US2053003A - Combustion apparatus - Google Patents

Combustion apparatus Download PDF

Info

Publication number
US2053003A
US2053003A US614076A US61407632A US2053003A US 2053003 A US2053003 A US 2053003A US 614076 A US614076 A US 614076A US 61407632 A US61407632 A US 61407632A US 2053003 A US2053003 A US 2053003A
Authority
US
United States
Prior art keywords
tube
combustion
chamber
air
combustion chamber
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
US614076A
Inventor
George R Koeln
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.)
Electrol Inc
Original Assignee
Electrol Inc
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 Electrol Inc filed Critical Electrol Inc
Priority to US614076A priority Critical patent/US2053003A/en
Application granted granted Critical
Publication of US2053003A publication Critical patent/US2053003A/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
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00Subject-matter not provided for in other groups of this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02Combustion apparatus using liquid fuel
    • F23C2700/023Combustion apparatus using liquid fuel without pre-vaporising means

Definitions

  • An object of the invention is to provide a combustion apparatus in which oil is mixed with a primary and secondary supply of air and drawn through the combustion chamber in a manner to increase the emciency of the apparatus, so that a greatly increased quantity of fuel may be burned within a reduced space, thereby minimizing the overall dimensions of the apparatus.
  • Another object of the invention is to provide an apparatus of the class mentioned in which fuel in the form of oil is injected into a combustion chamber with a supply of primary and secondary air to initiate and complete combustion and then the products of combustion withdrawn from the combustion chamber through a tortuous passage, increasing the heat transfer surface commensurate with the amount of oil injected into the combustion chamber.
  • Another object of the invention is to provide an oil burner associated with a combustion chamber and means for causing travel of currents through said chamber, with provision for supplying secondary air for combustion insuch a manner as to promote substantially complete combustion within the combustion chamber, together with means foi* withdrawing the products of combustion through conduits leading from ,the
  • Fig. 1 is a longitudinal section through the apparatus.
  • Fig. 2 is an end elevation taken substantially on the line 2-2 of Fig. 1.
  • Fig. 3 is a vertical section taken on the line 3 3 of Fig. 1.
  • Fig. 4 is a vertical section taken on the line 4-4 of Fig. 1.
  • the apparatus is shown as including a support I upon which is mounted an outer shell 2 having a front plate 3 and a back plate 4.
  • the outer shell 2 ⁇ is equipped with the usual risers 5 and drain openings 6, it being understood that the return conduits may be connected into the outer shell at any suitable point, preferably on the side thereof.
  • an innerv shell 'I arranged eccentrically with respect to the shell 2 to provide an enlarged steam space (Cl. 15S-1.5)
  • the combustion chamber 9 is concentrically mounted within the shell 1 and abuts against the head plate 3 at its forward end, but the upper segment of the combustion chamber shell 9 terminates short of the back plate forming a vertically extending combustion chamber I0.
  • the combustion chamber shell 9 is provided with a refractory lining iI and, at its forward end, with a refractory heat block I2 having an opening I3 in the form of a truncated cone with flaring inner l5 walls, as clearly illustrated in Fig. 1.
  • the products of combustion from the combustion chamber are withdrawn through a series of spaced fire tubes I4 occupying the upper segmental space between the shells 1 and 9 and extendlng from a header I5 to the inner wall of the chamber I0.
  • the header I5 is spaced inwardly from the head plate 3 forming an annular chamber that communicates with a second series of fire tubes I6, so that the products of combustion exiting from the tubes I4 pass downwardly through the chamber at its forward end and return through the tubes I6, which open at their f rear ends into a chamber formed by a fitting I'I.
  • a suction lblower I is connected with the tting I1 and discharges into a stack connection I9.
  • the suction blower I8 is driven by a motor M conveniently mounted below the shell 2 on a support 20" ⁇ c"arrled by the lower frame of the apparatus.
  • the motor M in addition to operating the suction blower, also may be operatively connected with a fuel pump 2
  • the returned water or condensate as Well as the raw water supply, is introduced into the space between the shells 2 andv 1 and rises within the shell 'I to a point approximately at the top of the shell and over the tubes I4.
  • Both the tubes I4 and I6 are, therefore, in heat exchange relationship with the water circulating in the boiler and, since the hottest part of the body of water will be at the top of the shell 1, the water vapor will discharge from the shell 'I through the pipes 22 into the vapor space at the top of the shell 2, from which it may be conducted for use through the risers 5.
  • the form of boiler described provides an efcient embodiment for the combustion apparatus because the fuel fed to the combustion chamber is rapidly burned at a high temperature, substantially complete combustion taking place in the combustion chamber, the full heat transfer eiect being conserved by passing the products of combustion endwise in both directions of the boiler by the suction device communicating with the return re tubes.
  • the form of boiler disclosed also prevents the accumulation of a rich combustible mixture in the combustion chamber in the event of failure of ignition o-f the burner.
  • the form of boiler described is the most etlicient construction for the embodiment of the novel burra; apparatus, although other forms of boilers may be employed with suction draft connections by which a part at least of the eiv ciency of the invention may be attained.
  • the director ring has inwardly inclined walls and fits into the outer end of the opening I3.
  • a series of curved plates 28 are mounted in and extend across the space between the plates 25 and 26 and form a series of outwardly aring curved chambers (Fig. 3). The outer ends of these chambers open to atmosphere through the space between a band 29 and the peripheral edges 'of the plates 25 and 26. The inner ends of the plates 28 are spaced apart, forming a series of restricted openings arranged annularly that communicate with the outer end of the tube 23.
  • a band 29 is mounted around the peripheries of the plates 25 and 26 and has its ends connected by a thumb bolt 3U.
  • 'I'he band 29 is loose upon the plates 25 and 26, leaving a narrow space between said band and the peripheries of said plates for the passage of air into the chambers formed between said plates 25 and 26 by the plates 28.
  • the thumb bolt 30 may be tightened or loosened in order to reduce or enlarge the space between the band 29 and the edges of the plates 25 and 26 and thereby regulate the amount of air that may pass therethrough.
  • the size of the space between the band 29 and the peripheral edges of the plates 25 and 26 is small, such space shown in Figs. 2 and 3 being somewhat exaggerated.
  • a second tube 3l constituting the primary air supply.
  • the tube 3l is open at itsouter end and in the opening a spider 32 is tted.
  • the primary air supply enters between the arms of the spider 32 and is delivered through the inwardly tapered end 33 of the tube 3 l
  • the oil nozzle 3d extends axially through the tube 3l and terminates inwardly a slight distance from the inner edge of the tube 3l.
  • the suction on the combustion chamber vdraws air into the primary air supply tube 3l, which mixes with the oil ejected from the nozzle 3d, forming a combustible mixture aosaoos that is ignited by the ignition devices 35.
  • the secondary air supply is drawn down through the chambers formed by the plates 28 and is given an initial rotary movement.
  • the rotary movement thus imparted to the incoming air currents causes 'a circular movement of the air currents as they pass through the space between the tube 23 and the tube 3
  • the entire burning mixture of atomized oil and air is rapidly drawn through the combustion chamber' with a circular movement, so that the burning volume of oil and air maintains a circular and longitudinal movement against the refractory walls of the combustion chamber.
  • a combustion apparatus comprising a primary air tube terminating adjacent said inlet opening and having unobstructed communication therewith, a fuel nozzle discharging into said inlet opening, a secondary air tube surrounding said first named tube and connected at one end with the inlet to the combustion chamber and forming a tubular chamber that discharges air only into said inlet opening, an air inlet chamber having a substantially enlarged chamber with respect to said secondary air tube and connected with the outer end of said 4secondary air tube and extending normal to the axis of said secondary air tube, and curved vanes in said air inlet chamber for imparting a spiral movement to the air currents A in said air inlet chamber and in said secondary air tube.
  • a combustion apparatus comprising a primary air tube discharging into the inlet opening of the combustion chamber, a fuel nozzle extending axially through said primary air tube, ligniting means mounted adjacent said nozzle, a secondary air tube surrounding and spaced from said rst named tube and connecting with the wall of said inlet opening of the combustion chamber, a casing connected with and opening into the outer end of said secondary air tube having a greater diameter than said secondary air tube and being open at its periphery, and walls in said casing forming i inwardly converging chambers which tdischarge tangentially into said secondary air ube.
  • a combustion apparatus having a com-"- bustion chamber with an inlet opening
  • said second tube having an air inlet and an air outlet discharging into ythe inlet opening of the combustion chamber, spaced plates connected to said second tube adjacent .the air inlet thereof, a loose fitting closure about the periphery of said plates permitting the passage of air therebetween, said plates and said closure defining a second chamber opening into said outlet of said tube, transverse plates between said spaced plates converging inwardly to form compartments in said second chamber and said compartments having outlets discharging tangentlally to the inlet of said second tube,
  • an air chamber including spaced walls having a peripheral opening therebetween.
  • band means substantially and variably covering said opening, and means for contracting said band relatively tightly against said walls and for relieving it from 20 saidcontraction to tl't only loosely about said walls whereby to vary the size of the opening.

Description

sept. 1, 1936. 'Q R; KOELN A 2,053,003 COMBUSTION APPARATUS Filed May 28, 1932 2 Sheets-Sheet l Az 1J Y l@ l j y Sept. E936. G. R. Kol-:LN
COMBUSTION APPARATUS Filed may 28, 1932/ 2 Sheets-Sheet 2 Patented Sept. l, 1936 UNITED STATES PATENT oFFica COMBUSTION APPARATUS Delaware Application May as, 1932, serial No. 614,016
5 Claims.
'Ihis invention relates to improvements in combustion apparatus; and consists in the novel construction hereinafter disclosed.
An object of the invention is to provide a combustion apparatus in which oil is mixed with a primary and secondary supply of air and drawn through the combustion chamber in a manner to increase the emciency of the apparatus, so that a greatly increased quantity of fuel may be burned within a reduced space, thereby minimizing the overall dimensions of the apparatus.
Another object of the invention is to provide an apparatus of the class mentioned in which fuel in the form of oil is injected into a combustion chamber with a supply of primary and secondary air to initiate and complete combustion and then the products of combustion withdrawn from the combustion chamber through a tortuous passage, increasing the heat transfer surface commensurate with the amount of oil injected into the combustion chamber.
Another object of the invention is to provide an oil burner associated with a combustion chamber and means for causing travel of currents through said chamber, with provision for supplying secondary air for combustion insuch a manner as to promote substantially complete combustion within the combustion chamber, together with means foi* withdrawing the products of combustion through conduits leading from ,the
combustion chamber, said conduits being in heatfil exchange relation with the medium to be heated.
Additional advantages of the construction will be apparent from the following detail description thereof taken in connection with the accompanying drawings, in which- Fig. 1 is a longitudinal section through the apparatus. I
Fig. 2 is an end elevation taken substantially on the line 2-2 of Fig. 1.
Fig. 3 is a vertical section taken on the line 3 3 of Fig. 1.
Fig. 4 is a vertical section taken on the line 4-4 of Fig. 1.
In the embodiment of the invention as illustrated in the drawings, the apparatus is shown as including a support I upon which is mounted an outer shell 2 having a front plate 3 and a back plate 4. The outer shell 2`is equipped with the usual risers 5 and drain openings 6, it being understood that the return conduits may be connected into the outer shell at any suitable point, preferably on the side thereof. Within the shell 2 is an innerv shell 'I arranged eccentrically with respect to the shell 2 to provide an enlarged steam space (Cl. 15S-1.5)
at the top of the boiler and a preheating feed water jacket around the shell 1. Water from the space between the outer shell 2 and the inner shell is fed through openings 8 into the inner shell.
The combustion chamber 9 is concentrically mounted within the shell 1 and abuts against the head plate 3 at its forward end, but the upper segment of the combustion chamber shell 9 terminates short of the back plate forming a vertically extending combustion chamber I0. The combustion chamber shell 9 is provided with a refractory lining iI and, at its forward end, with a refractory heat block I2 having an opening I3 in the form of a truncated cone with flaring inner l5 walls, as clearly illustrated in Fig. 1.
The products of combustion from the combustion chamber are withdrawn through a series of spaced fire tubes I4 occupying the upper segmental space between the shells 1 and 9 and extendlng from a header I5 to the inner wall of the chamber I0. The header I5 is spaced inwardly from the head plate 3 forming an annular chamber that communicates with a second series of lire tubes I6, so that the products of combustion exiting from the tubes I4 pass downwardly through the chamber at its forward end and return through the tubes I6, which open at their f rear ends into a chamber formed by a fitting I'I.
A suction lblower I is connected with the tting I1 and discharges into a stack connection I9. The suction blower I8 is driven by a motor M conveniently mounted below the shell 2 on a support 20"`c"arrled by the lower frame of the apparatus. The motor M, in addition to operating the suction blower, also may be operatively connected with a fuel pump 2| for supplying fuel to the burner nozzle.
It will be understood that the returned water or condensate, as Well as the raw water supply, is introduced into the space between the shells 2 andv 1 and rises within the shell 'I to a point approximately at the top of the shell and over the tubes I4. Both the tubes I4 and I6 are, therefore, in heat exchange relationship with the water circulating in the boiler and, since the hottest part of the body of water will be at the top of the shell 1, the water vapor will discharge from the shell 'I through the pipes 22 into the vapor space at the top of the shell 2, from which it may be conducted for use through the risers 5. a
The form of boiler described provides an efcient embodiment for the combustion apparatus because the fuel fed to the combustion chamber is rapidly burned at a high temperature, substantially complete combustion taking place in the combustion chamber, the full heat transfer eiect being conserved by passing the products of combustion endwise in both directions of the boiler by the suction device communicating with the return re tubes.
Thus, a suction draft is created throughout the combustion-chamber, causing a rapid velocity through the combustion chamber and through the fire tubes and, additionally, preventing the formation of pockets of the explosive mixture within the combustion chamber. In addition to providing for the eicient combustionY of the fuel, the form of boiler disclosed also prevents the accumulation of a rich combustible mixture in the combustion chamber in the event of failure of ignition o-f the burner.
The form of boiler described is the most etlicient construction for the embodiment of the novel burra; apparatus, although other forms of boilers may be employed with suction draft connections by which a part at least of the eiv ciency of the invention may be attained.
` The director ring has inwardly inclined walls and fits into the outer end of the opening I3. A cylindrical chamber formed from spaced circular plates 25 and 26, supported on the head plate 3 by means of bolts 2l, is in communication with the outer end of the tube 23.
A series of curved plates 28 are mounted in and extend across the space between the plates 25 and 26 and form a series of outwardly aring curved chambers (Fig. 3). The outer ends of these chambers open to atmosphere through the space between a band 29 and the peripheral edges 'of the plates 25 and 26. The inner ends of the plates 28 are spaced apart, forming a series of restricted openings arranged annularly that communicate with the outer end of the tube 23. A band 29 is mounted around the peripheries of the plates 25 and 26 and has its ends connected by a thumb bolt 3U. 'I'he band 29 is loose upon the plates 25 and 26, leaving a narrow space between said band and the peripheries of said plates for the passage of air into the chambers formed between said plates 25 and 26 by the plates 28. The thumb bolt 30 may be tightened or loosened in order to reduce or enlarge the space between the band 29 and the edges of the plates 25 and 26 and thereby regulate the amount of air that may pass therethrough. The size of the space between the band 29 and the peripheral edges of the plates 25 and 26 is small, such space shown in Figs. 2 and 3 being somewhat exaggerated.
Within the tube 23 is a second tube 3l constituting the primary air supply. The tube 3l is open at itsouter end and in the opening a spider 32 is tted. The primary air supply enters between the arms of the spider 32 and is delivered through the inwardly tapered end 33 of the tube 3 l The oil nozzle 3d extends axially through the tube 3l and terminates inwardly a slight distance from the inner edge of the tube 3l.
In operation, the suction on the combustion chambervdraws air into the primary air supply tube 3l, which mixes with the oil ejected from the nozzle 3d, forming a combustible mixture aosaoos that is ignited by the ignition devices 35. The secondary air supply is drawn down through the chambers formed by the plates 28 and is given an initial rotary movement. The rotary movement thus imparted to the incoming air currents causes 'a circular movement of the air currents as they pass through the space between the tube 23 and the tube 3| and, as the air is emitted from said space at the inner end of the tube 23, it continues to rapidly revolve and mix with the combustible mixture of atomized oil and primary air. The entire burning mixture of atomized oil and air is rapidly drawn through the combustion chamber' with a circular movement, so that the burning volume of oil and air maintains a circular and longitudinal movement against the refractory walls of the combustion chamber. The
f rapid movement of the burning mixture imparts to the refractory walls a high temperature, promoting rapid combustion of substantially all of the oil before it reaches the chamber l0, so that only dry products of combustion enter the tubes l d, thus preventing the deposit of any substantial amount of carbon in the tubes and maintaining free passageways for the circulation of the products of combustion at a high temperature in their heat exchange relationship with the water in the boiler.
From the foregoingdescription, it will be understood that a combustion apparatus of high eniciency hasv been provided, and that the structure may be made extremely compact.
I am aware that the invention may be modiiied in numerous particulars without departing from the spirit and scope thereof. I do not limit myself, therefore, to the exact construction shown and described, but what I claim and desire to secure by Letters Patent is:-
1. In a combustion apparatus, the combination with a combustion chamber having an inlet opening, of a burner head comprising a primary air tube terminating adjacent said inlet opening and having unobstructed communication therewith, a fuel nozzle discharging into said inlet opening, a secondary air tube surrounding said first named tube and connected at one end with the inlet to the combustion chamber and forming a tubular chamber that discharges air only into said inlet opening, an air inlet chamber having a substantially enlarged chamber with respect to said secondary air tube and connected with the outer end of said 4secondary air tube and extending normal to the axis of said secondary air tube, and curved vanes in said air inlet chamber for imparting a spiral movement to the air currents A in said air inlet chamber and in said secondary air tube.
2. In a combustion apparatus, the combination with a combustion chamber having an air inlet opening, of a burner head comprising a primary air tube discharging into the inlet opening of the combustion chamber, a fuel nozzle extending axially through said primary air tube, ligniting means mounted adjacent said nozzle, a secondary air tube surrounding and spaced from said rst named tube and connecting with the wall of said inlet opening of the combustion chamber, a casing connected with and opening into the outer end of said secondary air tube having a greater diameter than said secondary air tube and being open at its periphery, and walls in said casing forming i inwardly converging chambers which tdischarge tangentially into said secondary air ube.
3. In a combustion apparatus, the combination with a combustion chamber provided 'an inwardly flared inlet opening, of a burner with with said secondary air tube, and `baille walls arranged in Ysaid chamber forming means for imparting a spiral movement to air currents dis-l charging into said secondary air tube.
4. In a combustion apparatus having a com-"- bustion chamber with an inlet opening, the combination of an oil nozzle, a tube ,having an inwardly converging wall`for discharging air adjacent the nozzle, a second tube surrounding said rst named tube and spaced therefrom to form an annular chamber, said second tube having an air inlet and an air outlet discharging into ythe inlet opening of the combustion chamber, spaced plates connected to said second tube adjacent .the air inlet thereof, a loose fitting closure about the periphery of said plates permitting the passage of air therebetween, said plates and said closure defining a second chamber opening into said outlet of said tube, transverse plates between said spaced plates converging inwardly to form compartments in said second chamber and said compartments having outlets discharging tangentlally to the inlet of said second tube,
whereby air drawn inwardly from said chamber and through said tube into said combustion chamber will be given a spiral motion.
5. In a device of the kind described, an air chamber including spaced walls having a peripheral opening therebetween. band means substantially and variably covering said opening, and means for contracting said band relatively tightly against said walls and for relieving it from 20 saidcontraction to tl't only loosely about said walls whereby to vary the size of the opening.
GEORGE R. KoELN.
US614076A 1932-05-28 1932-05-28 Combustion apparatus Expired - Lifetime US2053003A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US614076A US2053003A (en) 1932-05-28 1932-05-28 Combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US614076A US2053003A (en) 1932-05-28 1932-05-28 Combustion apparatus

Publications (1)

Publication Number Publication Date
US2053003A true US2053003A (en) 1936-09-01

Family

ID=24459762

Family Applications (1)

Application Number Title Priority Date Filing Date
US614076A Expired - Lifetime US2053003A (en) 1932-05-28 1932-05-28 Combustion apparatus

Country Status (1)

Country Link
US (1) US2053003A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424154A (en) * 1940-09-12 1947-07-15 Ex Lab Inc Subatmospheric gas burner
US2675865A (en) * 1950-03-24 1954-04-20 Gen Motors Corp Fluid fuel furnace and antipuffing means therefor
US2980171A (en) * 1949-04-16 1961-04-18 Selas Corp Of America Gas and oil burner
US3071181A (en) * 1958-10-16 1963-01-01 Iron Fireman Mfg Co Oil burning furnace
DE1231836B (en) * 1958-10-16 1967-01-05 Iron Fireman Mfg Co Oil burner
US3329131A (en) * 1964-12-14 1967-07-04 Space Conditioning Inc Fuel burner and combination thereof with a fire tube boiler
US3576384A (en) * 1968-11-29 1971-04-27 British American Oil Co Multinozzle system for vortex burners
US3720495A (en) * 1971-04-05 1973-03-13 Zink Co John Burner assembly for liquid fuel
US4701123A (en) * 1986-12-24 1987-10-20 The Scott & Fetzer Company Gas fuel burner

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424154A (en) * 1940-09-12 1947-07-15 Ex Lab Inc Subatmospheric gas burner
US2980171A (en) * 1949-04-16 1961-04-18 Selas Corp Of America Gas and oil burner
US2675865A (en) * 1950-03-24 1954-04-20 Gen Motors Corp Fluid fuel furnace and antipuffing means therefor
US3071181A (en) * 1958-10-16 1963-01-01 Iron Fireman Mfg Co Oil burning furnace
DE1231836B (en) * 1958-10-16 1967-01-05 Iron Fireman Mfg Co Oil burner
US3329131A (en) * 1964-12-14 1967-07-04 Space Conditioning Inc Fuel burner and combination thereof with a fire tube boiler
US3576384A (en) * 1968-11-29 1971-04-27 British American Oil Co Multinozzle system for vortex burners
US3720495A (en) * 1971-04-05 1973-03-13 Zink Co John Burner assembly for liquid fuel
US4701123A (en) * 1986-12-24 1987-10-20 The Scott & Fetzer Company Gas fuel burner

Similar Documents

Publication Publication Date Title
US2787318A (en) Burner with tangential air admission and restricted throat
US2053003A (en) Combustion apparatus
US4875465A (en) High efficiency submersible chamber water heater
US4666587A (en) Waste oil purifying process
US20110073048A1 (en) Pressure gain combustion heat generator
US2287057A (en) Steam production system
ES390338A1 (en) Steam generator having at least one combustion chamber for burning solid, liquid and/or gaseous fuels
US2048373A (en) Steam generator
US3329131A (en) Fuel burner and combination thereof with a fire tube boiler
US2486481A (en) Liquid fuel burner
US3174530A (en) Furnace combustion chamber
US2638878A (en) Water heater having extensive heat transfer surfaces
US3793994A (en) Boiler
US3539284A (en) Two-chamber fuel burner
US1924209A (en) Boiler
KR101535772B1 (en) Pellet boiler system
US2892451A (en) Boiler
US1986561A (en) High pressure boiler
US2054162A (en) Heating apparatus
US3677532A (en) Two chamber fuel burner
US2021605A (en) Heating apparatus
US2220486A (en) Boiler
US2098841A (en) Steam generator
US707216A (en) Steam-boiler.
US2206398A (en) Boiler