CA2632412A1 - Pulverized coal burner for firing fuel which is fed by dense phase conveyance - Google Patents
Pulverized coal burner for firing fuel which is fed by dense phase conveyance Download PDFInfo
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- CA2632412A1 CA2632412A1 CA002632412A CA2632412A CA2632412A1 CA 2632412 A1 CA2632412 A1 CA 2632412A1 CA 002632412 A CA002632412 A CA 002632412A CA 2632412 A CA2632412 A CA 2632412A CA 2632412 A1 CA2632412 A1 CA 2632412A1
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- burner
- fuel
- primary air
- tube
- air tube
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Classifications
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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
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
- F23C7/006—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes adjustable
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
Abstract
With a burner, especially pulverized coal burner (1), with a fuel conveying tube (7) and a primary air tube (9) which is concentrically arranged within it, wherein the primary air tube (9) on the mouth discharge side terminates at a distance to the mouth opening of the fuel conveying tube (7), and the burner (1) is connected, or can be connected, to a feed line which conveys pulverous fuel in dense phase, a solution is to be created which enables a low-NO x burner, which is suitable for firing the furnace of a steam generator, to be equipped with a dense phase conveyance of the fuel, without the low-NO x combustion characteristic being disadvantageously affected. This is achieved by the inside space of the primary air tube (9) being able to be connected, or being connected, to a primary air feed line, and by the fuel conveying space (13), which is formed between the primary air tube (9) and the fuel conveying tube (7), being able to be connected, or being connected, to the feed line which feeds pulverous fuel to the burner (1) in dense phase.
Description
1 Pulverized coal burner for firing fuel which is fed by dense phase conveyance 3 The invention is directed towards a burner, especially a pulverized coal burner, with a fuel 4 conveying tube and a primary air tube which is concentrically arranged within it, wherein the primary air tube on the mouth discharge side terminates at a distance to the mouth opening of 6 the fuel conveying tube, and the burner is connected, or can be connected, to a feed line which 7 conveys pulverous fuel in dense phase. Furthermore, the invention is directed towards a 8 method for combustion of particulate fuel, especially pulverized coal, preferably dry brown coal, 9 in a burner with primary air tube and fuel conveying tube, wherein the fuel is fed to the burner by dense phase conveyance and is conveyed by dense phase conveyance inside the burner along 11 the longitudinal axis of the burner and mixed with combustion air.
13 For the combustion of particulate fuel, especially pulverized coal and pulverized dry brown coal, 14 it is known to combust this in burners which in addition to a core air feed have a primary air feed, a secondary air feed and a tertiary air feed. Such burners are especially used in 16 conjunction with the firing of furnaces of large steam generators. The primary air feed, 17 secondary air feed and tertiary air feed in this case are formed and arranged in the form of 18 annular conveying cross sections, which are arranged concentrically to each other, or in the 19 form of concentric arrangements coaxially around a central core air tube, in which an oil burner lance or suchlike can be arranged. The pulverous fuel in this case as a rule is guided together 21 with the primary combustion air (primary air) in a primary air tube inside the burner to the burner 22 mouth. Swirlers, which are arranged on the outer side of the core jacket tube, are then provided 23 in this primary air tube and impart a desired swirl to the pulverized coal/primary air mixture, so 24 that as a result the combustion is optimized, but at least improved, especially with regard to a low-NOx combustion of the fuel. These burners as a rule are used in plants in which the 26 pulverous fuel is conveyed by means of a pneumatic conveyor from the mill directly to the 27 burner. Attached to this is the disadvantage of being operated with low transporting gas loads 28 and high conveying speeds in the process. This leads to an extensive wear of the transporting 29 tubes. Furthermore, the conveying tubes have relatively large dimensions (conveying cross sections).
32 For avoiding these disadvantages, a generic-type burner and a generic-type method, in which 33 the pulverous fuel is pneumatically conveyed to the burner, and in the bumer, by means of 34 dense phase in a dense phase conveying system, have already been proposed in DE 197 15 373 Al. With this, pulverized dry brown coal is conveyed in a single stage by means of a dense 21772023.1 1 phase conveying system, and with a transporting gas load of at least 60 kg of pulverized coal/kg 2 of transporting gas, or with a conveyed stream density of between 100 and 350 kg of pulverized 3 coal/m3, is fed to a steam generator burner. For controlling the mass stream of pulverized coal 4 and the loading of the conveying lines, water vapour or a hot inert gas, such as flue gas or nitrogen, is used as pneumatic conveying medium. In this case, burners are described in DE
6 197 15 973 Al, in which the fuel is fed to the burner in a central feed line, and then, during 7 discharge from this central line, is mixed with primary and secondary air streams which issue 8 from annular passage-form openings arranged concentrically around it, is dispersed, and 9 distributed into the furnace in a suspended state. Another burner has a central primary air tube which is concentrically encompassed by secondary and tertiary air lines. With this burner, the 11 fuel is introduced into the burner in a pulverized coal pipe which is guided in a coiled manner 12 around the primary air tube, and inside the burner is discharged into the secondary air passage 13 at a distance from the mouth opening of the burner.
This known burner indeed already has the advantage that the combustion air streams, which 16 are fed to the burner, and the fuel stream are spatially separated from each other so that a 17 dense phase conveyance of the fuel is possible, wherein transporting gas loads of over 20 kg of 18 pulverized coal/kg of transporting gas and conveying gas speeds of 3 to about 20 m/s at 19 pressures of < 10 bar, are understood by dense phase conveyance in the present application, but the combustion is not yet optimized with regard to a low-NOX combustion.
In particular, with 21 the so-called DS (swirl flow) burners, which are characterized by an especially low-NO,, 22 combustion, it is not possible to feed the pulverous fuel to the burner either in the central core 23 air tube or in a central air tube, or via an additional fuel conveying line which is guided in a 24 coiled manner in the secondary air feed passage. In order to achieve a low-NOx combustion, it is a technical aim to enrich the fuel concentration in the radially viewed outermost zone of the 26 primary air stream which is guided in the burner, before its discharge into the furnace, wherein 27 this enrichment is to be carried out uniformly over the circumference of the primary air jet. In the 28 case of the burners which are known from DE 197 15 973 Al, this aim is not achievable. In the 29 case of the burner with feed of fuel by dense phase conveyance through a central conveying tube, the feed of the fuel is directly centred in the region of the extension of the longitudinal axis 31 of the burner, so that the primary air stream which is arranged around it just has no enrichment 32 by fuel particles in its radial outer region. In the case of the other burner which is known from 33 this publication, the fuel is indeed conveyed in a secondary air stream which in the radial 34 direction is circumferentially arranged around the primary air stream.
However, this is carried out with a coiled conveying tube of small cross section so that the fuel discharges into the 21772023.1 2 1 secondary air only in a small area of the annular passage which conveys the secondary air, and 2 consequently there is no uniform distribution of the pulverous fuel over the cross section of the 3 entire annular conveying passage of the secondary air. Also, in this case, the fuel is conveyed 4 into the secondary air stream so that an enrichment of the outer region of the primary air stream with fuel is not carried out.
7 A pulverized coal burner for the steam-oxygen gasification of pulverized coal which is 8 introduced in dense phase, is indeed already known from DD 251 476 A3, in which the fuel, 9 which is uniformly distributed around a central feed of a combustion gas and of an oxidizing agent, via an annular passage cross section, is fed by dense phase conveyance.
In this case, 11 however, the admixing of a steam-oxidizing agent mixture is only then carried out in the further, 12 subsequent stream path outside a combustion chamber. This burner serves for the gasification 13 of the fuel and for producing a gasifying gas, which is why in addition to the oxidizing agent 14 steam is also blown into the pulverized coal stream. This technology, however, cannot be used with a burner for the firing of a furnace of a steam generator.
17 The invention is based on the object of creating a solution which makes it possible to equip a 18 low-NOX burner, which is suitable for firing the furnace of a steam generator, with a dense 19 phase conveyance of fuel, without disadvantageously affecting the low-NOX
combustion characteristic of the burner.
22 In the case of a burner of the type which is referred to in the introduction, this object is achieved 23 according to the invention by the inside space of the primary air tube being able to be 24 connected, or being connected, to a primary air feed line, and the fuel conveying space which is formed between the primary air tube and the fuel conveying tube being able to be connected, or 26 being connected, to the feed line which feeds pulverous fuel in dense phase to the burner.
28 In the case of a method of the type which is referred to in the introduction, this object is 29 achieved according to the invention by the fuel being conveyed inside the burner in an annular passage-form fuel conveying space which is formed radially outside a primary air line, and also 31 by the primary air stream which issues from the primary air line being admixed in a swirled state 32 with the fuel stream after discharge from the fuel conveying space inside the fuel conveying 33 tube.
21772023.1 3 1 By means of the invention, a solution is now created by which it is possible, without 2 disadvantageously affecting the low-NOx combustion characteristic of the burner, to feed 3 pulverous fuel to the burner by dense phase conveyance and to first mix the fuel with 4 combustion air in the bumer. This is achieved by an annular passage being formed and provided, in which just before the mouth region on the discharge side of the burner to the 6 fumace, the pulverous fuel, especially puiverized dry brown coal, is conveyed in the bumer 7 along the longitudinal axis of the burner. This annular passage in this case is concentrically 8 circumferentially arranged around the primary air stream. The primary air stream is now 9 furthermore swirled, for which swirlers are arranged and formed in the primary air stream at a suitable point, so that at the end of the annular passage-form conveying channel it mixes with 11 the fuel which is conveyed by dense phase conveyance, so that consequently at the mouth end 12 on the discharge side of the burner to the furnace the radially outer region of the primary air 13 stream is circumferentially uniformly enriched with the fuel, or there is fuel exclusively in this 14 region. By means of this measure, fuel is therefore conveyed by dense phase conveyance almost only in the outer circumferential region of the primary air stream.
This does not 16 disadvantageously affect the low-NOx combustion characteristics of the respective burner, on 17 the contrary these are assisted, boosted and optimized as a result. By means of the invention, 18 it is possible to maintain the swirling of the primary air stream and to distribute the pulverized 19 coal stream or coal mass stream uniformly over the circumference of the primary air stream on its radial outer edge region. Since, furthermore, the swiriers which are provided for swirling the 21 primary air stream are not arranged in the pulverized coal stream or coal mass stream, these 22 are also not exposed to the abrasive wear of the fuel particles, so that the burner according to 23 the invention is characterized as well by a reduced wear compared with the conveyance of fuel 24 in the primary air mixture.
26 In order to swirl the primary air stream and to be able to also use the dense phase conveyance 27 which is provided according to the invention with a swirl flow burner, it is expedient if at least 28 one swirler is arranged in the inside space of the primary air tube, which the invention provides 29 in a development.
31 In order to also be able to operate the bumer with an oil bumer lance or suchlike, it is 32 advantageous according to a development of the invention if a core air tube is arranged 33 concentrically to the primary air tube within it. An oil burner lance or suchlike, as this is known 34 from customary burners, can then be arranged in the core air tube.
21772023.1 4 1 Since the conveyance of the particulate fuel, especially pulverous fuel, is carried out in dense 2 phase, large conveying cross sections, such as annular passage cross sections or pipeline 3 cross sections, are not necessary for this conveyance, so that the invention is furthermore 4 characterized in that the radial distance between core air tube and primary air tube is greater than the radial distance between primary air tube and fuel conveying tube.
7 In this case, it is furthermore especially advantageous and especially expedient if the core air 8 tube extends in the longitudinal axial direction beyond the mouth end on the discharge side of 9 the primary air tube into the region of the mouth opening on the discharge side of the fuel conveying tube. As a result of this, a mixing chamber, in which the swirled primary air stream 11 and the dense stream conveyed stream of fuel are mixed with each other, is formed inside the 12 burner at the mouth end on the discharge side of the burner to the furnace.
As a result of this, it 13 is especially possible to re-use the geometry of previously existing burners and to retrofit these 14 simply by introducing a new primary air tube for the combustion of fuel which is conveyed in dense phase. The originally available primary air tube then becomes the fuel conveying tube.
16 Greater or more costly constructional steps are not to be otherwise taken on the furnace which 17 is provided with burners.
19 Since for conveying the primary air stream a furthermore relatively larger opening cross section is made available, it is possible to arrange there a plurality of swirlers, to arrange these on the 21 outer generated surface of the core air tube, especially when a central coaxial core air tube is 22 available. The invention, therefore, furthermore provides that a plurality of swirlers, preferably in 23 the form of a vane ring, circumferentially distributed on the outer surface of the core air tube, are 24 arranged radially on the outer side in the annular passage to the primary air tube.
26 Furthermore, it is advantageous if the burner according to the invention is also equipped with an 27 oil burner ignition lance, for which reason, according to a development of the invention, an 28 ignition lance, especially an oil burner ignition lance, is arranged coaxially in the core air tube.
Since with the configuration according to the invention especially low-NOX
burners are to be 31 provided, it is expedient if these additionally also have a secondary air feed and a tertiary air 32 feed. The invention, therefore, is further characterized by a secondary air feed which 33 encompasses the fuel conveying tube, and also a tertiary air feed which encompasses the 34 secondary air feed.
21772023.1 5 1 In a further expedient development, it is then also expedient, especially for low-NOx burners, if a 2 radially inwards extending stabilizing ring is arranged at the end on the combustion chamber 3 mouth side of the fuel conveying tube.
The method according to the invention in an expedient development first of all provides that the 6 primary air is admixed with the fuel stream in the mouth region of the burner in a mixing 7 chamber before discharging into the furnace. As a result of this, the possibility arises of using 8 the geometry of existing burners and of creating an intensive mixture of primary air and 9 pulverous fuel for low-NOx combustion. Finally, in this case then it is still especially advantageous if air, especially heated air, recirculated flue gas or a mixture of air and 11 recirculated flue gas, is fed to the burner as primary air.
13 The invention is subsequently exemplarily explained in more detail with reference to a drawing.
14 This shows in the single figure, in schematic view in detail, a cross section along the longitudinal axis of the end on the combustion chamber side of a low-NOx burner which is arranged in the 16 wall of a combustion chamber or of a furnace of a steam generator, especially of a large power 17 plant.
19 The burner 1, on the discharge side, leads into the combustion chamber or into the furnace 2 of a steam generator and is arranged in its circumferential wall. The burner 1 has an oil burner 21 ignition lance 4 which is arranged centrally along its longitudinal axis 3.
This is arranged in the 22 centre of a core air tube 5 which coaxially encompasses the oil burner ignition lance 4. The air 23 guiding device 6, which is arranged around the oil burner ignition lance 4 at its end which faces 24 the furnace 2, ends flush with the mouth end on the burner discharge side of a fuel conveying tube 7, in which primary air, which is fed to the burner through a primary air line 18 and mixed 26 with particulate fuel which is fed through the fuel conveying tube 7, discharges into the furnace 27 2. The fuel conveying tube 7 is concentrically arranged around the oil burner ignition lance 4 28 and also around the core air tube 5, and with the outer generated surface of a primary air tube 29 9, and, downstream of the end of the primary air tube towards the furnace 2, with the outer generated surface of the core air tube 5, forms in each case an annular passage-form 31 conveying cross section. At the end on the combustion chamber discharge side of the fuel 32 conveying tube 7, an air deflecting throat 8, which extends over the whole circumference of the 33 fuel conveying tube 7, is formed on the outer side. On the inner side of the fuel conveying tube 34 7, a stabilizing ring 14, which is provided with teeth, extends in this region radially inwards into the conveying cross section of the fuel conveying tube 7 and forms the termination of the fuel 21772023.1 6 1 conveying tube 7 at this point. The core air tube 5 terminates on the burner inner side at a 2 distance to the mouth end on the combustion chamber discharge side of the fuel conveying tube 3 7 in the region of the air guiding device 6.
In the annular passage-form conveying cross section, which is formed between core air tube 5 6 and fuel conveying tube 7, the primary air tube 9 is arranged coaxially to the core air tube 5 and 7 to the fuel conveying tube 7 so that a fuel conveying space 13 is formed with an annular 8 passage-form conveying cross section. The mouth end of the primary air tube 9 which faces 9 the furnace 2 terminates at a distance from the mouth ends on the burner discharge side both of the core air tube 5 and of the fuel conveying tube 7, so that on the burner inner side a mixing 11 cross section or mixing chamber 10 is formed. The end on the mouth side of the primary air 12 tube 9 is located approximately in the region of the arrangement of swirlers 15 which in the case 13 of low-NOX burners are customarily provided in the primary air stream. In the exemplary 14 embodiment, the primary air tube 9 extends into the burner 1 to such an extent that its end on the mouth side is arranged in the positioning region of adjustable swirlers 11, 12 which are 16 located in a secondary air feed 19 and in a tertiary air feed 20. The primary air tube 9, 17 furthermore, is arranged relative to the core air tube 5 and to the fuel conveying tube 7 in such a 18 way that its radial distance to the core air tube 5 is greater than to the fuel conveying tube 7.
19 Therefore, the annular passage-form fuel conveying space 13 is formed between the outer side of the primary air tube 9 and the inner side of the fuel conveying tube 7.
This annular fuel 21 conveying space 13 is connected, or can be connected, to a feed line, which is not shown, by 22 which fuel is pneumatically fed by dense phase conveyance to the burner 1, and then is also 23 pneumatically conveyed in the fuel conveying space 13 in dense phase. The fuel is particulate 24 fuel, especially pulverized coal, preferably pulverous dry brown coal. The dense phase conveyance is carried out with a load of 20 - 90 kg of pulverized coal/kg of conveying gas, and a 26 conveying speed of 3 to 20 m/s at pressures of < 10 bar. The radial distance between the outer 27 side of the primary air tube 9 and the inner side of the fuel conveying tube 7, and consequently 28 the passage height of the fuel conveying cross section or fuel conveying space 13, can be 29 approximately as great as the length by which the teeth of the stabilizing ring 14 extend radially inwards in the direction of the burner axis 3.
32 Primary air is fed to the burner 1 through the annular passage-form conveying cross section 33 which is formed between the inner side of the primary air tube 9 and the outer side of the core 34 air tube 5. The primary air can be air, especially preheated air, but can also be recirculated flue gas or a mixture of recirculated flue gas and air. The primary air, which is conveyed through the 21772023.1 7 1 primary air line 18 with circular passage-form conveying cross section, when discharging is 2 transferred into a swirled stream by means of adjustable swirlers 15 which are arranged on the 3 inner side on the primary air tube 9 between core air tube 5 and primary air tube 9 at the end on 4 the discharge side. The swirlers 15 are formed in the form of a vane ring consisting of guide vanes which are arranged in a uniformly distributed manner on the outer circumference of the 6 core air tube 5.
8 Furthermore, the burner 1, as known from customary burners, has a secondary air tube 16 9 which is arranged on the outer side coaxially around the fuel conveying tube 7, and a tertiary air tube 17 which in turn is arranged on the outer side coaxially at a distance around the secondary 11 air tube. Secondary air is fed through the secondary air tube 16 to the furnace 2, and tertiary air 12 is fed through the tertiary air tube 17 to the furnace 2, as this is known from known burners for 13 creating a multistage low-NOx combustion.
For controlling a possibly desired swirling both of the primary air and of the secondary air in the 16 secondary air feed and of the tertiary air in the tertiary air feed, it is provided that the respective 17 swirlers 15, 11 and 12 which are arranged therein are formed with adjustment capability.
18 However, it is also possible to form the swirlers 15, 11 and/or 12 in each case without 19 adjustment capability.
21 During operation of the burner 1 according to the invention, pulverized coal is pneumatically 22 conveyed through the fuel conveying space 13 by dense phase conveyance inside the burner 1 23 along the burner axis 3. This fuel conveying space 13 is located radially outside the primary air 24 line 18 through which primary air is conveyed and which is formed by the inside space of the primary air tube 9 and the outer generated surface of the core air tube 5. The supplied primary 26 air is swirled in the discharge region of the primary air line 18, or of the primary air conveying 27 cross section, by means of swirlers 15, and mixes with the dense stream of fuel which leaves 28 the fuel conveying space 13. In the mixing cross section or mixing space 10, which is formed in 29 this region of the burner 1, a mixing-through of the two components, which are primary air and fuel, is carried out, forming an enrichment of the radial outer region of the developing air stream 31 with fuel, so that the coal material is conveyed into the region of the teeth of the stabilizing ring 32 14 and then discharges into the furnace 2. The primary air stream which is loaded with coal 33 particles in this way leaves the burner 1 with a conveying speed of about 15 - 25 m/s, preferably 34 18 - 20 m/s.
21772023.1 8 1 With the burner construction according to the invention, it is therefore possible to convey fuel by 2 pneumatic dense phase conveyance into the direct discharge region of a burner 1 and to first 3 mix the fuel with primary air there. Only the smaller cross sections which are required for the 4 dense phase conveyance are necessarily made available. Moreover, the swiriers 15 which cause swirling of the primary air are not exposed to the pulverized coal stream, so that these 6 are not subjected to wear loading by pulverized coal particles.
8 Even if the embodiment above represents a construction with a centrally arranged ignition 9 burner, then, however, it is also possible to provide burners which are constructed without core air feed and ignition burners. The necessary geometric conditions are then created depending 11 upon burner construction. According to the invention, it is only important in this case that 12 primary air is conveyed centrally on the inner side in a primary air tube with regard to the 13 longitudinal axis of the burner, and then, in a swirled state, is admixed with a fuel stream which 14 is conveyed radially outside the primary air stream in dense phase.
21772023.1 9
13 For the combustion of particulate fuel, especially pulverized coal and pulverized dry brown coal, 14 it is known to combust this in burners which in addition to a core air feed have a primary air feed, a secondary air feed and a tertiary air feed. Such burners are especially used in 16 conjunction with the firing of furnaces of large steam generators. The primary air feed, 17 secondary air feed and tertiary air feed in this case are formed and arranged in the form of 18 annular conveying cross sections, which are arranged concentrically to each other, or in the 19 form of concentric arrangements coaxially around a central core air tube, in which an oil burner lance or suchlike can be arranged. The pulverous fuel in this case as a rule is guided together 21 with the primary combustion air (primary air) in a primary air tube inside the burner to the burner 22 mouth. Swirlers, which are arranged on the outer side of the core jacket tube, are then provided 23 in this primary air tube and impart a desired swirl to the pulverized coal/primary air mixture, so 24 that as a result the combustion is optimized, but at least improved, especially with regard to a low-NOx combustion of the fuel. These burners as a rule are used in plants in which the 26 pulverous fuel is conveyed by means of a pneumatic conveyor from the mill directly to the 27 burner. Attached to this is the disadvantage of being operated with low transporting gas loads 28 and high conveying speeds in the process. This leads to an extensive wear of the transporting 29 tubes. Furthermore, the conveying tubes have relatively large dimensions (conveying cross sections).
32 For avoiding these disadvantages, a generic-type burner and a generic-type method, in which 33 the pulverous fuel is pneumatically conveyed to the burner, and in the bumer, by means of 34 dense phase in a dense phase conveying system, have already been proposed in DE 197 15 373 Al. With this, pulverized dry brown coal is conveyed in a single stage by means of a dense 21772023.1 1 phase conveying system, and with a transporting gas load of at least 60 kg of pulverized coal/kg 2 of transporting gas, or with a conveyed stream density of between 100 and 350 kg of pulverized 3 coal/m3, is fed to a steam generator burner. For controlling the mass stream of pulverized coal 4 and the loading of the conveying lines, water vapour or a hot inert gas, such as flue gas or nitrogen, is used as pneumatic conveying medium. In this case, burners are described in DE
6 197 15 973 Al, in which the fuel is fed to the burner in a central feed line, and then, during 7 discharge from this central line, is mixed with primary and secondary air streams which issue 8 from annular passage-form openings arranged concentrically around it, is dispersed, and 9 distributed into the furnace in a suspended state. Another burner has a central primary air tube which is concentrically encompassed by secondary and tertiary air lines. With this burner, the 11 fuel is introduced into the burner in a pulverized coal pipe which is guided in a coiled manner 12 around the primary air tube, and inside the burner is discharged into the secondary air passage 13 at a distance from the mouth opening of the burner.
This known burner indeed already has the advantage that the combustion air streams, which 16 are fed to the burner, and the fuel stream are spatially separated from each other so that a 17 dense phase conveyance of the fuel is possible, wherein transporting gas loads of over 20 kg of 18 pulverized coal/kg of transporting gas and conveying gas speeds of 3 to about 20 m/s at 19 pressures of < 10 bar, are understood by dense phase conveyance in the present application, but the combustion is not yet optimized with regard to a low-NOX combustion.
In particular, with 21 the so-called DS (swirl flow) burners, which are characterized by an especially low-NO,, 22 combustion, it is not possible to feed the pulverous fuel to the burner either in the central core 23 air tube or in a central air tube, or via an additional fuel conveying line which is guided in a 24 coiled manner in the secondary air feed passage. In order to achieve a low-NOx combustion, it is a technical aim to enrich the fuel concentration in the radially viewed outermost zone of the 26 primary air stream which is guided in the burner, before its discharge into the furnace, wherein 27 this enrichment is to be carried out uniformly over the circumference of the primary air jet. In the 28 case of the burners which are known from DE 197 15 973 Al, this aim is not achievable. In the 29 case of the burner with feed of fuel by dense phase conveyance through a central conveying tube, the feed of the fuel is directly centred in the region of the extension of the longitudinal axis 31 of the burner, so that the primary air stream which is arranged around it just has no enrichment 32 by fuel particles in its radial outer region. In the case of the other burner which is known from 33 this publication, the fuel is indeed conveyed in a secondary air stream which in the radial 34 direction is circumferentially arranged around the primary air stream.
However, this is carried out with a coiled conveying tube of small cross section so that the fuel discharges into the 21772023.1 2 1 secondary air only in a small area of the annular passage which conveys the secondary air, and 2 consequently there is no uniform distribution of the pulverous fuel over the cross section of the 3 entire annular conveying passage of the secondary air. Also, in this case, the fuel is conveyed 4 into the secondary air stream so that an enrichment of the outer region of the primary air stream with fuel is not carried out.
7 A pulverized coal burner for the steam-oxygen gasification of pulverized coal which is 8 introduced in dense phase, is indeed already known from DD 251 476 A3, in which the fuel, 9 which is uniformly distributed around a central feed of a combustion gas and of an oxidizing agent, via an annular passage cross section, is fed by dense phase conveyance.
In this case, 11 however, the admixing of a steam-oxidizing agent mixture is only then carried out in the further, 12 subsequent stream path outside a combustion chamber. This burner serves for the gasification 13 of the fuel and for producing a gasifying gas, which is why in addition to the oxidizing agent 14 steam is also blown into the pulverized coal stream. This technology, however, cannot be used with a burner for the firing of a furnace of a steam generator.
17 The invention is based on the object of creating a solution which makes it possible to equip a 18 low-NOX burner, which is suitable for firing the furnace of a steam generator, with a dense 19 phase conveyance of fuel, without disadvantageously affecting the low-NOX
combustion characteristic of the burner.
22 In the case of a burner of the type which is referred to in the introduction, this object is achieved 23 according to the invention by the inside space of the primary air tube being able to be 24 connected, or being connected, to a primary air feed line, and the fuel conveying space which is formed between the primary air tube and the fuel conveying tube being able to be connected, or 26 being connected, to the feed line which feeds pulverous fuel in dense phase to the burner.
28 In the case of a method of the type which is referred to in the introduction, this object is 29 achieved according to the invention by the fuel being conveyed inside the burner in an annular passage-form fuel conveying space which is formed radially outside a primary air line, and also 31 by the primary air stream which issues from the primary air line being admixed in a swirled state 32 with the fuel stream after discharge from the fuel conveying space inside the fuel conveying 33 tube.
21772023.1 3 1 By means of the invention, a solution is now created by which it is possible, without 2 disadvantageously affecting the low-NOx combustion characteristic of the burner, to feed 3 pulverous fuel to the burner by dense phase conveyance and to first mix the fuel with 4 combustion air in the bumer. This is achieved by an annular passage being formed and provided, in which just before the mouth region on the discharge side of the burner to the 6 fumace, the pulverous fuel, especially puiverized dry brown coal, is conveyed in the bumer 7 along the longitudinal axis of the burner. This annular passage in this case is concentrically 8 circumferentially arranged around the primary air stream. The primary air stream is now 9 furthermore swirled, for which swirlers are arranged and formed in the primary air stream at a suitable point, so that at the end of the annular passage-form conveying channel it mixes with 11 the fuel which is conveyed by dense phase conveyance, so that consequently at the mouth end 12 on the discharge side of the burner to the furnace the radially outer region of the primary air 13 stream is circumferentially uniformly enriched with the fuel, or there is fuel exclusively in this 14 region. By means of this measure, fuel is therefore conveyed by dense phase conveyance almost only in the outer circumferential region of the primary air stream.
This does not 16 disadvantageously affect the low-NOx combustion characteristics of the respective burner, on 17 the contrary these are assisted, boosted and optimized as a result. By means of the invention, 18 it is possible to maintain the swirling of the primary air stream and to distribute the pulverized 19 coal stream or coal mass stream uniformly over the circumference of the primary air stream on its radial outer edge region. Since, furthermore, the swiriers which are provided for swirling the 21 primary air stream are not arranged in the pulverized coal stream or coal mass stream, these 22 are also not exposed to the abrasive wear of the fuel particles, so that the burner according to 23 the invention is characterized as well by a reduced wear compared with the conveyance of fuel 24 in the primary air mixture.
26 In order to swirl the primary air stream and to be able to also use the dense phase conveyance 27 which is provided according to the invention with a swirl flow burner, it is expedient if at least 28 one swirler is arranged in the inside space of the primary air tube, which the invention provides 29 in a development.
31 In order to also be able to operate the bumer with an oil bumer lance or suchlike, it is 32 advantageous according to a development of the invention if a core air tube is arranged 33 concentrically to the primary air tube within it. An oil burner lance or suchlike, as this is known 34 from customary burners, can then be arranged in the core air tube.
21772023.1 4 1 Since the conveyance of the particulate fuel, especially pulverous fuel, is carried out in dense 2 phase, large conveying cross sections, such as annular passage cross sections or pipeline 3 cross sections, are not necessary for this conveyance, so that the invention is furthermore 4 characterized in that the radial distance between core air tube and primary air tube is greater than the radial distance between primary air tube and fuel conveying tube.
7 In this case, it is furthermore especially advantageous and especially expedient if the core air 8 tube extends in the longitudinal axial direction beyond the mouth end on the discharge side of 9 the primary air tube into the region of the mouth opening on the discharge side of the fuel conveying tube. As a result of this, a mixing chamber, in which the swirled primary air stream 11 and the dense stream conveyed stream of fuel are mixed with each other, is formed inside the 12 burner at the mouth end on the discharge side of the burner to the furnace.
As a result of this, it 13 is especially possible to re-use the geometry of previously existing burners and to retrofit these 14 simply by introducing a new primary air tube for the combustion of fuel which is conveyed in dense phase. The originally available primary air tube then becomes the fuel conveying tube.
16 Greater or more costly constructional steps are not to be otherwise taken on the furnace which 17 is provided with burners.
19 Since for conveying the primary air stream a furthermore relatively larger opening cross section is made available, it is possible to arrange there a plurality of swirlers, to arrange these on the 21 outer generated surface of the core air tube, especially when a central coaxial core air tube is 22 available. The invention, therefore, furthermore provides that a plurality of swirlers, preferably in 23 the form of a vane ring, circumferentially distributed on the outer surface of the core air tube, are 24 arranged radially on the outer side in the annular passage to the primary air tube.
26 Furthermore, it is advantageous if the burner according to the invention is also equipped with an 27 oil burner ignition lance, for which reason, according to a development of the invention, an 28 ignition lance, especially an oil burner ignition lance, is arranged coaxially in the core air tube.
Since with the configuration according to the invention especially low-NOX
burners are to be 31 provided, it is expedient if these additionally also have a secondary air feed and a tertiary air 32 feed. The invention, therefore, is further characterized by a secondary air feed which 33 encompasses the fuel conveying tube, and also a tertiary air feed which encompasses the 34 secondary air feed.
21772023.1 5 1 In a further expedient development, it is then also expedient, especially for low-NOx burners, if a 2 radially inwards extending stabilizing ring is arranged at the end on the combustion chamber 3 mouth side of the fuel conveying tube.
The method according to the invention in an expedient development first of all provides that the 6 primary air is admixed with the fuel stream in the mouth region of the burner in a mixing 7 chamber before discharging into the furnace. As a result of this, the possibility arises of using 8 the geometry of existing burners and of creating an intensive mixture of primary air and 9 pulverous fuel for low-NOx combustion. Finally, in this case then it is still especially advantageous if air, especially heated air, recirculated flue gas or a mixture of air and 11 recirculated flue gas, is fed to the burner as primary air.
13 The invention is subsequently exemplarily explained in more detail with reference to a drawing.
14 This shows in the single figure, in schematic view in detail, a cross section along the longitudinal axis of the end on the combustion chamber side of a low-NOx burner which is arranged in the 16 wall of a combustion chamber or of a furnace of a steam generator, especially of a large power 17 plant.
19 The burner 1, on the discharge side, leads into the combustion chamber or into the furnace 2 of a steam generator and is arranged in its circumferential wall. The burner 1 has an oil burner 21 ignition lance 4 which is arranged centrally along its longitudinal axis 3.
This is arranged in the 22 centre of a core air tube 5 which coaxially encompasses the oil burner ignition lance 4. The air 23 guiding device 6, which is arranged around the oil burner ignition lance 4 at its end which faces 24 the furnace 2, ends flush with the mouth end on the burner discharge side of a fuel conveying tube 7, in which primary air, which is fed to the burner through a primary air line 18 and mixed 26 with particulate fuel which is fed through the fuel conveying tube 7, discharges into the furnace 27 2. The fuel conveying tube 7 is concentrically arranged around the oil burner ignition lance 4 28 and also around the core air tube 5, and with the outer generated surface of a primary air tube 29 9, and, downstream of the end of the primary air tube towards the furnace 2, with the outer generated surface of the core air tube 5, forms in each case an annular passage-form 31 conveying cross section. At the end on the combustion chamber discharge side of the fuel 32 conveying tube 7, an air deflecting throat 8, which extends over the whole circumference of the 33 fuel conveying tube 7, is formed on the outer side. On the inner side of the fuel conveying tube 34 7, a stabilizing ring 14, which is provided with teeth, extends in this region radially inwards into the conveying cross section of the fuel conveying tube 7 and forms the termination of the fuel 21772023.1 6 1 conveying tube 7 at this point. The core air tube 5 terminates on the burner inner side at a 2 distance to the mouth end on the combustion chamber discharge side of the fuel conveying tube 3 7 in the region of the air guiding device 6.
In the annular passage-form conveying cross section, which is formed between core air tube 5 6 and fuel conveying tube 7, the primary air tube 9 is arranged coaxially to the core air tube 5 and 7 to the fuel conveying tube 7 so that a fuel conveying space 13 is formed with an annular 8 passage-form conveying cross section. The mouth end of the primary air tube 9 which faces 9 the furnace 2 terminates at a distance from the mouth ends on the burner discharge side both of the core air tube 5 and of the fuel conveying tube 7, so that on the burner inner side a mixing 11 cross section or mixing chamber 10 is formed. The end on the mouth side of the primary air 12 tube 9 is located approximately in the region of the arrangement of swirlers 15 which in the case 13 of low-NOX burners are customarily provided in the primary air stream. In the exemplary 14 embodiment, the primary air tube 9 extends into the burner 1 to such an extent that its end on the mouth side is arranged in the positioning region of adjustable swirlers 11, 12 which are 16 located in a secondary air feed 19 and in a tertiary air feed 20. The primary air tube 9, 17 furthermore, is arranged relative to the core air tube 5 and to the fuel conveying tube 7 in such a 18 way that its radial distance to the core air tube 5 is greater than to the fuel conveying tube 7.
19 Therefore, the annular passage-form fuel conveying space 13 is formed between the outer side of the primary air tube 9 and the inner side of the fuel conveying tube 7.
This annular fuel 21 conveying space 13 is connected, or can be connected, to a feed line, which is not shown, by 22 which fuel is pneumatically fed by dense phase conveyance to the burner 1, and then is also 23 pneumatically conveyed in the fuel conveying space 13 in dense phase. The fuel is particulate 24 fuel, especially pulverized coal, preferably pulverous dry brown coal. The dense phase conveyance is carried out with a load of 20 - 90 kg of pulverized coal/kg of conveying gas, and a 26 conveying speed of 3 to 20 m/s at pressures of < 10 bar. The radial distance between the outer 27 side of the primary air tube 9 and the inner side of the fuel conveying tube 7, and consequently 28 the passage height of the fuel conveying cross section or fuel conveying space 13, can be 29 approximately as great as the length by which the teeth of the stabilizing ring 14 extend radially inwards in the direction of the burner axis 3.
32 Primary air is fed to the burner 1 through the annular passage-form conveying cross section 33 which is formed between the inner side of the primary air tube 9 and the outer side of the core 34 air tube 5. The primary air can be air, especially preheated air, but can also be recirculated flue gas or a mixture of recirculated flue gas and air. The primary air, which is conveyed through the 21772023.1 7 1 primary air line 18 with circular passage-form conveying cross section, when discharging is 2 transferred into a swirled stream by means of adjustable swirlers 15 which are arranged on the 3 inner side on the primary air tube 9 between core air tube 5 and primary air tube 9 at the end on 4 the discharge side. The swirlers 15 are formed in the form of a vane ring consisting of guide vanes which are arranged in a uniformly distributed manner on the outer circumference of the 6 core air tube 5.
8 Furthermore, the burner 1, as known from customary burners, has a secondary air tube 16 9 which is arranged on the outer side coaxially around the fuel conveying tube 7, and a tertiary air tube 17 which in turn is arranged on the outer side coaxially at a distance around the secondary 11 air tube. Secondary air is fed through the secondary air tube 16 to the furnace 2, and tertiary air 12 is fed through the tertiary air tube 17 to the furnace 2, as this is known from known burners for 13 creating a multistage low-NOx combustion.
For controlling a possibly desired swirling both of the primary air and of the secondary air in the 16 secondary air feed and of the tertiary air in the tertiary air feed, it is provided that the respective 17 swirlers 15, 11 and 12 which are arranged therein are formed with adjustment capability.
18 However, it is also possible to form the swirlers 15, 11 and/or 12 in each case without 19 adjustment capability.
21 During operation of the burner 1 according to the invention, pulverized coal is pneumatically 22 conveyed through the fuel conveying space 13 by dense phase conveyance inside the burner 1 23 along the burner axis 3. This fuel conveying space 13 is located radially outside the primary air 24 line 18 through which primary air is conveyed and which is formed by the inside space of the primary air tube 9 and the outer generated surface of the core air tube 5. The supplied primary 26 air is swirled in the discharge region of the primary air line 18, or of the primary air conveying 27 cross section, by means of swirlers 15, and mixes with the dense stream of fuel which leaves 28 the fuel conveying space 13. In the mixing cross section or mixing space 10, which is formed in 29 this region of the burner 1, a mixing-through of the two components, which are primary air and fuel, is carried out, forming an enrichment of the radial outer region of the developing air stream 31 with fuel, so that the coal material is conveyed into the region of the teeth of the stabilizing ring 32 14 and then discharges into the furnace 2. The primary air stream which is loaded with coal 33 particles in this way leaves the burner 1 with a conveying speed of about 15 - 25 m/s, preferably 34 18 - 20 m/s.
21772023.1 8 1 With the burner construction according to the invention, it is therefore possible to convey fuel by 2 pneumatic dense phase conveyance into the direct discharge region of a burner 1 and to first 3 mix the fuel with primary air there. Only the smaller cross sections which are required for the 4 dense phase conveyance are necessarily made available. Moreover, the swiriers 15 which cause swirling of the primary air are not exposed to the pulverized coal stream, so that these 6 are not subjected to wear loading by pulverized coal particles.
8 Even if the embodiment above represents a construction with a centrally arranged ignition 9 burner, then, however, it is also possible to provide burners which are constructed without core air feed and ignition burners. The necessary geometric conditions are then created depending 11 upon burner construction. According to the invention, it is only important in this case that 12 primary air is conveyed centrally on the inner side in a primary air tube with regard to the 13 longitudinal axis of the burner, and then, in a swirled state, is admixed with a fuel stream which 14 is conveyed radially outside the primary air stream in dense phase.
21772023.1 9
Claims (13)
1. Burner, especially pulverized coal burner (1), with a fuel conveying tube (7) and a primary air tube (9) which is concentrically arranged within it, wherein the primary air tube (9) on the mouth discharge side terminates at a distance to the mouth opening of the fuel conveying tube (7), and the burner (1) is connected, or can be connected, to a feed line which conveys pulverous fuel in dense phase, characterized in that the inside space of the primary air tube (9) can be connected, or is connected, to a primary air feed line (18), and the fuel conveying space (13), which is formed between the primary air tube (9) and the fuel conveying tube (7), can be connected, or is connected, to the feed line which feeds pulverous fuel in dense phase to the burner.
2. Burner according to Claim 1, characterized in that at least one swirler (15) is arranged in the inside space of the primary air tube (9).
3. Burner according to either of Claims 1 or 2, characterized in that a core air tube (5) is arranged concentrically to the primary air tube (9) within it.
4. Burner according to Claim 3, characterized in that the radial distance between core air tube (5) and primary air tube (9) is greater than the radial distance between primary air tube (9) and fuel conveying tube (7).
5. Burner according to either of Claims 3 or 4, characterized in that the core air tube (5), in the longitudinal axial direction, extends beyond the mouth end on the discharge side of the primary air tube (9) into the region of the mouth opening on the discharge side of the fuel conveying tube (7).
6. Burner according to one of Claims 3 to 5, characterized in that a plurality of swirlers (15), preferably in the form of a vane ring, circumferentially distributed on the outer surface of the core air tube (5), are arranged radially on the outer side in the annular passage to the primary air tube (9).
7. Burner according to one of the preceding claims, characterized in that an ignition lance, especially an oil burner ignition lance (4), is coaxially arranged in the core air tube (5).
8. Burner according to one of the preceding claims, characterized by a secondary air feed (19) which encompasses the fuel conveying tube (7).
9. Burner according to one of the preceding claims, characterized by a tertiary air feed (20) which encompasses the secondary air feed (19).
10. Burner according to one of the preceding claims, characterized in that a radially inwards extending stabilizing ring (14) is arranged at the end on the combustion chamber mouth side of the fuel conveying tube (7).
11. Method for combusting particulate fuel, especially pulverized coal, preferably dry brown coal, in a burner (1) with primary air tube (9) and fuel conveying tube (7), wherein the fuel is fed to the burner (1) by dense phase conveyance, and by dense phase conveyance is conveyed inside the burner (1) along the longitudinal axis (3) of the burner, and mixed with combustion air, characterized in that the fuel is conveyed inside the burner (1) in an annular passage-form fuel conveying space (13) which is formed radially outside a primary air line (18), and also the primary air stream, which issues from the primary air line (18), is admixed in a swirled state with the fuel stream after discharge from the fuel conveying space (13) inside the fuel conveying tube (7).
12. Method according to Claim 11, characterized in that the primary air is admixed with the fuel stream in the mouth region of the burner (1) in a mixing space (10) before discharge into the furnace (2).
13. Method according to either of Claims 11 or 12, characterized in that air, especially heated air, recirculated flue gas or a mixture of air and recirculated flue gas, is fed to the burner (1) as primary air.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102007030269.1-13 | 2007-06-28 | ||
| DE102007030269.1A DE102007030269B4 (en) | 2007-06-28 | 2007-06-28 | Pulverized coal burner for burning fuel supplied in dense phase conveying |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2632412A1 true CA2632412A1 (en) | 2008-12-28 |
Family
ID=39743804
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002632412A Abandoned CA2632412A1 (en) | 2007-06-28 | 2008-05-23 | Pulverized coal burner for firing fuel which is fed by dense phase conveyance |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US20090000532A1 (en) |
| EP (1) | EP2009351B1 (en) |
| JP (1) | JP2009024991A (en) |
| CN (1) | CN101334166A (en) |
| AT (1) | ATE525615T1 (en) |
| AU (1) | AU2008202470B2 (en) |
| CA (1) | CA2632412A1 (en) |
| DE (1) | DE102007030269B4 (en) |
| PL (1) | PL2009351T3 (en) |
| RU (1) | RU2008123264A (en) |
| SI (1) | SI2009351T1 (en) |
| ZA (1) | ZA200805541B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102767824A (en) * | 2012-07-06 | 2012-11-07 | 南阳市沧田工程机械有限公司 | Novel efficient pulverized coal combustion device |
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| JO3598B1 (en) * | 2006-10-10 | 2020-07-05 | Infinity Discovery Inc | Boronic acids and esters as inhibitors of fatty acid amide hydrolase |
| DE102007025051B4 (en) * | 2007-05-29 | 2011-06-01 | Hitachi Power Europe Gmbh | Cabin gas burner |
| SI2369230T1 (en) | 2010-03-22 | 2015-12-31 | Mitsubishi Hitachi Power Systems Europe Gmbh | Burner with tangential spiral intake elbow |
| DE102010030904B4 (en) | 2010-07-02 | 2017-07-27 | Mitsubishi Hitachi Power Systems Europe Gmbh | Burner with tangential spiral inlet manifold |
| US20110271885A1 (en) * | 2010-05-04 | 2011-11-10 | Hans Tim Chadwick | Method and apparatus for improving combustion efficiency of carbonaceous fuel-fired furnaces by injecting oxyhydrogen gas |
| US20120103237A1 (en) * | 2010-11-03 | 2012-05-03 | Ronny Jones | Tiltable multiple-staged coal burner in a horizontal arrangement |
| KR101065594B1 (en) | 2011-06-13 | 2011-09-19 | 한국기계연구원 | Low nox combustor with air staging |
| GB201114894D0 (en) | 2011-08-30 | 2011-10-12 | Doosan Power Systems Ltd | Combustion apparatus |
| GB201202907D0 (en) | 2012-02-21 | 2012-04-04 | Doosan Power Systems Ltd | Burner |
| CN102878553B (en) * | 2012-09-17 | 2015-05-20 | 华中科技大学 | Anti-slag-bonding whirling pulverized coal combustor with low NOx |
| CN103062764B (en) * | 2013-01-25 | 2015-11-18 | 福建永恒能源管理有限公司 | A kind of low nitrogen powder fuel combustor |
| DE102013111504B4 (en) | 2013-10-18 | 2017-12-07 | Mitsubishi Hitachi Power Systems Europe Gmbh | Method for igniting a power plant burner and suitable pulverized coal burner |
| CN103528059A (en) * | 2013-11-12 | 2014-01-22 | 哈尔滨前程科技发展有限公司 | Multifunction substep high-oxygen combustor for industrial furnace |
| US10126015B2 (en) | 2014-12-19 | 2018-11-13 | Carrier Corporation | Inward fired pre-mix burners with carryover |
| CN106594711A (en) * | 2016-12-28 | 2017-04-26 | 浙江宜清环境技术有限公司 | Low-nitrogen combustion device for chain furnace |
| CN108728168A (en) * | 2017-04-14 | 2018-11-02 | 航天长征化学工程股份有限公司 | Gasification burner |
| CN107726310A (en) * | 2017-11-22 | 2018-02-23 | 北京神雾电力科技有限公司 | A kind of New-type Swirl Flow coal burner |
| CN110566944A (en) * | 2019-09-09 | 2019-12-13 | 内蒙古工业大学 | aggregate drying pulverized coal burner with tooth-shaped stable combustion device and control method thereof |
| DE102021002508A1 (en) * | 2021-05-12 | 2022-11-17 | Martin GmbH für Umwelt- und Energietechnik | Nozzle for injecting gas into an incinerator with a tube and a swirler, flue with such a nozzle and method for using such a nozzle |
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| US4776289A (en) * | 1987-06-18 | 1988-10-11 | Fuel Tech, Inc. | Method and apparatus for burning pulverized solid fuel |
| DE19527083A1 (en) * | 1995-07-25 | 1997-01-30 | Lentjes Kraftwerkstechnik | Process and burner for reducing NO¶x¶ formation from coal dust combustion |
| AT402963B (en) * | 1995-09-07 | 1997-10-27 | Voest Alpine Ind Anlagen | METHOD FOR BURNING FUEL |
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| RS50092B (en) * | 2000-08-04 | 2009-01-22 | Babcock-Hitachi Kabushiki Kaisha, | Solid fuel burner and method of combustion using solid fuel burner |
| DE102006011326C5 (en) * | 2006-03-09 | 2015-03-19 | Alstom Technology Ltd. | circular burner |
| US8961170B2 (en) * | 2007-05-14 | 2015-02-24 | Babcock-Hitachi K.K. | Dust coal boiler, dust coal combustion method, dust coal fuel thermal power generation system, and waste gas purification system for dust coal boiler |
-
2007
- 2007-06-28 DE DE102007030269.1A patent/DE102007030269B4/en active Active
-
2008
- 2008-05-20 JP JP2008132098A patent/JP2009024991A/en active Pending
- 2008-05-23 CA CA002632412A patent/CA2632412A1/en not_active Abandoned
- 2008-06-04 AU AU2008202470A patent/AU2008202470B2/en not_active Ceased
- 2008-06-11 CN CNA2008100997861A patent/CN101334166A/en active Pending
- 2008-06-16 RU RU2008123264/06A patent/RU2008123264A/en not_active Application Discontinuation
- 2008-06-19 EP EP08158605A patent/EP2009351B1/en not_active Not-in-force
- 2008-06-19 PL PL08158605T patent/PL2009351T3/en unknown
- 2008-06-19 AT AT08158605T patent/ATE525615T1/en active
- 2008-06-19 SI SI200830490T patent/SI2009351T1/en unknown
- 2008-06-23 US US12/144,236 patent/US20090000532A1/en not_active Abandoned
- 2008-06-25 ZA ZA2008/05541A patent/ZA200805541B/en unknown
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102767824A (en) * | 2012-07-06 | 2012-11-07 | 南阳市沧田工程机械有限公司 | Novel efficient pulverized coal combustion device |
| CN102767824B (en) * | 2012-07-06 | 2015-08-05 | 南阳市沧田工程机械有限公司 | A kind of new and effective coal powder burner |
Also Published As
| Publication number | Publication date |
|---|---|
| ATE525615T1 (en) | 2011-10-15 |
| AU2008202470B2 (en) | 2010-10-28 |
| DE102007030269B4 (en) | 2014-07-17 |
| EP2009351A3 (en) | 2009-11-04 |
| ZA200805541B (en) | 2009-12-30 |
| US20090000532A1 (en) | 2009-01-01 |
| JP2009024991A (en) | 2009-02-05 |
| PL2009351T3 (en) | 2012-02-29 |
| DE102007030269A1 (en) | 2009-01-02 |
| EP2009351A2 (en) | 2008-12-31 |
| AU2008202470A1 (en) | 2009-01-15 |
| CN101334166A (en) | 2008-12-31 |
| RU2008123264A (en) | 2009-12-27 |
| EP2009351B1 (en) | 2011-09-21 |
| SI2009351T1 (en) | 2012-01-31 |
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Legal Events
| Date | Code | Title | Description |
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| EEER | Examination request |
Effective date: 20130214 |
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| FZDE | Discontinued |
Effective date: 20150911 |