US3592578A - Gas burners - Google Patents

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US3592578A
US3592578A US5166A US3592578DA US3592578A US 3592578 A US3592578 A US 3592578A US 5166 A US5166 A US 5166A US 3592578D A US3592578D A US 3592578DA US 3592578 A US3592578 A US 3592578A
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manifold
gas
apertures
manifolds
series
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US5166A
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Richard N Weatherston
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Weather Rite Manufacturing
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Weather Rite Manufacturing
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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
    • F23D14/34Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/21Burners specially adapted for a particular use
    • F23D2900/21003Burners specially adapted for a particular use for heating or re-burning air or gas in a duct

Definitions

  • a gas burner formed from an elon extrusion having three manifolds formed therei manifolds comprises a high-pressure manifold deliverin gas through a series of apertures to the main flame w second manifold delivers a combustible through a second series of apertures to the flame.
  • the third manifold delivers h series of transfer apertures to the secon along the entire length of the second manifold.
  • admission apertures along the second manifold allow air to pass into the gas in the second manifold under the influence of aspiration.
  • GASBURNERS [50] FieldofSearch...
  • the new extruded gas burners described in the above-referenced copending application are formed with an internal partition dividing them into two elongated parallel manifolds each having a series of spaced apertures therein which apertures face the scholar-tion area.
  • Regulated relatively highpressure gas is introduced into one of the manifolds which passes out of the apertures and generates a large main flame for the main heating function.
  • the second manifold receives a mixture of gas and air under a relatively low-pressure which serves to generate a small pilot flame for low heating requirements and for igniting the main flame.
  • the low-pressure manifold tends to have a more stable flame near the end at which the gas-air mixture is introduced than at the more distant end. Due to the gradual loss of pressure along the length of the pilot manifold and the inconsistent mixing of air and gas afforded by a single mixing device the flame characteristics along the manifold change. This uneven flame along the length of the burner produces uneven heating over the length of the burner with a number of consequent disadvantages. Since the burner depends wholly or partly on the pilot flame for low-level heating the heat output of the burner is uneven over its length. Another difficulty is that the large volume of air and gas mixture necessary to supply a long pilot manifold requires a complicated and expensive air and gas mixing device.
  • the novel design of the present invention avoids the above described problems.
  • the present invention contemplates using an elongated extrusion with three elongated parallel manifolds formed therein. Two of the manifolds supply the main flame and the pilot flame apertures while the third manifold accepts high-pressure gas which is transferred to the pilot flame manifold through a series of periodic apertures along the length of the pilot manifold. The gas, thus, enters the pilot manifold at the same pressure everywhere along the entire length of the pilot manifold alleviating the uneven flame problem.
  • Another set of air admission apertures are formed in the outside wall of the pilot manifold adjacent the transfer apertures in a one-to-one relationship so that the high-pressure gas passing form the third manifold to the pilot manifold will aspirate air along with it from the air admission apertures automatically so as to eliminate the need for the expensive and complicated prior art air-gas mixing apparatus.
  • FIG. 1 is a partially cutaway perspective view of the main elements of the present inventive gas burner.
  • FIG. 2 is a cross-sectional view of the burner assembly of FIG. 1 in which the improved extruded manifold is shown in greater detail.
  • FIG. 1 a portion of a burner compartment 10 is shown partially cutaway so as to provide a better view of the burner assembly 12 mounted in compartment 10.
  • Burner assembly 12 comprises an extruded hollow member 14, upper and lower plates 16 and 18, end plates 20 and 22 and a pair of diverging foraminous plates 24 and 26.
  • Foraminous plates 26 and 26 define a combustion area between them where air mixes with gas emerging from a series of holes 30 in member 14.
  • Holes 30 connect with the large manifold 31 inside member 14 which manifold receives gas from a regulated source through a pipe 32.
  • End plates such as plate 34 in FIG. 1 serve to close the ends of the manifolds in hollow member 14.
  • burner assembly 12 is shown in section.
  • high-pressure gas is introduced into manifold 42 which extends the full length of member 14 generally parallel to manifold 40.
  • Manifold 42 connects with manifold 40 by means of a series of transfer apertures 46.
  • Apertures 46 are relatively small so that the gas metered into manifold 40 at a slow predetermined rate.
  • apertures 46 are formed by a no. 44 drill and spaced at approximately 24 -inch intervals. This has been found to yield a pressure in manifold 40 which.
  • a series of air admission holes 50 are provided in the bottom of manifold 40.
  • One hole 50 is provided adjacent each transfer aperture 46.
  • the high-velocity gas entering through aperture 46 sucks air through hole 50 into manifold 4 by means of aspiration.
  • This flow of air mixes with the gas from aperture 46 and continues on out through pilot apertures 38 assisted by the low-pressure area which exists between foraminous plates 24 and 26 when the flame is burning in the combustion area between plates 24 and 26.
  • Holes 50 have been made approximately one-half inch in diameter in the preferred embodiment which size has been found to provide the proper air-to-gas ratio for proper combustion.
  • the size of the furnace can be varied simply by varying the length of extrusion 14. Since the gas is supplied equally along the length of the burner and since air is aspirated equally along the length of the burner any length may be chosen for the burner without adjustments to any of the gas or air supply apparatus. Furthermore, an even flame is produced over the length of the chosen burner due to the constant pressure characteristics along the pilot manifold.
  • Transfer apertures 46 may be drilledthrough the pilot flame holes 38 if desired but in the preferred embodiment separate access holes 52 are provided in manifold 42 opposite transfer holes 46. Holes 46 may be drilled through access holes 52 and, in addition, transfer holes 46 may be conveniently cleaned by means of access holes 52. In operation, access holes 52 are plugged by means of small sealing screws 54 to prevent escape of the gas.
  • a gas burner comprising in combination:
  • an elongated hollow extrusion having a front side facing the combustion area with two sets of longitudinally spaced outlet apertures therein;
  • partitions in said extrusion dividing the interior of the extrusion into first, second, and third longitudinally extending manifolds, said first manifold in communication with one of said sets of outlet apertures and said second manifold in communication with the other set of outlet apertures; means closing the ends of said manifolds;
  • the apparatus of claim 1 including a series of air admission apertures in said second manifold sized to pass air at a rate dependent on the flow of gas through said transfer apertures.
  • said air admission apertures comprise a series of holes positioned one each next to the transfer apertures so that the flow of gas through said transfer apertures aspirates air into said second manifold through said air admission apertures.
  • said gas-supplying means comprise a pair of inlet pipes connected to said first and third manifolds whereby gas pressure in one of the manifolds may differ from the gas pressure in the other manifold.

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

Abstract

A gas burner formed from an elongated hollow extrusion having three manifolds formed therein. One of the manifolds comprises a high-pressure manifold delivering raw gas through a series of apertures to the main flame while the second manifold delivers a combustible gas and air mixture through a second series of apertures to the pilot or low-heat flame. The third manifold delivers high-pressure gas through a series of transfer apertures to the second manifold periodically along the entire length of the second manifold. A series of air admission apertures along the second manifold allow air to pass into the gas in the second manifold under the influence of aspiration.

Description

gated hollow n. One of the g raw hile the gas and air mixture pilot or low-heat -pressure gas through a d manifold periodically series of air igh 2,613,737 10/1952 Schwietert.....
3,051,464 8/1962 Yeo et al.
Primary Examiner-Carroll B. Dority, Jr.
AttorneyRobert M. Dunning ABSTRACT: A gas burner formed from an elon extrusion having three manifolds formed therei manifolds comprises a high-pressure manifold deliverin gas through a series of apertures to the main flame w second manifold delivers a combustible through a second series of apertures to the flame. The third manifold delivers h series of transfer apertures to the secon along the entire length of the second manifold. A
admission apertures along the second manifold allow air to pass into the gas in the second manifold under the influence of aspiration.
r. c E
III/111111111, A
Richard N. Weatherston Saint Paul Minn. 5.166 Jan. 23, 1970 Patented July 13, 1971 Weather-Rite Manufacturing County of Ramsey, Minn.
References Cited UNITED STATES PATENTS 6/1906 lnventor Appl. No.
Filed Assignee 5 Claims, 2 Drawing Figs.
United States Patent [54] GASBURNERS [50] FieldofSearch...
PATENT'EU Jun 319?! lhh INVENTOR R/CHARD /V. WEATHERSTO/V ATTORNEY GAS BURNERS BACKGROUND OF THE INVENTION Recently, improved gas burners have been designed which employ extruded hollow manifolds to carry the gas and support the flame. Such burners may be formed from aluminum and therefore are lighter and less expensive. Furthermore, the size and capacity of the burner can be controlled simply by cutting the extrusion to the desired length rather than altering expensive castings or using a number of separate castings or burners. This new type of extruded burner is shown and described in copending US. Pat. application Ser. No. 779,671 filed Nov. 29, I968, and invented BY Richard Weatherston.
Briefly, the new extruded gas burners described in the above-referenced copending application are formed with an internal partition dividing them into two elongated parallel manifolds each having a series of spaced apertures therein which apertures face the confess-tion area. Regulated relatively highpressure gas is introduced into one of the manifolds which passes out of the apertures and generates a large main flame for the main heating function. The second manifold receives a mixture of gas and air under a relatively low-pressure which serves to generate a small pilot flame for low heating requirements and for igniting the main flame. Experience has pointed up a number of difficulties inherent in this design especially in longer versions of the burner which to date have been made as long as l2 feet. The low-pressure manifold tends to have a more stable flame near the end at which the gas-air mixture is introduced than at the more distant end. Due to the gradual loss of pressure along the length of the pilot manifold and the inconsistent mixing of air and gas afforded by a single mixing device the flame characteristics along the manifold change. This uneven flame along the length of the burner produces uneven heating over the length of the burner with a number of consequent disadvantages. Since the burner depends wholly or partly on the pilot flame for low-level heating the heat output of the burner is uneven over its length. Another difficulty is that the large volume of air and gas mixture necessary to supply a long pilot manifold requires a complicated and expensive air and gas mixing device. The novel design of the present invention avoids the above described problems.
SUMMARY OF THE INVENTION Briefly, the present invention contemplates using an elongated extrusion with three elongated parallel manifolds formed therein. Two of the manifolds supply the main flame and the pilot flame apertures while the third manifold accepts high-pressure gas which is transferred to the pilot flame manifold through a series of periodic apertures along the length of the pilot manifold. The gas, thus, enters the pilot manifold at the same pressure everywhere along the entire length of the pilot manifold alleviating the uneven flame problem. In addition, another set of air admission apertures are formed in the outside wall of the pilot manifold adjacent the transfer apertures in a one-to-one relationship so that the high-pressure gas passing form the third manifold to the pilot manifold will aspirate air along with it from the air admission apertures automatically so as to eliminate the need for the expensive and complicated prior art air-gas mixing apparatus. Thus, it may be seen that it is an object of the present invention to provide an improved gas burner. It is a further object of the present invention to provide a gas burner in which an even pilot flame is supported over the total length of the burner and in which air is automatically aspirated over the length of the pilot manifold. Further objects and advantages will become apparent upon reference to the following description and drawings.
BRIEF DESCRIPTION OF THE DRAWING FIG. 1 is a partially cutaway perspective view of the main elements of the present inventive gas burner.
FIG. 2 is a cross-sectional view of the burner assembly of FIG. 1 in which the improved extruded manifold is shown in greater detail.
DESCRIPTION OF THE PREFERRED EMBODIMENT In FIG. 1 a portion of a burner compartment 10 is shown partially cutaway so as to provide a better view of the burner assembly 12 mounted in compartment 10. Burner assembly 12 comprises an extruded hollow member 14, upper and lower plates 16 and 18, end plates 20 and 22 and a pair of diverging foraminous plates 24 and 26. Foraminous plates 26 and 26 define a combustion area between them where air mixes with gas emerging from a series of holes 30 in member 14. Holes 30 connect with the large manifold 31 inside member 14 which manifold receives gas from a regulated source through a pipe 32. End plates such as plate 34 in FIG. 1 serve to close the ends of the manifolds in hollow member 14. As gas enters through pipe 32, manifold 31, and holes 30, air enters burner compartment 10 from the rear in FIG. 1. Some of the air passes into the rear of the burner assembly between plates l6, 18, 20, and 22 and through foraminous diverging plates 24 and 26 into the combustion area. Initially, the mixture is ignited by a spark plug or other suitable igniting device 36. After initial ignition, however, the flame is maintained by a pilot flame from a second series of holes 38 which connect with a second manifold 40. Manifol-i 40 receives gas from a pipe 44 through a third manifold 42". The unique operation of the pilot flame manifold 40 may be better inderstood with reference to FIG. 2.
In FIG. 2, burner assembly 12 is shown in section. In order to prevent an inordinate pressure drop along the length of manifold 40, high-pressure gas is introduced into manifold 42 which extends the full length of member 14 generally parallel to manifold 40. Manifold 42 connects with manifold 40 by means of a series of transfer apertures 46. Apertures 46 are relatively small so that the gas metered into manifold 40 at a slow predetermined rate. In the preferred embodiment apertures 46 are formed by a no. 44 drill and spaced at approximately 24 -inch intervals. This has been found to yield a pressure in manifold 40 which. although relatively low, is consistent along the entire length of manifold 40 so that when the gas passes out of manifold 40 through a series of pilot holes 38 the flame characteristics are similar along the entire length of r' nifold 4.0. Even, predictable, low-level heating is thus achieved as discussed earlier.
In order to eliminate the need for an expensive, complicated air-gas mixing apparatus to supply the pilot flame as in the past, a series of air admission holes 50 are provided in the bottom of manifold 40. Even predictable, low-level heating is thus achieved as discussed earlier.
In order to eliminate the need for an expensive, complicated air-gas mixing apparatus to supply the pilot flame as in the past, a series of air admission holes 50 are provided in the bottom of manifold 40. One hole 50 is provided adjacent each transfer aperture 46. The high-velocity gas entering through aperture 46 sucks air through hole 50 into manifold 4 by means of aspiration. This flow of air mixes with the gas from aperture 46 and continues on out through pilot apertures 38 assisted by the low-pressure area which exists between foraminous plates 24 and 26 when the flame is burning in the combustion area between plates 24 and 26. Holes 50 have been made approximately one-half inch in diameter in the preferred embodiment which size has been found to provide the proper air-to-gas ratio for proper combustion.
It may be seen that the size of the furnace can be varied simply by varying the length of extrusion 14. Since the gas is supplied equally along the length of the burner and since air is aspirated equally along the length of the burner any length may be chosen for the burner without adjustments to any of the gas or air supply apparatus. Furthermore, an even flame is produced over the length of the chosen burner due to the constant pressure characteristics along the pilot manifold.
Transfer apertures 46 may be drilledthrough the pilot flame holes 38 if desired but in the preferred embodiment separate access holes 52 are provided in manifold 42 opposite transfer holes 46. Holes 46 may be drilled through access holes 52 and, in addition, transfer holes 46 may be conveniently cleaned by means of access holes 52. In operation, access holes 52 are plugged by means of small sealing screws 54 to prevent escape of the gas.
I claim:
1. A gas burner comprising in combination:
an elongated hollow extrusion having a front side facing the combustion area with two sets of longitudinally spaced outlet apertures therein;
partitions in said extrusion dividing the interior of the extrusion into first, second, and third longitudinally extending manifolds, said first manifold in communication with one of said sets of outlet apertures and said second manifold in communication with the other set of outlet apertures; means closing the ends of said manifolds;
means for supplying pressurized gas to said first manifold and said third manifold; and
a series of spaced transfer apertures between said third and second manifolds sized and spaced to admit gas to said second manifold at a controlled rate.
2. The apparatus of claim 1 including a series of air admission apertures in said second manifold sized to pass air at a rate dependent on the flow of gas through said transfer apertures.
3. The apparatus of claim 2 in which said air admission apertures comprise a series of holes positioned one each next to the transfer apertures so that the flow of gas through said transfer apertures aspirates air into said second manifold through said air admission apertures.
4. The apparatus of claim 3 in which said extrusion has a generally rectangular cross section with said first and second manifolds positioned along said front side.
5. The apparatus of claim 4 in which said gas-supplying means comprise a pair of inlet pipes connected to said first and third manifolds whereby gas pressure in one of the manifolds may differ from the gas pressure in the other manifold.

Claims (5)

1. A gas burner comprising in combination: an elongated hollow extrusion having a front side facing the combustion area with two sets of longitudinally spaced outlet apertures therein; partitions in said extrusion dividing the interior of the extrusion into first, second, and third longitudinally extending manifolds, said first manifold in communication with one of said sets of outlet apertures and said second manifold in communication with the other set of outlet apertures; means closing the ends of said manifolds; means for supplying pressurized gas to said first manifold and said third manifold; and a series of spaced transfer apertures between said third and second manifolds sized and spaced to admit gas to said second manifold at a controlled rate.
2. The apparatus of claim 1 including a series of air admission apertures in said second manifold sized to pass air at a rate dependent on the flow of gas through said transfer apertures.
3. The apparatus of claim 2 in which said air admission apertures comprise a series of holes positioned one each next to the transfer apertures so that the flow of gas through said transfer apertures aspirates air into said second manifold through said air admission apertures.
4. The apparatus of claim 3 in which said extrusion has a generally rectangular cross section with said first and second manifolds positioned along said front side.
5. The apparatus of claim 4 in which said gas-supplying means comprise a pair of inlet pipes connected to said first and third manifolds whereby gas pressure in one of the manifolds may differ from the gas pressure in the other manifold.
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4523905A (en) * 1983-07-21 1985-06-18 Nu-Way Energy Limited Burner for gaseous fuels
US4573907A (en) * 1984-11-07 1986-03-04 Maxon Corporation Low oxygen and low pressure drop burner
US4610626A (en) * 1983-06-23 1986-09-09 Matsushita Electric Industrial Co., Ltd. High load gas combustion apparatus
US4737100A (en) * 1986-04-30 1988-04-12 John Zink Company Duct burner apparatus
US4869665A (en) * 1987-04-01 1989-09-26 Maxon Corporation Carbon monoxide reducing endplate apparatus
US4963089A (en) * 1989-08-24 1990-10-16 Eclipse, Inc. High turndown burner with integral pilot
US20040101797A1 (en) * 2002-11-27 2004-05-27 Pawel Mosiewicz Direct gas-fired burner assembly with two-stage combustion
US10260742B2 (en) * 2012-06-22 2019-04-16 Ferndale Investments Pty Ltd Heating torch

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US822932A (en) * 1905-05-03 1906-06-12 Frank L Golding Burner for gas-ranges.
US1580995A (en) * 1924-10-31 1926-04-13 William P Capps Gas burner
US2613737A (en) * 1950-12-09 1952-10-14 Schwietert Gustav Oil burner nozzle
US3051464A (en) * 1958-10-20 1962-08-28 Maxon Premix Burner Company Air-heating gas burner

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US822932A (en) * 1905-05-03 1906-06-12 Frank L Golding Burner for gas-ranges.
US1580995A (en) * 1924-10-31 1926-04-13 William P Capps Gas burner
US2613737A (en) * 1950-12-09 1952-10-14 Schwietert Gustav Oil burner nozzle
US3051464A (en) * 1958-10-20 1962-08-28 Maxon Premix Burner Company Air-heating gas burner

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4610626A (en) * 1983-06-23 1986-09-09 Matsushita Electric Industrial Co., Ltd. High load gas combustion apparatus
US4523905A (en) * 1983-07-21 1985-06-18 Nu-Way Energy Limited Burner for gaseous fuels
US4573907A (en) * 1984-11-07 1986-03-04 Maxon Corporation Low oxygen and low pressure drop burner
US4737100A (en) * 1986-04-30 1988-04-12 John Zink Company Duct burner apparatus
US4869665A (en) * 1987-04-01 1989-09-26 Maxon Corporation Carbon monoxide reducing endplate apparatus
US4963089A (en) * 1989-08-24 1990-10-16 Eclipse, Inc. High turndown burner with integral pilot
US20040101797A1 (en) * 2002-11-27 2004-05-27 Pawel Mosiewicz Direct gas-fired burner assembly with two-stage combustion
US7481650B2 (en) * 2002-11-27 2009-01-27 Midco International, Inc. Direct gas-fired burner assembly with two-stage combustion
US10260742B2 (en) * 2012-06-22 2019-04-16 Ferndale Investments Pty Ltd Heating torch

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