EP3322935B1 - Brûleur à charbon pulvérisé comprenant une buse à combustible monobloc chauffée électriquement - Google Patents

Brûleur à charbon pulvérisé comprenant une buse à combustible monobloc chauffée électriquement Download PDF

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Publication number
EP3322935B1
EP3322935B1 EP16723351.9A EP16723351A EP3322935B1 EP 3322935 B1 EP3322935 B1 EP 3322935B1 EP 16723351 A EP16723351 A EP 16723351A EP 3322935 B1 EP3322935 B1 EP 3322935B1
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EP
European Patent Office
Prior art keywords
fuel
heating
burner
air
resistance wire
Prior art date
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Active
Application number
EP16723351.9A
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German (de)
English (en)
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EP3322935A1 (fr
Inventor
Alfons Leisse
Sebastian Rehfeldt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Power Europe GmbH
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Mitsubishi Hitachi Power Systems Europe GmbH
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Priority to PL16723351T priority Critical patent/PL3322935T3/pl
Publication of EP3322935A1 publication Critical patent/EP3322935A1/fr
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Publication of EP3322935B1 publication Critical patent/EP3322935B1/fr
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00Subject-matter not provided for in other groups of this subclass
    • F23C99/001Applying electric means or magnetism to combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D1/00Burners for combustion of pulverulent fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/10Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of field or garden waste or biomasses
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q7/00Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs
    • F23Q7/02Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs for igniting solid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2207/00Ignition devices associated with burner

Definitions

  • the invention relates to a burner for the combustion of particulate, in particular dust-like, carbon-containing fuel, preferably coal or biomass, comprising a fuel or primary air pipe carrying a fuel mass flow with a fuel nozzle formed at its end of the burner opening, which has a stabilizing ring with teeth pointing radially inwards of a ring gear and on the outside has a conical radially outwardly widening jacket air or secondary air deflection cone, and comprises a jacket air or secondary air pipe coaxially surrounding the fuel or primary air pipe and preferably a core air pipe arranged coaxially within the fuel or primary air pipe, the fuel nozzle having at least one Electric heating or resistance wire heating and / or ignition device that forms within the burner for the emergence and the course of the initial pyrolysis and ignition of the fuel conveyed in the fuel or primary air pipe provides the required amount of thermal energy in the region of the fuel ignition location that is formed.
  • the burner comprises a fuel or primary air pipe, which has a fuel nozzle at its end on the burner mouth, which is formed in one piece and has a toothed ring with teeth pointing radially inwards and, on the outside, a conical radially outwardly widening jacket air or secondary air deflection cone.
  • the fuel or primary air pipe is coaxially surrounded by a jacket air or secondary air pipe, which in turn is coaxially surrounded by a tertiary air pipe.
  • a core air tube equipped with an ignition lance is arranged coaxially to the center of the fuel or primary air tube. Acting at the fuel nozzle it is a component which is produced in one piece, for example by centrifugal casting, and which forms the mouth cross section of the fuel or primary air pipe, also called the dust pipe in the case of combustion of coal dust.
  • the stabilizing ring has in particular the function of detecting the fuel conveyed in the fuel or primary air pipe, in particular coal dust, of decelerating its flow rate and of redirecting the fuel mass flow.
  • the definition of the location and the time of the ignition are of crucial importance, since only in this way can the combustion conditions, in particular the stoichiometry, be influenced. This does not allow an indefinite ignition of the fuel in the combustion chamber, since the fuel-air ratio can only be influenced to a limited extent here.
  • Such burners are also from the DE 42 17 879 A1 , the DE 43 25 643 A1 and the DE 195 27 083 A1 known.
  • particulate, carbon-containing fuel-fired power plants which result from the increased feeding of regenerative electrical energy into the power grid. Since the feeding of electrical energy from renewable energy sources into the power grid does not take place evenly, but depends on the availability of sun or wind, conventional, fossil-fired power plants higher demands on load flexibility.
  • particulate carbonaceous fuel such as coal or biomass boilers in particular dust-like fuel with the aid of suitable for this purpose is, in particular NO x fed-poor burners of the kind described above, together with the necessary quantity of combustion air to the combustion chamber.
  • the burners or burner groups are assigned to a number of grinding plants or mills.
  • the steam generator output currently called up is changed by changing the mill or burner output and by switching on or off individual grinding plants and the burners assigned to them. This means that the steam generator output is usually regulated based on the number of burners or burner groups in operation. This means that if the load changes frequently, the burner must be started and stopped accordingly.
  • the ignition generally consists of ignition lances or similar burners, which are arranged in the burner, and with which by combustion of gaseous or liquid auxiliary fuel, such as natural gas or heating oil, for ignition of the burner necessary pilot flame to be burned fuel is generated.
  • gaseous or liquid auxiliary fuel such as natural gas or heating oil
  • the duration results, among other things, from the time required for the preparation of the transportable fuel / fuel dust and the actual transport process to the burner (s). With a frequent load change and thus frequent start-up and shutdown processes of individual mills or grinding plants, this leads to a considerable increase in the costs and expenses for the pilot fuels such as heating oil or gas required when starting a burner, which has a negative impact on the economy of conventional power generation.
  • the invention is therefore based on the object of providing an alternative or improved solution which makes it possible to use a fuel nozzle of a burner equipped with a jacket air or secondary air repellency cone and a stabilizing ring with ring gear as an electrical heating and / or ignition device for the ignition of in the burner trained fuel.
  • the object is achieved according to the invention in that the fuel nozzle is formed in one piece and, in addition to the stabilizing ring and the jacket air or secondary air deflection cone, comprises a fuel or primary air pipe section and in that surface of the jacket air facing the jacket air or secondary air pipe - or secondary air repellency cone is formed at least one spiral groove, in which the at least one heating or resistance wire is spirally wound in at least one heating or resistance wire winding comprising a plurality of turns.
  • an electrical heating or resistance wire is integrated to one for the initial ignition of the burner, that is in the fuel or primary air tube supported fuel mass flow suitable location in the fuel nozzle of a designed for low NOx combustion burner, without adversely changing the mode of operation of the fuel nozzle for continuous operation even after the fuel has been ignited. Since the heating or resistance wire is wound onto the outside surface of the fuel nozzle, in particular the jacket air or secondary air repellency cone, in one or more grooves, the configuration of the fuel nozzle with its functions as part of the fuel or primary air pipe remains as a secondary air repelling groove (jacket air - or secondary air deflection cone) and received as a stabilizing ring.
  • Shaping of the fuel required by the introduction of the heating or resistance wire in or on the material of the fuel nozzle, while maintaining the x low-carbon for NO combustion can be advantageously a generally electrically heated fuel form, the simple construction and by mechanically Machining the surface of the fuel nozzle is simple and inexpensive to manufacture. Since a fuel nozzle is usually exposed to a high thermal load from the combustion chamber and abrasive wear from the fuel mass flow, it is usually made from a high-alloy steel. The surface of the fuel nozzle made from such steel can be machined well with a technically and economically justifiable effort.
  • the heating or resistance wire is not exposed to the fuel nozzle in the configuration of the fuel nozzle according to the invention, since it is arranged on the outer surface of the fuel nozzle. With this outer surface, it can protrude into the flow area of the jacket air or secondary air tube which promotes jacket air or secondary air and in which no abrasive media or only a small number of abrasive particles are conveyed.
  • the outer surface of the spiral heating or resistance wire winding can be covered with an appropriate insulating material.
  • the heating or resistance wire is according to the invention in the area of the most suitable place for the initial ignition, namely in the immediate vicinity of the stabilization ring of the fuel nozzle, so that the area formed in the fuel or primary air pipe in front of the stabilization ring reaches a possible high temperature with the lowest possible electrical heat absorption and thus the lowest possible electrical energy consumption of the resistance wire.
  • grooves or groove-shaped depressions are incorporated in the oblique, conically widening surface of the jacket air or secondary air repellency cone advantageously creates the possibility of a heating or resistance wire with good heat-transferring connection to the material body of the jacket air on this oblique surface - or secondary air deflection cone and at the same time to achieve a good fixation of the heating or resistance wire on the inclined surface.
  • one or more circumferential grooves are formed over the entire length of the jacket air or secondary air deflection cone on its surface facing the jacket air or secondary air pipe, which are aligned spirally and parallel to one another and adjoining one another over the course of the winding and with a diameter of the width and depth of the at least one heating or resistance wire are formed and into which the at least one heating or resistance wire is spirally wound in the heating or resistance wire winding comprising several turns, which the invention provides in one embodiment.
  • the width and depth of the groove corresponds at least approximately to the diameter of the heating or resistance wire, a particularly deep embedding of the heating or resistance wire in the base material and the material body of the jacket air or secondary air repellency cone is ensured and thus a particularly good heat transfer from the Heating or resistance wire reached to the adjacent material areas.
  • the heating or resistance wire winding has a plurality of spirally wound heating or resistance wires, which also distinguishes the invention.
  • a particularly good fixation of the at least one heating or resistance wire or the plurality of heating or resistance wires in the groove or in the grooves can be achieved in that these are connected to the base material or the body material of the fuel nozzle by brazing, this measure It also enables the heat transfer surface to be made more uniform, since areas where the respective heating or resistance wire does not lie directly on the base material or body material are filled by the molten hard solder initially, thereby creating a heat transfer bridge.
  • the invention is therefore characterized in a further embodiment in that the at least one heating or resistance wire or the plurality of heating or resistance wires is / are integrally connected to the material of the jacket air or secondary air repellency cone and the fuel nozzle by means of a molten hard braze.
  • the heating or resistance wire winding on its Jacket air or secondary air pipe facing surface is covered with a heat insulating material.
  • the invention provides that A circumferential stabilization ring groove is formed in the inside of the fuel nozzle facing away from the casing air or secondary air deflection cone in the immediate foot region of the toothed ring of the stabilization ring facing the casing air or secondary air deflection cone. Because a circumferential stabilizing ring groove is formed in the foot region of the ring gear of the stabilizing ring, more fuel is trapped here and the fuel mass flow is stopped more intensely, so that there is more time for heat transfer and ignition compared to the prior art.
  • the invention also provides that the depth of the stabilizing ring groove is at least 5% of the width of the stabilizing ring 5 or the toothed ring 6.
  • the burner designated as a whole by 1, comprises a fuel or primary air pipe 3 arranged coaxially to the burner longitudinal axis 2, at the end of the burner mouth of which a fuel nozzle 4 is formed.
  • the fuel nozzle 4 is formed in one piece and comprises a stabilizing ring 5, which has a ring gear 6 with radially inwardly pointing teeth 7 and on the outside a conical radially outwardly widening jacket air or secondary air deflection cone 8. Furthermore, the fuel nozzle 4 has the fuel or End facing the primary air pipe 3 has a fuel or primary air pipe section 9.
  • the fuel or primary air tube 3 is coaxially surrounded by a jacket air or secondary air tube 10, which in turn is coaxially surrounded by a tertiary air tube 11.
  • a core air tube 12 is arranged coaxially to the fuel or primary air tube 3, the mouth of which lies within the fuel or primary air tube 3 at a distance from the teeth 7 of the stabilizing ring 5.
  • an annular fuel delivery cross section 13 is formed in the round burner shown here, in which a fuel mass flow of the fuel intended for combustion to the mouth area of the fuel or primary air pipe 3, i.e. the fuel nozzle 4 is promoted.
  • the fuel delivered here is a particulate, in particular dusty, carbon-containing fuel, preferably coal or biomass or mixtures of these fuels.
  • At least one groove 15 is formed which spirally surrounds the surface 14.
  • the grooves 15 are from the Fig. 2 can be seen, which schematically represents a segment-like section from a fuel nozzle 4 according to the invention above the burner longitudinal axis 2.
  • the groove (s) 15 run around the surface 14 in multiple passages and extend in the longitudinal direction of the burner over the jacket air or secondary air deflection cone 8 and a partial region of the fuel or primary air pipe section 9.
  • An electrical heating or resistance wire 16 is embedded in a respective groove 15, being in the Fig. 2 three adjacent turns of a heating wire 16, which is embedded in a groove 15, are indicated.
  • the other grooves 15 are also covered in the same way with a heating or resistance wire 16 or a portion of such a heating or resistance wire 16 wound on the surface 14 to form a multi-start heating or resistance wire winding 17.
  • the at least one heating or resistance wire 16 is wound spirally in a heating or resistance wire winding 17 comprising a plurality of turns onto the surface 14 of the fuel nozzle 4, which in FIG Fig. 2 is only indicated by the heating or resistance wires 16 shown, but extends over the entire number of grooves 15.
  • a heating or resistance wire winding 17 wound on the surface 14 of the fuel nozzle 4 is shown in FIG Fig. 3 can be seen, here a total of three heating or resistance wire windings 17, each having its own electrical connection 21a, 21b, 21c, are wound in the grooves 15.
  • each groove 15 The width and the depth of each groove 15 are adapted to the diameter of the heating or resistance wire 16 to be inserted therein, so that a tight winding of the heating or resistance wires 16 is possible and these do not protrude, or at most only slightly, above the upper edge of each groove 15
  • the at least one heating or resistance wire 16 or the plurality of heating or resistance wires 16 are integrally connected to the material of the jacket air or secondary air repellency cone 8 or the fuel nozzle 4 by means of a hard solder applied in a molten form.
  • the heating or Resistance wire winding 17 is covered on its surface 22 facing the jacket air or secondary air 10 with a heat insulating material.
  • the grooves 15 are introduced into the base material of the fuel nozzle 4 by mechanical processing and serve to guide and fix the heating or resistance wire 16 or the heating or resistance wires 16 on the conically widening and thus inclined surface 14 of the jacket air or secondary air repellency cone 8 the fuel nozzle 4.
  • a circumferential stabilization groove 18 is formed on the inside of the fuel nozzle 4 facing away from the jacket air or secondary air repellency cone 8 in the immediate foot region of the ring gear 6 of the stabilization ring 5 facing the jacket air or secondary air repellency cone 8. This has the effect that the fuel particles conveyed in the fuel delivery cross section 13 remain sufficiently long in the area of the fuel nozzle 4 which is designed as at least one wound heating or resistance wire 16 as a heating and / or ignition device 19 and that there is an initial pyrolysis and ignition of the fuel or primary air pipe 3 with the aid of a carrier gas, in particular air, fuel delivered.
  • the depth of the stabilizing groove 18 in the axial direction of the burner 1 is at least 5% of the width B of the stabilizing ring 5 or the ring gear 6 in the axial direction of the burner.
  • the one or more feed ends or connections 21a, 21b, 21c of the heating or resistance wires 16, to which these are connected to an electrical voltage source, are preferably led out of the burner 1 through the jacket air or secondary air pipe 10 or its wall.
  • these supply lines are designed in such a way that they can withstand the usual temperatures of around 300 ° C. occurring in the long term.
  • a heat insulating material can be placed on the surface 22 of the heating or resistance wire winding 17 facing the jacket air or secondary air tube 10, which is preferably one with low thermal conductivity and high heat resistance, for example mineral fibers, rock wool, ceramic wool or ceramic textiles.
  • the heat insulation covering the heating or resistance wire winding 17 With the aid of the heat insulation covering the heating or resistance wire winding 17, the heat losses due to the convective cooling, which causes the secondary air conveyed in the jacket air or secondary air pipe 10, and radiation losses are reduced, which leads to a reduction in the electrical energy required for the desired heat emission to the fuel leads.
  • this layer of insulating material offers protection against ashes that may be contained in the secondary air or jacket air.
  • the insulation or the heat insulating material covering the heating or resistance wire winding 17 can be covered, clad and fixed with components made of thin, heat-resistant steel sheet, which are adapted to the outer shape of the fuel nozzle 4.
  • a heating and / or ignition device 19 is created which, within the burner 1, preferably the amount of thermal energy required for the formation and the course of the initial pyrolysis and ignition of the fuel conveyed in the fuel or primary air pipe 3 in the area of the stabilization groove 18 forming fuel ignition location and generated exclusively by means of electrical energy.
  • the fuel ignition location usually forms in the area of the stabilization ring 5, to which the stabilization groove 18 also contributes, which causes a backflow of the supplied particulate fuel and thus a delay in the flow rate of the fuel mass flow supplied through the fuel or primary air pipe 3 and its fuel delivery cross section 13, so that Adequate heat transfer from the exclusively electrically operated heating and / or ignition device 19 to the fuel mass flow, ie the individual fuel particles, can take place.
  • Adequate heat transfer from the exclusively electrically operated heating and / or ignition device 19 to the fuel mass flow, ie the individual fuel particles can take place.
  • the initial pyrolysis necessary for the ignition of the fuel and then the ignition which takes place first of the pyrolysis products and then the fuel particles is ensured.
  • the promotion of the particulate fuel mass flow into the region of the stabilizing groove 18 is supported by the usual swirl elements 20 formed in the fuel delivery cross section 13.
  • thermocouples can be arranged in the fuel nozzle 4 or at a suitable point on the burner 1.

Claims (7)

  1. Brûleur (1) pour la combustion d'un carburant contenant du carbone, sous forme de particules, plus particulièrement sous forme de poussières, de préférence du charbon ou de la biomasse, comprenant un tube de carburant ou d'air primaire (3) conduisant un flux massique de carburant, avec une buse de carburant (4), réalisée à son extrémité du côté de l'embouchure du brûleur, qui comprend un anneau de stabilisation (5) avec des dents (7), orientées radialement vers l'intérieur, d'une couronne dentée (6) et, à l'extérieur, un cône de déviation d'air d'enveloppe ou d'air secondaire (8), et comprenant un tube d'air d'enveloppe ou d'air secondaire (10) entourant de manière coaxiale le tube de carburant ou d'air primaire (3) ainsi que, de préférence, un tube d'air central (12) disposé coaxialement à l'intérieur du tube de carburant ou d'air primaire (3), dans lequel la buse de carburant (4) forme un dispositif de chauffage et/ou d'allumage (19) comprenant au moins un fil électrique de chauffage ou de résistance (16), qui met à disposition, à l'intérieur du brûleur (1), la quantité d'énergie thermique nécessaire pour l'apparition et le déroulement de la pyrolyse initiale et de l'allumage du carburant transporté dans le tube de carburant ou d'air primaire (3) au niveau de la zone d'allumage du carburant,
    caractérisé en ce que
    la buse de carburant (4) est réalisée d'une seule pièce et comprend, en plus de l'anneau de stabilisation (5) et du cône de déviation d'air d'enveloppe ou d'air secondaire (8), une portion de tube de carburant ou d'air primaire (9) et en ce que, dans la surface (14) orientée vers le tube d'air d'enveloppe ou d'air secondaire (10) du cône de déviation d'air d'enveloppe ou d'air secondaire (8), est réalisée au moins une rainure périphérique en spirale (15), dans laquelle l'au moins un fil de chauffage ou de résistance (16) est enroulé en spirale selon au moins un enroulement de fil de chauffage ou de résistance (17) comprenant plusieurs spires.
  2. Brûleur (1) selon la revendication 1, caractérisé en ce que, sur toute la longueur du cône de déviation d'air d'enveloppe ou d'air secondaire (8), sur la surface (14), orientée vers le tube d'air d'enveloppe ou d'air secondaire (10), de celui-ci, sont réalisées une ou plusieurs rainures périphériques (15), qui sont réalisées en spirale et sont orientées parallèlement entre elles et sont adjacentes entre elles sur l'étendue de l'enroulement et sont réalisées avec une largeur et une profondeur correspondant au diamètre de l'au moins un fil de chauffage ou de résistance (16) et dans la ou lesquelles l'au moins un fil de chauffage ou de résistance (16) est enroulé dans l'enroulement de fil de chauffage ou de résistance (17) comprenant plusieurs spires.
  3. Brûleur (1) selon la revendication 1 ou 2, caractérisé en ce que l'enroulement de fil de chauffage ou de résistance (17) comprend plusieurs fils de chauffage ou de résistance (16) enroulés en spirale.
  4. Brûleur (1) selon l'une des revendications précédentes, caractérisé en ce que l'au moins un fil de chauffage ou de résistance (16) ou les plusieurs fils de chauffage ou de résistance (16) est/sont relié(s), par liaison de matière, au moyen d'un brasage dur appliqué par fusion, avec le matériau du cône de déviation d'air d'enveloppe ou d'air secondaire (8) et de la buse de carburant (4).
  5. Brûleur (1) selon l'une des revendications précédentes, caractérisé en ce que l'enroulement de fil de chauffage ou de résistance (17) est recouvert, sur sa surface (22) orientée vers le tube d'air d'enveloppe ou d'air secondaire (3), avec un matériau d'isolation thermique.
  6. Brûleur (1) selon l'une des revendications précédentes, caractérisé en ce que, sur le côté interne, opposé au cône de déviation d'air d'enveloppe ou d'air secondaire (8), de la buse de carburant (4), est réalisée, directement dans la zone de pied, orientée vers le cône de déviation d'air d'enveloppe ou d'air secondaire (8), de la couronne dentée (6) de l'anneau de stabilisation (5), une rainure de stabilisation périphérique (18).
  7. Brûleur (1) selon la revendication 6, caractérisé en ce que la profondeur de la rainure de stabilisation (18) représente au moins 5 % de la largeur (B) de l'anneau de stabilisation (5) ou de la couronne dentée (6).
EP16723351.9A 2015-07-16 2016-05-13 Brûleur à charbon pulvérisé comprenant une buse à combustible monobloc chauffée électriquement Active EP3322935B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL16723351T PL3322935T3 (pl) 2015-07-16 2016-05-13 Palnik na pył węglowy z jednoczęściową, ogrzewaną elektrycznie dyszą paliwową

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102015111585.9A DE102015111585A1 (de) 2015-07-16 2015-07-16 Kohlenstaubbrenner mit einstückiger, elektrisch beheizter Brennstoffdüse
PCT/EP2016/060842 WO2017008937A1 (fr) 2015-07-16 2016-05-13 Brûleur à charbon pulvérisé comprenant une buse à combustible monobloc chauffée électriquement

Publications (2)

Publication Number Publication Date
EP3322935A1 EP3322935A1 (fr) 2018-05-23
EP3322935B1 true EP3322935B1 (fr) 2020-05-27

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EP16723351.9A Active EP3322935B1 (fr) 2015-07-16 2016-05-13 Brûleur à charbon pulvérisé comprenant une buse à combustible monobloc chauffée électriquement

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EP (1) EP3322935B1 (fr)
DE (1) DE102015111585A1 (fr)
PL (1) PL3322935T3 (fr)
WO (1) WO2017008937A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106907707B (zh) * 2017-04-17 2023-08-29 北京盛恒鑫业能源科技有限公司 一种煤粉雾化电点火燃烧器
DE102019103640A1 (de) * 2019-02-13 2020-08-13 Mitsubishi Hitachi Power Systems Europe Gmbh Brennstoffdüse mit Dehnungsschlitzen für einen Kohlenstaubbrenner

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD249828A3 (de) * 1985-05-28 1987-09-23 Luebbenau Vetschau Kraftwerke Anordnung einer elektrischen zuendeinrichtung in einem kohlenstaubbrenner

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4649260A (en) * 1983-03-16 1987-03-10 Coal-O-Matic Pvba Lighter for stove, open hearth and similar
DD231962A3 (de) * 1983-07-08 1986-01-15 Luebbenau Vetschau Kraftwerke Elektrische zuendeinrichtung fuer haupt- und zuendbrenner, insbesondere fuer kohlenstaub-zuendbrenner
DE4217879A1 (de) 1992-05-29 1993-12-02 Babcock Energie Umwelt Brenner für staubförmigen Brennstoff
DE4325643A1 (de) 1993-07-30 1995-02-02 Lentjes Kraftwerkstechnik Brenner zum Verbrennen von staubförmigem Brennstoff
DE19527083A1 (de) 1995-07-25 1997-01-30 Lentjes Kraftwerkstechnik Verfahren und Brenner zur Verminderung der Bildung von NO¶x¶ bei der Verbrennung von Kohlenstaub
DE102005032109B4 (de) 2005-07-07 2009-08-06 Hitachi Power Europe Gmbh Kohlenstaubbrenner für niedrige NOx-Emissionen
ATE448447T1 (de) * 2007-03-23 2009-11-15 Rauschert Steinbach Gmbh Zündeinrichtungen und verfahren zum zünden festen brennstoffs
AT511814B1 (de) * 2012-04-27 2013-03-15 Karl Stefan Riener Elektrische Zündvorrichtung für Brennmaterial in einer Heizeinrichtung sowie damit ausgestattete Heizeinrichtung
DE102013111504B4 (de) * 2013-10-18 2017-12-07 Mitsubishi Hitachi Power Systems Europe Gmbh Verfahren zur Zündung eines Kraftwerkbrenners und dafür geeigneter Kohlenstaubbrenner

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD249828A3 (de) * 1985-05-28 1987-09-23 Luebbenau Vetschau Kraftwerke Anordnung einer elektrischen zuendeinrichtung in einem kohlenstaubbrenner

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DE102015111585A1 (de) 2017-01-19
WO2017008937A1 (fr) 2017-01-19
EP3322935A1 (fr) 2018-05-23
PL3322935T3 (pl) 2020-11-16

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