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US3176749A - Liquid fuel-burning heater - Google Patents

Liquid fuel-burning heater Download PDF

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Publication number
US3176749A
US3176749A US260627A US26062763A US3176749A US 3176749 A US3176749 A US 3176749A US 260627 A US260627 A US 260627A US 26062763 A US26062763 A US 26062763A US 3176749 A US3176749 A US 3176749A
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Prior art keywords
spinner
wall
liquid fuel
droplets
absorbent
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US260627A
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Edgar S Downs
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BURNER DEV CORP
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BURNER DEV CORP
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Priority to BE644312D priority Critical patent/BE644312A/xx
Application filed by BURNER DEV CORP filed Critical BURNER DEV CORP
Priority to US260627A priority patent/US3176749A/en
Priority to NL6401765A priority patent/NL6401765A/xx
Priority to DE19641451352 priority patent/DE1451352A1/en
Priority to CH230164A priority patent/CH407389A/en
Application granted granted Critical
Publication of US3176749A publication Critical patent/US3176749A/en
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    • 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
    • F23D11/04Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action
    • F23D11/08Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action using a vertical shaft

Definitions

  • My invention relates to a liquid-fuel-burning heater. It has to do, moreparticularly, with the burner of a heater of the oil-burning type. It relates to that general type of oil-burning burner which uses a mechanical spinner that receives theoil from a source of supply and throws it outwardly by centrifugal force through a surrounding combustion chamber so thatit is directed onto an: annular wall of high capillarity which receives and absorbs, the' droplets thrown otf by the spinner and in which the droplets spread to provide a large area for rapid-evaporation and burning of the oil.
  • this invention relates to that type of burner disclosed in my Patent No; 3,029,863, issued April 17, 1962.
  • the burner disclosed in said patent has gone into wide commercial use as a lightweight portable space heater, especially by building contractors and the like who need a smokeless burner that will developa high heat at a relatively low cost.
  • FIGURE 2 is an enlarged axial sectional view taken along line 22:of FIGURE 1 through the burner, showing the non-absorbent bafiie ring and associated annular absorbentwall.
  • FIGURE 3 is an enlarged, axial, sectional view taken along line 3-3 of FIGURE 2 through the spinner.
  • FIGURE 4 is a transverse, sectionalview taken along FIGURES is a transverse, sectional view taken along line"5-5 of FIGURE 2.
  • FIGURE 6 is an enlarged, sectional, diagrammatic view taken at the position indicated by line 6-6 of FIGURE'7 is a diagrammatic, transverse, sectional view illustrating a modification of the bafiie ring.
  • FIGURE 8 is a diagrammatic, transverse, sectional view illustrating another modification of the bafile ring.
  • FIGURE 9 is a diagrammatic, sectional view showing,
  • FIGURE 10 is a view similarto FIGURE 9 but show- 6 ing the ring made of a plurality of wires or the like.
  • FIGURE 11 is another view similar'to FIGURE 9 but showing a baffle ring of another cross section.
  • the burner of this invention in its general structure is stalled heating equipment whichoperatesjat higher tem- United State P atent O peratures. It is shown in the drawings as having its spinner axis upright but his to be understood that the burner will function equally as well with the spinner axis t in FIGURE '2.
  • FIGURE 2 is a diagrammatic representation of FIGURE 1
  • the burner is shown in FIGURE 1 disposed within a tubular outer casing 15 which may be suitably connected to a stack or vent when incorporated in a domestic furnace.
  • a fan 16 is disposed within the casing 15 coaxial therewith at the lower inlet portion thereof being mounted on a shaft 17 which is preferably driven by an electric motor.
  • combustion chamber 18 Disposed within the t casing 15 in spaced concentric relationship therewith upwardly toward the outlet thereof is the combustion chamber 18 which is mainly of tubular form. Since it is of smaller diameter than the casing 15 an annular air-passageway 19 is provided between the wall of the combustion chamber and the casing 19.
  • the fan 16 is of suitable form to draw air upwardly into the casing 15 and force it upwardly toward the outletof the casing through the annular space 19. and the combustion chamber 18.
  • the burner is indicated generally at 20 and is concentrically disposed withinthe combustion chamber 18 at .the lower or inlet end thereof. Just above or beyond provided with a disc or back plate 22which substantially close s it except that it is provided with an. air inlet opening 23.
  • This opening 23 serves as the primary air metering opening through which'the main supply of primary air is supplied to the burner 20 by the fan 16.
  • the shaft 17 extends forwardly through the opening 23 and it will .be noted that this shaft is hollow for conducting the fuel oil to a supply of which it maybe suitably connected.
  • the burner 20 includes the annular absorbent ring or burner wall 25 fitted snugly within 'the combustion chamber wall at the lower or inlet end thereof as shown best It may be suitably fastened in position as by means ofthe screws 26.
  • the wall 25 is made of a suitable liquid-absorbent, heat-resistant material of high capillarity. It may be of various materials such as ceramic paper or felt but I preferto use a ceramic woven cloth;
  • a suitable liquid-absorbent, heat-resistant material of high capillarity It may be of various materials such as ceramic paper or felt but I preferto use a ceramic woven cloth;
  • one or more rows of angularly spaced openings- 27 are provided extending through thewall or the combustion chamber 18 at thewall25. However, it will be noted that these openings do not extend thro ugh.
  • the front'or upper surface of the forwardmost or uppermost metal spinner disc 31 is completely covered with a thick disc or lamination 32 of thermal insulating material.
  • openings in the plate or disc 33 which is directly behind or beneath the plate 31 and in spaced relationship thereto.
  • These openings 34 may be in spaced angular relationship around the center of the plate 33 concentric with a bolt 35 which holds the plate 31 on the plate 33, a spacer washer 36 spacing the two plates apart to providethe air space 37 therebetwecn. This allows air fromthe fan 16 to flow forwardly through the holes '34 and outwardly through the space 37 between the two plates 31 and 33 to further aid in keeping the forward part of the spinner cooler and make the plates more effective as radiation shields.
  • the holes 34 may be of various size and shapes but arepreferably aligned with the air passageways 38 around the oil-slinging tube 39.
  • the tube 39 communicates with the hollow shaft 17 and its structure and thev structure of associated cooperating parts is the same as disclosed in said patent.
  • the forward or upper end of the tube 323 is flared and provides a knife edge or lip 4% from which the oil is thrown in the form of droplets upon high-speed rotation of the tube.
  • These droplets pass between the plate 33 and the flange or plate dl of the spinner hub 42.
  • cooperating bafiles 43 are arranged to aid in directing the droplets outwardly after they are thrown off the tube lip it) as described in my patent.
  • the principle I use and which has proven very beneficial in actual operation, is to use a non-absorbent ring or band 45 which is fairly narrow in the axial direction radially between the spin-' ner and the wall 25 so as to intercept thetdroplets in the main stream ,of droplets, to break them up and then to direct them onto the absorbent wall 25.
  • the ring may be located and supported in various ways'such as by the band is disposed radially closer to the wall 25 than to the periphery of the spinner to provide a sufficient radial path for the oil droplets before they strike the non-absorbent band 4-5.
  • the band 45 closer to the Wall 25 than to the spinner and have found that the distance between the band 45 and the wall 25 should be about to /4 the radius from the center of'the spinner to the surface of the absorbent wall 25. Then when the heavy droplets strike the ring &5, they will be broken up into smaller droplets and be directed axially forwardly and rearwardly onto the surface of the porous wall 25 which extends axially forwardly and rearwardly to a substantial extent relative to the ring band 45.
  • any suitable lighting means may be employed.
  • an ignition spark device46' may be provided in the burner directly adjacent the exposed surface of the wall 25.
  • the non-absorbent surface which interrupts the travel of the main stream of droplets may take various forms in addition to that of the continuous bandor ring 45 shown in FIGURES Z, 5 and 6 and described above.
  • the band or ring instead of providing a continuous surface may be formed as indicated at 45a in FIGURE 7 where it is provided with angular-1y spaced openings or spaces 5t ⁇ that permit a certain portion of the droplets of the main stream to contact directly with the wall 25.
  • FIGURE 8 a similar arrangement is shown except thattadjace'nt the openings 5 012, the material from the openings formed in the ring 451) is upturned about 45 and extends intthe direction of rotation of the spinner so as to provide baffle tabs which effectively engage the droplets from the spinner which are thrown off at approximately 45 from with its angle facing toward the spinner. ln each case,
  • a non-absorbent surface is provided as a baffle for preventing all of the droplets from striking directly on the wall 25.
  • Other baffle arrangements may be'provided.
  • means is provided for preventing at leasta portion of the droplets thrown off by the spinner from contacting directly with the absorbent wall but for permitting a certain portion thereof to contact that wall.
  • a liquid fuel burner comprising a combustion chamher having a peripheral wall, a spinner rotatably mounted on its axis within the combustion chamber in radially spaced relationship to the surrounding peripheral wall of the combustion chamber and in a transverse plane relative thereto, means for supplying liquid fuel to the spinner, means a supplying air for combustion to the spinner in cooperative relationship with the liquid fuel supplied thereto, means for rotating the spinner so as to throw off the liquid fuel supplied thereto in the form of droplets in a main transverse planar stream, a liquid fuel absorbent wall surrounding said-spinner and spaced radially outwardly therefrom between the spinner and the peripheral wall of the combustion chamber, said absorbent wall being of material of high capillarity for receiving droplets, of the liquid fuel thrown off by the spinner and spreading it throughout the area thereof to provide a large area forrapid evaporation and burning of the fuel, said absorbent wall extending axiallyin both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of
  • said nonabsorbent bafiie means being provided with angularly spaced, substantially radial openings through which some of the droplets will pass from the spinner directly onto said absorbent wall, and baffle tabs extending angularly inwardly over said openings in the direction of rotationof the spinner.
  • a liquid fuel burner comprising a combustion cham- V her having, a peripheral wall, a spinner rotatably mounted spinner, means forsupplying air for combustion to the spinner in cooperative relationship withthe liquid fuel supplied thereto, means for rotating the spinner so as to throw off the liquid fuel supplied thereto in the form of droplets in a main transverse planar stream, a liquid fuel absorbent wall surrounding said spinner and spaced radially outwardly therefrom between the spinner and f the peripheral wall of the combustion chamber, said absorbent wall being of material of high capillarity for receiving droplets of the liquid fuel thrown off by the spinner and spreading it throughout the area thereof to provide a large area for rapid evaporation and burning of the fuel, said absorbent wall extending axially in both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets created thereby, and a baflle means of nonabsorbent ma terial located in said transverse plane radially between said spinner and said absorbent wall ,s
  • said means for supplying liquid fuel to the spinner means for supplying air for combustion to the spinner in cooperative relationship with the liquid fuel supplied thereto, means for rotating the spinner so as to throw oif the liquid fuel supplied thereto in the form of droplets in a transverse planar stream, a liquid fuel absorbent wall surrounding said spinner and spaced radially outwardly therefrom between the spinner and the peripheral Wall of the combustion chamber, said absorbent wallbeing of materialof-high capillarity for receiving droplets of the liquid fuel thrown olf by the spinner and spreading it throughout the area thereof to provide a large area for rapid evaporation and burning of the fuel, said absorbent wall extending axially in both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets created thereby, said spinner comprising an innermost wall and an intermediate wall spaced axially outwardly therefrom to provide a fuel space for receiving the liquid fuel to permit it to be thrown outwardly in the form of droplets upon rotation of the spinner, said
  • said insulating lamination preventing direct exposure of the outermost wall to the flame produced in the combustion chamber of the burner and said insulating lamination and said air space reducing heat transmitted from the flame to the fuel space between said intermediate and said innermost walls, and means for mounting all of said walls for rotation together about the spinner axis as a unit.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wick-Type Burners And Burners With Porous Materials (AREA)

Description

April 6, 1965 E. s. DOWNS 3,176,749
LIQUID FUEL-BURNING HEATER Filed Feb. 25, 1965 3 Sheets-Sheet 1 [8 i I I 2 \1 w INV NTOR EDGAR s pow/vs fi -g MAli/VEY, MILLERQRAMBO ATTORNEYS April 1965 E. s. DOWNS 3,176,749
LIQUID FUEL-BURNING HEATER Filed Feb. 25, 1963 3 Sheets-Sheet 2 INVENTOR. EDGAR 5'. DOW/V5 BY MAHONEY, MILLER 8 RAMBO ATTORNEYS A ril 6, 1965 E. s. DOWNS 3,175,749
LIQUID FUEL-BURNING HEATER Filed Feb. 25, 1963 s Sheets-Sheet s INVENTOR. E 0634/? S DOW/VS ,M/LLER aanwaa FIGURE 5.
LiQUIi) FUEL-BURNING HEATER Edgar S. Downs, Worthington, Ohio, assignor to Burner This application is a continuation-in-part' of my'copending application Serial No. 183,251, filed March 28, 1962-, now Patent No. 3,127,924 dated April 7, 1964, and which, in turn, is a division of application Serial No. 37,874, filed June 22, 1960, now Patent No. 3,029,863, dated April 17, 1962. i
My invention relates to a liquid-fuel-burning heater. It has to do, moreparticularly, with the burner of a heater of the oil-burning type. It relates to that general type of oil-burning burner which uses a mechanical spinner that receives theoil from a source of supply and throws it outwardly by centrifugal force through a surrounding combustion chamber so thatit is directed onto an: annular wall of high capillarity which receives and absorbs, the' droplets thrown otf by the spinner and in which the droplets spread to provide a large area for rapid-evaporation and burning of the oil.
More specifically, this invention relates to that type of burner disclosed in my Patent No; 3,029,863, issued April 17, 1962. The burner disclosed in said patent has gone into wide commercial use as a lightweight portable space heater, especially by building contractors and the like who need a smokeless burner that will developa high heat at a relatively low cost. However, in adapting this burner to permanently installed commercial and residential heating equipment, it was found desirable to make certain improvements therein whichwould make the burner function even more efliciently in' such equipment wherethe' burner operates at a higher temperature.
embodying the "present I invention.
' FIGURE 2 is an enlarged axial sectional view taken along line 22:of FIGURE 1 through the burner, showing the non-absorbent bafiie ring and associated annular absorbentwall. i
. FIGURE 3 is an enlarged, axial, sectional view taken along line 3-3 of FIGURE 2 through the spinner.
FIGURE 4 is a transverse, sectionalview taken along FIGURES is a transverse, sectional view taken along line"5-5 of FIGURE 2.
FIGURE 6 is an enlarged, sectional, diagrammatic view taken at the position indicated by line 6-6 of FIGURE'7 is a diagrammatic, transverse, sectional view illustrating a modification of the bafiie ring.
FIGURE 8 is a diagrammatic, transverse, sectional view illustrating another modification of the bafile ring.
FIGURE 9 is a diagrammatic, sectional view showing,
a baffler'ing of different cross section.
FIGURE 10 is a view similarto FIGURE 9 but show- 6 ing the ring made of a plurality of wires or the like.
FIGURE 11 is another view similar'to FIGURE 9 but showing a baffle ring of another cross section.
. The burner of this invention in its general structure is stalled heating equipment whichoperatesjat higher tem- United State P atent O peratures. It is shown in the drawings as having its spinner axis upright but his to be understood that the burner will function equally as well with the spinner axis t in FIGURE '2.
FIGURE 2.
in a horizontal position. v
The burner is shown in FIGURE 1 disposed withina tubular outer casing 15 which may be suitably connected to a stack or vent when incorporated in a domestic furnace. A fan 16 is disposed within the casing 15 coaxial therewith at the lower inlet portion thereof being mounted on a shaft 17 which is preferably driven by an electric motor. x
Disposed within the t casing 15 in spaced concentric relationship therewith upwardly toward the outlet thereof is the combustion chamber 18 which is mainly of tubular form. Since it is of smaller diameter than the casing 15 an annular air-passageway 19 is provided between the wall of the combustion chamber and the casing 19. The fan 16 is of suitable form to draw air upwardly into the casing 15 and force it upwardly toward the outletof the casing through the annular space 19. and the combustion chamber 18.
The burner is indicated generally at 20 and is concentrically disposed withinthe combustion chamber 18 at .the lower or inlet end thereof. Just above or beyond provided with a disc or back plate 22which substantially close s it except that it is provided with an. air inlet opening 23. This opening 23 serves as the primary air metering opening through which'the main supply of primary air is supplied to the burner 20 by the fan 16. The shaft 17 extends forwardly through the opening 23 and it will .be noted that this shaft is hollow for conducting the fuel oil to a supply of which it maybe suitably connected.
The burner 20 includes the annular absorbent ring or burner wall 25 fitted snugly within 'the combustion chamber wall at the lower or inlet end thereof as shown best It may be suitably fastened in position as by means ofthe screws 26. As disclosed in my prior patent, the wall 25 is made of a suitable liquid-absorbent, heat-resistant material of high capillarity. It may be of various materials such as ceramic paper or felt but I preferto use a ceramic woven cloth; For supplying part of the primary air for] combustion, through the porous cloth wall, one or more rows of angularly spaced openings- 27 are provided extending through thewall or the combustion chamber 18 at thewall25. However, it will be noted that these openings do not extend thro ugh. the
absorbent porous cloth wall 25. Between the primary spinner inits general construction is likejthat disclosed in said patent but is improved to make it function even axial with the absorbent burner wall 25. The spinner is located directly forward or above the plate 22 inassociation with the opening 23-therein as shown best in Although this spinner is of the. general structure =disclosed in my patent, I have found that in some instances, as in a residential furnace where temperatures are higher,
it isflnecessary to provide for a redncedtemperature at 3,i76,749 Patented Apr.- 6,1965
It is carried by the shaft17 and is co the oil spinner or slinger so as to prevent evaporation of the oil before it leaves the surface of the spinner. If oil leaves the surface of the spinner in the vaporized state, it does not travel far from the spinner due to its low inertia as compared to the liquid oil, thus causing an overly rich area in the vicinity of the spinner which causes excessive carbon formation on the spinner;
As one means of preventing overheating of the spinner, the front'or upper surface of the forwardmost or uppermost metal spinner disc 31 is completely covered with a thick disc or lamination 32 of thermal insulating material.
This has been found to reduce very sharply the temperature at the rear or lower portion of the spinner due to the fact that metal at the forward side and which is attached to the rear side of the spinner is not exposed directly in the flame produced by the burner.
Another means of reducing the temperature of the spinner is in providing openings in the plate or disc 33 which is directly behind or beneath the plate 31 and in spaced relationship thereto. These openings 34 may be in spaced angular relationship around the center of the plate 33 concentric with a bolt 35 which holds the plate 31 on the plate 33, a spacer washer 36 spacing the two plates apart to providethe air space 37 therebetwecn. This allows air fromthe fan 16 to flow forwardly through the holes '34 and outwardly through the space 37 between the two plates 31 and 33 to further aid in keeping the forward part of the spinner cooler and make the plates more effective as radiation shields. The holes 34 may be of various size and shapes but arepreferably aligned with the air passageways 38 around the oil-slinging tube 39. The tube 39 communicates with the hollow shaft 17 and its structure and thev structure of associated cooperating parts is the same as disclosed in said patent. Thus, the forward or upper end of the tube 323 is flared and provides a knife edge or lip 4% from which the oil is thrown in the form of droplets upon high-speed rotation of the tube. These droplets pass between the plate 33 and the flange or plate dl of the spinner hub 42. Between these plates 33 and 41 cooperating bafiles 43 are arranged to aid in directing the droplets outwardly after they are thrown off the tube lip it) as described in my patent. i i I have found that under certain high temperature conditions, the main transverse planar stream of fuel droplets strike the wall or pad 25 in such' heavy concentration that a band of carbon builds up at the surface of thewall in the transverse plane of the travel of the heavier droplets which is in the plane of the outlet space between the spinnerplates 33 and 41. This is only true along a narrow band intermediate the axial extent of the absorbent wall 25. To prevent this build-up, I provide a ring 45 i of non-absorbent material, such as metal, in the path of the main stream of heavy droplets thrown off by the spinner. 'However, this ring must be of a limited extent in an axial'direction so that the satellite droplets will contact directly with the absorbent wall 25.
Studies of this burner have shown that the spinner throws off the oil as a concentration of droplets in the transverse plane of the outlet space of the spinner and that this center stream contains a relatively large percentage of the total volume of the discharged oil but that it is restricted to aaquite narrow band, The same studies have also shown that in diverging transverse planes to either side of the main transverse planar stream of oil droplets, there are quite a number of less concentrated oil droplets which -I call satellite droplets. The principle I use and which has proven very beneficial in actual operation, is to use a non-absorbent ring or band 45 which is fairly narrow in the axial direction radially between the spin-' ner and the wall 25 so as to intercept thetdroplets in the main stream ,of droplets, to break them up and then to direct them onto the absorbent wall 25. The ring may be located and supported in various ways'such as by the band is disposed radially closer to the wall 25 than to the periphery of the spinner to provide a sufficient radial path for the oil droplets before they strike the non-absorbent band 4-5. I prefer to have the band 45 closer to the Wall 25 than to the spinner and have found that the distance between the band 45 and the wall 25 should be about to /4 the radius from the center of'the spinner to the surface of the absorbent wall 25. Then when the heavy droplets strike the ring &5, they will be broken up into smaller droplets and be directed axially forwardly and rearwardly onto the surface of the porous wall 25 which extends axially forwardly and rearwardly to a substantial extent relative to the ring band 45.
Thus, it will be apparent from the diagrammatic illustrations in FIGURES 5 and 6 that by using a band 45 of the type indicated and located as indicated, the main stream of droplets thrown off by the spinner in the transverse plane of the lip 40 is broken up and dispersed and directed onto the absorbent wall, while at the same time the satellite droplets which are in streams in forwardly and rearwardly diverging planes on axiallyopposite sides of the main stream travel, directly onto the wall 25 and will spread axially, as well as circumferentially, in both directions in the absorbent wallf Similarly, when the droplets bounce off the band 45, they contact the absorbent wall forwardly and rearwardly thereof and spread axially in both directions, as well as circumferentially, in the wall 25. Thus, formation of carbon on the absorbent wall by the concentrated droplets is prevented but at the 7 same time, the lighter droplets are allowed to contact directly with the absorbent Wall to provide for smooth quick starting or lighting of the burner as well as more efiicient sustained burning without carbon formation. Tests have 'such surface to the bottom of the burner and the burner could not be lighted inthe horizontal position which it does so easily when the droplets strike the absorbent wall.
25. Any suitable lighting means may be employed. For example, an ignition spark device46' may be provided in the burner directly adjacent the exposed surface of the wall 25.
The non-absorbent surface which interrupts the travel of the main stream of droplets may take various forms in addition to that of the continuous bandor ring 45 shown in FIGURES Z, 5 and 6 and described above.
'For example, as shown in FIGURE 7, the band or ring instead of providing a continuous surface may be formed as indicated at 45a in FIGURE 7 where it is provided with angular-1y spaced openings or spaces 5t} that permit a certain portion of the droplets of the main stream to contact directly with the wall 25. In FIGURE 8. a similar arrangement is shown except thattadjace'nt the openings 5 012, the material from the openings formed in the ring 451) is upturned about 45 and extends intthe direction of rotation of the spinner so as to provide baffle tabs which effectively engage the droplets from the spinner which are thrown off at approximately 45 from with its angle facing toward the spinner. ln each case,
' a strictly radial direction.
V In FIGURE 9, I show the ring Q50 in theform'ofa heavy Wire whereas in FIGURE 10 the'ring 45d is formed of several wires arranged in a triangular cross section.
a non-absorbent surface is provided as a baffle for preventing all of the droplets from striking directly on the wall 25. Other baffle arrangements may be'provided.
spinner and resulting excessive carbon formation thereon. Also, according to this invention, means is provided for preventing at leasta portion of the droplets thrown off by the spinner from contacting directly with the absorbent wall but for permitting a certain portion thereof to contact that wall. With this arrangement, excessive carbon formation on the absorbent wall isprevented but quick and easy lighting and sustained burning is insured.
Having thus described my invention, what I claim is:
1. A liquid fuel burner comprising a combustion chamher having a peripheral wall, a spinner rotatably mounted on its axis within the combustion chamber in radially spaced relationship to the surrounding peripheral wall of the combustion chamber and in a transverse plane relative thereto, means for supplying liquid fuel to the spinner, means a supplying air for combustion to the spinner in cooperative relationship with the liquid fuel supplied thereto, means for rotating the spinner so as to throw off the liquid fuel supplied thereto in the form of droplets in a main transverse planar stream, a liquid fuel absorbent wall surrounding said-spinner and spaced radially outwardly therefrom between the spinner and the peripheral wall of the combustion chamber, said absorbent wall being of material of high capillarity for receiving droplets, of the liquid fuel thrown off by the spinner and spreading it throughout the area thereof to provide a large area forrapid evaporation and burning of the fuel, said absorbent wall extending axiallyin both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets created thereby, and a battle means of nonabsorbent material located in said main transverse plane radially between said spinner and said absorbent wall so that part of the droplets thrown off by said spinner will first contact said baflle means and be broken up and then be directed onto said absorbent wall, said nonabsorbent bafiie means extending axially only a portion of the axial extent of said absorbent wall to expose said absorbent wall to direct contact of some of the droplets thrown off by the spinner, said nonabsorbent baflle means extending axially A to the axial extent of theabsorbent wall and the radial spacing of the nonabsorbent baffie means from the absorbent Wall being about to A the radius from the axis of the spinner to the surface of the absorbent wall.
2. A liquid fuel burner according to claim 1 in which .the nonabsorbent battle means is in the form of an annular band of flat cross-section in a direction parallel to the supplied thereto, means for rotating the spinner so as tothrow off the liquid fuel supplied thereto in the form of droplets in a main transverse planar stream, a liquid fuel absorbent wall surrounding said spinner and spaced radially outwardly therefrom between the spinner and the peripheral wall of the combustion chamber, said absorbent wall being of material of high capillarity for receiving droplets of the liquid fuel thrown off by the spinner and spreading it throughout the area thereof to provide a large area for rapid evaporation and burning of 1 the fuel, said absorbent wall extending axially in both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets material locatedinsaid transverse plane radially between said spinner and said absorbent walllso that partof the droplets thrown off by said spinner will first contact said baffle means and be broken up and then be directed onto said absorbentwall, said nonabsorbent bafile means extending axially only-a portion. of the axial extent of said absorbentwall to expose said. absorbent wallto direct contact of some of the droplets thrown off by the spinner, said nonabsorbent bafiie means being provided with angularly spaced, substantially radial openings through which some of the droplets will pass from the spinner directly onto said absorbent wall, and baffle tabs extending angularly inwardly over said openings in the direction of rotationof the spinner.
4. A liquid fuel burner comprising a combustion cham- V her having, a peripheral wall, a spinner rotatably mounted spinner, means forsupplying air for combustion to the spinner in cooperative relationship withthe liquid fuel supplied thereto, means for rotating the spinner so as to throw off the liquid fuel supplied thereto in the form of droplets in a main transverse planar stream, a liquid fuel absorbent wall surrounding said spinner and spaced radially outwardly therefrom between the spinner and f the peripheral wall of the combustion chamber, said absorbent wall being of material of high capillarity for receiving droplets of the liquid fuel thrown off by the spinner and spreading it throughout the area thereof to provide a large area for rapid evaporation and burning of the fuel, said absorbent wall extending axially in both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets created thereby, and a baflle means of nonabsorbent ma terial located in said transverse plane radially between said spinner and said absorbent wall ,so that part of the droplets thrown off by said spinner will first contact said baffle means and be broken up and then be directed onto said absorbent Wall, said nonabsorbent bafile means extending axially only a portion of the axial extent of said absorbent wall to expose said absorbent wall to direct contact of some of the droplets thrown off by the spinner, said spinner being provided with an outer wall covered with insulation, said wall being spaced axially from an inner wall to provide a space which receives some of the air supplied for combustion, said inner wall being prober having a peripheral wall, a spinner rotatably mounted within the combustion chamber in radially spaced relationship to the surrounding peripheral wall of the combustion chamber and in a transverse plane relative thereto,
means for supplying liquid fuel to the spinner, means for supplying air for combustion to the spinner in cooperative relationship with the liquid fuel supplied thereto, means for rotating the spinner so as to throw oif the liquid fuel supplied thereto in the form of droplets in a transverse planar stream, a liquid fuel absorbent wall surrounding said spinner and spaced radially outwardly therefrom between the spinner and the peripheral Wall of the combustion chamber, said absorbent wallbeing of materialof-high capillarity for receiving droplets of the liquid fuel thrown olf by the spinner and spreading it throughout the area thereof to provide a large area for rapid evaporation and burning of the fuel, said absorbent wall extending axially in both directions relative to the transverse plane of the spinner and the main transverse plane of the stream of droplets created thereby, said spinner comprising an innermost wall and an intermediate wall spaced axially outwardly therefrom to provide a fuel space for receiving the liquid fuel to permit it to be thrown outwardly in the form of droplets upon rotation of the spinner, said means for supplying liquid fuel to the spinner comprising a passage means around the spinner axis leading into said fuel space, said means for supplying air for combustion comprising a passage means surrounding said liquid fuel passage means leading into said fuel space, and means for providing for a reduced temperature at said fuel space in the spinner to prevent evaporation of the oil before it leaves said space so that the fuel will be thrown outwardly from that space in the formof droplets which will reach said absorbent wall,
outer surface of said outermost wall, said insulating lamination preventing direct exposure of the outermost wall to the flame produced in the combustion chamber of the burner and said insulating lamination and said air space reducing heat transmitted from the flame to the fuel space between said intermediate and said innermost walls, and means for mounting all of said walls for rotation together about the spinner axis as a unit.
References Cited by the Examiner UNITED STATES PATENTS JAMES W. WESTHAVER, Primary Examiner.
MEYER PERLIN, Examiner.

Claims (1)

1. A LIQUID FUEL BURNER COMPRISING A COMBUSTION CHAMBER HAVING A PERIPHERAL WALL, A SPINNER ROTATABLY MOUNTED ON ITS AXIS WITHIN THE COMBUSTION CHAMBER IN RADIALLY SPACED RELATIONSHIP TO THE SURROUNDING PERIPHERAL WALL OF THE COMBUSTION CHAMBER AND IN A TRANSVERSE PLANE RELATIVE THERETO, MEANS FOR SUPPLYING LIQUID FUEL TO THE SPINNER, MEANS FOR SUPPLYING AIR FOR COMBUSTION TO THE SPINNER IN COOPERATIVE RELATIONSHIP WITH THE LIQUID FUEL SUPPLIED THERETO, MEANS FOR ROTATING THE SPINNER SO AS TO THROW OFF THE LIQUID FUEL SUPPLIED THERETO IN THE FORM OF DROPLETS IN A MAIN TRANSVERSE PLANAR STREAM, A LIQUID FUEL ABSORBENT WALL SURROUNDING SAID SPINNER AND SPACED RADIALLY OUTWARDLY THEREFROM BETWEEN THE SPINNER AND THE PERIPHERAL WALL OF THE COMBUSTION CHAMBER, SAID ABSORBENT WALL BEING OF MATERIAL OF HIGH CAPILLARITY FOR RECEIVING DROPLETS OF THE LIQUID FUEL THROWN OFF BY THE SPINNER AND SPREADING IT THROUGHOUT THE AREA THEREOF TO PROVIDE A LARGE AREA FOR RAPID EVAPORATION AND BURNING OF THE FUEL, SAID ABSORBENT WALL EXTENDING AXIALLY IN BOTH DIRECTIONS RELATIVE TO THE TRANSVERSE PLANE OF THE SPINNER
US260627A 1963-02-25 1963-02-25 Liquid fuel-burning heater Expired - Lifetime US3176749A (en)

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BE644312D BE644312A (en) 1963-02-25
US260627A US3176749A (en) 1963-02-25 1963-02-25 Liquid fuel-burning heater
NL6401765A NL6401765A (en) 1963-02-25 1964-02-25
DE19641451352 DE1451352A1 (en) 1963-02-25 1964-02-25 Liquid fuel burners
CH230164A CH407389A (en) 1963-02-25 1964-02-25 Liquid fuel burner

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3291118A (en) * 1964-10-09 1966-12-13 La Roy A Wilson Snow melter
US3386794A (en) * 1965-06-08 1968-06-04 Howden James & Co Ltd Liquid-fuel burner
US3603711A (en) * 1969-09-17 1971-09-07 Edgar S Downs Combination pressure atomizer and surface-type burner for liquid fuel
US4504215A (en) * 1981-10-09 1985-03-12 Nippon Gakki Seizo Kabushiki Kaisha Liquid fuel burner
US4618323A (en) * 1980-02-19 1986-10-21 Southers California Edison Method and burner tip for suppressing emissions of nitrogen oxides
US5056501A (en) * 1989-11-16 1991-10-15 Zexel Corporation Combustion heater
US20120193452A1 (en) * 2009-12-11 2012-08-02 Nv Bekaert Sa Burner with low porosity burner deck

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1497829A (en) * 1922-07-01 1924-06-17 Herman J Allen Oil burner
US1949260A (en) * 1931-12-15 1934-02-27 Petroleum Heat & Power Co Oil burning apparatus
US2058196A (en) * 1933-07-15 1936-10-20 Rotor Oil Burner Corp Oil burner
US2062633A (en) * 1934-03-06 1936-12-01 Oscar J Appel Hearth construction for oil burners
US2112888A (en) * 1934-02-09 1938-04-05 John E Greenawalt Burner
USRE20939E (en) * 1938-12-06 Apparatus for producing
US3029863A (en) * 1960-06-22 1962-04-17 Edgar S Downs Liquid fuel burning heater
US3053314A (en) * 1959-11-16 1962-09-11 John J Mcgillis Rotary oil burners

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE20939E (en) * 1938-12-06 Apparatus for producing
US1497829A (en) * 1922-07-01 1924-06-17 Herman J Allen Oil burner
US1949260A (en) * 1931-12-15 1934-02-27 Petroleum Heat & Power Co Oil burning apparatus
US2058196A (en) * 1933-07-15 1936-10-20 Rotor Oil Burner Corp Oil burner
US2112888A (en) * 1934-02-09 1938-04-05 John E Greenawalt Burner
US2062633A (en) * 1934-03-06 1936-12-01 Oscar J Appel Hearth construction for oil burners
US3053314A (en) * 1959-11-16 1962-09-11 John J Mcgillis Rotary oil burners
US3029863A (en) * 1960-06-22 1962-04-17 Edgar S Downs Liquid fuel burning heater

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3291118A (en) * 1964-10-09 1966-12-13 La Roy A Wilson Snow melter
US3386794A (en) * 1965-06-08 1968-06-04 Howden James & Co Ltd Liquid-fuel burner
US3603711A (en) * 1969-09-17 1971-09-07 Edgar S Downs Combination pressure atomizer and surface-type burner for liquid fuel
US4618323A (en) * 1980-02-19 1986-10-21 Southers California Edison Method and burner tip for suppressing emissions of nitrogen oxides
US4504215A (en) * 1981-10-09 1985-03-12 Nippon Gakki Seizo Kabushiki Kaisha Liquid fuel burner
US5056501A (en) * 1989-11-16 1991-10-15 Zexel Corporation Combustion heater
US20120193452A1 (en) * 2009-12-11 2012-08-02 Nv Bekaert Sa Burner with low porosity burner deck

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