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US2532740A - Fuel burner provided with combustion gas recirculating means - Google Patents

Fuel burner provided with combustion gas recirculating means Download PDF

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US2532740A
US2532740A US7370A US737048A US2532740A US 2532740 A US2532740 A US 2532740A US 7370 A US7370 A US 7370A US 737048 A US737048 A US 737048A US 2532740 A US2532740 A US 2532740A
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air
gases
combustion
burner
flame
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US7370A
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William H Speer
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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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details
    • F23D11/40Mixing tubes; Burner heads
    • F23D11/402Mixing chambers downstream of the nozzle

Definitions

  • This invention relates to heating apparatus and particularly to systems of combustion where mechanical firing of oil, gas or otherfuel receives air from a blower or other pressure source to support combustion.
  • the object of the invention is to provide for the combustion of a fluid fuel by control of jet and air supply formations and in particular by combining with the main air supply a recirculation of gases from the combustion chamber and the supply of these gases to the flame by syphonic action in the air supply.
  • Fig. 1 is a sectional view taken on the line ll of Fig. 2 and showing a typical combustion head with a periphera1 recirculation area around the central burner parts;
  • Fig. 2 is a front elevation of the apparatus shown in Fig. l;
  • Fig. 3 is a view similar to Fig. 1 and illustrating a modification.
  • burner head 5 is set in place in the furnace wall F and opens to the right into the combustion chamber C.
  • the burner head comprises an inner cylindrical portion 8 and an outer ribbed portion I of annular form providing the air inlet 8 leading to the contracting wall 9 concentrating the air stream and delivering it through the opening l into the space within the head portion 6.
  • a liner member H has an air inlet l2 positioned to receive the air entering from the opening Hi, this liner being slidably supported coaxially within the head portion 8 by ribs IS.
  • the oil supply tube l leads to the nozzle [6 forming the spray jet l'l under pressure, which jet is surrounded by the air stream from openings l0, l2.
  • Ignition terminals l8 are provided supported from the insulators I 9 at the outer portion of the head.
  • the liner II is surrounded by annular recircutaining ribs I3 and rod 24 engages lug 23 to provide for this adjustment from the outside of the apparatus.
  • the front edge 25 of the liner is positioned near the base of the jet and preferably within theedge 26 of the burner 'head 5.
  • the nozzle I6. is of the atomizing type giving a jet mist of very finely divided particles.
  • the air stream is ample in cross section with correspondingly moderate velocity completely surrounding each atom of oil and holding the particles in suspension. This together with the ignition gives control of the resulting flame and results in complete combustion within the high temperature of the flame generated gases within the high temperature refractory zone and until combustion is completed.
  • the body of the burner comprises a tubular member 36 sleeved on the inner end 31 of an outer housing member 38, the oil pipe 35 being located at the center and mounted to be longitudinally adjustable fromoutside the unit so as to position the nozzle 39 at the inner end of the burner as shown or a few inches forward or back of this position.
  • the oil supply to this nozzle is under pressure, low or high, sufiicient to atomize the oil being. used into a spreading jet having an angle of spread of about or or of about 50 to where conditions make it preferable.
  • the burner is thus of the gun type producing a spray jet by pressure and burning this jet by a supply of air to the jet as atomized and spread.
  • this recirculation is provided by the annular members 40, 4
  • the outer member 40 is press fitted or otherwise fastened in place in the inner end of tube 36 as shown so that the inturned end 42 of the insert will be at a slant across the path of the main air supply.
  • is of less diameter and is slid-- ingly centered and supported in thecylindrical end of member 40 by radial fins 44 carried either by the outer member 40 orthe inner member member 40 and having between them an inward directed passage 48. opening into the venturi formed by the contraction of the air flow by the conical flange 42.
  • the suction of the flow through the venturi draws gases inward from passage 46 supplied from the annular entrance 41 between the members 40, 4
  • the width of the passage 48 may be varied by longitudinal adjustment of the member 4
  • the size of the intervening space S may be varied by longitudinal adjustment of the oil supply pipe 35 to shift nozzle 39 forward or back from the position shown.
  • This recirculation of gases from the space S around the jet l1 uses these gases to decrease the amount of fresh air supplied while at the same time maintaining an adequate volume of gas mixture to float the flame as well as maintain the combustion.
  • the supply for the recirculation is drawn in through an annular area surrounding the space S and thus includes a large part of the unconsumed air and gases around the flame and not mixing therewith, the recirculation being remixed with the main air stream on its way to the flame. Increments of the unconsumed air are thus carried around in the recirculation circuit and the combustion is rendered more complete.
  • the action automatically adjusts itself to the varying conditions in the furnace permitting a wide control of the flame while attaining eflicient conditions of combustion.
  • the combustion itself is quieter due to the mufliing eflect of the recirculation, and the creation of a Venturi pressure area in the air stream tends to equalize the fan impulses.
  • Good flring adjustment is not dependent upon higher draft setting and a lower more normalized draft pull may be employed and thus fluttering is obthrough the venturi 2
  • the air consumption is made more complete and the volume of new air to be supplied is correspondingly reduced, avoiding excess air and improving the overall eiflciency.
  • will depend upon the Venturi action desired and most eflicient in each individual case.
  • the atomized fuel and the air mixture will float the flame a predetermined distance into the combustion chamber C and the recirculated gases will be drawn in through the annular area surrounding the base of the flame so that the flame near the burner head is encased in counter currents of the combustion gases.
  • the burner head may be supplied as an accessory or may be built into the equipment as originally installed. It is nonmechanical in operation.
  • the fuel is burned at approximately atmospheric pressure due to the relief of pressure either directly in the combustion chamber or from some remote point, for instance adjacent the smoke pipe.
  • the mixture is accomplished by the Venturi action which produces a partial vacuum at 20, 41 resulting in a mixture of the fresh and recirculated gases at 2
  • Theactual primary air for combustion is relatively reduced in amount due to the pick-up of gases from the combustion chamber or other source.
  • the flame is' thus supported by the recirculated gases with a consequent saving in the primary air and greater efliciency in the overall burning of the fuel.
  • the oil pressure line is at relatively high pressure but the air supply and recirculation is equally applicable to burners using a lower pressure oil supply in the neighborhood of five pounds for instance or less.
  • the burner head of Figs. 1 and 2 is of simple forma- .tion involving merely the tubular casting 6, l-
  • the burner head of Fig. 3 involves in its structure a simple assembly of the recirculation rings 40, 4
  • a fuel burner adapted to project a flame into the combustion chamber of a furnace comprising a forward member having an outer wall adapted to fit into the furnace wall and formed with a nozzle chamber and with a rear air supply opening, a fuel nozzle at the forward portion of said chamber adapted to atomize a liquid fuel supply and direct the atomized jet into the combustion chamber, a rear conduit providing a fresh air supply flowing through said opening forward into the rear air supply opening of said nozzle chamber, an inward directed wall member around said rear air supply opening, and a liner spaced from said outer wall surrounding said fuel nozzle to provide a passage and having a rear wall cooperating with said inward directed wall to form an inward directed passage opening into said air supply at the rear of said nozzle chamber to feed auxiliary gases into said air supply on the way to said nozzle, said passage leading from the combustion chamber to said inward directed passage for withdrawing gases from said chamber and leading said withdrawn gases into said inward directed passage for blending with the said air flow on its way to the nozzle.
  • a fuel burner as set forth in claim 1 in which the conduit for the fresh air is tapered to a contraction forming a Venturi passage into which the inwardly directed passage opens at the rear wardly open end and an air supply portion rearwardly thereof, aliner slidingly mounted in said head portion, a fuel supply means having a nozzle positioned in the forward portion of said head, a contraction of said air supply portion forming a Venturi passage directing the air flow into said head portion, said liner and head portion being spaced to form passages between them for supplying gases to said Venturi passage, and means for relatively adjusting said liner and said casing to vary the cross sectional areas of said passages and correspondingly vary the induction or Venturi effect of the air flow into said head portion and the relative proportions of the fresh air and auxiliary gases.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Description

Dec. 5, 1950 Filed Feb. 10, 1948 W. H. SPEER FUEL BURNER PROVIDED WITH COMBUSTION GAS RECIRCULATING MEANS 2 Sheets-Sheet l 41 5 /zr 19 c :1 IHHHHHHHHHI INVENTOR.
Dec. 5, 1950 w, sPEER $532,740
FUEL BURNER PROVIDED WITH COMBUSTION GAS RECIRCULATING MEANS Filed Feb. 10, 1948 2 Sheets-Sheet 2 INVENTOR. WE Swear Patented Dec. 5, 1950 FUEL BURNER PROVIDED WITH COMBUS- TION GAS RECIRCULATING MEANS William H. Speer, Moosup, Conn. v Application February 10, 1948, Serial No. 7,370
4 Claims.
This invention relates to heating apparatus and particularly to systems of combustion where mechanical firing of oil, gas or otherfuel receives air from a blower or other pressure source to support combustion. This is a continuationin-part of my prior application Number 585,111, filed March 27, 1945, now abandoned.
recirculation passages. 20. The liner n is adjusted longitudinally by sliding it in the re- The object of the invention is to provide for the combustion of a fluid fuel by control of jet and air supply formations and in particular by combining with the main air supply a recirculation of gases from the combustion chamber and the supply of these gases to the flame by syphonic action in the air supply. I
Further objects of the invention particularly in the construction of the combustion member to provide for this recirculation and admixture of gases will appear from the following description taken in connection with the following drawings in which Fig. 1 is a sectional view taken on the line ll of Fig. 2 and showing a typical combustion head with a periphera1 recirculation area around the central burner parts;
Fig. 2 is a front elevation of the apparatus shown in Fig. l; and
Fig. 3 is a view similar to Fig. 1 and illustrating a modification.
In the specific embodiment illustrated, the
burner head 5 is set in place in the furnace wall F and opens to the right into the combustion chamber C. The burner head comprises an inner cylindrical portion 8 and an outer ribbed portion I of annular form providing the air inlet 8 leading to the contracting wall 9 concentrating the air stream and delivering it through the opening l into the space within the head portion 6.
A liner member H has an air inlet l2 positioned to receive the air entering from the opening Hi, this liner being slidably supported coaxially within the head portion 8 by ribs IS.
The oil supply tube l leads to the nozzle [6 forming the spray jet l'l under pressure, which jet is surrounded by the air stream from openings l0, l2. Ignition terminals l8 are provided supported from the insulators I 9 at the outer portion of the head.
The liner II is surrounded by annular recircutaining ribs I3 and rod 24 engages lug 23 to provide for this adjustment from the outside of the apparatus. The front edge 25 of the liner is positioned near the base of the jet and preferably within theedge 26 of the burner 'head 5.
Preferably the nozzle I6. is of the atomizing type giving a jet mist of very finely divided particles. The air stream is ample in cross section with correspondingly moderate velocity completely surrounding each atom of oil and holding the particles in suspension. This together with the ignition gives control of the resulting flame and results in complete combustion within the high temperature of the flame generated gases within the high temperature refractory zone and until combustion is completed.
In the modification illustrated in Fig. 3 the body of the burner comprises a tubular member 36 sleeved on the inner end 31 of an outer housing member 38, the oil pipe 35 being located at the center and mounted to be longitudinally adjustable fromoutside the unit so as to position the nozzle 39 at the inner end of the burner as shown or a few inches forward or back of this position. The oil supply to this nozzle is under pressure, low or high, sufiicient to atomize the oil being. used into a spreading jet having an angle of spread of about or or of about 50 to where conditions make it preferable. The burner is thus of the gun type producing a spray jet by pressure and burning this jet by a supply of air to the jet as atomized and spread.
I have found it important to suspend or float this pressure formed jet in the combustion chamber by surrounding gases and to this end the' fresh air supply is brought longitudinally around the nozzle and is supplemented by a recirculation of gases drawn from the combustion chamber and preferably from the space S back of the floating flame as in the forms illustrated in the drawings.
In Fig. 3 this recirculation is provided by the annular members 40, 4|. The outer member 40 is press fitted or otherwise fastened in place in the inner end of tube 36 as shown so that the inturned end 42 of the insert will be at a slant across the path of the main air supply. The inner member 4| is of less diameter and is slid-- ingly centered and supported in thecylindrical end of member 40 by radial fins 44 carried either by the outer member 40 orthe inner member member 40 and having between them an inward directed passage 48. opening into the venturi formed by the contraction of the air flow by the conical flange 42. The suction of the flow through the venturi draws gases inward from passage 46 supplied from the annular entrance 41 between the members 40, 4| leading to the space S which intervenes between this passage and the base of the flame H. The width of the passage 48 may be varied by longitudinal adjustment of the member 4| for instance by the rod 48 leading to adjusting means accessible from outside of the burner and engaging the lug 49 projecting upward from the member 4|. The size of the intervening space S may be varied by longitudinal adjustment of the oil supply pipe 35 to shift nozzle 39 forward or back from the position shown.
This recirculation of gases from the space S around the jet l1 uses these gases to decrease the amount of fresh air supplied while at the same time maintaining an adequate volume of gas mixture to float the flame as well as maintain the combustion.
The result is a lowering of the excess air passing through the combustion chamber and an increase in the percentage of carbon dioxide in the flue gases. In the apparatus as illustrated in Fig. 3 the Venturi action is concentrated at or just back of the base of the flame.
Consequently the main air supply and the recirculated gases combine with the jet all around in the space S as the jet is projected from the burner holding the flame in suspension in the high temperature combustion chamber to complete the burning of the oil. Contact of the flame with surrounding surfaces of the burner is avoided altogether and there is ample separation preventing any coking or accumulation of deposits on the metal parts.
In the device shown the supply for the recirculation is drawn in through an annular area surrounding the space S and thus includes a large part of the unconsumed air and gases around the flame and not mixing therewith, the recirculation being remixed with the main air stream on its way to the flame. Increments of the unconsumed air are thus carried around in the recirculation circuit and the combustion is rendered more complete. The action automatically adjusts itself to the varying conditions in the furnace permitting a wide control of the flame while attaining eflicient conditions of combustion.
At the same time the recirculation of the accessory gases from the combustion chamber and its admixture with the incoming air aids in insuring efllcient overall combustion and adds to the control of the combustion gases in the burner and the combustion chamber. 1
By withdrawing and recirculating the gases from the combustion chamber, the pressure in the boiler is reduced. The draft requirements as ordinarily flgured are necessarily less and the release of products of combustion through the boiler is slowed down with consequent permissible restriction of the boiler passages and greater efliciency in their heat absorption.
The combustion itself is quieter due to the mufliing eflect of the recirculation, and the creation of a Venturi pressure area in the air stream tends to equalize the fan impulses. Good flring adjustment is not dependent upon higher draft setting and a lower more normalized draft pull may be employed and thus fluttering is obthrough the venturi 2|, 4'6 thus rat ng the temperature of the mixture. The air consumption is made more complete and the volume of new air to be supplied is correspondingly reduced, avoiding excess air and improving the overall eiflciency.
The particular adjustment of the liner 4| will depend upon the Venturi action desired and most eflicient in each individual case. The wider the venturi 2| the further the orifice I! will be spaced from the air jet orifice l0 and the narrower will be the air jet at the point of entry into the oriflce l2, so that the tendency will be to increase recirculation with widening of the Venturi neck by inward movement of the liner.
Normally the atomized fuel and the air mixture will float the flame a predetermined distance into the combustion chamber C and the recirculated gases will be drawn in through the annular area surrounding the base of the flame so that the flame near the burner head is encased in counter currents of the combustion gases.
The burner head may be supplied as an accessory or may be built into the equipment as originally installed. It is nonmechanical in operation. The fuel is burned at approximately atmospheric pressure due to the relief of pressure either directly in the combustion chamber or from some remote point, for instance adjacent the smoke pipe. The mixture is accomplished by the Venturi action which produces a partial vacuum at 20, 41 resulting in a mixture of the fresh and recirculated gases at 2|, 46 (Figs. 2 and 3). Theactual primary air for combustion is relatively reduced in amount due to the pick-up of gases from the combustion chamber or other source. The flame is' thus supported by the recirculated gases with a consequent saving in the primary air and greater efliciency in the overall burning of the fuel.
It also provides, for favorable expansion of the flame in a heating boiler permitting it to be distributed and supplied most advantageously to the surfaces to be heated. The only draft needed is from the breach to the chimney in order to vent the released products of combustion from the heat unit.
In the burner shown, the oil pressure line is at relatively high pressure but the air supply and recirculation is equally applicable to burners using a lower pressure oil supply in the neighborhood of five pounds for instance or less. The burner head of Figs. 1 and 2 is of simple forma- .tion involving merely the tubular casting 6, l-
and the liner- H with the rod 24 extending backward for accessible manipulation at the outside of the burner. The burner head of Fig. 3 involves in its structure a simple assembly of the recirculation rings 40, 4| at the inner end of the tubular member 36. These typical embodiments illustrate the operation and advantages of this system of recirculation, but the invention is not limited to the specific details shown. It is intended to cover such modifications as fall within the scope of the appended claims.
I claim:
1. A fuel burner adapted to project a flame into the combustion chamber of a furnace comprising a forward member having an outer wall adapted to fit into the furnace wall and formed with a nozzle chamber and with a rear air supply opening, a fuel nozzle at the forward portion of said chamber adapted to atomize a liquid fuel supply and direct the atomized jet into the combustion chamber, a rear conduit providing a fresh air supply flowing through said opening forward into the rear air supply opening of said nozzle chamber, an inward directed wall member around said rear air supply opening, and a liner spaced from said outer wall surrounding said fuel nozzle to provide a passage and having a rear wall cooperating with said inward directed wall to form an inward directed passage opening into said air supply at the rear of said nozzle chamber to feed auxiliary gases into said air supply on the way to said nozzle, said passage leading from the combustion chamber to said inward directed passage for withdrawing gases from said chamber and leading said withdrawn gases into said inward directed passage for blending with the said air flow on its way to the nozzle.
2. A fuel burner as set forth in claim 1 in which the conduit for the fresh air is tapered to a contraction forming a Venturi passage into which the inwardly directed passage opens at the rear wardly open end and an air supply portion rearwardly thereof, aliner slidingly mounted in said head portion, a fuel supply means having a nozzle positioned in the forward portion of said head, a contraction of said air supply portion forming a Venturi passage directing the air flow into said head portion, said liner and head portion being spaced to form passages between them for supplying gases to said Venturi passage, and means for relatively adjusting said liner and said casing to vary the cross sectional areas of said passages and correspondingly vary the induction or Venturi effect of the air flow into said head portion and the relative proportions of the fresh air and auxiliary gases.
WILLIAM H. SPEER.
REFERENCES CITED The following references are of record in the file of this patent:
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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
US2918117A (en) * 1956-10-04 1959-12-22 Petro Chem Process Company Inc Heavy fuel burner with combustion gas recirculating means
US2925858A (en) * 1957-01-14 1960-02-23 Zink Co John Shroud for fuel burners
US2959215A (en) * 1948-06-19 1960-11-08 Robert I Warnecke Apparatus for opposing flare back in fluid fuel burners
DE1127523B (en) * 1957-05-07 1962-04-12 Wagner Hochdruck Dampfturbinen Liquid fuel burners
DE1177271B (en) * 1955-01-11 1964-09-03 Thermal Res & Engineering Corp Liquid fuel burner
DE1247530B (en) * 1963-03-29 1967-08-17 Robert Von Linde Dipl Ing Burners for flowing fuels
DE1258007B (en) * 1956-02-04 1968-01-04 Eugen Klein Dipl Ing Burners for flowing fuels
US4425854A (en) 1982-06-30 1984-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Micronized coal burner facility
WO1993019325A1 (en) * 1992-03-21 1993-09-30 Deutsche Forschungsanstalt Fuer Luft-Und Raumfahrte.V Nitrogen oxide-poor burner
US20050084812A1 (en) * 2003-10-03 2005-04-21 Alm Blueflame Llc Combustion method and apparatus for carrying out same
US20100170263A1 (en) * 2001-07-23 2010-07-08 Ramgen Power Systems, Llc Vortex Combustor for Low NOX Emissions when Burning Lean Premixed High Hydrogen Content Fuel
US20110061392A1 (en) * 2009-09-13 2011-03-17 Kendrick Donald W Combustion cavity layouts for fuel staging in trapped vortex combustors
US20130269576A1 (en) * 2010-11-18 2013-10-17 Linde Aktiengesellschaft Burner with adjustable flue gas recirculation
ITMI20131507A1 (en) * 2013-09-11 2015-03-12 Christian Atzeni METHOD OF COMBUSTION AND INDUSTRIAL BURNER

Citations (10)

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Publication number Priority date Publication date Assignee Title
US269720A (en) * 1882-12-26 Glaus russmann
US657228A (en) * 1899-08-16 1900-09-04 W H Remington Burning pulverized and liquid hydrocarbons for fuel and heating.
US1614359A (en) * 1922-10-16 1927-01-11 Wayne Co Liquid-fuel burner
US1658462A (en) * 1927-05-16 1928-02-07 Supreme Oilburner Company Oil burner
GB371056A (en) * 1931-01-23 1932-04-21 Reginald Percy Fraser Improvements relating to oil-burning apparatus
US2110209A (en) * 1934-10-13 1938-03-08 Baker Perkins Co Inc Furnace
US2200278A (en) * 1933-02-09 1940-05-14 Motor Parts Company Oil burner
US2207010A (en) * 1937-09-20 1940-07-09 Robert C Hopkins Recuperating burner block
US2224544A (en) * 1940-12-10 Temperature control foe tubular
US2357622A (en) * 1941-06-23 1944-09-05 Williams Oil O Matic Heating Pulsation relief device

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US269720A (en) * 1882-12-26 Glaus russmann
US2224544A (en) * 1940-12-10 Temperature control foe tubular
US657228A (en) * 1899-08-16 1900-09-04 W H Remington Burning pulverized and liquid hydrocarbons for fuel and heating.
US1614359A (en) * 1922-10-16 1927-01-11 Wayne Co Liquid-fuel burner
US1658462A (en) * 1927-05-16 1928-02-07 Supreme Oilburner Company Oil burner
GB371056A (en) * 1931-01-23 1932-04-21 Reginald Percy Fraser Improvements relating to oil-burning apparatus
US2200278A (en) * 1933-02-09 1940-05-14 Motor Parts Company Oil burner
US2110209A (en) * 1934-10-13 1938-03-08 Baker Perkins Co Inc Furnace
US2207010A (en) * 1937-09-20 1940-07-09 Robert C Hopkins Recuperating burner block
US2357622A (en) * 1941-06-23 1944-09-05 Williams Oil O Matic Heating Pulsation relief device

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959215A (en) * 1948-06-19 1960-11-08 Robert I Warnecke Apparatus for opposing flare back in fluid fuel burners
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
DE1177271B (en) * 1955-01-11 1964-09-03 Thermal Res & Engineering Corp Liquid fuel burner
DE1258007B (en) * 1956-02-04 1968-01-04 Eugen Klein Dipl Ing Burners for flowing fuels
US2918117A (en) * 1956-10-04 1959-12-22 Petro Chem Process Company Inc Heavy fuel burner with combustion gas recirculating means
US2925858A (en) * 1957-01-14 1960-02-23 Zink Co John Shroud for fuel burners
DE1127523B (en) * 1957-05-07 1962-04-12 Wagner Hochdruck Dampfturbinen Liquid fuel burners
DE1247530B (en) * 1963-03-29 1967-08-17 Robert Von Linde Dipl Ing Burners for flowing fuels
US4425854A (en) 1982-06-30 1984-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Micronized coal burner facility
WO1993019325A1 (en) * 1992-03-21 1993-09-30 Deutsche Forschungsanstalt Fuer Luft-Und Raumfahrte.V Nitrogen oxide-poor burner
US5370526A (en) * 1992-03-21 1994-12-06 Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt E.V. Burner poor in nitrogen oxide
US8312725B2 (en) 2001-07-23 2012-11-20 Ramgen Power Systems, Llc Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel
US20100170263A1 (en) * 2001-07-23 2010-07-08 Ramgen Power Systems, Llc Vortex Combustor for Low NOX Emissions when Burning Lean Premixed High Hydrogen Content Fuel
WO2005040677A3 (en) * 2003-10-03 2006-02-16 Alm Blueflame Llc Combustion method and apparatus for carrying out same
US7086854B2 (en) * 2003-10-03 2006-08-08 Alm Blueflame, Llc Combustion method and apparatus for carrying out same
US20050084812A1 (en) * 2003-10-03 2005-04-21 Alm Blueflame Llc Combustion method and apparatus for carrying out same
US20110061392A1 (en) * 2009-09-13 2011-03-17 Kendrick Donald W Combustion cavity layouts for fuel staging in trapped vortex combustors
US20110061391A1 (en) * 2009-09-13 2011-03-17 Kendrick Donald W Vortex premixer for combustion apparatus
US20110061395A1 (en) * 2009-09-13 2011-03-17 Kendrick Donald W Method of fuel staging in combustion apparatus
US20110061390A1 (en) * 2009-09-13 2011-03-17 Kendrick Donald W Inlet premixer for combustion apparatus
US8549862B2 (en) 2009-09-13 2013-10-08 Lean Flame, Inc. Method of fuel staging in combustion apparatus
US8689562B2 (en) 2009-09-13 2014-04-08 Donald W. Kendrick Combustion cavity layouts for fuel staging in trapped vortex combustors
US8689561B2 (en) 2009-09-13 2014-04-08 Donald W. Kendrick Vortex premixer for combustion apparatus
US20130269576A1 (en) * 2010-11-18 2013-10-17 Linde Aktiengesellschaft Burner with adjustable flue gas recirculation
ITMI20131507A1 (en) * 2013-09-11 2015-03-12 Christian Atzeni METHOD OF COMBUSTION AND INDUSTRIAL BURNER
WO2015036914A1 (en) * 2013-09-11 2015-03-19 Atzeni Christian Combustion method and industrial burner

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