US1818471A - Burner - Google Patents
Burner Download PDFInfo
- Publication number
- US1818471A US1818471A US420897A US42089730A US1818471A US 1818471 A US1818471 A US 1818471A US 420897 A US420897 A US 420897A US 42089730 A US42089730 A US 42089730A US 1818471 A US1818471 A US 1818471A
- Authority
- US
- United States
- Prior art keywords
- tube
- gas
- barrel
- air
- helix
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/82—Preventing flashback or blowback
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/62—Mixing devices; Mixing tubes
- F23D14/64—Mixing devices; Mixing tubes with injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/14—Special features of gas burners
- F23D2900/14701—Swirling means inside the mixing tube or chamber to improve premixing
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87571—Multiple inlet with single outlet
- Y10T137/87587—Combining by aspiration
- Y10T137/87619—With selectively operated flow control means in inlet
- Y10T137/87627—Flow control means is located in aspirated fluid inlet
Definitions
- My invention relates to burners of the class generally designated Bunsen burners, and
- Such burners comprise, in general, a gas and air mixing tube, a gas inlet orifice which is arranged axially of the tube, and one or more relatively large valved air inlet ports in the tube.
- the gas and air enter one end ,10 of the tube, and, in burners heretofore provided, are mixedv to a greater or lesser extent as they pass through the tube.
- burners of this simple construction have been quite well adapted for ordinary uses, they Y 15 havebeen subject to disadvantages resulting from inadequate mixing ofthe gas and air, one of the chief disadvantages being that such burners have exhibited a marked tendf ency to backfire, so that combustion, instead of taking place only at the outlet end of the tube, has at tim-es taken place immediately adjacent the gas inlet orifice.
- Figure l isa central vertical sectional view of a burner embodying my invention.
- Figure 2 is a detail View in front elevation ofl a mixing tube, with parts within shown by dotted lines; Y
- Figure 3- is a detail perspective view in elevation of a helix
- Figure l is a detail view in elevation of an air valve sleeve; and 1 1lIigure 5 is a top plan view of the burner tu e.
- a burner including a base A, a gasvalve B securedv to thebase, and a burner tube generally designated C mounted on the gas valve.
- the base A is Aformedwith acentrally located threaded opening 1 intoV which l'is' screwed an exteriorly kthreaded boss 2 on a gas valve casing 3.
- the valve casing is formed with a vcentral chambers: which is adapted to receive gas from a nipple 5 threadably connected to the body 3, and to discharge gas upwardly into the tube C through a gas orifice 6 locatedfaxially of the tube.
- the boss 2 on the valve body is formed with an internally threaded opening 7 into which is screwed a threaded valve stem 8,
- the barrel is also provided with air inlet ports 'I3-13 i and with a rotatable sleeve 14 mounted on the outside of the barrel and having 'openings -15 adapted to register with the openings 13-13 in the barrel forcontrollin the ow of air into the barrel.
- the helix 12 is so constructed that its pitch, or in other words the distance between adjacent turns of the helix, increases from the inlet end of the tube towards the outlet end thereof. Because of this increasing pitch of the helix, the air entering the tube and travelling close to the inner surface of the tube and upwardly towards the outlet end will be given a rapid swirling motion and also an expansion of the air which promotes better mixing of the air and gas; and, at the same time, the air is deflected inwardly towards the center of the tube which prevents the slow movement of a combustible mixture along the inner surface Aof the tube and thus lessens the tendency for the flame to backfire.
- the helix is preferably of gradually increasing pitch and thus produces the same effect as a Vent-uri tube kin that the gas is graduallyexpanded as it flows around the successive turns of the helix and up through the tube. It is evident that any particular volume of gas, say for instance that contained between the second'and third turns of the helix at a given ⁇ instant,-will, uponflowing into the space between the third andfourth turns thereof, tend to occupy a larger volume, since the third and ⁇ fourth turns are :spaced farther apart than the --second and third turns.
- the' helix-be of varying pitch and preferably the pitch in-A creases from the inner end ofthe tube to the outer end thereof, although it is not neces- ⁇ sary that the pitch vary uniformly or even :'Ihus, the first and'second turns may be spaced the same distance apart as the second and third turns,
- T he helix 12 is illustrated as comprising a spirally wound springwhich is positioned in the barrel 10 and maintained therein by the frictional contact of the several turns of the spring with the inner surface of thebarrel. Obviously, the helix may, if desired, be
- Vwithfthe barrel formed integrally Vwithfthe barrel; but theY form illustrated is believed to be most suit-V n able in that it is adapted to be easily applied l to a tube of standardl form.
- a reticulated baflie 16 which includes a rim 17 adapted to be frictionally held within the upper end of the barrel and a screen 18 secured to the rim.
- a mixing tube for a burner comprising a barrel having an inlet end and an outlet end, and a helix in the barrel and arranged coa-xiallv therewith, the pitch of said helix Y increasing from the inlet end of said tube to Y and means in said barrel for expanding gas passing fromthe inlet end to the outlet end thereof in the manner of a Venturi tube,com prising a spirallywound element the turns of which are arranged in contacting relation with the inner surface of the barrel, the distance between adjacent turns of said elementI ⁇ increasing progressively from the inlet end 4to .the outlet end of the barrel.
- a burner mixing tube In a burner mixing tube, the comb-ination with a barrel havingv gas inlet and outlet ends, of aspirally wound spring posiz;l tionedl within-.said barrel and maintained therein by frictionalcontact of the spring with the inner surface ofthe barrel, the pitch of said spring increasing from the inlet end to the outlet endof said barrel.
- the combination with a gas and air mixing tube including a barrel having intake and outlet ends, of a gas inlet openand the outlet endof the barrel, tlievpitch of;u said helix increasing from said air port to said outlet end.
- the combination witha gas and air mixingtubre including a barrelhaving intake and outlet ends, of aV gas inletN opening at the intake endof the barrel and disposed substantially at ⁇ the axis thereof.
- a gas and air mixing tube including a barrel having intake and outlet ends, of a gas inlet opening at the intake end of the barrel and disposed substantially at the aXis thereof, and an air port in said barrel adjacent said gas inlet opening, the inner surface of said barrel being provided With a spiral of gradually increasing pitch from the intake end of said barrel to the outlet end thereof, the
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Description
Aug. 11, 1931.
BURNER H. A. GEAUQUE A Filed Jan. 15, 1930 (Itt'omegs Patented Aug. 11, 1931 UNITED STATES HARRY A. GEAUQUE, `OF GALESBURG, ILLINOIS BURNER Application filed January 15, 1930. Serial No. 420,897.
My invention relates to burners of the class generally designated Bunsen burners, and
more particularly to gas and air mixing tubes Y for this kind of burner.
Such burners comprise, in general, a gas and air mixing tube, a gas inlet orifice which is arranged axially of the tube, and one or more relatively large valved air inlet ports in the tube. The gas and air enter one end ,10 of the tube, and, in burners heretofore provided, are mixedv to a greater or lesser extent as they pass through the tube. Although burners of this simple construction have been quite well adapted for ordinary uses, they Y 15 havebeen subject to disadvantages resulting from inadequate mixing ofthe gas and air, one of the chief disadvantages being that such burners have exhibited a marked tendf ency to backfire, so that combustion, instead of taking place only at the outlet end of the tube, has at tim-es taken place immediately adjacent the gas inlet orifice. This tend-vv ency is, I believe, fundamentally due to the fact that the gas which enters the tube from aA relatively small orifice at the center of the tube flows through the center ofthe tubeat a lhigh velocity, whereas the'airV entering from the sides of the tube, and through relatively large ports, passes up through the tube ad-l jacentits inner surface at a relatively low velocity. By the time the air and gas have reaohedthe outlet end of the tube, a combustible'mixture has been formed adjacent the inner surface of the tube, and, since this mixture is travelling at a low velocity, it is quite easy for the flame to travel down through the tube along itsinner surface until the gas issuing from the gas nozzle is ignited at that point.
as to cause the gas and air passing through-the f tube to be given a rapid swirling movement and an expansion of the mixture for effecting '59 better mixing of the gas and air and at the I have found that by increasing the veloc` same time deflecting the mixture towards the center of the tube so as topreventthe Slow movement of a combustible mixture along the inner surface of the tube.
vOther objects will become apparent from` the followingv description, the appended claims, and the several views of the invention illustrated in the drawings, in which:
Figure l isa central vertical sectional view of a burner embodying my invention;
Figure 2 is a detail View in front elevation ofl a mixing tube, with parts within shown by dotted lines; Y
Figure 3- is a detail perspective view in elevation of a helix;`
Figure l is a detail view in elevation of an air valve sleeve; and 1 1lIigure 5 is a top plan view of the burner tu e.
In the drawings, therevis shown a burner including a base A, a gasvalve B securedv to thebase, anda burner tube generally designated C mounted on the gas valve.
The base A is Aformedwith acentrally located threaded opening 1 intoV which l'is' screwed an exteriorly kthreaded boss 2 on a gas valve casing 3. The valve casing is formed with a vcentral chambers: which is adapted to receive gas from a nipple 5 threadably connected to the body 3, and to discharge gas upwardly into the tube C through a gas orifice 6 locatedfaxially of the tube.-
The boss 2 on the valve body is formed with an internally threaded opening 7 into which is screwed a threaded valve stem 8,
as at 11, anda helix 12 located within the barrel l0 between the gas inlet orifice 6 and the upper or outlet end of the barrel. The barrel is also provided with air inlet ports 'I3-13 i and with a rotatable sleeve 14 mounted on the outside of the barrel and having 'openings -15 adapted to register with the openings 13-13 in the barrel forcontrollin the ow of air into the barrel.
In accordance with my invention, the helix 12 is so constructed that its pitch, or in other words the distance between adjacent turns of the helix, increases from the inlet end of the tube towards the outlet end thereof. Because of this increasing pitch of the helix, the air entering the tube and travelling close to the inner surface of the tube and upwardly towards the outlet end will be given a rapid swirling motion and also an expansion of the air which promotes better mixing of the air and gas; and, at the same time, the air is deflected inwardly towards the center of the tube which prevents the slow movement of a combustible mixture along the inner surface Aof the tube and thus lessens the tendency for the flame to backfire. The helix is preferably of gradually increasing pitch and thus produces the same effect as a Vent-uri tube kin that the gas is graduallyexpanded as it flows around the successive turns of the helix and up through the tube. It is evident that any particular volume of gas, say for instance that contained between the second'and third turns of the helix at a given`instant,-will, uponflowing into the space between the third andfourth turns thereof, tend to occupy a larger volume, since the third and` fourth turns are :spaced farther apart than the --second and third turns. This of course results inV an expansion of that volume of gas and aconsequent more perfect mixing thereof.:l lVhen gas flows towardV the outlet end ofthe tube J and thereby successively passes around the several turns of the helix, it'will'be still further expanded. This comb-ined swirling and simultaneous expansion of the .gas and air progressively in a strict sense.
mixtureV has been found to mix the air and gas more efficientlythan was heretofore possible and to also prevent backfiring of the flame. c Y
To the attainment ofthe .obj ects of the invention, it is necessary that the' helix-be of varying pitch, and preferably the pitch in-A creases from the inner end ofthe tube to the outer end thereof, although it is not neces-` sary that the pitch vary uniformly or even :'Ihus, the first and'second turns may be spaced the same distance apart as the second and third turns,
Ybut the turns adjacent the inner end :of thetube should, in general, be closer together than the turns at the 'outer end of thev tube. T he helix 12 is illustrated as comprising a spirally wound springwhich is positioned in the barrel 10 and maintained therein by the frictional contact of the several turns of the spring with the inner surface of thebarrel. Obviously, the helix may, if desired, be
formed integrally Vwithfthe barrel; but theY form illustrated is believed to be most suit-V n able in that it is adapted to be easily applied l to a tube of standardl form.
For still better mixing of the air and-gas emerging from the o utletendof the tube, I
employ a reticulated baflie 16 which includes a rim 17 adapted to be frictionally held within the upper end of the barrel and a screen 18 secured to the rim.
Experience has demonstrated that a baille of this kind when used in connection with a burned vtube provided with a helix of varying pitch cooperates with the tube in providing a flame o f great uniformity and at the same time eliminates the heretofore existent tendency for the flame to backfire.
I claim as my invention:
1. A mixing tube for a burner, comprising a barrel having an inlet end and an outlet end, and a helix in the barrel and arranged coa-xiallv therewith, the pitch of said helix Y increasing from the inlet end of said tube to Y and means in said barrel for expanding gas passing fromthe inlet end to the outlet end thereof in the manner of a Venturi tube,com prising a spirallywound element the turns of which are arranged in contacting relation with the inner surface of the barrel, the distance between adjacent turns of said elementI` increasing progressively from the inlet end 4to .the outlet end of the barrel. c
4. In a burner mixing tube, the comb-ination with a barrel havingv gas inlet and outlet ends, of aspirally wound spring posiz;l tionedl within-.said barrel and maintained therein by frictionalcontact of the spring with the inner surface ofthe barrel, the pitch of said spring increasing from the inlet end to the outlet endof said barrel. f 5. In a burner, the combination with a gas and air mixing tube including a barrel having intake and outlet ends, of a gas inlet openand the outlet endof the barrel, tlievpitch of;u said helix increasing from said air port to said outlet end. Y
6. In a burner, the combination witha gas and air mixingtubre including a barrelhaving intake and outlet ends, of aV gas inletN opening at the intake endof the barrel and disposed substantially at `the axis thereof.
an air port in said barrel adjacent the intake end thereof, and a helix mounted in contactingrelation withthe inner surfaceof the bare..
ing atthe intake vend of the barrel and disposed substantially at the axis thereof, an;
rel and disposed between said air port and the outlet end of the barrel, the pitch of said helix gradually increasing from said air port to said outlet end, and a screen at the outlet end of said barrel.
7. In a burner, the combination with a gas and air mixing tube including a barrel having intake and outlet ends, of a gas inlet opening at the intake end of the barrel and disposed substantially at the aXis thereof, and an air port in said barrel adjacent said gas inlet opening, the inner surface of said barrel being provided With a spiral of gradually increasing pitch from the intake end of said barrel to the outlet end thereof, the
minimum pitch of said spiral being adjacent said gas inlet opening and said air port, whereby gas and air passing from the inlet to the outlet end of the barrel will be expanded as in a Venturi tube.
In testimony whereof, I have hereunto subscribed my name.
HARRY A. GEAUQUE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US420897A US1818471A (en) | 1930-01-15 | 1930-01-15 | Burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US420897A US1818471A (en) | 1930-01-15 | 1930-01-15 | Burner |
Publications (1)
Publication Number | Publication Date |
---|---|
US1818471A true US1818471A (en) | 1931-08-11 |
Family
ID=23668292
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US420897A Expired - Lifetime US1818471A (en) | 1930-01-15 | 1930-01-15 | Burner |
Country Status (1)
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US (1) | US1818471A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2776706A (en) * | 1953-10-09 | 1957-01-08 | Lee H Drake | Mixing and turbulence producing means for a gas burner tip |
US3006738A (en) * | 1957-10-10 | 1961-10-31 | Degussa | Burner for production of finely divided oxides |
US3322506A (en) * | 1963-03-19 | 1967-05-30 | Columbian Carbon | Carbon black apparatus |
US3408005A (en) * | 1966-05-09 | 1968-10-29 | Willard R. Struble | Snow making nozzle |
EP0132831A2 (en) * | 1983-07-27 | 1985-02-13 | Philipp Kreis GmbH & Co. TRUMA-Gerätebau | Gas burner, particularly for liquid gas, to be mounted in a heat exchanger |
US4715354A (en) * | 1984-08-03 | 1987-12-29 | Roberto Longobardi | Fuel-economy and emission-control device for internal combustion engines |
US4732559A (en) * | 1986-02-11 | 1988-03-22 | Uniweld Products Incorporated | Combustion device |
US4781578A (en) * | 1984-01-24 | 1988-11-01 | John Zink Company | Pilot burner apparatus |
US4846670A (en) * | 1986-02-11 | 1989-07-11 | Pearl Ii David S | Combustion device |
US6015286A (en) * | 1996-09-11 | 2000-01-18 | Windmill Kabushiki Kaisha | Internal-combustion type of gas lighter |
US6213761B1 (en) * | 1999-08-10 | 2001-04-10 | The Coleman Company, Inc. | Heating apparatus |
WO2007118737A1 (en) * | 2006-04-11 | 2007-10-25 | Spot Spirit Of Technology Ag | Method and device for allowing better heat transfer rates of impulse burners |
US20080179061A1 (en) * | 2006-11-13 | 2008-07-31 | Alberta Energy Partners, General Partnership | System, apparatus and method for abrasive jet fluid cutting |
WO2012001714A1 (en) * | 2010-06-30 | 2012-01-05 | Sabaf S.P.A. | Gas burner |
US8475230B2 (en) * | 2008-03-10 | 2013-07-02 | The Curators Of The University Of Missouri | Method and apparatus for jet-assisted drilling or cutting |
WO2014170830A1 (en) | 2013-04-16 | 2014-10-23 | Cti S.A. | Gas stove oven burner, and method for its manufacture |
-
1930
- 1930-01-15 US US420897A patent/US1818471A/en not_active Expired - Lifetime
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2776706A (en) * | 1953-10-09 | 1957-01-08 | Lee H Drake | Mixing and turbulence producing means for a gas burner tip |
US3006738A (en) * | 1957-10-10 | 1961-10-31 | Degussa | Burner for production of finely divided oxides |
US3322506A (en) * | 1963-03-19 | 1967-05-30 | Columbian Carbon | Carbon black apparatus |
US3408005A (en) * | 1966-05-09 | 1968-10-29 | Willard R. Struble | Snow making nozzle |
EP0132831A2 (en) * | 1983-07-27 | 1985-02-13 | Philipp Kreis GmbH & Co. TRUMA-Gerätebau | Gas burner, particularly for liquid gas, to be mounted in a heat exchanger |
DE3327140A1 (en) * | 1983-07-27 | 1985-02-14 | Philipp Kreis GmbH & Co Truma-Gerätebau, 8000 München | GAS BURNER, ESPECIALLY FOR LIQUID GAS, FOR INSTALLATION IN A HEAT EXCHANGER |
EP0132831A3 (en) * | 1983-07-27 | 1985-07-03 | Philipp Kreis Gmbh & Co. Truma-Geratebau | Gas burner, particularly for liquid gas, to be mounted in a heat exchanger |
US4781578A (en) * | 1984-01-24 | 1988-11-01 | John Zink Company | Pilot burner apparatus |
US4715354A (en) * | 1984-08-03 | 1987-12-29 | Roberto Longobardi | Fuel-economy and emission-control device for internal combustion engines |
US4846670A (en) * | 1986-02-11 | 1989-07-11 | Pearl Ii David S | Combustion device |
US4732559A (en) * | 1986-02-11 | 1988-03-22 | Uniweld Products Incorporated | Combustion device |
US6015286A (en) * | 1996-09-11 | 2000-01-18 | Windmill Kabushiki Kaisha | Internal-combustion type of gas lighter |
US6213761B1 (en) * | 1999-08-10 | 2001-04-10 | The Coleman Company, Inc. | Heating apparatus |
WO2007118737A1 (en) * | 2006-04-11 | 2007-10-25 | Spot Spirit Of Technology Ag | Method and device for allowing better heat transfer rates of impulse burners |
US20090084036A1 (en) * | 2006-04-11 | 2009-04-02 | Oliver Neumann | Method and device for achieving better heat transfer when using pulse heaters |
US20080179061A1 (en) * | 2006-11-13 | 2008-07-31 | Alberta Energy Partners, General Partnership | System, apparatus and method for abrasive jet fluid cutting |
US8475230B2 (en) * | 2008-03-10 | 2013-07-02 | The Curators Of The University Of Missouri | Method and apparatus for jet-assisted drilling or cutting |
WO2012001714A1 (en) * | 2010-06-30 | 2012-01-05 | Sabaf S.P.A. | Gas burner |
US9115892B2 (en) | 2010-06-30 | 2015-08-25 | Sabaf S.P.A. | Gas burner |
WO2014170830A1 (en) | 2013-04-16 | 2014-10-23 | Cti S.A. | Gas stove oven burner, and method for its manufacture |
US10401033B2 (en) | 2013-04-16 | 2019-09-03 | Cti S.A. | Gas stove oven burner, and method for its manufacture |
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