US2647568A - Burner throat - Google Patents
Burner throat Download PDFInfo
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- US2647568A US2647568A US218298A US21829851A US2647568A US 2647568 A US2647568 A US 2647568A US 218298 A US218298 A US 218298A US 21829851 A US21829851 A US 21829851A US 2647568 A US2647568 A US 2647568A
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- burner
- throat
- ribs
- air
- peripheral surface
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- 230000002093 peripheral effect Effects 0.000 description 33
- 239000000446 fuel Substances 0.000 description 22
- 239000000203 mixture Substances 0.000 description 17
- 230000000994 depressogenic effect Effects 0.000 description 7
- 239000007789 gas Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 102000018062 Taperin Human genes 0.000 description 1
- 108050007169 Taperin Proteins 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- VUQUOGPMUUJORT-UHFFFAOYSA-N methyl 4-methylbenzenesulfonate Chemical compound COS(=O)(=O)C1=CC=C(C)C=C1 VUQUOGPMUUJORT-UHFFFAOYSA-N 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
Definitions
- This invention relates to fuelburn'ers'and has for an object to provide a burner which is stable in operation.
- Another object is to provide a burner which maintains ignition even in the presence of a large excess of air.
- Another object is to provide a novel and im proved burner throat having greatly improved stability.
- the throat diameter is increased to form an annular ledge which provides a sharp drop-off for the air-fuel mixture as it passes thereover to the zone of larger diameter.
- This drop-off produces eddy currents in the mixture which serve to retain combustion and prevent the flame from being blown out even by a large excess of air.
- the portion of increased diameter may be formed by recessed segmental areas in the throat surface and extending from the ledge rearwardly to the furnace end of the throat
- the recessed segmental areas may be spaced to leave raised ribs therebetween which extend either axially or in a direction inclined thereto and have radial sides adapted to form additional ledgeswith a sharp drop-ofi'over which the rotating mixture passes-and forms additional eddy currents.
- ribs are preferably so formed that the upper surfaces thereof do not project above the normal burner throat contour so as to impede the normal rotation of the gases.
- Fig. 1 is a rear elevation of a burner throat as seen from the furnace end;
- Fig. 2 is a broken side elevation, partly in tion taken on the line 2-2 of Fig. 1 showing the complete burner; and a 1 i I Fig. 3 is a partial rear elevation of a burner throat illustrating a different arrangement of ribs.
- a burner tube It having a flange l I which is attached to the front plate [2 of a furnace wall I3 and has formed therein an annular gas ring I4 having exit orifices l5 extending around the i periphery of the burner tube through which gas is supplied to the throat.
- the gas ring i4. is connected to a suitable supply pipe l6.
- Theburner tube 10 is mounted in registration with an air register 20 having a front plate 2
- the air register is provided with the usual peripheral air doors 26 which are mounted for relative rotation to vary the rotation of the air supplied therethrough to the burner tube.
- the burner is also shown as including an oil atomizer tip 30 carried by a barrel 3
- a diffusion plate 33 is positioned on the barrel 3
- the furnace wall I3 is provided with a burner opening in which throat tile 35 are secured by suitable means as by angle bolts 36.
- the throat tile in the embodiments shown are formed with a cylindrical annular surface 31 which registers with and forms a continuation of the inner surface of the burner tube I0 and with a plurality SEO- Referring to the drawings more in detaiL'the' 3 of segmental recessed portions 38 which extend toward the furnace end of the throat from the annular portion 31 and form therebetween a plurality of. ribs 39.
- the recessed portions 38 are flared and are shown as comprising a forward slightly flared portion 40 and a rearward more highly flared portion 4
- the segments 38 terminate in a radial wall 43 which forms a sharp angle with the annular surface 31.
- the sides A l to 45 of the ribs 39 are preferably formed along radial lines so that a sharp edge is formed Withtheir upper surfaces.
- the upper surfaces of the ribs extend from the annular surface 3'! in a gradual curve flaring outwardly to meet the flared surface M of the recessed portions 38' at the furnace end of the throat tile.
- the ribs 39 taper in thickness from their formed end to the furnace end.
- the ribs 39 are inclined with respect to the axis of the burner and are preferably inclined in the direction to cross the rotating air-fuel mixture" sothat the rotating mixture flows over the trailing edges of the ribs to form eddy currents which assist in retaining combustion.
- the throat may be formed of segmental tile in accordance with usual practice, as indicated by dotted lines in Fig. 2.
- the ribs 3 9a extend in an axial direction. This may be preferred in certain instances and permits the rib to be formed on a single tile segment.
- the greatest zone of eddy current formation is at the annular ledge formed by the wall 43 and at the forward ends of the ribs 39 Where their thickness is greatest.
- ribs 39 may be omitted and increased stability obtained by means of annulus 31 and wall 4.3, although. for
- the ribs have been found essential. Likewise, the ribs may be employed without the an.- nulus under certain conditions.
- the wall 43 and the sides of the ribs have been shown as radial to provide sharp ledges over which the mixture flows with a sharp drop-off. Obviously the shape may be modifiedsomewhat provided the ledge effect is retained as distinguished from a sloping surface which may change the direction of the mixture flowing thereover without producing substantial eddy currents.
- the oil atomizer may be used in conjunctionwithor in place of the gas ring.
- the throat construction is not restricted to any specific burner construction although it is most effective inburners having peripheral fuel injection and rotating air-fuel mixtures at the throat.
- a burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a' burner throat, said throat having a. narrow peripheral surface and having an outwardly said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said pe ripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover.
- a burner having air and fuel admission means: and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover,
- ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said peripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover, said ribs tapering in radial thickness from said first peripheral surface rearwardly and merging rearwardly in said flared surface.
- a burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardli from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion, of which.
- a burner having air and fuel admission means and. a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardlyfiared surface extending rearwardly therefrom, said outwardly flared surface being depressed 1 radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said peripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover, said ribs tapering in radial thickness from said first peripheral surface rearwardly and merging rearwardly into said flared surface, said ribs extending axially along said flared surface
- a burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being formed by depressed segments spaced peripherally to leave raised ribs therebetween and defined by an annular front wall extending substantially normal to said peripheral surface and by side walls substantially normal to the inner surface of said ribs, said walls forming ledges adapted to produce eddy currents in the air-fuel mixture flowing thereover.
- a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat through which air flows from said air admission means, said throat surface having depressed portions forming raised ribs therebetween having peripheral and radial surfaces forming ledges adapted to produce eddy currents in the air flowing thereover, said ribs having their maximum radial thickness at their forward ends and taperin in thickness toward their rearward ends.
- a burner as set forth in claim 6, in which said ribs are inclined to the axis of said throat.
- a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat through which air flows from said air admission means, said throat surface having depressed portions forming raised ribs of rectangular cross section therebetween having peripheral and radial surfaces forming ledges adapted to produce eddy currents in the air flowing thereover.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
Aug. 4, 1953 s. A. SLOAN 2,647,568
' BURNER THROAT Filed March 30, 1951 2 Sheets-Sheet 1 (Ittorneg Patented Aug. 4, 1953 2,647,568 BURNER THROAT Stephen A. Sloan, Darien, Conn., assignor to Peabody Engineering Corporation, New York, N. Y.,
a corporation of New York Application March 30, 1951, Serial No. 218,298
8 Claims. (Cl. 158-46) This invention relates to fuelburn'ers'and has for an object to provide a burner which is stable in operation.
Another object is to provide a burner which maintains ignition even in the presence of a large excess of air.
Another object is to provide a novel and im proved burner throat having greatly improved stability.
Various other objects and advantages will be apparent as the nature of the invention is more fully disclosed.
In fuel burners of the type in which the fuel is burned in suspension there may be a tendency toward instability, particularly at extremely low burner capacities where a large excess of air is available. For example if the burner were set to operate at one-tenth of its'maximum' capacity, the airsupply normally would be cut to one-tenth of its maximum. However, the fans would be capable of delivering ten times as much air as would be required to burn this reduced amount of fuel and if, due tosome malfunctioning of the controls, the full amount of air were supplied even temporarily, it could cause the burner to blow out. Such conditions might also exist in normal plant operations when starting up a unit as well as under other circumstances.
-Thepresent burner throat obviates this diificulty and'prevents the flame from being blown outunder such conditions. i i
This is accomplished in general in accordance with the present invention by providing the burner throat with a short annular portion adjacent the fuel injection zone of the same diameter as the burner tube and forming an unimpeded continuation thereof.
Beyond this annular portion the throat diameter is increased to form an annular ledge which provides a sharp drop-off for the air-fuel mixture as it passes thereover to the zone of larger diameter. This drop-off produces eddy currents in the mixture which serve to retain combustion and prevent the flame from being blown out even by a large excess of air.
The portion of increased diameter may be formed by recessed segmental areas in the throat surface and extending from the ledge rearwardly to the furnace end of the throat The recessed segmental areas may be spaced to leave raised ribs therebetween which extend either axially or in a direction inclined thereto and have radial sides adapted to form additional ledgeswith a sharp drop-ofi'over which the rotating mixture passes-and forms additional eddy currents. The
2 a ribs are preferably so formed that the upper surfaces thereof do not project above the normal burner throat contour so as to impede the normal rotation of the gases. Y
The nature of the invention will be better understood by referring to the following description, taken in connection with the accompanying drawing in which a specific embodiment has been se forth for purposes of illustration.
In the drawings: 1 Fig. 1 is a rear elevation of a burner throat as seen from the furnace end;
Fig. 2 is a broken side elevation, partly in tion taken on the line 2-2 of Fig. 1 showing the complete burner; and a 1 i I Fig. 3 is a partial rear elevation of a burner throat illustrating a different arrangement of ribs.
invention is shown as applied to a burner comprising a burner tube It having a flange l I which is attached to the front plate [2 of a furnace wall I3 and has formed therein an annular gas ring I4 having exit orifices l5 extending around the i periphery of the burner tube through which gas is supplied to the throat. The gas ring i4. is connected to a suitable supply pipe l6.
Theburner tube 10 is mounted in registration with an air register 20 having a front plate 2| connected to a wall 22 which is spaced from the furnace wall to provide a plenum chamber or wind box 23, and having a back plate 24 provided with an opening which registers with the burner tube Ill. The air register is provided with the usual peripheral air doors 26 which are mounted for relative rotation to vary the rotation of the air supplied therethrough to the burner tube.
The burner is also shown as including an oil atomizer tip 30 carried by a barrel 3| extending axially through the air register and having coupling means 32 at its forward end to, provide for the supply of fuel to the burner. A diffusion plate 33 is positioned on the barrel 3| adjacent the atomizer tip 30. It is to be understood that the portion of the burner thus far described is of standard construction and only so much thereof has been set forth as is necessary to an understanding of the invention. I
The furnace wall I3 is provided witha burner opening in which throat tile 35 are secured by suitable means as by angle bolts 36. The throat tile in the embodiments shown are formed with a cylindrical annular surface 31 which registers with and forms a continuation of the inner surface of the burner tube I0 and with a plurality SEO- Referring to the drawings more in detaiL'the' 3 of segmental recessed portions 38 which extend toward the furnace end of the throat from the annular portion 31 and form therebetween a plurality of. ribs 39. The recessed portions 38 are flared and are shown as comprising a forward slightly flared portion 40 and a rearward more highly flared portion 4| intersecting along a peripheral line'42 although it is to be understood that the recessed segments 38 may be flared along a smooth curve or a straight line if desired. At the forward end the segments 38 terminate in a radial wall 43 which forms a sharp angle with the annular surface 31. The sides A l to 45 of the ribs 39 are preferably formed along radial lines so that a sharp edge is formed Withtheir upper surfaces. The upper surfaces of the ribs extend from the annular surface 3'! in a gradual curve flaring outwardly to meet the flared surface M of the recessed portions 38' at the furnace end of the throat tile. Hence the ribs 39 taper in thickness from their formed end to the furnace end. Y
In theembodiment shown in Figs. 1 and 2 the ribs 39 are inclined with respect to the axis of the burner and are preferably inclined in the direction to cross the rotating air-fuel mixture" sothat the rotating mixture flows over the trailing edges of the ribs to form eddy currents which assist in retaining combustion. The throat may be formed of segmental tile in accordance with usual practice, as indicated by dotted lines in Fig. 2.
In the embodiment of Fig. 3 the ribs 3 9a extend in an axial direction. This may be preferred in certain instances and permits the rib to be formed on a single tile segment.
In thisinvention the annular ledge formed by the surface 31 and wall 43 and the ledge formed by the trailing sides of the ribs 39 produce eddy currents which serve to stabilize combustion. It has been found that burners embodying this invention are stable under the most adverse conditions encountered in commercial operations. I
The greatest zone of eddy current formation is at the annular ledge formed by the wall 43 and at the forward ends of the ribs 39 Where their thickness is greatest.
Under moderate conditions the ribs 39 may be omitted and increased stability obtained by means of annulus 31 and wall 4.3, although. for
maximum stability under most extreme conditions the ribs have been found essential. Likewise, the ribs may be employed without the an.- nulus under certain conditions.
The wall 43 and the sides of the ribs have been shown as radial to provide sharp ledges over which the mixture flows with a sharp drop-off. Obviously the shape may be modifiedsomewhat provided the ledge effect is retained as distinguished from a sloping surface which may change the direction of the mixture flowing thereover without producing substantial eddy currents.
The oil atomizer may be used in conjunctionwithor in place of the gas ring. The throat construction is not restricted to any specific burner construction although it is most effective inburners having peripheral fuel injection and rotating air-fuel mixtures at the throat.
' What is claimed is:
l. A burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a' burner throat, said throat having a. narrow peripheral surface and having an outwardly said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said pe ripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover.
2. A burner having air and fuel admission means: and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover,
.' and a plurality of ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said peripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover, said ribs tapering in radial thickness from said first peripheral surface rearwardly and merging rearwardly in said flared surface.
3. A burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being depressed radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardli from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion, of which. extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said peripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover, said ribs tapering in radial thickness from said first peripheral surface rearwardly and merging rearwardly into said flared surface, said ribs being inclined to the axis of said throat in a directionto extend across the rotating air-fuel stream flowing therethrough.
4. A burner having air and fuel admission means and. a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardlyfiared surface extending rearwardly therefrom, said outwardly flared surface being depressed 1 radially beyond said peripheral surface to form an annular ledge adapted to produce eddy currents in the air-fuel mixture flowing thereover, and a plurality of ribs spaced peripherally around said flared surface and extending rearwardly from said peripheral surface to the rearward end of said throat, said ribs having a peripheral surface no portion of which extends radially inward beyond said first peripheral surface and having sides extending substantially normal to said peripheral surface of said ribs to form a ledge adapted to form eddy currents in the mixture passing thereover, said ribs tapering in radial thickness from said first peripheral surface rearwardly and merging rearwardly into said flared surface, said ribs extending axially along said flared surface.
5. A burner having air and fuel admission means and a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat, said throat having a narrow peripheral surface and having an outwardly flared surface extending rearwardly therefrom, said outwardly flared surface being formed by depressed segments spaced peripherally to leave raised ribs therebetween and defined by an annular front wall extending substantially normal to said peripheral surface and by side walls substantially normal to the inner surface of said ribs, said walls forming ledges adapted to produce eddy currents in the air-fuel mixture flowing thereover.
6. In a burner having fuel and air admission means, a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat through which air flows from said air admission means, said throat surface having depressed portions forming raised ribs therebetween having peripheral and radial surfaces forming ledges adapted to produce eddy currents in the air flowing thereover, said ribs having their maximum radial thickness at their forward ends and taperin in thickness toward their rearward ends.
'7. A burner, as set forth in claim 6, in which said ribs are inclined to the axis of said throat. 8. In a burner having fuel and air admission means, a refractory member having an imperforate annular surface flaring rearwardly to form a burner throat through which air flows from said air admission means, said throat surface having depressed portions forming raised ribs of rectangular cross section therebetween having peripheral and radial surfaces forming ledges adapted to produce eddy currents in the air flowing thereover.
. STEPHEN A. SLOAN.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,132,521 Voorheis Oct. 11, 1938 2,515,845 Van Den Bussche July 18, 1950 2,527,503 Sinclair et al. Oct. 24, 1950 2,560,078 Bloomer July 10, 1951
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US218298A US2647568A (en) | 1951-03-30 | 1951-03-30 | Burner throat |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US218298A US2647568A (en) | 1951-03-30 | 1951-03-30 | Burner throat |
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Publication Number | Publication Date |
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US2647568A true US2647568A (en) | 1953-08-04 |
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US218298A Expired - Lifetime US2647568A (en) | 1951-03-30 | 1951-03-30 | Burner throat |
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US (1) | US2647568A (en) |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2973032A (en) * | 1957-02-14 | 1961-02-28 | Dravo Corp | Gas or oil burner |
US4026670A (en) * | 1976-04-19 | 1977-05-31 | Phillips Petroleum Company | Apparatus for producing carbon black |
US4271789A (en) * | 1971-10-26 | 1981-06-09 | Black Robert B | Energy conversion system |
US4412509A (en) * | 1973-06-11 | 1983-11-01 | Black Robert B | Energy conversion system and components thereof |
US4464108A (en) * | 1980-11-21 | 1984-08-07 | Donald Korenyi | Combustion apparatus |
US4561841A (en) * | 1980-11-21 | 1985-12-31 | Donald Korenyi | Combustion apparatus |
US4828487A (en) * | 1988-03-21 | 1989-05-09 | Earl Arnold M | Swirl generator |
US5713291A (en) * | 1996-04-03 | 1998-02-03 | The Babcock & Wilcox Company | Rotated multi-cylinder air delivery port |
US5755567A (en) * | 1996-02-21 | 1998-05-26 | The Babcock & Wilcox Company | Low vortex spin vanes for burners and overfire air ports |
US5827054A (en) * | 1996-01-11 | 1998-10-27 | The Babcock & Wilcox Company | Compound burner vane |
US6152726A (en) * | 1998-10-14 | 2000-11-28 | Asea Brown Boveri Ag | Burner for operating a heat generator |
US20060035183A1 (en) * | 2003-02-14 | 2006-02-16 | Richard Carroni | Mixer |
US20070259296A1 (en) * | 2004-12-23 | 2007-11-08 | Knoepfel Hans P | Premix Burner With Mixing Section |
US20090081601A1 (en) * | 2007-09-25 | 2009-03-26 | United States of America as represented by the Administrator of the National Aeronautics and | Flame Holder System |
US20090123882A1 (en) * | 2007-11-09 | 2009-05-14 | Alstom Technology Ltd | Method for operating a burner |
US20100266970A1 (en) * | 2007-11-27 | 2010-10-21 | Alstom Technology Ltd | Method and device for combusting hydrogen in a premix burner |
US20140065562A1 (en) * | 2012-08-31 | 2014-03-06 | Alstom Technology Ltd | Premix burner |
US10208960B2 (en) * | 2007-11-27 | 2019-02-19 | Ansaldo Energia Switzerland AG | Method for operating a gas turbine installation and equipment for carrying out the method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2132521A (en) * | 1934-12-26 | 1938-10-11 | Joseph T Voorheis | Burner construction |
US2515845A (en) * | 1946-06-25 | 1950-07-18 | Shell Dev | Flame pocket fluid fuel burner |
US2527503A (en) * | 1949-02-12 | 1950-10-24 | Harvey Whipple Inc | Burner head for gun-type oil burners |
US2560078A (en) * | 1950-12-21 | 1951-07-10 | Lummus Co | Combustion apparatus and method |
-
1951
- 1951-03-30 US US218298A patent/US2647568A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2132521A (en) * | 1934-12-26 | 1938-10-11 | Joseph T Voorheis | Burner construction |
US2515845A (en) * | 1946-06-25 | 1950-07-18 | Shell Dev | Flame pocket fluid fuel burner |
US2527503A (en) * | 1949-02-12 | 1950-10-24 | Harvey Whipple Inc | Burner head for gun-type oil burners |
US2560078A (en) * | 1950-12-21 | 1951-07-10 | Lummus Co | Combustion apparatus and method |
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2973032A (en) * | 1957-02-14 | 1961-02-28 | Dravo Corp | Gas or oil burner |
US4271789A (en) * | 1971-10-26 | 1981-06-09 | Black Robert B | Energy conversion system |
US4412509A (en) * | 1973-06-11 | 1983-11-01 | Black Robert B | Energy conversion system and components thereof |
US4026670A (en) * | 1976-04-19 | 1977-05-31 | Phillips Petroleum Company | Apparatus for producing carbon black |
US4464108A (en) * | 1980-11-21 | 1984-08-07 | Donald Korenyi | Combustion apparatus |
US4561841A (en) * | 1980-11-21 | 1985-12-31 | Donald Korenyi | Combustion apparatus |
US4828487A (en) * | 1988-03-21 | 1989-05-09 | Earl Arnold M | Swirl generator |
US6386863B1 (en) | 1996-01-11 | 2002-05-14 | The Babcock & Wilcox Company | Compound burner vane |
US5827054A (en) * | 1996-01-11 | 1998-10-27 | The Babcock & Wilcox Company | Compound burner vane |
US6146130A (en) * | 1996-01-11 | 2000-11-14 | The Babcock & Wilcox Company | Compound burner vane |
US5755567A (en) * | 1996-02-21 | 1998-05-26 | The Babcock & Wilcox Company | Low vortex spin vanes for burners and overfire air ports |
US5713291A (en) * | 1996-04-03 | 1998-02-03 | The Babcock & Wilcox Company | Rotated multi-cylinder air delivery port |
US6152726A (en) * | 1998-10-14 | 2000-11-28 | Asea Brown Boveri Ag | Burner for operating a heat generator |
US20060035183A1 (en) * | 2003-02-14 | 2006-02-16 | Richard Carroni | Mixer |
US8057224B2 (en) * | 2004-12-23 | 2011-11-15 | Alstom Technology Ltd. | Premix burner with mixing section |
US20070259296A1 (en) * | 2004-12-23 | 2007-11-08 | Knoepfel Hans P | Premix Burner With Mixing Section |
US20090081601A1 (en) * | 2007-09-25 | 2009-03-26 | United States of America as represented by the Administrator of the National Aeronautics and | Flame Holder System |
US10072840B2 (en) | 2007-09-25 | 2018-09-11 | The United States Of America As Represented By The Administator Of Nasa | Flame holder system |
US8529249B2 (en) * | 2007-09-25 | 2013-09-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Flame holder system |
US20090123882A1 (en) * | 2007-11-09 | 2009-05-14 | Alstom Technology Ltd | Method for operating a burner |
US9103547B2 (en) * | 2007-11-09 | 2015-08-11 | Alstom Technology Ltd | Method for operating a burner |
JP2009121806A (en) * | 2007-11-09 | 2009-06-04 | Alstom Technology Ltd | Method for operating burner |
US8066509B2 (en) * | 2007-11-27 | 2011-11-29 | Alstom Technology Ltd. | Method and device for combusting hydrogen in a premix burner |
US20100266970A1 (en) * | 2007-11-27 | 2010-10-21 | Alstom Technology Ltd | Method and device for combusting hydrogen in a premix burner |
US10208960B2 (en) * | 2007-11-27 | 2019-02-19 | Ansaldo Energia Switzerland AG | Method for operating a gas turbine installation and equipment for carrying out the method |
US20140065562A1 (en) * | 2012-08-31 | 2014-03-06 | Alstom Technology Ltd | Premix burner |
US9400105B2 (en) * | 2012-08-31 | 2016-07-26 | General Electric Technology Gmbh | Premix burner |
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