US1953590A - Gas burner - Google Patents

Gas burner Download PDF

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Publication number
US1953590A
US1953590A US668733A US66873333A US1953590A US 1953590 A US1953590 A US 1953590A US 668733 A US668733 A US 668733A US 66873333 A US66873333 A US 66873333A US 1953590 A US1953590 A US 1953590A
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Prior art keywords
air
tube
tunnel
chamber
gas
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Expired - Lifetime
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US668733A
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Cone Carroll
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Surface Combustion Corp
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Surface Combustion Corp
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Priority to US668733A priority Critical patent/US1953590A/en
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    • 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

Definitions

  • Fig. 1 is a longitudinal section through the improved burner, a portion of the wall of the furnace to be fired being also shown;
  • Fig. 2 is a section 'on line 2-2 of Fig. 1, and
  • Fig. 3 is'a section on line 3--3 of Fig. 1.
  • numeral 10 indicates a portion of a furnace wall which is apertured to receive a refractory body or tunnel 11.
  • a chambered casing generally indicated at 12.
  • annular flange 13 At one side of this casing'is an annular flange 13 whereinto one end of the tunnel 11 projects.
  • the casing 12 is provided with an air chamber 14, the inlet to which is indicated at 15, and a gas chamber 16, the inlet to which is indicated at 17.
  • These two chambers are separated from each other by a common partition wall 18 having a relatively large circular aperture 1 coaxial with that of the flange13.
  • a refractory tube Secured to the wall 18 and projecting therefrom into the tunnel 11 in radially spaced relation is a refractory tube, generally indicated at 20.
  • a radial flange 21 which is clamped between said wall and a clamping ring 22 by means of bolts 23 secured in the wall 18.
  • On the outside of the tube are longitudinally ex tending ribs 24 for maintaining the tubeand tunnel in spaced concentric relation.
  • the annular passage 25 thus formed between the inner wall of the tunnel and the outer wall of the tube 20 is in direct communication with the air chamber 14.
  • a refractory tube 26 Concentrically positioned within the tube 20 in radially spaced relation to form an annular passage 38 and projecting therefrom is a refractory tube 26.
  • the tube 26 is secured to an annular wall section 2'1 as by means of bolts 28 secured to said section and a ring 29 bethe chamber 1% is in direct connection with the tween which and said wall section a flange on the tube 26 is clamped.
  • the annular wall. section 2'? is part of a chambered structure 30 which is removably secured to the outer face'of the casing 12 as by means of bolts 31. It will be understood that when the structure 30 is disconnected from the casing 12, the tube 26 will be withdrawn from. the tube 20.
  • the annular passage 38 is in direct communication with the gas chamber 16.
  • the chamber of the structure 30 is indicated at 32 and this chamber and the air chamber 14 are in direct communication by way of a passage 33 in the form of a relatively wide slot as clearly shown in Fig. 2. From this it will be understood that interior of the tube 26. As already stated the chamber 14 is also in direct communication with the annular passage 25 between the tunnel 11 and the tube 20.
  • the air and gas will ordinarily be supplied to their respective chambers 14 and 16 at relatively low and preferably equal pressures.
  • the vane 34 When the vane 34 is in vertical position as indicatedin'full 106 lines in Fig. 2, the air and gas will flow from' the tunnel 11 as a composite stream made up of well defined streams of air and gas. In such composite stream, mixing of the air and gas takes place primarily by interdiifusion with the result- 1053 ant production of a luminous flame of substantial length.
  • the ribs 24 and 24' materially assist in causing the air and gas to leave their passages 25 and 38 in stream line flow as will be readily appreciated.
  • a gas burner comprising in combination, a casing providedwith pressure air and gas supply chambers respectively, a tunnel amociated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas supply chamber with the outer tube, the outertube being radially spaced from the walls or the tunnel.
  • a gas burner comprising in combination, a casing provided with pressure air and gas supply chambers respectively, a tunnel associated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas' supply chamber with the outer tube, the outer tube being radially spaced from the walls of the tunnel, and means between the inner tube and its communicating chamber for causing the air from such chamber to enter the tube with a rotary motion.
  • said inner tube projecting from the tunnel to a greater extent than the outer tube, and the gas chamber surrounding the projecting end of the inner tube.
  • a gas burner comprising in combination, a casing provided with pressure air and gas supply chambers respectively, a tunnel associated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas supply chamber with the outer tube, the outer tube being radially spaced from the walls of the tunnel, and circumferentially spaced means dividing the annular spaces formed by said tubes into individual straightaway passages.

Description

C. CONE GAS BURNER April 3,1934.
Filed may 1, 1935 v INVENTOR. CARROLL (0N5 ATTORNEY.
Patented Apr. 3, 1934 GAS BURNER Carroll Cone, Lucas County, Ohio, assignor to Surface Combustion Corporation, Toledo, Ohio, a corporation of New York Application May 1, 1933, SerialNo. 668,733
6 Claims.
' Joe *simple in construction and well adapted for its intended purpose.
The various features of novelty and invention will fully appear from the detailed description taken in connection with the accompanying drawing forming part of this specification and where- Fig. 1 is a longitudinal section through the improved burner, a portion of the wall of the furnace to be fired being also shown;
Fig. 2 is a section 'on line 2-2 of Fig. 1, and
Fig. 3 is'a section on line 3--3 of Fig. 1.
1n the drawing, numeral 10 indicates a portion of a furnace wall which is apertured to receive a refractory body or tunnel 11. At one end of the tunnel is a chambered casing generally indicated at 12. At one side of this casing'is an annular flange 13 whereinto one end of the tunnel 11 projects. The casing 12 is provided with an air chamber 14, the inlet to which is indicated at 15, and a gas chamber 16, the inlet to which is indicated at 17. These two chambers are separated from each other by a common partition wall 18 having a relatively large circular aperture 1 coaxial with that of the flange13.
Secured to the wall 18 and projecting therefrom into the tunnel 11 in radially spaced relation is a refractory tube, generally indicated at 20. For seeming the tube to the wall 18, there is provided on the tube a radial flange 21 which is clamped between said wall and a clamping ring 22 by means of bolts 23 secured in the wall 18. On the outside of the tube are longitudinally ex tending ribs 24 for maintaining the tubeand tunnel in spaced concentric relation. The annular passage 25 thus formed between the inner wall of the tunnel and the outer wall of the tube 20 is in direct communication with the air chamber 14. Concentrically positioned within the tube 20 in radially spaced relation to form an annular passage 38 and projecting therefrom is a refractory tube 26. Internal longitudinally extending ribs 24' onthe tube 20 maintain the tubes 20 and 426 in radially spaced relation. "The tube 26 is secured to an annular wall section 2'1 as by means of bolts 28 secured to said section and a ring 29 bethe chamber 1% is in direct connection with the tween which and said wall section a flange on the tube 26 is clamped. The annular wall. section 2'? is part of a chambered structure 30 which is removably secured to the outer face'of the casing 12 as by means of bolts 31. It will be understood that when the structure 30 is disconnected from the casing 12, the tube 26 will be withdrawn from. the tube 20. The annular passage 38 is in direct communication with the gas chamber 16.
The chamber of the structure 30 is indicated at 32 and this chamber and the air chamber 14 are in direct communication by way of a passage 33 in the form of a relatively wide slot as clearly shown in Fig. 2. From this it will be understood that interior of the tube 26. As already stated the chamber 14 is also in direct communication with the annular passage 25 between the tunnel 11 and the tube 20.
Positioned within the chamber 32 is an air defiector or vane 3 Laflixed to a shaft 35 having a crank arm 36 arranged in abutting relation with an arcuate locking flange 37 on the face of the structure 30. When the vane is in the position indicated by the broken lines in Fig. 2 the air flowing through the passage 33 from the chamber 14 will be deflected toward the right as viewed in Fig. 2 and hence the air will tend to flow as indicated by the arrows in Fig. 2, that is to say, in a clockwise direction with the result that the air will enter the tube 26 with a rotary motion.
When the 'vane 34 is vertically disposed as shown in Fig. 2 it will, of course, have no particular effect on the air flowing through the passage 33 and hence the air will enter and flow through the tube 26 Without rotary motion. The vane may be locked by the crank arm 36 at any degree of angularity within its limits of movement and hence the degree of rotation of the air entering the tube 26 can be readily controlled as will now be readily appreciated.
The air and gas will ordinarily be supplied to their respective chambers 14 and 16 at relatively low and preferably equal pressures. When the vane 34 is in vertical position as indicatedin'full 106 lines in Fig. 2, the air and gas will flow from' the tunnel 11 as a composite stream made up of well defined streams of air and gas. In such composite stream, mixing of the air and gas takes place primarily by interdiifusion with the result- 1053 ant production of a luminous flame of substantial length. On the other hand it is possible, without disturbing the governing apparatus (not shown) which controls the admission of air and gas to the burner, to cause a more rapid mixing of the 10 air and gas by the simple expedient of so adlusting the vane 34 that rotary motion will be imparted to the air flowing into the tube 26. Upon leaving the tunnel the mixture tends to spread out radially and hence there is produced a relatively short spreading iiame as will now be readily understood.
The ribs 24 and 24' materially assist in causing the air and gas to leave their passages 25 and 38 in stream line flow as will be readily appreciated.
What I claim is:-
1. A gas burner comprising in combination, a casing providedwith pressure air and gas supply chambers respectively, a tunnel amociated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas supply chamber with the outer tube, the outertube being radially spaced from the walls or the tunnel.
2. A gas burner comprising in combination, a casing provided with pressure air and gas supply chambers respectively, a tunnel associated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas' supply chamber with the outer tube, the outer tube being radially spaced from the walls of the tunnel, and means between the inner tube and its communicating chamber for causing the air from such chamber to enter the tube with a rotary motion.
3. In the combination specified in claim 2,-said means comprising an adiustably mounted vane disposed in-the path of flow oi! the air.
4. In the combination specified in claim 1, said inner tube projecting from the tunnel to a greater extent than the outer tube, and the gas chamber surrounding the projecting end of the inner tube.
5. A gas burner comprising in combination, a casing provided with pressure air and gas supply chambers respectively, a tunnel associated with the casing and receiving air from the air supply chamber, a pair of radially spaced concentric tubes within and projecting from said tunnel, said air supply chamber being in communication with the inner tube and the gas supply chamber with the outer tube, the outer tube being radially spaced from the walls of the tunnel, and circumferentially spaced means dividing the annular spaces formed by said tubes into individual straightaway passages.
6. In a gas burner, the combination of an air chamber divided into two communicating compartments by a wall having a slot, a combustion tunnel in communication with one of said compartments, a tube in communication with the other compartment andprojecting into said tunnel,
a vane in that compartment which is in communicati'on with said tube, means for turnably CARROLL CONE.
Ill
ill
US668733A 1933-05-01 1933-05-01 Gas burner Expired - Lifetime US1953590A (en)

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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458542A (en) * 1944-11-16 1949-01-11 Comb Processes Company Low velocity oil and gas burner
US2480657A (en) * 1944-02-17 1949-08-30 Lawson Mfg Company Water heater
US2515300A (en) * 1950-07-18 Heating apparatus fob bonding
US2796118A (en) * 1954-07-21 1957-06-18 Hanck Mfg Co Burner for tube firing
US2821246A (en) * 1951-05-14 1958-01-28 Synchronous Flame Inc Combination oil-gas burner and gas burner adapter for gun-type oil burner
DE1079259B (en) * 1953-09-21 1960-04-07 Iaofuia Ofenbau Union Ges Mit Device for influencing the flow in a cylindrical chamber
US2952307A (en) * 1955-10-26 1960-09-13 Midland Ross Corp Burner apparatus
US2992678A (en) * 1951-11-19 1961-07-18 Midland Ross Corp Burner apparatus and controls therefor
US3049173A (en) * 1959-08-31 1962-08-14 Nat Heater Company Inc Burner
US3097073A (en) * 1957-11-29 1963-07-09 Hooker Electrochemical Co Hydrogen chloride production system
DE1265333B (en) * 1962-11-26 1968-04-04 Chemetron Corp burner
US3412987A (en) * 1965-09-27 1968-11-26 Maximilian Linker Thermoconverter run with universal fuel for the production of pure air
DE1301415B (en) * 1964-09-24 1969-08-21 Entpr Generale De Chauffage In Device for generating a mixture of flue gas and secondary air
US3836315A (en) * 1971-10-14 1974-09-17 Pyronics Inc Burner apparatus for flame propagation control
FR2429965A1 (en) * 1978-06-28 1980-01-25 Matsushita Electric Ind Co Ltd APPARATUS FOR COMBUSTING A MIXTURE OF AIR AND FUEL
US4281984A (en) * 1979-07-18 1981-08-04 Kawasaki Steel Corporation Method of heating a side-burner type heating furnace for slab
US4626195A (en) * 1984-05-09 1986-12-02 Kawasaki Steel Corporation Low load burning burner
US5743723A (en) * 1995-09-15 1998-04-28 American Air Liquide, Inc. Oxy-fuel burner having coaxial fuel and oxidant outlets
WO2009122049A1 (en) * 2008-04-03 2009-10-08 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Combustion tool comprising tap hole block and injector, the structure and furnace of which are equipped with said tool
US20100304314A1 (en) * 2007-05-10 2010-12-02 Saint-Gobain Emballage Low nox mixed injector

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2515300A (en) * 1950-07-18 Heating apparatus fob bonding
US2480657A (en) * 1944-02-17 1949-08-30 Lawson Mfg Company Water heater
US2458542A (en) * 1944-11-16 1949-01-11 Comb Processes Company Low velocity oil and gas burner
US2821246A (en) * 1951-05-14 1958-01-28 Synchronous Flame Inc Combination oil-gas burner and gas burner adapter for gun-type oil burner
US2992678A (en) * 1951-11-19 1961-07-18 Midland Ross Corp Burner apparatus and controls therefor
DE1079259B (en) * 1953-09-21 1960-04-07 Iaofuia Ofenbau Union Ges Mit Device for influencing the flow in a cylindrical chamber
US2796118A (en) * 1954-07-21 1957-06-18 Hanck Mfg Co Burner for tube firing
US2952307A (en) * 1955-10-26 1960-09-13 Midland Ross Corp Burner apparatus
US3097073A (en) * 1957-11-29 1963-07-09 Hooker Electrochemical Co Hydrogen chloride production system
US3049173A (en) * 1959-08-31 1962-08-14 Nat Heater Company Inc Burner
DE1265333B (en) * 1962-11-26 1968-04-04 Chemetron Corp burner
DE1301415B (en) * 1964-09-24 1969-08-21 Entpr Generale De Chauffage In Device for generating a mixture of flue gas and secondary air
US3412987A (en) * 1965-09-27 1968-11-26 Maximilian Linker Thermoconverter run with universal fuel for the production of pure air
US3836315A (en) * 1971-10-14 1974-09-17 Pyronics Inc Burner apparatus for flame propagation control
FR2429965A1 (en) * 1978-06-28 1980-01-25 Matsushita Electric Ind Co Ltd APPARATUS FOR COMBUSTING A MIXTURE OF AIR AND FUEL
US4265614A (en) * 1978-06-28 1981-05-05 Matsushita Electric Industrial Co., Ltd. Combustion apparatus
US4281984A (en) * 1979-07-18 1981-08-04 Kawasaki Steel Corporation Method of heating a side-burner type heating furnace for slab
US4626195A (en) * 1984-05-09 1986-12-02 Kawasaki Steel Corporation Low load burning burner
US5743723A (en) * 1995-09-15 1998-04-28 American Air Liquide, Inc. Oxy-fuel burner having coaxial fuel and oxidant outlets
US20100304314A1 (en) * 2007-05-10 2010-12-02 Saint-Gobain Emballage Low nox mixed injector
US9169148B2 (en) * 2007-05-10 2015-10-27 Saint-Gobain Emballage Low NOx mixed injector
WO2009122049A1 (en) * 2008-04-03 2009-10-08 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Combustion tool comprising tap hole block and injector, the structure and furnace of which are equipped with said tool
FR2929687A1 (en) * 2008-04-03 2009-10-09 Air Liquide COMBUSTION TOOL COMPRISING A CLOSURE BLOCK AND AN INJECTOR, ITS ASSEMBLY AND OVEN EQUIPPED WITH SAID TOOL
US20110183278A1 (en) * 2008-04-03 2011-07-28 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Combustion Tool Comprising a Quarl Block and an Injector, Assembly of Said Tool and Furnace Equipped with Said Tool

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