US1023422A - Hydrocarbon-burner. - Google Patents

Hydrocarbon-burner. Download PDF

Info

Publication number
US1023422A
US1023422A US49415309A US1909494153A US1023422A US 1023422 A US1023422 A US 1023422A US 49415309 A US49415309 A US 49415309A US 1909494153 A US1909494153 A US 1909494153A US 1023422 A US1023422 A US 1023422A
Authority
US
United States
Prior art keywords
air
fuel
chamber
burner
combustion
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
Application number
US49415309A
Inventor
Robert Lucien D Espujols
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US49415309A priority Critical patent/US1023422A/en
Application granted granted Critical
Publication of US1023422A publication Critical patent/US1023422A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/44Preheating devices; Vaporising devices

Definitions

  • My invention relates to hydro-carbon burners and it has for its object to provide an apparatus adaptedfor the combustion of hydro-carbons ingeneral, oils, residues derived from the distillation of coal, coal-tar, and petroleum and its residues.
  • Figures 1 and 1 show an elevation, partly in section, of an apparatus embodying my invention, Fig. 1 showing the left-hand portion of the apparatus, and Fig. l the right-hand portion.
  • Fig. 2 is a vertical sectional View of a horizontal burner for marine furnaces or the like.
  • ' 3 is an end view of the air-regulating device.
  • Fig. 4 is a front view of a portion of the burner.
  • My invention comprises two essential parts, cooperating together, i. e. the burner, and the devices for feeding said burner.
  • My invention relates particularly to apparatus of the type in which liquid fuel
  • the fuel is rendered fluid in order that it may circulate freely in the apparatus. ⁇ Vith this object it is 'heated but not excessively which presents the further ad vantage, while raising its temperature progressively, of bringing it closer to its point of vaporization. This fluidity is obtained in Specification of Letters Patent.
  • the liquid fuel is conveyed, that is to say conducted, to the discharge orifices, this result being attained by supplying it under an appropriate pressure.
  • the fuel coming from the filter tank (Z (Fig. 1 in communication with suitable reservoirs or magazines (not shown) by means of a pipe (1 is sucked by the pump at which forces it into an apparatus 6 termed the automatic feed compressor.
  • This compressor serves, whatever the running of the pump a. may be, to regulate the predetermined pressure uniform upon any point of the conduit m From this compressor the fuel is sent to the burner through the conduit m passlng through the stop valves 7 and w and distributed through the conduit n to the flow orifices c c (Fig.
  • the valve y serves to regulate the annular flow orifice in proximity to the diffuser b..
  • the fuel is converted into a fine sprayby admitting at the same time a current of compressed air which becomes heatedv in chamber 2', before entering the blast pipe h which surrounds the inlet for the liquid. This heated air mixes with the liquid which leaves the outlet opening with a whirling motion and in the form of a fine spray.
  • the compressed air is obtained by the employment of a compressor, pump or blowing engine at (Fig.
  • the mixture thus gasified is rendered more highly inflammable this result being attained by supplying to it stipulate. sively freshatmospheric air drawn along by the partial vacuum which is proportionate to the delivery.
  • vent'hole is arranged which supplies to the gasified mixture the volume of fresh air which renders it inflammable and ldefinitely insures the combustion.
  • a regu- I later which comprises a rod a held in the with claws e.
  • the diffuser b" is fixed to body of the regulating valve y and formed one end ofa. rod a and may be cone-shaped.
  • S is a spring adjustable in a very sensitive manner by means of the micrometric screw a b, terminating in a hea'd'a, a, and engaging a threaded aperture in a blockw' sliding on the rods'a' andw' and bearing against the spring S.
  • the function of the spring 8 is to produce an equihbrium between the diverse-reactions produced upon the diffusing cone 7;, 'z'. a. the reaction of the opening produced by the arrival of the liquid fuel under pres sure as well as by the arrival of the air in chamber h, and the closingreaction produced by the combustion of the mixture.
  • the difluser When the combustion increases in intensity the inverse takes place, the difluser approaches its seat and less fuel passes .in such a manner that the diffuser is constantly movably axially and acts as an extremely sen sitive regulator no matter for what supply the valve 3 has been regulated.
  • the diffuser b is provided on the part which constitutes it's-seat with a certain number of fine grooves, the depihof which is such that they permit the passage of just the amount of liquid necessary for the starting. In these conditions in order to form the by-pass it is only necessary for the operator to pull toward him by hand the knob of the rod a;
  • the running is rendered automatic, continuous and uniform by means comprising an air compressor n,
  • the fuel supply pump a constant feed compressor e, and these operate continuously.
  • the air compressor 12 forcesthe air through the conduit 7) into the reservoir 0 provided with a safety-valve g and with a stop cock 1 opening into a conduit S which proceeds to the burners and has a pressure regulator t, the object of which is to render the pressure of the air invariable at all the points where it is utilized whatever the 'number of burners may be.
  • the feed pump u forces the liquid fuel coming from the filters d a? into the fuel compressor 6.
  • the compressor of the feeding device 6 receives the liquid fuel under -a piston, the rod of which is extended above and below the body of the cylinder 6,- below, the rod supports a heavy mass 6 formed of counterweights, the force of the inertia ofwhich exercises upon the liquid introduced under the piston of this compressor an invariable pressure whatever the output of the pump is or the consumption of the burners might be; above, the piston rod is connected with another'movable piston in a steam cylinder 6 fed by a pipe branched off from the single conduit and subject to the influence of a stop in common with the pump u and compressor a. This steam exercises upon the piston of cylinder 6 and consequently upon the piston of compressor e, a pressure which is added to that of the counterweights.
  • 0 is the operating lever for rod 3 and carries a pointer 90 playing over a scale 00 to indicate the degree of adjustment of the valve 3
  • X X is a valve controlling the admissionof fuel into the conduit M.
  • A indicates the device to be heated, in this instance a steam generator.
  • a burner comprlsing a combustion chamber, a plurality of concentrically arranged conduits for conducting fuel, compressed air and free atmospheric air to the combustion chamber, means for heatlng the fuel and compressed air during their passage to the combustion chamber, and a controlling device for varying the proportions of fuel and air comprising a difiuser arranged to divide the fuel before reaching the combustion chamber, a rod carried by the difiuser, a spring acting upon said rod, and meansv for varying the stress of the spring.
  • a burner comprising a combustion chamber, a plurality of concentrically arbust-ion chamber, a rod carried by the diffuser, a spring acting upon said rod, and means for varying the stress of the spring comprising a block shdably mounted on the said rod and against which block one end of the spring bears, a second rod on which said block is also slidably mounted, and a micrometric screw engaging a threaded aperture in the said block.

Description

R. L. DESIfUJOLS. HYDROGARBON BURNER.
APPLICATION FILED MAY 5, 1909.
Patented Apr. 16, 1912.
3 SHEETS-SHEET 1.
R. L. DESPUJOLS. HYDROGA RBON BURNER.
APPLICATION FILED MAY 5, 1909- Patented Apr. 16, 1912.
3 SHEETS-SHEET 2 Fig/1 R. L. DESPUJOLS.
HYDROGARBON BURNER.
APPLICATION FILE]? M11115, 1909.
Patented Apr. 16, 1912.
3 SHEETS-SHEET 3.
GIIII ns iPATE -ROBERT LUCIEN DESPUJOLS, 0F ALFORT, FRANCE.
HYDROGARBON-BUIRNER.
Application filed May 5, 1909.
To all whom '1' t may] concern:
Be it known that I, ROBERT LUCTEN nEsruJoLs, a citizen of the Republic of France, and resident of Rue Boulay, Alfort, Seine. l' rance. have invented Improvements in I-Iydrocarbon-Burners, of which the following is a specification.
My invention relates to hydro-carbon burners and it has for its object to provide an apparatus adaptedfor the combustion of hydro-carbons ingeneral, oils, residues derived from the distillation of coal, coal-tar, and petroleum and its residues.
The invention consists in the novel construction, arranger'nent and combination of parts as hereinafter fully described, illustrated in the drawings and pointed out in the appended claims.
In the drawings, Figures 1 and 1 show an elevation, partly in section, of an apparatus embodying my invention, Fig. 1 showing the left-hand portion of the apparatus, and Fig. l the right-hand portion. Fig. 2 is a vertical sectional View of a horizontal burner for marine furnaces or the like. Fig.
' 3 is an end view of the air-regulating device.
Fig. 4 is a front view of a portion of the burner.
My invention comprises two essential parts, cooperating together, i. e. the burner, and the devices for feeding said burner.
My invention relates particularly to apparatus of the type in which liquid fuel,
' compressed air, atmospheric air and addi tional compressed air, are supplied through four concentric passages to the combustion chamber,-and it is so constructed and arranged as to cause the liquid fuel, the atmospheric air, and the primary and secondary supplies of compressed air to be heated during their passage to the combustion chamber, and thus effect the complete gasification of the liquid fuel inside the burner.
The actions to which the liquid fuel is subjected, .the transformations that they produce, and the manner in which they are realized, are explained below in detail and in order.
First. The fuel is rendered fluid in order that it may circulate freely in the apparatus. \Vith this object it is 'heated but not excessively which presents the further ad vantage, while raising its temperature progressively, of bringing it closer to its point of vaporization. This fluidity is obtained in Specification of Letters Patent.
Patented Apr. 16, 1912.
Serial No. 494,153.
two ways. (1) On starting by a supply of steam through'the pipe m to the heater Z through which steam circulatesand which heater communicates the appropriate temperature to the fuel contained in the chamber Z (2) The apparatus being operative and the admission of steam being interrupted the heating takes place automatically by the conductivity of the parts which transmit and preserve in the heater the initial temperature. In order to do this "the dimensions and the position of the heater relatively to the other parts are absolutely fixed. L
Secondly. The liquid fuel is conveyed, that is to say conducted, to the discharge orifices, this result being attained by supplying it under an appropriate pressure. The fuel coming from the filter tank (Z (Fig. 1 in communication with suitable reservoirs or magazines (not shown) by means of a pipe (1 is sucked by the pump at which forces it into an apparatus 6 termed the automatic feed compressor. This compressor serves, whatever the running of the pump a. may be, to regulate the predetermined pressure uniform upon any point of the conduit m From this compressor the fuel is sent to the burner through the conduit m passlng through the stop valves 7 and w and distributed through the conduit n to the flow orifices c c (Fig. 2) through which it reaches the part 7) termed the diffusion cone the form of which is such that it tends to divide the liquid into molecules. The valve y serves to regulate the annular flow orifice in proximity to the diffuser b.. Thirdly. The fuel is converted into a fine sprayby admitting at the same time a current of compressed air which becomes heatedv in chamber 2', before entering the blast pipe h which surrounds the inlet for the liquid. This heated air mixes with the liquid which leaves the outlet opening with a whirling motion and in the form of a fine spray. The compressed air is obtained by the employment of a compressor, pump or blowing engine at (Fig. 1") which delivers through a pipe 37 into a reservoir 0 thence distributes it through a valve 1' to a gas pipe S to which a pressure regulator t isfitted. The air reaches the burner through port S in the chamber 2' (Fig. 2) likewise provided with a steam heating chamber h with conduits k g for admitting the steam, where it l ..,its path encounters the extremity f of the is heated by the steam (or by any other source ofheat) on starting and then automatically by the heat radiated from the flame issuing at q. Thus heated, the air coming from chamber 2', passes through a regulating register provided exteriorly with the letters 0 and F. The letter 0 indicates if the register is open, whilethe letter F indicates if it is closed. On leaving the register through a passage :12 which communicates with the chamber n a portion of the 1 air enters said chamber a while a portion of the air passing through the register passes into chamber From the chamber 7" the air passes to the nozzle h and during part cl; this extremity, forming the body of the diffuser, is constructed in such a manner that the air carries along by suction the molecules of fuel already obtained by the diffusion cone 6 with which molecules .it becomes progressively saturated. The. air being hot the fine spray with which it'is thus saturated assumes its temperature and begins to vaporize.
Fourthly. The fine spray is vaporized. Inorder'todo this a fresh current of air under pressure and heated to a temperature approximating that of the vaporizing point of mazout is caused to reach the fuel thus divided mechanically. ,..The air just mentioned is heated by its passage through chamber i, which latter is heated by steam passing through jacket h, and the heated air after reaching theichamber 11/ passes thence into chamber m, which communicates, as seen in Fig. 2, with chamber n. The conducting of heated air to the fuel 'isnecessary because the first current of hot air having served to transform the fuel into spray and to begin its vaporization has become expanded and consequently lost all its @718 m'ca. Accordall along its ingly it could not alone complete the physical transformation. From the chamber a the hot'air under pressure passing through m surrounds the nozzles h and is, through which the fine spray referred to above is projected, and in flowing oft carries this spray along, completing the vaporization ath as far as 0 where this vaporization ishes under the influence of the temperature which is increasingly high in proportion as the chamber 9 is approached. At the same time the reduction of pressure, resulting from the two con centric drafts, produced by the currents of hot air from 3" and n, carrles along in the mixture a volume of atmospheric air admitted through the orifices Z. At this moment the mixture has become completely vaporous and begins to becomecombustible.
Fifthly. These vapors are then gasified that is to say their temperature is increased much beyond the point of vaporization in order to. obtain a mixture upon which the Upon its path and by the mixture becomes superheated until complete gasification takes place. Independently of the conductivity of the parts the direct radiation of the fiame is felt to a decreasing extent to the rear of the burner. Consequently in the chamber 0 the mixture then attains a high temperature approximating that which it will attain when it has passed through the port p and reached the combustion chamber 9.
Sixthly. The mixture thus gasified is rendered more highly inflammable this result being attained by supplying to it progres. sively freshatmospheric air drawn along by the partial vacuum which is proportionate to the delivery.
At 1 a vent'hole is arranged which supplies to the gasified mixture the volume of fresh air which renders it inflammable and ldefinitely insures the combustion.
At 2. there is an electric ignition plug for starting, but anyother ignition device may be employed, the gas at this point lighting as readily as illuminating gas.
I will now explain the automaticand uniform operation of the arts of the burner and of. its 'auxiliaryapp iances which insure stable equilibrium between the proportions of fuel, artificial air and fresh ambient air.
This result is obtained principallyby a regu- I later which comprises a rod a held in the with claws e. The diffuser b" is fixed to body of the regulating valve y and formed one end ofa. rod a and may be cone-shaped.
S is a spring adjustable in a very sensitive manner by means of the micrometric screw a b, terminating in a hea'd'a, a, and engaging a threaded aperture in a blockw' sliding on the rods'a' andw' and bearing against the spring S.
In operation, the liquid fuel coming under. pressure through conduit m heats up in chamber Z whence it leaves through pipe n in order to pass into chamber 0'. From this chamber the liquidfinds a passage between the conical end of the valve '1 and the bear:
ing 03 of chamber 0'. Through the grooves provided on the rod (1' this fuel passes out and strikes the periphery of the difiusing cone 1), which, by the aid of the diffuser body f helps to effect a molecular division of the jet of liquid fuel, or in other words,
to produce a fine spray. This spray subjected to the action of hot air which, it meets in the blast pipe lb (the hot air coming from '1 is very finely subdivided and becomes a vaporous mixture which combined with the fresh air coming through the channel h from openings Z and besides with the additional air current coming through channel at from chamber n, forms in chamber 0' acombus tible mixture which the contracted portion 7) renders still more intimate. By contact with the igniter 2, this mixture ignites in the combustion chamber 1 which is fed with fresh air through vent In, the same way the current of compressed air coming from chamber j exercises an energetic influence on the diffuser and in the same direction that the liquid passes in under pressure. The combustion of the liquid exercises a reaction on the diffuser but in a direction opposed to the inflow produced by the air current coming from j, that is it tends to return the diffuser to its seat. This counter pressure is proportionate to the intensity of the combustion.
The function of the spring 8 is to produce an equihbrium between the diverse-reactions produced upon the diffusing cone 7;, 'z'. a. the reaction of the opening produced by the arrival of the liquid fuel under pres sure as well as by the arrival of the air in chamber h, and the closingreaction produced by the combustion of the mixture.
This equilibrium is unstable for it changes 'veryquickly by reason of the more or less voluminous quantity of fuel and, consequently, the intensity of combustion; for this reason the sensibility of spring 8 must be very great 'and the regulation must be made with a micrometric screwQ When during the operation the supply of fuel diminishes (or if while it remains the same the liquid supplied varies in density) the intensity of the combustion immediately feels the effectand becomes less. Its reaction upon the diffuser 7). becomes weaker and the latter under the double influence of the pressure of the fuel and of the artificial air suction separates farther from its seat permitting of the passage of a larger quantity of fuel which increases the combustion. When the combustion increases in intensity the inverse takes place, the difluser approaches its seat and less fuel passes .in such a manner that the diffuser is constantly movably axially and acts as an extremely sen sitive regulator no matter for what supply the valve 3 has been regulated.
If a foreign body should enter the discharge orifice partial or total obstruction might result therefrom. In this case it is only necessary to press the knob of a several times; the foreign body seized by the claws e with which the rod 02 is provided is carried from the seat of the diffuser and expelled outside the apparatus by the pressure-0f the fuel and the artificial air suction.
In the case of blockage resulting from the accumulation of particles of sand, gravel or other body the intensity of the combustion diminishes and the diffuser separates from its seat and the foreign bodies are expelled as before.
In orderto be able to effect the starting the diffuser b is provided on the part which constitutes it's-seat with a certain number of fine grooves, the depihof which is such that they permit the passage of just the amount of liquid necessary for the starting. In these conditions in order to form the by-pass it is only necessary for the operator to pull toward him by hand the knob of the rod a;
Instantaneous interrupter.In accordance with the structure of the diffusing cone 7), by pulling the knob a" the apparatus is extinguished while running fully.
In the auxiliary appliances the running is rendered automatic, continuous and uniform by means comprising an air compressor n,
fuel supply pump a, constant feed compressor e, and these operate continuously. The air compressor 12 forcesthe air through the conduit 7) into the reservoir 0 provided with a safety-valve g and with a stop cock 1 opening into a conduit S which proceeds to the burners and has a pressure regulator t, the object of which is to render the pressure of the air invariable at all the points where it is utilized whatever the 'number of burners may be. The feed pump u forces the liquid fuel coming from the filters d a? into the fuel compressor 6.
The compressor of the feeding device 6, receives the liquid fuel under -a piston, the rod of which is extended above and below the body of the cylinder 6,- below, the rod supports a heavy mass 6 formed of counterweights, the force of the inertia ofwhich exercises upon the liquid introduced under the piston of this compressor an invariable pressure whatever the output of the pump is or the consumption of the burners might be; above, the piston rod is connected with another'movable piston in a steam cylinder 6 fed by a pipe branched off from the single conduit and subject to the influence of a stop in common with the pump u and compressor a. This steam exercises upon the piston of cylinder 6 and consequently upon the piston of compressor e, a pressure which is added to that of the counterweights.
0 is the operating lever for rod 3 and carries a pointer 90 playing over a scale 00 to indicate the degree of adjustment of the valve 3 X X is a valve controlling the admissionof fuel into the conduit M.
A indicates the device to be heated, in this instance a steam generator.
What I claim is 1. In an apparatus of the character de: scribed, a burner comprlsing a combustion chamber, a plurality of concentrically arranged conduits for conducting fuel, compressed air and free atmospheric air to the combustion chamber, means for heatlng the fuel and compressed air during their passage to the combustion chamber, and a controlling device for varying the proportions of fuel and air comprising a difiuser arranged to divide the fuel before reaching the combustion chamber, a rod carried by the difiuser, a spring acting upon said rod, and meansv for varying the stress of the spring.
'2. In an apparatus of the character described, a burner comprising a combustion chamber, a plurality of concentrically arbust-ion chamber, a rod carried by the diffuser, a spring acting upon said rod, and means for varying the stress of the spring comprising a block shdably mounted on the said rod and against which block one end of the spring bears, a second rod on which said block is also slidably mounted, and a micrometric screw engaging a threaded aperture in the said block.
In testimony whereof I atfixmy signature in presence of two witnesses.
ROBERT LUCIEN DESPUJOLS.
Witnesses: J DEAN B. MASON, HECTOR MATRAN.
US49415309A 1909-05-05 1909-05-05 Hydrocarbon-burner. Expired - Lifetime US1023422A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US49415309A US1023422A (en) 1909-05-05 1909-05-05 Hydrocarbon-burner.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US49415309A US1023422A (en) 1909-05-05 1909-05-05 Hydrocarbon-burner.

Publications (1)

Publication Number Publication Date
US1023422A true US1023422A (en) 1912-04-16

Family

ID=3091718

Family Applications (1)

Application Number Title Priority Date Filing Date
US49415309A Expired - Lifetime US1023422A (en) 1909-05-05 1909-05-05 Hydrocarbon-burner.

Country Status (1)

Country Link
US (1) US1023422A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2440491A (en) * 1935-03-21 1948-04-27 Des Vehicules Sev Soc Et Oil burner
US2443940A (en) * 1943-04-10 1948-06-22 Stewart Warner Corp Heating system
US2458541A (en) * 1944-11-16 1949-01-11 Comb Processes Company Low velocity oil burner
US2472720A (en) * 1944-12-19 1949-06-07 Nagel Theodore Method of burning oil
US2499207A (en) * 1945-12-22 1950-02-28 John J Wolfersperger Pressure-type burner and method of burning fuel
US2500787A (en) * 1944-12-15 1950-03-14 Orr & Sembower Inc Fluid fuel burner apparatus for effecting diffusion combustion
US2518364A (en) * 1946-10-19 1950-08-08 Surface Combustion Corp Direct fired air heater
US2530019A (en) * 1944-11-11 1950-11-14 Elliott Co Combustion chamber with side air entrance and hollow ignition cone
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
US2735481A (en) * 1956-02-21 Reichhelm
US3005288A (en) * 1959-01-26 1961-10-24 Co2 Land Healers Inc Method and apparatus for treating soils by adding carbonic acid
US3033545A (en) * 1959-10-01 1962-05-08 Azbe Corp Firing apparatus for kilns

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735481A (en) * 1956-02-21 Reichhelm
US2440491A (en) * 1935-03-21 1948-04-27 Des Vehicules Sev Soc Et Oil burner
US2443940A (en) * 1943-04-10 1948-06-22 Stewart Warner Corp Heating system
US2530019A (en) * 1944-11-11 1950-11-14 Elliott Co Combustion chamber with side air entrance and hollow ignition cone
US2458541A (en) * 1944-11-16 1949-01-11 Comb Processes Company Low velocity oil burner
US2500787A (en) * 1944-12-15 1950-03-14 Orr & Sembower Inc Fluid fuel burner apparatus for effecting diffusion combustion
US2472720A (en) * 1944-12-19 1949-06-07 Nagel Theodore Method of burning oil
US2499207A (en) * 1945-12-22 1950-02-28 John J Wolfersperger Pressure-type burner and method of burning fuel
US2518364A (en) * 1946-10-19 1950-08-08 Surface Combustion Corp Direct fired air heater
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
US3005288A (en) * 1959-01-26 1961-10-24 Co2 Land Healers Inc Method and apparatus for treating soils by adding carbonic acid
US3033545A (en) * 1959-10-01 1962-05-08 Azbe Corp Firing apparatus for kilns

Similar Documents

Publication Publication Date Title
US1023422A (en) Hydrocarbon-burner.
US1923614A (en) Burner control system
US2688360A (en) Fuel combustion system, including gas assisted atomizer
US1956506A (en) Oil burner
US1832280A (en) Process for burning oil
US662319A (en) Apparatus for burning liquid fuel.
US227695A (en) Vapor-burner
US1747613A (en) Gas-generator oil heater
US471671A (en) Process of and apparatus for making gas
US437013A (en) Hydrocarbon-oil burner
US1006442A (en) Incandescent gas-burner.
US1618565A (en) Oil burner
US1356239A (en) Gaseous-fuel generator
US238695A (en) John l
US740959A (en) Oil-burner.
US1566417A (en) Oil burner
US471673A (en) Boiler-furnace
US1246305A (en) Kerosene-carbureter.
US1560367A (en) Production of radiant heat
US1134240A (en) Hydrocarbon-burner.
USRE4910E (en) Improvement in apparatus for generating and burning vapors from hydrocarbons
US518694A (en) Walter m
US796949A (en) Oil-heater.
US413762A (en) Retort-vaporizer
US2611425A (en) Self-gasifying heating equipment