flow path is reduced by providing the cylindrical member 55 in which the cross-sectional area of the inner flow path increases toward the opening at the tip of the fuel nozzle 51. Can do.
- the blow-off of the flame can be suppressed by bringing the flow rate of the fuel gas close to the combustion speed, more stable flame holding becomes possible. Therefore, by strengthening the internal flame holding, it is possible to suppress the high temperature and high oxygen region that may occur on the outer peripheral side of the fuel nozzle 51, and to reduce NOx.
- the combustion burner 21 has a cross-sectional area of the outer flow path partitioned by the cylindrical member 55 that decreases in the flow direction of the fuel gas. Therefore, of the fuel gas blown into the furnace by the fuel nozzle 51, the combustion burner 21 The flow rate of the fuel gas in the outer flow path that flows in the vicinity of the combustion burner air blown by the air nozzle 52 can be further increased. As a result, the difference in flow rate between the fuel gas flowing in the outer flow path and the combustion burner air can be reduced, and ignition at the boundary between the fuel gas flowing in the outer flow path and the combustion burner air, so-called external ignition, is suppressed. be able to.
- the combustion gas 90 that has passed between the flame holding member 61 and the flame holding member 62 of the flame holder 54 is injected from the combustion burner 21 at a low flow rate, for example, 10 m / s, and is internally ignited.
- the combustion gas 90 that passes outside the space between the flame holding member 61 and the flame holding member 62 of the flame holder 54 and passes through the space surrounded by the cylindrical member 55 is burned at a low flow rate, for example, 10 m / s. It is injected from 21 and internally ignited.
- the combustion gas 90 that is outside the space surrounded by the cylindrical member 55 and that has passed through the space surrounded by the fuel nozzle 51 is injected from the combustion burner 21 at a flow rate faster than the inner fuel gas, for example, 30 m / s. Is done.
- the combustion burner air that is outside the space surrounded by the fuel nozzle 51 and that has passed through the space surrounded by the combustion burner air nozzle 52 is burned at a flow rate faster than the inner fuel gas, for example, 40 m / s. Injected from the burner 21.
- the secondary air that is outside the space surrounded by the combustion burner air nozzle 52 and that has passed through the space surrounded by the secondary air nozzle 53 has a higher flow rate than the inner fuel gas, for example, 60 m / s. It is injected from the combustion burner 21.
- the fuel nozzle 51 capable of injecting fuel gas mixed with pulverized coal and air, and the combustion burner capable of injecting combustion burner air from the outside of the fuel nozzle 51.
- an air nozzle 52 for combustion, and a flame holder 54 is provided on the axial center side at the tip of the fuel nozzle 51 to reduce the flow rate of the fuel gas flowing on the axial center side in the fuel nozzle 51, thereby A cylinder member 55 is provided to increase the flow rate of the fuel gas flowing on the 52 side.
- the fuel gas flowing in the fuel nozzle 51 can be made closer to the combustion speed by reducing the flow velocity of the fuel gas flowing in the axial center side of the fuel nozzle 51 from the cylinder member 55, that is, the inner flow path on the flame holder 54 side.
- the internal flame holding performance of the flame holder 54 can be improved. Since internal flame holding can be strengthened in this way, NOx can be further reduced by promoting combustion in a reducing atmosphere where oxygen becomes insufficient.
- the flow rate of the fuel gas flowing in the outer flow path on the combustion burner air nozzle 52 side from the cylindrical member 55 out of the fuel gas flowing in the fuel nozzle 51 can be increased.
- the difference in flow velocity at the boundary between the flowing fuel gas and the combustion burner air can be reduced, and external ignition, which is ignition in the region where the combustion burner air is flowing, can be suppressed.
- the downstream end of the flame holder 54 is positioned so as to overlap the downstream end of the fuel nozzle 51, that is, the opening 51a in the fuel gas flow direction.
- the present invention is not limited to this.
- the combustion burner 21 only needs to have the flame holder 54 disposed in the vicinity of the tip of the fuel nozzle 51.
- the vicinity of the tip is inside the nozzle of the fuel burner 21.
- the combustion burner 21 includes the burner angle adjustment unit 80 as in the present embodiment, it is preferable to arrange the flame holder 54 inside the burner angle adjustment unit 80.
- pulverized coal has been described as an example of fuel for combustion, the present invention is not limited to pulverized coal (solid fuel), but biomass (biomass chip, biomass pellet), residue, petroleum coke, LNG, shale gas Or a mixture of two or more of these fuels may be used.
- FIG. 5 is a sectional view showing a combustion burner according to Embodiment 2 of the present invention.
- symbol is attached
- the combustion burner 21a shown in FIG. 5 of the second embodiment is provided with a fuel nozzle 51, a combustion burner air nozzle 52, and a secondary air nozzle 53 from the center side, and a flame holder 54 and a cylindrical member 55a. It has been.
- the cylinder member 55a includes plate members 65a and 66b.
- the cylinder member 55 a also includes plate portions corresponding to the plate members 67 and 68 of the cylinder member 55.
- the plate member 65a includes an inclined portion 84 with respect to the fuel gas flow direction and a horizontal portion 85 that is horizontal with respect to the fuel gas flow direction.
- the inclined portion 84 is disposed upstream of the horizontal portion 85 in the fuel gas flow direction, and is connected to the horizontal portion 85.
- the plate member 66b includes an inclined portion 86 with respect to the fuel gas flow direction and a horizontal portion 87 that is horizontal with respect to the fuel gas flow direction.
- the inclined portion 86 is disposed upstream of the horizontal portion 87 in the fuel gas flow direction, and is connected to the horizontal portion 87.
- the cylindrical member 55a is a region where the upstream inclined portions 84 and 86 in the flow direction of the fuel gas are arranged, and a region where the flow passage cross-sectional area of the inner flow passage becomes large and the horizontal portions 85 and 87 are arranged.
- the channel cross-sectional area of the inner channel is constant.
- the cylindrical member 55a is configured such that the flow passage cross-sectional area of the inner flow passage is changed in a partial region in the fuel gas flow direction, and the flow passage cross-sectional area of the inner flow passage is constant in the remaining region. The same effect as above can be obtained. Further, the combustion burner 21a is rectified in the straight traveling direction so that the fuel gas does not flow to the outside and cause ignition of the outer periphery by making the flow path cross-sectional area of the cylindrical member 55a on the tip side of the fuel nozzle 51 constant. In this state, the fuel gas can be injected from the nozzle.
- the shape of the cylindrical member of the combustion burner is not limited to the shape of the cylindrical members 55 and 55a, and can be various shapes.
- the cylinder member may have a configuration in which a plurality of cylinders having different inner areas are connected in the fuel gas flow direction to change the shape of the connection portion.
- the cylindrical member is not limited to a shape in which the cross-sectional shape parallel to the axis is a straight line, and may be a curved line.
- the cylindrical member has a shape in which the inclination angle, which is an angle formed with the direction parallel to the flow direction of the fuel gas, becomes smaller toward the tip side in the flow direction of the fuel gas, that is, the angle approaches 0.
- the angle approaches 0.
- a guide surface 88 may be provided on the inner side of the downstream end of the cylindrical member 55a so as to be inclined toward the axial center of the fuel nozzle 51 as it goes toward the downstream side of the fuel gas flow. .
- the guide surface 88 is preferably provided over the entire circumference of the cylindrical member 55a, but may be provided partially.
- the guide surface 88 may be a linear inclined surface as shown in the figure, or may be a curved surface.
- FIG. 7 is a cross-sectional view showing a combustion burner according to Embodiment 3 of the present invention.
- symbol is attached
- the combustion burner 21b shown in FIG. 7 of the third embodiment is provided with a fuel nozzle 51, a combustion burner air nozzle 52, and a secondary air nozzle 53 from the center side, and a flame holder 54, a cylindrical member 55, and a guide.
- Members 102 and 104 are provided.
- the guide members 102 and 104 guide the fuel gas flowing in the fuel nozzle 51 to the axial center side, thereby separating the combustion burner air blown by the combustion burner air nozzle 52 as indicated by an arrow 208. Lead fuel gas.
- the guide members 102 and 104 are provided in the pipe line portion 82 of the fuel nozzle 51. That is, the guide members 102 and 104 are positions that do not face the flame holder 54 and the cylinder member 55 arranged in the fuel nozzle 51, and are located upstream of the flame holder 54 and the cylinder member 55 in the fuel gas flow direction. Is arranged.
- the guide members 102 and 104 are disposed on the inner wall surface of the fuel nozzle 51 along the circumferential direction.
- the guide member 102 is disposed on the upper wall surface of the fuel nozzle 51, and the guide member 104 is disposed on the lower wall surface of the fuel nozzle 51.
- the guide member may also be provided on the side wall surface of the fuel nozzle 51.
- the guide members 102 and 104 have a shape protruding from the inner wall surface of the fuel nozzle 51 toward the flame holder 54, and a guide surface (inclined surface or curved surface) for guiding the fuel gas in the fuel nozzle 51 toward the axial center is formed. Has been.
- the guide members 102 and 104 are arranged in the pipe line portion 82 of the fuel nozzle 51, so that the fuel gas flowing in the fuel nozzle 51 is axially located by the guide members 102 and 104, that is, the flame stabilizer. It is guided to the inner flow path inside the cylindrical member 55 on the 54 side. Thereby, the solid fuel contained in the fuel gas is moved to the axial center side, and in the cross section of the fuel nozzle 51, the concentration of the pulverized coal on the axial side becomes higher than that on the combustion burner air nozzle 52 side. In addition, since the primary air which is carrier gas has higher fluidity than pulverized coal, the distribution in the fuel nozzle 51 becomes uniform over a shorter distance than pulverized coal.
- the combustion burner 21 b is provided with guide members 102 and 104, and moves the pulverized coal to the axial center side upstream of the cylindrical member 55, whereby the concentration of pulverized coal in the fuel gas flowing into the inner flow path of the cylindrical member 55. Can be high. Thereby, the density
- FIG. 8 is a sectional view showing a combustion burner according to Example 4 of the present invention.
- symbol is attached
- the combustion burner 21c shown in FIG. 8 according to the fourth embodiment is provided with a fuel nozzle 51, a combustion burner air nozzle 52, and a secondary air nozzle 53 from the center side, and a flame holder 54, a cylindrical member 55, and a guide.
- Members 102 and 104 are provided.
- the inner side surface 112 and the outer side surface 114 of the portion corresponding to the burner angle adjustment unit 80 that is a part of the tip side of the secondary air nozzle 53 are inclined in a direction away from the axis of the fuel nozzle 51. ing. That is, the secondary air nozzle 53 has the inner surface 112 and the outer surface 114 inclined in the same direction as the cylindrical member 55.
- the secondary air nozzle 53 tilts the secondary air 98a in a direction away from the axis of the fuel nozzle 51 by tilting the inner surface 112 and the outer surface 114 away from the axis of the fuel nozzle 51. Spray.
- the combustion burner air 96 can be easily spread in the direction away from the axis.
- the combustion burner air 96 on the boundary side with the fuel gas 94 can be reduced, and NOx reduction in the high temperature and high oxygen region on the flame periphery can be promoted.
- the combustion burner 21c has adjusted the direction of the nozzle by adjusting the direction of the inner side surface 112 and the outer side surface 114 of the secondary air nozzle 53. However, the position of the secondary air nozzle 53 is separated from the combustion nozzle air nozzle 53. May be.
- FIG. 9 is a cross-sectional view showing a combustion burner according to Embodiment 5 of the present invention.
- FIG. 10 is a front view of the combustion burner according to the fifth embodiment.
- symbol is attached
- the combustion burner 21d shown in FIG. 9 of the fifth embodiment is provided with a fuel nozzle 51, a combustion burner air nozzle 52, and a secondary air nozzle 53 from the center side, and a flame holder 54d.
- the flame holder 54d is disposed in the fuel nozzle 51, on the downstream side in the fuel gas blowing direction and on the axial center side, thereby functioning for ignition of the fuel gas and flame holding. is there.
- the flame holder 54d is a so-called so-called cross-shaped arrangement in which first flame holding members 161 and 162 along the horizontal direction and second flame holding members 63 and 64 along the vertical direction (vertical direction) are arranged. It has a double cross split structure.
- each 1st flame holding member 161,162 has flat part 161a, 162a which makes flat plate shape with the constant thickness, and the front end part (downstream end part of the flow direction of fuel gas) of these flat parts 161a, 162a
- the widened portions 161b and 162b are integrally provided.
- the widened portions 161b and 162b have an isosceles triangular cross section, the width increases toward the downstream side in the fuel gas flow direction, and the front end is a plane perpendicular to the fuel gas flow direction.
- the flat portions 161a and 162a are inclined with respect to the fuel gas flow direction.
- each 1st flame holding member 161,162 is a partition member which partitions an inner side flow path and an outer side flow path. That is, the flow path sandwiched between the first flame holding members 161 and 162 is the inner flow path, and the space between the first flame holding members 161 and 162 and the inner wall surface of the combustion burner air nozzle 52 is the outer flow path.
- the second flame holding members 63 and 64 have the same shape as the flame holder 54 of the first embodiment, and the flat portion extends in a direction parallel to the fuel gas flow direction.
- the inner flow path is composed of flat portions 161 a and 162 a and portions between the flat portions 161 a and 162 a of the side wall surface of the combustion burner air nozzle 52. That is, a cylindrical inner flow path is constituted by a part of the flame holder 54d and a part of the combustion burner air nozzle 52.
- the inner channel is inclined in a direction in which the flat portions 161a and 162a approach the wall surface of the combustion burner air nozzle 52 toward the downstream side in the fuel gas flow direction.
- the cross-sectional area increases as it goes downstream in the fuel gas flow direction.
- the flame stabilizer 54d it is not necessary to provide a portion on the side wall surface side of the combustion burner air nozzle 52 with respect to the flat portions 161a and 162a in the widened portions 161b and 162b. That is, the flame holder 54d does not need to provide a widened portion having a flame holding function in a portion outside the cylindrical member 55d. Thereby, the possibility of external ignition can be further reduced.
- FIG. 11 is a front view of a combustion burner according to a modification.
- the combustion burner 21e shown in FIG. 11 is provided with a fuel nozzle 51, a combustion burner air nozzle 52, and a secondary air nozzle 53 from the center side, and is also provided with a flame holder 54e and a cylindrical member 55. .
- the flame holder 54e is disposed in the fuel nozzle 51 at the downstream side in the fuel gas blowing direction and at the axial center side, thereby functioning for fuel gas ignition and flame holding. is there.
- the flame holder 54e includes first flame holding members 61e and 62e along the horizontal direction and second flame holding members 63e and 64e along the vertical direction (vertical direction), and the first flame holding members 61e and 62e,
- the second flame holding members 63e, 64e form a quadrangular structure. That is, the first flame holding members 61e and 62e are provided between the second flame holding member 63e and the side wall surface of the combustion burner air nozzle 52, and between the second flame holding member 64e and the side wall surface of the combustion burner air nozzle 52.
- the second flame holding members 63e and 64e are provided between the first flame holding member 61e and the upper wall surface of the combustion burner air nozzle 52, and between the first flame holding member 62e and the lower wall surface of the combustion burner air nozzle 52. Not arranged between and between.
- the flame-holding members 61e, 62e, 63e, and 64e are the same as the flame-holding members 61, 62, 63, and 64 of the first embodiment described above, except that the arrangement positions are different.
- the cylinder member 55 is disposed at a position surrounding a square formed by the flame holding members 61e, 62e, 63e, and 64e.
- the combustion burner 21e has a quadrangular shape formed by the flame holding members 61e, 62e, 63e, and 64e of the flame holder 54e, and is not disposed up to a position in contact with the combustion burner air nozzle 52.
- the device 54e may be arranged. Thereby, the flow velocity of all the fuel gases passing around the flame holder 54e can be reduced.
- the flame holder of the present embodiment is provided with the widened portion having a triangular cross-sectional shape, but is not limited to this shape, and may be a quadrangular shape or the widened portion may be eliminated.
- the cross-sectional shape of the combustion burner 21 was made into square, circular may be sufficient and another polygon may be sufficient.
- 12 and 13 show a combustion nozzle of a combustion burner according to the sixth embodiment.
- the combustion burner of the present embodiment is common to the above-described embodiments in that an inner flow path whose flow path cross-sectional area expands in the fuel gas flow direction is formed by the partition member. However, it is different in that the plurality of flame holders are arranged at different positions in the fuel gas flow direction. Note that description of matters common to the above-described embodiments is omitted. 12 and 13 omit the combustion burner air nozzle and the secondary air nozzle, and only the fuel nozzle 51 is shown.
- the combustion burner of the present embodiment is disposed on both sides so as to sandwich the central flame holding member 71 with one central flame holding member 71 extending in the vertical direction at the central portion of the fuel nozzle 51 and in the vertical direction.
- Two side flame holding members 72 that extend, and two partition members 73 that are arranged on both sides so as to sandwich the side flame holding members 72 and extend in the vertical direction are provided.
- the flame holding members 71 and 72 of the present embodiment are so-called vertical splitters that extend in the vertical direction without crossing each other as in the above-described embodiments.
- the central flame holding member 71 includes a plate-like portion 71a located on the upstream side of the fuel gas flow, and a widened portion 71b connected to the downstream end of the plate-like portion 71a.
- the upper and lower ends of the central flame-holding member 71 are connected to the inner wall of the fuel nozzle 51, that is, the inner wall of the combustion burner air nozzle, as shown in FIG.
- the center flame holding member 71 is provided along the fuel gas flow direction.
- FIG. 13 the position of the upstream end of the plate-like portion 71a is indicated by a broken line.
- Each of the two side flame holding members 72 includes a plate-like portion 72a located on the upstream side of the fuel gas flow, and a widened portion 72b connected to the downstream end of the plate-like portion 72a.
- the upper and lower ends of each side flame holding member 72 are connected to the inner wall portion of the fuel nozzle 51, that is, the inner wall portion of the combustion nozzle air nozzle, as shown in FIG.
- the side flame holding members 72 are provided so that the distance between the side flame holding members 72 increases in the fuel gas flow direction.
- the position of the upstream end of the plate-like portion 72a is indicated by a broken line.
- Each of the two partition members 73 includes a plate-like portion 73a located on the upstream side of the fuel gas flow, and a guide surface 73b provided on the downstream side of the plate-like portion 73a. Similar to the guide surface 88 shown in FIG. 6, the guide surface 73 b is inclined so as to guide the fuel gas toward the center side of the fuel nozzle 51.
- the shape where the outer side shape of the plate-shaped part 73a was linearly extended downstream was employ
- the upper and lower ends of each partition member 73 are connected to the inner wall portion of the fuel nozzle 51, that is, the inner wall portion of the combustion nozzle air nozzle, as shown in FIG. As shown in FIG. 12, the partition members 73 are provided so that the distance between the partition members 73 increases in the fuel gas flow direction. In FIG. 13, the position of the upstream end of the plate-like portion 73a is indicated by a broken line.
- a flow path surrounded by the partition member 73 is an inner flow path, and a flow path surrounded by the partition member 73 and the inner wall of the fuel nozzle 51, that is, the inner wall of the combustion burner air nozzle, is an outer flow path.
- the Accordingly, the flow path cross-sectional area of the inner flow path is increased according to the fuel gas flow, so that the flow rate of the fuel gas is reduced. Since the flow path cross-sectional area of the outer flow path decreases according to the fuel gas flow, the flow rate of the fuel gas increases. Since the operational effects when the fuel gas velocity in the inner flow path decreases and the operational effects when the fuel gas velocity in the outer flow path increases are the same as those of the above-described embodiments, the description thereof is omitted.
- the downstream end of the central flame-holding member 71 (the downstream end of the widened portion 71b) and the downstream end of each partition member 73 (the downstream end of the guide surface 73b) are positioned at the downstream end of the fuel nozzle 51 ( (Opening position).
- the downstream end of each side flame holding member 72 (the downstream end of the widened portion 72 b) is located upstream of the downstream end of the central flame holding member 71 and the downstream end of each partition member 73. That is, the center flame holding member 71 becomes a downstream flame holding member, and each side flame holding member 72 becomes an upstream flame holding member.
- the downstream ends of the flame holding members 71 and 72 in the fuel gas flow direction so as to be arranged in steps, the widened portions 71b and 72b located at the downstream ends of the flame holding members 71 and 72 occupy.
- the channel cross-sectional area to be narrowed can be made as small as possible.
- the increase in the fuel gas flowing through the inner flow path can be suppressed, and the internal ignition can be further enhanced by bringing the flow rate of the fuel gas flowing through the inner flow path close to the combustion speed.
- the downstream end of the central flame-holding member 71 and the downstream end of each partition member 73 are aligned with the position of the downstream end of the fuel nozzle 51, but the present invention is not limited to this.
- the nozzle 51 may be arranged on the upstream side of the downstream end.
- a burner angle adjusting unit that adjusts the angle in the vertical direction (see, for example, reference numeral 80 in FIG. 2). Even if it is provided, the flow is hardly affected, which is advantageous.
- the downstream end of the flame holding member is distributed in the fuel gas flow direction as described above even for the horizontal splitter in which the flame holding member and the partition member extend in the horizontal direction. May be arranged.
- the combustion burner provided with the fuel nozzle having the rectangular cross section has been described.
- the circular combustion provided with the fuel nozzle having the circular cross section may be arranged in the fuel gas flow direction.
- the circular combustion burner of the present modification is a conical central circular flame-holding member 75 whose channel cross-sectional area is widened in the fuel gas flow direction, and is positioned on the outer peripheral side of the central circular flame-holding member 75 and flows in the fuel gas flow direction.
- a side circular flame-holding member 76 having an enlarged road cross-sectional area and a circular partition member 77 located on the outer peripheral side of the side circular flame-holding member 76 and having a flow passage cross-sectional area extending in the fuel gas flow direction are provided.
- the downstream end of the central circular flame-holding member 75 is positioned downstream of the downstream end of the side circular flame-holding member 76.
- the central circular flame-holding member 75 includes a constant thickness portion 75a having a constant thickness located on the upstream side of the fuel gas flow, and a widened portion 75b connected to the downstream end of the constant thickness portion 75a.
- the side circular flame holding member 76 includes a constant thickness portion 76a having a constant thickness located on the upstream side of the fuel gas flow, and a widening portion 76b connected to the downstream end of the constant thickness portion 76a.
- the circular partition member 77 includes a constant thickness portion 77a having a constant thickness located on the upstream side of the fuel gas flow, and a guide surface 77b connected to the downstream end of the constant thickness portion 77a.
- the outer periphery of the downstream end of the circular partitioning member 77 has a shape in which the outer peripheral shape of the constant thickness portion 77a is extended to the downstream side as it is, the surface protruding to the outer peripheral side.
- the widened portion located at the downstream end of the flame-holding members 75 and 76 can be provided by distributing the downstream ends of the flame-holding members 75 and 76 in the fuel gas flow direction.
- the channel cross-sectional area narrowed by occupying can be made as small as possible.
- FIG. 16 to 18 show a fuel nozzle according to a seventh embodiment.
- the combustion burner of the present embodiment is common to the above-described embodiments in that an inner flow path whose flow path cross-sectional area expands in the fuel gas flow direction is formed by the partition member. Therefore, the description of matters common to the above-described embodiments is omitted. Also, in FIG. 16 to FIG. 18, the combustion burner air nozzle and the secondary air nozzle are omitted, and only the fuel nozzle 51 is shown.
- the combustion burner of this embodiment extends in the vertical direction of the fuel nozzle 51 and has a plurality of (5 in this embodiment) flame holding members 81 provided at predetermined intervals in the horizontal direction, and these flame holding members.
- Two partition members 73 are provided at both upper and lower ends so as to sandwich 81 and extend in the horizontal direction.
- the flame holding member 81 of the present embodiment is a so-called vertical splitter in which the flame holding members extend in the vertical direction without crossing each other as in the above-described sixth embodiment.
- the flame holding members 81 are arranged so as to be inclined in parallel with each other.
- the interval between the partition members 73 gradually increases toward the downstream side of the fuel gas. It has come to expand.
- the flow path cross-sectional area of the inner flow path partitioned by the partition member 73 is increased in the fuel gas flow direction.
- the flow rate of the fuel gas in the inner flow path can be reduced by the partition member 73, so that more stable flame holding is possible.
- the combustion apparatus 12 is configured by arranging four combustion burners 21, 22, 23, 24, and 25 provided on the wall surface of the furnace 11 along the vertical direction. It is not limited to this configuration. That is, the combustion burner may be arranged at the corner without being arranged on the wall surface.
- the combustion apparatus is not limited to the swirl combustion method, and may be a front combustion method in which the combustion burner is disposed on one wall surface, or an opposed combustion method in which the combustion burner is disposed opposite to the two wall surfaces.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
Description
また、特許文献1のように燃焼ノズルの内側に保炎器を設けたとしても、微粉炭のような固体燃料の場合にはガス燃料に比べれば燃焼速度が遅く、火炎の吹き飛び等が生じるおそれがあり、保炎器での安定した着火が比較的困難となる。そこで、燃料ガスの流速を下げて燃焼速度に近づけて安定な着火を得ることが望まれる。
なお、外側流路としては、典型的には、仕切部材と燃料ノズルの内壁部(場合によっては燃焼バーナ用空気ノズルの内壁部が燃料ノズルの内壁部を兼ねる)との間の流路を意味する。
ただし、筒部材55aの下流端の外側には、外側に突出する案内面を設けずに、筒部材55aの外形状が下流側にそのまま直線状に延長された形状が採用されている。筒部材55aの下流端に外側へ案内する面を設けると、燃焼バーナ用空気との混合による外部着火のおそれがあるからである。
なお、案内面88は、上述した実施例1の構成に対しても適用可能である。
第2保炎部材63,64は、実施例1の保炎器54と同様の形状であり、平坦部が燃料ガスの流れ方向と平行な方向に延在している。
また、図12及び図13には、燃焼バーナ用空気ノズル及び2次空気ノズルが省略されており、燃料ノズル51のみが示されている。
各仕切部材73の上下端は、図13に示すように、燃料ノズル51の内壁部すなわち燃焼バーナ用空気ノズルの内壁部に接続されている。仕切部材73は、図12に示すように、燃料ガス流れ方向に行くにしたがい互いの仕切部材73間の間隔が広がるように設けられている。なお、図13には、板状部73aの上流端の位置が破線にて示されている。
このように、保炎部材71,72の下流端を燃料ガス流れ方向に振り分けて段違いに配置することで、保炎部材71,72の下流端に位置する拡幅部71b,72bが占有することによって狭められる流路断面積を可及的に小さくすることができる。これにより、内側流路を流れる燃料ガスの増速を抑えることができ、内側流路を流れる燃料ガスの流速を燃焼速度に近づけて内部着火を更に強化することができる。
なお、本実施例では、中央保炎部材71の下流端と各仕切部材73の下流端は、燃料ノズル51の下流端の位置に揃えられているが、これに限定されるものではなく、燃料ノズル51の下流端よりも上流側に揃えて配置されていても良い。
側部円形保炎部材76は、燃料ガス流れ上流側に位置する一定厚とされた定厚部76aと、この定厚部76aの下流端に接続された拡幅部76bとを備えている。
円形仕切部材77は、燃料ガス流れ上流側に位置する一定厚とされた定厚部77aと、この定厚部77aの下流端に接続された案内面77bとを備えている。なお、円形仕切部材77の下流端の外周には、外周側に突出する面を、定厚部77aの外周形状がそのまま下流側に延長された形状が採用されている。
また、図16乃至図18には、燃焼バーナ用空気ノズル及び2次空気ノズルが省略されており、燃料ノズル51のみが示されている。
11 火炉
21,22,23,24,25 燃焼バーナ
51 燃料ノズル
52 燃焼バーナ用空気ノズル
53 2次空気ノズル
54 保炎器
55 筒部材
61,62,63,64 保炎部材
65,66,67,68 板部材
69,70 開口
71 中央保炎部材
72 側部保炎部材
73 仕切部材
80 バーナ角度調整部
82 管路部
102,104 案内部材
Claims (13)
- 燃料と空気とを混合した燃料ガスを吹き込み可能な燃料ノズルと、
該燃料ノズルの先端近傍における軸心側に設けられた少なくとも1つの保炎器と、
前記燃料ノズル内にて、前記保炎器が配置された内側流路と該内側流路の外側の外側流路とを仕切る仕切部材と、
を備え、
前記仕切部材によって仕切られた前記内側流路の流路断面積が燃料ガスの流れ方向に拡大する燃焼バーナ。 - 前記仕切部材は、筒部材とされている請求項1に記載の燃焼バーナ。
- 前記仕切部材は、前記保炎器を挟んで互いに間隔を有して延在する2つの板状体を有し、
各前記板状体が燃料ノズルの外周を区画する壁面に対して接続されている請求項1に記載の燃焼バーナ。 - 前記燃料ノズルの外側から空気を供給する燃焼バーナ用空気ノズルを備え、
前記仕切部材によって仕切られた前記外側流路の流路断面積が燃料ガスの流れ方向に減少する請求項1から3のいずれか一項に記載の燃焼バーナ。 - 前記仕切部材は、先端側に向かうにしたがって、燃料ガスの流れ方向と平行な方向とのなす角である傾斜角が燃料ガスの流れ方向上流端部に対して小さくなる請求項1から4のいずれか一項に記載の燃焼バーナ。
- 前記仕切部材の内壁面には、燃料ガスの流れ方向に行くにしたがい前記燃料ノズルの軸心側に傾斜する案内面が設けられている請求項1から5のいずれか一項に記載の燃焼バーナ。
- 前記燃料ノズルの外側から空気を供給する燃焼バーナ用空気ノズルを備え、
前記燃焼バーナ用空気ノズルは、先端に向かうにしたがって、外側の面で囲われた面の面積が、燃料ガスの流れ方向上流端部に対して小さくなる請求項1から6のいずれか一項に記載の燃焼バーナ。 - 前記仕切部材よりも上流側に配置され、前記燃料ノズル内を流れる燃料ガスを軸心側に導く案内部材をさらに有する請求項1から7のいずれか一項に記載の燃焼バーナ。
- 前記燃料ノズルの外側から空気を供給する燃焼バーナ用空気ノズルを備え、
前記燃焼バーナ用空気ノズルの外側から空気を吹き込み可能な2次空気ノズルをさらに有し、
前記2次空気ノズルは、軸心側の面が先端側に向かうにしたがって、軸心から離れる傾斜を有し、前記2次空気ノズル内を流れる空気を前記2次空気ノズルにより吹き込まれる空気から離間して軸の外側に導く方向に噴出する請求項1から8のいずれか一項に記載の燃焼バーナ。 - 前記保炎器は、水平方向に沿って鉛直方向に所定隙間をもって平行をなす2つの第1保炎部材と、鉛直方向に沿って水平方向に所定隙間をもって平行をなす2つの第2保炎部材とが交差するように配置された構造をなしている請求項1から9のいずれか一項に記載の燃焼バーナ。
- 前記保炎器は、燃料ガス流れの上流側に設けた上流側保炎部材と、該上流側保炎部材に対して燃料ガスの下流側に設けた下流側保炎部材とを備えている請求項1から10のいずれか一項に記載の燃焼バーナ。
- 前記保炎器は、燃料ガスの流れ方向における下流側に拡幅部を有する請求項1から11のいずれか一つに記載の燃焼バーナ。
- 火炉と、
該火炉に対して設置された請求項1から12のいずれか一項に記載の燃焼バーナと、
前記火炉の下流側にて前記燃焼バーナからの燃焼ガスと熱交換する熱交換器と、
を備えているボイラ。
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MX2017009771A MX2017009771A (es) | 2015-03-31 | 2016-02-22 | Quemador de combustión y caldera proporcionada con este. |
US15/553,273 US10458645B2 (en) | 2015-03-31 | 2016-02-22 | Combustion burner and boiler provided with same |
JP2017509379A JP6408135B2 (ja) | 2015-03-31 | 2016-02-22 | 燃焼バーナ及びこれを備えたボイラ |
RU2017130391A RU2661993C1 (ru) | 2015-03-31 | 2016-02-22 | Горелка для сжигания и котел, оснащенный такой горелкой для сжигания |
KR1020177021755A KR101972249B1 (ko) | 2015-03-31 | 2016-02-22 | 연소 버너 및 이를 구비한 보일러 |
CN201680011710.1A CN107250668A (zh) | 2015-03-31 | 2016-02-22 | 燃烧器以及具备该燃烧器的锅炉 |
EP16771965.7A EP3279563B1 (en) | 2015-03-31 | 2016-02-22 | Combustion burner and boiler provided therewith |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2015073498 | 2015-03-31 | ||
JP2015-073498 | 2015-03-31 | ||
JP2015179762 | 2015-09-11 | ||
JP2015-179762 | 2015-09-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2016158081A1 true WO2016158081A1 (ja) | 2016-10-06 |
Family
ID=57006705
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2016/055008 WO2016158081A1 (ja) | 2015-03-31 | 2016-02-22 | 燃焼バーナ及びこれを備えたボイラ |
Country Status (9)
Country | Link |
---|---|
US (1) | US10458645B2 (ja) |
EP (1) | EP3279563B1 (ja) |
JP (1) | JP6408135B2 (ja) |
KR (1) | KR101972249B1 (ja) |
CN (1) | CN107250668A (ja) |
CL (1) | CL2017002187A1 (ja) |
MX (1) | MX2017009771A (ja) |
RU (1) | RU2661993C1 (ja) |
WO (1) | WO2016158081A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101918726B1 (ko) | 2017-06-08 | 2018-11-14 | 한국지역난방공사 | 원료 미립화가 가능한 버너 |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6568192B2 (ja) * | 2017-12-19 | 2019-08-28 | 中外炉工業株式会社 | バーナ |
US11305302B2 (en) | 2020-01-22 | 2022-04-19 | General Electric Company | Nozzle assembly for a solid fuel burner and method of operating a nozzle assembly for a solid fuel burner |
CN113324242B (zh) * | 2021-06-18 | 2022-03-11 | 哈尔滨工业大学 | 一种采用循环烟气型缝隙式直流煤粉燃烧器的w火焰锅炉 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0424404A (ja) * | 1990-05-21 | 1992-01-28 | Babcock Hitachi Kk | 微粉炭バーナ |
JPH11281010A (ja) * | 1998-03-26 | 1999-10-15 | Babcock Hitachi Kk | 固体燃料燃焼バーナと固体燃料燃焼装置 |
JP2010270992A (ja) * | 2009-05-22 | 2010-12-02 | Mitsubishi Heavy Ind Ltd | 石炭焚ボイラ |
WO2012137573A1 (ja) * | 2011-04-01 | 2012-10-11 | 三菱重工業株式会社 | 燃焼バーナ、固体燃料焚きバーナ並びに固体燃料焚きボイラ、ボイラ及びボイラの運転方法 |
Family Cites Families (68)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2360548A (en) | 1944-10-17 | Combustion method | ||
US766494A (en) | 1902-12-17 | 1904-08-02 | Francis G Crone | Gas and air mixing burner. |
US1103253A (en) | 1910-10-24 | 1914-07-14 | Horatio S Bennett | Burner. |
US1887330A (en) | 1929-11-15 | 1932-11-08 | William S Shaw | Gas burner |
US2149980A (en) | 1937-11-04 | 1939-03-07 | Jr Henry Wilbur Paret | Method and apparatus for controlling furnace combustion |
US2259010A (en) | 1939-05-24 | 1941-10-14 | William F Doyle | Apparatus for combustion of fluid fuel |
US2895435A (en) * | 1954-03-15 | 1959-07-21 | Combustion Eng | Tilting nozzle for fuel burner |
US3112988A (en) | 1960-02-26 | 1963-12-03 | Sheil Oil Company | Mixing gases at supersonic velocity |
US3213919A (en) | 1962-05-14 | 1965-10-26 | Calzolari Roberto | Nozzle apparatus for burning fuel |
US3209811A (en) | 1963-03-28 | 1965-10-05 | Loftus Engineering Corp | Combination high velocity burner |
US3823875A (en) | 1973-08-24 | 1974-07-16 | T Bauer | Burner nozzle tip for pulverized coal and method for its production |
US4284402A (en) | 1979-05-02 | 1981-08-18 | Atlantic Richfield Company | Flame modifier to reduce NOx emissions |
DE8005891U1 (de) | 1980-03-01 | 1981-10-01 | Joh. Vaillant Gmbh U. Co, 5630 Remscheid | Mit einem gasluftgemisch gespeister vormischbrenner geringer schalleistung |
JPS599414A (ja) | 1982-07-08 | 1984-01-18 | Babcock Hitachi Kk | 低窒素酸化物燃焼装置 |
WO1984000314A1 (en) | 1982-07-12 | 1984-02-02 | Combustion Eng | Improved nozzle tip for pulverized coal burner |
JPS5977206A (ja) | 1982-10-25 | 1984-05-02 | Babcock Hitachi Kk | 燃焼装置 |
DE3472154D1 (en) | 1983-04-22 | 1988-07-21 | Combustion Eng | Pulverized fuel burner nozzle tip and splitter plate therefor |
US4634054A (en) | 1983-04-22 | 1987-01-06 | Combustion Engineering, Inc. | Split nozzle tip for pulverized coal burner |
JPS60103207A (ja) | 1983-11-10 | 1985-06-07 | Mitsubishi Heavy Ind Ltd | コ−ルバ−ナノズル |
JP2791029B2 (ja) | 1988-02-23 | 1998-08-27 | バブコツク日立株式会社 | 微粉炭バーナ |
US5292246A (en) | 1988-05-02 | 1994-03-08 | Institut Francais Du Petrole | Burner for the manufacture of synthetic gas comprising a solid element with holes |
EP0445938B1 (en) * | 1990-03-07 | 1996-06-26 | Hitachi, Ltd. | Pulverized coal burner, pulverized coal boiler and method of burning pulverized coal |
US5215259A (en) | 1991-08-13 | 1993-06-01 | Sure Alloy Steel Corporation | Replaceable insert burner nozzle |
RU2038535C1 (ru) * | 1992-04-23 | 1995-06-27 | Акционерное общество "Котэс" | Пылеугольная горелка с низким выходом оксидов азота |
GB9322016D0 (en) * | 1993-10-26 | 1993-12-15 | Rolls Royce Power Eng | Improvements in or relating to solid fuel burners |
US5529000A (en) | 1994-08-08 | 1996-06-25 | Combustion Components Associates, Inc. | Pulverized coal and air flow spreader |
JPH08135919A (ja) | 1994-11-11 | 1996-05-31 | Babcock Hitachi Kk | 燃焼装置 |
DE19539246A1 (de) | 1995-10-21 | 1997-04-24 | Asea Brown Boveri | Airblast-Zerstäuberdüse |
US6003793A (en) | 1995-12-22 | 1999-12-21 | Mann; Jeffrey S. | Boundary layer coal nozzle assembly for steam generation apparatus |
JPH09203505A (ja) | 1996-01-29 | 1997-08-05 | Babcock Hitachi Kk | 固体燃料用バーナと固体燃焼システム |
WO1998001704A1 (en) | 1996-07-08 | 1998-01-15 | Combustion Engineering, Inc. | Pulverized solid fuel nozzle tip |
CN2281479Y (zh) | 1996-11-18 | 1998-05-13 | 浙江大学 | 宽调节比、多煤种、浓稀相煤粉旋流燃烧装置 |
JP3448190B2 (ja) | 1997-08-29 | 2003-09-16 | 三菱重工業株式会社 | ガスタービンの燃焼器 |
FR2784449B1 (fr) | 1998-10-13 | 2000-12-29 | Stein Heurtey | Bruleur a combustible fluide notamment pour fours de rechauffage de produits siderurgiques |
FR2790309B1 (fr) | 1999-02-25 | 2001-05-11 | Stein Heurtey | Perfectionnements apportes aux bruleurs a flamme plate |
CN2415254Y (zh) | 2000-02-25 | 2001-01-17 | 华中理工大学 | 带整流板的钝体燃烧器 |
US6579085B1 (en) | 2000-05-05 | 2003-06-17 | The Boc Group, Inc. | Burner and combustion method for the production of flame jet sheets in industrial furnaces |
CN1407274A (zh) | 2001-09-05 | 2003-04-02 | 清华同方股份有限公司 | 一种煤粉直流燃烧器 |
US7163392B2 (en) | 2003-09-05 | 2007-01-16 | Feese James J | Three stage low NOx burner and method |
US7500849B2 (en) | 2004-01-16 | 2009-03-10 | Air Products And Chemicals, Inc. | Emulsion atomizer nozzle, and burner, and method for oxy-fuel burner applications |
NO324171B1 (no) | 2006-01-11 | 2007-09-03 | Ntnu Technology Transfer As | Metode for forbrenning av gass, samt gassbrenner |
FR2899313B1 (fr) | 2006-03-31 | 2008-05-09 | Huau Christian Bernard Louis | Bruleur polyvalent a flamme creuse pour hydrocarbures |
CA2664769C (en) | 2006-09-27 | 2013-03-19 | Babcock-Hitachi Kabushiki Kaisha | Burner, and combustion equipment and boiler comprising burner |
US20080206696A1 (en) | 2007-02-28 | 2008-08-28 | Wark Rickey E | Tilt nozzle for coal-fired burner |
EP1985926B1 (en) | 2007-04-26 | 2018-09-05 | Mitsubishi Hitachi Power Systems, Ltd. | Combustion equipment and combustion method |
CN101675301B (zh) | 2007-05-30 | 2011-05-18 | 大阳日酸株式会社 | 无机质球状化粒子制造用燃烧器 |
CN201228965Y (zh) * | 2007-08-06 | 2009-04-29 | 国际壳牌研究有限公司 | 燃烧器 |
DE202007018718U1 (de) | 2007-08-29 | 2009-05-14 | Siemens Aktiengesellschaft | Kohlenstaubkombinationsbrenner mit integriertem Pilotbrenner |
US7775791B2 (en) | 2008-02-25 | 2010-08-17 | General Electric Company | Method and apparatus for staged combustion of air and fuel |
JP5072650B2 (ja) | 2008-02-28 | 2012-11-14 | 三菱重工業株式会社 | 微粉炭バーナ |
US8701572B2 (en) * | 2008-03-07 | 2014-04-22 | Alstom Technology Ltd | Low NOx nozzle tip for a pulverized solid fuel furnace |
US8104412B2 (en) | 2008-08-21 | 2012-01-31 | Riley Power Inc. | Deflector device for coal piping systems |
CN201302156Y (zh) | 2008-11-07 | 2009-09-02 | 浙江大学 | 一种外燃式微油点火和超低负荷稳燃煤粉燃烧器 |
JP5374404B2 (ja) | 2009-12-22 | 2013-12-25 | 三菱重工業株式会社 | 燃焼バーナおよびこの燃焼バーナを備えるボイラ |
DE102010004787B4 (de) | 2010-01-16 | 2014-02-13 | Lurgi Gmbh | Verfahren und Brenner zur Herstellung von Synthesegas |
JP2012122653A (ja) | 2010-12-07 | 2012-06-28 | Mitsubishi Heavy Ind Ltd | 燃焼バーナ |
US8915731B2 (en) | 2010-12-30 | 2014-12-23 | L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | Flameless combustion burner |
US20130291770A1 (en) | 2011-01-21 | 2013-11-07 | Babcock-Hitachi Kabushiki Kaisha | Solid fuel burner and combustion device using same |
CN102620291B (zh) | 2011-01-31 | 2014-09-24 | 中国科学院过程工程研究所 | 低氮氧化物排放煤粉解耦燃烧器及煤粉解耦燃烧方法 |
JP5763389B2 (ja) | 2011-04-01 | 2015-08-12 | 三菱重工業株式会社 | 燃焼バーナ |
JP5670804B2 (ja) | 2011-04-01 | 2015-02-18 | 三菱重工業株式会社 | 燃焼バーナ |
JP5897363B2 (ja) * | 2012-03-21 | 2016-03-30 | 川崎重工業株式会社 | 微粉炭バイオマス混焼バーナ |
CN202938290U (zh) | 2012-11-05 | 2013-05-15 | 徐州燃控科技股份有限公司 | 一种内燃式兼多通道低氮燃烧器 |
CN104100969B (zh) * | 2013-04-12 | 2017-04-12 | 气体产品与化学公司 | 宽焰氧‑固体燃料喷燃器 |
CN103267282B (zh) | 2013-06-11 | 2016-05-11 | 牛博申 | 浓淡分离煤粉燃烧器 |
CN103672883B (zh) | 2013-12-21 | 2017-02-22 | 哈尔滨锅炉厂有限责任公司 | 栅格式旋流燃烧器 |
CN203718765U (zh) | 2014-02-10 | 2014-07-16 | 四川川锅锅炉有限责任公司 | 一种带三次风低NOx燃烧器 |
JP5901737B2 (ja) | 2014-12-18 | 2016-04-13 | 三菱重工業株式会社 | 燃焼バーナ |
-
2016
- 2016-02-22 CN CN201680011710.1A patent/CN107250668A/zh active Pending
- 2016-02-22 WO PCT/JP2016/055008 patent/WO2016158081A1/ja active Application Filing
- 2016-02-22 EP EP16771965.7A patent/EP3279563B1/en active Active
- 2016-02-22 MX MX2017009771A patent/MX2017009771A/es unknown
- 2016-02-22 KR KR1020177021755A patent/KR101972249B1/ko active IP Right Grant
- 2016-02-22 US US15/553,273 patent/US10458645B2/en active Active
- 2016-02-22 RU RU2017130391A patent/RU2661993C1/ru active
- 2016-02-22 JP JP2017509379A patent/JP6408135B2/ja active Active
-
2017
- 2017-08-28 CL CL2017002187A patent/CL2017002187A1/es unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0424404A (ja) * | 1990-05-21 | 1992-01-28 | Babcock Hitachi Kk | 微粉炭バーナ |
JPH11281010A (ja) * | 1998-03-26 | 1999-10-15 | Babcock Hitachi Kk | 固体燃料燃焼バーナと固体燃料燃焼装置 |
JP2010270992A (ja) * | 2009-05-22 | 2010-12-02 | Mitsubishi Heavy Ind Ltd | 石炭焚ボイラ |
WO2012137573A1 (ja) * | 2011-04-01 | 2012-10-11 | 三菱重工業株式会社 | 燃焼バーナ、固体燃料焚きバーナ並びに固体燃料焚きボイラ、ボイラ及びボイラの運転方法 |
Non-Patent Citations (1)
Title |
---|
See also references of EP3279563A4 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101918726B1 (ko) | 2017-06-08 | 2018-11-14 | 한국지역난방공사 | 원료 미립화가 가능한 버너 |
Also Published As
Publication number | Publication date |
---|---|
JPWO2016158081A1 (ja) | 2017-10-19 |
CN107250668A (zh) | 2017-10-13 |
EP3279563A4 (en) | 2018-03-14 |
EP3279563B1 (en) | 2019-05-01 |
US10458645B2 (en) | 2019-10-29 |
JP6408135B2 (ja) | 2018-10-17 |
KR20170102940A (ko) | 2017-09-12 |
KR101972249B1 (ko) | 2019-04-24 |
CL2017002187A1 (es) | 2018-03-02 |
US20180045403A1 (en) | 2018-02-15 |
MX2017009771A (es) | 2018-03-28 |
RU2661993C1 (ru) | 2018-07-23 |
EP3279563A1 (en) | 2018-02-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101972247B1 (ko) | 연소 버너 및 보일러 | |
JP6408135B2 (ja) | 燃焼バーナ及びこれを備えたボイラ | |
JP2012122653A (ja) | 燃焼バーナ | |
JP5901737B2 (ja) | 燃焼バーナ | |
JP6049503B2 (ja) | 燃焼バーナ及びボイラ | |
JP5960022B2 (ja) | ボイラ | |
JP5854620B2 (ja) | ボイラ及びボイラの運転方法 | |
JP6560885B2 (ja) | 燃焼バーナ及びボイラ | |
JP5763389B2 (ja) | 燃焼バーナ | |
JP3204014U (ja) | 燃焼バーナ | |
JP6058077B2 (ja) | 燃焼バーナ | |
JP6258160B2 (ja) | 燃焼バーナ及びボイラ | |
CN111656096B (zh) | 燃烧炉及锅炉 | |
JP6804318B2 (ja) | 燃焼バーナ及びこれを備えたボイラ | |
JP2016118330A (ja) | 燃焼バーナ及びボイラ | |
JP6057784B2 (ja) | ボイラ | |
JP6289343B2 (ja) | ボイラ | |
JP6087796B2 (ja) | ボイラ |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 16771965 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2017509379 Country of ref document: JP Kind code of ref document: A |
|
REEP | Request for entry into the european phase |
Ref document number: 2016771965 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: MX/A/2017/009771 Country of ref document: MX |
|
ENP | Entry into the national phase |
Ref document number: 20177021755 Country of ref document: KR Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 15553273 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2017130391 Country of ref document: RU |
|
NENP | Non-entry into the national phase |
Ref country code: DE |