US1273466A - Fuel-burner. - Google Patents
Fuel-burner. Download PDFInfo
- Publication number
- US1273466A US1273466A US16515217A US16515217A US1273466A US 1273466 A US1273466 A US 1273466A US 16515217 A US16515217 A US 16515217A US 16515217 A US16515217 A US 16515217A US 1273466 A US1273466 A US 1273466A
- Authority
- US
- United States
- Prior art keywords
- fuel
- burner
- air
- tube
- spray
- 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
- 239000000446 fuel Substances 0.000 description 47
- 238000002485 combustion reaction Methods 0.000 description 18
- 239000007921 spray Substances 0.000 description 17
- 239000000203 mixture Substances 0.000 description 14
- 239000007789 gas Substances 0.000 description 13
- 239000007788 liquid Substances 0.000 description 10
- 239000004215 Carbon black (E152) Substances 0.000 description 8
- 229930195733 hydrocarbon Natural products 0.000 description 8
- 150000002430 hydrocarbons Chemical class 0.000 description 8
- 239000010779 crude oil Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 239000004020 conductor Substances 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011369 resultant mixture Substances 0.000 description 1
Images
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
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
- F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
Definitions
- the invention relates to fuel burners and particularly to liquid or gaseous fuel burners.
- Another object of the invention is to provide a method of burning heavy liquid fuels whereby gases of, combustion of high velocity are'produced.
- Another object of the invention is to provide a fuel burner in which the kinetic energy of the burning fuel induces sufficient air into the burner to complete combustion of the heavy fuel.
- Figure 1 is a longitudinal section of one form of burner of my invention shown somewhat diagrammatically and associated fuel and air containers and conductors.
- Fig. 2 is a similar view of a slightly modified form of burner.
- Fig. 3 is a similar view of another modified formof burner.
- the burner of my invention may be employed for the production of power in engines and turbines and for heating and for other useful purposes and it is to be understood that I do not limit myself to any particular use of the burner.
- I produce initial ignition of a mixture of fuel and insufiicicnt air to produce complete combustion and cause the velocity or kinetic energy of the flame so produced to induce suflicient air into the burner to complete combustion.
- I cmploy the heat of combustion to volatilize or break up heavy hydrocarbon fuel'such as crude oil and the expansion of this crude oil vapor or gas further increases the velocity of the gases resulting in the induction of suflicient air to produce complete combustion of all of the fuel.
- the high velocity gases can be effectively utilized in steam generators and other heating devices which cannot readily be provided with stacks or other draft producing means and can be utilized to produce power by being directly introduced to the blades of a turbine, constructed on the general principle of steam turbines.
- the burner comprises a cup or shell 2, preferably elongated in form, in the end of which is arranged the combined air and fuel nozzle 3.
- the nozzle is so constructed and arranged that the fuel spray produced thereby is directed toward the open end of the shell 2.
- a spark plug 14 or other ignition device for igniting the spray.
- the air in the spray mixture is preferably only that which it has been necessary to employ to spray the fuel and is insufficient to complete combustion, but is sufficient to allow the mixture to become ignited.
- the burning of the mixture greatly increases its volume, so that the burning mixture is expelled from the shell at high velocity.
- the Venturi tube flares out into the steam generator or other apparatus.
- the venturi When used in connection with a heat-absorbing medium containing apparatus, the venturi is short, so that the mixture is burned within the apparatus, but when used in connection with .a turbine, the flaring mouthed tube is preferably of such length that combustion'is complete before the gases contact with the turbine blades.
- the expansion of the gases in the flaring, mouth inthe pressure on the fuel is preferably produced by a pump 19, connected to the engin'e, but when the burner is employed for other uses, the pressure may be produced in any desirable manner.
- Means are provided for varying the flow of air and fuel to the nozzle and the flow of the heavy fuel to the burner in accordance with variations in conditions in the apparatus to which the burner is applied.
- the control means When applied to a steam generating apparatus, the control means are arranged to vary the flow of air and fuelslin accordance with variations in temperature and pressure within the steam generatingunit.
- valves 21, 22 and 23 Arranged in the pipes 12, 6 and 17 respectively are valves 21, 22 and 23 which are connected to a thermostatic control device 24 which is operated by variations in temperature in the steam generating unit, so that the amount of air and fuels fed'to the burner varies inversely with the steam temperature.
- the pipes 12, 6 and 17 are also provided respectively with valves 25, 26 and 27 which are connected to a pressure operated device 28 connected to the steam generator, so that the flow through the pipes is varied inversely as the pressure.
- Fig. 3 I have shown a modification in which the air under pressure is eliminated and the fuel spray produced by the pressure (9f the fuel.
- the light fuel spray nozzle 31, to which the fuel is fedunder pressure, is arranged in the Venturi tube 32, which is supported within the Venturi tube 15.
- the nozzle discharge end is arranged at the narrow portion of the'venturi 32 and is con; structed to discharge a spray of fuel in the direction of the length of the venturi 32.
- the spray and the partial combustion of the fuel in the venturi32 induce suflicient air to support such combustion and the tube 32 is heated.
- the heavy fuel is introduced onto. the surface of the hot tube 32 where it is broken up, its products increasing the volume of the gases and increasing. the kinetie energy of the gas.
- the kinetic energy of the gases or of the burning mixture induces a sufficient supply of air through the venturi 15 to complete combustion.
- a liquid fuel burner comprising means for projecting a spray of light liquid fuel, means for igniting the spray, means forintroducing heavy hydrocarbon fuel into thermal communication with the resultant flame whereby the heavy fuel isvaporized and mixed with the ignited spray, and
- a fuel burner comprising a chamber having an open end, means for projecting a spray of fuel and air in the chamber toward the open end thereof, means for igniting the mixture within the chamber, a conduit for flowing heavy hydrocarbon onto the hot surface of said chamber and a tube surrounding the discharge end of the chamber and spaced therefrom.
- a fuel burner comprising a tube, an
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
W. A. DOBLE.
FUEL BURNER.
APPLICATION FILED APR-28. I91].
1 ,273,466. Patented July 23, 1918 /Z L m INVENTOI? W. /i. DOBLIE H A TTOR/VEYS s PATEN s i WILLIAM A. DOBLE, OF SAN FRANCISCO, CALIFORNIA, ASSIGNOR T0 DOBLE LABORA- TORIES, OF SAN FRANCISCO, CALIFORNIA, A CORPORATION OF CALIFORNIA.
FUEL-BURNER.
Specification of Letters Patent.
Patented July 23, 1918.
Application filed April 28, 1917. Serial No. 165,152.
To all whom it may concern:
Be it known that I, WILLIAM A. DoBLn,-a citizen of the United States, and a resident of the city and county of San Francisco,
State of California, have invented a certain new and useful Fuel-Burner, of which the following is a specification.
The invention relates to fuel burners and particularly to liquid or gaseous fuel burners.
An object of the invention is to provide a method of burning very heavy liquid fuels.
Another object of the invention is to provide a method of burning heavy liquid fuels whereby gases of, combustion of high velocity are'produced.
Another object of the invention is to provide a fuel burner in which the kinetic energy of the burning fuel induces sufficient air into the burner to complete combustion of the heavy fuel.
The invention possesses other advanta geous features, some of which, with the foregoing, will be set forth at length in the following description where I shall outline in full that form of the invention which I have selected for illustration in the drawings accompanying and forming part of the present specification. In said drawings I have shown one specific embodiment of my generic invention and several modifications thereof, but it is to be understood that I do not limit myself to such forms, since the invention as expressed in the claims may be embodied in a plurality of forms.
Referring to the drawings:
Figure 1 is a longitudinal section of one form of burner of my invention shown somewhat diagrammatically and associated fuel and air containers and conductors.
Fig. 2 is a similar view of a slightly modified form of burner.
Fig. 3 is a similar view of another modified formof burner.
The burner of my invention may be employed for the production of power in engines and turbines and for heating and for other useful purposes and it is to be understood that I do not limit myself to any particular use of the burner. In the burner of my invention I produce initial ignition of a mixture of fuel and insufiicicnt air to produce complete combustion and cause the velocity or kinetic energy of the flame so produced to induce suflicient air into the burner to complete combustion. I also cmploy the heat of combustion to volatilize or break up heavy hydrocarbon fuel'such as crude oil and the expansion of this crude oil vapor or gas further increases the velocity of the gases resulting in the induction of suflicient air to produce complete combustion of all of the fuel. The high velocity gases can be effectively utilized in steam generators and other heating devices which cannot readily be provided with stacks or other draft producing means and can be utilized to produce power by being directly introduced to the blades of a turbine, constructed on the general principle of steam turbines.
The burner comprises a cup or shell 2, preferably elongated in form, in the end of which is arranged the combined air and fuel nozzle 3.- Fuel under pressure and preferably liquid fuel, such as kerosene or distillate, from a suitable source, such as the tank 4, is introduced into the nozzle 3, through the pipe 6, which is provided with a manually operated valve 7. Air under pressure, from a suitable source, such as the tank 8, is introduced into the nozzle through the pipe 12 which is provided with a manually operated valve 13. The nozzle is so constructed and arranged that the fuel spray produced thereby is directed toward the open end of the shell 2. Arranged in the shell, in front of the nozzle is a spark plug 14 or other ignition device for igniting the spray. The air in the spray mixture is preferably only that which it has been necessary to employ to spray the fuel and is insufficient to complete combustion, but is sufficient to allow the mixture to become ignited. The burning of the mixture greatly increases its volume, so that the burning mixture is expelled from the shell at high velocity.
The combustion of the mixture heats the shell to a high temperature and I have found that heavy oils, such as crude oil, may be advantageously used and completely burned,
by flowing the oil into the hot shell where be flowed onto the outer-surface, as shown 4 in Fig. 2. When flowed onto the inner surface, the reat increase in volume of the oil due to its volatilization' and gasificatlon,
' --greatly increases the velocity or kinetic enshell 2. The kinetic energy of the high velocity gases discharging from the shell into the Venturi tube causes air to be drawn into the tube and past the end of the shell and to mix with the burning mixture, thereby producing complete combustion and greatly increasing the velocity of the gases. For a given sized opening between the shell and the venturi, the amount of air drawn will Vary with the amount of fuel discharged and the opening is preferably made-of such size that the amount of air drawn in is that which is required for complete combustion of the fuel, although for turbine use, a greater amount of air may be introduced. From the end of the shell, the Venturi tube flares out into the steam generator or other apparatus. When used in connection with a heat-absorbing medium containing apparatus, the venturi is short, so that the mixture is burned within the apparatus, but when used in connection with .a turbine, the flaring mouthed tube is preferably of such length that combustion'is complete before the gases contact with the turbine blades. The expansion of the gases in the flaring, mouth inthe pressure on the fuel is preferably produced by a pump 19, connected to the engin'e, but when the burner is employed for other uses, the pressure may be produced in any desirable manner.
In Fig. 2, the pipe 17 discharges the heavy fuel onto the outer surface of the shell 2,
C where'it is broken up and its products are drawn into the burner with the air, and the combustion of its products greatly increases the velocity of the gases in the 'Vent-uri tube which results in inducing suffieient air to complete combustion.
Means are provided for varying the flow of air and fuel to the nozzle and the flow of the heavy fuel to the burner in accordance with variations in conditions in the apparatus to which the burner is applied. When applied to a steam generating apparatus, the control means are arranged to vary the flow of air and fuelslin accordance with variations in temperature and pressure within the steam generatingunit. Arranged in the pipes 12, 6 and 17 respectively are valves 21, 22 and 23 which are connected to a thermostatic control device 24 which is operated by variations in temperature in the steam generating unit, so that the amount of air and fuels fed'to the burner varies inversely with the steam temperature. The pipes 12, 6 and 17 are also provided respectively with valves 25, 26 and 27 which are connected to a pressure operated device 28 connected to the steam generator, so that the flow through the pipes is varied inversely as the pressure.
In Fig. 3 I have shown a modification in which the air under pressure is eliminated and the fuel spray produced by the pressure (9f the fuel. The light fuel spray nozzle 31, to which the fuel is fedunder pressure, is arranged in the Venturi tube 32, which is supported within the Venturi tube 15. The nozzle discharge end is arranged at the narrow portion of the'venturi 32 and is con; structed to discharge a spray of fuel in the direction of the length of the venturi 32.
The spray and the partial combustion of the fuel in the venturi32 induce suflicient air to support such combustion and the tube 32 is heated. The heavy fuel is introduced onto. the surface of the hot tube 32 where it is broken up, its products increasing the volume of the gases and increasing. the kinetie energy of the gas. The kinetic energy of the gases or of the burning mixture induces a suficient supply of air through the venturi 15 to complete combustion.
1 claim: I
1. The method of burning liquid fuelwhich consists in producing. a continuous spray of light liquid fuel and-air, igniting said spray to produce a high velocity flame, employing heat from said flame tovolatilize a heavy hydrocarbon, the products of which mix with said flame and increase the velocity of the flame, and causing the kinetic energy of themixture to induce suflicient air into the flame to complete combustion and further increase the velocity-of the gases of combustion. Y
2. A liquid fuel burner comprising means for projecting a spray of light liquid fuel, means for igniting the spray, means forintroducing heavy hydrocarbon fuel into thermal communication with the resultant flame whereby the heavy fuel isvaporized and mixed with the ignited spray, and
means for causing the resultant mixture to means for introducing heavy hydrocarbon fuel into the tube in thermal contact with the flame and means for adding air to the mixture thus produced.
4. A fuel burner comprising a chamber having an open end, means for projecting a spray of fuel and air in the chamber toward the open end thereof, means for igniting the mixture within the chamber, a conduit for flowing heavy hydrocarbon onto the hot surface of said chamber and a tube surrounding the discharge end of the chamber and spaced therefrom.
5. A fuel burner comprising atube, means in the tube for producing an ignited combustible mixture projected in the direction of the axis of the tube and means for introducing heavy liquid hydrocarbon fuel into the tube in thermal contact with the ignited mixture,
6. A fuel burner comprising a tube, an
air and fuel nozzle arranged within the tube, conduits for supplying fuel and air under pressure to said nozzle, means in the tube for igniting the resultant spray, and a conduit for introducing heavy liquid hydrocarbon into the tube and in thermal contact with the ignited spray.
7. A fuel burner comprising a chamber having an open end, an air and fuel nozzle arranged in said chamber, conduits for conducting fuel and air under pressure to said nozzle, means in the chamber for igniting the spray produced by the nozzle, a conduit for flowing heavy hydrocarbon fuel onto the surface of said chamber and an open ended tube surrounding and spaced from said chamber.
In testimony whereof I have my hand at San Francisco, California, this 23d day of April, 1917.
WILLIAM A. DOBLE.
hereunto set
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16515217A US1273466A (en) | 1917-04-28 | 1917-04-28 | Fuel-burner. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16515217A US1273466A (en) | 1917-04-28 | 1917-04-28 | Fuel-burner. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1273466A true US1273466A (en) | 1918-07-23 |
Family
ID=3341082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US16515217A Expired - Lifetime US1273466A (en) | 1917-04-28 | 1917-04-28 | Fuel-burner. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1273466A (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2460451A (en) * | 1946-06-13 | 1949-02-01 | Farhall Inc | Gasifying fuel burner |
| US2482394A (en) * | 1945-02-12 | 1949-09-20 | Edwin T Wyman | Gas turbine |
| US2579614A (en) * | 1944-06-23 | 1951-12-25 | Allis Chalmers Mfg Co | Combustion chamber with rotating fuel and air stream surrounding a flame core |
| US2635425A (en) * | 1949-09-07 | 1953-04-21 | Westinghouse Electric Corp | Dual flow fuel nozzle system having means to inject air in response to low fuel pressure |
| US2658340A (en) * | 1945-02-01 | 1953-11-10 | Power Jets Res & Dev Ltd | Apparatus for igniting fuel in fast-moving hot gas streams |
| US2692480A (en) * | 1948-05-07 | 1954-10-26 | Onera (Off Nat Aerospatiale) | Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines |
| US2715436A (en) * | 1951-08-09 | 1955-08-16 | Swingfire Bahamas Ltd | Resonant pulse jet combustion heating device |
| US2780916A (en) * | 1952-08-22 | 1957-02-12 | Continental Aviat & Engineerin | Pilot burner for jet engines |
| US2828605A (en) * | 1951-03-19 | 1958-04-01 | Power Jets Res & Dev Ltd | Method of generating combustion gases by burning a gaseous combustible mixture |
| US2854819A (en) * | 1946-01-23 | 1958-10-07 | Power Jets Res & Dev Ltd | Apparatus for igniting fuel in a fastmoving hot gas stream by means of a spontaneously ignitable pilot fuel |
| US2894368A (en) * | 1946-02-06 | 1959-07-14 | Philips Corp | Hot-gas engine comprising more than one device for the supply of heat |
| DE973514C (en) * | 1943-02-26 | 1960-03-17 | Alfred Dipl-Ing Kaercher | Device for generating fog u. like |
| US2952122A (en) * | 1955-04-29 | 1960-09-13 | Phillips Petroleum Co | Fuel system for ducted rocket ramjet power plants |
| US2958192A (en) * | 1958-09-19 | 1960-11-01 | Donald E Dresselhaus | Turbine jet engine |
| US2987875A (en) * | 1955-05-26 | 1961-06-13 | Phillips Petroleum Co | Ramjet power plants for missiles |
| US3025669A (en) * | 1957-07-31 | 1962-03-20 | Fischoff Etienne | Methods of and devices for stabilizing turbine rating, notably in power missiles |
| US3236280A (en) * | 1962-01-23 | 1966-02-22 | United States Steel Corp | Method and apparatus for burning two incompatible liquid hydrocarbon fuels |
| US4170110A (en) * | 1976-07-19 | 1979-10-09 | Edward Radin | Combustion process |
| US5282359A (en) * | 1991-10-17 | 1994-02-01 | Chester Robert G | Impulse jet engine |
-
1917
- 1917-04-28 US US16515217A patent/US1273466A/en not_active Expired - Lifetime
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE973514C (en) * | 1943-02-26 | 1960-03-17 | Alfred Dipl-Ing Kaercher | Device for generating fog u. like |
| US2579614A (en) * | 1944-06-23 | 1951-12-25 | Allis Chalmers Mfg Co | Combustion chamber with rotating fuel and air stream surrounding a flame core |
| US2658340A (en) * | 1945-02-01 | 1953-11-10 | Power Jets Res & Dev Ltd | Apparatus for igniting fuel in fast-moving hot gas streams |
| US2482394A (en) * | 1945-02-12 | 1949-09-20 | Edwin T Wyman | Gas turbine |
| US2854819A (en) * | 1946-01-23 | 1958-10-07 | Power Jets Res & Dev Ltd | Apparatus for igniting fuel in a fastmoving hot gas stream by means of a spontaneously ignitable pilot fuel |
| US2894368A (en) * | 1946-02-06 | 1959-07-14 | Philips Corp | Hot-gas engine comprising more than one device for the supply of heat |
| US2460451A (en) * | 1946-06-13 | 1949-02-01 | Farhall Inc | Gasifying fuel burner |
| US2692480A (en) * | 1948-05-07 | 1954-10-26 | Onera (Off Nat Aerospatiale) | Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines |
| US2635425A (en) * | 1949-09-07 | 1953-04-21 | Westinghouse Electric Corp | Dual flow fuel nozzle system having means to inject air in response to low fuel pressure |
| US2828605A (en) * | 1951-03-19 | 1958-04-01 | Power Jets Res & Dev Ltd | Method of generating combustion gases by burning a gaseous combustible mixture |
| US2715436A (en) * | 1951-08-09 | 1955-08-16 | Swingfire Bahamas Ltd | Resonant pulse jet combustion heating device |
| US2780916A (en) * | 1952-08-22 | 1957-02-12 | Continental Aviat & Engineerin | Pilot burner for jet engines |
| US2952122A (en) * | 1955-04-29 | 1960-09-13 | Phillips Petroleum Co | Fuel system for ducted rocket ramjet power plants |
| US2987875A (en) * | 1955-05-26 | 1961-06-13 | Phillips Petroleum Co | Ramjet power plants for missiles |
| US3025669A (en) * | 1957-07-31 | 1962-03-20 | Fischoff Etienne | Methods of and devices for stabilizing turbine rating, notably in power missiles |
| US2958192A (en) * | 1958-09-19 | 1960-11-01 | Donald E Dresselhaus | Turbine jet engine |
| US3236280A (en) * | 1962-01-23 | 1966-02-22 | United States Steel Corp | Method and apparatus for burning two incompatible liquid hydrocarbon fuels |
| US4170110A (en) * | 1976-07-19 | 1979-10-09 | Edward Radin | Combustion process |
| US5282359A (en) * | 1991-10-17 | 1994-02-01 | Chester Robert G | Impulse jet engine |
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