US3365136A - Burner for tempered flame operation - Google Patents

Burner for tempered flame operation Download PDF

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Publication number
US3365136A
US3365136A US460094A US46009465A US3365136A US 3365136 A US3365136 A US 3365136A US 460094 A US460094 A US 460094A US 46009465 A US46009465 A US 46009465A US 3365136 A US3365136 A US 3365136A
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US
United States
Prior art keywords
zone
burner
air inlet
air
flame
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
US460094A
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English (en)
Inventor
Rolland L Hoffman
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.)
Bloom Engineering Co Inc
Original Assignee
Bloom Engineering Co Inc
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
Priority to FR1481636D priority Critical patent/FR1481636A/fr
Application filed by Bloom Engineering Co Inc filed Critical Bloom Engineering Co Inc
Priority to US460094A priority patent/US3365136A/en
Priority to NL6607529A priority patent/NL6607529A/xx
Priority to LU51216A priority patent/LU51216A1/xx
Priority to GB24297/66A priority patent/GB1073120A/en
Priority to BE681862D priority patent/BE681862A/xx
Priority to AT519066A priority patent/AT290706B/de
Application granted granted Critical
Publication of US3365136A publication Critical patent/US3365136A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D99/00—Subject matter not provided for in other groups of this subclass
    • F27D99/0001—Heating elements or systems
    • F27D99/0033—Heating elements or systems using burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space

Definitions

  • This invention relates to a burner for tempered flame operation for the heat treatment of work such as billets, blooms, bars and the like, particularly at low ternmratures, such as in the range 300l500 F. It is concerned especially with a burner for delivering to the work a clear substantially non-luminous flame, which flame can be tempered (i.e., its temperature controlled) over a wide range and is delivered at such velocity as to assure optimum circulation and conversion.
  • a flame which is substantially non-luminous, i.e., clear, since a luminous flame radiates more heat than a non-luminous flame and results in localized hot spots in the work having disadvantages well known to those skilled in the art.
  • a clear or non-luminous flame delivers most of its heat to the work by convection. When adequate circulation is provided for the work is heated with optimum uniformity. It is also important to be able to temper 'the flame, i.e., deliver it to the work at a controlled temperature lower than the temperature produced under stoichiometric operation and close to the final work temperature.
  • M burner may also be employed under reducing conditions, i.e., with a deficiency of air relative to stoichiornetric proportions.
  • I provide a burner for tempered flame operation comprising a burner body having two communicating coaxial zones, at first zone of relatively small transverse dimension and a second zone of relatively great transverse dimension, generally axially directed fuel inlet means admitting fuel into the first zone in a direction to pass through the first zone into the second zone, means for controlling the quantity of fuel admitted through the fuel inlet means, first air inlet means admitting air into the first zone at the end of the first zone at which the fuel is admitted, second air inlet means admitting air into the second zone at the end of the second zone where the second zone communicates with the first zone and third air inlet means admitting air into the second zone at a location spaced from the end of the second zone where the second zone communicates with the first zone.
  • the first and second air inlet means preferably admit air in a direction generally parallel to the direction of fuel flow through the burner and the third air inlet means admit air in a direction inwardly at an angle to the direction of fuel flow through the burner.
  • each of the first and second zones of by burner has at the inlet end thereof a generally radial wall with the first and second air inlet means constituted by series of air inlet openings through such respective radial walls.
  • the radial distance from the inner edge of each of the air inlet openings of the second air inlet means to the inside face of the first zone should be no greater than .336 inch.
  • the air inlet openings of the first air inlet means should have a length to diameter ratio substantially in the range 1.16- 3.00 and the air inlet openings of the second air inlet means should have a length to diameter ratio substantially in the range .831.20.
  • Means should be provided for delivering air to the burner at a pressure substantially in the range 6-7 inches'water column.
  • burner preferably has a jacket constituting a part of the burner body generally surrounding the two communicating coaxial zones and defining an air supply manifold communicating with the first, second and third air inlet means, the manifold having an air inlet port through which air is delivered thereto.
  • FIGURE 1 is an axial cross-sectional view through a burner constructed in accordance with my invention.
  • FIGURES 2, 3, 4, 5 and 6 are diagrams illustrating operation of the burner shown in FIGURE 1.
  • FIGURE 1 there is shown a burner for tempered flame operation which comprises a burner body designated generally by reference numeral 2 having two communicating coaxial zones 3 and 4 respectively, the first zone 3 being of relatively small transverse dimen sion and the second zone 4 being relatively great transverse dimension.
  • the zone 3 is defined by a cylindrical wall 5 and zone 4 is defined by a cylindrical wall 6.
  • the zone 3 has a diameter substantially less than that of the zone 4 and the cylindrical wall 5 is joined to the cylindrical wall 6 by a radial wall 7 which is in radial alignment with the right-hand extremity, viewing FIGURE 1, of the zone 3 which, as will presently appear, is the outlet extremity of that zone.
  • the left-hand extremity of the zone 3, which is the inlet extremity of that zone, is defined by a radial wall 8.
  • Fuel normally gas, although oil may be used, is admitted to the burner through an axial port 9 opening into the zone 3.
  • the fuel is delivered through a suitable conduit adapted to be connected to the burner at 10.
  • a jacket 11 constituting a part of the burner body 2 generally surrounds the zones 3 and 4 and defines an air supply manifold designated generally by reference numeral 12. Air is delivered to the manifold 12 through an air inlet port 13.
  • Air is delivered from the manifold 12 into the zone 3 through first air inlet means in the form of a series of air inlet openings 14 in the Wall 8 surrounding the fuel inlet port 9. Air is delivered from the manifold 12 into the zone 4 through second air inlet means in the form of a series of air inlet openings 15 in the wall 7 surrounding the outlet extremity of the first zone. Air is delivered from the manifold 12 into the zone 4 at a location spaced from the inlet end of zone 4 through third air inlet means in the form of a series of air inlet openings 16 in the cylindrical wall 6. The openings 16 admit air in a direction inwardly at an angle to the direction of fuel flow through the burner.
  • the air inlet openings 16 are shown as having their axes inclined at an acute angle to the axis of the burner the axes of the openings 16 may be at right angles to the axis of the burner. Also while in the form shown the axes of the openings 16 intersect the axis of the burner the openings may be arranged with their axes offset from the axis of the burner to create a swirl in the burner.
  • a pilot duct is shown at 17.
  • each of the openings 15 should be no greater than .336 inch. This dimension is indicated by the letter X in FIGURE 1.
  • the length to diameter ratio of each of the Openings 14 should be substantially in the range 1.16-3.00 and the length to diameter ratio of each of the openings 15 should be substantially in the range .83-l.20.
  • the length of one of the openings 15 is designated by L and the diameter by D. It is found that when the openings are thus proportioned an optimum jet effect of the air is created.
  • FIGURES 2, 3, 4, 5 and 6 illustrate the operation of my burner respectively with 425%, 600%, 1000% and 1500% excess air.
  • air and fuel are induced in stoichiometric proportions.
  • the flame is stabilized at the openings 15 which in reference to operation of the burner may be referred to as the second stage air inlet openings.
  • the openings 141 may be referred to as the first stage air inlet openings.
  • the openings 16 may be referred to as the third stage air inlet openings.
  • the second and third stages and the port block 18 are filled with flame. There is no combustion in the first stage, i.e., in the zone 3.
  • FIGURE 3 shows the operating condition when the gas flow is reduced so that 425% excess air is supplied. It is desirable to maintain the air flow constant and control the temperature of the flame by varying the fuel input. In FIGURE 3 combustion begins to occur in the first stage but it is not stabilized there. The flame front is still well established at the second stage air inlet openings 15.
  • FIGURE 4 shows the operating condition when the gas flow is reduced so that 600% excess air is supplied.
  • the flame front establishes itself at the first stage air inlet openings 14 but most of the combustion is still occurring at the second stage air inlet openings 15. In effect there are now two flame fronts established.
  • FIGURE 5 shows the operating condition when the gas flow is reduced so that 1000% excess air is supplied. Combustion is still occurring in the first and second stages but stabilization is occurring at the first stage air inlet openings 14. There is still some burning occurring around the second stage air inlet openings but such burning is not contributing to the stabilization of the flame.
  • FIGURE 6 shows the operating condition when the gas flow is reduced so that 1500% excess air is supplied. There is no more flame around the second stage air inlet openings 15 and the flame front is still well established at the first stage air inlet openings 14. Maximum excess air for the burner would be 2500%, more or less, the flame having the general character shown in FIG- URE 6.
  • the flame is clear or substantially non-luminous so that the heat is transmitted to the work by convection rather than by radiation, avoiding hot spots in the work.
  • the flame may be tempered over a wide range while maintaining the flame clear and also maintaining adequate circulation to insure optimum uniformity of heat transfer to the work by convection.
  • the burner is also adapted when conditions so indicate to operate with a deficiency of air resulting in reducing conditions in the furnace.
  • the length to diameter ratios of the air inlet openings 14 and 15 specified above provide for a desired jet action promoting adequate velocity of flow through the burner and optimum convection in the furnace.
  • the above mentioned radial distance from the inner edge of each of the air inlet openings 15 to the inside face of the first zone is independent of the size of the air inlet openings or the diameter of the zone 3.
  • the jets of air from the air inlet openings 15 entrain the mixture from the first stage, lowering the pressure there. This in turn allows the gas to expand and be more readily entrained by the first stage jets when the burner is operating with an excess of air.
  • the entrainment of the gas into the air jets that provides flame retention; i.e., in each stage the flame front is established in small zones surrounding the perimeters of the air jets.
  • the entrainment effect of the second stage jets is too small to contirbute effectively to the lowering of the pressure in the first stage.
  • the dimension is independent of air inlet opening size because it is determined by the jet velocity and flow conditions which in turn are determined by the pressure drop and the length to diameter ratio of the air inlet openings. As the flow is made more laminar entrainment is improved.
  • the burner is capable of operation at a higher excess of air when the air pressure is reduced and the length to diameter ratio of the air inlet means of the second stage (15) is increased. Both of these changes cause the flame to tend to be somewhat luminous so the extent of their use is limited.
  • a suitable balance between excess air capacity and luminosity has been achieved in existing burners with air pressure in the range 6-7 inches water column and length to diameter ratios of the air inlet openings as above specified.
  • the first stage velocity should be less than 155,000 B.t.u. per square inch of cross sectional area based on the nominal capacity of the burner. If the velocity is further increased the velocity of the mixture leaving the first stage exceeds the flame velocity and the flame front will not transfer from the second to the first stage when the gas is turned down.
  • the critical velocity for the transfer may be increased by increasing the air pressure, increasing the gas pressure or decreasing the distance from the inner edge of the second stage air inlet openings 15 to the inside face of the first zone or stage 3. All of these changes increase the rate of mixing in the first stage but then the range of gas turndown after the flame front has transferred is decreased.
  • a burner for tempered flame operation comprising a burner body having two communicating coaxial combustion zones disposed for the passage of fuel successively therethrough, a first zone of relatively small transverse dimension and a second zone of relatively great transverse dimension, said first zone having an outlet opening adjoining an inlet opening of said second zone, generally axially directed fuel inlet means disposed in an inlet opening of said first zone and admitting fuel into the first zone in a direction to pass through the first zone into the second zone, first air inlet means admitting air into the first zone adjacent said inlet means, second air inlet means admitting air into the second zone adjacent said first zone where the second zone communicates with the first zone, and third air inlet means admitting air into the second Zone at a location therein remote from said first zone, whereby the turn-down ratio of said burner is greatly increased, the operation of said burner being that as the fuel is turned down the flame generated by combustion thereof progressively recedes from said second zone into said first zone.
  • a burner as claimed in claim 1 in which the first and second air i t l means admit air in a direction generally parallel to the direction of fuel flow through the burner and the third air inlet means admit air in a direction inwardly at an angle to the direction of fuel flow through the burner.
  • a burner as claimed in claim 1 in which the second zone has the inlet opening thereof defined by a generally radial wall in radial alignment with the outlet opening of the first zone with the second air inlet means constituted by a series of air inlet openings through such radial wall, the radial distance between each of such air inlet openings and an inner surface of the first zone being no greater than .336 inch.
  • each of the first and second zone inlet openings is defined by a generally radial wall with the first and second air inlet means constituted by series of air inlet openings through such respective radial Walls.
  • a burner as claimed in claim 5 in which the air inlet openings of the first air inlet means have a length to diameter ratio substantially in the range 1.16-3.00 and the air inlet openings of the second air inlet means have a length to diameter ratio substantially in the range .83- 1.20.
  • a burner as claimed in claim 1 having a jacket constituting a part of the burner body generally surrounding the two communicating coaxial zones and defining an air supply manifold communicating with the first, second and third air inlet means, the manifold having an air inlet port through which air is delivered thereto.
  • each of the first and second zones has at the inlet opening thereof a generally radial wall with the first and second air inlet means constituted by series of air inlet openings through such respective radial walls, the radial distance from the inner edge of each of the air inlet openings of the second air inlet means to the inside face of the first zone being no greater than .336 inch, the air inlet openings of the first air inlet means having a length to diameter ratio substantially in the range 1.163.00 and the air inlet openings of the second air inlet means having a length to diameter ratio substantially in the range .83l.20.
  • a burner as claimed in claim 1 in which a port block member is secured to said burner body adjacent an outlet opening of said second zone, said member having an opening therethrough communicating with said second zone and disposed substantially co-axially therewith, said port block opening defining a combustion area.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
US460094A 1965-06-01 1965-06-01 Burner for tempered flame operation Expired - Lifetime US3365136A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR1481636D FR1481636A (de) 1965-06-01
US460094A US3365136A (en) 1965-06-01 1965-06-01 Burner for tempered flame operation
NL6607529A NL6607529A (de) 1965-06-01 1966-05-31
LU51216A LU51216A1 (de) 1965-06-01 1966-05-31
GB24297/66A GB1073120A (en) 1965-06-01 1966-05-31 Burner for tempered flame operation
BE681862D BE681862A (de) 1965-06-01 1966-05-31
AT519066A AT290706B (de) 1965-06-01 1966-06-01 Regelbarer Brenner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US460094A US3365136A (en) 1965-06-01 1965-06-01 Burner for tempered flame operation

Publications (1)

Publication Number Publication Date
US3365136A true US3365136A (en) 1968-01-23

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ID=23827364

Family Applications (1)

Application Number Title Priority Date Filing Date
US460094A Expired - Lifetime US3365136A (en) 1965-06-01 1965-06-01 Burner for tempered flame operation

Country Status (7)

Country Link
US (1) US3365136A (de)
AT (1) AT290706B (de)
BE (1) BE681862A (de)
FR (1) FR1481636A (de)
GB (1) GB1073120A (de)
LU (1) LU51216A1 (de)
NL (1) NL6607529A (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3664315A (en) * 1970-03-16 1972-05-23 Allied Chem Lp-gas ram-air charger
US3705690A (en) * 1972-04-17 1972-12-12 Joseph W Brown Combustion heads
US4014639A (en) * 1975-04-10 1977-03-29 Minnesota Mining And Manufacturing Company Recirculating vortex burner

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US533400A (en) * 1895-01-29 Air-injector and oil-burner
US837571A (en) * 1906-03-16 1906-12-04 Frank A Hawes Gas-furnace.
US1069243A (en) * 1912-03-13 1913-08-05 George L Fogler Furnace-burner.
US1451063A (en) * 1923-04-10 Burner
GB687662A (en) * 1949-10-05 1953-02-18 Ronald Calvert Improvements in or relating to gas burners
US2732255A (en) * 1956-01-24 Apparatus for obtaining an exceedingly
GB805902A (en) * 1955-08-01 1958-12-17 Wistra Ofenbau Oil-gasifying burner
US3050112A (en) * 1960-09-02 1962-08-21 Eclipse Fuel Eng Co Radiant gas burner

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US533400A (en) * 1895-01-29 Air-injector and oil-burner
US1451063A (en) * 1923-04-10 Burner
US2732255A (en) * 1956-01-24 Apparatus for obtaining an exceedingly
US837571A (en) * 1906-03-16 1906-12-04 Frank A Hawes Gas-furnace.
US1069243A (en) * 1912-03-13 1913-08-05 George L Fogler Furnace-burner.
GB687662A (en) * 1949-10-05 1953-02-18 Ronald Calvert Improvements in or relating to gas burners
GB805902A (en) * 1955-08-01 1958-12-17 Wistra Ofenbau Oil-gasifying burner
US3050112A (en) * 1960-09-02 1962-08-21 Eclipse Fuel Eng Co Radiant gas burner

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3664315A (en) * 1970-03-16 1972-05-23 Allied Chem Lp-gas ram-air charger
US3705690A (en) * 1972-04-17 1972-12-12 Joseph W Brown Combustion heads
US4014639A (en) * 1975-04-10 1977-03-29 Minnesota Mining And Manufacturing Company Recirculating vortex burner

Also Published As

Publication number Publication date
GB1073120A (en) 1967-06-21
FR1481636A (de) 1967-08-21
NL6607529A (de) 1966-12-02
LU51216A1 (de) 1966-08-01
AT290706B (de) 1971-06-11
BE681862A (de) 1966-11-30

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