US3802827A - Method and apparatus for producing a protective atmosphere in heating furnaces - Google Patents

Method and apparatus for producing a protective atmosphere in heating furnaces Download PDF

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US3802827A
US3802827A US00208084A US20808471A US3802827A US 3802827 A US3802827 A US 3802827A US 00208084 A US00208084 A US 00208084A US 20808471 A US20808471 A US 20808471A US 3802827 A US3802827 A US 3802827A
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air
fuel
chamber
combustion
heating furnace
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N Semenov
L Gussak
V Boboley
E Unxov
A Astafiev
M Khazanov
V Moroz
L Baranovsky
V Afanasiev
I Zubov
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    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/74Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
    • C21D1/76Adjusting the composition of the atmosphere
    • 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

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  • the present invention relates to a method and a plant o asnevc for producing a protective atmosphere in a heating i k H 2 furnace.
  • the invention provides for the incomplete k 8 5 g: i s 1 combustion of an insufficient amount of an air-fuel R 2. i u I mixture in a secondary combustion chamber and the 2 2?
  • the invention contemplates providing for stabilization of the combustion process at an air excess ratio of 0.5 alongside with simultaneous improvement in the blending of gaseous fuel and air due to chemically active gaseousp'roducts.
  • a plant for putting into effect the method of the invention comprises a burning device with a main nozzle and auxiliary nozzles in communication with a special chamber of combustion.
  • the present invention is best suited for the precise hot working of metal bodies in preference for highprecision stamping, rolling and die stamping ofblanks (e.g., turbine blanks),-all the above operations being final in the production process.
  • bladenks e.g., turbine blanks
  • the present invention relates to heating furnaces for heating metal bodies either during heat-treating processes or-for subsequent processing by plastic flow at elevated temperatures. More particularly the present in-v vention relates to a method and-a plant forproducing a protective atmosphere directly'in said furnaces.
  • the present invention is'best suited for precise hot working of metal bodies, and preferably, for highprecision stamping, rolling and die'stampingof blanks (e.g., turbine blades), with all the above operations being final in the production process.
  • blanks e.g., turbine blades
  • the products of complete combustion are partially directed to a zone accommodating the metal bodies being preheated, withthe intention of utilizing the heat of these products.
  • the combustion products then p'assedfrom the furnace to 'recuperators (see, for instance, the GFR Patent N 1 116255).
  • the main object of the present invention is to stabilize the combustion process using an air excess ratio of 0.5 which assures simultaneously better mixing of air and 'gas.
  • this is achieved by continuously introducing into a'flow of an air-gas mixture being ignited and burnt with an insufficient amount of air, chemically active gaseous products, such as aldehydes, peroxides, atoms and radicals of combustible gases amounting to 1 percent by volume of the total quantity of the fuel to be burnt, said additions being aimed at stabilizing the ignition process and providefor more complete combustion.
  • chemically active gaseous products such as aldehydes, peroxides, atoms and radicals of combustible gases amounting to 1 percent by volume of the total quantity of the fuel to be burnt, said additions being aimed at stabilizing the ignition process and providefor more complete combustion.
  • the above-products they may be the products of combustion of any. combustible gases though preference shall be given to the products'of combustion of the air-gas mixture containing the same constituents as those being burnt in the fumace. It would be expedient to burnthe major part of the fuel at an air excess ratio exceeding thatpe
  • the above arrangement of the nozzles assures highly intensive turbulence of the air-gas mixture admitted into the furnace for combustion.
  • a most compact plant design is assured if the chamber for combustion of the minor part of the fuel is ring-shaped and is arranged at the circumference of the exit nozzle of the-'buming device.
  • the process of ignition in the chamber for burning the minor portion of the fuel is stabilized by making the chamber inlet in the form of a ring-shaped slot arranged in a-radialsection. It is also expedient to locate an inlet passage for admitting the above mixture into the slot across one of its sides.
  • an igniter for the chamber for burning a part of the air-gas mixture it is expedient to use a constantacting electro-spark generator. This rules out intermissions which may be hazardous when combustion is carried out with insufficient air.
  • a substantial advantage of the present invention lies in that the torch temperature remains constant and relatively high at a stable air excess ratio not over 0.5 which can vary, if desired, from 800 to 1250C.
  • FIG. 1 is a fragmentary longitudinal sectional view of a plant conforming to the invention
  • FIG. 2 is a view along arrow A of FIG. 1.
  • a plant is fitted with burning device 1 (FlG 1) comprising mixer 2 of a conventional design and coupled to it by bolts 4 is a cone-shaped outlet nozzle 3 referred to hereinafter as a main nozzle.
  • Mixer 2 and main nozzle 3 are fastened on flange 5 by means of dowels (not shown in the drawing).
  • the walls of central bore 6 provided in flange 5 and the external walls of main nozzle 3 are separated by asbestos lining 7.
  • Burning device 1 is secured with the aid of flanges 5 and bolts 8 to disc 9 embedded in the brickwork of heating furnace 10.
  • the places of contact of flange 5 and disc 9 are insulated by asbestos annular linings 11 and 12.
  • the linings are placed at the ends of circular centering bosses 13 and 14 made on disc 9.
  • flange 5 is fitted with recesses to receive the above bosses.
  • a ringshaped section between bosses 13 and 14 of disc has annular depression 15. Opposite this depression there is another annular depression 16 in flange 5. Both depressions form cavity 17 acting as a chamber for burning'the minor part of the fuel admitted into the chamber after being mixed with air along sleeve 18 welded to flange 5 and conduits l9 and 20 provided in flange 5 and disc 9 respectively.
  • Sleeve 18 and each of conduits l9 and 20 have similar cross-sections designed for passing of the total amount of the'fuel supplied to mixer 2.
  • Mounted in cavity 17 are two annular parts 21 and 22 the first of which is located in depression 16 and the second in depression 15. Both parts are fitted with alternating projections and recesses forming an altogether circular V- shaped radial section slot 23 in the intake of chamber 17.
  • the walls of the foregoing parts having an appropriate design, serve as the slot walls.
  • Conduit 20 which is an inlet passage in relation to chamber 17, and one of the sides of slot 23 are perpendicular to each other.
  • the above arrangement of the plant provides for the stabilization of the process of combustion of the air-gas mixture in chamber 17.
  • the latter is located at the circumference of main nozzle 3 and being in communication with auxiliary nozzles 24 (FIGS. 1 and 2) distributed uniformly around main nozzle 3.
  • the nozzles are cylindrical passages provided in disc 9 with their exits being arranged on the walls of central bore 25 having cone-shaped walls made in disc 9 and positioned opposite main nozzle 3 of burning device 1.
  • Section 26 of the passage of main nozzle 3 is cylindrical at the exit with a large cone-shaped base formed by the wall faces of hole 25 in the middle portion of the furnace.
  • the above embodiment of the plant assures favourable conditions for blending the products of combustion emerging from auxiliary nozzles 24 with the flow of the air-gas mixture issuing from main nozzle
  • the upper part of chamber 17 is provided with a constant-acting known electro-spark generator 27 set up on lug '28 welded to flange 5.
  • a tail portion of generator 27 is located in passage 29 running in lug 28, passage 30 in flange 5 and in passage 31, located in annular part 21 with all said passages being coaxial.
  • the plant is designed to obtain a protective atmosphere in heating furance 10 which serves to heating metal bodies under conditions which prevent the formation of oxides on these bodies in the process of said heating.
  • Mixer 2 is designedand calculated to form an air-gas mixture, for example, a mixture of natural gas and air, at an air excess ratio of 0.5. From 3 to 10 percent by volume of the fuel, as indicated above, is mixed with air and passed via sleeve 18 and conduit 19 to inlet conduit 20 arranged perpendicularly to, one of the circular V- shaped sides of the radial sectioned slot 23 forming the inlet of chamber 17. Due to the arrangement of conduit 20 and slot 23 as well as the said shape of this slot an intense swirling of the air-gas mixture is obtained at the inlet of the relatively small chamber 17, where the mixture is continuously ignited by generator 27.
  • an air-gas mixture for example, a mixture of natural gas and air
  • Chemically active products of incomplete combustion effected at an air excess ratio of 0.55-0.7 which slightly exceeding that of the air excess ratio used for the burning of the main part of the fuel, are added via additional nozzles 24 to the main flow of the air-gas mixture and passed into the zone of the most intense turbulence contributed by the chemical initiation process upon ignition.
  • a stable high-temperature torch is produced whose temperature can be altered, if required, within the range of from 800 to 1250C by adjusting the volume of the mixture fed to the burner.
  • the proposed method assures stable combustion of the overwhelming amount of the air-gas mixture at said air excess ratio of 0.5. This eliminates completely the need for regenerators.
  • the present invention does not, in any way, preclude the possibility of using the products of combustion of any known combustible gases as chemically active gaseous products amounting to not more than 10 percent of the total fuel being burnt for stabilizing the process of ignition. If that is the case the chamber for burning air-gas mixture becomes useless.
  • a method for producing a protective atmosphere in a heating furnace in which the stabilization of an ignition process providing more complete combustion is accomplished comprising adding chemically active gaseous products amounting to 10% by volume of the narcissist ⁇ ofiii'fiil' bmgisarni aid asses 56m continuously introduced into a flow of an air-gas mixture which is intended to be burned with an insufficient amount of air.
  • a plant for producing a protective atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 3-10 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzle; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.
  • a plant for producing a protective atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 31 0 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzle, said chamber being provided with an inlet in the form of a circular V-shaped slot in a radial section with an inlet conduit for feeding said mixture into the slot being located across one of its sides; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.

Abstract

The present invention relates to a method and a plant for producing a protective atmosphere in a heating furnace. The invention provides for the incomplete combustion of an insufficient amount of an air-fuel mixture in a secondary combustion chamber and the directing of the combustion products produced therein to the main combustion chamber, also for incomplete combustion. As a result, a protective atmosphere is obtained with an air excess ratio not exceeding 0.5. The present invention is particularly well suited for heating steel bodies.

Description

United States Patent 1191 1111 3,802,827 Semenov et al., 1 Apr. 9, 1974 [5 METHOD AND APPARATUS FOR July 23. 1969 U.S.S.R t. 1351706 PRODUCING A PROTECTIVE ATMOSPHERE IN HEATING FURNAQES 1521 us. 01 431/8, 432/222, 431/285 Inventors: se nenov lnt. vol-obievskoe shossev 2 1; Lev [58] Field of Search 431/2, 4. 176. 158, 187, Abramovich Gussak, Leninsky 431/284 285; 432/219- 222 prospekt, 57, kv. 86; Vasily Konstantinovich Boboley, i Vorobievskoe Shosse, 1 1, kv. 36; [56] References C' Evgmy Pavhvich UNITED STATES PATENTS Rusakovskaya, ulitsa, 6, kv, 95; Anatoly Alexandrovich Asmfiev, 2,697,482 12/1954 Bhzard 6 0/39.46 X Sharikopodshipnikovskaya ulitsa, 2, v kv. 34; Mikhail Semenovich Primary Examiner-William F. ODea Khazanov, Festivalnaya ulitsa, '14, Assistant E.\'aminerWilliam C. Anderson korpus 3, kv. 67; Vitaly Iosifovich Attorney, Agent, or Firm-Holman & Stern Moroz, Sharikopodshipnikovskaya ulitsa, 2a, kv. 76; Leonid Semenovich Baranovsky, v ABSTRACT y ii g gsii i Q) i The present invention relates to a method and a plant o asnevc for producing a protective atmosphere in a heating i k H 2 furnace. The invention provides for the incomplete k 8 5 g: i s 1 combustion of an insufficient amount of an air-fuel R 2. i u I mixture in a secondary combustion chamber and the 2 2? i z s g directing of the combustion products produced a O oscow therein to the main combustion chamber, also for in- [22] Filed: Dec. 15, 1971 complete combustion. As a result, a protective atmosphere is obtained with an air excess ratio not exceed- [211 App! 208084 ing 0.5. The present invention is particularly well suited for heatingsteel bodies. [30] Foreign Application Priority Data July 23, 1969 U.S.S.R 1351705 8 2 Drawmg F'gures 5\ 27 /4. g9 26 8 in 50/2: j 4 1/ I110," 2 l7 J 0 2.7 )2 E 7 T I I It? /9 4 I\ t s 1 METHOD AND APPARATUS FOR PRODUCING A PROTECTIVE ATMOSPHERE IN HEATING FURNACES The invention contemplates providing for stabilization of the combustion process at an air excess ratio of 0.5 alongside with simultaneous improvement in the blending of gaseous fuel and air due to chemically active gaseousp'roducts.
A plant for putting into effect the method of the invention comprises a burning device with a main nozzle and auxiliary nozzles in communication with a special chamber of combustion.
The present invention is best suited for the precise hot working of metal bodies in preference for highprecision stamping, rolling and die stamping ofblanks (e.g., turbine blanks),-all the above operations being final in the production process.
No less successfullythe present invention can be utilized in metallurgical furnaces, for-instance, in cupolas as well as in gas-fired boilers.
The present invention relates to heating furnaces for heating metal bodies either during heat-treating processes or-for subsequent processing by plastic flow at elevated temperatures. More particularly the present in-v vention relates to a method and-a plant forproducing a protective atmosphere directly'in said furnaces.
The present invention is'best suited for precise hot working of metal bodies, and preferably, for highprecision stamping, rolling and die'stampingof blanks (e.g., turbine blades), with all the above operations being final in the production process.
No less successfullythis invention can be utilizedin metallurgical furnaces, for instance, in cupolas as well as in gas fired boilers.
I Methods of producing a protective atmosphere directly ina heating furnace which uses a combustible air-gas mixture being burnt intheafores'aid furnace at an excess air ratio of about 0.5 are known in the prior art. Accordingly, before the mixture is prepared and burnt, both the gas and combustion air are'preheated in recuperators to temperature of from 300 to 700C. Then themixtnre may be burnt bymeans of intermixing-ingas burners mounted at one end of the furnace. The products of incomplete combustion reach the metal bodies to be heated, and go up to the furnace roof where they areburnt up at an excess air ratio of 1.0 due to air nozzles arranged in the furnace roof which are designed to supply secondary air.
The products of complete combustion (fuel gases) are partially directed to a zone accommodating the metal bodies being preheated, withthe intention of utilizing the heat of these products. The combustion products then p'assedfrom the furnace to 'recuperators (see, for instance, the GFR Patent N 1 116255).
However inherent in this'procedu're are inevitable difficulties associated with the factthat methane, being a major combustible component of the gasemployed in the above procedure,is-difficult to ignite at an air excess ratio approaching 0.5. This leads to an unstable process of combustion and'leaves excess oxygen in the products of-conibustion amounting'to 1.0 percent, a methane percentage amountingto '4 percent and soot at to-8 g/m". The composition of the'products of combustion and their temperature are not compatible with the latterbeing gradually decreasing with the ensuing cessation of the combustion process.
Attempts to stabilize the combustion process and increase air preheat temperature to 900l ,0O0C are commonly known. However in such cases gas and air are fed to the combustion zone separately which tends to hamper the mixing process and results in incomplete combustion. This also leads to a substantial increase in the overall dimensions of the furnaces.
Also well-known are endeavors to increase the air excess ratio to a value of 0.6-0.65. This can stabilize the combustion process, yet the degree of oxidation of the steel pieces will be 2-4 times as great as that obtained using an air excess ratio amounting to 0.5. I
The main object of the present invention is to stabilize the combustion process using an air excess ratio of 0.5 which assures simultaneously better mixing of air and 'gas.
According to the invention, this is achieved by continuously introducing into a'flow of an air-gas mixture being ignited and burnt with an insufficient amount of air, chemically active gaseous products, such as aldehydes, peroxides, atoms and radicals of combustible gases amounting to 1 percent by volume of the total quantity of the fuel to be burnt, said additions being aimed at stabilizing the ignition process and providefor more complete combustion. Asfor the above-products, they may be the products of combustion of any. combustible gases though preference shall be given to the products'of combustion of the air-gas mixture containing the same constituents as those being burnt in the fumace. It would be expedient to burnthe major part of the fuel at an air excess ratio exceeding thatpeculiar to the process of combustion of the minor fuel part, which simplifies appreciably the process of production of the specified chemically active gaseous products.
It would also be sound practice inproducing chemically active gaseous products to employ a gaseous fuel having a 3 10 percent excessby volume of the total quantity admitted into the furnace. It is expedient to burn the fuel at the air excess ratio ranging within 0.55-0.7 and passing the resultant products of combustion into the flow of the major portionof the fuel (about percent)being burnt at the air'excess ratio of 0.5.
Conforming to the present invention and preferring a plant version comprising a burning device, it would a be sound practice to encompass the exterior of a main 'nozzle of that device with auxiliary nozzles and to provide a chamber for burning a part of the air-gas mixture which communicates with said auxiliary-nozzles. The above arrangement of the nozzles assures highly intensive turbulence of the air-gas mixture admitted into the furnace for combustion. A most compact plant design is assured if the chamber for combustion of the minor part of the fuel is ring-shaped and is arranged at the circumference of the exit nozzle of the-'buming device.
The process of ignition in the chamber for burning the minor portion of the fuel is stabilized by making the chamber inlet in the form of a ring-shaped slot arranged in a-radialsection. It is also expedient to locate an inlet passage for admitting the above mixture into the slot across one of its sides.
In order to simplify the constructiom'it wouldbe sound practice to employ the walls of two circular parts, having an appropriate design, as the walls of the said slot. The parts can be positioned in a cavity employed as a combustion chamber.
As for an igniter for the chamber for burning a part of the air-gas mixture, it is expedient to use a constantacting electro-spark generator. This rules out intermissions which may be hazardous when combustion is carried out with insufficient air.
A substantial advantage of the present invention lies in that the torch temperature remains constant and relatively high at a stable air excess ratio not over 0.5 which can vary, if desired, from 800 to 1250C.
A detailed description of the preferable version of the plant embodiments for accomplishing the foregoing method while conforming to this invention and of the method proper, examples of the plant operation with due reference to the accompanying drawings are given below, wherein:
FIG. 1 is a fragmentary longitudinal sectional view of a plant conforming to the invention;
FIG. 2 is a view along arrow A of FIG. 1.
A plant is fitted with burning device 1 (FlG 1) comprising mixer 2 of a conventional design and coupled to it by bolts 4 is a cone-shaped outlet nozzle 3 referred to hereinafter as a main nozzle. Mixer 2 and main nozzle 3 are fastened on flange 5 by means of dowels (not shown in the drawing). The walls of central bore 6 provided in flange 5 and the external walls of main nozzle 3 are separated by asbestos lining 7. Burning device 1 is secured with the aid of flanges 5 and bolts 8 to disc 9 embedded in the brickwork of heating furnace 10. The places of contact of flange 5 and disc 9 are insulated by asbestos annular linings 11 and 12. The linings are placed at the ends of circular centering bosses 13 and 14 made on disc 9. Accordingly flange 5 is fitted with recesses to receive the above bosses. A ringshaped section between bosses 13 and 14 of disc has annular depression 15. Opposite this depression there is another annular depression 16 in flange 5. Both depressions form cavity 17 acting as a chamber for burning'the minor part of the fuel admitted into the chamber after being mixed with air along sleeve 18 welded to flange 5 and conduits l9 and 20 provided in flange 5 and disc 9 respectively.
Sleeve 18 and each of conduits l9 and 20 have similar cross-sections designed for passing of the total amount of the'fuel supplied to mixer 2. Mounted in cavity 17 are two annular parts 21 and 22 the first of which is located in depression 16 and the second in depression 15. Both parts are fitted with alternating projections and recesses forming an altogether circular V- shaped radial section slot 23 in the intake of chamber 17. Thus, the walls of the foregoing parts, having an appropriate design, serve as the slot walls.
Conduit 20, which is an inlet passage in relation to chamber 17, and one of the sides of slot 23 are perpendicular to each other. The above arrangement of the plant provides for the stabilization of the process of combustion of the air-gas mixture in chamber 17. The latter is located at the circumference of main nozzle 3 and being in communication with auxiliary nozzles 24 (FIGS. 1 and 2) distributed uniformly around main nozzle 3. The nozzles are cylindrical passages provided in disc 9 with their exits being arranged on the walls of central bore 25 having cone-shaped walls made in disc 9 and positioned opposite main nozzle 3 of burning device 1. Section 26 of the passage of main nozzle 3 is cylindrical at the exit with a large cone-shaped base formed by the wall faces of hole 25 in the middle portion of the furnace. The above embodiment of the plant assures favourable conditions for blending the products of combustion emerging from auxiliary nozzles 24 with the flow of the air-gas mixture issuing from main nozzle The upper part of chamber 17 is provided with a constant-acting known electro-spark generator 27 set up on lug '28 welded to flange 5. A tail portion of generator 27 is located in passage 29 running in lug 28, passage 30 in flange 5 and in passage 31, located in annular part 21 with all said passages being coaxial.
The plant is designed to obtain a protective atmosphere in heating furance 10 which serves to heating metal bodies under conditions which prevent the formation of oxides on these bodies in the process of said heating.
Mixer 2 is designedand calculated to form an air-gas mixture, for example, a mixture of natural gas and air, at an air excess ratio of 0.5. From 3 to 10 percent by volume of the fuel, as indicated above, is mixed with air and passed via sleeve 18 and conduit 19 to inlet conduit 20 arranged perpendicularly to, one of the circular V- shaped sides of the radial sectioned slot 23 forming the inlet of chamber 17. Due to the arrangement of conduit 20 and slot 23 as well as the said shape of this slot an intense swirling of the air-gas mixture is obtained at the inlet of the relatively small chamber 17, where the mixture is continuously ignited by generator 27. Chemically active products of incomplete combustion, effected at an air excess ratio of 0.55-0.7 which slightly exceeding that of the air excess ratio used for the burning of the main part of the fuel, are added via additional nozzles 24 to the main flow of the air-gas mixture and passed into the zone of the most intense turbulence contributed by the chemical initiation process upon ignition. Thus, a stable high-temperature torch is produced whose temperature can be altered, if required, within the range of from 800 to 1250C by adjusting the volume of the mixture fed to the burner.
As a result the proposed method assures stable combustion of the overwhelming amount of the air-gas mixture at said air excess ratio of 0.5. This eliminates completely the need for regenerators.
Owing to the stable combustion of the fuel gaseous medium in the furnace free from oxygen and methane and the amount of soot does not exceed 1.5 3 g/m".
The present invention does not, in any way, preclude the possibility of using the products of combustion of any known combustible gases as chemically active gaseous products amounting to not more than 10 percent of the total fuel being burnt for stabilizing the process of ignition. If that is the case the chamber for burning air-gas mixture becomes useless.
What is claimed is 1. A method for producing a protective atmosphere in a heating furnace in which the stabilization of an ignition process providing more complete combustion is accomplished, comprising adding chemically active gaseous products amounting to 10% by volume of the narcissist} ofiii'fiil' bmgisarni aid asses 56m continuously introduced into a flow of an air-gas mixture which is intended to be burned with an insufficient amount of air.
2. The method of claim 1 in which the products of combustion of an air-gas mixture containing the same constituents as that being burnt in said furnace are employed as the said chemically active gaseous products with the first of the said mixtures being burnt at the air excess ratio exceeding that of the second mixture.
3. The method of claim 1 in which gaseous fuel amounting to from 3 to percent by volumeof the total quantity of the fuel supplied to the said furnace is burnt at the air excess ratio of O.550.7 and the products of combustion are passed into the flow'of the remaining part of the fuel.
4. A plant for producing a protective atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air, comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 3-10 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzle; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.
5., The plant of claim 4 in which said chamber for burning the minor part of the fuel is ring-shaped and is arranged at the circumference of the main nozzle outlet nozzle.
6. The plant of claim 4 in which a constant-acting electro-spark generator is employed as the igniter in the said chamber for burning a portion of the fuel.
7. A plant for producing a protective atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air, comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 31 0 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzle, said chamber being provided with an inlet in the form of a circular V-shaped slot in a radial section with an inlet conduit for feeding said mixture into the slot being located across one of its sides; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.
8. The plant of claim 7 wherein two annular parts of appropriate design serve as the walls of said V-shaped slot.

Claims (8)

1. A method for producing a protective atmosphere in a heating furnace in which the stabilization of an ignition process providing more complete combustion is accomplished, comprising adding chemically active gaseous products amounting to 10% by volume of the total quantity of the fuel being burnt, said gasses being continuously introduced into a flow of an air-gas mixture which is intended to be burned with an insufficient amount of air.
2. The method of claim 1 in which the products of combustion of an air-gas mixture containing the same constituents as that being burnt in said furnace are employed as the said chemically active gaseous products with the first of the said mixtures being burnt at the air excess ratio exceeding that of the second mixture.
3. The method of claim 1 in which gaseous fuel amounting to from 3 to 10 percent by volume of the total quantity of the fuel supplied to the said furnace is burnt at the air excess ratio of 0.55-0.7 and the products of combustion are passed into the flow of the remaining part of the fuel.
4. A plant for producing a protective atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air, comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 3-10 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzle; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.
5. The plant of claim 4 in which said chamber for burning the minor part of the fuel is ring-shaped and is arranged at the circumference of the main nozzle outlet nozzle.
6. The plant of claim 4 in which a constant-acting electro-spark generator is employed as the igniter in the said chamber for burning a portion of the fuel.
7. A plant for producing a productive atmosphere in a heating furnace by burning gaseous fuel with an insufficient amount of combustion air, comprising at least one mixer for blending the gaseous fuel with air, pipe lines means for feeding the said fuel and air to the said mixer, a main nozzle in communication with the said mixer on one side and with the said heating furnace on the other, a chamber for burning the minor part of the said gaseous fuel amounting to 3-10 percent by volume of the total amount of the fuel admitted to be burnt in said heating furnace via the said main nozzles, said chamber being provided with an inlet in the form of a circular V-shaped slot in a radial section with an inlet conduit for feeding said mixture into the slot being located across one of its sides; auxiliary nozzles arranged around said main nozzle and communicating on one side with said chamber with the said heating furnace on the other side.
8. The plant of claim 7 wherein two annular parts of appropriate design serve as the walls of said V-shaped slot.
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0046898A1 (en) * 1980-08-18 1982-03-10 Nauchno-Proizvodstvennoe Obiedinenie Po Tekhnologii Mashinostroenia "Tsniitmash" Method and apparatus for pulse-burning of fuel gases in industrial furnaces, particularly metallurgical furnaces
US4416615A (en) * 1981-02-17 1983-11-22 Ketchum Jr Elmer Fuel burner construction
WO2004085801A1 (en) * 2003-03-26 2004-10-07 Ashot Armenovich Madoyan Power supply unit
US20060131442A1 (en) * 2004-12-22 2006-06-22 Norman Ivans Irrigation unit including a nozzle greater accuracy and improved adjustment properties
US20070235002A1 (en) * 2006-04-07 2007-10-11 Blank David Alan Combustion control via homogeneous combustion radical ignition (hcri) or partial hcri in cyclic ic engines
US20080206697A1 (en) * 2005-07-29 2008-08-28 Christophe Trochou Gas Burner With Multiple Concetric Flame Rings
US20110232589A1 (en) * 2006-04-07 2011-09-29 Blank David A Combustion control via homogeneous combustion radical ignition (hcri) or partial hcri in cyclic ic engines
US8567369B2 (en) 2010-11-11 2013-10-29 Cameron International Corporation Spark ignited radical injection system
US8844498B2 (en) 2010-11-11 2014-09-30 Ge Oil & Gas Compression Systems, Llc Positive displacement radical injection system
US8857405B2 (en) 2010-11-01 2014-10-14 Mahle Powertrain, Llc Turbulent jet ignition pre-chamber combustion system for spark ignition engines
US9353674B2 (en) 2010-11-01 2016-05-31 Mahle Powertrain, Llc Turbulent jet ignition pre-chamber combustion system for spark ignition engines

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4473348A (en) * 1980-08-18 1984-09-25 Nauchno-Proizvodstvennoe Obiedinenie Po Tekhnologii Mashinostroenia "Tsniitmash" Method for pulse-burning fuel gases in industrial furnaces
EP0046898A1 (en) * 1980-08-18 1982-03-10 Nauchno-Proizvodstvennoe Obiedinenie Po Tekhnologii Mashinostroenia "Tsniitmash" Method and apparatus for pulse-burning of fuel gases in industrial furnaces, particularly metallurgical furnaces
US4416615A (en) * 1981-02-17 1983-11-22 Ketchum Jr Elmer Fuel burner construction
WO2004085801A1 (en) * 2003-03-26 2004-10-07 Ashot Armenovich Madoyan Power supply unit
US20060131442A1 (en) * 2004-12-22 2006-06-22 Norman Ivans Irrigation unit including a nozzle greater accuracy and improved adjustment properties
US7901205B2 (en) * 2005-07-29 2011-03-08 Burner Systems International (Bsi) Gas burner with multiple concentric flame rings
US20080206697A1 (en) * 2005-07-29 2008-08-28 Christophe Trochou Gas Burner With Multiple Concetric Flame Rings
US20110232589A1 (en) * 2006-04-07 2011-09-29 Blank David A Combustion control via homogeneous combustion radical ignition (hcri) or partial hcri in cyclic ic engines
US7832372B2 (en) 2006-04-07 2010-11-16 Hcri Technologies International, Llc Combustion control via homogeneous combustion radical ignition (HCRI) or partial HCRI in cyclic IC engines
US7493886B2 (en) 2006-04-07 2009-02-24 Blank David Alan Combustion control via homogeneous combustion radical ignition (HCRI) or partial HCRI in cyclic IC engines
US20070235002A1 (en) * 2006-04-07 2007-10-11 Blank David Alan Combustion control via homogeneous combustion radical ignition (hcri) or partial hcri in cyclic ic engines
US9010293B2 (en) 2006-04-07 2015-04-21 David A. Blank Combustion control via homogeneous combustion radical ignition (HCRI) or partial HCRI in cyclic IC engines
US9638093B2 (en) 2006-04-07 2017-05-02 Hcri Technologies International, Llc Combustion control via homogeneous combustion radical ignition (HCRI) or partial HCRI in cyclic IC engines
US8857405B2 (en) 2010-11-01 2014-10-14 Mahle Powertrain, Llc Turbulent jet ignition pre-chamber combustion system for spark ignition engines
US9353674B2 (en) 2010-11-01 2016-05-31 Mahle Powertrain, Llc Turbulent jet ignition pre-chamber combustion system for spark ignition engines
US8567369B2 (en) 2010-11-11 2013-10-29 Cameron International Corporation Spark ignited radical injection system
US8844498B2 (en) 2010-11-11 2014-09-30 Ge Oil & Gas Compression Systems, Llc Positive displacement radical injection system
US8875678B2 (en) 2010-11-11 2014-11-04 Ge Oil & Gas Compression Systems, Llc Spark ignited radical injection system
US20140331965A1 (en) * 2010-11-11 2014-11-13 Cameron International Corporation Positive displacement radical injection system
US9631591B2 (en) * 2010-11-11 2017-04-25 Ge Oil & Gas Compression Systems, Llc Positive displacement radical injection system

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