US478295A - george h - Google Patents
george h Download PDFInfo
- Publication number
- US478295A US478295A US478295DA US478295A US 478295 A US478295 A US 478295A US 478295D A US478295D A US 478295DA US 478295 A US478295 A US 478295A
- Authority
- US
- United States
- Prior art keywords
- fuel
- air
- axis
- burner
- passage
- 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
Links
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
- F23D11/001—Spraying nozzle combined with forced draft fan in one unit
Definitions
- Our invention relates to that class ofburners in which liquid fuel-such as hydrocarbon oil-is atomized and combined with air.
- Our improved burner comprises a central fuel-passageand a series of air-passages inclining inwardly from their rear ends toward the front and having their axes arranged tangentially to a circle drawn from the axis of the fuel-passage as a center.
- the jets of air issuing from the air-passages act tangentially upon the fuel-jet outside the burner in an inclined direction, the combined effect being to rotate the oil-jet, spread it by centrifugal force, and carry it forwardly and outwardly to form a conical mass of finely-subdivided and commingled oil and air in the best pos- 3 5 sible condition for burning.
- Figure l is a front elevation of our burner, and Fig. 2a vertical central section on the line cf of Fig. 1.
- the head B of the burner is provided with a central passage, (shown as containingapipe A,) through which liquid fuel is fed.
- the pipe A preferably projects a short distance in front of the burner-head, and may connect with any suitable reservoir or source of sup- 5o ply for feeding fuel under pressure.
- burner-head in this instance is shown as circular and screw-threaded on its periphery, being secured to the casing C of an air-chamber D.
- Air is supplied in any suitable Way to this chamber and is delivered through passages a to the front or outside of the burner.
- the passages a extend through the burnerhead and are arranged obliquely around the central fuel-passage A, being inclined from their inner ends toward the central passage, and they are arranged tangentially theretothat is to say, the axes of the openings at are tangential to a circle drawn from the axis of the fuel-opening A as a center.
- the airopenings are inclined from theirinner ends toward the center; but they do not point directly at the center, and so their axes do not come to a focus, although they do come close together and pass each other, so that the jets of air act on the oil-jet to produce arotary, whirling, or whirlwind-like motion to throw the oil out into a conical mass, finely subdivided, atomized, and mixed with air.
- a liquid-fuel burner comprising a central fuel-passage and a series ofseparate and distinct rectilinear air passages arranged around it, each of which is inclined inwardly from its rear end toward the front and has its axis arranged tangentially to a circle drawn from the axis of the fuel-passage as a center and lying in a plane transverse to said axis.
- a liquid-fuel burner having a central f uel-passage, around which are arranged separate and distinct passages for the discharge of the atomizing medium, the axis of discharge of each of said latter passages being inclined inwardly toward the axis of the fuelpassage and tangential to a circle of which
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)
Description
(No Model.) v
E. SQUIRE, G. H. COBB 8v 1?. M. TOWL.
LIQUID FUEL BURNER.
No. 478,295. r Patented July 5, 1892.
w BY
* @M'mmvw ma NORRIS FETERE cm, mom-mum WASNINGYON, n. c.
UMTED STATES ATENT OFFICE.
EDWIN SQUIRE, OF MONTCLAIR, NEW JERSEY, GEORGE 'H. COBB, OF ELMIRA, AND FORREST M. TOWL, OF BROOKLYN, N. Y.
LIQUID-FUEL BU RNER:
SPECIFICATION forming part of Letters Patent No. 478,295, dated July 5, 1892.
Application filed September 15, 1891- Serial No. 405,783. (No model.)
To all whom it may concern:
Be it known that we, EDWIN SQUIRE, residing at Montclair, County of Essex, State of New Jersey, GEORGE H. COBB, residing at Elmira,
5 county of Obemung, and FORREST M. ToWL, residing at Brooklyn, county of Kings, State of New York, have invented certain new and useful Improvements in Liquid-Fuel Burners, of which the following is a specification.
[ Our invention relates to that class ofburners in which liquid fuel-such as hydrocarbon oil-is atomized and combined with air.
By our invention we cause jets of air to act immediately in front of the burner on a jet of oil tangentially and in an inwardly and forwardly inclined direction, whereby the oil-jet is given a rotary motion, is atomized, sprayed, and commingled with the air and spread by centrifugal force and by the action of the airjets into a wide conical form best adapted for burning.
Our improved burner comprises a central fuel-passageand a series of air-passages inclining inwardly from their rear ends toward the front and having their axes arranged tangentially to a circle drawn from the axis of the fuel-passage as a center. The jets of air issuing from the air-passages act tangentially upon the fuel-jet outside the burner in an inclined direction, the combined effect being to rotate the oil-jet, spread it by centrifugal force, and carry it forwardly and outwardly to form a conical mass of finely-subdivided and commingled oil and air in the best pos- 3 5 sible condition for burning.
The accompanying drawings show our improvements embodied in a simple and practical form; but our improvements may be embodied in apparatus differing in details of construction from that shown.
Figure l is a front elevation of our burner, and Fig. 2a vertical central section on the line cf of Fig. 1.
The head B of the burner is provided with a central passage, (shown as containingapipe A,) through which liquid fuel is fed. The pipe A preferably projects a short distance in front of the burner-head, and may connect with any suitable reservoir or source of sup- 5o ply for feeding fuel under pressure. The
burner-head in this instance is shown as circular and screw-threaded on its periphery, being secured to the casing C of an air-chamber D. Air is supplied in any suitable Way to this chamber and is delivered through passages a to the front or outside of the burner. The passages a extend through the burnerhead and are arranged obliquely around the central fuel-passage A, being inclined from their inner ends toward the central passage, and they are arranged tangentially theretothat is to say, the axes of the openings at are tangential to a circle drawn from the axis of the fuel-opening A as a center. Thus the airopenings are inclined from theirinner ends toward the center; but they do not point directly at the center, and so their axes do not come to a focus, although they do come close together and pass each other, so that the jets of air act on the oil-jet to produce arotary, whirling, or whirlwind-like motion to throw the oil out into a conical mass, finely subdivided, atomized, and mixed with air.
When we speak of the air-passages as being arranged tangentially to the fuel-passage, we mean that although the air-passages are obliquely arranged and inclined from their innor ends toward the axis of the fuel-passage they do not point directly at the axis of the fuel-passage and their axes do not focus at the axis of the fuel-passage or with each other. After the air-jets leave the burner they cut the oil-jet to an extent sufficient to produce the requisite frictional contact to eifect the rotary and outwardly inclined movement thereof.
When We speak of the axis of discharge, we mean the line of projection of the spraying or atomizing medium, as air or well-known equivalent mediums. 9
When we speak of the air-passages or their axes of discharge being tangential to a circle of which the axis of the oil-passage is the center, we-refer to a circle lying in a plane transverse to said axis, and we do not mean that they are true tangents in the sense that they are in the same plane as the circle, but that they are inclined to the plane of the circle and occupy a tangential relation thereto, as shown in the drawings.
We claim as of our invention- 1. A liquid-fuel burner comprising a central fuel-passage and a series ofseparate and distinct rectilinear air passages arranged around it, each of which is inclined inwardly from its rear end toward the front and has its axis arranged tangentially to a circle drawn from the axis of the fuel-passage as a center and lying in a plane transverse to said axis.
2. A liquid-fuel burner having a central f uel-passage, around which are arranged separate and distinct passages for the discharge of the atomizing medium, the axis of discharge of each of said latter passages being inclined inwardly toward the axis of the fuelpassage and tangential to a circle of which
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US478295A true US478295A (en) | 1892-07-05 |
Family
ID=2547150
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US478295D Expired - Lifetime US478295A (en) | george h |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US478295A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2517015A (en) * | 1945-05-16 | 1950-08-01 | Bendix Aviat Corp | Combustion chamber with shielded fuel nozzle |
| US4583941A (en) * | 1982-08-13 | 1986-04-22 | Ben-Gurion University Of The Negev Research And Development Authority | Burner for gaseous fuel |
| US4765540A (en) * | 1985-11-21 | 1988-08-23 | Fluidyne Corporation | Process and apparatus for generating multiple fluid jets |
| US6378787B1 (en) * | 1997-09-15 | 2002-04-30 | Alstom | Combined pressure atomizing nozzle |
| US20060147861A1 (en) * | 2005-01-05 | 2006-07-06 | Charles Czajka | Gas circuit and pilot light system for cooking range |
| US20060144253A1 (en) * | 2005-01-05 | 2006-07-06 | Charles Czajka | Cooking range assembly and monolithic drip pan |
| US20120187220A1 (en) * | 2011-01-24 | 2012-07-26 | Illinois Tool Works Inc. | High swirl air cap |
-
0
- US US478295D patent/US478295A/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2517015A (en) * | 1945-05-16 | 1950-08-01 | Bendix Aviat Corp | Combustion chamber with shielded fuel nozzle |
| US4583941A (en) * | 1982-08-13 | 1986-04-22 | Ben-Gurion University Of The Negev Research And Development Authority | Burner for gaseous fuel |
| US4765540A (en) * | 1985-11-21 | 1988-08-23 | Fluidyne Corporation | Process and apparatus for generating multiple fluid jets |
| US6378787B1 (en) * | 1997-09-15 | 2002-04-30 | Alstom | Combined pressure atomizing nozzle |
| US20060147861A1 (en) * | 2005-01-05 | 2006-07-06 | Charles Czajka | Gas circuit and pilot light system for cooking range |
| US20060144253A1 (en) * | 2005-01-05 | 2006-07-06 | Charles Czajka | Cooking range assembly and monolithic drip pan |
| US7363923B2 (en) | 2005-01-05 | 2008-04-29 | Illinois Tool Works Inc. | cooking range assembly and monolithic drip pan |
| US7811082B2 (en) | 2005-01-05 | 2010-10-12 | Premark Feg, Llc | Gas circuit and pilot light system for cooking range |
| US20120187220A1 (en) * | 2011-01-24 | 2012-07-26 | Illinois Tool Works Inc. | High swirl air cap |
| US9302281B2 (en) * | 2011-01-24 | 2016-04-05 | Carlisle Fluid Technologies, Inc. | High swirl air cap |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2353854C2 (en) | Mechanical atomiser | |
| US391865A (en) | schutte | |
| US2602292A (en) | Fuel-air mixing device | |
| US721900A (en) | Oil-burner. | |
| US3667679A (en) | Apparatus for mixing a plurality of gaseous streams | |
| US478295A (en) | george h | |
| US1719090A (en) | Oil burner | |
| US1150940A (en) | Liquid-atomizer. | |
| US1587249A (en) | Method of and apparatus for burning oil | |
| US1020612A (en) | Hydrocarbon-burner. | |
| US733579A (en) | Hydrocarbon-burner. | |
| US1428896A (en) | Steam-atomizing fuel-oil burner | |
| US422222A (en) | Injector oil-burner | |
| US1055411A (en) | Oil-burner. | |
| US433639A (en) | Oil-burner | |
| US418582A (en) | Santo | |
| US1762356A (en) | Liquid-fuel burner | |
| US895668A (en) | Oil-burner. | |
| US1197600A (en) | Oil-atomizer. | |
| US715044A (en) | Oil-burner. | |
| US449315A (en) | Bykon h | |
| US467427A (en) | Steam-jet blower for furnaces | |
| US614194A (en) | Oil-burner | |
| US752900A (en) | Hydrocarbon-burner | |
| US1193819A (en) | Oil-burner |