US3918834A - Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant - Google Patents

Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant Download PDF

Info

Publication number
US3918834A
US3918834A US387128A US38712873A US3918834A US 3918834 A US3918834 A US 3918834A US 387128 A US387128 A US 387128A US 38712873 A US38712873 A US 38712873A US 3918834 A US3918834 A US 3918834A
Authority
US
United States
Prior art keywords
fuel
air
burners
combustion
flow
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.)
Expired - Lifetime
Application number
US387128A
Inventor
Isaak Yakovlevich Sigal
Georgy Fedorovich Naidenov
Sergei Savatievich Nizhnik
Nikolai Alexandrovich Gurevich
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US387128A priority Critical patent/US3918834A/en
Priority to NL7311040.A priority patent/NL155937B/en
Priority to DE2340737A priority patent/DE2340737C3/en
Application granted granted Critical
Publication of US3918834A publication Critical patent/US3918834A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B5/00Combustion apparatus with arrangements for burning uncombusted material from primary combustion
    • 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 
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • F23C7/002Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B2700/00Combustion apparatus for solid fuel
    • F23B2700/018Combustion apparatus for solid fuel with fume afterburning by staged combustion

Definitions

  • the two-stage combustion being accomplished by redistributing the flows of fuel and air inside the burners so that some air mixed with fuel is introduced in a spiral flow at periphery of the passages through the burners, and the rest of the air required for complete combustion of the fuel being introduced in a straight-line flow directed along the axis of the burners.
  • the present invention relates to the protection of the atmosphere by products of combustion of a natural fuel, predominantly a gaseous one, and more specifically to a method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant.
  • This object is attained in that a two-stage combustion ofthe fuel is employed under the conditions of oxygen deficiency in a high-temperature zone, the two-stage combustion being accomplished by redistributing the flow of the fuel and the air inside the burner or burners so that some air mixed with fuel is introduced in a spiral flow at the periphery of a passage through the burner, and the rest of the air, required for complete combustion of the fuel, is introduced in a straight-line flow directed along the axis of the burner.
  • the inventive method of reducing the concentration of nitrogen oxides is accomplished by directly redistributing the fuel and air flow directly so that the nitrogen oxide content of gaseous effluent is reduced by 30 to 35% without installing special nozzles, disturbing the brickwork of the thermal plant or branching of water tubes.
  • the method also allows to control the parameters of the flame over a wide range, under variable conditions so, that the fuel is utilized in a more effective way and thus a higher operational reliability of the plant is achieved.
  • the disclosed method has been tested in a laboratory of the Institute of Gas, Ukrainian Academy of Sciences, and in industrial plants. The tests have proved the efficiency of the invention in burning fuel in thermal plants of various designs.
  • FIG. 1 is a schematic longitudinal section of a burner for carrying out the inventive method
  • FIG. 2 is an end view of FIG. 1 in the direction of arrow I. g
  • the method of reducing the concentration of nitrogen oxides in the gaseous effluent from a thermal plant equipped with burners consists in a two-stage combustion of the fuel under the conditions of oxygen deficiency in a high-temperature zone at the first stage.
  • the two-stage combustion is accomplished by redistributing the flow of fuel and air inside the burners so that some of the air mixed with the fuel is introduced in a spiral flow at the periphery of a passage through the burner, and the rest of the air, required for complete combustion of the fuel, is introduced in a straight-line flow directed along the axis of the burner.
  • the method is performed with the aid of a burner comprising a cylindrical part 1 (FIG. 1) and a tapered part 2.
  • a burner comprising a cylindrical part 1 (FIG. 1) and a tapered part 2.
  • the gas chamber 3 and the cylindrical part 1 are provided with holes 4 drilled peripherally in preferably two rows so as to admit gaseous fuel from the gas chamber 3 into the inner passage of the cylindrical part 1 of.
  • Disposed inside the burner, concentrically with its cylindrical part 1 (FIG. 1 is a cylindrical tube 6 through which the rest of the air, required for the complete combustion of the fuel at the second stage of combustion, is introduced in a straight-line flow along the axis of the burner.
  • the tapered part 2 of the burner forms a port in a brick-work 7 of the thermal plant (not shown), the port widening towards a fire chamber.
  • the inventive method of reducing the concentration of nitrogen oxides in the gaseous effluent of the thermal plant is accomplished as follows. Only part of the air required for the combustion of the gaseous fuel is introduced through the tangential branch 5 (FIGS. 1 and 2). The flow of this air spirals around the periphery of the passage through the cylindrical part 1 of the burner.
  • the gaseous fuel is introduced from the gas chamber 3 through the holes 4 into the spiral flow of some of the air required for combustion.
  • the gaseous fuel mixes with the flow of air spiralling around the periphery.
  • the gas/air mixture (all the fuel and the peripherally spiralling flow of air), being imparted a spiral motion, spreads out into the periphery of the tapered part 2 of the burner and thence to the periphery of the port where partial combustion of the fuel takes place in a cone-shaped flame expanding towards the fire chamher. this place being where a high-temperature zone is formed at the first stage of combustion.
  • the axial space in the port (formed by the tapered part 2) is not filled with the flame, and introduced into this space is the rest of the air (roughly between 30 and 60% of the total amount required for the complete combustion of the fuel), as it is issued from the axial tube 6 in a straight-line flow.
  • the sucking action of the axial cocurrent flow of air causes the products of incomplete combustion to move inwardly, towards the axis, at a point away from the burner port, where the centrifugal force tending to separate the peripheral flow from the axial one is low enough not to counteract this sucking action.
  • a method of reducing the concentration of nitrogen oxides in a gaseous effluent of the combustion in a thermal plant fitted with burners having axial passages comprising the steps of burning a fuel in two stages within the same heat-receiving chamher of the thermal plant, under the conditions of oxygen deficiency in a high-temperature zone, the twostage combustion being accomplished by redistributing the flow of the fuel and air inside the burners so that part of the air is introduced in a first, spiral flow at the periphery of the passages of the burners, and introducing the rest of the air, required for complete combustion of the fuel, in a second, straight-line flow directed along the axis of the burners, all of the fuel being introduced in a peripheral zone surrounding the axial passages, together with the first air flow, with which all fuel is intermixed, thereby causing a cone-shaped flame to emerge from the peripheral zone, constituting a first, high-temperature combustion stage, while the second air flow contributes to a second, lower
  • straight-line flow is 60 to 30 per cent of the supply.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

A method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant fitted with burners, consisting in the burning of the fuel in two stages under the conditions of oxygen deficiency in a high-temperature zone, the two-stage combustion being accomplished by redistributing the flows of fuel and air inside the burners so that some air mixed with fuel is introduced in a spiral flow at periphery of the passages through the burners, and the rest of the air required for complete combustion of the fuel being introduced in a straight-line flow directed along the axis of the burners.

Description

United States Patent [191 Sigal et al.
METHOD OF REDUCING THE CONCENTRATION OF NITROGEN OXIDES IN A GASEOUS EFFLUENT FROM A THERMAL PLANT Inventors: Isaak Yakovlevich Sigal, ulitsa Ezhena Potie, l1, kv. 107; Georgy Fedorovich Naidenov, Saratovskaya ulitsa 39, kv. 2]; Sergei Savatievich Nizhnik, ulitsa I. Sergienko, 23, kv. 60; Nikolai Alexandrovich Gurevich, ulitsa Frunze, 118/2, kv. 13, all of Kiev, U.S.S.R.
Filed: Aug. 9, 1973 Appl. No.: 387,128
US. Cl. 431/10; 431/185; 431/187 Int. Cl. F233 7/00 Field of Search 431/9, 10, 185, 187;
References Cited UNITED STATES PATENTS 5/1941 Lucke 431/9 Nov. 11, 1975 3,228,451 1/1966 Fraser et a1 431/10 3.266.549 8/1966 Wolfersperger 431/9 3.729.285 4/1973 Schwedersky 431/8 3.730.668 5/1973 lida et a1 431/10 3.758.258 9/1973 Kolhi 431/9 Primary Examiner-Charles J. Myhre Assistant Examiner-Wil1iam C. Anderson Attorney, Agent, or Firm-Waters, Schwartz & Nissen [5 7 ABSTRACT A method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant fitted with burners. consisting in the burning of the fuel in two stages under the conditions of oxygen deficiency in a high-temperature zone, the two-stage combustion being accomplished by redistributing the flows of fuel and air inside the burners so that some air mixed with fuel is introduced in a spiral flow at periphery of the passages through the burners, and the rest of the air required for complete combustion of the fuel being introduced in a straight-line flow directed along the axis of the burners.
2 Claims, 2 Drawing Figures US. Patent Nov. 11, 1975 METHOD OF REDUCING THE CONCENTRATION OF NITROGEN OXIDES IN A GASEOUS EFFLUENT FROM A THERMAL PLANT The present invention relates to the protection of the atmosphere by products of combustion of a natural fuel, predominantly a gaseous one, and more specifically to a method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant.
Known in the art is a method of reducing the concentration of nitrogen oxides in flue gases of boilers by burning the fuel in two stages. This method consists in that some of the air required for burning the fuel is introduced through burners and the balance required to obtain a complete combustion of the fuel is admitted through special inlets (nozzles) outside the burners, the inlets being arranged as a rule above the top row of burners.
It is known that nitrogen oxides are apt to form in a high-temperature zone and that their concentration increases with the amount of free oxygen present in the high-temperature zone. The known method of burning fuel in two stages prevents the presence of surplus oxygen in the high-temperature zone because the combustion of the fuel at the first stage, which is the hightemperature one, takes place under conditions with a deficiency in the oxidizer.
In the known method, which employs partial admission of air through special inlets outside the burners, a number of disadvantages is encountered such as:
the necessity in additional branching of water tubes to give room for nozzles; this reduces the area of heat transfer, involves extra cost and impairs the'integrity of the brickwork;
the necessity in additional lines which must be made and installed in order to admit air into the nozzles;
difficulties experienced in controlling the requisite relationship between the rates of air flow to the burners and the nozzles; this makes the plant difficult to operate; and
inability to control the temperature of the flame from the burners so as to maintain the temperature specified for superheating the steam.
It is the object of the present invention to provide a method of reducing the concentration of nitrogen oxides in the gaseous effluent of thermal plants which eliminates the need for special inlets (nozzles), the additional branching of water tubes, and keeps intact the brickwork of the thermal plant while reducing the concentration of the nitrogen oxides in gaseous effluent.
This object is attained in that a two-stage combustion ofthe fuel is employed under the conditions of oxygen deficiency in a high-temperature zone, the two-stage combustion being accomplished by redistributing the flow of the fuel and the air inside the burner or burners so that some air mixed with fuel is introduced in a spiral flow at the periphery of a passage through the burner, and the rest of the air, required for complete combustion of the fuel, is introduced in a straight-line flow directed along the axis of the burner.
The inventive method of reducing the concentration of nitrogen oxides is accomplished by directly redistributing the fuel and air flow directly so that the nitrogen oxide content of gaseous effluent is reduced by 30 to 35% without installing special nozzles, disturbing the brickwork of the thermal plant or branching of water tubes. The method also allows to control the parameters of the flame over a wide range, under variable conditions so, that the fuel is utilized in a more effective way and thus a higher operational reliability of the plant is achieved.
The disclosed method has been tested in a laboratory of the Institute of Gas, Ukrainian Academy of Sciences, and in industrial plants. The tests have proved the efficiency of the invention in burning fuel in thermal plants of various designs.
The present invention will be best understood from the following detailed description of a preferred, exemplary embodiment when read in conjunction with the accompanying drawings, in which FIG. 1 is a schematic longitudinal section of a burner for carrying out the inventive method, and
FIG. 2 is an end view of FIG. 1 in the direction of arrow I. g
The method of reducing the concentration of nitrogen oxides in the gaseous effluent from a thermal plant equipped with burners consists in a two-stage combustion of the fuel under the conditions of oxygen deficiency in a high-temperature zone at the first stage. The two-stage combustion is accomplished by redistributing the flow of fuel and air inside the burners so that some of the air mixed with the fuel is introduced in a spiral flow at the periphery of a passage through the burner, and the rest of the air, required for complete combustion of the fuel, is introduced in a straight-line flow directed along the axis of the burner.
The method is performed with the aid of a burner comprising a cylindrical part 1 (FIG. 1) and a tapered part 2. Welded to the cylindrical part 1 there is an annular latter. The gas chamber 3 and the cylindrical part 1 are provided with holes 4 drilled peripherally in preferably two rows so as to admit gaseous fuel from the gas chamber 3 into the inner passage of the cylindrical part 1 of. Welded to the cylindrical part 1 (FIGS. 1 and 2) of the burner there is also a tangential branch 5 serving to admit some of the air supply, the direction of flow being indicated by an arrow. Disposed inside the burner, concentrically with its cylindrical part 1 (FIG. 1 is a cylindrical tube 6 through which the rest of the air, required for the complete combustion of the fuel at the second stage of combustion, is introduced in a straight-line flow along the axis of the burner.
The tapered part 2 of the burner forms a port in a brick-work 7 of the thermal plant (not shown), the port widening towards a fire chamber.
The inventive method of reducing the concentration of nitrogen oxides in the gaseous effluent of the thermal plant is accomplished as follows. Only part of the air required for the combustion of the gaseous fuel is introduced through the tangential branch 5 (FIGS. 1 and 2). The flow of this air spirals around the periphery of the passage through the cylindrical part 1 of the burner.
The gaseous fuel is introduced from the gas chamber 3 through the holes 4 into the spiral flow of some of the air required for combustion. The gaseous fuel mixes with the flow of air spiralling around the periphery. The gas/air mixture (all the fuel and the peripherally spiralling flow of air), being imparted a spiral motion, spreads out into the periphery of the tapered part 2 of the burner and thence to the periphery of the port where partial combustion of the fuel takes place in a cone-shaped flame expanding towards the fire chamher. this place being where a high-temperature zone is formed at the first stage of combustion.
The axial space in the port (formed by the tapered part 2) is not filled with the flame, and introduced into this space is the rest of the air (roughly between 30 and 60% of the total amount required for the complete combustion of the fuel), as it is issued from the axial tube 6 in a straight-line flow. The sucking action of the axial cocurrent flow of air causes the products of incomplete combustion to move inwardly, towards the axis, at a point away from the burner port, where the centrifugal force tending to separate the peripheral flow from the axial one is low enough not to counteract this sucking action.
This is why the rest of the fuel burns up in a straightline axial flow at a distance from the burner and the first, or high-temperature, zone of combustion, and the second stage of combustion is located at this distance.
What is claimed is:
1. A method of reducing the concentration of nitrogen oxides in a gaseous effluent of the combustion in a thermal plant fitted with burners having axial passages, the method comprising the steps of burning a fuel in two stages within the same heat-receiving chamher of the thermal plant, under the conditions of oxygen deficiency in a high-temperature zone, the twostage combustion being accomplished by redistributing the flow of the fuel and air inside the burners so that part of the air is introduced in a first, spiral flow at the periphery of the passages of the burners, and introducing the rest of the air, required for complete combustion of the fuel, in a second, straight-line flow directed along the axis of the burners, all of the fuel being introduced in a peripheral zone surrounding the axial passages, together with the first air flow, with which all fuel is intermixed, thereby causing a cone-shaped flame to emerge from the peripheral zone, constituting a first, high-temperature combustion stage, while the second air flow contributes to a second, lower-temperature combustion stage axially located with respect to but spaced at a distance from the first stage.
2. The method as defined in claim 1, wherein the amount of air allotted to the first, spiral flow is between 40 to per cent of the total air supply while the amount of air constituting the rest, for the second,
straight-line flow is 60 to 30 per cent of the supply.

Claims (2)

1. A METHOD OF REDUCING THE CONCENTRATION OF NITROGEN OXIDES IN A GASOUS EFFLUENT OF THE COMBUSTION IN A THERMAL PLANT FILLED WITH BURNERS HAVING AXIAL PASSAGES, THE METHOD COMPRISING THE STEPS OF BURNING A FUEL IN TWO STAGES WITHIN THE SAME HEAT-RECEIVING CHAMBER OF THE THERMAL PLANT, UNDER THE CONDITIONS OF OXYGEN DEFICIENCY IN A HIGH TEMPERATURE ZONE THE TWO-STAGE COMBUSTION BEING ACCOMPLISHED BY REDISTRIBUTING THE FLOW OF THE FUEL AND AIR INSIDE THE BURNERS SO THAT PART OF THE AIR IS INTRODUCED IN A FIRST, SPIRAL AT THE PERIPHERY OF THE PASSAGES OF THE BURNERS, AND INTRODUCING THE REST OF THE AIR, REQUIRED FOR COMPLETE COMBUSTION OF THE FUEL, IN A SECOND STRAIGHT-LINE FLOW DIRECTED ALONG THE AXIS OF THE BURNERS, ALL OF THE FUEL BEING INTRODUCED IN A PERIPHERAL ZONE SURROUNDING THE AXIAL PASSAGES, TOGETHER WITH THE FIRST AIR FLOW, WITH WHICH ALL FUEL IS INTERMIXED, THEREYCAUSING A CONE-SHAPED FLAME TO EMERGE FROM THE PERIPHERAL ZNE CONSTITUTING A FIRST, HIGHTEMPERATURE COMBUSTION STAGE, WHILE THE SECOND AIR FLOW CONTRIBUTES TO A SECOND LOWER-TEMPERATURE COMBUSTION STAGE AXIALLY LOCATED WITH RESPECT TO BUT SPACED AT A DISTANCE FROM THE FIRST STAGE.
2. The method as defined in claim 1, wherein the amount of air allotted to the first, spiral flow is between 40 to 70 per cent of the total air supply while the amount of air constituting the rest, for the second, straight-line flow is 60 to 30 per cent of the supply.
US387128A 1973-08-09 1973-08-09 Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant Expired - Lifetime US3918834A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US387128A US3918834A (en) 1973-08-09 1973-08-09 Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant
NL7311040.A NL155937B (en) 1973-08-09 1973-08-09 BURNER CONSISTING OF A TUBULAR MIXING CHAMBER.
DE2340737A DE2340737C3 (en) 1973-08-09 1973-08-11 Gas burner for a thermal power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US387128A US3918834A (en) 1973-08-09 1973-08-09 Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant

Publications (1)

Publication Number Publication Date
US3918834A true US3918834A (en) 1975-11-11

Family

ID=23528577

Family Applications (1)

Application Number Title Priority Date Filing Date
US387128A Expired - Lifetime US3918834A (en) 1973-08-09 1973-08-09 Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant

Country Status (3)

Country Link
US (1) US3918834A (en)
DE (1) DE2340737C3 (en)
NL (1) NL155937B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4206712A (en) * 1978-06-29 1980-06-10 Foster Wheeler Energy Corporation Fuel-staging coal burner
FR2485692A1 (en) * 1980-06-27 1981-12-31 Kawasaki Steel Co METHOD AND BURNER FOR PRODUCING LOW NITROXY OXIDE COMBUSTION OF EXHAUST GASES IN A RADIANT TUBE
US4629413A (en) * 1984-09-10 1986-12-16 Exxon Research & Engineering Co. Low NOx premix burner
US6663381B2 (en) * 2001-09-20 2003-12-16 Carrier Corporation Burner arrangement for low NOX emissions
US20110048293A1 (en) * 2009-08-26 2011-03-03 R-V Industries, Inc. Nozzle for feeding combustion media into a furnace

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2242797A (en) * 1938-02-26 1941-05-20 Babcock & Wilcox Co Method of and apparatus for burning fluid fuel
US3228451A (en) * 1957-06-25 1966-01-11 Urquhart S 1926 Ltd Method of burning fuels
US3266549A (en) * 1964-07-03 1966-08-16 John J Wolfersperger Gas burner
US3729285A (en) * 1972-05-22 1973-04-24 G Schwedersky Burner and method of operating it to control the production of nitrogen oxides
US3730668A (en) * 1971-03-03 1973-05-01 Tokyo Gas Co Ltd Combustion method of gas burners for suppressing the formation of nitrogen oxides and burner apparatus for practicing said method
US3758258A (en) * 1970-03-24 1973-09-11 Collin Consult A method for combusting fuels in a substantially conically shaped curtain

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2242797A (en) * 1938-02-26 1941-05-20 Babcock & Wilcox Co Method of and apparatus for burning fluid fuel
US3228451A (en) * 1957-06-25 1966-01-11 Urquhart S 1926 Ltd Method of burning fuels
US3266549A (en) * 1964-07-03 1966-08-16 John J Wolfersperger Gas burner
US3758258A (en) * 1970-03-24 1973-09-11 Collin Consult A method for combusting fuels in a substantially conically shaped curtain
US3730668A (en) * 1971-03-03 1973-05-01 Tokyo Gas Co Ltd Combustion method of gas burners for suppressing the formation of nitrogen oxides and burner apparatus for practicing said method
US3729285A (en) * 1972-05-22 1973-04-24 G Schwedersky Burner and method of operating it to control the production of nitrogen oxides

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4206712A (en) * 1978-06-29 1980-06-10 Foster Wheeler Energy Corporation Fuel-staging coal burner
FR2485692A1 (en) * 1980-06-27 1981-12-31 Kawasaki Steel Co METHOD AND BURNER FOR PRODUCING LOW NITROXY OXIDE COMBUSTION OF EXHAUST GASES IN A RADIANT TUBE
DE3124986A1 (en) * 1980-06-27 1982-03-04 Kawasaki Steel Corp., Kobe, Hyogo LOW NO (ARROW DOWN) X (ARROW DOWN) LEVEL COMBUSTION METHOD IN A PIPE TORCH, AND DETERMINED COMBUSTION DEVICE THEREFOR
US4629413A (en) * 1984-09-10 1986-12-16 Exxon Research & Engineering Co. Low NOx premix burner
US6663381B2 (en) * 2001-09-20 2003-12-16 Carrier Corporation Burner arrangement for low NOX emissions
US20110048293A1 (en) * 2009-08-26 2011-03-03 R-V Industries, Inc. Nozzle for feeding combustion media into a furnace
US8413595B2 (en) * 2009-08-26 2013-04-09 R-V Industries, Inc. Nozzle for feeding combustion media into a furnace

Also Published As

Publication number Publication date
NL7311040A (en) 1975-02-11
NL155937B (en) 1978-02-15
DE2340737C3 (en) 1979-05-31
DE2340737A1 (en) 1975-03-06
DE2340737B2 (en) 1978-09-07

Similar Documents

Publication Publication Date Title
EP0657689B1 (en) Staged air, low NOx burner with internal recuperative flue gas recirculation
US5020479A (en) Watertube boiler and its method of combustion
US5158445A (en) Ultra-low pollutant emission combustion method and apparatus
EP0432153B1 (en) Method and apparatus for generating highly luminous flame
US5029557A (en) Cyclone combustion apparatus
US4879959A (en) Swirl combustion apparatus
EP0575043B1 (en) Fuel-burner method and apparatus
US5220888A (en) Cyclonic combustion
JPH09159107A (en) Method and equipment for reducing nox formed during combustion of air-oxygen-fuel
GB2028490A (en) Recuperative burner
US5181475A (en) Apparatus and process for control of nitric oxide emissions from combustion devices using vortex rings and the like
US5059117A (en) Radiant tube furnace and method of burning a fuel
US6971336B1 (en) Super low NOx, high efficiency, compact firetube boiler
US3918834A (en) Method of reducing the concentration of nitrogen oxides in a gaseous effluent from a thermal plant
US3187799A (en) Self-stabilizing combustion apparatus and method
US4860695A (en) Cyclone combustion apparatus
US3204936A (en) Shaft furnace
JPS6137541B2 (en)
US5248252A (en) Enhanced radiant output burner
EP0913639B1 (en) Apparatus and method for burning combustible gases
US5823759A (en) Apparatus and method for burning combustible gases
US3273623A (en) Self-stabilizing combustion apparatus
US3994670A (en) Furnace heating
US3115120A (en) Apparatus for burning low heat value fuels
US3373981A (en) Apparatus for operating a burner fired shaft furnace