US3510238A - Tubular uniform temperature heat source - Google Patents

Tubular uniform temperature heat source Download PDF

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US3510238A
US3510238A US722690A US3510238DA US3510238A US 3510238 A US3510238 A US 3510238A US 722690 A US722690 A US 722690A US 3510238D A US3510238D A US 3510238DA US 3510238 A US3510238 A US 3510238A
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housing
sleeve
burner
nozzle
flame
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US722690A
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Albert Biber
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Chevron USA Inc
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Gulf Research and Development Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M9/00Baffles or deflectors for air or combustion products; Flame shields

Definitions

  • a uniform temperature heat source utilizing liquid fuel comprising means to reduce the amount of heat imparted to the tubular housing by the combustion products adjacent the flame, and means to gradually increase the amount of heat imparted along the tubular housing away from the flame.
  • the burner is particularly suited for use in thermoelectric generators.
  • This invention relates to the art of oil burners, and more particularly is concerned with a relatively small burner which is of generally tubular shape and which will produce a substantially uniform temperature along its outer wall.
  • thermoelectric generators A burner of the character described is particularly useful in fabricating small, portable, thermoelectric generators.
  • the use of such portable generators is described in a paper published by the American Society of Automotive lEngineers, Paper No. 670452, dated May 1519, 1967, by A. Bayne Neild.
  • the heat source is surrounded by an elongated annular thermopile, and the temperature difference across the thermopile is utilized to produce electrical energy in the thermopile.
  • the thermopile itself, and, in fact, use in thermoelectric generators itself does not form a material part of the present invention, since the burner of the invention can be used in any application wherein a tubular uniform temperature heat source is required.
  • the burner of the invention provides a radiant heat source without flame or combustion gases in the external heated area.
  • An object of the invention is to provide a burner of the character described which will be rugged and insensitive to orientation.
  • the burner In its use as a heat source for a portable thermoelectric generator, the burner must be able to operate, for example, in a military back pack to be carried by a soldier and thus be capable of operation in all attitudes, vertically, horizontally, and while in motion. Because of the self-contained nature of the burner of the invention, it will operate under all of these highly adverse conditions. It will be understood that some suitable means, such as a check valve or the like not shown, will be provided to prevent direct flow of fuel from the fuel source.
  • Another object of this invention is to provide a burner of the character described which shall be simple and economical to fabricate, positive and highly reliable in operation, able to spontaneously re-light itself if it should extinguish during operation, inexpensive, and practical and efiicient to a high degree in use.
  • FIG. 1 is a side elevational view of the burner of the invention embodied in a thermoelectric generator
  • FIG. 2 is a cross-sectional side elevational view of the burner of the invention.
  • Burner 12 comprises a burner housing tube 14 and a fuel nozzle 16.
  • the nozzle 16 will be selected to suit the fuel, and will usually include means to supply air under pressure and fuel under pressure or suction through the feed lines 18 and 20 from a fuel source and an air compressor, respectively, forming part of the thermoelectric generator, but not shown.
  • nozzle 16 be able to burn any fuel available such as gasoline, diesel fuel, kerosene, jet and aviation fuel and the like.
  • Generator 10 comprises an outer housing 22 which is tubular and of a length slightly shorter than the overall length of housing tube 14.
  • the annular space between housing 22 and tube 14 is filled with a thermopile, not shown.
  • the temperature difference between outside of housing 22 and the outside of tube 14 across the thermopile is the motive force which produces electricity in the thermopile.
  • Generator 10 will also include suitable ignition means, not shown, in the form of spark electrodes, a glow plug, or other suitable means, which will be positioned at a suitable location. The positioning of the ignition means, and the ancillary ignition equipment required, does not form a material part of the present invention.
  • housing 14 com rises a straight length of plain tubing, formed of a suitable material that will resist the relatively high temperatures that burner 12 generates, uniformly, along the entire outside surface of tubing 14.
  • tubing 14 is about 13 inches in length, having an outside diameter of about 1% inches, an inside diameter of about one inch, and formed of a stainless steel based material known as Hastelloy, available from the Haynes Stellite Company.
  • Other suitable materials include stainless steel.
  • air was supplied under pressure from about 1 p-.s.i.g. to about 2 p.s.i.g., and No. 2 fuel oil or kerosene was supplied at a rate of about .047 g.p.h.
  • the average uniform temperature along the entire length of tube 14 was about 1200 F. with a heat output in the range of 6500 to 12,000 B.t.u./hr.
  • the nozzle was of the air aspirating type, i.e., the air under pressure passing through the nozzle draws suflicient fuel into itself for proper combustion. Such nozzles are known, and any other suitable type of nozzle may be used.
  • the natural tendency is for the flame to create a hot spot or region of higher temperature adjacent the flame, with a decreasing temperature gradient away from the flame within the means housing the flame.
  • the present invention provides a combination of means within the main housing 14 which mitigate this effect to spread the heat from the flame through the entire length of the housing 14 to thereby create a uniform temperature on the outside surface of housing 14.
  • tube 14 is provided with a front end member 24, which fits within the inlet end of main housing 14 and is secured thereto by any suitable means such as the abutting shoulder 26, set screws, welding or the like.
  • End member 24 is formed with a venturi orifice 28 of reduced diameter.
  • the reduced venturi diameter was about 7 of an inch.
  • the nozzle is positioned in spaced relation and in axial alignment with venturi opening 28. The gap permits entry of ambient or secondary air and may be on the order of about A to about of an inch, dependent upon a combination of factors such as the angle of spray from nozzle 16, flow rate, heat rate, and other factors well known to those skilled in this art.
  • End member 24 is formed with a plurality of longitudinal secondary air openings 30, the operation of which will appear below.
  • eight openings 30 each of a diameter of about A of an inch located on an imaginary circle having a diameter of about W inch were provided in end member 24.
  • a combustion chamber sleeve 32 is provided with its front end in abutting relation to the rear surface of end member 24.
  • the inside diameter of sleeve 32 is larger than the imaginary diameter on which openings 30 are located plus the diameter of one of said openings, so that said openings will communicate atmosphere to the inside of sleeve 32.
  • the outside diameter of sleeve 32 is smaller than the inside diameter of main housing 14 so that a longitudinal annular space is created between the sleeve 32 and the housing 1-4. In the successfully built embodiment of the invention, the outside diameter of sleeve 32 was about of an inch.
  • each end of the sleeve is formed with a plurality of upstanding lugs 34, the outer ends of which abut the inside of the main housing 14.
  • Sleeve 32 is reversible, and each end is provided with a plurality of Openings 36, which provide a recirculation of hot gases, as will appear in more detail below.
  • the sleeve 32 is held in place Within the tube 14 by welding to end member 24.
  • Means are provided to increase the residence time of the hot combustion gases at selected, spaced positions along the length of housing 14 to achieve the desirable uniform external temperature as described above.
  • a first space of predetermined length separates the outlet end of the combustion sleeve 32 from a first restricting means 38, and a second shorter space separates restrictor 38 from a second, longer restrictor 40.
  • Restrictor 38 is in the form of a flat strip of a suitable metal, such'as stainless steel or Hastelloy, to which has been imparted a 180 twist.
  • Restrictor 40 is similar to restrictor 38 except that it is substantially longer and has a twist slightly less than 180 imparted to it, and is placed in the main housing 14 so that the direction of twist is opposite to the direction of twist of restrictor 38.
  • the space between sleeve 32 and restrictor 38 is substantially longer than the space between the restrictors because said first mentioned space contains gases that are at a temperature very close to the temperature at which it is desired to maintain housing 14.
  • the first restrictor 38 is relatively short because residence time of the gases need not be increased a great deal, relatively, to permit said gases to bring the housing to the desired uniform temperature.
  • the space between the restrictors is relatively short because the gases here have given up a relatively large portion of the heat they contain.
  • Restrictor 40 is twisted oppositely to restrictor 38 to increase the residence time of the combustion gases in the space between the restrictors.
  • Restrictor 40 is relatively long and extends all the Way to the exit end of the housing 14 because the gases here are relatively cool by the time they arrive at the exit end and residence time must be increased substantially to bring the adjacent portion of housing 14 to the desired uniform temperature.
  • Restrictor 40 is twisted less than 180 because excess restriction will cause the flame to flash back to the nozzle.
  • the restrictors are preferably held in place by spot welding for vertical or in motion operation, friction fit for horizontal stationary operation, or the like easily disassembled means since it may be desirable to move them for changes in the nozzle, fuel, flow rate, heat rate, or the like.
  • a finely divided pressurized mist of fuel and air is supplied from nozzle 16 through the gap between the nozzle and the inlet end of housing 14 and through the venturi throat 28.
  • the motion of the fuel and air mixture through the gap draws secondary air into itself from the gap.
  • the motion of the fuel and increased air mixture through the venturi throat draws still additional secondary air into itself through the row of openings 30 in the end member 24.
  • Combustion is initiated by any suitable ignition means, not shown, and the flame front is located at some position inwardly of the end member 24 and within the combustion sleeve 32. Recirculation hot gases will be drawn through the annular space between the sleeve 32 and the tube 14, which layer of combustion gases serves to insulate the adjacent regions of tubing 14 from the higher temperature of the flame itself.
  • the combustion gases proceed through the tubing 14, are slowed down to a relatively small extent by the first restrictor 38, are slowed in their passage through the space between the restrictors by the reversal of twist existing between the restrictors, and are still further slowed by second restrictor 40 for a relatively longer period of time.
  • a relatively uniform temperature is achieved over the entire length of the main tubing 14, including the region adjacent end member 24 to which heat is supplied by conduction through the metal parts in that region.
  • each of the elements shown in FIG. 2 contributes its portion alone and in combination with the other elements to achieve the uniform temperature along the outside of the main housing 14. Experiments have shown this to be so. With restrictor 40 removed, the temperature in the region of restrictor 38 increases, and the temperature at the exit and decreases. With restrictor 38 moved closer to sleeve 32, the front end of the burner is much hotter than the'exit end of the burner. If the sleeve 32 is omitted, the front end of the burner becomes considerably hotter at the expense of the remaining portions of the burner. When the tubular sleeve 32 was moved closer to restrictor 38, a cooler region was created between end member 24 and the sleeve, while the area immediately adjacent the sleeve experienced an increased temperature.
  • restrictor 38 helps in locating the flame front inside of the sleeve 32.
  • the burner of the invention may be used with virtually any fuel within the ability of the nozzle.
  • a vapor lock problem in the nozzle may occur. Because the nozzle 16 is in closely spaced relation to the inlet end of the burner 12, the heat from the burner may cause such highly volatile fuels to vaporize prematurely in the nozzle, thus disrupting normal fuel flow.
  • heat shield means 42 may be interposed between the nozzle and the inlet end of the burner when using such fuels, if required.
  • Shield 42 may take any convenient form, and for example purposes is shown as a curved metal disc formed with an opening 44 to permit passage of the spray from the nozzle therethrough.
  • Shield 42 may be mounted on the nozzle and/ or the supply pipes 18 and 20 or other part of the apparatus with the use of heat insulating means, all not shown but in a manner known to those skilled in this art, so that the shield will not heat the portion of the apparatus on which it is mounted by conduction.
  • the convex surface 46 of the shield preferably faces the burner and is provided with a heat reflective finish, such as bright chromium plating, to maximize the amount of heat directed away from the nozzle.
  • a burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing being imperforate over its length and comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, and combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means.
  • said combustible mixture supplying means comprising a fuel nozzle, means to position and fuel nozzle in spaced relation to said constricted opening, whereby the velocity of said combustible mixture issuing from said fuel nozzle will draw air into itself from the gap between said fuel nozzle and said inlet end of said housing.
  • said constricting opening forming means comprising an end member seated within the inlet end of said housing, said end member being of generally toroidal configuration and formed with a curved innermost radial surface, whereby said constricted opening comprises a venturi opening.
  • said flame containing means comprising a sleeve having a diameter a predetermined amount less than the inside diameter of said housing, and said sleeve comprising means to hold said sleeve in concentric relation to said housing.
  • said concentric holding means comprising a plurality of upstanding lugs formed on the ends of said sleeve, the end edges of said lugs being adapted to tightly fit within the inside diameter of said housing.
  • said restricting means comprising a first twisted member extending a predetermined distance into said housing from said outlet end and a second twisted member in spaced relation to said first twisted member positioned mediately the ends of said housing.
  • a burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said constricting opening forming means comprising an end member seated within the inlet end of said housing, said end member being of generally toroidal configuration and formed with a curved innermost radial surface, whereby said constricted opening comprises a vent
  • a burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said flame containing means comprising a sleeve having a diameter a predetermined amount less than the inside diameter of said housing, said sleeve comprising means to hold said sleeve in concentric relation to said housing, said means
  • a burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said 7 housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said combustible mixture supplying means comprising a fuel nozzle, means to position said fuel nozzle in spaced relation to said constricted opening, whereby the velocity of said combustible mixture issuing from said fuel nozzle will draw air

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  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
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  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Description

A. BIBER TUBULAR UNIFORM TEMPERATURE HEAT SOURCE Filed April 19, 1968 INVENTOR.
14L BERT B/BER United States Patent 3,510,238 TUBULAR UNIFORM TEMPERATURE HEAT SOURCE Albert Biher, Verona, Pa., assignor to Gulf Research 8: Development Company, Pittsburgh, Pa., a corporation of Delaware Filed Apr. 19, 1968, Ser. No. 722,690 Int. Cl. F23d 11/02 U.S. Cl. 431116 12 Claims ABSTRACT OF THE DISCLOSURE A uniform temperature heat source utilizing liquid fuel comprising means to reduce the amount of heat imparted to the tubular housing by the combustion products adjacent the flame, and means to gradually increase the amount of heat imparted along the tubular housing away from the flame. The burner is particularly suited for use in thermoelectric generators.
This invention relates to the art of oil burners, and more particularly is concerned with a relatively small burner which is of generally tubular shape and which will produce a substantially uniform temperature along its outer wall.
A burner of the character described is particularly useful in fabricating small, portable, thermoelectric generators. The use of such portable generators is described in a paper published by the American Society of Automotive lEngineers, Paper No. 670452, dated May 1519, 1967, by A. Bayne Neild. Generally, the heat source is surrounded by an elongated annular thermopile, and the temperature difference across the thermopile is utilized to produce electrical energy in the thermopile. The thermopile itself, and, in fact, use in thermoelectric generators itself, does not form a material part of the present invention, since the burner of the invention can be used in any application wherein a tubular uniform temperature heat source is required. For example, water or air heat exchangers, and heat treating and annealing furnaces, rolls for sheet metal processing, drying equipment, and bake ovens. The burner of the invention provides a radiant heat source without flame or combustion gases in the external heated area.
An object of the invention is to provide a burner of the character described which will be rugged and insensitive to orientation. In its use as a heat source for a portable thermoelectric generator, the burner must be able to operate, for example, in a military back pack to be carried by a soldier and thus be capable of operation in all attitudes, vertically, horizontally, and while in motion. Because of the self-contained nature of the burner of the invention, it will operate under all of these highly adverse conditions. It will be understood that some suitable means, such as a check valve or the like not shown, will be provided to prevent direct flow of fuel from the fuel source.
Another object of this invention is to provide a burner of the character described which shall be simple and economical to fabricate, positive and highly reliable in operation, able to spontaneously re-light itself if it should extinguish during operation, inexpensive, and practical and efiicient to a high degree in use.
The above and other advantages of the invention will be pointed out or will become evident in the following detailed description and claims, and in the accompanying drawing also forming a part of the disclosure, in which: FIG. 1 is a side elevational view of the burner of the invention embodied in a thermoelectric generator;
3,510,238 Patented May 5, 1970 and FIG. 2 is a cross-sectional side elevational view of the burner of the invention.
Referring now in detail to the drawing, 10 designates a thermoelectric generator embodying the burner 12 of the invention. Burner 12 comprises a burner housing tube 14 and a fuel nozzle 16. The nozzle 16 will be selected to suit the fuel, and will usually include means to supply air under pressure and fuel under pressure or suction through the feed lines 18 and 20 from a fuel source and an air compressor, respectively, forming part of the thermoelectric generator, but not shown. For military use, it is desirable that nozzle 16 be able to burn any fuel available such as gasoline, diesel fuel, kerosene, jet and aviation fuel and the like.
Generator 10 comprises an outer housing 22 which is tubular and of a length slightly shorter than the overall length of housing tube 14. The annular space between housing 22 and tube 14 is filled with a thermopile, not shown. The temperature difference between outside of housing 22 and the outside of tube 14 across the thermopile is the motive force which produces electricity in the thermopile. Generator 10 will also include suitable ignition means, not shown, in the form of spark electrodes, a glow plug, or other suitable means, which will be positioned at a suitable location. The positioning of the ignition means, and the ancillary ignition equipment required, does not form a material part of the present invention.
Referring now to FIG. 2, the burner 12 of the invention is shown in detail. Housing 14 com rises a straight length of plain tubing, formed of a suitable material that will resist the relatively high temperatures that burner 12 generates, uniformly, along the entire outside surface of tubing 14. In the embodiment of the invention which has been successfully built, tubing 14 is about 13 inches in length, having an outside diameter of about 1% inches, an inside diameter of about one inch, and formed of a stainless steel based material known as Hastelloy, available from the Haynes Stellite Company. Other suitable materials include stainless steel.
In said successful embodiment, air was supplied under pressure from about 1 p-.s.i.g. to about 2 p.s.i.g., and No. 2 fuel oil or kerosene was supplied at a rate of about .047 g.p.h. The average uniform temperature along the entire length of tube 14 was about 1200 F. with a heat output in the range of 6500 to 12,000 B.t.u./hr. The nozzle was of the air aspirating type, i.e., the air under pressure passing through the nozzle draws suflicient fuel into itself for proper combustion. Such nozzles are known, and any other suitable type of nozzle may be used.
In any burner where the flame is contained, the natural tendency is for the flame to create a hot spot or region of higher temperature adjacent the flame, with a decreasing temperature gradient away from the flame within the means housing the flame. The present invention provides a combination of means within the main housing 14 which mitigate this effect to spread the heat from the flame through the entire length of the housing 14 to thereby create a uniform temperature on the outside surface of housing 14.
Referring now in detail to FIG. 2, tube 14 is provided with a front end member 24, which fits within the inlet end of main housing 14 and is secured thereto by any suitable means such as the abutting shoulder 26, set screws, welding or the like. End member 24 is formed with a venturi orifice 28 of reduced diameter. In the embodiment .of the invention which has been successfully built, the reduced venturi diameter was about 7 of an inch. As shown in FIG. 1, the nozzle is positioned in spaced relation and in axial alignment with venturi opening 28. The gap permits entry of ambient or secondary air and may be on the order of about A to about of an inch, dependent upon a combination of factors such as the angle of spray from nozzle 16, flow rate, heat rate, and other factors well known to those skilled in this art. End member 24 is formed with a plurality of longitudinal secondary air openings 30, the operation of which will appear below. In the successfully built embodiment of the invention, eight openings 30 each of a diameter of about A of an inch located on an imaginary circle having a diameter of about W inch were provided in end member 24.
Means are provided to prevent the creation of a hot spot at the inlet end of housing 14. To this end, a combustion chamber sleeve 32 is provided with its front end in abutting relation to the rear surface of end member 24. The inside diameter of sleeve 32 is larger than the imaginary diameter on which openings 30 are located plus the diameter of one of said openings, so that said openings will communicate atmosphere to the inside of sleeve 32. The outside diameter of sleeve 32 is smaller than the inside diameter of main housing 14 so that a longitudinal annular space is created between the sleeve 32 and the housing 1-4. In the successfully built embodiment of the invention, the outside diameter of sleeve 32 was about of an inch. Means are provided to hold sleeve 32 centralized within housing 14. To this end, each end of the sleeve is formed with a plurality of upstanding lugs 34, the outer ends of which abut the inside of the main housing 14. Sleeve 32 is reversible, and each end is provided with a plurality of Openings 36, which provide a recirculation of hot gases, as will appear in more detail below. The sleeve 32 is held in place Within the tube 14 by welding to end member 24.
Means are provided to increase the residence time of the hot combustion gases at selected, spaced positions along the length of housing 14 to achieve the desirable uniform external temperature as described above. To this end, a first space of predetermined length separates the outlet end of the combustion sleeve 32 from a first restricting means 38, and a second shorter space separates restrictor 38 from a second, longer restrictor 40. Restrictor 38 is in the form of a flat strip of a suitable metal, such'as stainless steel or Hastelloy, to which has been imparted a 180 twist. Restrictor 40 is similar to restrictor 38 except that it is substantially longer and has a twist slightly less than 180 imparted to it, and is placed in the main housing 14 so that the direction of twist is opposite to the direction of twist of restrictor 38. The space between sleeve 32 and restrictor 38 is substantially longer than the space between the restrictors because said first mentioned space contains gases that are at a temperature very close to the temperature at which it is desired to maintain housing 14. The first restrictor 38 is relatively short because residence time of the gases need not be increased a great deal, relatively, to permit said gases to bring the housing to the desired uniform temperature. The space between the restrictors is relatively short because the gases here have given up a relatively large portion of the heat they contain. Restrictor 40 is twisted oppositely to restrictor 38 to increase the residence time of the combustion gases in the space between the restrictors. Restrictor 40 is relatively long and extends all the Way to the exit end of the housing 14 because the gases here are relatively cool by the time they arrive at the exit end and residence time must be increased substantially to bring the adjacent portion of housing 14 to the desired uniform temperature. Restrictor 40 is twisted less than 180 because excess restriction will cause the flame to flash back to the nozzle. The restrictors are preferably held in place by spot welding for vertical or in motion operation, friction fit for horizontal stationary operation, or the like easily disassembled means since it may be desirable to move them for changes in the nozzle, fuel, flow rate, heat rate, or the like.
By way of example, the following lengths and distances were incorporated in the successfully built embodiment of the invention:
Operation A finely divided pressurized mist of fuel and air is supplied from nozzle 16 through the gap between the nozzle and the inlet end of housing 14 and through the venturi throat 28. The motion of the fuel and air mixture through the gap draws secondary air into itself from the gap. The motion of the fuel and increased air mixture through the venturi throat draws still additional secondary air into itself through the row of openings 30 in the end member 24. Combustion is initiated by any suitable ignition means, not shown, and the flame front is located at some position inwardly of the end member 24 and within the combustion sleeve 32. Recirculation hot gases will be drawn through the annular space between the sleeve 32 and the tube 14, which layer of combustion gases serves to insulate the adjacent regions of tubing 14 from the higher temperature of the flame itself. The combustion gases proceed through the tubing 14, are slowed down to a relatively small extent by the first restrictor 38, are slowed in their passage through the space between the restrictors by the reversal of twist existing between the restrictors, and are still further slowed by second restrictor 40 for a relatively longer period of time. Thus, a relatively uniform temperature is achieved over the entire length of the main tubing 14, including the region adjacent end member 24 to which heat is supplied by conduction through the metal parts in that region.
Each of the elements shown in FIG. 2 contributes its portion alone and in combination with the other elements to achieve the uniform temperature along the outside of the main housing 14. Experiments have shown this to be so. With restrictor 40 removed, the temperature in the region of restrictor 38 increases, and the temperature at the exit and decreases. With restrictor 38 moved closer to sleeve 32, the front end of the burner is much hotter than the'exit end of the burner. If the sleeve 32 is omitted, the front end of the burner becomes considerably hotter at the expense of the remaining portions of the burner. When the tubular sleeve 32 was moved closer to restrictor 38, a cooler region was created between end member 24 and the sleeve, while the area immediately adjacent the sleeve experienced an increased temperature. When the holes 36 in the sleeve 32 were plugged, ignition occurred in the region of restrictor 38. With restrictor 38 removed, the entrance end was very much colder than the remaining portions, and ignition was diificult to achieve. Thus, it can be seen that in addition to increasing the residence time of the gases when they pass over it, restrictor 38 helps in locating the flame front inside of the sleeve 32.
As mentioned above, the burner of the invention may be used with virtually any fuel within the ability of the nozzle. However, when burning certain highly volatile fuels, such as gasoline, a vapor lock problem in the nozzle may occur. Because the nozzle 16 is in closely spaced relation to the inlet end of the burner 12, the heat from the burner may cause such highly volatile fuels to vaporize prematurely in the nozzle, thus disrupting normal fuel flow.
Referring again to FIG. 1, heat shield means 42 may be interposed between the nozzle and the inlet end of the burner when using such fuels, if required. Shield 42 may take any convenient form, and for example purposes is shown as a curved metal disc formed with an opening 44 to permit passage of the spray from the nozzle therethrough. Shield 42 may be mounted on the nozzle and/ or the supply pipes 18 and 20 or other part of the apparatus with the use of heat insulating means, all not shown but in a manner known to those skilled in this art, so that the shield will not heat the portion of the apparatus on which it is mounted by conduction. The convex surface 46 of the shield preferably faces the burner and is provided with a heat reflective finish, such as bright chromium plating, to maximize the amount of heat directed away from the nozzle.
While the invention has been described in detail above, it is to be understood that this detailed description is by way of example only, and the protection granted is to be limited only within the spirit of the invention and the scope of the following claims.
I claim:
1. A burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing being imperforate over its length and comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, and combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means.
2. The combination of claim 1, said combustible mixture supplying means comprising a fuel nozzle, means to position and fuel nozzle in spaced relation to said constricted opening, whereby the velocity of said combustible mixture issuing from said fuel nozzle will draw air into itself from the gap between said fuel nozzle and said inlet end of said housing.
3. The combination of claim 1, said constricting opening forming means comprising an end member seated within the inlet end of said housing, said end member being of generally toroidal configuration and formed with a curved innermost radial surface, whereby said constricted opening comprises a venturi opening.
4. The combinaion of claim 1, said flame containing means comprising a sleeve having a diameter a predetermined amount less than the inside diameter of said housing, and said sleeve comprising means to hold said sleeve in concentric relation to said housing.
5. The combination of claim 4, said concentric holding means comprising a plurality of upstanding lugs formed on the ends of said sleeve, the end edges of said lugs being adapted to tightly fit within the inside diameter of said housing.
6. The combination of claim 1, said restricting means comprising a first twisted member extending a predetermined distance into said housing from said outlet end and a second twisted member in spaced relation to said first twisted member positioned mediately the ends of said housing.
7. The combination of claim 6, said first twisted memher being twisted in a direction opposite to the direction of twist of said second twisted member.
8. The combination of claim 6, said first twisted member having a length greater than the length of said second twisted member.
9. The combination of claim 2, and heat shield means interposed between said nozzle and said inlet end of said burner.
10. A burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said constricting opening forming means comprising an end member seated within the inlet end of said housing, said end member being of generally toroidal configuration and formed with a curved innermost radial surface, whereby said constricted opening comprises a venturi opening, said flame containing means comprising a sleeve having a diameter a predetermined amount less than the inside diameter of said housing, said sleeve comprising means to hold said sleeve in concentric relation to said housing, said secondary air supply means comprising a plurality of longitudinal openings formed in said end member with the outlet ends of said longitudinal openings positioned on a diameter less than the inside diameter of said sleeve, whereby the velocity of said combustible mixture through said venturi will draw additional air for combustion through said longitudinal openings into said combustible mixture within said sleeve.
11. A burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said flame containing means comprising a sleeve having a diameter a predetermined amount less than the inside diameter of said housing, said sleeve comprising means to hold said sleeve in concentric relation to said housing, said means to supply a portion of the combustion products to the annular space between said sleeve and said housing comprising a first plurality of openings formed in spaced relation to the outlet end of said sleeve, and a second plurality of openings formed in spaced relation to the inlet end of said sleeve, both of said pluralities of openings communicating said annular space with the space within said sleeve.
12. A burner comprising an elongated hollow housing adapted to produce a uniform temperature over the length of the housing, said housing comprising an inlet end and an outlet end, means to form a constricted opening at the inlet end of said housing, means to supply a combustible mixture through said constricted opening, means to supply secondary air for combustion to said combustible mixture after said combustible mixture has passed through said constricted opening, flame containing means within said 7 housing extending from said opening forming means a predetermined distance towards said outlet end, said flame containing means comprising means to supply a portion of the products of combustion to the annular space between the inside of said housing and the outside of said flame containing means, combustion products restricting means in said housing in spaced relation to said outlet end and to said flame containing means, said combustible mixture supplying means comprising a fuel nozzle, means to position said fuel nozzle in spaced relation to said constricted opening, whereby the velocity of said combustible mixture issuing from said fuel nozzle will draw air into itself from the gap between said fuel nozzle and said inlet end of said housing, and heat shield means interposed between said nozzle and said inlet end of said burner, said heat shield means comprising a curved plate having its convex side facing said inlet end of said burner and provided 8 with a heat reflective coating on the outer surface of said convex side.
References Cited UNITED STATES PATENTS 166,180 8/1875 Bailey. 1,975,033 9/1934 Wolif 431-9 XR 2,368,179 1/1945 Turpin 431347 2,560,275 7/1951 Clark 110970 2,918,117 12/1959 Griflin 431-116 3,238,990 3/1966 Linde et a1 431-116 FREDERICK L. MATTERSON, JR., Primary Examiner H. B. RAMEY, Assistant Examiner U.S. Cl. X.R. 431-350
US722690A 1968-04-19 1968-04-19 Tubular uniform temperature heat source Expired - Lifetime US3510238A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844707A (en) * 1971-05-11 1974-10-29 Wingaersheek Turbine Co Inc Low cost, wind proof cigarette lighter burner
US3915623A (en) * 1973-08-20 1975-10-28 Wingaersheek Wind-proof cigarette lighter burner
US4318688A (en) * 1979-05-08 1982-03-09 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Oil burner
US4639215A (en) * 1980-02-01 1987-01-27 Bernard Marks And Company Limited Gas burner
US6743011B2 (en) * 2001-12-19 2004-06-01 Corning Incorporated Multi-layer burner module, adapter, and assembly therefor
US9672474B2 (en) 2014-06-30 2017-06-06 Amazon Technologies, Inc. Concurrent binning of machine learning data

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US166180A (en) * 1875-08-03 Improvement in fire-tubes for steam-boilers
US1975033A (en) * 1931-02-23 1934-09-25 Firm Selas Ag Oil burner
US2368179A (en) * 1943-12-17 1945-01-30 Hauck Mfg Co Reigniting liquid-fuel burner
US2560275A (en) * 1948-02-19 1951-07-10 Acme Tank & Welding Co Baffle for boiler tubes
US2918117A (en) * 1956-10-04 1959-12-22 Petro Chem Process Company Inc Heavy fuel burner with combustion gas recirculating means
US3238990A (en) * 1963-03-29 1966-03-08 Von Linde Burner

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US166180A (en) * 1875-08-03 Improvement in fire-tubes for steam-boilers
US1975033A (en) * 1931-02-23 1934-09-25 Firm Selas Ag Oil burner
US2368179A (en) * 1943-12-17 1945-01-30 Hauck Mfg Co Reigniting liquid-fuel burner
US2560275A (en) * 1948-02-19 1951-07-10 Acme Tank & Welding Co Baffle for boiler tubes
US2918117A (en) * 1956-10-04 1959-12-22 Petro Chem Process Company Inc Heavy fuel burner with combustion gas recirculating means
US3238990A (en) * 1963-03-29 1966-03-08 Von Linde Burner

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844707A (en) * 1971-05-11 1974-10-29 Wingaersheek Turbine Co Inc Low cost, wind proof cigarette lighter burner
US3915623A (en) * 1973-08-20 1975-10-28 Wingaersheek Wind-proof cigarette lighter burner
US4318688A (en) * 1979-05-08 1982-03-09 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Oil burner
US4639215A (en) * 1980-02-01 1987-01-27 Bernard Marks And Company Limited Gas burner
US6743011B2 (en) * 2001-12-19 2004-06-01 Corning Incorporated Multi-layer burner module, adapter, and assembly therefor
US9672474B2 (en) 2014-06-30 2017-06-06 Amazon Technologies, Inc. Concurrent binning of machine learning data

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