US3730438A - Fuel burner nozzle - Google Patents
Fuel burner nozzle Download PDFInfo
- Publication number
- US3730438A US3730438A US00149679A US3730438DA US3730438A US 3730438 A US3730438 A US 3730438A US 00149679 A US00149679 A US 00149679A US 3730438D A US3730438D A US 3730438DA US 3730438 A US3730438 A US 3730438A
- Authority
- US
- United States
- Prior art keywords
- nozzle
- angle
- nozzle body
- cone angle
- fuel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/14—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means with multiple outlet openings; with strainers in or outside the outlet opening
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/34—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
- B05B1/3405—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
Definitions
- the present invention relates to a fuel nozzle tip. More particularly, the invention concerns itself with pressure atomized fuel oil burner nozzle tips for use in a narrow firebox.
- the primary and secondary jets are disposed concentric to and outward from a central fluid opening in the nozzle such that the primary steam jets are directed tangentially to and against the circumference of the fuel to be atomized flowing from the central opening.
- the secondary steam jets which are disposed concentric to and outward from the primary steam jets are utilized for more complete atomization of the fuel prior to combustion.
- a second approach has used a mixing chamber with tangential slots which impart a whirling action to the fuel by discharging steam tangentially about the circumference of the fuel discharge passage.
- Nozzles of the above mentioned design while providing atomization of the'fuel, will not produce a narrow flame to avoid flame impingement of the tubes in a narrow firebox.
- this invention provides an advantageous approach whereby a long narrow flame is produced by an unique method of swirling the pressure atomized fuel prior to combustion for use in a narrow firebox without loss of heat release by the burner.
- the above advantages have been attained in the present invention by the drilling of the cylindrical ducts at a compound angle in the direction of the air swirl in addition to the main cone angle.
- the main cone angle is an included angle defining an outwardly directed cone with its apex in the nozzle tip.
- FIG. 1 is a view in side elevation of the device
- FIG. 2 is a centrallongitudinal section through a nozzle tip for practicing my invention.
- FIG. 3 is a view in front elevation of the device shown in FIGS. 1 and 2, showing the outlet side of the nozzle tip.
- 1 indicates the nozzle body in which an internal passageway 2 is formed such that it is symmetrical about longitudinal centerline 44 of nozzle body 1 and is closed on one end by a hemispherical chamber and is open at the opposite end for entry of pressure atomized fuel into nozzle body 1.
- piercing the external truncated cone formed by external surface 5 are formed such that cylindrical ducts 3 are equally spaced along the circumference 6 on external surface 5 and projecting inwardly such that a plane extending along a longitudinal centerline of cylindrical ducts 3 would form a first acute angle of 28 to 32 at the intersection of longitudinal centerline 4-4 of nozzle body '1 forming the main cone angle.
- an acute lead angle of 8 to 12 is used to position cylindrical ducts 3 such that a compound angle is formed in the direction of external air swirl A at the closed end of nozzle body 1.
- the main cone angle, lead angle, and nozzle body cone angle are important in order that a long narrow flame be produced during combustion of the pressure atomized fuel in a narrow firebox without reducing heat release and avoiding flame impingement of the tubes.
- Nozzle designs with reduced main cone angles and the same nozzle body cone angle but no lead angle were tested by heat release was substantially reduced even though a long narrow flame resulted.
- a nozzle for swirling pressure atomized fuel to produce a long narrow flame comprising:
- a nozzle body an internal passageway in said nozzle body open at one end and closed by a hemispherical chamber at the other end, said passageway being symmetrical about the longitudinal centerline of said nozzle body; the nozzle body having an external surface at the closed end in the form of a truncated cone forming a nozzle body cone angle having its apex forward of said closed end and symmetrical about the longitudinal centerline of said nozzle body; and a plurality of cylindrical ducts in said nozzle body piercing the external conical surface and communicating with said hemispherical chamber, each of .which is positioned with a main cone angle and lead angle.
- nozzle body cone angle is an acute angle of 45 to 50 degrees.
- main cone angle is an acute angle of 28 to 32.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
In a pressure atomized oil burner having air louvers to swirl primary air, a long narrow flame is produced without reducing heat release by using a nozzle tip having cylindrical ducts drilled at a compound angle in the direction of the air swirl in addition to the main cone angle.
Description
llnited States Patent 1 Howe [ FUEL BURNER NOZZLE [75] Inventor: Frank C. Howe, Bakersfield, Calif.
[73] Assignee: Shell Oil Company, New York,
[22] Filed: June 3, 1971 [21] Appl.No.: 149,679
52 'u.s .cl..-...... ..239/490 51 Int.Cl. ..B05b 1/34 [58] FieldofSearch.. ..239/,490,567,596,
[ 56] I References Cited .1 UNITED STATES PATENTS 3,279,705 10/1966 Stiefel ..239/49O [4 1 May 1,1973
3,452,933 7/1969 Hakluytt ..239/567 X 1,408,521 3/1922 Lathrop ..239/490 2,462,704 2/1949 Zink ..239/596 X Primary ExaminerM. Henson Wood, Jr. Assislant Examiner-Reinhold W. Thieme Attorney-Theodore E. Bieber and-Harold L. Denkler [57] ABSTRACT In a pressure atomized oil burner having air louvers to swirl primary air, a long narrow flame is produced without reducing heat release by using a nozzle tip having cylindrical ducts drilled at a compound angle in the direction of the air swirl in addition to the main cone angle.
6 Claims, 3 Drawing Figures PATENTEDHAY H y 3.730.438
' F. C, Howe INVENTOR FUEL BURNER NOZZLE BACKGROUND OF THE INVENTION The present invention relates to a fuel nozzle tip. More particularly, the invention concerns itself with pressure atomized fuel oil burner nozzle tips for use in a narrow firebox.
It is common practice to atomize fuel used in fireboxes in order to effectively disperse the fuel into a fine mist for more efficient combustion. In one approach used to steam atomize fuel prior to burning, the primary and secondary jets are disposed concentric to and outward from a central fluid opening in the nozzle such that the primary steam jets are directed tangentially to and against the circumference of the fuel to be atomized flowing from the central opening. The secondary steam jets which are disposed concentric to and outward from the primary steam jets are utilized for more complete atomization of the fuel prior to combustion.
A second approach has used a mixing chamber with tangential slots which impart a whirling action to the fuel by discharging steam tangentially about the circumference of the fuel discharge passage.
Nozzles of the above mentioned design, while providing atomization of the'fuel, will not produce a narrow flame to avoid flame impingement of the tubes in a narrow firebox.
SUMMARY OF THE INVENTION Accordingly, this invention provides an advantageous approach whereby a long narrow flame is produced by an unique method of swirling the pressure atomized fuel prior to combustion for use in a narrow firebox without loss of heat release by the burner.
The above advantages have been attained in the present invention by the drilling of the cylindrical ducts at a compound angle in the direction of the air swirl in addition to the main cone angle. The main cone angle is an included angle defining an outwardly directed cone with its apex in the nozzle tip.
DESCRIPTION OF THE DRAWING The above noted and other advantages of the present invention will be understood from the following description taken with reference to the accompanying drawing. In describing the invention in detail, reference will be made to the drawing in which like reference'numerals designate like parts throughout corresponding views in which:
FIG. 1 is a view in side elevation of the device;
FIG. 2 is a centrallongitudinal section through a nozzle tip for practicing my invention; and
FIG. 3 is a view in front elevation of the device shown in FIGS. 1 and 2, showing the outlet side of the nozzle tip.
DESCRIPTION OF PREFERRED EMBODIMENT Referring more particularly to the drawing, 1 indicates the nozzle body in which an internal passageway 2 is formed such that it is symmetrical about longitudinal centerline 44 of nozzle body 1 and is closed on one end by a hemispherical chamber and is open at the opposite end for entry of pressure atomized fuel into nozzle body 1. An external truncated cone O ternal passageway 2 with external air swirl A, and
piercing the external truncated cone formed by external surface 5 are formed such that cylindrical ducts 3 are equally spaced along the circumference 6 on external surface 5 and projecting inwardly such that a plane extending along a longitudinal centerline of cylindrical ducts 3 would form a first acute angle of 28 to 32 at the intersection of longitudinal centerline 4-4 of nozzle body '1 forming the main cone angle. In addition to the main cone angle, an acute lead angle of 8 to 12 is used to position cylindrical ducts 3 such that a compound angle is formed in the direction of external air swirl A at the closed end of nozzle body 1.
OPERATION The operation of the above disclosed arrangement is as follows. As pressure atomized fuel enters the nozzle body at internal passageway 2 and passes through ducts 3 for combustion, a swirling action is imposed on the pressure atomized fuel by the compound angle formed by drilling of the ducts 3 at the main cone angle and lead angle simultaneously. For example, a main cone angle of approximately 30 degrees and lead angle of approximately 10 in combination with a nozzle body cone angle in the range of 45 has been found to produce a long narrow flame without reduction of heat release of the burner. The lead angle is drilled in the direction of the external air swirl A which can be either clockwise or counterclockwise, but in this case is counterclockwise. The main cone angle, lead angle, and nozzle body cone angle are important in order that a long narrow flame be produced during combustion of the pressure atomized fuel in a narrow firebox without reducing heat release and avoiding flame impingement of the tubes. Nozzle designs with reduced main cone angles and the same nozzle body cone angle but no lead angle were tested by heat release was substantially reduced even though a long narrow flame resulted.
I claim as my invention: 1. A nozzle for swirling pressure atomized fuel to produce a long narrow flame, comprising:
a nozzle body; an internal passageway in said nozzle body open at one end and closed by a hemispherical chamber at the other end, said passageway being symmetrical about the longitudinal centerline of said nozzle body; the nozzle body having an external surface at the closed end in the form of a truncated cone forming a nozzle body cone angle having its apex forward of said closed end and symmetrical about the longitudinal centerline of said nozzle body; and a plurality of cylindrical ducts in said nozzle body piercing the external conical surface and communicating with said hemispherical chamber, each of .which is positioned with a main cone angle and lead angle.
2. The nozzle of claim 1 wherein said nozzle body cone angle is an acute angle of 45 to 50 degrees. a 3. The nozzle of claim 1 wherein said main cone angle is an acute angle of 28 to 32.
5. The nozzle of claim 1 wherein said plurality of cylindrical ducts are equally spaced.
6. The nozzle of claim 1 wherein said lead angle is 4. The nozzle of claim 1 wherein said lead angle is an 5 positioned in the direction of external air Swirl acute angle of 8 to 12.
Claims (6)
1. A nozzle for swirling pressure atomized fuel to produce a long narrow flame, comprising: a nozzle body; an internal passageway in said nozzle body open at one end and closed by a hemispherical chamber at the other end, said passageway being symmetrical about the longitudinal centerline of said nozzle body; the nozzle body having an external surface at the closed end in the form of a truncated cone forming a nozzle body cone angle having its apex forward of said closed end and symmetrical about the longitudinal centerline of said nozzle body; and a plurality of cylindrical ducts in said nozzle body piercing the external conical surface and communicating with said hemispherical chamber, each of which is positioned with a main cone angle and lead angle.
2. The nozzle of claim 1 wherein said nozzle body cone angle is an acute angle of 45 to 50 degrees.
3. The nozzle of claim 1 wherein said main cone angle is an acute angle of 28* to 32* .
4. The nozzle of claim 1 wherein said lead angle is an acute angle of 8* to 12* .
5. The nozzle of claim 1 wherein said plurality of cylindrical ducts are equally spaced.
6. The nozzle of claim 1 wherein said lead angle is positioned in the direction of external air swirl.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14967971A | 1971-06-03 | 1971-06-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3730438A true US3730438A (en) | 1973-05-01 |
Family
ID=22531354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00149679A Expired - Lifetime US3730438A (en) | 1971-06-03 | 1971-06-03 | Fuel burner nozzle |
Country Status (1)
Country | Link |
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US (1) | US3730438A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5372312A (en) * | 1993-08-23 | 1994-12-13 | Spraying Systems Co. | Air atomizing spray nozzle assembly with angled discharge orifices |
GB2454247A (en) * | 2007-11-02 | 2009-05-06 | Siemens Ag | A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle |
CN101879487A (en) * | 2009-05-06 | 2010-11-10 | 安德烈亚斯.斯蒂尔两合公司 | Be used to spray the shower nozzle that blows jet pipe of apparatus |
RU170439U1 (en) * | 2017-01-11 | 2017-04-25 | Михаил Николаевич Оверченко | NOZZLE |
RU171370U1 (en) * | 2017-01-13 | 2017-05-29 | Михаил Николаевич Оверченко | NOZZLE |
RU171619U1 (en) * | 2017-01-11 | 2017-06-07 | Михаил Николаевич Оверченко | NOZZLE |
US20180363551A1 (en) * | 2017-06-16 | 2018-12-20 | General Electric Company | System and method for combusting liquid fuel in a gas turbine combustor |
US20190217137A1 (en) * | 2018-01-12 | 2019-07-18 | Carrier Corporation | End cap agent nozzle |
US20220048051A1 (en) * | 2020-08-17 | 2022-02-17 | Medtronic, Inc. | Helical Nozzle |
EP4407233A1 (en) * | 2023-01-24 | 2024-07-31 | Hamilton Sundstrand Corporation | Fuel nozzles |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1408521A (en) * | 1920-06-21 | 1922-03-07 | Harry D Lathrop | Spray head |
US2462704A (en) * | 1945-02-07 | 1949-02-22 | John S Zink | Burner and burner nozzle |
US3279705A (en) * | 1964-03-13 | 1966-10-18 | Cleaver Brooks Co | Gas burner nozzle |
US3452933A (en) * | 1966-04-30 | 1969-07-01 | Nat Res Dev | Oil fuel burning equipment |
-
1971
- 1971-06-03 US US00149679A patent/US3730438A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1408521A (en) * | 1920-06-21 | 1922-03-07 | Harry D Lathrop | Spray head |
US2462704A (en) * | 1945-02-07 | 1949-02-22 | John S Zink | Burner and burner nozzle |
US3279705A (en) * | 1964-03-13 | 1966-10-18 | Cleaver Brooks Co | Gas burner nozzle |
US3452933A (en) * | 1966-04-30 | 1969-07-01 | Nat Res Dev | Oil fuel burning equipment |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5372312A (en) * | 1993-08-23 | 1994-12-13 | Spraying Systems Co. | Air atomizing spray nozzle assembly with angled discharge orifices |
EP0640401A1 (en) * | 1993-08-23 | 1995-03-01 | Spraying Systems Co. | Air atomizing spray nozzle assembly with angled discharge orifices |
GB2454247A (en) * | 2007-11-02 | 2009-05-06 | Siemens Ag | A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle |
US8984889B2 (en) | 2007-11-02 | 2015-03-24 | Siemens Aktiengesellschaft | Combustor for a gas-turbine engine with angled pilot fuel nozzle |
CN101879487A (en) * | 2009-05-06 | 2010-11-10 | 安德烈亚斯.斯蒂尔两合公司 | Be used to spray the shower nozzle that blows jet pipe of apparatus |
CN101879487B (en) * | 2009-05-06 | 2015-06-17 | 安德烈亚斯.斯蒂尔两合公司 | Spray head for a blower tube of a spray apparatus |
RU170439U1 (en) * | 2017-01-11 | 2017-04-25 | Михаил Николаевич Оверченко | NOZZLE |
RU171619U1 (en) * | 2017-01-11 | 2017-06-07 | Михаил Николаевич Оверченко | NOZZLE |
RU171370U1 (en) * | 2017-01-13 | 2017-05-29 | Михаил Николаевич Оверченко | NOZZLE |
US20180363551A1 (en) * | 2017-06-16 | 2018-12-20 | General Electric Company | System and method for combusting liquid fuel in a gas turbine combustor |
US10982593B2 (en) * | 2017-06-16 | 2021-04-20 | General Electric Company | System and method for combusting liquid fuel in a gas turbine combustor with staged combustion |
US20190217137A1 (en) * | 2018-01-12 | 2019-07-18 | Carrier Corporation | End cap agent nozzle |
US11305142B2 (en) * | 2018-01-12 | 2022-04-19 | Carrier Corporation | End cap agent nozzle |
US20220048051A1 (en) * | 2020-08-17 | 2022-02-17 | Medtronic, Inc. | Helical Nozzle |
EP4407233A1 (en) * | 2023-01-24 | 2024-07-31 | Hamilton Sundstrand Corporation | Fuel nozzles |
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