[go: up one dir, main page]

US3589845A - Power burner - Google Patents

Power burner Download PDF

Info

Publication number
US3589845A
US3589845A US818727A US3589845DA US3589845A US 3589845 A US3589845 A US 3589845A US 818727 A US818727 A US 818727A US 3589845D A US3589845D A US 3589845DA US 3589845 A US3589845 A US 3589845A
Authority
US
United States
Prior art keywords
plate
tubular member
air
burner
gas
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
US818727A
Inventor
James A Morse
Donald A Dray
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.)
Adams Manufacturing Corp
Original Assignee
Adams Manufacturing Corp
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 Adams Manufacturing Corp filed Critical Adams Manufacturing Corp
Application granted granted Critical
Publication of US3589845A publication Critical patent/US3589845A/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
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • 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
    • F23D14/34Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air

Definitions

  • ABSTRACT A power gas burner 18 provided having a per- [52] US. Cl. 431/10, f m d p
  • a gas burner having a deflector plate against which air flowing through a blast tube impinges, and through perforations of which the major portion of the air delivered by the blast tube passes forwardly through a mixing chamber in a streamline flow confined by a sheath of gas emanating from holes in a retention plate.
  • This air constitutes what is referred to as the secondary air supply and remains largely unmixed with the gas for a considerable distance forwardly of the deflector plate.
  • the deflector plate also forms a sufficient restriction to the flow of air therethrough that it builds up a slight static pressure in the blast tube behind the deflector plate, with the result that a minor proportion of the air, instead of passing through the perforations of the deflector plate with a streamline flow, is deflected laterally outwardly past the edges of the deflector plate, and is thereby caused to impinge against jets of gas emerging from holes in the retention plate and to intermix therewith.
  • This deflected air constitutes what is referred to as the primary air supply," mixing thereof with the gas occurring during the time the air and gas traverse the axial length of what is termed an extension tube, which forms a mixing chamber.
  • the deflector plate forms a restriction to the flow of air therethrough to an extent such that a slight static pressure in the blast tube behind the deflector plate is built up, it follows that only a slight vacuum is produced by the air flowing through the deflector plate, which vacuum is insufficient to hold the fire or flame tightly against the forward face of the deflector plate, and thereby avoid pulsation of the flame.
  • the gas in the Misner patent, flows in a direction parallel with the direction of airflow, so that complete and thorough mixing of the gas and air, and particularly of the gas with the secondary air, is not possible. There is, in fact, a mixing with or aeration of only a small portion of the gas by the primary air, similar to what is normally obtainable by a venturi effect.
  • the present invention has, as its primary object, the provision of a gas burner which overcomes all of the aforesaid disadvantages, and in which the gas and air are mixed as completely as possible before the air from the blast tube passes appreciably beyond the perforated plate, so that combustion is virtually completed before the combustible mixture reaches the end of the extension tube or nozzle of the burner.
  • Another object of the invention is to'provide a burner of the character described, in which a very short flame is maintained against the forward face of the plate, which flame is free from lifting and pulsation.
  • a further object of the invention is to provide a burner of the character described, in which a mantle of air is maintained 'between the extension tube or nozzle of the burner and the periphery of the flame, to thereby blanket the inside of the tube or noule and avoid corrosion or blistering thereof.
  • a further object of the invention is to provide a burner of the character described, in which the air which passes through the perforated plate at a high velocity such as to produce a partial vacuum on the plate which holds the gas-air mixture back against the plate, so that thorough mixing takes place inside the surrounding air mantle.
  • a still further object of the invention is to provide a burner of the character described, in which the gas is introduced into the burner at right angles to the direction of airflow, in controlled amounts, such as to produce a complete and homogeneous combustible mixture of the gas and air adjacent the plate.
  • FIG. 1 is a longitudinal cross-sectional view of the power burner, taken on the line 1-1 of FIG. 2, and
  • FlG. 2 is a transverse cross-sectional view, taken on the line 22 of H6. 1.
  • the burner will be seen to comprise a tubular member or hood 1, preferably made of steel, having a conical inturned flange 2 at its forward end, which comprises the nozzle of the burner.
  • a plate 3 Disposed within the forward portion of the tubular member 1, rearwardly of the junction of the member I with its flange 2, is a plate 3, of generally circular configuration, made of stainless steel, which extends diametrically across the tubular member 1, and has peripheral portions thereof removed to provide circumferentially spaced arcuate openings 4 and5, which serve a purpose to be presently described.
  • the plate 3 is also provided with a multiplicity of spaced holes or openings 8 which serve a purpose to be presently described.
  • the plate is' provided below its center or axis with an enlarged opening 9, within which is mounted the forward end of a pilot assembly 10, to which gas is supplied, as by a gas line 11. Noteworthy at this point is the fact that virtually the entire pilot assembly is disposed rearwardly of the plate 3.
  • the plate 3 is also provided at diametrically opposite points adjacent the top and bottom of the plate with recesses or openings 12 and 13, within which are mounted gas jet nozzles 14 and 15, respectively, which may be welded to the plate.
  • These gas jet nozzles have axes parallel with the axis of the plate 3, and extend from a point spaced rearwardly of the plate 3 to a point spaced forwardly of the plate but at a relatively short distance from the plate, as compared with the entire distance from the plate to the forward edge of the flange 2.
  • the nozzles 14 and 15 are closed at the front and open at the rear.
  • the nozzle 14 is provided in its side wall with axially aligned orifices 16 and 17 and in its bottom with an orifice 18, the axis of which is perpendicular to the common axis of the orifices 16 and 17.
  • the nozzle 15 is provided in its side wall with axially aligned orifices 19 and 20.
  • the axes of the orifices 16, 17, 18, 19 and 20 lie in a common plane parallel to the plane of the plate 3 and disposed in closely spaced relation to the front face of the plate 3 forwardly of'the latter.
  • the nozzles 14 and 15 are coupled to gas supply pipes or lines 21, as by means of couplings 22.
  • the pipes 21 and couplings 22 are coaxial with their respective gas jets.
  • the operation or use of the burner may be described as folopenings 8 of the plate 3, and a lesser portion of the air passing through the arcuate openings 4 and 5 to provide a mantle of air which blankets the inner wall of the member 1 and flange 2.
  • the gas introduced into the gas jet nozzles 14 and 15 is blown across the front of the plate 3 through the orifices l6, l7, l8, l9 and 20.
  • This gas mixes with the air which passes through the holes or openings 8 to form a combustible mixture which is ignited by the pilot assembly 10.
  • the air issuing from the holes or openings 8 is moving at a high velocity, producing a partial vacuum on the plate 3, which holds the air and gas back against the plate, so that thorough mixing of the air and gas takes place in a narrow zone immediately forwardly of the plate 3, and inside of the surrounding air mantle or blanket provided by the air issuing from the openings 4 and 5. This produces a short hard fire free of lifting and pulsation.
  • the burner as described, is free from all of the disadvantages described with reference to the Misner patent, and is characterized by the fact that the gas and major portion of the air are mixed as completely, as possible before the air introduced into the tubular member 1 passes appreciably beyond the plate 3, so that combustion is virtually completed before the combustible mixture reaches the end of the member 1.
  • the flame is a very short and intense flame, which is maintained against the forward or front face of the plate 3, so that it is virtually free from lifting and pulsation, burning very quietly.
  • a mantle or blanket of air, substantially free of gas, is maintained between the inner wall of the member 1 and the periphery of the flame, to thereby insulate the flame from the member 1 and avoid corrosion or blistering thereof.
  • the gas is introduced into the burner at right angles to the direction of the airflow, in controlled amounts such as to produce a complete and homogeneous combustible mixture of the gas and air adjacent the front face of the plate.
  • the pilot assembly and associated parts, being disposed rearwardly of the plate 3 are shielded or guarded against oxidation or corrosion produced by the burner flame, and the vacuum or partial vacuum produced by the combustion air is effective to prevent ingress of the burner flame into the pilot assembly, thereby protecting the pilot assembly from the effects of the flame.
  • a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means for introducing gas through said plate at points adjacent the periphery of said plate, and means for directing said gas into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said last-named means including tubular gas jet nozzles extending through said plate and having orifices in the said sidewalls thereof, said plate having peripheral portions thereof removed to provide arcuate openings or passageways adjacent the inner wall of said tubular member, so that a portion of the air passing through said tubular member passes through said passageways to provide a blanket or mantle of air which encompasses the periphery
  • a burner as defined in claim 1, wherein said gas jet nozzles are closed at their forward ends.
  • a burner as defined in claim 2, wherein said tubular member is provided at its forward end with an inwardly directed conical flange, which is effective to cause said blanketing air to be directed inwardly adjacent the forward end of said member.
  • a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having perforations for the passage of air therethrough, means for introducing a fuel gas through said plate, said means comprising at least two spaced conduits disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, said conduits being diametrically opposed and at the outer periphery of said plate and having at least a pair of oppositely directed ports in the walls thereof forwardly of said plate for directing said fuel gas from said conduits and into said air in a direction substantially perpendicular to the direction of airflow, and generally away from direct impingement against the inner wall of the tubular member in the vicinity of said conduits and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame across the face of said plate
  • the method of operating a burner comprising a tubular member, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member and having perforations therein, and at least two spaced conduits extending through said plate and disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, and having ports in the wall thereof forwardly of said plate, said method comprising the steps of directing air through said plate from behind said plate and through said perforation, further directing a fuel gas through said conduits and out of said ports in at least two diametrically spaced points and into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate and generally away from the periphery of said plate in the vicinity of said conduits, whereby to provide a combustible mixture which produces a short flame.
  • a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means adjacent the periphery of said plate for introducing gas through said plate and for directing said gas into said air in a direction substantially perpendicular to the direction of the airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said burner having elongated passageways or openings between the periphery of said plate and the inner wall of said tubular member, for the passage of a portion of the air passing through said tubular member to provide a blanket or mantle of air which encompasses the periphery of said flame and is effective to prevent oxidation or corrosion of said tubular member.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

A power gas burner is provided having a perforated plate through which air passes and is mixed with gas introduced into the burner at right angles to the direction of airflow and immediately in front of the plate, to provide a combustible mixture which burns with a short, intense, flame, free from lifting and pulsation. A mantle of gas-free air surrounds the flame to avoid corrosion of parts of the burner. The air for combustion passes through the plate at a high velocity such as to create a partial vacuum at the front of the plate, which is effective to maintain the flame against the plate.

Description

0 United States Patent in] 9,
{72] lnvcntors James A. Morse 1,549,390 8/1925 Smith 431/354 X Cleveland Heights; 1,588,792 6/1926 Dodge l 1 4 431/353 X Donald A. Dray. Parma, both of, Ohio 1,644,505 10/1927 Beckett 239/426 [211 Appl. No. 818,727 2,804,919 9/1957 Kinnison 239/431 X [22] Filed Apr. 23, 1969 3,180,394 4/1965 Conway 431/353 X [45] Patented June 29, 1971 mary Examiner-Carroll B. Donty, Jr. [73] Assignee The Adams Manufacturing Company Cleveland Ohio Attorney lsler and Omstein [54] POWER BURNER 7Clai 2 D w F m n mg .88 ABSTRACT: A power gas burner 18 provided having a per- [52] US. Cl. 431/10, f m d p|ate through which air passes and is mixed with gas 431/263 431/285 431/353, 239/426 239/431 introduced into the burner at right angles-to the direction of [51] Int. CL 1.1.; F23m 3/04 i fl and immediate), in from of the plate to provide a [50] Fleld 01 Search 431/349, combustible mixture which bums with a short, imehse flame 3, 10; 239/426, 431 free from lifting and pulsation. A mantle of gas-free air sur- 56 R f CM rounds the flame to avoid corrosion of parts of the burner. The I 1 e erenccs I air for combustion passes through the plate at a high velocity UNITED STATES PATENTS 1,941,163 12/1933 Carver such as to create a partial vacuum at the front of the plate, which is effective to maintain the flame against the plate.
Muir/mas JAMES A. MORSE BY DONALD A. DRAY Mimi ATTORN EY S PATENTEU JUN29 :sn
Fig. 2
POWER BURNER ln Misner US. Pat. No. 3,330,485, a gas burner is disclosed having a deflector plate against which air flowing through a blast tube impinges, and through perforations of which the major portion of the air delivered by the blast tube passes forwardly through a mixing chamber in a streamline flow confined by a sheath of gas emanating from holes in a retention plate. This air constitutes what is referred to as the secondary air supply and remains largely unmixed with the gas for a considerable distance forwardly of the deflector plate.
The deflector plate also forms a sufficient restriction to the flow of air therethrough that it builds up a slight static pressure in the blast tube behind the deflector plate, with the result that a minor proportion of the air, instead of passing through the perforations of the deflector plate with a streamline flow, is deflected laterally outwardly past the edges of the deflector plate, and is thereby caused to impinge against jets of gas emerging from holes in the retention plate and to intermix therewith. This deflected air constitutes what is referred to as the primary air supply," mixing thereof with the gas occurring during the time the air and gas traverse the axial length of what is termed an extension tube, which forms a mixing chamber.
Although the aforesaid burner design is stated in the patent to cause the flame to burn quietly from the exit face of the extension tube, without pulsating or popping, we have found that the burner flame does, in fact, pulsate, and does not burn efficiently as stated. The reasons for this may be enumerated as follows:
1. Since the secondary air supply remains, as stated, largely unmixed with the gas for a considerable distance forwardly of the deflector plate, the flame burns at the exit end or face of the extension tube, but the distance or space between such flame and the deflector plate is, in fact, so great that the flame is a substantially long flame, which completely fills this space. With a flame of such length, considerable pulsating occurs, and moreover, this flame also causes combustion of the mixture of primary air and gas, causing the extension tube to become excessively heated and to a point at which corrosion of blistering of the tube occur. At the same time, portions of the pilot burner assembly within this space become corroded or otherwise damaged.
2. Since, as stated, the deflector plate forms a restriction to the flow of air therethrough to an extent such that a slight static pressure in the blast tube behind the deflector plate is built up, it follows that only a slight vacuum is produced by the air flowing through the deflector plate, which vacuum is insufficient to hold the fire or flame tightly against the forward face of the deflector plate, and thereby avoid pulsation of the flame.
3. The gas, in the Misner patent, flows in a direction parallel with the direction of airflow, so that complete and thorough mixing of the gas and air, and particularly of the gas with the secondary air, is not possible. There is, in fact, a mixing with or aeration of only a small portion of the gas by the primary air, similar to what is normally obtainable by a venturi effect.
The present invention has, as its primary object, the provision of a gas burner which overcomes all of the aforesaid disadvantages, and in which the gas and air are mixed as completely as possible before the air from the blast tube passes appreciably beyond the perforated plate, so that combustion is virtually completed before the combustible mixture reaches the end of the extension tube or nozzle of the burner.
Another object of the invention is to'provide a burner of the character described, in which a very short flame is maintained against the forward face of the plate, which flame is free from lifting and pulsation.
A further object of the invention is to provide a burner of the character described, in which a mantle of air is maintained 'between the extension tube or nozzle of the burner and the periphery of the flame, to thereby blanket the inside of the tube or noule and avoid corrosion or blistering thereof.
A further object of the invention is to provide a burner of the character described, in which the air which passes through the perforated plate at a high velocity such as to produce a partial vacuum on the plate which holds the gas-air mixture back against the plate, so that thorough mixing takes place inside the surrounding air mantle.
A still further object of the invention is to provide a burner of the character described, in which the gas is introduced into the burner at right angles to the direction of airflow, in controlled amounts, such as to produce a complete and homogeneous combustible mixture of the gas and air adjacent the plate.
Other objects and advantages of our invention will be apparent during the course of the following description.
ln the accompanying drawing, forming a part of this specification, and in which like numerals are employed to designate like parts throughout the same,
FIG. 1 is a longitudinal cross-sectional view of the power burner, taken on the line 1-1 of FIG. 2, and
FlG. 2 is a transverse cross-sectional view, taken on the line 22 of H6. 1. v Referring more particularly to the drawing, the burner will be seen to comprise a tubular member or hood 1, preferably made of steel, having a conical inturned flange 2 at its forward end, which comprises the nozzle of the burner.
Disposed within the forward portion of the tubular member 1, rearwardly of the junction of the member I with its flange 2, is a plate 3, of generally circular configuration, made of stainless steel, which extends diametrically across the tubular member 1, and has peripheral portions thereof removed to provide circumferentially spaced arcuate openings 4 and5, which serve a purpose to be presently described.
Removal of these peripheral portions of the plate 3 leaves circumferentially spaced tongues 6 and 7 which may be welded to the inner wall of the memberv 1 to maintain the plate 3 in position.
The plate 3 is also provided with a multiplicity of spaced holes or openings 8 which serve a purpose to be presently described. The plate is' provided below its center or axis with an enlarged opening 9, within which is mounted the forward end of a pilot assembly 10, to which gas is supplied, as by a gas line 11. Noteworthy at this point is the fact that virtually the entire pilot assembly is disposed rearwardly of the plate 3.
The plate 3 is also provided at diametrically opposite points adjacent the top and bottom of the plate with recesses or openings 12 and 13, within which are mounted gas jet nozzles 14 and 15, respectively, which may be welded to the plate. These gas jet nozzles have axes parallel with the axis of the plate 3, and extend from a point spaced rearwardly of the plate 3 to a point spaced forwardly of the plate but at a relatively short distance from the plate, as compared with the entire distance from the plate to the forward edge of the flange 2. The nozzles 14 and 15 are closed at the front and open at the rear.
The nozzle 14 is provided in its side wall with axially aligned orifices 16 and 17 and in its bottom with an orifice 18, the axis of which is perpendicular to the common axis of the orifices 16 and 17.
The nozzle 15 is provided in its side wall with axially aligned orifices 19 and 20.
The axes of the orifices 16, 17, 18, 19 and 20 lie in a common plane parallel to the plane of the plate 3 and disposed in closely spaced relation to the front face of the plate 3 forwardly of'the latter.
The nozzles 14 and 15 are coupled to gas supply pipes or lines 21, as by means of couplings 22. The pipes 21 and couplings 22 are coaxial with their respective gas jets.
The operation or use of the burner may be described as folopenings 8 of the plate 3, and a lesser portion of the air passing through the arcuate openings 4 and 5 to provide a mantle of air which blankets the inner wall of the member 1 and flange 2.
At the same time, the gas introduced into the gas jet nozzles 14 and 15 is blown across the front of the plate 3 through the orifices l6, l7, l8, l9 and 20. This gas mixes with the air which passes through the holes or openings 8 to form a combustible mixture which is ignited by the pilot assembly 10. The air issuing from the holes or openings 8 is moving at a high velocity, producing a partial vacuum on the plate 3, which holds the air and gas back against the plate, so that thorough mixing of the air and gas takes place in a narrow zone immediately forwardly of the plate 3, and inside of the surrounding air mantle or blanket provided by the air issuing from the openings 4 and 5. This produces a short hard fire free of lifting and pulsation.
The burner, as described, is free from all of the disadvantages described with reference to the Misner patent, and is characterized by the fact that the gas and major portion of the air are mixed as completely, as possible before the air introduced into the tubular member 1 passes appreciably beyond the plate 3, so that combustion is virtually completed before the combustible mixture reaches the end of the member 1.
The flame is a very short and intense flame, which is maintained against the forward or front face of the plate 3, so that it is virtually free from lifting and pulsation, burning very quietly.
A mantle or blanket of air, substantially free of gas, is maintained between the inner wall of the member 1 and the periphery of the flame, to thereby insulate the flame from the member 1 and avoid corrosion or blistering thereof.
The gas is introduced into the burner at right angles to the direction of the airflow, in controlled amounts such as to produce a complete and homogeneous combustible mixture of the gas and air adjacent the front face of the plate. I
The pilot assembly and associated parts, being disposed rearwardly of the plate 3 are shielded or guarded against oxidation or corrosion produced by the burner flame, and the vacuum or partial vacuum produced by the combustion air is effective to prevent ingress of the burner flame into the pilot assembly, thereby protecting the pilot assembly from the effects of the flame.
It is to be understood that the form of our invention, herewith shown and described, is to be taken as a preferred example of the same, and that various changes may be made in the shape, size and arrangement of parts thereof, without departing from the spirit of the invention or the scope of the subjoined claims.
We claim:
1. In a burner of the character described, a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means for introducing gas through said plate at points adjacent the periphery of said plate, and means for directing said gas into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said last-named means including tubular gas jet nozzles extending through said plate and having orifices in the said sidewalls thereof, said plate having peripheral portions thereof removed to provide arcuate openings or passageways adjacent the inner wall of said tubular member, so that a portion of the air passing through said tubular member passes through said passageways to provide a blanket or mantle of air which encompasses the periphery of said flame and is effective to prevent oxidation or corrosion of said tubular member.
2. A burner, as defined in claim 1, wherein said gas jet nozzles are closed at their forward ends.
3. A burner, as defined in claim 2, wherein said tubular member is provided at its forward end with an inwardly directed conical flange, which is effective to cause said blanketing air to be directed inwardly adjacent the forward end of said member.
4. in a burner of the character described, a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having perforations for the passage of air therethrough, means for introducing a fuel gas through said plate, said means comprising at least two spaced conduits disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, said conduits being diametrically opposed and at the outer periphery of said plate and having at least a pair of oppositely directed ports in the walls thereof forwardly of said plate for directing said fuel gas from said conduits and into said air in a direction substantially perpendicular to the direction of airflow, and generally away from direct impingement against the inner wall of the tubular member in the vicinity of said conduits and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame across the face of said plate and substantially free of pulsation.
5. The method of operating a burner comprising a tubular member, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member and having perforations therein, and at least two spaced conduits extending through said plate and disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, and having ports in the wall thereof forwardly of said plate, said method comprising the steps of directing air through said plate from behind said plate and through said perforation, further directing a fuel gas through said conduits and out of said ports in at least two diametrically spaced points and into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate and generally away from the periphery of said plate in the vicinity of said conduits, whereby to provide a combustible mixture which produces a short flame.
6. In a burner of the character described, a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means adjacent the periphery of said plate for introducing gas through said plate and for directing said gas into said air in a direction substantially perpendicular to the direction of the airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said burner having elongated passageways or openings between the periphery of said plate and the inner wall of said tubular member, for the passage of a portion of the air passing through said tubular member to provide a blanket or mantle of air which encompasses the periphery of said flame and is effective to prevent oxidation or corrosion of said tubular member.
7. The method of operating a burner as defined in claim 5 including the further step of passing a portion of the air adjacent the inner wall of said tubular member in the form of a blanket or mantle of air which encompasses the periphery of the flame to prevent oxidation and corrosion of said tubular member.

Claims (7)

1. In a burner of the character described, a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means for introducing gas through said plate at points adjacent the periphery of said plate, and means for directing said gas into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said last-named means including tubular gas jet nozzles extending through said plate and having orifices in the said sidewalls thereof, said plate having peripheral portions thereof removed to provide arcuate openings or passageways adjacent the inner wall of said tubular member, so that a portion of the air passing through said tubular member passes through said passageways to provide a blanket or mantle of air which encompasses the periphery of said flame and is effective to prevent oxidation or corrosion of said tubular member.
2. A burner, as defined in claim 1, wherein said gas jet nozzles are closed at their forward ends.
3. A burner, as defined in claim 2, wherein said tubular member is provided at its forward end with an inwardly directed conical flange, which is effective to cause said blanketing air to be directed inwardly adjacent the forward end of said member.
4. In a burner of the character described, a tubular member for passage of air under pressure, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having perforations for the passage of air therethrough, means for introducing a fuel gas through said plate, said means comprising at least two spaced conduits disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, said conduits being diametrically opposed and at the outer periphery of said plate and having at least a pair of oppositely directed ports in the walls thereof forwardly of said plate for directing said fuel gas from said conduits and into said air in a direction substantially perpendicular to the direction of airflow, and generally away from direct impingement against the inner wall of the tubular member in the vicinity of said conduits and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame across the face of said plate and substantially free of pulsation.
5. The method of operating a burner comprising a tubular member, a plate extending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member and having perforations therein, and at least two spaced conduits extending through said plate and disposed closely adjacent the inner wall of said tubular member and having their axes substantially parallel with the axis of said tubular member, and having ports in the wall thereof forwardly of said plate, said method comprising the steps of directing air through said plate from behind said plate and through said perforation, further directing a fuel gas through said conduits and out of said ports in at least two diametrically spaced points and into said air in a direction substantially perpendicular to the direction of airflow and in a plane closely adjacent and parallel to the forward face of said plate and generally away from the periphery of said plate in the vicinity of said conduits, whereby to provide a combustible mixture which produces a short flame.
6. In a burner of the character described, a tubular member for passage of air under pressure, a plate exTending diametrically across said tubular member at a point spaced rearwardly from the forward end of said member, said plate having spaced perforations for the passage of air therethrough, means adjacent the periphery of said plate for introducing gas through said plate and for directing said gas into said air in a direction substantially perpendicular to the direction of the airflow and in a plane closely adjacent and parallel to the forward face of said plate, to provide a combustible mixture which produces a short flame, substantially free of pulsation, said burner having elongated passageways or openings between the periphery of said plate and the inner wall of said tubular member, for the passage of a portion of the air passing through said tubular member to provide a blanket or mantle of air which encompasses the periphery of said flame and is effective to prevent oxidation or corrosion of said tubular member.
7. The method of operating a burner as defined in claim 5 including the further step of passing a portion of the air adjacent the inner wall of said tubular member in the form of a blanket or mantle of air which encompasses the periphery of the flame to prevent oxidation and corrosion of said tubular member.
US818727A 1969-04-23 1969-04-23 Power burner Expired - Lifetime US3589845A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US81872769A 1969-04-23 1969-04-23

Publications (1)

Publication Number Publication Date
US3589845A true US3589845A (en) 1971-06-29

Family

ID=25226262

Family Applications (1)

Application Number Title Priority Date Filing Date
US818727A Expired - Lifetime US3589845A (en) 1969-04-23 1969-04-23 Power burner

Country Status (1)

Country Link
US (1) US3589845A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1980002451A1 (en) * 1979-05-08 1980-11-13 R Babington Improvements in liquid fuel burners
US4373896A (en) * 1978-10-31 1983-02-15 Zwick Eugene B Burner construction
US4892475A (en) * 1988-12-08 1990-01-09 Union Carbide Corporation Ignition system and method for post-mixed burner
EP0347834A3 (en) * 1988-06-21 1991-07-24 Walter Dreizler Burner head for a forced-draft gas burner
EP0511878A3 (en) * 1991-05-01 1993-03-17 Callidus Technologies Inc. Low nox burner assemblies
WO1994025800A1 (en) * 1993-04-26 1994-11-10 Werner Bachmann Device for burning combustible gas residues
NL9300934A (en) * 1993-06-01 1995-01-02 Ingbureaugoedkoop B V Burner head
US5460515A (en) * 1991-11-22 1995-10-24 Aichelin Gmbh Burner for an industrial furnace
US5984665A (en) * 1998-02-09 1999-11-16 Gas Research Institute Low emissions surface combustion pilot and flame holder
US5993193A (en) * 1998-02-09 1999-11-30 Gas Research, Inc. Variable heat flux low emissions burner
US6007325A (en) * 1998-02-09 1999-12-28 Gas Research Institute Ultra low emissions burner
US6062848A (en) * 1998-05-29 2000-05-16 Coen Company, Inc. Vibration-resistant low NOx burner
US6322353B1 (en) * 1998-10-05 2001-11-27 Asea Brown Boveri Ag Ignition appliance for a heat generator
US20140000263A1 (en) * 2009-05-20 2014-01-02 General Electric Company Multi-premixer fuel nozzle support system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1549390A (en) * 1924-03-26 1925-08-11 Edison M Smith Oil burner
US1588792A (en) * 1925-08-29 1926-06-15 Harry H Dodge Gas burner
US1644505A (en) * 1926-03-29 1927-10-04 Beckett William Austin Gas burner
US1941163A (en) * 1932-10-10 1933-12-26 Donald C Carver Automatic gas valve
US2804919A (en) * 1949-07-20 1957-09-03 Kinnison John Emmett Volumetric combustion method and apparatus
US3180394A (en) * 1955-04-26 1965-04-27 Bloom Eng Co Inc Gas burner

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1549390A (en) * 1924-03-26 1925-08-11 Edison M Smith Oil burner
US1588792A (en) * 1925-08-29 1926-06-15 Harry H Dodge Gas burner
US1644505A (en) * 1926-03-29 1927-10-04 Beckett William Austin Gas burner
US1941163A (en) * 1932-10-10 1933-12-26 Donald C Carver Automatic gas valve
US2804919A (en) * 1949-07-20 1957-09-03 Kinnison John Emmett Volumetric combustion method and apparatus
US3180394A (en) * 1955-04-26 1965-04-27 Bloom Eng Co Inc Gas burner

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298338A (en) * 1976-12-30 1981-11-03 Owens-Illinois, Inc. Liquid fuel burners
US4373896A (en) * 1978-10-31 1983-02-15 Zwick Eugene B Burner construction
WO1980002451A1 (en) * 1979-05-08 1980-11-13 R Babington Improvements in liquid fuel burners
EP0347834A3 (en) * 1988-06-21 1991-07-24 Walter Dreizler Burner head for a forced-draft gas burner
US4892475A (en) * 1988-12-08 1990-01-09 Union Carbide Corporation Ignition system and method for post-mixed burner
EP0511878A3 (en) * 1991-05-01 1993-03-17 Callidus Technologies Inc. Low nox burner assemblies
US5460515A (en) * 1991-11-22 1995-10-24 Aichelin Gmbh Burner for an industrial furnace
WO1994025800A1 (en) * 1993-04-26 1994-11-10 Werner Bachmann Device for burning combustible gas residues
NL9300934A (en) * 1993-06-01 1995-01-02 Ingbureaugoedkoop B V Burner head
US5984665A (en) * 1998-02-09 1999-11-16 Gas Research Institute Low emissions surface combustion pilot and flame holder
US5993193A (en) * 1998-02-09 1999-11-30 Gas Research, Inc. Variable heat flux low emissions burner
US6007325A (en) * 1998-02-09 1999-12-28 Gas Research Institute Ultra low emissions burner
US6062848A (en) * 1998-05-29 2000-05-16 Coen Company, Inc. Vibration-resistant low NOx burner
US6322353B1 (en) * 1998-10-05 2001-11-27 Asea Brown Boveri Ag Ignition appliance for a heat generator
US20140000263A1 (en) * 2009-05-20 2014-01-02 General Electric Company Multi-premixer fuel nozzle support system
US8769956B2 (en) * 2009-05-20 2014-07-08 General Electric Company Multi-premixer fuel nozzle support system

Similar Documents

Publication Publication Date Title
US3589845A (en) Power burner
US2701608A (en) Burner
US4575332A (en) Method of and burner for burning liquid or gaseous fuels with decreased NOx formation
US3275057A (en) Tunnel burners
US2219696A (en) Art of combustion
US2044296A (en) Burner
US2773350A (en) Combustion chamber assembly for ram jet fuel burner
US4125360A (en) Steam atomizing burner
US4211073A (en) Combustion chamber principally for a gas turbine
US1987972A (en) Decoking lance
US3529917A (en) Air-mixing device for fuel burner
US1956857A (en) Gas burner
JPS63220015A (en) Igniter for cold-state nozzle type high-speed burner and burner using said device
CA1183767A (en) Forced draft radiant wall fuel burner
US3737281A (en) Fuel mixing shroud for heating torches
US3160401A (en) Space heater with flame spreader
US1788716A (en) Gas burner
US4023923A (en) Burner for heating an airstream
US3977186A (en) Impinging air jet combustion apparatus
US3545908A (en) Gas burner
JPH0237206A (en) Burner
US3644077A (en) Flame stabilizing system for power gas burners
US5102329A (en) High intensity burner
US3226038A (en) Combustor for a steam generator
US3625495A (en) Gas burner