US2368370A - Gas burner - Google Patents
Gas burner Download PDFInfo
- Publication number
- US2368370A US2368370A US488797A US48879743A US2368370A US 2368370 A US2368370 A US 2368370A US 488797 A US488797 A US 488797A US 48879743 A US48879743 A US 48879743A US 2368370 A US2368370 A US 2368370A
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- Prior art keywords
- burner
- ports
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- casing
- gas
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- 238000010304 firing Methods 0.000 description 14
- 239000000203 mixture Substances 0.000 description 10
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 8
- 238000009434 installation Methods 0.000 description 8
- 238000002485 combustion reaction Methods 0.000 description 5
- 238000013021 overheating Methods 0.000 description 4
- 238000005192 partition Methods 0.000 description 4
- MFRCZYUUKMFJQJ-UHFFFAOYSA-N 1,4-dioxane-2,5-dione;1,3-dioxan-2-one Chemical compound O=C1OCCCO1.O=C1COC(=O)CO1 MFRCZYUUKMFJQJ-UHFFFAOYSA-N 0.000 description 3
- 241000196324 Embryophyta Species 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 238000002791 soaking Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 238000005496 tempering Methods 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 235000003197 Byrsonima crassifolia Nutrition 0.000 description 1
- 240000001546 Byrsonima crassifolia Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 210000000481 breast Anatomy 0.000 description 1
- 239000011449 brick Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011872 intimate mixture Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
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
Definitions
- the burner system must have a sufficiently large maximum capacity to provide adequate speed of heat input for initially 'bringing the charge of metal pieces to be treated, up to desired control temperature.
- the burner system must have a sufficiently low minimum capacity to prevent overheating* after the control temperature will have been' reached. Such conditions may require a minimum firing rate as low as one eighth of the maximum burner .capacity (particularly when the charge of metal pieces is held inthe furnace for a soaking period of several hours after the desired temperature will have been reached). ⁇ Under conditions as above indicated, it is understood that the lburner system must have a turn down range of 8 to 1. That is to say, there must be an 8 to 1 ratio between' the maximum and the minimum ring rates. y
- the burner system must be large enough whereby to bring the charge-of metal pieces rapidly up to the. desired 1750 degree control temperature
- the burner system just mentioned must be capable of throttling low enough (usually a turn down cf ⁇ 8 to 1) to avoid overheating during the soaking period. That is to say, that while the charge in the car-type 4furnace cited above is lbeing soaked at 1750 degrees control temperature, the actual heat input required, may drop so low that the.
- burner firing rate is only 300,000 B. t. u. per hour, or one eighth of maximum.
- the maximum burner firing rate required for bringing the charge quickly up to temperature may be (as outlined in C above) as little as one fourth, or even one fifth, of the previous maximum firing rate. That is to say, the actual heat input required for bringing the charge quickly up to the desired 800 degree 'temperature will -be approximately 480,000 B. t. u. per hour. But of far greater importance, the minimum firing rate required of the burners, in order to prevent overheating the charge while soaking at 800 degrees.-
- the burner system for the furnace just cited must have an overall maximum of 2,400,000 B. t. u. per hour (for plenty of speed of heat input at 1750 degrees), and it must have an overall minimum as low as 60,000 B. t. u. per hour (to avoid overheating when hold' ing at 800 degrees), or a combinedoverall turn down range of 40 to 1. v
- the car-type furnace above mentioned is typical of a large variety of heat treating furnaces now :being designed for multiple purpose service.
- the burner systernmust have a turn down range of at least 40 to 1. If the,furnace is to be equipped with automatic temperature control (as a very high percentage of recent installations are), a still wider turn-down range on the part of the burner system, is required.
- Modern devices for automatic temperature control in industrial furnaces require, that in order to provide a margin of safety for the automatic and piping, and also preventing the burner from being throttled to extreme low firing rate.
- the object of my invention is to provide a burner device which will afford a scope of turn down suilicient to accomplsh temperature control over a range of ring capacities as great as 100 to 1, a range of such scope being highly desirable if a single furnace is to be used in operations alternating between low ktemperature work and high temperature wor
- further aims are to provide a burner which will lend itself especially to use in industrial heat treating furnaces and ovens, it being kept in mind that for such an apparatus, there must be, at all stages of firing rates (from low minimum to high maximum), combustion ofsuch dependability and such constancy, that in throttling, the change in heat input from any intermediate capacity to another, may be smooth and even.
- the eiect of the above required margin of safety is to increase the turn down requirements by an additional twenty iive per cent, thus making the overy all turn down range, for the above described furnace when automatically controlled, to l (inlimitation of the turn down range of previously designed burners, aref Tendency of the air-gas mixture to flash back into the supply pipe, thereby limiting minimum tiring rate, such flash back damaging the burner tion is embodied in, the new construction, combination, and arrangement of parts illustrated in the accompanying drawings, described in the following specification, and dened in the claims.
- Figure 1 is a front'view ofmy improved gas burner.
- Figure 2 isa side'view in the direction of arrow 2'in Figure 1, a portion of the mount frame being broken away, and the ⁇ mouth or inlet portion of the burner block being shown in cross section.
- Figure 3 is a top"plan view in the direction of arrow 3 in Figure 2, ⁇ a portion of the mount frame, and a portion of the burner block being broken away, and the latter being shown in cross section.l
- Figure 4 is an enlarged vertical central longitu- I dinal sectional view of Figure 2.
- Figure 5 is a side view of the burner-insert, removed, the head portion thereof being shownin cross section. f y
- Figure 6 is an end view in the direction of arrow 6 in Figure 5.
- Figure 'l is an end view in the direction of arrow 'I in Figure 5.
- Figure 8 is a central longitudinal sectional view of said burner-insert, taken on the broken line .-8, in the direction of arrow 8 in Figure 7.
- Figure 9 is an end ,view of the burner block, taken in the direction of arrow 9 in Figure 4.
- Figure 10 is an enlarged perspective view of the head portion of the said burner-insert.
- Figure 11 is a diagrammatic view showing the location of the flame at a low nring rate.
- Figure 12 is a diagrammatic view showing the location of the flame at an intermediate firing rate.
- Figure 13 is a diagrammatic view showing the location of the flame at a high firing rate, and its full length being not shown.
- Figure 14 diagrammatically illustrates. the appearance of the invention in a typical installation.
- Figure 15 illustrates a modification
- Figure 16 is an end view of Figure 15.
- a metal casing I5 is provided with lateral'opening I6 in which is received the air inlet feed pipe I1.
- Forward end I8 of said casing has inturned wall portion 20 provided with machined annular beveled seat 2I. of said casing is provided with circular opening 24.
- the rearward end portion 22 united relation as shown, constitute and end wall which is common to the outer casing I5 and to the conduit 40, and common to the chambers thus formed, namely, the air chamber 50, and
- an elongated aperture 34 for vthe reception of fastener bolts (not shown) and by which the said frame is secured in its inf- -stalled position, as indicated in Figure 14.
- a hinged cover plate 31 provided at that one of the pilot holes 35 which is in registration with the peripheral face of said shoulder is a conical recess 44.
- Castellated rear end 45 of said burner-insert permits holding by a wrench when connecting the gas inlet pipe 46 at the threaded opening therefor.
- a pointed set screw- 48 is so positioned, that when tightened, the burner-insert will have been tightened to and made fast is a series of uniformly spaced ports or orifices 52.
- a series of uniformly spaced ports 54 Provided in the outward or marginal area of said head portion of plate 4I of the said burner-insert in close proximity to, and concentric with the said ports 52, is a series of uniformly spaced ports 54 and which are in staggered rela'- tion to said ports 52.
- the ports 54 are of larger area than the ports 52 and their corners are of filleted formation.
- the radial partitions 55 between sad ports 54 are in alignment with the transverse axes of said ports 52, as indicated in Figure 10.
- Each of said partitions is of a minimum width, and all are of the minimum widths with relation to the widths of the said ports 54, substantially as shown in Figure 10.
- the central mass of the head portion of said burner-insert is of bulged formation.
- the anterior rims of the ports-52 may be in close proximity with the planes of the ports 54, the said ports 52 are inclined at an an'gle toward the longitudinal axis of the burner insert.
- the structural forma- I tion just mentioned simplifies the operation of drilling the ports 52 so that they open from the gas chamber directly at the forward internal marginal portion thereof.
- these sub-- divisions may be referred to as zones, and hence, the tunnel, as zonate in longitudinal formation.
- the said block is united with the Said mount frame, as by the application of high temperature cement51 at the lateral recesses 59, and at holes accordingly.
- the mouth zone or inlet 60 of said tunnel is of diameter to closely encircle the area' defined by a line bounding the outer series of ports 54.
- Each of the succeeding zones 6I and 62 is of progressively larger diameter to the discharge end of the block, and they are joined by theannular offsets 64 and $5.l
- An aperture 58 which is in registration with the pilot hole 35 hereinbefore mentioned in connection with the mount frame, extends into the zone 6I of the said tunnel, and it affords access thereinto for applying a lighter' torch, or for observation purposes.
- the hinged cover plate 31v I would be fitted to a different one of the pilot My improved burner is capable of being installed with the casing so poised that the air feed line I1 may be either in a vertical alignment, or at an angular aligment,thus accommodating itself ⁇ to local cor itions affecting the pipe lines.
- Air supply is through pipe I1
- -and gas supply is through pipe 46 which is fitted with this thorough mixture in the 'zone of a shut-ot! cock G.
- the said pipes are connected with throttling devices and regulators (not shown) usual to industrial furnace installations and equipment.
- the mass so formed constitutes a mixture which is thorough and complete.
- the burner accordingly is responsive at every stage of and throughout the full turn down range. 'I'he thorough and intimate mixture accomplished by my invention, occurring as it does, immediately in the mouth4 of the tunnel; and ignited, as it is, at the offsets of the progressive stages of the tunnel leading to the outlet of the block, the combustion is of such dependability and constancy that the wide range turn down so long sought for, is at last accomplished.
- the casing which constitutes the two chambers is of structural formation so arranged that the air is introduced into the outer chamber
- the invention is capable of such modification that when special or unusual conditions affecting processing of the parts, or affecting installation of the invention, might suggest a change from said embodiment, the air feed may be providedfor in the inner chamber, and the gas in the' outer chamber.
- the air feed may be providedfor in the inner chamber, and the gas in the' outer chamber.
- Figures 15 and 16 Such a modiiication is illustrated in Figures 15 and 16, wherein 10 designates the air chamber, and 'Il the gas chamber. 12 and 14 designate the closely adjacent and staggered gas ports and air ports respectively.
- each stage of progressively larger diameter from its inlet to its outlet, and each joining span the inlet of said tunnel is provided with av series of ports circularly arranged and which open directly from one of the conduits into the tunnel inlet, and is provided with a series of ports circularly arranged in close adjacency to and alternated with the ports of the first named series,
- a mixer, ignition, and combustion apparatus -consisting of a casing provided with an air inlet
- a burner block having a ,tunnel therethrough, zonate in formation and provided I with an annular seat, said casing at its rear portion having a circular opening, a conduit exy tended into said casing and embodying at its forward end a circular transverse head plate to l5 engage said annular seat, said head plate -having a lseries of circularly arranged radially partitioned ports therethrough exteriorly of said conduit, and having a series of circularly arranged ports therethrough interiorly of said conduit, the ports zo of one series being alternated with and in close adjacency to the ports of the other series, a closure interconnecting the said gas conduit with the rear portion of said casing, inlet means for l l said gas conduit, and a burner block united with the forward end of said casing, said block having a tunnel therethrough of zonate formation, the zones thereof being of progressively larger ⁇ diameter from the inlet to the outlet of said tunnel, and the inlet zone being of diameter coincident
- a casing having an open forward end provided with an internal annular seat, and being provided at its rearward end with a circular opening, an air inlet into said casing, a conduit j having at its forward end 'a transverse circular head plate to engage said annular seat,- and embodying at its rearward portion a shoul- 40 der to close the said circular opening of said with a lighter aperture, a mount frame in which (said block is received and secured, said frame ⁇ having a bulgedbreast portion 'and provided with an opening in axial alignment with said casing, the said head plate having a series of circularly arranged equally spaced ports that open therethrough exteriorly of said conduit, and having a series of circularly arranged equally spaced ports that open therethrough interiorly tunnel,.a casing retained at its forward portion.
- saidv casing having lan air inlet in the side thereof, and having a central opening in its rear portion, and an internal annular seat at its forward end, agas conduit which embodies at its rear portion 'an annular shoulder which' is fastened in the openingof said casing, and at'it's forward end a circular head plate that engages the annular seat of said casing thereby spanning the relation to th diameters of the ports ofthat of said conduit, the portsmf one series being alternated withfthe ports of the other seriesand thel webs between the ports of one of the series being radial and of predetermined width with series, a gas inlet means for said conduit, and a burner block united with the forward end of said casing and having a zonate tunnel therethrough, the inlet of which is in axial alignmentr and registration with the head plate of said conmiet of'said tunnel, the said head-platehavmg y nduit HARRY R
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- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
Description
Jan. 30, 1945.
F1a. 2 A
H. R. MA-xoN, JR
GAS BURNER Filed May 2e, 1945 FIG'. 1
3 Sheets-Sheet l i ifi mwen-rok.l BY v HARRY R. AXUNJR A TTORNEY Jan. 30, 14945.
H. R. MAXONy JR GAS BURNER Filed May Q6, 1945 3 Sheets-Sheet 5 y IYENTOR.- HARRY R. MAXON. ';JR
ATTORNEY Patented Jan. 30, 1945 GAS Buisman Harry R. Maxon. Jr., Muncie, 1nd., assignor to Maxon Premix Burner Company, Muncie, Ind., a corporation of Delaware Application May as, 1943, serial No. 438,791
e claims. (ci. 15s-L7) In operations of heat treating wherein a wide range of furnace temperatures is required, there has long --been the problem of how best to obtain, and of how best to control heat inputs.
One of the many problems which vhave confronted the designer of an installation for heat treating of metal, is the securing of adequate turn down range in the burnerl system. By burner system being ymeant, the lburner or burners u sed in connection with a furnace, or furnaces. Such problem is especially present in the handling of a batch-type furnace, because of the `following factors:
A. The burner system must have a sufficiently large maximum capacity to provide adequate speed of heat input for initially 'bringing the charge of metal pieces to be treated, up to desired control temperature.
lthe installation of duplicate heat treating furnaces or ovens in thousands of plantsthere having been no choice other than to install one iurna'ce for' suchoper'ations as fall rin the 1500 to 1-700 degree range, and also to install -a different furnace for heat treating operations that fall B. The burner system must have a sufficiently low minimum capacity to prevent overheating* after the control temperature will have been' reached. Such conditions may require a minimum firing rate as low as one eighth of the maximum burner .capacity (particularly when the charge of metal pieces is held inthe furnace for a soaking period of several hours after the desired temperature will have been reached).` Under conditions as above indicated, it is understood that the lburner system must have a turn down range of 8 to 1. That is to say, there must be an 8 to 1 ratio between' the maximum and the minimum ring rates. y
C.- 'The burner system must be suflcientlyflexible to permit ring of the -furnace or oven at more than one control temperature. For examwithin the 800 to 1200 degree range. Resultant, r
in many instances, has been a duplication of `capital investment, especially undesirable in plants where nances are limited, and where heat treating operations are only occasional.
Many plants are out of balance in their heat treating facilities, having an excess of furnaces for high temperature operations, and at the same time, being inadequately equipped for operations wherein drawing, tempering, or stress relieving,
ple, steel parts to .be treated, are frequently heated to a temperaturewithin the range of 1500 -to 1700 degrees and then suddenly quenched in oil or Water to impart characteristics of additional hardness to the metal. It is customary, after the steel will thus have been hardened, to reheat same to a temperature within a range of 800 to 1200 degrees, for the drawing out ofundesirable stresses or strainswhich may have been set up during the quenching operation.
Hitherto it has been found impossible to obtain suillcient burner ilexibility to permit of the handling of both of the above named operations l that is, to quench at 1500l to 1700 degrees, and to draw at 800 to 1200 degrees) in the same furnace without shutting off part of the lburners,
and thus impairing uniformity of heat distribution. There is needed, for operationsV at' 1700 degrees, approximately five times as much heat in the 800 to 1200 degree range are involved. Conversely, numerous other plants may be pos, sessed of large and costly facilities for vthe low temperature work, but are acutely bottle necked when confronted with operations of normalizing at 1700 degrees. f
Frm the conditions above sketched, there has developed an urgent demand for a multiple purpose lfurnace; one that can be operated at any of the higher heat treating temperatures, or alperatures.
In endeavors 'to meet contingencies such as ternately, at any of the lower heat treating temi those above outlined,'extensive efforts have been as is required for re-processing the'same mate- 55 put forth to work out a b urner system having a sufficient turn down range to make a multiple purpose furnace possible. 'Elaborate tests along this line have indicated that to assure any practicable degreeof flexibility of furnace operation a burner system having a turn down range of at least 40 to 1, and preferably, 50 to 1, is required'.
For illustration, the case of a certain type of annealing furnace operating at 1750 degrees, may
' be cited. As hereinbefore pointed out at A, the burner system must be large enough whereby to bring the charge-of metal pieces rapidly up to the. desired 1750 degree control temperature, and
which in this instance requires a maximum ring rate of 2,400,000 B. t. u. per hour. A't the same time, as pointed out in"B above, the burner system just mentioned must be capable of throttling low enough (usually a turn down cf` 8 to 1) to avoid overheating during the soaking period. That is to say, that while the charge in the car-type 4furnace cited above is lbeing soaked at 1750 degrees control temperature, the actual heat input required, may drop so low that the.
burner firing rate is only 300,000 B. t. u. per hour, or one eighth of maximum.
Now let it :be assumed that the above charge of metal (or an equivalent charge) be placed in the aforesaid furnace, for drawing or tempering at 800 degrees. At this lower temperature, the maximum burner firing rate required for bringing the charge quickly up to temperature may be (as outlined in C above) as little as one fourth, or even one fifth, of the previous maximum firing rate. That is to say, the actual heat input required for bringing the charge quickly up to the desired 800 degree 'temperature will -be approximately 480,000 B. t. u. per hour. But of far greater importance, the minimum firing rate required of the burners, in order to prevent overheating the charge while soaking at 800 degrees.-
must |he as low as 60,000 B. t. u. per hour W; of the 480,000 B. t. u. per hour maximum firing rate).
It will thus be seen that the burner system for the furnace just cited, must have an overall maximum of 2,400,000 B. t. u. per hour (for plenty of speed of heat input at 1750 degrees), and it must have an overall minimum as low as 60,000 B. t. u. per hour (to avoid overheating when hold' ing at 800 degrees), or a combinedoverall turn down range of 40 to 1. v
The car-type furnace above mentioned is typical of a large variety of heat treating furnaces now :being designed for multiple purpose service. In each ofsuch cases, the burner systernmust have a turn down range of at least 40 to 1. If the,furnace is to be equipped with automatic temperature control (as a very high percentage of recent installations are), a still wider turn-down range on the part of the burner system, is required.
Modern devices for automatic temperature control in industrial furnaces require, that in order to provide a margin of safety for the automatic and piping, and also preventing the burner from being throttled to extreme low firing rate.
Blowing away or the flame, and therefore the prevention of operation at high ring rates.
Failure to hold name continuously throughout tum down.
impossibility of throttling smoothly in cases where double burners are used (a larger burner being used for handling higher heat inputs, and a smaller burner being used for handling low and minimum heat inputs), there being either a sudden gap between the minimum of a large burner and the maximum of a small burner, or else a sudden step up or a sudden step down at that 4phase of the throwing range at which the two firing rates overlap.
To 'the end that above named disadvantages may be overcome, and that there may be rendered practicable the utilization of a single furnace for heat treating operations wherein wide ranges of temperatures are required, the object of my invention is to provide a burner device which will afford a scope of turn down suilicient to accomplsh temperature control over a range of ring capacities as great as 100 to 1, a range of such scope being highly desirable if a single furnace is to be used in operations alternating between low ktemperature work and high temperature wor Accordingly, in carrying out the purposes of my invention, further aims are to provide a burner which will lend itself especially to use in industrial heat treating furnaces and ovens, it being kept in mind that for such an apparatus, there must be, at all stages of firing rates (from low minimum to high maximum), combustion ofsuch dependability and such constancy, that in throttling, the change in heat input from any intermediate capacity to another, may be smooth and even.
The above named objects, as well as other and more speciiic endeavors of my invention, and which have to do with improved structural features leading to economy of manufacture, facility of installation and use, and to efficiency vand durability, are accomplished by, and my invencontrol system, so that over-shooting or unf f der-shooting of vdesired temperature may be quickly corrected, the burner system must be capable of turning slightly higher, or turning slightly lower than is actually necessary for supplying A the heat input needed at any given moment. The eiect of the above required margin of safety, is to increase the turn down requirements by an additional twenty iive per cent, thus making the overy all turn down range, for the above described furnace when automatically controlled, to l (inlimitation of the turn down range of previously designed burners, aref Tendency of the air-gas mixture to flash back into the supply pipe, thereby limiting minimum tiring rate, such flash back damaging the burner tion is embodied in, the new construction, combination, and arrangement of parts illustrated in the accompanying drawings, described in the following specification, and dened in the claims.
The several parts of the inventionare identi fied in the different views in the drawings, by suitable characters of reference applied to them.
In the drawings:
Figure 1 is a front'view ofmy improved gas burner.
Figure 2 isa side'view in the direction of arrow 2'in Figure 1, a portion of the mount frame being broken away, and the` mouth or inlet portion of the burner block being shown in cross section.
Figure 3 is a top"plan view in the direction of arrow 3 in Figure 2,`a portion of the mount frame, and a portion of the burner block being broken away, and the latter being shown in cross section.l
Figure 4 is an enlarged vertical central longitu- I dinal sectional view of Figure 2.
Figure 5 is a side view of the burner-insert, removed, the head portion thereof being shownin cross section. f y
Figure 6 is an end view in the direction of arrow 6 in Figure 5. A
Figure 'l is an end view in the direction of arrow 'I in Figure 5.
Figure 8 is a central longitudinal sectional view of said burner-insert, taken on the broken line .-8, in the direction of arrow 8 in Figure 7.
Figure 9 is an end ,view of the burner block, taken in the direction of arrow 9 in Figure 4.
Figure 10 is an enlarged perspective view of the head portion of the said burner-insert.
Figure 11 is a diagrammatic view showing the location of the flame at a low nring rate.
Figure 12 is a diagrammatic view showing the location of the flame at an intermediate firing rate.n
Figure 13 is a diagrammatic view showing the location of the flame at a high firing rate, and its full length being not shown.
Figure 14 diagrammatically illustrates. the appearance of the invention in a typical installation.
Figure 15 illustrates a modification.
Figure 16 is an end view of Figure 15.
The embodiment of my invention as it is described herein and depicted in the drawings, is typical. It will be understood of course, that the details of construction and arrangement of parts are capable of minor changes, alterations and modifications, such as may occur to those persons skilled in the' art to which the invention appertains, without departing from the spirit or principle of the inventionvor sacrificing any of its advantages. I
A metal casing I5 is provided with lateral'opening I6 in which is received the air inlet feed pipe I1. Forward end I8 of said casing has inturned wall portion 20 provided with machined annular beveled seat 2I. of said casing is provided with circular opening 24. A hole in a side of said casing, and which is closed by a removable plug I9, affords facility The rearward end portion 22 united relation as shown, constitute and end wall which is common to the outer casing I5 and to the conduit 40, and common to the chambers thus formed, namely, the air chamber 50, and
l the internal marginal portion of the chamber 5I,
for making tests of the air pressure within the 'casing.
A metal mount frame 26, box-like in formation, embodies bulged breast portion 21 having a circular opening 28 within which the forward end I8 of said casing is received, and at its annularflange 29 is secured as by the cap screws I0. In each of thev flanges 32 and- 33 of said mount frame, is an elongated aperture 34 for vthe reception of fastener bolts (not shown) and by which the said frame is secured in its inf- -stalled position, as indicated in Figure 14.
A hinged cover plate 31 provided at that one of the pilot holes 35 which is in registration with the peripheral face of said shoulder is a conical recess 44. Castellated rear end 45 of said burner-insert permits holding by a wrench when connecting the gas inlet pipe 46 at the threaded opening therefor. A pointed set screw- 48 is so positioned, that when tightened, the burner-insert will have been tightened to and made fast is a series of uniformly spaced ports or orifices 52. Provided in the outward or marginal area of said head portion of plate 4I of the said burner-insert in close proximity to, and concentric with the said ports 52, is a series of uniformly spaced ports 54 and which are in staggered rela'- tion to said ports 52. The ports 54 are of larger area than the ports 52 and their corners are of filleted formation. The radial partitions 55 between sad ports 54 are in alignment with the transverse axes of said ports 52, as indicated in Figure 10. Each of said partitions is of a minimum width, and all are of the minimum widths with relation to the widths of the said ports 54, substantially as shown in Figure 10.
For reasons that are incident to convenience and economy in processing, the central mass of the head portion of said burner-insert is of bulged formation. For the same reasons, and for the further reason, that the anterior rims of the ports-52 may be in close proximity with the planes of the ports 54, the said ports 52 are inclined at an an'gle toward the longitudinal axis of the burner insert. Also the structural forma- I tion just mentioned simplifies the operation of drilling the ports 52 so that they open from the gas chamber directly at the forward internal marginal portion thereof.
A burner block 56 made of suitable refractory material such as fire brick, and which is of formation in cross section to fit into the said mount frame 2B, is provided with a tunnel formed in circular subdivisions or stages which are concentric and'which at their proximal edges are joined by annular oii'sets. For brevity these sub-- divisions may be referred to as zones, and hence, the tunnel, as zonate in longitudinal formation.
- The said block is united with the Said mount frame, as by the application of high temperature cement51 at the lateral recesses 59, and at holes accordingly.
in the position indicated in Figure 4, the annular the end recess 25, the latter constituting a seal at thel forward wall of the casing I5. The mouth zone or inlet 60 of said tunnel is of diameter to closely encircle the area' defined by a line bounding the outer series of ports 54. Each of the succeeding zones 6I and 62 is of progressively larger diameter to the discharge end of the block, and they are joined by theannular offsets 64 and $5.l An aperture 58 which is in registration with the pilot hole 35 hereinbefore mentioned in connection with the mount frame, extends into the zone 6I of the said tunnel, and it affords access thereinto for applying a lighter' torch, or for observation purposes. In case the block may be set so that its aperture 58 is at a reverse posi-` tion, or is at a position at a right angle to that shown in Figure 3, the hinged cover plate 31v I would be fitted to a different one of the pilot My improved burner is capable of being installed with the casing so poised that the air feed line I1 may be either in a vertical alignment, or at an angular aligment,thus accommodating itself` to local cor itions affecting the pipe lines. Illustrative of a typical installation, is Figure 14. Air supply is through pipe I1,-and gas supply is through pipe 46 which is fitted with this thorough mixture in the 'zone of a shut-ot! cock G. "The said pipes are connected with throttling devices and regulators (not shown) usual to industrial furnace installations and equipment.
`In operation of my new burner, the air fed into the chamber 50 nows through the air ports duced along the side edges and in the space be- 1G tween said edges and at the gas ports 52 and ahead of the partitions 55, low pressure areas, there being such an area immediately at the front of and extending forwardly of each of said partitions. In each of these low pressure areas there is set up a partial vacuum. The gas streams issuing from the gas ports 52, being sucked into said low pressure areas, collapsing, and coming' into contact with the highly agitated and brokensurfaced streams of air, are caused to fill the space between and around the air streams, the effect being that the gas becomes infused in and completely co-mingled with the air streams, hence the volume composed of all of the air-gas streams` will have become merged into an intensively and intimately mixed homogenized mass.
The mass so formed constitutes a mixture which is thorough and complete.
It is considered that the accomplishment of the 1511111181 mouth and closely adjacent to the front of said ports is of the essence of this invention, the degree of thoroughness of said mixture distinguishing my improved burner from all prior nozzle` type mixers. 3
The air and gas having not been combined until they have entered the inlet or mouth of the tunnel of the burner block, there is no possibility of flash back such as exists with burners of the premix type. By reason of the thorough and effec' 40 tive mixture so obtained, immediately at the said mouth 60, flame retention at minimum air pressure (that is to say, low ringrate) is assured, the tiny names, at low pressure, burning quietly and steadily in the rst small stage or inlet zone 45 of the tunnel of the burner block, as indicated in Figure 11.
As the firing rate 0f the burner is increased (incident to increase of air pressure entering the air chamber) and the velocity of the air-gas mix- 50 ture in the mouth zone becomes too great for the continuation of self-ignition thereat, the said mixture is discharged, unignited, beyond the offset 64 andinto the second zone 6| of the tunnel. Tiny eddy currents (see Figure 12) yin the air-gas 55 mixture, and which are' automatically created at the said oifset 64, whip small portions of said mixture into the dead area. immediately at the lee of the edge of said odset, and wherejtliey burni continuously and ignite the mass `volume of air- 60 gas mixture issuing from the said mouth zone into the next or second -zone 8| of the tunnel, thus combustion is had in the remaining zones of the tunnel, or in the area or space immediately beyond the outlet end of same, as indicated in 65 Figure 12.
Similarly, when the ring rate is still further increased, and the velocity of the mixture is increased to such degree that ignition ceases in the said second zone 6| ofthe tunnel, thenfat the 70 protected space at the lee of the edge of the next offset 65 (see Figure A12) combustion occurs in the manner 'as above described, as indicated diagrammatically in Figure 13.
Whereas in most cases, atunnel or duct having furnace temperatures. The ame being constant.
and dependable at every stage of throttling, the burner accordingly is responsive at every stage of and throughout the full turn down range. 'I'he thorough and intimate mixture accomplished by my invention, occurring as it does, immediately in the mouth4 of the tunnel; and ignited, as it is, at the offsets of the progressive stages of the tunnel leading to the outlet of the block, the combustion is of such dependability and constancy that the wide range turn down so long sought for, is at last accomplished.
Continuous ignition and constant flame is had at all firing rates -from low minimum to high maximum, and without any interruption when throttling from one iiring rate' to the other. Because of the flexibility and the easiness of control of my improved burner it's use is not limited to any' one type of industrial furnace or oven, and it provides advantages in a wide variety of heat applications. A eld in which it is especially, distinguished is the heat treating of metals in those furnaces used for the processing of steel, aluminum or brass. In any of said applications, the
5 ratio between the maximum and the minimum firing rates may be as great as to 1, if desired, and the extremely wide range of turn down is accomplished without the use of any secondary or auxiliary burners or appliances, and same is without interruption when throttlng from one iiring rate to another.
Whereas in the preferred form of embodiment i of my invention as it is illustrated and described herein, the casing which constitutes the two chambers is of structural formation so arranged that the air is introduced into the outer chamber,
I wish it to be understood that the invention is capable of such modification that when special or unusual conditions affecting processing of the parts, or affecting installation of the invention, might suggest a change from said embodiment, the air feed may be providedfor in the inner chamber, and the gas in the' outer chamber. Such a modiiication is illustrated in Figures 15 and 16, wherein 10 designates the air chamber, and 'Il the gas chamber. 12 and 14 designate the closely adjacent and staggered gas ports and air ports respectively.
What I claim as my invention is:
l. In combination with a refractory burner block having a multiple stage tunnel therethrough, each stage of progressively larger diameter from its inlet to its outlet, and each joining span the inlet of said tunnel, is provided with av series of ports circularly arranged and which open directly from one of the conduits into the tunnel inlet, and is provided with a series of ports circularly arranged in close adjacency to and alternated with the ports of the first named series,
and which said last named ports open from directly from the gas conduit into the tunnel ina series of equally spaced circularly arranged ports interiorly of saidconduit, and a seriesv of equally spaced circularly arranged ports exterorly of said conduit, the ports of one series being alternated withland in close adjacency .to the ports of the other series, and means to supply said gas conduit. n
5. A mixer, ignition, and combustion apparatus -consisting of a casing provided with an air inlet,
1'0 and having an inturned forward end providedr let, and is provided with a series of ports circularly Y arranged, equally and closely spaced, in close adjacency to and alternated with the ports of said gas conduit, and which said last named ports open' from the air conduit into the said.
tunnel inlet.
3. The combination of a refractory burner structure having a multiple stage tunnel therethrough, each stage of progressively larger diameter from its inlet to its outlet and each joining the next by an offset shoulder, a casing embodying two conduits, one within the other,`said casing having a wall that terminatesveach of the conduits, is abutted against said burner structure to span the inlet of said tunnel, is provided with a series of ports circularly arranged, equally and closely'spaced, and which open directly from one of said conduits into the tunnel inlet, and is provided with a series of ports equally and closely spaced in close adjacency to and alternated with the ports of the first named series, and which said last named ports open from the other of said conduits directly intoy said tunnel inlet, the webs between'the ports.of one series being of predetermined form with relation tothe forms of the ports of that series. 4. A burner apparatus of the kind described,
- consisting of a burner block having a ,tunnel therethrough, zonate in formation and provided I with an annular seat, said casing at its rear portion having a circular opening, a conduit exy tended into said casing and embodying at its forward end a circular transverse head plate to l5 engage said annular seat, said head plate -having a lseries of circularly arranged radially partitioned ports therethrough exteriorly of said conduit, and having a series of circularly arranged ports therethrough interiorly of said conduit, the ports zo of one series being alternated with and in close adjacency to the ports of the other series, a closure interconnecting the said gas conduit with the rear portion of said casing, inlet means for l l said gas conduit, and a burner block united with the forward end of said casing, said block having a tunnel therethrough of zonate formation, the zones thereof being of progressively larger` diameter from the inlet to the outlet of said tunnel, and the inlet zone being of diameter coincident with that of,the head plate of said conduit.
ing of-a casinghaving an open forward end provided with an internal annular seat, and being provided at its rearward end with a circular opening, an air inlet into said casing, a conduit j having at its forward end 'a transverse circular head plate to engage said annular seat,- and embodying at its rearward portion a shoul- 40 der to close the said circular opening of said with a lighter aperture, a mount frame in which (said block is received and secured, said frame` having a bulgedbreast portion 'and provided with an opening in axial alignment with said casing, the said head plate having a series of circularly arranged equally spaced ports that open therethrough exteriorly of said conduit, and having a series of circularly arranged equally spaced ports that open therethrough interiorly tunnel,.a casing retained at its forward portion.
within the opening of said mount frame and abutted against the inlet end of said block, saidv casing having lan air inlet in the side thereof, and having a central opening in its rear portion, and an internal annular seat at its forward end, agas conduit which embodies at its rear portion 'an annular shoulder which' is fastened in the openingof said casing, and at'it's forward end a circular head plate that engages the annular seat of said casing thereby spanning the relation to th diameters of the ports ofthat of said conduit, the portsmf one series being alternated withfthe ports of the other seriesand thel webs between the ports of one of the series being radial and of predetermined width with series, a gas inlet means for said conduit, and a burner block united with the forward end of said casing and having a zonate tunnel therethrough, the inlet of which is in axial alignmentr and registration with the head plate of said conmiet of'said tunnel, the said head-platehavmg y nduit HARRY R. MAXON, Jn:
6. A gas burner of the kind described, consist-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US488797A US2368370A (en) | 1943-05-26 | 1943-05-26 | Gas burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US488797A US2368370A (en) | 1943-05-26 | 1943-05-26 | Gas burner |
Publications (1)
Publication Number | Publication Date |
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US2368370A true US2368370A (en) | 1945-01-30 |
Family
ID=23941158
Family Applications (1)
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US488797A Expired - Lifetime US2368370A (en) | 1943-05-26 | 1943-05-26 | Gas burner |
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US (1) | US2368370A (en) |
Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2480255A (en) * | 1945-10-10 | 1949-08-30 | Nat Tube Co | Burner for soaking pit furnaces and the like |
US2515158A (en) * | 1945-11-19 | 1950-07-11 | Alexander J Turpin | Radiant gas burner having concentric gas and air nozzles |
US2596341A (en) * | 1945-03-29 | 1952-05-13 | Owens Illinois Glass Co | Burner block and burner |
US2670788A (en) * | 1949-10-10 | 1954-03-02 | Mac Mixer Inc | Fuel and air mixing unit for burner assemblies |
US2754895A (en) * | 1952-01-02 | 1956-07-17 | Borg Warner | Single port gas burner and removable flame deflector |
US2969833A (en) * | 1957-04-11 | 1961-01-31 | Bloom Eng Co Inc | Burner mechanism |
US3022815A (en) * | 1958-03-31 | 1962-02-27 | Bloom Eng Co Inc | Burner mechanism |
US3078915A (en) * | 1959-06-10 | 1963-02-26 | Otto Bernz Co Inc | Utility burner head |
US3180394A (en) * | 1955-04-26 | 1965-04-27 | Bloom Eng Co Inc | Gas burner |
US3861858A (en) * | 1972-12-11 | 1975-01-21 | Midland Ross Corp | Throat mix burner |
FR2459423A1 (en) * | 1979-06-18 | 1981-01-09 | Heurtey Metallurgie | Combustion gas burner with air premixer - having combustion air preheater to maintain lean mixture before combustion chamber |
WO1984000176A1 (en) * | 1982-06-24 | 1984-01-19 | Cadre Corp | Oxygen-fuel burner with lancing capability and method of producing steel |
US4473350A (en) * | 1982-06-24 | 1984-09-25 | The Cadre Corporation | Oxy-fuel burner |
US4622007A (en) * | 1984-08-17 | 1986-11-11 | American Combustion, Inc. | Variable heat generating method and apparatus |
FR2601756A1 (en) * | 1986-07-21 | 1988-01-22 | Maxon Corp | BURNER ASSEMBLY OPERATING AT HIGH TEMPERATURE |
US4883422A (en) * | 1988-04-05 | 1989-11-28 | T.T.C. Termo Tecnica Ceramica S.P.A. | Mixed air and gas nozzle for gas burners, in particular burners of low thermal output for firing kilns |
US4986748A (en) * | 1989-12-15 | 1991-01-22 | Corning Incorporated | Wide range oxy-fuel burner and furnace operation |
US5823759A (en) * | 1993-03-20 | 1998-10-20 | Cabot Corporation | Apparatus and method for burning combustible gases |
US20030175639A1 (en) * | 2002-03-16 | 2003-09-18 | Spicer David B. | Burner employing flue-gas recirculation system |
US20030175632A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Removable light-off port plug for use in burners |
US20030175634A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Burner with high flow area tip |
US20030175646A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Method for adjusting pre-mix burners to reduce NOx emissions |
US20030175635A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Burner employing flue-gas recirculation system with enlarged circulation duct |
WO2003081129A1 (en) * | 2002-03-16 | 2003-10-02 | Exxonmobil Chemical Patents Inc. | Burner tip and seal for optimizing burner performance |
US20040018461A1 (en) * | 2002-03-16 | 2004-01-29 | George Stephens | Burner with low NOx emissions |
US6866502B2 (en) | 2002-03-16 | 2005-03-15 | Exxonmobil Chemical Patents Inc. | Burner system employing flue gas recirculation |
US6869277B2 (en) | 2002-03-16 | 2005-03-22 | Exxonmobil Chemical Patents Inc. | Burner employing cooled flue gas recirculation |
US6881053B2 (en) | 2002-03-16 | 2005-04-19 | Exxonmobil Chemical Patents Inc. | Burner with high capacity venturi |
US6884062B2 (en) | 2002-03-16 | 2005-04-26 | Exxonmobil Chemical Patents Inc. | Burner design for achieving higher rates of flue gas recirculation |
US6887068B2 (en) | 2002-03-16 | 2005-05-03 | Exxonmobil Chemical Patents Inc. | Centering plate for burner |
US6890172B2 (en) | 2002-03-16 | 2005-05-10 | Exxonmobil Chemical Patents Inc. | Burner with flue gas recirculation |
US6893251B2 (en) | 2002-03-16 | 2005-05-17 | Exxon Mobil Chemical Patents Inc. | Burner design for reduced NOx emissions |
US6893252B2 (en) | 2002-03-16 | 2005-05-17 | Exxonmobil Chemical Patents Inc. | Fuel spud for high temperature burners |
US6986658B2 (en) | 2002-03-16 | 2006-01-17 | Exxonmobil Chemical Patents, Inc. | Burner employing steam injection |
USRE39425E1 (en) * | 1993-07-15 | 2006-12-12 | Maxon Corporation | Oxygen-fuel burner with integral staged oxygen supply |
US20090081601A1 (en) * | 2007-09-25 | 2009-03-26 | United States of America as represented by the Administrator of the National Aeronautics and | Flame Holder System |
-
1943
- 1943-05-26 US US488797A patent/US2368370A/en not_active Expired - Lifetime
Cited By (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2596341A (en) * | 1945-03-29 | 1952-05-13 | Owens Illinois Glass Co | Burner block and burner |
US2480255A (en) * | 1945-10-10 | 1949-08-30 | Nat Tube Co | Burner for soaking pit furnaces and the like |
US2515158A (en) * | 1945-11-19 | 1950-07-11 | Alexander J Turpin | Radiant gas burner having concentric gas and air nozzles |
US2670788A (en) * | 1949-10-10 | 1954-03-02 | Mac Mixer Inc | Fuel and air mixing unit for burner assemblies |
US2754895A (en) * | 1952-01-02 | 1956-07-17 | Borg Warner | Single port gas burner and removable flame deflector |
US3180394A (en) * | 1955-04-26 | 1965-04-27 | Bloom Eng Co Inc | Gas burner |
US2969833A (en) * | 1957-04-11 | 1961-01-31 | Bloom Eng Co Inc | Burner mechanism |
US3022815A (en) * | 1958-03-31 | 1962-02-27 | Bloom Eng Co Inc | Burner mechanism |
US3078915A (en) * | 1959-06-10 | 1963-02-26 | Otto Bernz Co Inc | Utility burner head |
US3861858A (en) * | 1972-12-11 | 1975-01-21 | Midland Ross Corp | Throat mix burner |
FR2459423A1 (en) * | 1979-06-18 | 1981-01-09 | Heurtey Metallurgie | Combustion gas burner with air premixer - having combustion air preheater to maintain lean mixture before combustion chamber |
WO1984000176A1 (en) * | 1982-06-24 | 1984-01-19 | Cadre Corp | Oxygen-fuel burner with lancing capability and method of producing steel |
US4473350A (en) * | 1982-06-24 | 1984-09-25 | The Cadre Corporation | Oxy-fuel burner |
US4622007A (en) * | 1984-08-17 | 1986-11-11 | American Combustion, Inc. | Variable heat generating method and apparatus |
FR2601756A1 (en) * | 1986-07-21 | 1988-01-22 | Maxon Corp | BURNER ASSEMBLY OPERATING AT HIGH TEMPERATURE |
DE3722446A1 (en) * | 1986-07-21 | 1988-02-04 | Maxon Corp | HIGH TEMPERATURE BURNER UNIT |
US4883422A (en) * | 1988-04-05 | 1989-11-28 | T.T.C. Termo Tecnica Ceramica S.P.A. | Mixed air and gas nozzle for gas burners, in particular burners of low thermal output for firing kilns |
US4986748A (en) * | 1989-12-15 | 1991-01-22 | Corning Incorporated | Wide range oxy-fuel burner and furnace operation |
US5823759A (en) * | 1993-03-20 | 1998-10-20 | Cabot Corporation | Apparatus and method for burning combustible gases |
USRE39425E1 (en) * | 1993-07-15 | 2006-12-12 | Maxon Corporation | Oxygen-fuel burner with integral staged oxygen supply |
WO2003081129A1 (en) * | 2002-03-16 | 2003-10-02 | Exxonmobil Chemical Patents Inc. | Burner tip and seal for optimizing burner performance |
US6890171B2 (en) | 2002-03-16 | 2005-05-10 | Exxonmobil Chemical Patents, Inc. | Apparatus for optimizing burner performance |
US20030175646A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Method for adjusting pre-mix burners to reduce NOx emissions |
US20030175635A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Burner employing flue-gas recirculation system with enlarged circulation duct |
US20030175632A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Removable light-off port plug for use in burners |
US20040018461A1 (en) * | 2002-03-16 | 2004-01-29 | George Stephens | Burner with low NOx emissions |
US20040018462A1 (en) * | 2002-03-16 | 2004-01-29 | George Stephens | Apparatus for optimizing burner performance |
US20040241601A1 (en) * | 2002-03-16 | 2004-12-02 | Spicer David B. | Burner tip for pre-mix burners |
US6846175B2 (en) | 2002-03-16 | 2005-01-25 | Exxonmobil Chemical Patents Inc. | Burner employing flue-gas recirculation system |
US6866502B2 (en) | 2002-03-16 | 2005-03-15 | Exxonmobil Chemical Patents Inc. | Burner system employing flue gas recirculation |
US6869277B2 (en) | 2002-03-16 | 2005-03-22 | Exxonmobil Chemical Patents Inc. | Burner employing cooled flue gas recirculation |
US6877980B2 (en) | 2002-03-16 | 2005-04-12 | Exxonmobil Chemical Patents Inc. | Burner with low NOx emissions |
US6881053B2 (en) | 2002-03-16 | 2005-04-19 | Exxonmobil Chemical Patents Inc. | Burner with high capacity venturi |
US6884062B2 (en) | 2002-03-16 | 2005-04-26 | Exxonmobil Chemical Patents Inc. | Burner design for achieving higher rates of flue gas recirculation |
US6887068B2 (en) | 2002-03-16 | 2005-05-03 | Exxonmobil Chemical Patents Inc. | Centering plate for burner |
US20030175634A1 (en) * | 2002-03-16 | 2003-09-18 | George Stephens | Burner with high flow area tip |
US6890172B2 (en) | 2002-03-16 | 2005-05-10 | Exxonmobil Chemical Patents Inc. | Burner with flue gas recirculation |
US6893251B2 (en) | 2002-03-16 | 2005-05-17 | Exxon Mobil Chemical Patents Inc. | Burner design for reduced NOx emissions |
US6893252B2 (en) | 2002-03-16 | 2005-05-17 | Exxonmobil Chemical Patents Inc. | Fuel spud for high temperature burners |
US6902390B2 (en) | 2002-03-16 | 2005-06-07 | Exxonmobil Chemical Patents, Inc. | Burner tip for pre-mix burners |
US20050147934A1 (en) * | 2002-03-16 | 2005-07-07 | George Stephens | Burner with high capacity venturi |
US6986658B2 (en) | 2002-03-16 | 2006-01-17 | Exxonmobil Chemical Patents, Inc. | Burner employing steam injection |
US7025587B2 (en) | 2002-03-16 | 2006-04-11 | Exxonmobil Chemical Patents Inc. | Burner with high capacity venturi |
US20030175639A1 (en) * | 2002-03-16 | 2003-09-18 | Spicer David B. | Burner employing flue-gas recirculation system |
US7322818B2 (en) | 2002-03-16 | 2008-01-29 | Exxonmobil Chemical Patents Inc. | Method for adjusting pre-mix burners to reduce NOx emissions |
US7476099B2 (en) | 2002-03-16 | 2009-01-13 | Exxonmobil Chemicals Patents Inc. | Removable light-off port plug for use in burners |
US20090081601A1 (en) * | 2007-09-25 | 2009-03-26 | United States of America as represented by the Administrator of the National Aeronautics and | Flame Holder System |
US8529249B2 (en) * | 2007-09-25 | 2013-09-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Flame holder system |
US10072840B2 (en) | 2007-09-25 | 2018-09-11 | The United States Of America As Represented By The Administator Of Nasa | Flame holder system |
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