US1474867A - Hydrocarbon burner - Google Patents
Hydrocarbon burner Download PDFInfo
- Publication number
- US1474867A US1474867A US367667A US36766720A US1474867A US 1474867 A US1474867 A US 1474867A US 367667 A US367667 A US 367667A US 36766720 A US36766720 A US 36766720A US 1474867 A US1474867 A US 1474867A
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- US
- United States
- Prior art keywords
- fuel
- combustion chamber
- air
- nozzle
- burner
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C99/00—Subject-matter not provided for in other groups of this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
- F23C2700/02—Combustion apparatus using liquid fuel
- F23C2700/023—Combustion apparatus using liquid fuel without pre-vaporising means
Definitions
- his invention relates t'o hydro-carbon burners of the atomizing type.
- primary object of the invention is to provide a burner which does not have the characteristic roaring noise common to burn- ⁇ ers of this type.
- a burner mixing tube 11 preferably of venturi shape, connects with and vopens into the combustion chamber 10, while its opposite endcommunicates with the at.- mosphere.
- a fuel spray nozzle 12 Within the mixing tube 11, and relatively close to the end of same incom- Amunication with the combustion chamber, is positioned a fuel spray nozzle 12.
- the object ofA the4 nozzle 13 is to induce the air supply for combustion to ow through the mixing tube 11, into the cbmbustion chamber 10.
- rllo increase the eiciency of the induction jet issuing from the nozzle 13, a series of frustoconical tubes 14e, are placed concentric with the mixing tube 11 and are located in front of the induction nozzle 13, so that its issuing jet will How there-thru. y
- Extending into the mixing tube 11 is an electric spark plug 15, so placed that the electric sparkproduced by it will take place within the zone ofthe diverging spray of fuel from the atomizing or spray nozzle 12, to insure prompt ignition.
- the atomizing fuel nozzle 12 Connected with the atomizing fuel nozzle 12, is the'pipel for conveying fuel under pressure from a fuel tank, or other source of supply.
- rlfhe fuel nozzle 12 may befofany approved design, but preferably suchthat the fuel is as finely atomized as possible.
- a pilot light or sub-burner whichmay be of the form of an ordinary blow torch burner, and supplied with fuel thru the pipe 20.
- rl'he pilot light 18 is placed so that it will project its flame within the combustion chamber 10 and preferably in close proximity to the incoming charge of air and fuel as it enters from the mining tube 11, the object-being to facilitate early ignition.
- the spark Iplug 15 or the pilot light 18 may be used as a means to ignite the atomized fuel, or both may be used; the chief object of the pilot light 18, aside from its function as a means Qf igniting the main burner, being to maintain steam in the boiler with which the burner is used, when the main burner for any reason is notin operation.
- the operation of the burner is as follows F rom a source of supply (not shown) fuel under pressure is turned through the pipe A17, leading to the nozzle 12, from which it issues in an atomized state and is ignited by an electric spark produced by the spark plug 15, or bythe flame of the pilot light 18. lmni'ediately following or simultaneously with the turning on of the fuel to the spray nozzle 12 ⁇ steam or compressed air under suitable pressure is turned into the pipe 19, connected to the inductionvnozzle 13 from 'which the jet of steam or compressed air ing through the frusto-conical tubes 14 and the Venturi mixing tube 11,*induces air to flow through the mixing tube 11 into the combustion chamber 10.
- This induced air as it passes the fuel spray nozzle 12, partially mixes With the spray issuing therefrom, and carries'it into the combustion chamber 10, which is preferably of such shape that the velocity of the incoming mixture of air and fuel Will cause the resulting flame to take a rotary or whirling motionV so that the combustion Will be completed Within the combustion chamber, thus preventing the flame from rising and imping ing on the surfaces of the boiler which is preferably located above the combustion chamber or tire box 10.
- the inducted air has attained considerable velocity before it reaches the spray fromtlie nozzle 12, which is located near the outlet ofthe mixing tube 1l, Where it enters the combustion chamber 10.
- the air and fuel are not thoroughly7 mixed until the charge has entered the combustion chamber.
- the atomized spray froml the fuel nozzle 12 spreads in the form of a cone and the air being forced past envelopes this spray and results in a relativelylean mixture adjacent the Walls of the mixing tube 11, Where it enters the combustion chamber While the central portion of this conical spray remains comparatively rich until it has entered the combustion chamber. rlhis condition prevents any tendency of the charge to back tire into the mixing tube 11 and hence eliminates the roaring noise characteristic of burners of the atomizing type as commonly constructed. It also facilitates ignition'by means of an electric spark.
- lt is understood that the relative amount of fuel and air in the mixture required for .perfect combustion may be regulated by suitable valves (not shown) located in the supply pipes 17 and 19. lt is also clear that any desirable method of producing and timing the electric ignitionspark may b'e employed.
- An important feature of my invention is the mixing of the charge of fuel and air which is vnot completed until it has entered the combustion chamber. This not only resuits in the elimination of the objectionable roaring noise as previously explained, but
- Vor steam may be used in connection with the induction nozzle 13 for inducing the air supply necessary for combustion. It will be also understood that compressed air may be used for the initial operation of the burner until steam pressure on the boiler is generated, when this steam pressure may be used instead of the compressed air.
- the burner is here illustrated in combination with a combustion chamber of substantially rectangular form with inner Walls of such contour as to cause the incoming charge of air and fuel to divide and rotate in two adjoining vortices, for the purpose of preventing the fire from rising out of the combustion chamber and to cause complete combustion by thoroughly mixing the incoming. charge, the burner may be used with other forms of combustion chambers.
- a hydrocarbon burner comprising an air induction tube, an induction nozzle stationed relatively near the air inlet of said in ⁇ duction tube, a fuel spray nozzle located Within said induction tube ahead of said induction nozzle and in the path of the issuing jet from said induction nozzle and the air supply induced thereby, both nozzles being located substantially concentric with the throat of the induction tube.
- a combustion chamber having an inlet Aopening and an outlet opening, a hydrocarbon burner in said inlet opening, comprising an induction tube, a nozzle adapted to deliver an air inducing jet of gas under pressure and located at the entering end of said induction tube, a fuel spray nozzle located at. the delivery end of the induction tube. adjacent 'the combustion chamber, and in the path ofthe induced air Laviana?
- a hydrocarbon burner comprising an air induction tube, an opening in said tube conmunicating with the atmosphere, a nozzle adapted to deliver an air inducing jet of gas under pressure and located at one end of said induction tube, and a fuel spray nozzle located at the other end of the induction tube and in the path of the induced air supply, said burner being so placed with relation to the combustion chamber as to produce a vortex therein, v
- a combustion chamber comprising an air induction tube, an opening in said tube communicating with the atmosphere.
- a nozzle adapted to deliver an air inducing jet of gas under pressure and located at. the entering end of said induction tube, and a fuel spray nozzle located at the delivery end of the in' duction tube and in the path of the induced air supply,
- Said combustion chamber having an internally projecting wall, the mixture from said burner being directed against said projecting Wall so as to form two vortices substantially filling the combustion chamber.
- hydrocarbon burner comprising an air induction tube, a series of frustro-conical tubes located therein, and substantially concentric -with said induction tube, a nozzle adapted to deliver an air inducing jet of gas under pressure through said frusto-conical tubes and said induction tube, a fuel spray nozzle located Within said induction tube and ahead ot said frusto-conical tubes and in the path of the issuing jet from said induction nozzle and an ignition spark plug in front of said fuel spray nozzle.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
E. c. WALKER HYDROCARBON BURNER Nov. 20, 1923..
Filed March 22 1920 Tx; MMIAIAMITMHW /Y IV IV IV .IV IIV IV IV m. u Q A PatenftedNov.. Ztl), i923., Y
j unuTnn sTeTns EARL C. WMKJER, l? CANTON, ELLIIINOIS, ASSGNR T0 WILLIAM l?. lINGERSOlLL, 0F
CANTON, ILLINOS.
f ineen/ PATENT ortica.;
Hannocnnnon nomina. y
To `all whom t may concer/1.'.
Be it known that l, EARL C. WALKER, a citizen of the United States, residinor at Canton, in the county bf Fulton and iate of Illinois, have invented new `and useful Hydrocarbon Burners, of which the followinfr isa specilication. A i
his invention relates t'o hydro-carbon burners of the atomizing type. M
primary object of the invention is to provide a burner which does not have the characteristic roaring noise common to burn- {ers of this type.
fbustion chamber as well as the boiler or other parts associated therewith.
'llhese and other objects are accomplished by my invention which is fully described in the following specification and shown in the drawing in which the 'igure is a longitudinal section thru the burner and combustion chamber.
l have illustra-ted an embodiment of my invention asapplied to-a combustion cham- Aber which is substantially rectangular "in form, with inner walls having such contour as to give proper direction or circulation of the Haine as indicated by the arrow points. A burner mixing tube 11, preferably of venturi shape, connects with and vopens into the combustion chamber 10, while its opposite endcommunicates with the at.- mosphere. Within the mixing tube 11, and relatively close to the end of same incom- Amunication with the combustion chamber, is positioned a fuel spray nozzle 12. supplied with fuel under pressure through the pipe.v 17, leading from the source of fuel supply (not shown), while back of the fuel 4spray nozzle 12 and relatively near the mouth or inlet of the`,mixing tube is` located the induction nozzle 13, supplied with compressed air or steam under pressure through the pipe 19. Both the fuel spray nozzle 12 .and the steam or compressed air nozzlel are placed substantially concentric with the v Application led March 22, 1920. Serial No. 367,667.
mixing tube 11 and set so that both discharge their respective issuing jets toward and into the combustion chamber 10. The object ofA the4 nozzle 13 is to induce the air supply for combustion to ow through the mixing tube 11, into the cbmbustion chamber 10. rllo increase the eiciency of the induction jet issuing from the nozzle 13, a series of frustoconical tubes 14e, are placed concentric with the mixing tube 11 and are located in front of the induction nozzle 13, so that its issuing jet will How there-thru. y
Extending into the mixing tube 11 is an electric spark plug 15, so placed that the electric sparkproduced by it will take place within the zone ofthe diverging spray of fuel from the atomizing or spray nozzle 12, to insure prompt ignition. Connected with the atomizing fuel nozzle 12, is the'pipel for conveying fuel under pressure from a fuel tank, or other source of supply. rlfhe fuel nozzle 12 may befofany approved design, but preferably suchthat the fuel is as finely atomized as possible. At 18 is shown a pilot light or sub-burner whichmay be of the form of an ordinary blow torch burner, and supplied with fuel thru the pipe 20. rl'he pilot light 18 is placed so that it will project its flame within the combustion chamber 10 and preferably in close proximity to the incoming charge of air and fuel as it enters from the mining tube 11, the object-being to facilitate early ignition. lt will be understood that either the spark Iplug 15 or the pilot light 18 may be used as a means to ignite the atomized fuel, or both may be used; the chief object of the pilot light 18, aside from its function as a means Qf igniting the main burner, being to maintain steam in the boiler with which the burner is used, when the main burner for any reason is notin operation. The operation of the burner is as follows F rom a source of supply (not shown) fuel under pressure is turned through the pipe A17, leading to the nozzle 12, from which it issues in an atomized state and is ignited by an electric spark produced by the spark plug 15, or bythe flame of the pilot light 18. lmni'ediately following or simultaneously with the turning on of the fuel to the spray nozzle 12` steam or compressed air under suitable pressure is turned into the pipe 19, connected to the inductionvnozzle 13 from 'which the jet of steam or compressed air ing through the frusto-conical tubes 14 and the Venturi mixing tube 11,*induces air to flow through the mixing tube 11 into the combustion chamber 10. This induced air, as it passes the fuel spray nozzle 12, partially mixes With the spray issuing therefrom, and carries'it into the combustion chamber 10, which is preferably of such shape that the velocity of the incoming mixture of air and fuel Will cause the resulting flame to take a rotary or whirling motionV so that the combustion Will be completed Within the combustion chamber, thus preventing the flame from rising and imping ing on the surfaces of the boiler which is preferably located above the combustion chamber or tire box 10.
It will be noted that the inducted air has attained considerable velocity before it reaches the spray fromtlie nozzle 12, which is located near the outlet ofthe mixing tube 1l, Where it enters the combustion chamber 10. The air and fuel are not thoroughly7 mixed until the charge has entered the combustion chamber. The atomized spray froml the fuel nozzle 12 spreads in the form of a cone and the air being forced past envelopes this spray and results in a relativelylean mixture adjacent the Walls of the mixing tube 11, Where it enters the combustion chamber While the central portion of this conical spray remains comparatively rich until it has entered the combustion chamber. rlhis condition prevents any tendency of the charge to back tire into the mixing tube 11 and hence eliminates the roaring noise characteristic of burners of the atomizing type as commonly constructed. It also facilitates ignition'by means of an electric spark.
lt is understoodthat the relative amount of fuel and air in the mixture required for .perfect combustion may be regulated by suitable valves (not shown) located in the supply pipes 17 and 19. lt is also clear that any desirable method of producing and timing the electric ignitionspark may b'e employed.
An important feature of my invention is the mixing of the charge of fuel and air which is vnot completed until it has entered the combustion chamber. This not only resuits in the elimination of the objectionable roaring noise as previously explained, but
what is of even greaterimportance,is the fact that a softer-flame results due to the longer Vtime required to burn the mixture and instead of this flame unpmging with concentrated intensity against the Wall of the lcombustion chamber and intensifying the heat at this point. the combustion of the charge of the flame propagation is gradual, taking place as the charge rotatesA or whirls in the combustion chamber. The result of this is better and more even heat distribution and hence it contributes not only to boiler eciency but also to boiler longevity. A common objection to ordinary forms of liquid fuel burners of the atomizing type, as previously constructed, has been the damage to boilers resulting from the concentration of the heat at one zone of the combustion chamber.
lt will be seen from the illustration and description that either compressed air Vor steam may be used in connection with the induction nozzle 13 for inducing the air supply necessary for combustion. It will be also understood that compressed air may be used for the initial operation of the burner until steam pressure on the boiler is generated, when this steam pressure may be used instead of the compressed air.
While the burner is here illustrated in combination with a combustion chamber of substantially rectangular form with inner Walls of such contour as to cause the incoming charge of air and fuel to divide and rotate in two adjoining vortices, for the purpose of preventing the fire from rising out of the combustion chamber and to cause complete combustion by thoroughly mixing the incoming. charge, the burner may be used with other forms of combustion chambers.
While I have shown and described but a single embodiment of my invention, it is to be understood that it is capable'of many modifications. Changes therefore in the construction and .arrangement :may be made Without departing from the spirit and scope of the invention as disclosed in the appended claims, in Which it is my intention to claim all novelty inherent in my inventionas broadly as possible in View of the prior art. j
What l claim as new and desire to secure by Letters ljatent is 1. A hydrocarbon burner comprising an air induction tube, an induction nozzle stationed relatively near the air inlet of said in` duction tube, a fuel spray nozzle located Within said induction tube ahead of said induction nozzle and in the path of the issuing jet from said induction nozzle and the air supply induced thereby, both nozzles being located substantially concentric with the throat of the induction tube.
2. In combination, a combustion chamber having an inlet Aopening and an outlet opening, a hydrocarbon burner in said inlet opening, comprising an induction tube, a nozzle adapted to deliver an air inducing jet of gas under pressure and located at the entering end of said induction tube, a fuel spray nozzle located at. the delivery end of the induction tube. adjacent 'the combustion chamber, and in the path ofthe induced air Laviana? a hydrocarbon burner comprising an air induction tube, an opening in said tube conmunicating with the atmosphere, a nozzle adapted to deliver an air inducing jet of gas under pressure and located at one end of said induction tube, and a fuel spray nozzle located at the other end of the induction tube and in the path of the induced air supply, said burner being so placed with relation to the combustion chamber as to produce a vortex therein, v
d. ln combination, a combustion chamber, a hydrocarbon burner comprising an air induction tube, an opening in said tube communicating with the atmosphere. a nozzle adapted to deliver an air inducing jet of gas under pressure and located at. the entering end of said induction tube, and a fuel spray nozzle located at the delivery end of the in' duction tube and in the path of the induced air supply, Said combustion chamber having an internally projecting wall, the mixture from said burner being directed against said projecting Wall so as to form two vortices substantially filling the combustion chamber. 15. hydrocarbon burner comprising an air induction tube, a series of frustro-conical tubes located therein, and substantially concentric -with said induction tube, a nozzle adapted to deliver an air inducing jet of gas under pressure through said frusto-conical tubes and said induction tube, a fuel spray nozzle located Within said induction tube and ahead ot said frusto-conical tubes and in the path of the issuing jet from said induction nozzle and an ignition spark plug in front of said fuel spray nozzle.
EARL C. WALKERO
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US367667A US1474867A (en) | 1920-03-22 | 1920-03-22 | Hydrocarbon burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US367667A US1474867A (en) | 1920-03-22 | 1920-03-22 | Hydrocarbon burner |
Publications (1)
Publication Number | Publication Date |
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US1474867A true US1474867A (en) | 1923-11-20 |
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ID=23448113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US367667A Expired - Lifetime US1474867A (en) | 1920-03-22 | 1920-03-22 | Hydrocarbon burner |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2440491A (en) * | 1935-03-21 | 1948-04-27 | Des Vehicules Sev Soc Et | Oil burner |
US2483737A (en) * | 1943-07-10 | 1949-10-04 | Stewart Warner Corp | Internal-combustion burner for heaters |
US2655205A (en) * | 1949-01-29 | 1953-10-13 | Linderoth Erik Torvald | Regenerative heating apparatus |
US2691966A (en) * | 1952-09-25 | 1954-10-19 | Young Paul G | Fluid fuel fired water-tube steam boiler |
US2765621A (en) * | 1953-01-23 | 1956-10-09 | Shell Dev | Combustion apparatus with toroidal eddy flame stabilizer |
US2920445A (en) * | 1957-01-15 | 1960-01-12 | Curtiss Wright Corp | Flame holder apparatus |
US2974485A (en) * | 1958-06-02 | 1961-03-14 | Gen Electric | Combustor for fluid fuels |
DE1148687B (en) * | 1959-08-24 | 1963-05-16 | Ziemann Gmbh Maschinenfabrik A | Firing for a brewing pan |
US4019851A (en) * | 1975-09-22 | 1977-04-26 | Combustion Engineering, Inc. | High energy arc ignitor for burner |
US4458480A (en) * | 1980-12-15 | 1984-07-10 | Irwin Everett F | Rotating cylinder external combustion engine |
US20050277074A1 (en) * | 2004-06-10 | 2005-12-15 | Zinn Ben T | Stagnation point reverse flow combustor |
US20080274021A1 (en) * | 2007-05-01 | 2008-11-06 | Jacobus Neels | Compact Fuel Processor |
-
1920
- 1920-03-22 US US367667A patent/US1474867A/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2440491A (en) * | 1935-03-21 | 1948-04-27 | Des Vehicules Sev Soc Et | Oil burner |
US2483737A (en) * | 1943-07-10 | 1949-10-04 | Stewart Warner Corp | Internal-combustion burner for heaters |
US2655205A (en) * | 1949-01-29 | 1953-10-13 | Linderoth Erik Torvald | Regenerative heating apparatus |
US2691966A (en) * | 1952-09-25 | 1954-10-19 | Young Paul G | Fluid fuel fired water-tube steam boiler |
US2765621A (en) * | 1953-01-23 | 1956-10-09 | Shell Dev | Combustion apparatus with toroidal eddy flame stabilizer |
US2920445A (en) * | 1957-01-15 | 1960-01-12 | Curtiss Wright Corp | Flame holder apparatus |
US2974485A (en) * | 1958-06-02 | 1961-03-14 | Gen Electric | Combustor for fluid fuels |
DE1148687B (en) * | 1959-08-24 | 1963-05-16 | Ziemann Gmbh Maschinenfabrik A | Firing for a brewing pan |
US4019851A (en) * | 1975-09-22 | 1977-04-26 | Combustion Engineering, Inc. | High energy arc ignitor for burner |
US4458480A (en) * | 1980-12-15 | 1984-07-10 | Irwin Everett F | Rotating cylinder external combustion engine |
US20050277074A1 (en) * | 2004-06-10 | 2005-12-15 | Zinn Ben T | Stagnation point reverse flow combustor |
US7425127B2 (en) * | 2004-06-10 | 2008-09-16 | Georgia Tech Research Corporation | Stagnation point reverse flow combustor |
US20080274021A1 (en) * | 2007-05-01 | 2008-11-06 | Jacobus Neels | Compact Fuel Processor |
US8747496B2 (en) * | 2007-05-01 | 2014-06-10 | Westport Power Inc. | Compact fuel processor |
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