US3174526A - Atomizing burner unit - Google Patents

Atomizing burner unit Download PDF

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US3174526A
US3174526A US51409A US5140960A US3174526A US 3174526 A US3174526 A US 3174526A US 51409 A US51409 A US 51409A US 5140960 A US5140960 A US 5140960A US 3174526 A US3174526 A US 3174526A
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means
prechamber
combustion
mixing pipe
mixing
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US51409A
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Linde Robert Albert Von
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Linde Robert Albert Von
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C9/00Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • F23C9/006Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber

Description

March 23, 1965 R, A. voN LINDE 3,174,526

` A'romzmc BURNER UNIT Filed Aug. 25. 1960 2 Sherets-.Sheet 1 March 23, 1965 R. A, VON LlNDE 3,174,526

ATOMIZING BURNER UNIT Filed Aug. 23, 1960 2 Sheets-Sheeh 2 ROJERT ALBERI' V011/ [JA/DE ATRA/EKS United States Patent ice 3,174,526 ATOMIZING BURNER UNIT Robert Albert von lLinde, Akilindastrasse 56,

Graefelting, near Munich, Germany Filed Aug. 23, 1960, Ser. No. 51,409 7 Claims. (Cl. 15S--4) The present invention relates to an atomizing burner, especially for fluid fuels, provided with a burner pipe or mixing tube in which the combustion air supplied at relatively high velocities absorbs the finely divided fuel supplied thereto and additionally draws or sucks in hot combustion gases from a chamber in open communication with the combustion space.

With the known burners of this general type, the atomizing nozzle is so arranged that the fluid fuel is atomized within the combustion air stream which is surrounded by a gaseous envelope consisting of drawn-back or suckedback combustion gases.

These combustion gases, the thermal contents of which could contribute very significantly to the rapid evaporation and preparation of the fuel mist, therefore, intermix themselves in the known prior art burners only subsequently with the fuel suspended in the combustion air and, therefore, can fulfill only incompletely the tasks assigned thereto. It is true that by preheating the combustion air, the preparation of the fuel may be improved considerably; however, the heat exchanger installation required therefor would increase considerably the cost of such an installation.

These disadvantages are avoided in the present invention by arranging the fuel atomizing nozzle in a prechamber, to which is supplied, in accordance with the present invention, the part of the combustion gases taken from the combustion chamber, and by discharging or terminating this prechamber in a mixing nozzle to which is admitted the combustion air. With such an arrangement, the combustion gases drawn or sucked-back to the mixing nozzle may give off the thermal contents thereof at relatively high temperatures directly to the fuel mist whereby a very rapid and complete evaporation and preparation of the fuel, as well as an advantageous mixture formation and therewith a very short and clear flame, i.e., a flame free of carbon black or soot, is formed.

These properties are also assured in case whenV a mixture very rich in combustible contents or constituents is supplied to the burner. Consequently, with the burner according to the present invention not only very high combustion temperatures may be achieved, which are of particularly great value with industrial furnaces, for example, for smelting or forging furnaces or the like, but also gas mixtures may be produced thereby with equally good combustion which, by reason of the large contents in reducing eifective component parts form a suitable furnace atmosphere for the heat treatment, for instance, of work tools.

Accordingly, it is an object of the present invention to provide a burner of the type mentioned hereinabove Which eliminates the aforementioned disadvantages encountered in the prior art devices and which additionally improves the combustion characteristics thereof.

Another object of the present invention is the provision of an atomizing burner in which the preparation of the fuel is considerably improved in a simple manner and without the necessity of relatively expensive installations such as heat exchangers.

Another object of the present invention resides in the provisionof an atomizing burner arrangement in which optimum use is made of the thermal contents of the combustion gases drawn back from the Vcombustion chamber 7 into the atomizing unit so as to increase the rapidity and lquality of the fuel preparation.

Still another object of the present invention resides in the provision of an atomizing burner arrangement in which an advantageous mixture formation is assured with a minimum of impurities in the resulting flame so as to render the gas mixtures produced thereby particularly suitable as reduction-effective atmosphere for furnaces.

A further object of the present invention resides in the provision of an atomizing burner which produces a gas mixture containing relatively large contents in reducing components appropriate for the heat treatment of work tools.

These and further objects, features and advantages of the present invention will become more obvious from the following description when taken in connection with the accompanying drawing which shows, for purposes of illustration only, four embodiments in accordance with the present invention and wherein:

FIGURE 1 is a cross-sectional view of a lirst embodiment of an atomizing burner in accordance with the present invention, and

FIGURES 2 through 4 are cross-sectional views, similar to FIGURE l, of three further modified embodiments of atomizing burners in accordance with the present invention.

Referring now to the drawing, wherein like reference numerals are used throughout the various views to designate corresponding parts, and more particularly to the embodiment of FIGURE 1, reference numeral 16 designates therein a combustion chamber which is limited at one end thereof by an annularly shaped flange 15 of a mixing tube or burner pipe 17. Apertures 18 are provided within the annular ange 15 which discharge into an annular space 20 limited at the front end thereof by a toroidal surface 19. The inner boundary surface of this annular space 20 is constituted by the outer wall surface of an intermediate jacket or wall 22 to which is connected the air supply pipe or conduit 21 and which passes over into a mixing nozzle 24 arranged concentrically to the mixing tube or burner pipe 17.Y A fuel supply line 26 provided with an atomizing nozzle 25 terminates in the mixing nozzle 24. The wall 22 and the mixing pipe 17 define therebetween an annular channel to which is supplied combustion air through the pipe connecting member 21. The combustion air thereby iiows about the freely exposed end surface of the mixing pipe 17 into the mixing chamber formed by the pipe 17. As a result of its ow energy, the combustion air draws in through the mixing nozzle 24 the combustion gases together with the combustible particles of the fuel distributed and prepared therein which are present in the prechamber 20 and continuously ilow through the apertures 18 from the combustion space 16 into the prechamber 20.`

The annular space 20 forming a prechamber is surrounded by a ceramic hollow body 30 whereas the combustion chamber'l isV constituted by the hollow space of a fire-proof hollow body member 31. The casing 27 of the burner is provided with a liange 28 by means of which the burner may be so secured at the edge of the tiring aperture of a heat-consuming device (not illustrated), for example, of an industrial furnace or of a gas producer which serves for purposes of obtaining neutral or reducing gaseous atmospheres that the combustion chamber 16 extends into the firing space thereof.

The embodiment of FIGURE 2 distinguishes itself from the embodiment of FIGURE l essentially by the fact that the section of the combustion chamber 16 adjoining the mixing pipe or burner tube 17 is enlarged conically. This section is formed by the hollow space of a ceramic body 32. In order to supply a partial stream of com- 0 bustion gases, requiredwithin the meaning of the present invention for the mixture formation, from the combustion chamber 16 to the apertures 18 and therewith to annular Patented Mar. 23, 1965 prechamber space 2t), the hollow body member 32 is provided with several channels 36 which, on the one hand, terminate in the conical inner wall of the hollow body member 32 and, on the other in an annular groove 37 facing the apertures 18. The combustion chamber 16 is closed ott by a hollow conical portion formed by the surrounding casing part 33 which decreases in cross section in the direction toward the discharge aperture 35.

In the embodiment of FIGURE 3, one end each of several tubes 42 are inserted into the liange 15, and at the other end terminate and discharge into a prechamber 40 having an end wall 41 providedl with a mixing nozzle 24. The atomizing nozzle 25 is arranged with au aperture of the other end wall of this prechamber 40'. A hollow space defined by cylindrical casing 44 and an end wall 43 serves for purposes ofv guiding the combustion air which thereby absorbs heat from the cornbustion gases sucked in through the pipes 42 out of the combustion chamber 16 and, therefore, absorbs in a preheated condition the mixture consisting of fuel, mist and combustion gases. A spark plug 45 of known construction serves thereby for purposes of igniting the mixture.

In the burner embodiment illustrated in FIGURE 4, the mixing pipe 17 discharges into a conical section 32 of the combustion chamber 16. A plurality of annularly distributed channels 36 are thereby provided in the walls of this section 32. The channels 36 terminate in an annular cylindrical prechamber 20, the inner wall of which is constituted b y the mixing pipe 17 and the outer wall of which is constituted by a jacket or wall 22. The wall 22 is secured at one end thereof at the annular flange and at the other end thereof is closed oft" by means of an end wall 48 into which is inserted a connecting pipe 49' for the insertion therein of the fuel nozzle 25. The mixing pipe 17 thereby forms-the forward portion of a chamber S0 into which extends a mixing nozzle 24 and which is in open communication by means of lateral hollow connecting conduit portions 51 with the cylindrical hollow space 52. The annular space 52 is thereby defined by the tiange 15, by the end wall 43 and the cylinder jackets 22 and 44 which are provided with an air-supply connecting member 21. A tubular connecting member 53 extending in tight sealing arrangement through the tubular walls 44, 22 and 17 serves for the support of a' spark plug 55. The hollow body section 32 consisting of ceramic material forms an inner insert for a hollow body 33 terminating the combustion chamber 16.

Operation The burner in accordance with the present invention operates as follows:

The combustion air supplied through the connecting pipe 21 ows with relatively high velocity into the mixing pipe or burner tube 17 and produces thereby at the orifice of the connecting portion or mixing nozzle 24 a vacuum or underpressure. Consequently, a` mixture-stream enters into the airstream which mixture-stream reaches the mixing nozzle 24 from the combustion chamber 16 along the path indicated by the arrows. This mixture-stream absorbs the fuel injected from the nozzle 25 in finely distributed form and `forms inthe first section of the mixing pipe` a very hot core stream which mixes completely with the combustion air only shortly ahead of the end of the mixing pipe 17. By reason of the fact thaty the liquid fuel is injected directly intothe hot drawnor sucked-back combustion gases, a very homogeneous, well-prepared and, therefore, also completely unobjectionably burning mixture results therefrom which burns even with a shortage of air with a short constant iiame without the formation of soot and carbon black, and which supplies a mixture usable as furnace atmosphere having a high content in reducing gas particles. If the stoichiometric quantity of air, i.e., the quantity of combustion air exactly necessary for complete combustion of the supplied fuel quantity, is supplied to the burner, there results the advantage in accordance with the present invention that relatively high iiame temperatures may be readily attained.

The heat exchange between the sucked-back combustion gases and the combustion air obtained through the wall 22 (FIGURE l) or through the walls of the pipes 42 (FIGURE 3) results in keeping the temperature of the combustion gases within the vicinity of the atomizing nozzle 25 within a limit favorable for the vaporization and preparation of the fuel mist. This is so as with excessive temperatures undesired side reactions may occur which may lead to a cracking of the fuel and thereby lead to the formation of soot, carbon black, or the like. On the other hand, this heat exchange is effective in such a manner that the combustion air also assumes a temperature favorable for the operation of the combustion process.

While have shown and described four embodiments in accordance with the present invention, it is understood that the same is not limited thereto but is susceptible of many changes and modifications within the spirit and scope thereof, and I, therefore, do not wish to be limited to the details shown and described herein, but intend to cover all such changes and modifications as are encompassed by the scope of the appended claims.

I claim:

1. An atomizing burner unit, especially for liquid fuels, comprising combustion chamber means, wall means forming prechamber means, means to enable combustion gases to pass from said combustion chamber means into Said:

prechamber means, mixing pipe means in communication with said prechamber means, means for supplying combustion air at relatively high velocities to said mixing pipe means to thereby draw-in hot combustion gases from said combustion chamber means through said prechamber means into said mixing pipe means, said wall means including two essentially concentric wall parts surrounding said mixing pipe means constituting therebetween twohollow spaces disposed one about the other, of which the' outer space forms said prechamber means in open communication with said combustion chamber means and the inner space forms a part of said means for supplying combustion air, a mixing nozzle portion secured to the inner one of said two essentially concentric wall parts and in communication with said mixing pipe means andl fuel atomizing means for distributing finely divided fuel toward said mixing pipe means into the drawn-in combustion gases.

2. An atomizing burner unit, especially for liquid fuels, comprising combustion chamber means, wall means forming prechamber means terminating at one end thereof in mixing nozzle means and also forming mixing pipe means in communication with said mixing nozzle means, said prechamber means being in communication near the other end thereof with said combustion chamber means to enable combustion gases to flow frorn'said combustion chamber means through said prechamber means into said mixing nozzle means, inducting means including combustion air supply means for supplying combustion air at relatively high velocities to said mixing pipe means to thereby draw-in hot combustion gases from said combustion chamber means through said prechamber means into said mixing pipe means by the iow energy in said combustion air, and fuel injection means arranged in said prechamber means for injecting finely divided fuel into said mixing nozzle means to be mixed therein with the drawn-in combustion gases prior to admixture thereof with said combustion air, said wall means including two concentrically arranged wall portions and a third wall portion forming said mixing pipe means-said two lirst-mentioned Wall portionsand said third wall portion forming therebetween two hollow spaces disposed one about the other, the outer of which constitutes a portion of said prechamber means and the inner of which constitutes a portion of said combustion air supply means.

3. An atomizing burner unit according to claim 2,

gases, said section having an inner wall provided with channels in communication with the prechamber means and with said combustion chamber means.

5. An atomizing burner unit, especially for liquid fuels, comprising combustion chamber means, wall means forming prechamber means terminating at one end thereof in mixing nozzle means .and also lforming mixing pipe means in communication with said mixing nozzle means, said prechamber means being in communication near the other end thereof with said combustion chamber means to enable combustion gases to flow `from said combustion chamber means through said prechamber means into said mixing nozzle means, inducting means including combustion air Supply means for supplying combustion air at relatively high velocities to said mixing pipe means to thereby draw-in hot combustion gases `from said combustion chamber means through said prechamber means into said mixing pipe means by the flow energy in said combustion air, and fuel injection means arranged in said prechamber means for injecting finely divided fuel into said mixing nozzle means to -be mixed therein with the drawnin combustion gases prior to admixture thereof with said combustion air, said wall means including a rst wall portion constituting an inner wall of said prechamber means and a second wall portion rigidly connected with said first wall portion and constituting said mixing nozzle means, and a .third wall portion forming said mixing pipe means and defining in conjunction with said first and second wall portions a passage forming part of said air supply means,

said air supply means including an annular gap provided between said second and third wall portions for the admission of the combustion `air into said mixing pipe means.

6. An 4atomizing burner unit comprising a mixing section having an upstream end, a mixing nozzle disposed essentially coaxially to and partially within said upstream end of said mixing section, a combustion section, return conduit means extending rearwardly from said combustion section into communication with said mixing nozzle to supply hot combustion gases essentially equally around the periphery of said mixing nozzle, fuel atomizing means disposed essentially coaxially to said mixing nozzle for dispersing nely divided fuel into the hot combustion gases passing through said mixing nozzle to vaporize said fue] prior to admixture with combustion air, said upstream end of said mixing section being spaced from said mixing nozzle to provide passage means therebetween, and conduit means for supplying combustion air into said passage means for educting hot combustion gases and dispersed fuel vaporizing therein from `said mixing nozzle into said mixing section.

7. An -atomizing burner unit according to claim 6, wherein said return conduit means include a plurality of spaced tubular members.

References Cited in the le of this patent UNITED STATES PATENTS 687,535 Machlet Nov. 26, 1901 2,048,321 Carruthers et al July 21, 1936 2,701,608 Johnson Feb. 8, 1955 2,722,372 Edwards Nov. 1, 1955 2,734,560 Harris et al Feb. 14, 1956 FOREIGN PATENTS 1,044,190 France June 17, 1953

Claims (1)

1. AN ATOMIZING BURNER UNIT, ESPECIALLY FOR LIQUID FUELS, COMPRISING COMBUSTION CHAMBER MEANS, WALL MEANS FORMING PRECHAMBER MEANS, MEANS TO ENABLE COMBUSTION GASES TO PASS FROM SAID COMBUSTION CHAMBER MEANS INTO SAID PRECHAMBER MEANS, MIXING PIPE MEANS IN COMMUNICATION WITH SAID PRECHAMBER MEANS, MEANS FOR SUPPLYING COMBUSTION AIR AT RELATIVELY HIGH VELOCITIES TO SAID MIXING PIPE MEANS TO THEREBY DRAW-IN HOT COMBUSTION GASES FROM SAID COMBUSTION CHAMBER MEANS THROUGH SAID PRECHAMBER MEANS INTO SAID MIXING PIPE MEANS, SAID WALL MEANS INCLUDING TWO ESSENTIALLY CONCENTRIC WALL PARTS SURROUNDING SAID MIXING PIPE MEANS CONSTITUTING THEREBETWEEN TWO HOLLOW SPACES DISPOSED SAID PRECHAMBER MEANS IN OPEN AND OUTER SPACE FORMS SAID PRECHAMBER MEANS IN OPEN COMMUNICATION WITH SAID COMBUSTION CHAMBER MEANS AND IN INNER SPACE FORMS A PART OF SAID MEANS FOR SUPPLYING COMBUSTION AIR, A MIXING NOZZLE PORTION SECURED TO THE INNER ONE OF SAID TWO ESSENTIALLY CONCENTRIC WALL PARTS AND IN COMMUNICATION WITH SAID MIXING PIPE MEANS AND FUEL ATOMIZING MEANS FOR DISTRIBUTING FINELY DIVIDED FUEL TOWARD SAID MIXING PIPE MEANS INTO THE DRAWN-IN COMBUSTION GASES.
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Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3276505A (en) * 1963-02-23 1966-10-04 Huber Resonant burner
US3319692A (en) * 1965-06-01 1967-05-16 Iit Res Inst Oil burner
US3325906A (en) * 1965-02-10 1967-06-20 Du Pont Process and apparatus for conveying continuous filaments
US3468616A (en) * 1967-11-24 1969-09-23 Hotwork Ltd Burners for furnaces
US3540821A (en) * 1968-04-01 1970-11-17 Exxon Research Engineering Co Flue gas recirculation burner
US3754393A (en) * 1970-12-05 1973-08-28 Nissan Motor Gas turbine engine combustor
US3910749A (en) * 1974-10-11 1975-10-07 James T Voorheis Induction burner
US3980422A (en) * 1975-08-11 1976-09-14 Hed Industries, Inc. Oil injection means for liquid fuel burner
US4005977A (en) * 1975-01-13 1977-02-01 Agency Of Industrial Science & Technology Gas circulating combustion means
US4083674A (en) * 1975-03-14 1978-04-11 Daimler-Benz Aktiengesellschaft Film evaporation combustion chamber
DE2917982A1 (en) * 1979-05-04 1980-11-06 Gaswaerme Inst E V Gas or liquid fuel burner - has horizontal and vertical air channels through body, communicating with central fuel and air inlet
US4255122A (en) * 1977-02-23 1981-03-10 Forenade Fabriksverken Apparatus for combusting liquid, gaseous or powdered fuels
US4408983A (en) * 1980-08-29 1983-10-11 British Gas Corporation Recuperative burners
US4445842A (en) * 1981-11-05 1984-05-01 Thermal Systems Engineering, Inc. Recuperative burner with exhaust gas recirculation means
US4954076A (en) * 1989-07-28 1990-09-04 Air Products And Chemicals, Inc. Flame stabilized oxy-fuel recirculating burner
US5098282A (en) * 1990-09-07 1992-03-24 John Zink Company Methods and apparatus for burning fuel with low NOx formation
US5118283A (en) * 1989-04-27 1992-06-02 Asea Brown Boveri Ltd. Combustion installation
US5147200A (en) * 1989-12-01 1992-09-15 Asea Brown Boveri, Ltd. Method of operating a firing installation
US5154596A (en) * 1990-09-07 1992-10-13 John Zink Company, A Division Of Koch Engineering Company, Inc. Methods and apparatus for burning fuel with low NOx formation
US5193995A (en) * 1987-12-21 1993-03-16 Asea Brown Boveri Ltd. Apparatus for premixing-type combustion of liquid fuel
DE19721937A1 (en) * 1997-05-26 1998-12-03 Abb Research Ltd Burner for operating a unit for generating a hot gas
EP0985882B1 (en) * 1998-09-10 2003-12-03 ALSTOM (Switzerland) Ltd Vibration damping in combustors
US20080085485A1 (en) * 2004-10-22 2008-04-10 Sandvik Intellectual Property Ab Method Of Combustion With The Aid Of Burners In Industrial Furnaces,And A Burner To This End
US20140237999A1 (en) * 2013-02-27 2014-08-28 Tenneco Automotive Operating Company Inc. Exhaust Aftertreatment Burner With Preheated Combustion Air
US8959902B2 (en) 2013-02-27 2015-02-24 Tenneco Automotive Operating Company Inc. Exhaust treatment burner and mixer system
US8991163B2 (en) 2013-02-27 2015-03-31 Tenneco Automotive Operating Company Inc. Burner with air-assisted fuel nozzle and vaporizing ignition system
US9027332B2 (en) 2013-02-27 2015-05-12 Tenneco Automotive Operating Company Inc. Ion sensor with decoking heater
US9074762B2 (en) * 2009-08-03 2015-07-07 Siemens Aktiengesellschaft Stabilizing the flame of a burner
WO2015154969A1 (en) * 2014-04-10 2015-10-15 Sofinter S.P.A. Burner
US9534525B2 (en) 2015-05-27 2017-01-03 Tenneco Automotive Operating Company Inc. Mixer assembly for exhaust aftertreatment system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US687535A (en) * 1901-02-08 1901-11-26 George Machlet Jr Burner for carbureting-machines.
US2048321A (en) * 1933-06-08 1936-07-21 Eben H Carruthers Fuel burning apparatus
FR1044190A (en) * 1951-10-26 1953-11-16 System and combustion process
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
US2722372A (en) * 1952-04-02 1955-11-01 John E Miller Draft control apparatus
US2734560A (en) * 1956-02-14 Burner and combustion system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734560A (en) * 1956-02-14 Burner and combustion system
US687535A (en) * 1901-02-08 1901-11-26 George Machlet Jr Burner for carbureting-machines.
US2048321A (en) * 1933-06-08 1936-07-21 Eben H Carruthers Fuel burning apparatus
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
FR1044190A (en) * 1951-10-26 1953-11-16 System and combustion process
US2722372A (en) * 1952-04-02 1955-11-01 John E Miller Draft control apparatus

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3276505A (en) * 1963-02-23 1966-10-04 Huber Resonant burner
US3325906A (en) * 1965-02-10 1967-06-20 Du Pont Process and apparatus for conveying continuous filaments
US3319692A (en) * 1965-06-01 1967-05-16 Iit Res Inst Oil burner
US3468616A (en) * 1967-11-24 1969-09-23 Hotwork Ltd Burners for furnaces
US3540821A (en) * 1968-04-01 1970-11-17 Exxon Research Engineering Co Flue gas recirculation burner
US3754393A (en) * 1970-12-05 1973-08-28 Nissan Motor Gas turbine engine combustor
US3910749A (en) * 1974-10-11 1975-10-07 James T Voorheis Induction burner
US4005977A (en) * 1975-01-13 1977-02-01 Agency Of Industrial Science & Technology Gas circulating combustion means
US4083674A (en) * 1975-03-14 1978-04-11 Daimler-Benz Aktiengesellschaft Film evaporation combustion chamber
US3980422A (en) * 1975-08-11 1976-09-14 Hed Industries, Inc. Oil injection means for liquid fuel burner
US4255122A (en) * 1977-02-23 1981-03-10 Forenade Fabriksverken Apparatus for combusting liquid, gaseous or powdered fuels
DE2917982A1 (en) * 1979-05-04 1980-11-06 Gaswaerme Inst E V Gas or liquid fuel burner - has horizontal and vertical air channels through body, communicating with central fuel and air inlet
US4408983A (en) * 1980-08-29 1983-10-11 British Gas Corporation Recuperative burners
US4445842A (en) * 1981-11-05 1984-05-01 Thermal Systems Engineering, Inc. Recuperative burner with exhaust gas recirculation means
US5193995A (en) * 1987-12-21 1993-03-16 Asea Brown Boveri Ltd. Apparatus for premixing-type combustion of liquid fuel
US5118283A (en) * 1989-04-27 1992-06-02 Asea Brown Boveri Ltd. Combustion installation
US4954076A (en) * 1989-07-28 1990-09-04 Air Products And Chemicals, Inc. Flame stabilized oxy-fuel recirculating burner
US5147200A (en) * 1989-12-01 1992-09-15 Asea Brown Boveri, Ltd. Method of operating a firing installation
US5098282A (en) * 1990-09-07 1992-03-24 John Zink Company Methods and apparatus for burning fuel with low NOx formation
US5344307A (en) * 1990-09-07 1994-09-06 Koch Engineering Company, Inc. Methods and apparatus for burning fuel with low Nox formation
US5154596A (en) * 1990-09-07 1992-10-13 John Zink Company, A Division Of Koch Engineering Company, Inc. Methods and apparatus for burning fuel with low NOx formation
DE19721937A1 (en) * 1997-05-26 1998-12-03 Abb Research Ltd Burner for operating a unit for generating a hot gas
DE19721937B4 (en) * 1997-05-26 2008-12-11 Alstom Premix burner for operating a unit for generating a hot gas
EP0985882B1 (en) * 1998-09-10 2003-12-03 ALSTOM (Switzerland) Ltd Vibration damping in combustors
US7993130B2 (en) * 2004-10-22 2011-08-09 Sandvik Intellectual Property Ab Method of combustion with the aid of burners in industrial furnaces, and a burner to this end
US20080085485A1 (en) * 2004-10-22 2008-04-10 Sandvik Intellectual Property Ab Method Of Combustion With The Aid Of Burners In Industrial Furnaces,And A Burner To This End
US9074762B2 (en) * 2009-08-03 2015-07-07 Siemens Aktiengesellschaft Stabilizing the flame of a burner
US20140237999A1 (en) * 2013-02-27 2014-08-28 Tenneco Automotive Operating Company Inc. Exhaust Aftertreatment Burner With Preheated Combustion Air
US8959902B2 (en) 2013-02-27 2015-02-24 Tenneco Automotive Operating Company Inc. Exhaust treatment burner and mixer system
US8991163B2 (en) 2013-02-27 2015-03-31 Tenneco Automotive Operating Company Inc. Burner with air-assisted fuel nozzle and vaporizing ignition system
US9027331B2 (en) * 2013-02-27 2015-05-12 Tenneco Automotive Operating Company Inc. Exhaust aftertreatment burner with preheated combustion air
US9027332B2 (en) 2013-02-27 2015-05-12 Tenneco Automotive Operating Company Inc. Ion sensor with decoking heater
WO2015154969A1 (en) * 2014-04-10 2015-10-15 Sofinter S.P.A. Burner
CN106415127A (en) * 2014-04-10 2017-02-15 索斐特公司 Burner
RU2689654C2 (en) * 2014-04-10 2019-05-28 Софинтер С.П.А. Burner
US10612773B2 (en) 2014-04-10 2020-04-07 Sofinter S.P.A. Burner
US9534525B2 (en) 2015-05-27 2017-01-03 Tenneco Automotive Operating Company Inc. Mixer assembly for exhaust aftertreatment system

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