US20120216730A1 - Method of Combusting Particulate Solid Fuel with a Burner - Google Patents

Method of Combusting Particulate Solid Fuel with a Burner Download PDF

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Publication number
US20120216730A1
US20120216730A1 US13/505,149 US201013505149A US2012216730A1 US 20120216730 A1 US20120216730 A1 US 20120216730A1 US 201013505149 A US201013505149 A US 201013505149A US 2012216730 A1 US2012216730 A1 US 2012216730A1
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US
United States
Prior art keywords
oxidant
fuel
flow
burner
outlet
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
US13/505,149
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English (en)
Inventor
Brenice Belasse
Jacques Mulon
Faustine Panier
Xavier Paubel
Remi Tsiava
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.)
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Original Assignee
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude filed Critical LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Assigned to L'AIR LIQUIDE SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE reassignment L'AIR LIQUIDE SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BELASSE, BRENICE, MULON, JACQUES, PANIER, FAUSTINE, PAUBEL, XAVIER, TSIAVA, REMI
Publication of US20120216730A1 publication Critical patent/US20120216730A1/en
Abandoned legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
    • F23L7/007—Supplying oxygen or oxygen-enriched air
    • 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
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Definitions

  • the present invention relates to an improved method of combusting particulate solid fuel, such as pulverized coal.
  • This known method as developed by the applicant enables various characteristics of the flame to be effectively controlled by changing the relative flow rates of the gaseous fuel and oxidant flows. For example, by decreasing the inner oxidant flow, the length and luminosity of the flame can be increased, and the flame momentum can be decreased without any mechanical modification of the burner.
  • An important advantage of said method is that it is possible to maintain an optimum flame length when varying the firing rate of the burner. Furthermore, the control of the relative flow rates can be used to change the luminosity of the flame.
  • coal is more abundantly available than gaseous fuel.
  • a new method of combining oxygen and conveyor-gas propelled particulate solid fuel in a burner to produce a flame comprises the steps of:
  • the fuel outlet and spaced radially inwardly therefrom, the fuel flow being a flow of conveyor-gas propelled particulate solid fuel.
  • a second inner oxidant flow is supplied to the burner.
  • Said second inner oxidant flow which has a higher oxygen concentration than the conveyor gas, is injected into the fuel-conducting passage and is thus mixed with the fuel flow inside said fuel-conducting passage so as to obtain, upstream of the fuel outlet and upstream of the inner oxidant end outlet, an oxygen-enriched conveyor-gas propelled particulate solid fuel flow having an oxygen content of at least 21% vol O 2 .
  • the fuel flow in the form of the oxygen-enriched conveyor-gas propelled particulate solid fuel flow, is discharged from the fuel-conducting passage with a fuel discharge velocity which differs from the inner oxidant discharge velocity with which the first inner oxidant flow is discharged from the inner oxidant-conducting passage so as to promote mixing between the fuel flow and the first inner oxidant flow downstream of the inner oxidant end outlet.
  • the second inner oxidant flow is injected into the fuel-conducting passage so as to obtain, upstream of the fuel outlet and upstream of the inner oxidant end outlet, an oxygen-enriched conveyor-gas propelled particulate solid fuel flow having an oxygen content of at least 28% vol, and more preferably of at least 32% vol.
  • the second inner oxidant flow advantageously has an oxygen content of at least 50% vol O 2 , preferably of at least 80% vol O 2 and more preferably of at least 90% vol O 2 .
  • both the first and second inner oxidant flows have an oxygen content of at least 50% vol O 2 , preferably of at least 80% vol O 2 and more preferably of at least 90% vol O 2 .
  • an oxygen content of about 21% vol O 2 such as air
  • a more diffuse flame and larger volume of combustion gases are obtained, as may be advantageous in some industrial combustion processes.
  • an outer oxidant flow with a higher oxygen content such as an outer oxidant having an oxygen content of at least 50% vol O 2 , of at least 80% vol O 2 , or even of at least 90% vol O 2
  • a more intense flame and smaller volumes of combustion gases are obtained, which may be preferable for other industrial combustion processes. It also enables lower NOx emissions.
  • the outer, the first inner and the second inner oxidant flows may all have the same oxygen content, in which case they may be supplied by a single oxidant source.
  • the method of the invention is useful for a wide range of particulate solid fuels, including pulverized coal, pet coke, particulate biomass and mixtures thereof. It is particularly useful for the combustion of pulverized coal, including low-grade pulverized coal which has been shown to be difficult to combust efficiently with known particulate fuel burners.
  • the burner used in the method of the invention advantageously comprises a burner block with a through passage into which the outer oxidant-conducting passage, the fuel-conducting passage and the inner oxidant-conducting passage are mounted.
  • the outlets of the respective gas conducting passages are then preferably set back from the outlet opening of the through passage in the burner block, which outlet faces the combustion chamber of the furnace.
  • the second inner oxidant flow is injected into the fuel-conducting passage at multiple points of injection along the length of the fuel-conducting passage.
  • the conveyor-gas propelled particulate solid fuel flow is progressively enriched with oxygen towards the fuel outlet.
  • This embodiment presents a number of advantages such as a lower risk of premature ignition or explosion.
  • Multiple-point injection of the second inner oxidant flow into the fuel-conducting passage also lowers the risk of inhomogeneous distribution of the particulate solid fuel in the conveyor gas, such as particle settling, roping, etc.
  • a particularly suited burner for use in the present invention is described in European patent application 09174622.2 filed on 30 Oct. 2009 and incorporated herein by reference, more specifically the embodiments of said burner with a central oxygen lance.
  • the present invention therefore also relates to the use of such a burner in the present method.
  • the upper limit for the oxygen enrichment of the conveyor-gas propelled particulate solid fuel flow is determined by the properties, and in particular the flammability, of the particulate solid fuel and, to a lesser extent, by the properties of the conveyor gas.
  • said oxygen content may for example reach levels of upto 60% vol, preferably upto 80% vol.
  • the fuel flow in the form of the oxygen-enriched conveyor-gas propelled particulate solid fuel flow, is preferably mixed with the first inner oxidant flow before being mixed with said outer oxidant flow. This can be achieved by having the inner oxidant end outlet upstream of the fuel outlet. In this manner increased flame stability and attachment is achieved.
  • the combustion is then a staged combustion, with the first inner oxidant flow acting as a primary oxidant flow and the outer oxidant flow acting as a secondary oxidant flow.
  • the total oxygen supply to the burner typically corresponds to the stoichiometrically required amount of combustion oxygen or a minor excess thereof (for example, a total oxygen supply of upto 115% of the stoichiometrically required amount).
  • the total oxygen supply to the burner may also be less than the stoichiometrically required amount of combustion oxygen, in particular when the method includes a separate supply of additional oxygen, which is injected separately from the burner.
  • the sum of the oxygen supplied through the first and second inner oxidant flows usefully corresponds to at least 22% of the total oxygen supply to the burner, preferably at least 25%, and not more than 65%, preferably not more than 50%.
  • the sum of the oxygen supplied through the first and second inner oxidant flows is preferably at least 22% and more preferably at least 25% of the stoichiometrically required amount of oxygen, and not more than 65%, preferably not more than 50%.
  • the first inner oxidant discharge velocity can advantageously be equal to or greater than the outer oxidant discharge velocity, and is preferably in the range of from about 10 to 200 m/s.
  • the fuel discharge velocity can notably be in the range of from 10 to 80 m/s, whereas the outer oxidant discharge velocity is suitably in the range of 10 to 50 m/s. It is, however, a particular advantage of the present invention, that efficient combustion of particulate solid fuel can be achieved at fuel discharge velocities as low as 5 m/s.
  • the present invention also includes methods, as described above, for combining oxygen and fuel in a burner to produce a flame, whereby the fuel discharge velocity is within the range of 5 to 80 m/s, preferably between from 5 to 40 m/s and more preferably from 5 to 25 m/s.
  • the present invention also relates to the use of the method to produce heat in a combustion zone of the furnace, whereby the furnace can in particular be a tunnel kiln or furnace, a passage kiln, a boiler, a rotary kiln or furnace or a tunnel furnace, the particulate solid fuel preferably being preferably pulverized coal.
  • the furnace can in particular be a tunnel kiln or furnace, a passage kiln, a boiler, a rotary kiln or furnace or a tunnel furnace, the particulate solid fuel preferably being preferably pulverized coal.
  • the method of the invention can in particular be advantageously used in a furnace for the production of hydraulically setting binder, such as cement lime or plaster.
  • FIGS. 1 to 4 The invention is illustrated in the example hereafter, reference being made to FIGS. 1 to 4 , whereby:
  • FIG. 1 is a schematic representation of a cross-section of a burner suitable for use in the invention
  • FIG. 2 is a schematic representation of a cross section of the injector assembly thereof.
  • FIGS. 3 and 4 are schematic representations in cross section of the type of flame obtained with said burner in accordance with the example.
  • Tests were conducted with different ratios of first to second inner oxidant flows.
  • a particulate solid fuel burner with a central oxygen lance as described in European patent application 09174622.2 filed on 30 Oct. 2009 was mounted in the side wall of a combustion furnace and illustrated in FIGS. 1 and 2 .
  • the illustrated burner comprises a burner block 100 and an injector assembly 200 .
  • the burner block 100 has an inlet face 110 and an outlet face 120 .
  • the block further presents an injector passage 130 extending through the burner block from the inlet face 110 to the outlet face 120 .
  • the injector passage 130 has a passage inlet 131 in the inlet face 110 and a passage outlet 132 in the outlet face 120 .
  • the burner block 100 is mounted or incorporated in the walls of a combustion chamber, so that the outlet face 120 faces the combustion zone inside the combustion chamber whereas the inlet face 110 faces outwards of the furnace and is generally accessible from outside the combustion chamber for burner control, maintenance and repair.
  • the burner block 100 is made of refractory material.
  • the injector passage 130 comprises a wider precombustion section 135 in the vicinity of the passage outlet 132 .
  • the burner block 100 is an assembly of two parts of refractory material 136 and 137 .
  • Inlet face 110 comprises several facets 110 a, 110 b and 110 c .
  • the length of the precombustion section (in longitudinal direction D 1 ) is determined by the relative position of the two parts 136 , 137 of refractory material.
  • the injector assembly 200 comprises an inner oxygen supply pipe 210 , a fuel injector 220 and an oxygen injector 230 .
  • Fuel injector 220 has a fuel injection nozzle 222 at its downstream end 221 and surrounds the inner oxidant supply pipe 210 at least in the vicinity of the downstream end 211 of said inner oxidant supply pipe so as to create a flow of particulate solid fuel propelled by a conveyor gas around the inner oxygen supply pipe 210 and directed towards the passage outlet 132 for injection therefrom into the combustion zone.
  • fuel injection nozzle 222 is a separate piece mounted on the downstream end 221 of the fuel injector 220 .
  • a swirler 229 is mounted in fuel injector 220 near its downstream end 221 . Said swirler 229 surrounds the inner oxidant supply pipe 210 .
  • Oxidant injector 230 has an outer oxidant nozzle 232 at its downstream end 231 for the injection of the outer oxidant.
  • the oxidant injector 230 surrounds the fuel injector 220 , at least in the vicinity of the downstream end 231 of the oxidant injector 230 .
  • the oxidant injector 230 thus provides a flow of outer oxidant around the fuel injector 220 and towards the passage outlet 132 for injection therefrom into the combustion zone.
  • downstream end 231 of the oxidant injector 230 is positioned further away from the passage outlet 132 than the downstream end 211 and 221 of respectively the inner oxidant supply pipe 210 and the fuel injector 220 .
  • the inner oxidant supply pipe 210 is positioned centrally within fuel injector 220 .
  • a number of lateral inner oxidant nozzles 212 are mounted on the lateral surface of inner oxidant supply pipe 210 , by means of perforations 215 in said lateral surface. These lateral inner oxidant nozzles and the corresponding perforations 215 are positioned at different distances from the downstream end 211 of the inner oxidant supply pipe 210 .
  • these lateral second inner oxidant nozzles 212 inject second inner oxidant into the fuel injector body thereby progressively enriching the conveyor gas as it projects the particulate solid fuel towards the fuel injection nozzle 222 and the passage outlet 132 .
  • the lateral inner oxidant nozzles 212 have an injection opening orientated so as to inject second inner oxidant into fuel injector 220 with an injection direction towards the passage outlet 132 , substantially tangential to the lateral surface of the oxygen supply pipe and forming an angle ⁇ with the longitudinal direction D 1 of the injector passage 130 .
  • the inner oxidant supply pipe 210 further comprises a central oxidant lance 213 which terminates in a terminal primary oxidant nozzle 216 .
  • the terminal nozzle 216 of the central oxidant lance 213 injects first inner oxidant in the longitudinal direction D 1 of the injector passage towards the passage outlet.
  • An annular passage 214 surrounding the central oxidant lance 213 is formed between the oxidant lance and the lateral surface of the inner oxidant supply pipe 210 , the lateral inner oxidant nozzles 212 being in fluid communication with said annular passage 214 via perforations 215 .
  • the fuel injector 220 is in fluid connection with a fuel supply line comprising an elbow 223 upstream of the fuel injector 220 .
  • Branch pipe 224 is mounted on the fuel supply line at said elbow 223 and extends in line with the fuel injector 220 .
  • Inner oxidant supply pipe 210 extends from said branch pipe 224 into the fuel injector 220 .
  • Oxidant distributor 240 is positioned at the upstream end of the inner oxidant supply pipe 210 .
  • the oxidant distributor 240 comprises an inlet chamber 241 and two outlet chambers 242 , 243 .
  • the inlet chamber 241 is connected to a source of inner oxidant via inlet opening 246 .
  • the first outlet chamber 242 is in fluid connection with the surrounding annular passage 214 of the inner oxidant supply pipe 210 .
  • the second outlet chamber 243 is in fluid connection with the central oxidant lance 213 .
  • the inlet chamber 241 communicates with the first outlet chamber 242 via first passage 247 .
  • the inlet chamber 241 communicates with the second outlet chamber 243 via second passage 248 .
  • the oxygen distributor 240 further comprises first and second means 247 a and 248 a for restricting the flow of inner oxidant through respectively the first and second passage 247 and 248 into respectively the first and second outlet chamber 242 and 243 and consequently for restricting the flow of inner oxidant to respectively the surrounding annular passage 214 and the central oxygen lance 213 .
  • Flow restriction can in particular be achieved by manually or automatically restricting the free cross section area of the first, respectively second passage.
  • first screw 247 a and second screw 248 a are used as respectively the first and second means for restricting the flow of inner oxidant.
  • inner oxidant flows from a source of inner oxidant into the inlet chamber 241 of oxidant distributor 240 via inlet opening 246 . Said flow of inner oxidant is then divided over the first and second outlet chambers 242 and 243 at a ratio determined by the settings of the first and second means for restricting the flow of inner oxidant. Thereafter, the inner oxidant flows from the first outlet chamber 242 to the central oxygen lance 213 , and then to the terminal nozzle 216 and from the second outlet chamber 243 to the surrounding annular passage 214 and then to the lateral inner oxidant nozzles 212 .
  • An auxiliary gaseous fuel burner was used to preheat the furnace to a temperature of 900° C., before starting up above-described the particulate solid fuel burner.
  • the particulate solid fuel was a standard pulverized coal with a particle size (diameter) in the range of 75 to 120 ⁇ m.
  • the conveyor gas was recycled combustion gas. Analogous results were obtained with air as the conveyor gas.
  • the conveyor gas was supplied to the burner at a rate of 17.6 Nm3/h. It propelled pulverized coal to the burner at a rate of 30 kg/h.
  • the outer oxidant was supplied to the burner at a rate of 33 Nm3/h.
  • the total inner oxidant supply to the burner (first and second inner oxidants) was 13 Nm3/h.
  • the same oxidant with an oxygen content of 90% vol O 2 was used for the outer, for the first inner and for the second inner oxidant.
  • the total oxygen supply to the furnace corresponded to 113% of the stoichiometrically required amount of combustion oxygen.
  • the outer oxidant supply to the burner corresponded to 71.74% of the total supply to the burner and to 68.07% of the stoichiometrically required amount of oxygen.
  • the total inner oxidant supply to the burner corresponded to 28.26% of the total oxygen supply to the burner and to 31.93% of the stoichiometrically required amount of oxygen.
  • the inner oxidant discharge velocity was higher than the fuel discharge velocity.
  • the oxygen-enriched fuel flow mixed with the first inner oxidant flow before mixing with the outer oxidant flow.
  • FIGS. 1 and 2 are schematic representations in cross section of the type of flame obtained.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)
US13/505,149 2009-10-30 2010-10-29 Method of Combusting Particulate Solid Fuel with a Burner Abandoned US20120216730A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP09174635.4 2009-10-30
EP09174635A EP2317222A1 (de) 2009-10-30 2009-10-30 Verfahren zum Verbrennen von Partikelfeststoffbrennstoff mit einem Brenner
PCT/EP2010/066500 WO2011051464A2 (en) 2009-10-30 2010-10-29 Method of combusting particulate solid fuel with a burner

Publications (1)

Publication Number Publication Date
US20120216730A1 true US20120216730A1 (en) 2012-08-30

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US13/505,149 Abandoned US20120216730A1 (en) 2009-10-30 2010-10-29 Method of Combusting Particulate Solid Fuel with a Burner

Country Status (9)

Country Link
US (1) US20120216730A1 (de)
EP (2) EP2317222A1 (de)
JP (1) JP2013509561A (de)
KR (1) KR20120099225A (de)
CN (1) CN102597629B (de)
BR (1) BR112012010219A2 (de)
EA (1) EA201290247A1 (de)
IN (1) IN2012DN03179A (de)
WO (1) WO2011051464A2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015034493A1 (en) * 2013-09-05 2015-03-12 Honeywell International Inc. Pulverized fuel-oxygen burner

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8707877B2 (en) 2011-06-05 2014-04-29 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Solid fuel and oxygen combustion with low NOx and efficient burnout
CN103663928A (zh) * 2013-12-06 2014-03-26 无锡顺鼎阿泰克科技有限公司 石油焦粉燃烧方法
JP6314637B2 (ja) * 2014-05-09 2018-04-25 株式会社Ihi バーナ
KR101726344B1 (ko) * 2016-04-29 2017-04-12 주식회사 컴버스텍 멀티연료 공급용 연소기
CN106090894B (zh) * 2016-08-23 2019-10-29 翼特新能源科技（上海）有限公司 一种低NOx的全氧燃烧装置及其燃烧方法和应用
CN107606629B (zh) * 2017-10-26 2024-07-19 北京启创天工电力技术应用有限公司 一种scr脱硝机组空预器防堵灰硫酸氢铵汽化加热装置
EP3586949A1 (de) 2018-06-26 2020-01-01 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Sauerstoffanreicherung und verbrennung eines brennstoffs in form von festpartikeln, die von einem trägergas befördert werden
CN114657294B (zh) * 2022-03-31 2023-02-07 北京科技大学 模拟高炉喷吹燃料燃烧的实验方法及装置

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US5743723A (en) * 1995-09-15 1998-04-28 American Air Liquide, Inc. Oxy-fuel burner having coaxial fuel and oxidant outlets
US5904475A (en) * 1997-05-08 1999-05-18 Praxair Technology, Inc. Dual oxidant combustion system
US6109913A (en) * 1999-10-20 2000-08-29 Texas Industries, Inc. Method and apparatus for disposing of waste dust generated in the manufacture of cement clinker
US20040185404A1 (en) * 2003-01-21 2004-09-23 Fabienne Chatel-Pelage Process and apparatus for oxygen enrichment in fuel conveying gases
US6843185B1 (en) * 2003-06-27 2005-01-18 Maxon Corporation Burner with oxygen and fuel mixing apparatus
US7756591B2 (en) * 2006-04-25 2010-07-13 Pegasus Technologies, Inc. System for optimizing oxygen in a boiler
US8105074B2 (en) * 2008-06-30 2012-01-31 Praxair Technology, Inc. Reliable ignition of hot oxygen generator

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Publication number Priority date Publication date Assignee Title
US5743723A (en) * 1995-09-15 1998-04-28 American Air Liquide, Inc. Oxy-fuel burner having coaxial fuel and oxidant outlets
US5904475A (en) * 1997-05-08 1999-05-18 Praxair Technology, Inc. Dual oxidant combustion system
US6109913A (en) * 1999-10-20 2000-08-29 Texas Industries, Inc. Method and apparatus for disposing of waste dust generated in the manufacture of cement clinker
US20040185404A1 (en) * 2003-01-21 2004-09-23 Fabienne Chatel-Pelage Process and apparatus for oxygen enrichment in fuel conveying gases
US6843185B1 (en) * 2003-06-27 2005-01-18 Maxon Corporation Burner with oxygen and fuel mixing apparatus
US7756591B2 (en) * 2006-04-25 2010-07-13 Pegasus Technologies, Inc. System for optimizing oxygen in a boiler
US8105074B2 (en) * 2008-06-30 2012-01-31 Praxair Technology, Inc. Reliable ignition of hot oxygen generator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015034493A1 (en) * 2013-09-05 2015-03-12 Honeywell International Inc. Pulverized fuel-oxygen burner
US20170343212A1 (en) * 2013-09-05 2017-11-30 Honeywell International Inc. Pulverized fuel-oxygen burner
US10371377B2 (en) * 2013-09-05 2019-08-06 Honeywell International Inc. Pulverized fuel-oxygen burner

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Publication number Publication date
KR20120099225A (ko) 2012-09-07
JP2013509561A (ja) 2013-03-14
EA201290247A1 (ru) 2012-11-30
WO2011051464A2 (en) 2011-05-05
EP2494274A2 (de) 2012-09-05
WO2011051464A3 (en) 2011-08-25
CN102597629A (zh) 2012-07-18
EP2494274B1 (de) 2014-07-09
BR112012010219A2 (pt) 2017-08-08
EP2317222A1 (de) 2011-05-04
CN102597629B (zh) 2014-09-24
IN2012DN03179A (de) 2015-09-25

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