US1934379A - Oil burner - Google Patents

Oil burner Download PDF

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Publication number
US1934379A
US1934379A US536337A US53633731A US1934379A US 1934379 A US1934379 A US 1934379A US 536337 A US536337 A US 536337A US 53633731 A US53633731 A US 53633731A US 1934379 A US1934379 A US 1934379A
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Prior art keywords
throat
fuel
venturi
burner
chamber
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US536337A
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Fred E Rudolph
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MIRACLE BURNER Corp
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MIRACLE BURNER CORP
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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
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • F23D11/102Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber

Definitions

  • Another object i's the provision of means for discharging fuel along a predetermined, path to effect the complete. atomization and, twirling movement .with consequent diffusion in the presenceof air or other oxidizingmediums.
  • .Still another object is to, provide a burner .whichgwill have a high fuel velocity discharge in the presence of a dispersing mediumvfor effecting complete atomization, emulsification and subsequent discharge, in a twirling path.
  • a further. object is the provision. ofmeansfor completely. atomizing. fuel at a high velocity with the consequent discharge thereof at an appreciablyureduced velocity. for. effective cominglingmwith. air .in..the..path thereof.
  • a still further object is to provide means, for completelyrfatomizingand emulsifying fuel and impartingmolecularactivity thereto in the presment of the present invention.
  • Still a further object is to provide an extremely simple and improved combination of'elements'for effectively preparing'low grade fuels for combustion in a completely emulsified state withincreased thermal'efiicienc'y. f
  • FIG. 1 is asectional view in elevation of the I burner element embodying features of the present invention.
  • Figure 2 is an end View in elevation of the device s'hown in Figurel;
  • Figure 3 is a front View shown in Figure l.
  • Figure 4 is a side view in elevation and .oil inlet nipple.
  • Figure 5 is a side view in elevationof the yenturi mixing chamber.
  • Figure 6 is'a side view'in elevation of of a hollow cone spray of the steam h holl w.
  • Figure 7 is an end'view ofthe cone spray shown in Figure 6 when viewed from the'interior thereof; 7 g i Figure 8 is a front View of an impeller disk arranged for disposition in the path of the fuel; and i V Figure 9 isan edge view of the impeller disk shown in Figure 8.
  • the structure selected for illustration comprises an oil burner having an elongated cylindrical tube orburner shell 19 Which'is threaded internally at both ends '20 and 21 thereof for'the' reception of acorrespondingly threaded nipple 22 and spray device 23. These serve as closures for the elongated tube 19, and the peripheries 24 and125, respectively, thereof serve as a complement to the interior of the casing 16 for aligned telescopic placement therein.
  • the nipple 2215 provided with threaded' inlets '26 and 27, in this instance twogwhich communicate with ports 28 and 29 leading through the opposite side'thereof'for communication with" the interior of the cylindrical casing or burner shell 19.
  • port 29 is comparatively large and terminates in an axial nipple projection 30, while the oil ports 28, in this instance two, are exceedingly smaller so as to effect the issuance of oil or liquid fuel at, a, highjvelocity for entry within an annular fuel chamber 31 defined by the reducedneck 32 which communicates'with the throat of a mixing t is to be noted that the v chamber 33.
  • the mixing chamber body 33 is of cylindrical exterior configuration of corresponding size with the interior of the burner shell 19 for confinement therein, and the interior thereof is provided with a frustro conical bore 34 diverging at the discharge end thereof.
  • the bore 3 1 communicates with an outwardly, oppositely tapered connecting bore 35 which is complemental to the nipple projection 30 for frictional engagement therewith.
  • the steam port 29 communicates directly with the frustro conical bore 34 defining a Venturi-shaped mixing chamber within the member 33, thus serving as a Venturi passage for progressive decreased velocity of the mixture passing therethrough.
  • ports 36 in this instance two, are provided in the neck 32 proximate to the shoulder defined by the mixing chamber body 33.
  • the ports 36 communicate with the annular chamber 31 for the reception of fuel such as oil issuing from the ports 28 to present a circular film 37 directly in the path of the steam port 29.
  • Steam under pressure issues from the port 29 to disperse the fuel film 37 for effecting complete atomization and molecular activity to theresulting mixture which proceeds at an instantaneously high velocity to promote the diffusion at the entrance of the Venturi 34.
  • the impeller plate 38 is of circular configuration for confinement within the burner shell 19, it being disposed in adjacent contact with the discharge end of the mixing chamber 33 to impart a twirling movement to the mixture issuing therethrough.
  • the twirling movement is occasioned by obliquely disposed slots 39 which are spirally arranged in the impeller plate 38 so as to produce and impart a twirling movement to the issuing liquid fuel.
  • the hollow cone spray 23 threadedly engages the extremity 21 of the burner shell 19 to maintain the impeller plate 38 in position and to guide and direct the fuel spray issuing therethrough.
  • This is effected by providing a cone shaped end 40 thereon of any desired angularity as commercial practice may dictate for the reception of circumferentially spaced apertures 41 therein.
  • the apertures 41 are preferably spaced at sufficient distances so -'as to preclude any destructive interference between the sprays, as well as provide for complete aeration conducive to complete oxidation and ensuing combustion.
  • the angularity of the cone piece 40 is dependent largely upon the desired expanse of the resulting flame which should clear a refractory annulus spaced sufficiently from a cone shield comprising a part of the burner support to admit air therebetween.
  • a member forming a Venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member having an enlarged chamber at the front of said throat, an atomizing medium inlet arranged axially of the Venturi immediately to the rear of the liquid inlets, said atomizing inlet having a diameter less than the diameter of the Venturi throat.
  • a member forming a .venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member. having an enlarged chamber at the front of said throat, an atomizing medium inlet arranged axially of the Venturi-immediately to the rear of the liquid inlets, said atomizing inlet having a diameter'less than the diameter of the Venturi throat, and an impeller disposed transversely of said enlarged chamber to impart atwirling movement tothe mixture issuing therethrough.
  • a member forming a Venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member having. an enlarged 115 chamber at the front of said throat, an atomizing medium inlet arranged axially of the venturi immediately to the rear of the liquid inlets, said atomizing inlet having a diameter less than the diameter of the Venturi throat, an impeller disposed transversely of said enlarged chamber to impart a twirling movement to the mixture issuing therethrough, and an apertured cap detachably associated with said enlarged chamber for directing the discharge of the mixture therefrom.
  • an enlarged chamber having a reduced axial throat at one end thereof, radial liquid fuel inlets provided in said throat immediately to'the' rear of said enlarged chamber, an .atomizing medium inlet arranged axially of said throat'im- 'mediately to the rear of said liquid fuel'inlets,
  • an enlarged chamber having areduced axial throat at one end thereof, radial liquid fuel inlets provided in said throat immediately to the rear of said enlarged chamber, an atomizing medium inlet arranged axially of said throat improximate to the discharge end thereof to impart a twirling movement to the mixture issuing therethrough, and an apertured discharge cap in threaded engagement with said chamber to maintain said impeller disc in position and direct the discharge from said chamber.

Description

Nov. 7, 1933; F. E. RUDOLPH OIL BURNER Filed May 11, 1931 mm mm Patented Nov. 7, 1933 ;U NITED STATES o L BURNER Fred E. Rudolph, Chicago, Ill., assignor, by direct and mesne assignments, to Miracle Burner Corv poration, Chicago, 111., a corporation of Illinois I Application'lvlay 11, 1931. Serial No. 536,337 6 Claims. (01. 158-75) This inventionrelates to fuel burners and more particularly to oil burners, although certain featuresthereof maybeemployed withequal advantage for other purposes.
"Itmonteniplates more. especially provision of novel means for directing liquid fuel along a predetermined path with varying velocity for effecting complete atomization and oxidation to insure thelcomplete combustion thereof.
Numerous types ofloil burners have heretofore been-proposed, butthese have not provenvery satisfactorylforthe consumption of low grade oils whichconstitute the by-lproductsof known processesof cracking oils. In fact, it has heretofore beenlthought impossible to burn such low grade fuels which finally result from commercial cracking processes, and many years ofresearch have been unsuccessful in'the. combustion thereof for commercial purposes with the consequent genera- 'One object of. the. present invention is to simplify.the.constisuction'and.improve the operationofidevices of the character mentioned.
Another object i's the provision of means for discharging fuel along a predetermined, path to effect the complete. atomization and, twirling movement .with consequent diffusion in the presenceof air or other oxidizingmediums.
.Still another object is to, provide a burner .whichgwill have a high fuel velocity discharge in the presence of a dispersing mediumvfor effecting complete atomization, emulsification and subsequent discharge, in a twirling path.
A further. object is the provision. ofmeansfor completely. atomizing. fuel at a high velocity with the consequent discharge thereof at an appreciablyureduced velocity. for. effective cominglingmwith. air .in..the..path thereof.
A still further object is to provide means, for completelyrfatomizingand emulsifying fuel and impartingmolecularactivity thereto in the presment of the present invention.
cone spray shown in Figure 3.
bustion.
, Still a further object is to provide an extremely simple and improved combination of'elements'for effectively preparing'low grade fuels for combustion in a completely emulsified state withincreased thermal'efiicienc'y. f
' Cthe'r objects and advantages will appear from the following'description of an illustratedembodi- In thedrawin'gz I Figure 1 is asectional view in elevation of the I burner element embodying features of the present invention.
Figure 2 is an end View in elevation of the device s'hown in Figurel;
Figure 3 is a front View shown in Figure l.
Figure 4 is a side view in elevation and .oil inlet nipple.
Figure 5 is a side view in elevationof the yenturi mixing chamber. w
Figure 6 is'a side view'in elevation of of a hollow cone spray of the steam h holl w.
'Figure 7 is an end'view ofthe cone spray shown in Figure 6 when viewed from the'interior thereof; 7 g i Figure 8 is a front View of an impeller disk arranged for disposition in the path of the fuel; and i V Figure 9 isan edge view of the impeller disk shown in Figure 8.
The structure selected for illustration comprises an oil burner having an elongated cylindrical tube orburner shell 19 Which'is threaded internally at both ends '20 and 21 thereof for'the' reception of acorrespondingly threaded nipple 22 and spray device 23. These serve as closures for the elongated tube 19, and the peripheries 24 and125, respectively, thereof serve as a complement to the interior of the casing 16 for aligned telescopic placement therein. i
"As shown, the nipple 2215 provided with threaded' inlets '26 and 27, in this instance twogwhich communicate with ports 28 and 29 leading through the opposite side'thereof'for communication with" the interior of the cylindrical casing or burner shell 19. port 29 is comparatively large and terminates in an axial nipple projection 30, while the oil ports 28, in this instance two, are exceedingly smaller so as to effect the issuance of oil or liquid fuel at, a, highjvelocity for entry within an annular fuel chamber 31 defined by the reducedneck 32 which communicates'with the throat of a mixing t is to be noted that the v chamber 33. The mixing chamber body 33 is of cylindrical exterior configuration of corresponding size with the interior of the burner shell 19 for confinement therein, and the interior thereof is provided with a frustro conical bore 34 diverging at the discharge end thereof. The bore 3 1 communicates with an outwardly, oppositely tapered connecting bore 35 which is complemental to the nipple projection 30 for frictional engagement therewith. In this position, the steam port 29 communicates directly with the frustro conical bore 34 defining a Venturi-shaped mixing chamber within the member 33, thus serving as a Venturi passage for progressive decreased velocity of the mixture passing therethrough.
It is to be noted that in order to inject a spray of fuel within the mouth or throat of the Venturi 34 for projection in the path of the steam issuing from the port 29, diametrically opposite ports 36, in this instance two, are provided in the neck 32 proximate to the shoulder defined by the mixing chamber body 33. It will thus be noted that the ports 36 communicate with the annular chamber 31 for the reception of fuel such as oil issuing from the ports 28 to present a circular film 37 directly in the path of the steam port 29. Steam under pressure issues from the port 29 to disperse the fuel film 37 for effecting complete atomization and molecular activity to theresulting mixture which proceeds at an instantaneously high velocity to promote the diffusion at the entrance of the Venturi 34.
With this arrangement, the diffusion and atomization of the fuel is instantaneously efiected and promoted by the consequent high velocity in the vicinity of the Venturi mouth, and thereafter the velocity is decreased for consequent discharge through an impeller plate 38, The impeller plate 38 is of circular configuration for confinement within the burner shell 19, it being disposed in adjacent contact with the discharge end of the mixing chamber 33 to impart a twirling movement to the mixture issuing therethrough. The twirling movement is occasioned by obliquely disposed slots 39 which are spirally arranged in the impeller plate 38 so as to produce and impart a twirling movement to the issuing liquid fuel.
As stated, the hollow cone spray 23 threadedly engages the extremity 21 of the burner shell 19 to maintain the impeller plate 38 in position and to guide and direct the fuel spray issuing therethrough. This is effected by providing a cone shaped end 40 thereon of any desired angularity as commercial practice may dictate for the reception of circumferentially spaced apertures 41 therein. The apertures 41 are preferably spaced at sufficient distances so -'as to preclude any destructive interference between the sprays, as well as provide for complete aeration conducive to complete oxidation and ensuing combustion. The angularity of the cone piece 40 is dependent largely upon the desired expanse of the resulting flame which should clear a refractory annulus spaced sufficiently from a cone shield comprising a part of the burner support to admit air therebetween.
It is thus apparent that the fuel is completely atomized, the maximum diffusion is effected at high velocity, and the velocity subsequently reduced prior to issuance or discharge in a twirling path for flaring combustion. Air is admitted around the burner shell 16 and preferably twirling movement imparted thereto for effecting complete turbulance, thereby resulting in complete combustion of the lowest grades of fuel oil.
It is to be noted that air may be substituted in lieu of the steam for this purpose, and any number of such expedients may be resorted to as commercial practice may dictate for any particular installation.
Various changes may be made in the embodiment of the invention herein specifically described without departing from or sacrificing any of the advantages of the invention as defined in the appended claims.
Having thus described my invention, what I claim as new and desire to secure by Letters Patent is:
1. In a burner sprayer of the character described, a member forming a Venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member having an enlarged chamber at the front of said throat, an atomizing medium inlet arranged axially of the Venturi immediately to the rear of the liquid inlets, said atomizing inlet having a diameter less than the diameter of the Venturi throat. r
2. In a burner sprayer of the character described, a member forming a .venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member. having an enlarged chamber at the front of said throat, an atomizing medium inlet arranged axially of the Venturi-immediately to the rear of the liquid inlets, said atomizing inlet having a diameter'less than the diameter of the Venturi throat, and an impeller disposed transversely of said enlarged chamber to impart atwirling movement tothe mixture issuing therethrough. Y i
3. In a burner sprayer of the character described, a member forming a Venturi, radial liquid inlets immediately to the rear of the Venturi throat, said member having. an enlarged 115 chamber at the front of said throat, an atomizing medium inlet arranged axially of the venturi immediately to the rear of the liquid inlets, said atomizing inlet having a diameter less than the diameter of the Venturi throat, an impeller disposed transversely of said enlarged chamber to impart a twirling movement to the mixture issuing therethrough, and an apertured cap detachably associated with said enlarged chamber for directing the discharge of the mixture therefrom. r
4. In a burner sprayer ofthe character described,an enlarged chamber having a reduced axial throat at one end thereof, radial liquid fuel inlets provided in said throat immediately to'the' rear of said enlarged chamber, an .atomizing medium inlet arranged axially of said throat'im- 'mediately to the rear of said liquid fuel'inlets,
the diameter of said throat, and an impeller disc disposed transversely of said enlarged chamber proximate to the discharge end thereof to impart a twirling movement to the mixture issuing therethrough. I
6. .In aburner sprayer of the'character described, an enlarged chamber having areduced axial throat at one end thereof, radial liquid fuel inlets provided in said throat immediately to the rear of said enlarged chamber, an atomizing medium inlet arranged axially of said throat improximate to the discharge end thereof to impart a twirling movement to the mixture issuing therethrough, and an apertured discharge cap in threaded engagement with said chamber to maintain said impeller disc in position and direct the discharge from said chamber.
FRED E. RUDOLPH.
US536337A 1931-05-11 1931-05-11 Oil burner Expired - Lifetime US1934379A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3519259A (en) * 1968-05-06 1970-07-07 Union Carbide Corp Furnace jet devices
US3534948A (en) * 1966-08-24 1970-10-20 Exxon Research Engineering Co Lance heads
US4367514A (en) * 1980-09-29 1983-01-04 The Boeing Company Recessed lighting system
EP0744999A1 (en) * 1994-12-30 1996-12-04 Lab S.A. Dual fluid spray nozzle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3534948A (en) * 1966-08-24 1970-10-20 Exxon Research Engineering Co Lance heads
US3519259A (en) * 1968-05-06 1970-07-07 Union Carbide Corp Furnace jet devices
US4367514A (en) * 1980-09-29 1983-01-04 The Boeing Company Recessed lighting system
EP0744999A1 (en) * 1994-12-30 1996-12-04 Lab S.A. Dual fluid spray nozzle
EP0744999A4 (en) * 1994-12-30 1998-05-13 Lab Sa Dual fluid spray nozzle

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