AU631391B2

AU631391B2 – High efficiency linear gas burner assembly
– Google Patents

AU631391B2 – High efficiency linear gas burner assembly
– Google Patents
High efficiency linear gas burner assembly

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Publication number
AU631391B2

AU631391B2
AU47629/90A
AU4762990A
AU631391B2
AU 631391 B2
AU631391 B2
AU 631391B2
AU 47629/90 A
AU47629/90 A
AU 47629/90A
AU 4762990 A
AU4762990 A
AU 4762990A
AU 631391 B2
AU631391 B2
AU 631391B2
Authority
AU
Australia
Prior art keywords
burner
plate
apertures
air
chamber
Prior art date
1989-01-10
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.)

Ceased

Application number
AU47629/90A
Other versions

AU4762990A
(en

Inventor
Willie H. Best
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.)

Haden Schweitzer Corp

Original Assignee
Haden Schweitzer 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.)
1989-01-10
Filing date
1990-01-03
Publication date
1992-11-26

1990-01-03
Application filed by Haden Schweitzer Corp
filed
Critical
Haden Schweitzer Corp

1990-07-19
Publication of AU4762990A
publication
Critical
patent/AU4762990A/en

1992-01-23
Assigned to HADEN SCHWEITZER CORPORATION
reassignment
HADEN SCHWEITZER CORPORATION
Alteration of Name(s) of Applicant(s) under S113
Assignors: BEST, WILLIE H.

1992-11-26
Application granted
granted
Critical

1992-11-26
Publication of AU631391B2
publication
Critical
patent/AU631391B2/en

2010-01-03
Anticipated expiration
legal-status
Critical

Status
Ceased
legal-status
Critical
Current

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Classifications

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES

F23D—BURNERS

F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid

F23D14/46—Details, e.g. noise reduction means

F23D14/48—Nozzles

F23D14/58—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES

F23D—BURNERS

F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid

F23D14/34—Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES

F23D—BURNERS

F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid

F23D14/46—Details, e.g. noise reduction means

F23D14/62—Mixing devices; Mixing tubes

F23D14/64—Mixing devices; Mixing tubes with injectors

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES

F23D—BURNERS

F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid

F23D14/46—Details, e.g. noise reduction means

F23D14/72—Safety devices, e.g. operative in case of failure of gas supply

F23D14/82—Preventing flashback or blowback

Description

BACKGROUND OF THE INVENTION 1. Field of the invention This invention relates to a linear-type burner assembly capable of discharging uniform heat over a long span, and is more particularly concerned with a burner assembly that has high combustion efficiency and requires minimum excess air for combustion. The burner assembly’s design will not allow flame retrogression through the burner apertures, even under extreme operating conditions, which normally would have resulted in flashback in the mixture manifold. The burner can be operated at any angle around its longitudinal axis, while maintaining stable combustion.
2. Description of the Prior Art There are many types of gas burners used in industrial heat processing, including packaged burners, air stream burners (make-up air type) and line burners. With the exception of line burners, most industrial type burners are rated at 500,000 BTUH or higher. For the present intended use of these types of burners, it is usually advantageous to keep the maximum input as high as practical and still achieve complete combustion. In most oven applications, a recirculating air system is used to distribute the heat energy from these high BTUH burners to the oven environment. In other words, in most burners of today’s technology there is a concentrated discharge of energy and a 4250E -2means must be provided independently from the combustion air supply to the burner to uniformly distribute the energy.
An example of a present line burner is the LINOFLAME
M
gas burner manufactured by the Maxon Corporation. These burners utilize a gas/air manifold that is an integral part of the burner structure. The sections of these burners are intended to be assembled together therefxe., the total amount of the gas/air mixture required down-stream of any burner must pass through the manifold of that burner. Therefore, it is not practical to assemble these types of burners in lengths longer than 7 ft. to 10 ft. because of the high mixture velocity which would affect the distribution of the mixture passing through the first several burners of a series of burners. Beyond a length of 7 ft. to 10 ft., the burners need to be broken into separately fed, shorter lengths (connected by cross-ignition end plate sets) to minimize burner distortion and stresses during alternate heating and cooling cycles. Also, the line type burners of present day technology have to be carefully matched to the equipment supplying air/gas premixture.
There are other disadvantages associated with present-day line burners. First, most line burners employ a premixture of the gas and air, and therefore, if for some reason the flame retrogresses into the mixture manifold, a fire an explosion, referred to as flashback, could occur. The work by me leading to the development of the burner assembly of 4250E this invention has included the investigation of laminar and turbulent flame flashback in mixtures of methane and air and propane and air in high temperature environments (400°F to 1700 0 Many factors influence flashback in a nozzle or burner port. It has been shown that flashback can be controlled to a large extent simply by a cooling process. A method utilized by present line burners to reduce flashback is to use raised burner ports. If the surfaces of the raised ports are kept cool during the combustion process, the flame will not penetrate into the ports beyond a distance of a few millimeters corresponding to the heated zone of the port rim.
Also, the ratio of the interior diameter to the exterior diameter of the raised ports influences flashback. The dead space (the space between the flame base and the burner surface), the mixture temperature, and the fuel and air mixture ratio also affect flashback in methane/air or propane/air (gas/air) mixtures. While all of the above factors influence flashback, it is widely accepted, and has been demonstrated in studies 1 have conducted, that the critical boundary velocity gradient of the gas/air mixture is a primary controlling factor in flashback. When the gas/air mixture velocity exceeds the flame velocity as it exits the burner port or aperture, the flame has a lifting tendency. When the gas/air mixture velocity is less than the rate of flame propagation, then the flame has a tendency to retrogress down the port or aperture.
In a premix-type burner, this retrogression could cause 4250E 9 I ignition within the burner body or the manifold. The burner assembly of the present invention provides a method of controlling the air/gas mixture velocity gradient, which controls lift-off of the flame and eliminates flashback through a wide range of percentages of stoichiometric combustion, gas/air mixture temperatures and turndown. Further, in most embodiments of this invention, the gas and air are not premixed in a combustible ratio at a mixture temperature above approximately 800 0
F.
In the case of line burners employing present technology, the input (BTUH) per linear foot might be decreased to the approximate energy requirement per foot of oven length, but there are other limitations in the use of conventional line burners when the total length exceeds 7 to 10 feet. As the mixture velocity increases through the body of the burner housing, the distribution of the gas/air mixture is affected, resulting in non-uniform burning. A further limitation of these line burners is that when long burner sections are interconnected, the burners have a tendency to arc or bow due to thermal expansion. These burners are further limited in that they are sensitive to the gas/air ratio.
The limitations of the present day line burners, and also of packaged-type burners, necessarily limits the performance of industrial ovens which utilize such burners.
For example, I have developed the High Heat Transfer Oven of U.S. Patent No. 4,235,023, the Radiant Wall Oven and Process of 4250E
A
Drying Coated Objects of U.S. Patent No. 4,546,S-3′, and the C f0 iN-t A 5″t -onvn-t4i-n.Stabilizied Radiant Oven (AirRadiant'» Oven) of U.S.
Patent No. 4,785,552. In the radiant-type ovens, conventional packaged-type burners have been employed, which release the energy of combustion in a rather confined space. Methods utilizing fans for distributing this energy are employed, which in one form or another distributes uniform heated air to the backside of the emitter walls. In the High Heat Transfer Oven, the mass movement of the air from the fans distributes the heat from the individual packaged burners well, but multiple burners and manifolds are required based upon the length of the High Heat Transfer Oven, which additional equipment increases the oven’s cost.
While the designs described by these patents have proven to be highly efficient in maintaining uniform temperature on the surfaces of a vehicle or other objects passing through the respective oven, fans are required to distribute the heated air over the inner side of the emitter surfaces of the Radiant Wall and AirRadiant'» ovens, and burners are usually required in the High Heat Transfer Oven. A desirable and beneficial improvement in these ovens could result if the heat of combustion could be distributed over the inner emitter wall surface without the requirement of fans. Also, multiple burners could be eliminated in the High Transfer Oven if the heat of combustion could be uniformly discharged throughout the oven length.
4250E -6r_ i The development of the burner assembly of the present invention provides a method by which heat can be transferred to the emitter walls in ovens described by U.S. Patent No.
4,546,553 and U.S. Patent No. 4,785,552, without the requirement of circulating fans in heater houses or within the internal cavity of the Radiant Wall module. Also, the burner assembly of the present invention can uniformly distribute the heat of combustion throughout the full length of a High Heat Transfer Oven. This burner assembly will have many other applications where it is desirable to release the energy of combustion over a long span, or where the temperature of the burner environment is highly elevated. While a present-day line burner has limitations as to the operational length, the burner of the present invention is capable of firing essentially any length of emitter wall or High Heat Transfer Oven. The limiting factor of length would not be because of distribution of the gas or air, or based upon thermal expansion and contraction problems, but based upon the time required for the flame to carry from the point of ignition to the other end of the burner. The burner assembly (burner) of the present invention overcomes these limitations and other problems that now exist with conventional line burners, and provides additional operational benefits, disclosed herein.
4250E 7 -8- SUMMARY OF THE INVENTION In one broad form the present invention provides a burner assembly for burning a combustible mixture of air and fluid, comprising: a pair of opposed inner and outer plates, each of which is provided with perimeters defining spaced apertures through which said mixture passes, the mixture flowing first through the apertures of the inner plate, then between said plates, then moving past the perimeters of the apertures of said outer plate and into the apertures of said outer plates; manifold means for introducing said mixture to the apertures of said inner plate; said plates being spaced a distance apart such that the mixture passing from between said plates and emerging from the apertures of said outer plate flows at a velocity, said distance being less than one-fourth of the diameter of one of said apertures of said outer pl.he; whereby said velocity of said mixture passing adjacent the perimeter defining each aperture in said outer plate is sufficient to prevent retrogression of the flame through the apertures of said outer plate.
9 Another broad form of the present invention provides a burner assembly comprising: a burner housing defining an interior chamber and an opening communicating with said chamber; a pair of juxtapose plates over said opening, one of said plates being an inner plate and the other of said plates being an outer plate extending over said inner plate, said outer plate being provided with a plurality of spaced burner ports therein, each of the burner ports having a perimeter, said inner plate being provided with a plurality of spaced apertures which are offset from said burner ports sufficiently that no portions of said burner ports is aligned with any portion of said apertures, the distance between the inner plate and the outer plate being less than one-fourth of the diameter of one of said burner ports; supply means for introducing air and a fluid into said chamber under sufficient pressure to provide a positive pressure in said chamber to cause the air and fluid to flow through said apertures and between said plates and past said perimeters of said burner ports at a radial velocity and through said burner ports at an axial velocity; and whereby the radial velocity of said air and fluid past the perimeters of the burner ports is greater than the axial velocity of the air and fluid through the burner ports.
10 A still further broad form of the present invention provides a burner assembly comprising: a pair of plates disposed closely adjacent to each other for defining therebetween a chamber, one of said plates being an outer plate provided with a plurality of burner ports at spaced locations, the burner ports having perimeters, the distance between the pair of plates being less than one-fourth of the diameter of one of said burner ports; means for introducing a fluid fuel under pressure into said chamber for movement at a velocity between said plates and out of said ports for providing flames burning at or adjacent to each of said ports; and said plates being sufficiently close together so that velocity of said fluid fuel around the perimeters of said burner ports is greater than the exit velocity so that retrogression of said flames into said chamber is prevented.
ml 11 A yet further broad form of the present invention provides a burner assembly for creating a flame by burning a combustible fluid comprising a burner plate provided with a plurality of spaced burner porters having perimeters, an inner plate disposed beneath each of said burner ports and extending laterally beyond the perimeters of said burner ports, said inner plate spaced from said burner plate a distance of less than one-fourth of a maximum distance across one of the burner ports; and fluid supply means for delivering the combustible fluid between said burner plate and said inner plate and radially past said perimeters of said burner ports and axially through the burner ports; whereby said inner plate is sufficiently close to said burner plate that said radial velocity of said fluid is greater than said axial velocity of said fluid to prevent such flame from retrogressing between the burner plate and the inner plate.
12 12 Another further broad form of the present invention provides a gas burner assembly comprising: a burner housing having a chamber therein; means for supplying a combustible gas under pressure to said chamber; and juxtaposed outer and inner, laterally extending plates disposed over said chamber, each said plates having offset apertures respectively in said plates, the offset of said apertures being sufficient that no portion of either of said apertures is in alignment with any portion of the other of said apertures, said plates being spaced from each other sufficiently for said combustible gas to pass from said chamber through the apertures of said inner plate, thence laterally between said plates at a first velocity and, thereafter, outwardly through said apertures of said outer plate at a second velocity for producing flames adjacent said apertures when the gas passing outwardly through said apertures of said outer plate is lighted, said plates being sufficiently close to each other that the first velocity of the gas around the perimeter of said apertures of said outer plate is greater than said second velocity to prevent retrogression of said flames into said chamber; wherein the distance between said outer and inner plates is less than one-fourth of a maximum distance across one of said apertures of said outer plate.
13 Yet another broad form of the present invention provides a process of burning fuel to produce heat, comprising: disposing a first plate and a second plate adjacent to each other to define therebetween a first chamber, each plate having spaced apertures therethrough which are misaligned with the holes of the other plate and have diameters; the distance between the first plate and the second plate being less than one-fourth of the diameter of one of said apertures of the second plate; passing a combustible fuel through the apertures of the first plate and into said first chamber under sufficient pressure that said fuel moves at a first velocity laterally in said chamber away from the apertures of said first plate and toward and through the apertures of the second plate for emerging at a second velocity from said apertures of said second plate: controlling the first velocity of said fuel in said chamber around said perimeters of said apertures of said second plate so that the first velocity of the fuel around the perimeters of said apertures of said second plate is greater than said second velocity of said fuel emerging from said apertures of the second plate; and igniting the fuel emerging from said apertures of said second plate.
14 It would be desirable to provide an improved or alternative gas burner which overcomes or alleviates one or more of the problems or disadvantages of the prior art devices.
15 Other features and advantages of the present invention will become apparent from the following description when taken in conjunction with the accompanying drawings, wherein like characters of reference designate corresponding parts through the several views.
DESCRIPTION OF THE DRAWINGS Figure 1 is a perspective view of the preferred embodiment of the present invention.
Figure 2 is a fragmentary plan view of the embodiment of Figure 1.
Figure 3 is a transverse cross-section taken along lines 3-3 of Figure 2.
Figure 4 is a longitudinal cross-section taken along lines 4-4 of Figure 2.
Figure 5 is a diagramatic, fragmentary perspective of a portion of the burner plates of Figure 3.
Figure 6 is a transverse cross-section of an alternate embodiment of the present invention.
Figure 7 is a transverse cross-section of another alternate embodiment of the present invention.
Figure 8 is a side view of still another embodiment of the present invention.
4250E -16- II I 16a Figure 9 is a cross-sectional end view taken along lines 9-9 of Figure 8.
I
I
iss an end view of the embodiment f FiguLe 8.
Figure 10 is a transverse cross-section of another embodiment of the present invention.
Figure 11 is a vertical sectional view of still another embodiment of the present invention in which raw gas is burned.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring now in detail to the embodiments chosen for the purpose of illustrating the present invention, numeral of Fig. 1 depicts generally a burner assembly having mixture manifold assembly 11 which includes an elongated, longitudinal extending, horizontally disposed channel-shaped manifold housing 9 which has a bottom wall 12, and a pair of opposed upstanding side walls 13. The ends of the manifold housing 9 are closed by end walls, such as wall 26. The upper edges of the side walls 13 and end walls, such as end wall 26 are provided with upwardly protruding flanges, such as flange 14, which form a perimeter in a horizontal plane, parallel to and above the bottom wall 12. The-.top plate 15 is provided with two, parallel outer rows of longitudinally spaced apertures 17 and a central row of longitudinally spaced apertures 16. Below the central row of apertures 16 and within the confines of the manifold housing 9 is a gas duct or gas manifold 18 which 4250E -17- I_ _1 41IP- 18 extends longitudinally, substantially throughout the length of :nanifold housing 9. The upper wall 20 of the gas manifold 18 is provided with a plurality of spaced orifices 19 which are respectively aligned vertically with the gas apertures 16. Each gas orifice 19 is provided with a gas restricting means such as a gas restricting means 7 which is externally threaded, defines orifice 8 therethrough and is provided with a hexagonal head so that it can be threadedly received in the gas orifice 19. By changing the size of the gas restricting means 7, the amount of gas passing through the restricting means 7 can be changed, as desired.
A centrifugal blower 27 is mounted on the end wall 26 of the manifold housing 9 so as to discharge air into the air chamber 24 of the manifold housing 9, to provide a source of air through the burner assembly 10. This blower 27 can be mounted externally of housing 9 for feeding air from an external source to appropriate ducts through the manifold housing, if desired.
Mounted over each of the restricting means 7 and extending upwardly from the upper wall 20 of the gas manifold 18, are a plurality of venturi tubes or mixing tubes 21, these mixing tubes 21 respectively ;.ommunicating at their upper ends with the gas apertures 16 in the plate 15. In an intermediate portion of each of the venturi tubes 21 are orifices or openings 22. The venturi 21 also serve the function of supporting the gas duct or gas manifold 18.
Gas manifold 18, venturi 21 and plate 15 are arranged as depicted in Fig. 3, and are preferably welded together, but can be joined by any common means well known in the art to 1 -m6~ s~ -ri~ allow for the flow of gas from manifold 18 through orifices 19 and 16. Although tube 21 can be in the shape of a venturi with air orifices 22 at the throat 23, tube 21 can also be cylindrical, having opposed apertures, and still achieve its desired function, as is detailed later. The communication of these elements, therefore, results in air supply chamber 24 which contains air under pressure and which is separated from the’ gas contained in gas manifold 18 and mixing tubes 21. When gas is directed through the restricting means 7, it entrains and mixes with the air passing into tubes 21 via orifices 22.
The gas line fittings (not shown), including gas intake fittings and end cap of gas manifold 18, and the mounting elements of centrifugal fan 27 to wall 26 are well know in the art and not further described herein.
Supported by plate 15 is air manifold or plenum 28 having upstanding.a U-shaped or channel-shaped outer housing 29 which includes bottom wall 30 and side walls 31 that terminate in laterally extending flange532. Bottom wall 30 defines air apertures 33 which are aligned with and are smaller in diameter than air apertures 17 of plate 15. The smaller apertures 33 in the wall 30 register with air apertures 17 in the top plate et~k.e–ma.n-i- 94-d- 15 so that the small apertures 33 define the size for the proper air flow to plenum 28. The diameter of dpertures 33 can be decreased, thereby decreasing air flow through apertures 33, by inserting a thin washer or apertured plate (not shown) between top plate 15 and bottom wall 4250E -19- Wall 30 also defines a centrally disposed longitudinal row of spaced orifices 34 which communicate respectively with apertures 16. Air manifold 28 also includes upstanding, U-shaped or channel-shaped inner housing 35 with bottom wall 36 and opposed upstanding side walls 37 that terminate in laterally extending flanges 38. Flanges 32 support flanges 38 so that the opposed inner walls 37 are spaced inwardly from outer wall529, and wall 36 is spaced from wall 30, as shown in Fig. 3, to form air plenum or chamber 39, closed at both ends.
Flanges 32 and 38 can a-t4ite-r- be welded or riveted for permanent mounting, or can be secured by bolts or other releasable means, as desired. Wall 36 defines a plurality of spaced central apertures 40 which are respectively aligned with orifices 34. Tubes 41 respectively surround orifices 34 and e-Q’e.
welded to walls 30 and 36 to connect apertures 34 and 40, and thus, define passageways 42, therebetween. Along the upper portion of inner walls 37 on each side of air manifold 28 are spaced, combustion air ports or secondary air discharge ports 43. Spaced secondary air discharge ports 43 are provided in opposed relationship along the entire length of inner walls 37.
Supported on bottom wall 36 of housing 35 is burner housing 44. Burner housing 44 comprises bottom wall 45 that defines longitudinally spaced central orifices 46, which are respectively in alignment with apertures 40. Tubes 41 extend to wall 45 and also are welded at their upper ends to wall the periphery of orifices 46. Housing 44 also includes 4250E GopFGesedupstanding side walls 47 and end walls (not shown) which terminate at their upper ends in inwardly opening, U-shaped retaining perimeteral frame 48. Baffles 49 are attached to the upper side of wall 45 and are mounted so that an apex 50 of a baffle 49 extends across each of the orifices 46 and curved arms 51 extend in the longitudinal direction of housing 44, as shown in Fig. 4.
Received in retaining frames 48 are two juxtaposed, rectangular, spaced, flat, metal, parallel plates, lower plate 52 and upper plate or burner plate 53. Plates 52 and 53 are held in spaced relationship by spacers S, which are preferably located along each side of plates 52 and 53. Plates 52 and 53 therefore, are held in parallel, spaced relationship along their entire lengths. The perimeteral frames 48 retain the two plates 52 and 53 closing the open upper end of housing 44.
When the plates 52 and 53 are heated, they expand into the frames 48 and when they cool, they retract partially from the frames 48.
As best shown in Fig. 5, plate 52 is provided with a pair of longitudinally extending rows of equally spaced apertures 54, therethrough. Plate 53 defines two rows of apertures or burner ports 55. Similarly, apertures 54 and are staggered, or offset in relation to one another so that gas or the gas/air mixture entering apertures 54 must travel in the chamber 56 between plates 52 and 53 before entering apertures 55. The plates 52 and 53 are opposed, 4250E -21juxtaposed, flat, parallel, elongated, rectangular, metal members which are preferably made from between about 20 gauge I CiOL 1 tA, r\m and about 11 gauge stainless steel sheets with a distance between centers of the burner ports 55 being about 1/2 inch, and the distance between centers of the apertures 54 of about 1 inch so that the inner plate 52 has about one half of the number of apertures 54 as there are ports 55 in plate 53.
The space or wafer-thin chamber 56 between plates 52 and 53 has horizontal dimension Y and vertical dimension X.
While dimension Y is fixed or constant and cannot be adjusted for a particular burner, dimension X can be varied by utilizing different sized spacers S.
Mounted between housing 44 and wall 3-1 are elongate, upwardly extending air baffles 57, which terminates in lateral deflectors 58, that extend inwardly.
In Fig. 3, secondary air manifold 28 and the mixture &hc i manifold assembly 11 are secured together by mounting brackets 59, bolts 60 and nuts 61. It is obvious, however, that manifold assembly 11 and manifold 28 can be joined by any desired means such as clamps or other releasable means. A gasket (not shown) can be placed between plate 15 and wall Because of the low air pressure at orifices 17, usually less than 1.5 inches water column, and the low pressure of the gas/air mixture in tube 41, however, it is not absolutely necessary to incorporate such a gasket, as long as plate 15 and wall 30 fit together correctly.
4250E -22- The input gas pressure in duct 18 can be selectively modulated using any conventional gas valve means (not shown) well known in the art. Similarly, the air pressure in chamber 24 can be selectively modulated by controlling centrifugal blower 27, as is also well known in the art.
In operation, gas is delivered through gas manifold 18, venturi or mixing tubes 21 and into the burner chamber of burner housing 44. Simultaneously, blower 27 delivers air through air supply chamber 24 of manifold assembly 11. The air travels through apertures 17 and 33, and into secondary air chamber 39 of air plenum 28. For a fixed air pressure in the manifold assembly 11, the volume of combustion air supplied to ports 43 can be controlled by the diameter of the orifices 33.
To ensure distribution throughout the length of the air plenum 28, a pressure drop should be taken across orifices 33. The secondary air from plenum 28 passes through secondary air ports 43, and ultimately mixes with the gas/air mixture near the burner ports 55, for combustion. Baffles 57, which can be removed if desired, direct the air in a horizontal direction across the plate or burner surface 53, and prevents the direct impingement of air on surface 53, which could affect flame stability at low fire.
While the mixture manifold assembly 11 independently delivers the gas and air for combustion, a coitrolled amount of of gas and a portion of the combustion air which enters the burner housing 44 is accomplished in each venturi or 4250E -23mixing tube 21 leading from the gas manifold 18 to the burner housing 44. The amount of premixing of air with the gas is controlled by the size of the orifices 22 through the wall of mixing tube 21. The mixing tube 21 can be a venturi with the air passages located at the throat 23. Since orifices 22 of mixing tube 21 are exposed to the ir pressure within mixture manifold assem ly 11, an air flow will occur due to the pressure differential in manifold assembly 11 and mixing tube 21. However, with the air pressure in -he manifold assembly 11 remaining constant, the amount of air entrained increases as the velocity of the gas in mixing tube 21 increases. As the gas pressure is increased, a proportional amount of air is entrained in mixing tube 21 and ultimately into the burner housing 44. While a venturi-shaped tube probably entrains air more efficiently, the burner assembly 10 works well with the wall of the mixing tube 21 being cylindrical. Since the air supply to mixing tube 21 is under positive pressure, the venturi shape is not as important as would be the case if the air were being entrained from a space with no positive air pressure. The quantity of air rentering each mixing tube 21 is dependent on the air pressure in the manifold assembly 11, the total area of the orifices 22, and the effect of the entrainment action of the gas discharged from its orifice at increased velocities with gas pressure.
There is an advantage to having a fixed pressure of the air entering orifice 22. As the gas pressure is decreased, for a fixed diameter of orifice 22 the ratio of air to gas 4250E -24increases as the burner is modulated down, in the preferred embodiment. This occurs because there is a constant flow of air independently of the entrainment action of mixing tube 21.
Therefore, while the gas input is being decreased, the air supplied to mixing tube 21 does not decrease in the same proportion, and the air to gas ratio increases, improving the flame stability at low fire.
The gas/air mixture then enters burner housing 44 through tube 41. Baffles 49 uniformly distribute the gas/air mixture flow longitudinally within housing 44. The mixture then enters apertures 54′ of lower plate 52, and travels laterally in the thin chamber 56 between plates 52 and 53 and into apertures 55 of burner plate 53. Burner plate 53 constitutes the combustion or burner surface. The arrangement of plates 52 and 53 and offset apertures 54 and 55 operate to prevent any retrogression of the flame through apertures 55 and into the chamber 56 between plates 52 and 53. Flame retrogression, and subsequent backflash, is prevented by controlling the velocity of the gas/air mixture entering ports 55. Flame liftoff from plate 53, however, can be prevented by controlling the mixture velocity exiting ports The gas/air mixture enters ports 55 at a velocity based upon the perimeter of port 55 and the thickness of spacers S. The flow area of each port is equal to x (port 55 diameter) x (dimension The thickness of spacers S (dimension X) should always be less than port 55 diameter divided by 4250E The total flow area of the gas/air mixture, determined by the total perimeter of all ports 55 times the separation distance (dimension X) of the plates 52 and 53, produces a velocity at the perimeter entrance of ports 55 which exceeds the rate of flame propagation at the lowest operating input of burner assembly 10. While other factors previously discussed may affect the quenching of the flame, if the profile of the velocity gradient at this point is at all times maintained greater than the rate of flame propagation, retrogression of the flame is prevented. When these conditions are met, the burner assembly 10 is incapable of back flashing due to flame retrogression.
To assure flame stability, or a flame front which is established and burns for a fixed firing rate without pulsating or quenching, the total cross-sectional area of all the ports can be such that the discharge velocity at high fire can be equal, or nearly equal, to ther flame propagation. It is not essential to achieve burner stability, however, for the mixture velocity at the discharge of ports 55 to be absolutely less than the flamae propagation. Because of an immediate divergence of the gas/air mixture from the apertures 55, stable combustion can occur with the base of the flame established within a minute distance above apertures 55. While this dead space can also be a contributing factor in the prevention of flashback, this burner does not depend upon dead space to preclude flashback. The flow area of all of the ports 55 can be an amount that would create an exit velocity less than the rate of 4250E -26flame propagation, and flashback would still be precluded, because of the higher velocity of the gas/air mixture around the perimeter at the entrance of ports 55. While the gas/air mixture velocity from the discharge of ports 55 does not have to be greater than the rate of flame propagation, because of t:h flame quenching ability of the burner design, in practical applications the velocity from ports 55, except at low firing rates, is usually higher than the rate of flame propagation.
At a distance of 1/2 the diameter of port 55 from port surface 53, the diameter of the flow pattern of the mixture would be 2 times port 55 diameter, if the divergence angle were 450, which is reasonable from a thin orifice. This would obviously produce a cross-sectional area of the flow pattern of the mixture of 4 times the actual port 55 area. As an example, if por 55 diameter of .125 inches is selected, the area of port 55 would be .01227 inches square. But just 1/16 inch above port 55, the area of flow would be .04909 inch square, or 4 times graater than the area of port 55. It is desirable for a space of at least 1/16 of an inch to exist between the base of the flame and port surface 53 at the ma ,imim firing rate of the burner. Tests have demonstrated that when port 55 diameter of 1/2 the calculated diameter for flame contact with port is used, complete and stable combustion is achieved.
When computing the mixture velocities, the expansion of the mixture due to an increase in temperature has to be considered. This increase in temperature of the mixture will vary with the environment temperature in which burner assembly 4250E -27-
A
_I 1_ is operated, and is easily determined by tests or could be approximated by calculations involving heat transfer theory.
Also, the coefficient of discharge of the orifices must be considered in computing the orifice diameters. To satisfy pure academic interest, every theoretical fluid flow variable might be considered, but as a practical matter, the design of gas burners is not an exact science. If, in the design, flashback of the flame is absolutely precluded and burner assembly 10 can operate without excessive air to achieve complete combustion, the exact position of the base of the flame with reference to burner surface 53 is not critical in the burner assembly 10 of this invention. Therefore, there is latitude in determining the diameter of ports 55. In other words, the performance of burner assembly 10 is not affected by any observed amount if the flame base contacts burner surface 53, or is established above the surface 53, so long as the flame is stable and does not lift off to the extent that it is extinguished.
To attest to the flexibility of burner assembly 10, a test burner using forty-eight (48) ports in plate 53 per foot of burner assembly 10 length, with a diameter of .1250 inches, and twenty-four (24) ports 54 in plate 52 per foot of burner with a diameter of .1250 inches, and with a separation between the plates (dimension X) of .020 inch performs well within a range of maximum inputs of 20,000 BTU/hr./ft. to 40,000 BTU/hr,/ft., with a maximum manifold 28 air pressure of 1 inch Cf c\ tts -s of water column. Calculalti~snand tests have shown the 4250E -28- (dimension X) could be increased to .050 inch, and flashback of the burner would still be absolutely precluded.
In another test burner, the number of ports 54 contained in plate 52 was left at twenty-four (24) with a diameter of .1250 inch, and the number of ports 55 contained in plate 53 were left at forty-eight (48) but the diameter of ports 55 were increased to .250 inch, and still good test results were obtained. In summary, when burner assembly 10 is used to heat ovens of my prior inventions, the following is a range of dimensions of flow areas of the air and the air/gas mixture, along with a range of air and gas pressures, which result in stable flame without flame retrogression.
MIXING TUBE 21 DIAMETER TYPE MIXING TUBE 21 ORIFICES 22 OF MIXING TUBE AIR ORIFICES 33 NUMBER OF ORIFICES 54 52) NUMBER OF ORIFICES 55 (PLATE 53) SPACE BETWEEN PLATES (X DIMENSION) GAS PRESSURE
PRESSURE
TURNDOWN RATIO RANGE OF MAXIMUM INPUTS .5 to 1.25 inch (2 ft. of burner) Entrance 1.25 inch (2 ft. of burner) Throat .625 inch Discharge 1.25 inch .00 to .098 inch. (2 ft. of burner) .4375 to ,687) inch (2 ft. of burner) 12 to 14 with diameter .125 inch (ft./burner) 24 with diameter .125 to .250 inch (ft./burner) .020 to .050 inch .2 to 20 inch water column .4 to 1.5 inch water column 6 1 20,000 BTU/hr./ft. to 50,000 BTU/hr./ft.
4250E -29- 1 The pressure drop across the outer and inner plate depends on the velocity through the plates and therefore is dependent on orifice size and burner BTUH input. However, the range of this pressure drop would be about .002 inches water column to about .18 inches water column for the drop across burner ports 55 of the outer plate 53 and the range would be about .002 inches water column to about .36 inches water column for the apetures 54 of inner plate 52.
The above dimensions of burner assembly 10 orifices and pressures does not represent a limitation, but indicate a range of dimensions that have been demonstrated by,tests to work well in the appliciation for providing the heat source for ovens or my prior inventions. The pressure drop across inner plate 52 should not exceed .4 inch of water and the drop across outer plate 53 snould not exceed .2 inch of water, while the total pressure drop across both plates 52 and 53 should not exceed .6 inch of water. The thickness of plates 52 or 53 should be from about 0.010 inch to about 0.060 inch. The range diameters of apertures 54 and 55 can be from about 1/16 inch to about 1/4 inch.
The range of inputs tested are more than adequate for most oven requirements. As an example, if the total heat load of an oven 100′ in length were 3,000,000 BTU/hr., burner assembly 10 with, for example, a maximum input of 30,000 could be used. Ii burner assembly 10 were used on each side of the oven, the maximum input would be 6,000,000 BTU/hr. for heat up, and then burner assembly 10 would modulate down to its mid-range of 15,000 BTU/hr./ft., with a turndown ratio of 6 to 1. The burner assembly 10 could further modulate 4250E I Ri’ to a total input to the oven of 1,000,000 BTU/hr. to accomodate conveyor stoppage or a slowing of the process.
The burner assembly 10 is capable of maintaining complete combustion with a minimum of excess air (less than 512%). As discussed, An important feature of this invention is that control of the input can be accomplished through manipulation of a gas valve (not shown) to modulate the gas pressure, only. The air pressure for combustion need not be changed or reduced during turndown. This feature simplifies l0the control design and at the same time allows a constant pressure in the air manifold 28 that will ensure good distribution throughout the burner length. As the input to the burner 10 is turned down, since the discharge of air from ports 43 is constant, excess air is supplied to the burner 10 during If, i certain applications, excess air would detract from the operating efficiency of burner assembly the air supply can also be modulated to maintain a constant fuel/air ratio, which ensures minimum excess air at all operating inputs.
During normal operation of burner assembly 10 at or near its highest rated input, the base of the flame is established above burner plate 53 and under the flange 58 of baffle 57. The flame emerges around baffle 57, and the remaining air required for combustion is supplied through ports 2543. The mixing effect created by the geometry of the burner allows complete combustion to occur with a fairly short flame length.
4250E -31- I I i The input per foot of burner assembly 10 is determined by its application. For example, if it is determined that 98 feet of burner assembly 10 will be used on each side of an oven, to produce a total heat input to the oven of 5,880,000 BTU/hr. (or 30,000 BTU/hr./ft. of burner length after the heat transfer efficiency is taken into account), the burner assembly maximum input is established. The burner assembly 10 will be designed for a BTU/hr./ft. turndown ratio of 6 to 1. Tests have demonstrated that the burner assembly 10 can achieve stable and complete combustion at this turndown ratio.
The amount of air entrained for premixing in mixing tube 21 contained within the manifold 11 has been determined from experimentation. At best it is difficult to theoretically design a venturi or mixing tube 21 when the air pressure at the entrance to the venturi or mixing tube 21 is the same as the air pressure at the burner surface 53, However, when the air is at a higher pressure (even as low as 1 inch of water column), it would be almost impossible to predict theoretically the total air entrained. The -ei-amo-e-t of the air ports 22 contained in mixing tube 21 have been varied in test work from a total area of .00614 inches square to .098 inches square.
Actually, in the second embodiment of the burner assembly no air is introduced into mixing tube 21. But when it has been determined to use some premixture, the smallest orifices 22 into tube 21 for which tests have been conducted have been two 1/16 inch diameter apertures. In the range of burner input 4250E -32- 1 at high fire of 20,000 BTU/hr./ft. to 40,000 BTU/hr./ft., good results have been achieved with a total area of around .050 inches square for ports 22.
In the tests conducted on burner assembly 10 using an aperture 22 area of approximately .05 inches square in the throat 23 of mixing tube 21, with manifold assembly 11 air pressure between .5 inches and 1.5 inches water column to introduce air for premixing with the gas, the burner assembly operates in a stable condition with complete combustion.
Approximately 30% to 60% of the air for premixing is supplied under these conditions, and a greater ratio of the air for combustion is supplied as the input to the burner assembly is reduced, as previously explained.
In order to determine the air pressure required to supply the premixture air through orifice 22 and to determine the pressure drop through the burner orifices 55, the equation relating to pressure difference and velocity of gas through an orifice or aperture is utilized, as follows: i.
V 2sAP where: V Velocity (ft/sec) g Acceleration of gravity (32ft./sec 2 AP Pressure difference (Ibs/ft.
2 p Density of the fluid (Ibs/ft. 3 4250E -33r__ For the purpose of burner assembly design, it is more useful to express the units of pressure in inches of water column. The equation can then be written as follows: 2.
V 2qAP5.197 Combining constants: V 18.294 Where A P is expressed in inches of water column and all other units remain as in Equation 1. Replacing Density in the equation to allow for properties of mixture of gases (such as methane and air) with the universal gas equation for atmospheric pressure, the equation is rewritten as follows: 4.
V 18.294 A.P RT I P Vo For atmospheric pressure, since all calculations are based on 3 incompressible flow, and 1 ft. of air or mixture since density of Equation 1 was in lb./ft.3 V 18.294 AP RT (14.7) (144) (1) 4250E -34- Combining constants: 6.
where: V .3977 AP RT V Velocity (ft./sec) P Pressure difference (inches H 2
O)
R Gas constant T Temperature The gas constant R for any gas is the quctient obtained by dividing the universal gas constant by the molecular weight of the gas: 7.
R 1545′ m R Gas constant m Molecular weight of the gas In a mixture of gas, such as methane and air, the proportions are known or can be measured. The weighted average molecular weight (the apparent molecular weight) may be calculated, and a value of R obtained from R is equal to 1545/m to apply to the mixture. The molecular weight of methane is 16.043, and of propane is 44.097 and of air is 28.97. The gas constant R can be calculated for any mixture of air and methane, and of air and propane.
In order to determine the pressure drop across an orifice, Equation 6 can be rewritten in the following form.
4250E 8.
ALP V 2 .3977 RT or v 2 .3977 RT Where: P Pressure drop across an orifice or a series of orifices (inches of water) V =Velocity through the orifice or series of orifices R =Gas constant T Temperature (0 R) The above equations in combination with the simple equation of flow will enable most of the burner calculations to be performed.
V V)
(A)
V Vol. (ft /hr.) V Vel. (ft./hr.) A Area ft 2 The following calculations are exemplary of the design of a typical burner assembly Given: input to the burner assembly 10 on high fire is to be 30,000 BTUH/ft; orifice 22 in the mixing tube 21 is to be inches square, based on test; combustion air temperature is 150 0
F:
4250E -36-
I_
amount of pre-mix is 30% of theoretical air (stoichiometric air), based on test dead space above burner port 55 is to be 1/2 the poir 55 diameter; mixture divergence angle is 450; and combustion blower, 1 inch static pressure is to be used.
At high fire the ratio air/gas mixture will not exceed that at low fire, because of the constant pressure in the manifold assembly 11. Therefore, assuming the worst case condition that the ratio will remain constant, the total mixture volume will be: Gas 30 ft.3/hr.
premix 90 ft.
3 /hr.
Total mixture 120 ft 3 /hr.
The air required for combustion, the flame velocity of methane and the heating value of natural gas would either be known by one skilled in the art, or a reference on combustion could be Orifice 22 diameter in mixing tube 21 when air in chamber 39 is at 1 inch static Vel a .3977 AP RT .3977 (1)(53.3)(610) a 71.7 ft/sec 4250E -37gl Vol (Vel) (Area) (71.7ft./sec)(.000349ft 2 )(3600 sec/hr.) 90 ft.
3 /hr A reasonable C D (coefficient of discharge) for flange entry is Therefore: ft.
3 /hr.) 45 ft 3 /hr. (for two ft. burner) S 22.5 ft 3 /hr. (for one ft. burner) Correcting for density: S 22.5 19.1 ft.
3 /hr./ft, of burner assembly Since the input at low fire will be 5,000 BTUH, requiring 15 ft.3 air/ft. for 30% premix, 19.1 ft.3 of air would increase the dir ratio to 38%, which is on the safe side to preclude flashback if the calculations are made for premix.
At a flame velocity of 1.5 ft./sec, the velocity of the mixture at 1/2 the diameter of port 55 above the burner surface 53 should be less than 1.5ft./sec, at high fire.
Therefore: Area Vo Vel 3/hr. z 5400ft. /hr. 2 ,03034ft.
2 or 4.36 in 2 4250E -38- I L Using orifice 55 spacing of two rows on 1/2 inch centers for a total of 48 orifices: 436 .0908 in 2 (area above each orifice 48 at 1/2 the port diameter above the burner surface) Therefore: Area of orifice 55 in plate 53 .0908 ,02270 in 2 4 Use CD of .85 to obtain actual flow area A 02270 0 .0267 in 2 From a table of areas of circles select a diameter 3/16 inch which has an area of .02761 in 2 and a circumference of .58905 inch.
To determine the space between plates 52 and 53 to preclude flashback: Flow Area Vol, (at low fire) Flame velocity (ft./hr.) A Total u fice circumference x (dimention x) Total Circumferences (48) (.58905) 28.27 in.
Total Flow Volume at low fire 20ft.
3 /hr.
6 4250E -39r_ Therefore: (Dimension X) x 28.74 2.t 710 \5400 ft./hr 520 Dimension X 20 71 \5400 ft./hr. (2.395ft.) 520 .00211 ft.
.0253 in.
Computing velocity across plate 53 at high fire Velocity Vo.
Area [(120)(144) (48)(.02761)(3600) 520 4.945 ft./sec In computing the velocity across plate 52 based on tests, good results are obtained when 1/2 of the flow area is used in plate 1552 as plate 53. Therefore, the velocity through the orifices 54 of plate 52 will be 9.89 ft/sec.
Computing the pressure drop across plate 52: .3977 RT AP 9 2 (6 1 (32977 (60)(710) .0142 inch H 2 0 NOTE: R for the mixture was determined to be Computing the pressure drop across plate 53: AP 2 4 ,3977 (60)(710) S .00362 inch H 2 0 4250E I1
FL
Computing the velocity and pressure of all orifices 55 at high fire: drop around the perimeter Flow Area (28.74 in.) 144 029″A i n. .00504 ft.
2 velocity .00504 K 5 2 0 Oq( I 9 9.Oft/sec 2 37, (60) (710)/ .01120 inches H 2 0 ter of air orifice 17 for secondary air tion: Computing the diame required for combus Total Air 12% excess Total Air Primary Ai Secondary (3Oft.
3 gas)(l0ft, 3 air/ft.
3 gas) 300ft.
3 air/hr.
36 336ft 3 /hr.
r Air 246/ft.
3 /hr.
.3977 (53 (610) 71.7 ft./sec 258,120 ft/hr.
Y, Vei 258,1520) .O0lll7Et.
2 .16099 in.
2 per one ft. of burner assembly 4250E -1 -41-
I
Therefore, use two 29/64 inch diameter orifices for a 2ft.
burner assembly. The above calculations are intended only to exemplify the calculations required to determine the design variables discussed, such as orifice diameters and flow rates.
Those skilled in the art understand that there are various methods for determining these variables.
It should be understood that while the burner of this invention provides complete flexibility in controlling the gas/air mixture inlet and exit velocity to ports 55 in plate 53, it is not always necessary or desirable for the velocity of the gas/air mixture to be less than the rate of flame propagation at or very near the discharge of ports 55. In some applications, as an example when the burner is used to heat the radiating walls described by U.S. Patent No. 4,546,553 or U.S.
Patent No. 4,785,552, the flame base can be established slightly below the level of flange 58 of baffle 57, when the burner is operated at or near its highest rated capacity.
Therefore, the selection of the number and the diameter of the ports 55 in plate 53 controls where the base of the flame stabilizes with reference to plate 53, from virtually contacting plate 53 to a controlled dimension above plate 53.
One advantage in establishing the base of the flame above plate 53 during operation at high energy inputs is that plate 53 will remain cooler if it is not in direct contact with the base of the flame. Even if the base of the flame is established above 4250E -42plate 53 at a high firing rate, the flame base will move closer to or contact the plate during turndown. There are other applications, such as when the burner assembly 10 is operated at lower inputs, when better stability of the flame can be maintained if the base of the flame is in relatively close contact with plate 53.
The diameter of apertures 54 does not have to be the same as the diameter of ports 55. Nor does the number of ports or apertures 54 need to be the same as the number of ports To achieve the desired results produced by this burner assembly there only needs to be an offset between the center line of ports 55 and of ports 54, that prevents alignment of any open area of either ports 54 or 55. Tests have indicated that it is desirable in most instances that the total area of ports 54 in plate 52 be less than the total area of ports 55 in plate 53.
Tests have indicated that good results are achieved when the area of ports 54 are 1/2 of the area of ports 55. This provides for a greater pressure drop across plate 52, therefore, ensuring good distribution of the gas/air mixture through the ports 55 of plate 53.
The fact that the area of the ports 55 increases to the second power of the diameter, while the perimeter only increases to the first power, attributes to the benefit of the design. As a port 55 diameter is increased to provide, for a discharge area to decrease the velocity of discharge of the air/gas mixture, for a fixed space (dimension the 4250E -43entrance area to port 55 only increases as the square root of the ratio increase of the discharge area. In a conventional port-type line burner, it is obvious that as the diameter of the port is increased, the area of the entrance and exit of the port are equally affected. While the specific desired flame pattern may vary among applications of the burner assembly the important consideration of this invention is to be able to control the characteristics of the flame pattern. Experiments have been conducted with the diameter of ports 55 of plate 53 ranging from 1/8 inch to 3 inches, with equal success in eliminating backflashing and controlling flame liftoff. A primary advantage of a burner of this invention is that the flame length at high fire can be kept confined (less than 4 inches).
This burner assembly 10 also includes the ability to change the input BTUH by simply changing the orifice diameter 9It/and the diameter of the air orifice 17. The air pressure for combustion can also be changed in lieu of an air orifice 17 diameter change or in combination with the orifice 17 diameter change. This flexibility allows one common burner assembly to be rated at different maximum inputs without the need of a design change or a change in the size of burner assembly Tests have been conducted by me wherein the maximum input to the burner assembly 10 ranged from 20,000 BTUH/ft. to 60,000 ft. with complete and stable combustion throughout the operating range. The maximum input to burner assembly 10 can 4250E -44be changed after it is installed in an application. The eorifice 9can be changed by removing or-iiGe L9-with a socket wrench. If the requirement is to increase the maximum input, air orifice 17 also can be enlarged. If the requirement is to decrease the maximum input, then a spacer (not shown) containing a smaller opening can be inserted which will effectively decrease the air orifice 17 diameter.
Manifold assembly 11 can be made any length required for the application. It can also be designed in sections to be interconnected with companion flanges (not shown). The combustion air contained within manifold assembly 11 cools assembly 11 and also prevents the gas manifold 18 from becoming overheated when the burner is operated in an environment at a relatively high temperature, such as when the burner is used to directly heat the radiant wall described by U.S. Patent No. 4,546,553 or by U.S. Patent No. 4,785,552.
Manifold assembly 11 is mounted to its supporting surface by brackets 62 which are slotted to provide expansion for the manifold assembly 11. Burner housing 44 mounted to the manifold assembly 11 is allowed to expand and contract independently of manifold assembly 11, since burner housing 44 is connected to manifold assembly 11 near its center. A typical mounting center distance would be 24 inches, with the burner housing 44 lengths slightly less than 24 inches to provide an expansion space between burner housings 44 arranged end to end.
4250E Tests have indicated that reliable and consistent carry-over of the flame from one burner assembly 10 to the next burner assembly 10 exists. For safety reasons, the flame is proven and monitored using conventional flame sensing technology. In a typicial application, an end burner assembly would be ignited with an electrically generated spark or pilot, and the flame on that burner assembly 10 would be sensed and monitored using conventional flame sensing components. If it can be demonstrated that there is consistent carry-over in a continuous length burner, most safety codes do not require that the opposite end of burner assembly 2-1 be monitored. However, if it were desired or required by the circumstances to not only monitor the initial burner assembly 10 on which ignition occurred, but monitor also the last burner assembly in a series of burners assemblies to ensure that carry-over was absolutely complete to all burner assemblies, a second flame monitoring system could be placed on the last burner assembly. Because of the delay in the flame carry-over from the initial burner assembly which was ignited to the last burner assembly, it +i-1-4usually be necessary to use some type of timer to delay the energizing of the second flame sensing system.
A second embodiment of the present invention is illustrated in Fig. 6. In this embodiment, the burner assembly is identical to the assembly previously described, except that in manifold assembly 11, the air orifices 22 in mixing tube 21 are eliminated. Therefore, only gas is delivered 4250E -46through tube 21 tc burner housing 44. Air is delivered under pressure through orifices 17 to upper air manifold 28, where all the air for combustion is supplied through ports 43. This embodiment of burner assembly 10 is employed when assembly must operate in environments of extremely high temperature, and auto-ignition of the gas (regardless of the mixture ratio) could occur if any oxygen were present in the burner housing 44. Since, however, all combustion air is supplied by ports 43 at the point of burning, it is impossible for ignition of the gas to occur within the burner housing 44. When nozzle mixing is used, the burner has operated successfully during tests when the combustion surface was exposed to an environment in which the ambient temperature was 1700°F.
Fig. 7 illustrates a third embodiment of the present invention. Burner assembly 110 is mounted to a mixture manifold assembly, (shown in fragmentary portion) which is identical in structure and function to manifold assembly 11 described in the second embodiment. Assembly 110 includes air manifold 128 having upstanding, U-shaped outer housing 129 which includes bottom wall 130 and side walls 131 that terminate in laterally extending flanges 132. Bottom wall 130 defines air apertures 133 which communicate with air apertures 1-6 of the mixture manifold assembly, Wall 130 also defines centrally disposed orifice 134 which communicates with the central gas aperture LJ-opf the mixture manifold assembly. Air manifold 128 also includes upstanding, U-shaped inner housing 4250E -47- 2 135 with bottom wall. 136 and side walls 137 that terminate in inwardly extending U-shaped retaining flange 138. Flange 132 supports flange 138 so that inner wall 137 i.s spaced from outer wall 131, and wall 136 is spaced from wall 130, as shown in Fig. 7, to form air chamber 139. Flanges 132 and 138 can either be secured by threaded bolts 160 and nuts 161 or other releasable means, or can be welded or riveted for permanent mounting, as desired. Wall 136 defines central aperture 140 which is aligned with an orifice 134. Tube 141 is welded to walls 130 and 136 around the periphery of apertures 134 and 140, to define passageway 142 therebetween. Along the upper portion of inner wall 137 on each side of air manifold 128 are spaced, air ports 143. Spaced ports 143 extend along the entire lengthsof inner walls 137.
Received in retaining flanges 138 are two, spaced, parallel plates, lower plate 162 and upper plate 163. Plates 162 and 163 are held in spaced relationship by spacers 164, which are preferably placed along each side of plates 162 and 163. Plates 162 and 163 therefore, are held in parallel, spaced relationship along their entire lengths, and retained within air manifold 128 within flanges 138.
Plate 162 defines a series of apertures 165 therethrough. Similarly, plate 163 defines apertures or burner ports 166. Apertures 165 and 166 are staggered, or offset in relation to one another so that gas or the gas/air mixture entering apertures 165 must travel laterally between plates 162 and 163 before entering apertures 166, 4250E -48- The space or chamber between plates 162 and 163, denoted generally as numeral 167, has a horizontal dimension Y and vertical dimension X (not shown), identically as illustrated in Fig. 5 regarding the first embodiment. While dimension Y is fixed or constant and cannot be adjusted for a particular burner, dimension X can be varied by utilizing different sized spacers 164.
Supported on bottom wall 136 of housing 135 is gas housing 144. Gas housing 144 comprises bottom wall 145 that defines central orifice 146, which is in alignment with aperture 140. Tube 141 extends to wall 145 and also is welded at its upper end wall 145 around the periphery of orifice 146.
Housing 144 also includes elongate side walls 147 which terminate at their upper ends in inwardly directed, U-shaped retaining flanges 148. Baffle 149 is attached to the upper side of wall 145 and is mounted so that the apex 150 (not shown) extends across orifice 146 and curved arms 151 (not shown) extend in the lateral direction of housing 144.
Received in retaining flanges 148 are two, spaced, parallel plates, lower plate 152 and upper plate 153. Plates 152 and 153 are held in spaced relationship by spacers S, which are preferably placed along each side of plates 152 and 153.
Plates 152 and 152 therefore, are held in parallel, spaced relationship along their entire lengths, and retained within burner housing 144 within flanges 148, and so define space 167A therebetween.
4250E -49- 50 Plate 152 defines a series of apertures 154 therethrough, and plate 153 defines apertures 155.
Apertures 154 and 155 are staggered, or offset in relation to one another sc that gas entering apertures 154 must travel laterally between plates 152 and 153 before entering apertures 155. As seen in Fig. 7, the cooperation of the above-described elements defines mixing chamber 168.
In operation, gas only is delivered to gas housing 144, and air is delivered to air manifold 128 from the mixture manifold assembly, identically as that described in the second embodiment. The gas enters gas housing 144 and is laterally distributed by baffle 149.
The gas then passes through apertures 154, between plates 152 and 153 and through apertures 155. Plate 153, however, does not constitute the burner surface in this embodiment. Plates 152 and 153 serve to distribute gas evenly over the surface of plate 153. Orifices 154 are usually less in total number and in diameter than orifices 155. Therefore, the gas is evenly distributed between plates 152 and 153, and emerges from orifice 155 uniformly over the total area of plate 153.
Air enters through orifices 133 into air chamber 139. All of the air for combustion is then discharged into the mixing chamber 168 through orifices 143, where the air mixes with the gas that enters the mixing chamber 168 through orifices 155. If desired, partial premixing of the gas and air can occur in chamber 168 with the remaining air required for
_A
1 combustion provided as secondary air from the atmosphere of the environment in which the burner is located. The gas/air mixture enters space 167 through orifices 165, then flows parallel to plates 162 and 163 and into orifices 166. The mixture velocity entering orifices 166 is controlled by the diameter of orifice 166, which dictates its perimeter, and by the space 167 between the plates 162 and 163. The velocity of the gas/air mixture entering orifice 166 around their perimeters is always greater than the rate of flame propagation, therefore back flashing is precluded as in the prior embodiments. Plate 163 constitutes the combustion surface of the burner 110.
By increasing the diameter of orifices 166, the area increases as the square of the diameter, while the perimeter only increases to the first power of the diameter. Therefore, as the diameter of orifice 166 is increased, the area to control flame liftoff is increased at a greater rate than the perimeter, in order to control flashback. Any predetermined space 167 between plates 162 and 163 to control flashback for a specific diameter of apertures 166, will also control flashback as the diameter of orifice 166 is increased, if the flow of gas/air mixture is increased proportionally to the diameter, The total port or orifice discharge area is determined by the number and diameter of ports 166. An area is used that will result in stable and complete combustion for the operating range of the burner. Since no additional secondary air may be 4250E -51- 7 required for combustion beyond the burner surface 163, as is the case of the burner assemblies previously described, it is usually necessary that the total port area of ports 166 be such that the velocity of the gas/air mixture emerging from ports 166 not be much greater than the rate of flame propagation in order to ensure against flame liftoff. The basic concept of the invention, that is, the ability to control the inlet velocity to the discharge port 166 independently of the outlet velocity, is extremely important in this configuration of the burner because a combustible mixture is present in chamber 168. By ensuring that the mixture velocity is greater than the flame propagation at all operating conditions at the entrance to orifices 166, backflashing of the flame into chamber 168 can always be precluded, so long as the temperature of plate 163 stays below the ignition temperature of the gas/air mixture.
Burner assembly 110 requires the modulation of both the gas and air to maintain nearly a constant gas/air ratio through the turndown range. The determination of sizes and numbers of apertures and other design variables is as previously discussed.
In a fourth embodiment, illustrated in Figs, 8 and 9, the burner assembly 210 includes a burner housing 244 which is identical in structure and function to housing 44 in Fig, 3.
The primary air for cnmbustion is entrained by the venturi 221 the air/gas mixture is delivered to housing 244. Assembly 2II includes gas manifold or gas line 218, threaded pipe ‘1250E «52- 1 1’2 fitting assembly 212 engaged thereto, and venturi assembly 221, which is secured at one end to bottom wall 245 of housing 244.
The free end of venturi assembly 221 is in spaced alignment with assembly 212, as illustrated in Fig. 8. A venturi arrangement such as described herein is well known to those skilled in the art, and other known such arrangements will perform satisfactorily, Gas is supplied by line 218 to orifice 222 of assembly 212. The gas is then directed by venturi 221 to housing 244. The primary air for combustion is entrained by the action of venturi 221. The air and gas are mixed while in venturi 221, and are discharged into the burner housing 244. A distribution baffle 249 uniformly distributes Lhe gas/ai.
mixture into housing 244, As in the previous embodiments, parallel platos 252 and 253 containing nonaligned poits 254 and 255 provide the basis for precluding backflashing and flame retrogression. The gas/aix mixture enters orifice 254 and then flows parallel to the surfaces and between the plates 252 and 253. The air/gas mixture then enters orifices 255 around their perimeters, As in the previous embodiments, backflashing is precluded by controlling the inlet velocity around t’he orifice 255 and selecting a diameter kind number of orifices or ports 255 to provide a dischargo area~ such that the discharge velocity of the mixture of air and gas from ports 2.55 can control flame liftoff to a point. that,. ensures stable combustion throughout the operaling rango of the burner.
In this embodiment, the need for an air manifold such as manifold 28 is eliminated. However, the environment in which the burner assembly 210 is operated must contain oxygen for combustion. Burner assembly 210 could be used in conjunction with incineration, when the atmosphere surrounding burner assembly 210 is essentially a normal atmosphere containing 20% oxygen, but also contains small amounts of volatile organic compounds. Since 100% of the air for combustion is supplied from the surrounding atmosphere, burner assembly 210 is capable of using all of the energy of combustion to heat the air of the surrounding atmosphere, as opposed to requiring its combustion air to be externally supplied.
Where flame length does not impose a restriction to the Oesign, burner assembly 210 can be operated as a raw gas burner with all of the air for combustion supplied as secondary air fromte-, environment. As shown in phantom lines in Fig. 8, the venturi assembly 221 is eliminated, and a straight gas line 156 connects bottom wall 245 of housing 244, and fitting assembly 212, Therefore, gas, only, flows into housing 244, Tests have indicated that complete combustion can be obtained with secondary air only if the combustion space is sufficiently large to allow complete combustion without the flame impinging on any cool surfaces that would have a quenching effect on the flame.
41250E -54- I A fifth embodiment of the present invention is illustrated in Fig. 10. A burner assembly 310 includes U-shaped mixture manifold assembly 311, having bottom wall 312 and upstanding, side walls 313 terminating in laterally extending flange 314. Plate 315, defining centrally disposed orifice 316, is supported on flanges 314. A tube 322 is welded at its upper end to the bottom side of plate 315 around the periphery of orifice 316, as shown in Fig. 10. Tube 322 includes cylindrical side wall 317 and bottom wall 318.
Disposed in bottom wall 318 is threaded mixture restricting member 319 defining orifice 320 therein. Mounted on plate 315 is burner housing 344, which is identical in structure and function to burner housing 44 previously described.
In this embodiment, gas and air are mixed in desired ratio by any common, commercial gas/air mixing device. A premixture of gas/air is supplied to the burner housing 344 through manifold assembly 311. The mixture of gas and air passes through orifice 320 into tube 322, In order to ensure even distribution to all burners attached to manifold assembly 311, a pressure drop of the gas/air mixture is taken across orifice 320, and the mixture is then diffused in tube 322 for entering burner housing 344 through orifice 316. The commercially available gas/air mixers are designed to maintain the proper &iye/air ratio throughout the turndown range of burner assembly 310. Once the gas/air mixture enters burner housing 344, it is distributed between plates 352 and 353 and 4250E I -_I their associated apertures, as previously described with regard to burner housing 44.
More than 20 burner models have been tested employing various combinations of diameters and number of apertures in the plates. In order for the perimeter area to be less than the cross-sectional area of the orifice in the upper plate, for example in the first embodiment orifices 55 in plate 53, the space between the parallel plates must be 7.ess than .25 timr9 the diameter of the discharge orifice. By experiment, it has been determined that consistent quenching of the flame occurs when the perimeter velocity of the mixture into the discharge port is always greater than 1.2ft. per second. This is consistent with other studies conducted on flame quenching of mixtures of methane and propane in air. While the space between the parallel plates only needs to be sufficiently thin to affect an area that will ensure a mixture velocity greater than the flame velocity, experiments indicate the thickness of the space between the parallel plates does not need to be greater than .050 in. with burner port diameters up to .750 in. For small diameters of orifices in the burner surface plate, the space between the plates would have to be decreased, and on some of the experimental burners on which tests have been conducted, excellent results have been achieved by using a separation distance between the parallel plates of ,020 in.
When the burner is used in conjunction with direct heating of the radiant walls described by U.S. Patent No.
4250E -56r_ il II 4,546,533 and U.S. Patent No. 4,785,552, it is desirable to incinearate the exhaust from the oven. This can be accomplished by using the exhaus>’ air from the oven to provide the secondary air for combustion. If venturis were used to provide the initial premix for eemfnsaupi-n/ then both the primary and secondary air could be supplied from within the chamber in which the burner is located. In this manner, if exhaust gases were being incinerated, the exhaust gases would make up both the primary and secondary air for combustion. The exhaust air is supplied to the combustion cavity on the inner side of the radiant emitter at a level that will allow good mixing for combustion. Under this operating conditioin, an exhaust fan (not shown) would be used to exhaust the products of combustion from the combustion zone which would place the combustion space under negative pressure and allow the exhaust air from the oven to be pulled into the eembu-st-i4-i-n zone.
Proper controls would ensure that the oven exhaust would remain above incineration temperature of approximately 1250°F for a dwell time of approximately .7 seconds. These conditions will ensure the minimum temperature required for auto ignition of the volatile organic compounds in the exhaust air.
The turndown ratio of the burner assembly 10 when the gas, only, is modulated, is in the order of 6 to 1, which is sufficient in most applications of burner assembly However, a greater range of turndown can be accomplished through modulation or partial modulation of the air along with 4250E -57the gas. If the air is modulated, the lowest air pressure should not be less than would be required to maintain good distribution in the manifold assembly 11. Also, in an application where the products of combustion are to be vented, it could improve the heat transfer efficiency by modulation of the combustion air in combination with the gas, in order to prevent excess air in the products of combustion at low input.
As previously discussed, the burner assembly 10 does not require an extensive amount of excess air for efficient and complete combustion, and therefore, air not required for the combustion process would lower the heat transfer efficiency in a vented a-pfi-a-4_it-.by increasing the losses attributed to the flue products. In the cases where the oven or heat transfer process directly utilizes the products of combustion, then efficiency is not affected because the combustion air is usually always less than the make-up air required for the process. Again, since the burner assembly 10 is not sensitive Lo the fe,/’air ratio, it provides flexibility in its appliciation for achieving maximum heat transfer efficiency, but allows the use of simple controls by modulating the gas pressure only when heat transfer efficiency is not a consideration.
Most embodiments of the burner assembly 10 of this invention can operate in an oxygen-free atmosphere. Tests have been conducted within an atmosphere primarily consisting of nitrogen aAd CO 2 Under these extreme operating conditions 4250E -58-
[II
with all of the oxygen for combustion being supplied from the mixture manifold assembly 11 and no oxygen available for combustion from the surrounding environment, the carbon monoxide in the products of combustion has been measured to be less than 200 parts per million. The CO 2 in the products of combustion has ranged as high as 11% when burning methane gas, while the CO continued to remain less than 200 parts per million. These tests indicate the capability of the burner assembly 10 to maintain complete combustion without excess air and without the requirement for combustion air that is not supplied through mixture manifold assembly 11. This feature allows burner assembly 10 to operate within a chamber or environment in which all of the oxygen is replaced by carbon dioxide.
The heat transfer efficiency through the radiant wall of my prior art patent No. 4,546,553 has been measured to be greater than 88% when the burner of this invention is used for the heat source. Additionally, the burner assembly 10 can be rotated 3600 around the longitudinal axis to any position, with good burner operation.
It will further be obvious to those skilled in the art that many variations may be made in the above embodiments here chosen for the purpose of illustrating the present invention, and full result may be had to the doctrine of equivalents without departing from the scope of the present invention, as defined by the appended claims.
4250E -59i j

Claims (25)

1. A burner assembly for burning a combustible mixture of air and iluid, comprising: a pair of opposed inner and outer plates, each of which is provided with perimecers defining spaced apertures through which said mixture passes, the mixture flowing first through the apertures of the inner plate, then between said plates, then moving past the perimeters of the apertures of said outer plate and into the apertures of said outer plates; manifold means for introducing said mixture to the apertures of said inner plate; said plates being spaced a distance apart such that the mixture passing from between said plates and emerging from the apertures of said outer plate flows at a velocity, said distance being less than one-fourth of the diameter of one of said apertures of said outer plate; whereby said velocity of said mixture passing adjacent the perimeter defining each aperture in said outer plate is sufficient to prevent retrogression of the flame through the apertures of said outer plate.

2. The burner assembly defined in Claim 1, wherein said apertures are from about 1/16 inch (l.6mm) to about 1/4 inch (6.4mm) in diameter.

3. The burner assembly defined in Claim i, wherein the thickness of each of said plates is between about 0.010 inch and about 0.060 inch. 61

4. The burner assembly defined in Claim 1, wherein the pressure drop of said mixture through the apertures of said inner plate is less than 0.4 inch of water. The burner assembly defined in Claim i, wherein the pressure drop of said mixture across both said inner plate and said outer plate is less than 0.6 inch of water.

6. The burner assembly defined in Claim 1, wherein said apertures in said first plates are offset from said apertures in said second plate.

7. A burner assembly comprising: a burner housing defining an interior chamber and an opening communicating with said chamber; a pair of juxtaposed plates over said opening, one of said plates being an inner plate and the other of said plates being an outer plate extending over said inner plate, said outer plate being provided with a plurality of spaced burner ports therein, each of the burner ports having a perimeter, said inner plate being provided with a plurality of spaced apertures which are offset from said burner ports sufficiently that no portions of said burner ports is aligned with any portion of said apertures, the distance between the inner plate and the outer plate being less than one-fourt,. r the diameter of one of said burner ports; supply means for introducing air and a fluid into said chamber under sufficient pressure to provide a positive pressure in said chamber to cause the air and fluid to flow through said apertures and between said plates and past said perimeters of said burner ports at a radial velocity and through said burner ports at an axial velocity; and 62 whereby the radial velocity of said air and fluid past the perimeters of the burner ports is greater than the axial velocity of the air and fluid through the burner ports.

8. A burner assembly comprising: a pair of plates disposed closely adjacent to each other for defining therebetween a chamber, one of said plates being an outer plate provided with a plurality of burner ports at spaced locations, the burner ports having perimeters, the distance between the pair of plates being less than one-fourth of the diameter of one of said burner ports; means for introducing a fluid fuel under pressure into said chamber for movement at a velocity between said plates and out of said ports for providing flames burning at or adjacent to each of said ports; and said plates being sufficiently close together so that velocity of said fluid fuel around the perimeters of said burner ports is greater than the exit velocity so that retrogression of said flames into said chamber is prevented.

9. The burner assembly defined in Claim 8, wherein said plates are flat, elongated, metal members disposed parallel to each other.

10. The burner assembly defined in claim 8, wherein said fluid is aa gas fuel and including means for mixing air with said gas fuel prior to the time that said gas fuel is introduced into said chamber.

11. The burner assembly defined in claim 8, wherein said other of said plates is an inner plate, said means for introducing fluid fuel into said chamber including a burner housing adjacent to said inner plate, said burner housing and said inner plate defining a second chamber within said housing, and said inner plate being provided with a plurality of apertures which are offset from said burner ports, said fuel being fed into said second chamber and thence through said apertures into the first-mentioned chamber and, thereafter, laterally in said first mentioned chamber for exiting through burner ports.

12. The burner assembly defined in claim 11 including an air plenum into which air under pressure is introduced, and means for directing air from said air plenum into said second for admixing with said fuel. 4 250E -63-

13. The burner assembly defined in claim 12 wherein said means for directing air into said second chamber includes fuel conduct means for directing the flow of fuel to said second chamber and means for admixing air with said fuel as said fuel flows toward said second chamber. 14, The burner assembly defined in claim 12, wherein said means for admixing air with said fuel includes orifices intermediate the ends of said conduit means and said air plenum surrounding said conduit means for permitting air to pass from said air plenum into said conduit means. The burner assembly defined in claim 10, wherein said air plenum is disposed on opposite sides of said outer plate, said air plenum having holes in opposed relationship to each other for feeding air from opposite sides of said outer plate over the surface of said outer plate.

16. The burner assembly defined in Claim 8, wherein said outer plate is a flat elongated member and wherein said burner ports are equally spaced in alignment throughout substantially the length of said outer plate, 4250E I

17. The burner assembly defined in Claim 8, wherein said outer plate is an elongated flat rectangular metal sheet and wherein said burner ports are arranged in parallel rows extending throughout substantially the length of said outer plate, said rows being spaced inwardly from the opposite edges of said outer plate.

18. The burner assembly defined in Claim 8, wherein said inner plate is provided with a plurality of apertures extending along the length of said inner plate, and wherein said burner ports are arranged in a longitudinal row which is laterally spaced from said apetures, the fuel being introduced to said apertures in said inner plate.

19. The burner assembly defined in Claim 8, wherein said apertures are arranged in parallel rows along the length of said inner plate, said burner ports being arranged in parallel rows which are disposed inwardly of the rows of apertures in said inner plate. 4250E 66 A burner assembly for creating a flame by burning a combustible fluid comprising a burner plate provided with a plurality of spaced burner porters having perimeters, an inner plate disposed beneath each of said burner ports and extending laterally beyond the perimeters of said burner ports, said inner plate spaced from said burner plate a distance of less than one-fourth of a maximum distance across one of the burner ports; and fluid supply means for delivering the combustible fluid between said burner plate and said inner plate and radially past said perimeters of said burner ports and axially through the burner ports; whereby said inner plate is sufficiently close to said burner plate that said radial velocity of said fluid is greater than said axial velocity of said fluid to prevent such flame from retrogressing between the burner plate and the inner plate.

21. A gas burner assembly comprising: a burner housing having a chamber therein; means for supplying a combustible gas under pressure to said chamber; and juxtaposed outer and inner, laterally extending plates disposed over said chamber, each said plates having offset apertures respectively in said plates, the offset of said apertures being sufficient that no portion of either of said apertures is in alignment with any portion of the other of said apertures, said plates being spaced from each other sufficiently for said combustible gas to pass from said chamber through the apertures of said inner plate, thence laterally between said plates at a first velocity and, thereafter, outwardly through said apertures of said outer plate at a second velocity for producing flames adjacent said apertures when the gas passing outwardly through said apertures of said outer plate is lighted, said plates being sufficiently close to each other that the first velocity of the gas around the 67 perimeter of said apertures of said outer plate is greater than said second velocity to prevent retrogression of said flames into said chamber; wherein the distance between said outer and inner plates is less than one-fourth of a maximum distance across one of said apertures of said outer plate.

22. Process of burning fuel to produce heat, comprising: disposing a first plate and a second plate adjacent to each other to define therebetween a first chamber, each plate having spaced apertures therethrough which are misaligned with the holes of the other plate and have diameters; the distance between the first plate and the second plate being less than one-fourth of the diameter of one of said apertures of the second plate; passing a combustible fuel through the apertures of the first plate and into said first chamber under sufficient pressure that said fuel moves at a first velocity laterally in said chamber away from the apertures of said first plate and toward and through the apertures of the second plate for emerging at a second velocity from said apertures of said second plate: controlling the first velocity of said fuel in said chamber around said perimeters of said apertures of said second plate so that the first velocity of the fuel around the perimeters of said apertures of said second plate is greater than said second velocity of said fuel emerging from said apertures of the second plate; and igniting the fuel emerging from said apertures of said second plate.

23. The process defined in claim 22 including mixing air with said fuel, prior to the time that said fuel is passed through the apertures of one plate and into said chamber.

24. The process defined in claim 22, wherein said fuel is gas and including providing a second chamber adjacent to a side of said one plate opposite to said their chamber, and passing air and said gas under pressure into said second chamber, prior to the time that said gas is passed through the apertures of one plate and into said first their chamber. The process defined in claim 24 including the step of directing secondary air under pressure toward said apertures 4.n said other of said plates for admixing the secondary air with the combustible gas/air mixture emerging from said apertures of said other plate.

26. The process defined in claim 25 in which said air is introduced from opposite sides of said apertures of said other plate and is directed inwardly toward the paths of the gas emerging from the holes of said other plate.

27. The process defined in claim 26 including the step of introducing additional air into said gas.

28. The process defined in claim 23 including varying the rate of flow of said fuel while maintaining the rate of flow of said air at a constant to thereby increase and decrease the yield of said burner. 4250E -68- 69

29. The process defined in claim 22 including disposing a second chamber adjacent to said one of said plates, introducing air into said second chamber, mixing air from said second chamber into said fuel passing into the first-mentioned chamber for producing a combustible mixture within said first-mentioned chamber. The process defined in claim 29 including the step of disposing a third chamber adjacent to but spaced from said second chamber and providing a communication between said second chamber and said third chamber for the passage of air to the fuel passing into said second chamber.

31. A burner assembly as hereinbefore described with reference to the accompanying drawings. DATED this 22 day of September 1992 HADEN SCHWEITZER CORPORATION Patent Attorneys for the Applicant: F.B. RICE CO.

AU47629/90A
1989-01-10
1990-01-03
High efficiency linear gas burner assembly

Ceased

AU631391B2
(en)

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US29526489A

1989-01-10
1989-01-10

US295264

1989-01-10

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1990-07-19

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1992-11-26

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AU47629/90A
Ceased

AU631391B2
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1989-01-10
1990-01-03
High efficiency linear gas burner assembly

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Improvements relating to gas burners

US4082497A
(en)

*

1976-03-29
1978-04-04

Ex-Cell-O Corporation

High capacity quiet burner for hot air heating system

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Panel-type gas burner

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Gaseous fuel burner

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Gas burners

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Radiant burner

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Gas burner especially useful for glazing glassware

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(en)

*

1974-11-29
1976-06-01
Toto Ltd

GASUBAANAA

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1976-02-23
1977-08-02
Mcgettrick Charles A
Infrared energy generator with orifice plate

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*

1978-06-16
1993-04-13

Radiant wall oven and process of drying coated objects

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1978-06-16
1980-11-25
Best Willie H
High heat transfer oven

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(en)

*

1983-06-30
1985-05-30
Всесоюзный Научно-Исследовательский И Экспериментально-Конструкторский Институт Торгового Машиностроения
Air heater gas burner

JPS6298110A
(en)

*

1985-10-24
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Tokyo Gas Co Ltd
High load combustion method and device thereof

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1985-11-06
1989-11-10
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BLOW AIR GAS BURNER

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Ruhrgas Ag, 4300 Essen, De

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1986-08-22
1990-08-17
Osaka Gas Co Ltd

GAS BURNER

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1992-03-15
Ruhrgas Ag

GAS BURNER.

1989

1989-12-13
CA
CA002005415A
patent/CA2005415C/en
not_active
Expired – Fee Related

1989-12-15
NZ
NZ231801A
patent/NZ231801A/en
unknown

1990

1990-01-03
AU
AU47629/90A
patent/AU631391B2/en
not_active
Ceased

1990-01-05
DK
DK90200046.2T
patent/DK0378272T3/en
active

1990-01-05
ES
ES90200046T
patent/ES2059983T3/en
not_active
Expired – Lifetime

1990-01-05
EP
EP90200046A
patent/EP0378272B1/en
not_active
Expired – Lifetime

1990-01-05
DE
DE69010697T
patent/DE69010697T2/en
not_active
Expired – Fee Related

1990-01-10
JP
JP2001657A
patent/JPH02263006A/en
not_active
Withdrawn

1991

1991-01-24
US
US07/647,173
patent/US5062788A/en
not_active
Expired – Lifetime

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Publication number
Priority date
Publication date
Assignee
Title

GB1133292A
(en)

*

1966-04-06
1968-11-13
Krieger Kurt
Improvements relating to gas burners

US4082497A
(en)

*

1976-03-29
1978-04-04
Ex-Cell-O Corporation
High capacity quiet burner for hot air heating system

Also Published As

Publication number
Publication date

JPH02263006A
(en)

1990-10-25

AU4762990A
(en)

1990-07-19

EP0378272A3
(en)

1991-09-11

NZ231801A
(en)

1992-12-23

US5062788A
(en)

1991-11-05

DE69010697T2
(en)

1995-02-02

DK0378272T3
(en)

1994-08-22

DE69010697D1
(en)

1994-08-25

EP0378272A2
(en)

1990-07-18

ES2059983T3
(en)

1994-11-16

CA2005415A1
(en)

1990-07-10

CA2005415C
(en)

1994-03-01

EP0378272B1
(en)

1994-07-20

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