US20150300633A1 - Burner tip and burner - Google Patents

Burner tip and burner Download PDF

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Publication number
US20150300633A1
US20150300633A1 US14/648,810 US201314648810A US2015300633A1 US 20150300633 A1 US20150300633 A1 US 20150300633A1 US 201314648810 A US201314648810 A US 201314648810A US 2015300633 A1 US2015300633 A1 US 2015300633A1
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US
United States
Prior art keywords
burner
burner tip
wall
displacement body
pilot
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US14/648,810
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English (en)
Inventor
Christoph Kiener
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Siemens AG
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Siemens AG
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Assigned to SIEMENS AKTIENGESELLSCHAFT reassignment SIEMENS AKTIENGESELLSCHAFT ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KIENER, CHRISTOPH
Publication of US20150300633A1 publication Critical patent/US20150300633A1/en
Abandoned legal-status Critical Current

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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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/48—Nozzles
    • F23D14/58—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/76—Protecting flame and burner parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/78—Cooling burner parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23Q—IGNITION; EXTINGUISHING-DEVICES
    • F23Q9/00—Pilot flame igniters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2214/00—Cooling

Definitions

  • the present invention relates to a burner tip, especially to a burner tip for high-temperature applications in synthesis gas production.
  • the invention relates to a burner, especially to a burner for synthesis gas production.
  • a burner for a synthesis gas reactor is described schematically in DE 10 2008 006 572 A1.
  • This comprises an outer burner element having a tip with a cavity and with a displacement body arranged in the cavity. Guided around the displacement body is a cooling water passage for cooling the burner tip.
  • the burner also comprises an inner burner element which is arranged concentrically to an outer tube. A passage is formed between the inner burner element and the outer burner element for the feed of a pulverized fuel, for example pulverized coal.
  • the inner burner element in the region of its tip, has a cavity with a displacement body arranged therein.
  • a cooling water passage is guided around the cavity and cools the tip of the inner burner element.
  • a pilot burner is arranged centrally to the inner burner element, wherein a feed passage for an oxygen/steam mixture is formed between the inner burner element and the pilot burner.
  • the pilot burner is of a hollow walled design, having a displacement body in the region of the tip of the pilot burner and around the body is guided a cooling water passage to be able to cool the pilot burner tip.
  • the tips of burners in synthesis gas reactors are subjected to high temperatures during operation of the reactors providing a considerable heat input into the burner tip.
  • the inputted heat is dissipated by means of the cooling water flowing in the described cooling water passages.
  • the burner tip can also be provided with a thermal barrier coating, as is described in DE 10 2008 006 572 A1.
  • the respective burner elements are usually constructed from a plurality of tubes and a tip which interconnects the tubes and in which a displacement body is also arranged.
  • the tip in this case is usually assembled from an outer annular part and an inner annular part, wherein the outer annular part is connected to the outer tube and the inner annular part is connected to the inner tube.
  • the annular parts are welded together by their ends which face away from the outer tube or the inner tube.
  • the displacement body is connected to a centrally arranged tube which divides the interspace between the outer tube and the inner tube into an annular feed passage for cooling water and an annular discharge passage for cooling water.
  • Each burner element therefore has a complex construction.
  • the burner tips are relatively large, and therefore heavy, which reduces their manageability, for example in the course of maintenance.
  • the wall thicknesses of the tubes or of the tip parts are typically at least 3 mm, which makes heat dissipation difficult and increases the susceptibility to temperature fluctuations. Furthermore, suspended particles and cooling water can lead over time to a constriction of the cooling water passages in the region of the burner tip or even to blocking of the cooling water passages, which entails an increased maintenance requirement so that such constrictions can be discovered in good time.
  • the materials from which the burner tips are produced are expensive and time consuming in processing since the parts of which the burner tips consist have to be welded together.
  • the welding of the parts for forming the respective burner tip is not simple since the typically used nickel-based superalloys require special welding procedures.
  • a burner tip with a burner discharge orifice and at least one burner tip part which encompasses the burner discharge orifice and has a burner-tip wall with an end wall which forms a closed end of the burner tip part.
  • the burner tip part in its interior has a cavity which reaches up the end wall and the burner-tip wall has an inner side pointing towards the cavity.
  • a displacement body with an outer side facing the inner side of the burner-tip wall, is arranged in the cavity, wherein at least one flow passage is formed between the inner side of the burner-tip wall and the outer side of the displacement body.
  • the displacement body is connected to the inner side of the burner-tip wall via support structures which extend from the outer side of the displacement body to the inner side of the burner-tip wall.
  • the position of the displacement body inside the burner-tip wall can be fixed. Furthermore, the entire structure consisting of burner-tip wall and displacement body can be of an altogether more stable design.
  • the support structures can be designed especially as rib-like or pillar-like structures, wherein adjacent rib-like or pillar-like structures converge to form arches on the outer side of the displacement body and/or on the inner side of the burner-tip wall, at least in the region of the burner tip end wall. These arches can especially be designed as pointed arches similar to the arches in gothic architecture.
  • the design of the support structures as rib-like or pillar-like structures with converging arches enables the production of the burner tip by means of an additive manufacturing process, for example by means of selective laser melting.
  • the density of support structures which connect the displacement body to the burner-tip wall, is increased at least in the region of the end wall in comparison to other regions of the burner-tip wall.
  • the burner-tip wall can then be of a thinner design in comparison to regions without increased density of support structures. They can especially have thicknesses of below 3 mm, for example thicknesses in the region of 0.5 to 2 mm. In this way, in regions which are subjected to especially high temperatures and/or to especially pronounced temperature fluctuations the heat which is absorbed by the burner-tip wall can be dissipated more rapidly to the cooling fluid.
  • the thinner wall can be kept cooler than a thicker wall, which in turn has a favorable effect upon the available operating period up to a maintenance.
  • the displacement body can especially be formed in one piece with the support structures and the burner-tip wall. This allows a particularly stable structure and enables the production with a large number of structures at the outset.
  • the production can in this case be carried out by means of an additive manufacturing process, for example by means of selective laser melting.
  • the burner-tip wall can be lined with a thermal barrier coating, at least in the region of the end wall.
  • a thermal barrier coating at least in the region of the end wall.
  • the thermal barrier coating is applied to the thinner regions, especially in the region of the end wall, is advantageous. Due to the fact that in this embodiment the burner-tip wall is thinner in the regions with a thermal barrier coating, it can achieve the effect of the entire wall thickness in these regions, despite the applied thermal barrier coating, not exceeding the thickness of the remaining regions without a thermal barrier coating.
  • the displacement body in the burner tip according to the invention can especially be of hollow design.
  • a saving can be made in weight and material in comparison to burner tips according to the prior art in which the displacement body is designed as a solid body.
  • the burner tip which can have diameters of 50 cm and more, is easier to manage, for example in the course of a maintenance or repair process.
  • this has near end in relation to the end wall, a far end in relation to the end wall, an interior space, and, in the region of the far end, has at least one opening which is open towards the interior space.
  • a cooling fluid for example cooling water
  • a flow guiding element can be arranged in the displacement-body opening in such a way that it divides the displacement-body opening into an inflow section and an outflow section and in such a way that a flow path around the flow guiding element is formed between the inflow section and the outflow section.
  • the displacement body has at least one additional opening which is open towards the interior space. This is then arranged between the near end of the displacement body and the displacement-body opening which is arranged in the region of far end. Between the displacement-body opening and the additional displacement-body opening, the displacement-body interior space forms a flow path for cooling fluid, such as cooling water.
  • a collecting chamber, branching from the flow path, for foreign bodies in the fluid flowing through the flow path can be located in the displacement-body interior space.
  • the collecting chamber in the displacement-body interior space is located in a region of the flow path in which a change of flow direction takes place. It is especially advantageous if the change of flow direction entails a substantial flow reversal. In this case, the space in the hollow displacement body is sufficient in order to provide an adequately large collecting chamber.
  • the collecting of foreign bodies, such as suspended particles, in the cooling fluid leads to the fluid passages leading around the outer side of the displacement body blocking more slowly and as a result a constriction of the flow cross section can be delayed for a longer period. This in turn has a favorable effect upon the maintenance intervals.
  • swirl vanes which at least partially project into the burner discharge orifice, can also be formed in one piece with the burner-tip wall.
  • swirl vanes have been inserted from the burner side facing away from the burner tip into the burner discharge orifice which is encompassed by the burner-tip wall. With this insertion, damage to the swirl vanes and/or to the burner tip wall can occur.
  • the insertion of swirl vanes is superfluous.
  • the flow passage which is formed between the inner side of the burner-tip wall and the outer side of the displacement body also extends at least partially through the swirl vanes.
  • the swirl blading assembly can also additionally be given the form of a nozzle which decreases the flow passage of the oxygen-steam mixture in specific regions.
  • the burner-tip wall and the displacement body are of toroidal design.
  • a burner tip with a burner discharge orifice and at least one burner tip part which encompasses the burner discharge orifice and has a burner-tip wall with an end wall which forms a closed end of the burner tip part.
  • swirl vanes which at least partially project into the burner discharge orifice, are formed in one piece with the burner-tip wall.
  • swirl vanes were inserted from the burner side facing away from the burner tip into the burner discharge orifice which is encompassed by the burner wall. With this insertion, damage to the swirl vanes and/or to the burner tip wall can occur. As a result of the one-piece design of the swirl vanes with the burner-tip wall, the insertion of swirl vanes is superfluous.
  • the flow passage which is formed between the inner side of the burner-tip wall and the outer side of the displacement body also extends at least partially through the swirl vanes. In this way, a common cooling of burner tip and swirl vanes is made possible.
  • a burner according to the invention is provided with a burner tip according to the invention.
  • the characteristics and advantages associated therewith are gathered from those of the burner tip according to the invention.
  • FIG. 1 shows a schematic diagram of a burner, as is used in synthesis gas reactors.
  • FIG. 2 shows the tip of a first burner element.
  • FIG. 3 shows the tip of a second burner element.
  • FIG. 4 shows the tip of pilot burner used in the burner.
  • FIG. 5 shows an alternative embodiment of the tip from FIG. 3 .
  • FIG. 6 shows a further alternative embodiment of the tip from FIG. 3 .
  • FIG. 7 shows yet another alternative embodiment from FIG. 3 .
  • FIG. 8 shows the embodiment from FIG. 7 in a section along the line VIII-VIII.
  • the burner is constructed in a rotationally symmetrical manner around a burner axis A and comprises a tubular feed line section and a burner tip 1 which is connected to the feed line section and encompasses a burner orifice 3 .
  • the burner comprises a first, outer burner element 2 which in the tubular section of the burner is formed from three inter-inserted tubes 4 , 6 , 8 .
  • a cooling fluid feed passage 7 and a cooling fluid discharge passage 9 are formed between the tubes.
  • cooling fluid water is especially considered.
  • the outer burner element 2 deviates from the pure tubular shape and is inclined in the direction towards the center of the burner discharge orifice 3 .
  • the region of the tip it has a cavity in which a displacement body 5 is arranged at a distance from the wall of the burner element 2 in this region.
  • a flow passage 10 formed in this case between the inner side of the wall 11 A of the burner element 2 in the tip region and the outer side of the displacement body is a flow passage 10 by means of which the cooling fluid, for example water, is directed through the tip of the outer burner element 2 in order to cool this.
  • the part of the outer burner element 2 which deviates from the tubular shape constitutes an outer burner tip part 11 which is formed as an independent part and the wall 11 A of which is welded to the tubular section of the outer burner element 2 .
  • the wall 11 A of the burner tip part 11 has an approximately U-shaped bend so that it can be connected both to the outer tube 4 and to the inner tube 8 of the tubular section of the outer burner element 2 .
  • the displacement body 5 is fitted onto the center tube 6 . To this end, it has a groove 5 A, the width of which is adapted to the wall thickness of the center tube 6 of the tubular section.
  • the burner furthermore comprises an inner burner element 12 which apart from in the region of the burner tip 1 is also formed from three inter-inserted tubes 14 , 16 , 18 .
  • an inner burner tip part 21 In the region of the burner tip 1 , an inner burner tip part 21 , with a cavity located therein, is connected to the tubular section of the inner burner element 12 .
  • a displacement body 15 is arranged in this cavity, wherein the outer side of the displacement body has a distance from the inner side of the burner-tip wall 21 A in the region of the inner burner tip part 21 so that a flow passage is formed between the two.
  • the feed of cooling fluid into the flow passage is carried out via a feed passage 17 which is formed between the inter-inserted tubes 14 , 16 of the tubular section of the inner burner element 12
  • the discharge of the cooling fluid from the region of the inner burner tip part 21 is carried out via a discharge passage 19 which is formed between the inter-inserted tubes 16 , 18
  • the inner burner tip part is designed as an independent part, the wall 21 A of which is welded to the outer tube 14 and to the inner tube 18 of the tubular section.
  • the wall 21 A in the widest sense is bent in a U-shaped manner so that it can be welded both to the outer tube 14 and to the inner tube 18 of the three inter-inserted tubes 14 , 16 , 18 of the tubular section.
  • the displacement body 15 is fitted onto the center tube 16 of the tubular section. To this end, it has a groove 15 A, the width of which is adapted to the wall thickness of the center tube 16 .
  • the inner burner element 12 has an outside diameter which is smaller than the inside diameter of the outer burner element 2 so that an annular passage is formed between the two, serving for the feed of a pulverized fuel, for example for the feed of pulverized coal.
  • the inner burner element 12 encloses a largely cylindrical chamber in which is arranged a pilot burner 22 .
  • this pilot burner comprises a tubular section 22 A which is formed from three tubes 24 , 26 , 28 and to which is connected a pilot burner tip part 31 in the region of the burner tip 1 .
  • the pilot burner tip part 31 has a cavity in which is arranged a displacement body 25 , wherein the outer side of the displacement body has a distance from the inner side of the wall 31 A of the pilot burner tip part 31 so that a flow passage 30 is formed between the two.
  • the wall 31 A of the tip part 31 is welded to the tubular section.
  • the wall 31 A of the pilot burner tip part 31 is bent in this case in the widest sense in a U-shaped manner so that on one side it can be welded to the outer tube 24 of the tubular section of the pilot burner 22 and to the inner tube 28 of the tubular section of the pilot burner 22 .
  • the displacement body 25 is fitted onto the center tube 26 of the tubular section. To this end, it has a groove 25 A, the width of which is adapted to the wall thickness of the center tube 26 .
  • the tubular section of the pilot burner 22 has an outside diameter which is smaller than the inside diameter of the inner burner element 12 so that an oxygen/steam passage 23 is formed between the two.
  • This serves for the feed of water vapor which is required in the synthesis gas reactor for converting pulverized fuel into synthesis gas, and, if necessary, for the feed of oxygen or air.
  • the supplied water vapor, and, if necessary, the supplied oxygen or the supplied air is swirled in order to promote the synthesis gas reaction.
  • swirl vanes 32 are arranged in the region of the burner tip 1 between the inner burner element 12 and the pilot burner 22 .
  • the pilot burner 22 encloses an essentially cylindrical cavity in which are arranged an ignition burner and a device for flame monitoring. These two elements are shown in only a greatly schematized form in FIG. 1 and are grouped under the designation 33 .
  • FIG. 2 shows the construction of the outer burner tip part 11 . Also to be seen are the inter-inserted tubes 4 , 6 , 8 of the tubular section of the outer burner element 2 .
  • the outer burner tip part 11 terminates in an end wall 34 which constitutes the end of the outer burner tip part.
  • This displacement body as is shown in FIG. 2 , is of hollow design. It has a near end 36 in relation to the end wall 34 and a far end 38 in relation to the end wall with a groove 5 A for fitting onto the center tube 6 of the tubular section of the burner element.
  • a displacement-body opening 40 which is open towards the interior space 42 of the hollow displacement body 5 so that the interior space 42 is accessible through the displacement-body opening 40 .
  • the burner-tip wall 11 A which is bent in an approximately U-shaped manner, is connected both to the outer tube 4 and to the inner tube 8 of the tubular section of the outer burner element 2 , whereas the displacement body 5 is connected to the center tube 6 of the tubular section of the outer burner element 2 in such a way that the displacement-body opening 40 is open towards the feed passage 7 which is formed between the outer tube 4 and the center tube 6 .
  • the displacement-body interior space 42 is consequently fluidically connected to the feed passage 7 for the cooling fluid.
  • the hollow displacement body 5 which consists in the main of a relatively thin wall 44 , is connected to the inner side of the burner-tip wall 11 A via support structures 46 .
  • These support structures can be of rib-like or pillar-like design so that they obstruct the flow in the flow passage 10 as little as possible and possibly even guide the flow.
  • FIG. 3 shows the construction of the inner burner tip part 21 and the inter-inserted tubes 14 , 16 , 18 , adjoining it, of the tubular section of the inner burner element 12 .
  • the inner burner tip part 21 has a wall 21 A with an end wall 47 which forms the closed end of the inner burner tip part 21 .
  • a displacement body 15 is located in the cavity of the inner burner tip part 21 .
  • This displacement body in turn is itself of hollow design and has a wall 54 enclosing an interior space 52 .
  • the displacement body 15 has a near end 48 in relation to the end wall 47 and a far end 49 in relation to the end wall 47 with a groove 15 A for fitting onto the center tube 16 of the tubular section of the burner element.
  • a displacement-body opening via which the displacement-body interior space 52 is accessible.
  • the wall 21 A of the inner burner tip part 21 is bent in an approximately U-shaped manner, wherein the ends of the burner-tip wall 21 A are connected to the outer tube 14 of the tubular section of the inner burner element 12 and to its inner tube 18 .
  • the displacement-body wall 54 is connected to the center tube 16 of the tubular section of the inner burner element 12 so that the displacement-body opening 50 is open towards the feed passage 17 formed between the outer tube 14 and the center tube 16 of the tubular section of the inner burner element 12 .
  • the displacement-body interior space 52 is fluidically connected to the feed passage 17 for the cooling fluid.
  • the displacement-body wall 54 is connected via support structures, which for example can be of rib-like or pillar-like design, to the inner side of the burner-tip wall 21 A so that a defined distance is provided between the outer side of the displacement body and the inner side of the burner-tip wall 21 A in order to form the flow passage 20 .
  • the support structures can also be designed in such a way that they guide the flow through the flow passage, but in any case they are designed so that they obstruct the flow as little as possible.
  • Swirl vanes 32 are formed in one piece with the burner tip part 21 of the inner burner element 12 .
  • the swirl vanes 32 are hollow and have in each case an interior space 58 which via a cooling fluid inlet opening 59 and a cooling fluid outlet opening 60 is fluidically connected to the flow passage 20 which leads around the displacement body 15 .
  • the displacement-body interior space 58 is therefore part of the cooling circuit so that the swirl vanes 32 together with the inner burner tip part 21 are cooled by the cooling fluid.
  • a tube 62 which serves as a guide for inserting the pilot burner 22 , is also formed in one piece with the inner burner tip part 21 and the swirl vanes 32 in the present exemplary embodiment. Exemplary embodiments without a tube 62 for guiding the pilot burner 22 are also possible, however.
  • the structure of the pilot burner 22 in the region of the burner tip 1 is shown in FIG. 4 .
  • the pilot burner tip part 31 and the tubular section of the pilot burner 22 which is formed from the three inter-inserted tubes 24 , 26 , 28 can be seen in the figure.
  • the pilot burner tip part 31 has a wall 31 A which is bent in an approximately U-shaped manner and encloses an interior space of the pilot burner tip part 31 .
  • a displacement body 25 is arranged in the interior space.
  • the displacement body 25 located in the interior space of the pilot burner tip part 21 is also of hollow design. It has a near end 66 pointing towards the end side 76 and a far end 68 facing away from this with a groove 25 A of fitting onto the center tube 26 of the tubular section of the burner element.
  • a displacement-body opening 70 via which the interior space 72 of the displacement body 25 is accessible.
  • the displacement-body interior space 72 is enclosed by a wall 74 which via support structures 76 , for example the already described pillar-like or rib-like structures, is connected to the inner side of the burner-tip wall 31 A.
  • the support structures 76 can be of a flow-guiding design. In any case, however, they are designed so that they do not obstruct the flow through the flow passage 30 which is formed between the outer side of the displacement body and the inner side of the burner-tip wall 31 A.
  • the two ends of the wall 31 A—which is bent in an approximately U-shaped manner—of the pilot burner tip part 31 are connected to the outer tube 24 and to the inner tube 28 of the tubular section of the pilot burner 22 , and the displacement-body wall 74 is connected to the center tube 26 of the tubular section.
  • the connection is constructed in this case at a point of the displacement-body wall 74 which is selected in such a way that the displacement-body opening 70 is open towards the feed passage which is formed between the outer tube 24 of the tubular section of the pilot burner 22 and its center tube 26 .
  • the displacement-body interior space 72 is consequently integrated into the cooling fluid circuit.
  • the outside diameter of the pilot burner 22 is selected so that it can be inserted into the tube 62 of the inner burner element 12 .
  • the pilot burner 22 also encloses a largely cylindrical interior space in which an ignition burner and a flame monitoring device can be arranged.
  • the burner tip parts 11 , 21 , 31 are produced separately in each case from the tubular sections which are formed by the inter-inserted tubes. Subsequently, the inter-inserted tubes are then connected to the respective burner tip parts by means of a welding process, for example.
  • the burner tip parts can especially be produced in one piece in each case by means of an additive manufacturing process.
  • the described complex structures in which hollow displacement bodies are connected to the burner-tip walls via support structures, are made possible.
  • the one-piece production of the swirl vanes 32 and the tube 62 with the inner burner tip part 21 can also be ensured by the additive production by means of an additive manufacturing process 5 .
  • an additive manufacturing process especially selective laser sintering can be applied.
  • FIG. 3 A modification of the exemplary embodiment shown in FIG. 3 is described below with reference to FIG. 5 .
  • the modification is concentrated in the main upon the embodiment of the displacement body and its interior space.
  • the remaining elements of the exemplary embodiment described in FIG. 3 such as the swirl vanes, are therefore not shown in FIG. 5 .
  • Elements which correspond to those from FIG. 3 are identified by the same designations as in FIG. 3 and are not explained again in order to avoid repetitions.
  • the displacement body of the exemplary embodiment shown in FIG. 5 differs from the displacement body of the exemplary embodiment shown in FIG. 3 mainly by the fact that its opening 50 is enlarged. Furthermore, a flow guiding element 80 projects from the inner side for the inner burner wall into the displacement-body opening 50 so that the flow guiding element 80 divides the opening into an inflow section 81 and an outflow section 82 .
  • a flow path 83 is formed around the flow guiding element 80 .
  • a collecting chamber 85 branches from the flow path 83 , wherein the access to the collecting chamber is arranged in approximately the original flow direction, that is to say the flow direction before the flow reversal. Suspended particles present in the cooling fluid are not able to reproduce the abrupt direction change, on account of their inertia, during the flow reversal as easily as the fluid itself so that the suspended particles make their way into the collecting chamber 85 and can be deposited there.
  • FIG. 6 A further alternative to the exemplary embodiment from FIG. 3 is shown in FIG. 6 . Elements which correspond to those from FIG. 3 are identified in this case by the same designations as in FIG. 3 and are not explained again in order to avoid repetitions. As in FIG. 5 , in FIG. 6 the swirl vanes 32 and also the cylindrical tube 62 are not shown since these do not differ from the exemplary embodiment shown in FIG. 3 .
  • the essential difference to the exemplary embodiment shown in FIG. 3 lies in the fact that the end wall 147 is of a thinner design than in the case of the exemplary embodiment shown in FIG. 3 .
  • the density of support structures 146 is increased in its region.
  • the support structures 146 are designed as pillar-like structures which converge to form arches on the displacement body 15 .
  • the arches are designed as pointed arches so that the pillar-like support structures form a type of arch which has the shape of a gothic arch.
  • the thin wall can also extend beyond the end wall 147 and even form the entire burner-tip wall 21 A.
  • the thin wall can also extend beyond the end wall 147 and even form the entire burner-tip wall 21 A.
  • the described pointed arch-like design of the support structures can be realized by means of the already mentioned additive manufacturing process.
  • the design of the support structures and of the wall thickness described with reference to FIG. 6 can also be realized in the case of the burner tip parts 11 , 31 of the outer burner element 2 and of the pilot burner 22 .
  • FIGS. 7 and 8 An alternative form of the support structures, which also enables a reduction of the wall thickness of the burner-tip wall, is shown in FIGS. 7 and 8 .
  • FIG. 8 shows a section along the line VIII-VIII shown in FIG. 7 .
  • the support structures shown in FIGS. 7 and 8 have the form of ribs 86 which are formed between the displacement-body wall 54 and the burner-tip wall 21 A and extend from the far end of the displacement body 15 around its near end and back towards the far end.
  • the ribs 86 extend in parallel and converge to form arches both on the outer side of the displacement body and on the inner side of the burner wall.
  • the arches are pointed arches so that between the individual ribs flow passages 20 are formed with cross sections which correspond to an ellipse running to a point at its ends.
  • This design of the support structures also allows a reduction of the wall thickness with high stability of the thinner wall.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Gas Burners (AREA)
US14/648,810 2012-12-14 2013-10-25 Burner tip and burner Abandoned US20150300633A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP12197209.5 2012-12-14
EP12197209.5A EP2743579A1 (de) 2012-12-14 2012-12-14 Brennerspitze und Brenner
PCT/EP2013/072422 WO2014090476A1 (de) 2012-12-14 2013-10-25 Brennerspitze und brenner

Publications (1)

Publication Number Publication Date
US20150300633A1 true US20150300633A1 (en) 2015-10-22

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ID=47351518

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/648,810 Abandoned US20150300633A1 (en) 2012-12-14 2013-10-25 Burner tip and burner

Country Status (4)

Country Link
US (1) US20150300633A1 (de)
EP (2) EP2743579A1 (de)
CN (1) CN104854405B (de)
WO (1) WO2014090476A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108485714A (zh) * 2018-05-28 2018-09-04 北京精益增材科技有限公司 一种内置水冷壁的一体式工艺烧嘴喷嘴

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014116411B4 (de) 2014-11-11 2024-05-29 Choren Industrietechnik GmbH Drallkörper und Brenner mit Drallkörper sowie Verfahren zur Herstellung des Drallkörpers
DE202014105403U1 (de) 2014-11-11 2014-12-08 Choren Industrietechnik GmbH Drallkörper und Brenner mit Drallkörper
DE102015115409A1 (de) 2015-07-09 2017-01-12 Choren Industrietechnik GmbH Verfahren zur Gestaltung von fluiddurchströmten Bauteilen
FR3067946A1 (fr) 2017-06-23 2018-12-28 IFP Energies Nouvelles Plateau distributeur pour colonne d'echange avec caisson pour la distribution du gaz
DE202017107794U1 (de) 2017-12-20 2018-01-22 Choren Industrietechnik GmbH Brennerspitze und Pilotbrenner

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4813867A (en) * 1985-10-31 1989-03-21 Nihon Nensho System Kabushiki Kaisha Radiant tube burner
DE102008006572A1 (de) * 2008-01-29 2009-07-30 Siemens Aktiengesellschaft Keramische Beschichtung von Vergasungsbrennerteilen
US20140123661A1 (en) * 2012-11-06 2014-05-08 Alstom Technology Ltd Axial swirler
US9032623B2 (en) * 2007-08-06 2015-05-19 Shell Oil Company Method of manufacturing a burner front face
US9170018B2 (en) * 2009-12-10 2015-10-27 Sk Innovation Co., Ltd. Top-feeding double-swirl type gasifier

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4865542A (en) * 1988-02-17 1989-09-12 Shell Oil Company Partial combustion burner with spiral-flow cooled face
JP2627552B2 (ja) * 1988-02-17 1997-07-09 シエル・インターナシヨネイル・リサーチ・マーチヤツピイ・ベー・ウイ スパイラルフロー冷却面付き部分燃焼用バーナ
JP4739090B2 (ja) * 2006-04-06 2011-08-03 大陽日酸株式会社 バーナ又はランスの冷却構造
US8438856B2 (en) * 2009-03-02 2013-05-14 General Electric Company Effusion cooled one-piece can combustor
DE102010004787B4 (de) * 2010-01-16 2014-02-13 Lurgi Gmbh Verfahren und Brenner zur Herstellung von Synthesegas

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4813867A (en) * 1985-10-31 1989-03-21 Nihon Nensho System Kabushiki Kaisha Radiant tube burner
US9032623B2 (en) * 2007-08-06 2015-05-19 Shell Oil Company Method of manufacturing a burner front face
DE102008006572A1 (de) * 2008-01-29 2009-07-30 Siemens Aktiengesellschaft Keramische Beschichtung von Vergasungsbrennerteilen
US9170018B2 (en) * 2009-12-10 2015-10-27 Sk Innovation Co., Ltd. Top-feeding double-swirl type gasifier
US20140123661A1 (en) * 2012-11-06 2014-05-08 Alstom Technology Ltd Axial swirler

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
English Translation of DE 102008006572 A1 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108485714A (zh) * 2018-05-28 2018-09-04 北京精益增材科技有限公司 一种内置水冷壁的一体式工艺烧嘴喷嘴

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WO2014090476A1 (de) 2014-06-19
CN104854405B (zh) 2017-05-17
CN104854405A (zh) 2015-08-19
EP2743579A1 (de) 2014-06-18
EP2898266A1 (de) 2015-07-29

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