US1745329A - Burner nozzle - Google Patents

Burner nozzle Download PDF

Info

Publication number
US1745329A
US1745329A US185616A US18561627A US1745329A US 1745329 A US1745329 A US 1745329A US 185616 A US185616 A US 185616A US 18561627 A US18561627 A US 18561627A US 1745329 A US1745329 A US 1745329A
Authority
US
United States
Prior art keywords
air
passage
oil
nozzle
fuel
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
US185616A
Inventor
Forrester L Hammer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US185616A priority Critical patent/US1745329A/en
Application granted granted Critical
Publication of US1745329A publication Critical patent/US1745329A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/40Mixing tubes or chambers; Burner heads
    • 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
    • F23D11/001Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space spraying nozzle combined with forced draft fan in one unit

Definitions

  • This invention relates to oil burners, and more especially tothat part of an oil burn# ing system which may be termed the burner proper, and which comprises the means for atomizing the liquid fuel and mixin a quantity of air, for the purpose o obtaining substantially complete combustion of the fuel.
  • the burner proper which comprises the means for atomizing the liquid fuel and mixin a quantity of air, for the purpose o obtaining substantially complete combustion of the fuel.
  • liquid fuel or oil is first atomized by the im- 4. l pinging on a stream of air under a certain amount of pressure. During the atomizing process, this air is, of course, mixed with the oil and itself serves in part to support the combustion of the fuel, although as shown in the drawings, the atomizedoil is thereafter mixed with a quantity of what may be termed volume air or air under a low pressure, in order to supplyT the necessary amount of oxygen to assure substantially complete combustion of the fuel.
  • volume air or air under a low pressure in order to supplyT the necessary amount of oxygen to assure substantially complete combustion of the fuel.
  • One object of my invention is to provide a more eilicient'oil burner than has been used heretofore. 4
  • Another object of my invention is to provide a burner wherein the atomized fuel and air is discharged therefrom in a rapidly spreading j et rather than in a straight stream which might be vdirected against the wall 3o of the furnace and result in uneven distribution of heat.
  • Another object of my invention is to provide an eiiicientoil burner of a type that may be used' economically in household furnaces.
  • a still further object of my invention is ,y the provision of an oil burner wherein the atomizing of the oil may be accomplished by a stream of air under a relatively low pressure.
  • burner nozzle embodying my invention, the wall of the burner housing being shown in section to expose the interior parts:
  • Fig. 3 is a sectional view on line 3-3 of Fig. 2; n ⁇ ig. 4 is a transverse sectional view on line 4-4 of Fig. 2;
  • Fig. 5 is arear face view of the diverter surrounding the atomizing nozzle
  • Fig. 6 is a side view of the same
  • FIG. 7 is a' sectional view on line VV7--7 of 'lo illustrate a preferred embodiment of my invention, I have shown a burner housing 10, the interior of which is in communicav tionwith the outlet 11 of a fan 12.
  • the fan may be of any preferred type, and it isv not considered necessary to show the details thereof in this application.
  • This fan is what may be termed the volume air fan and is designed to blow a considerable quantity of air through the interior of the housing 10 to support the combustion of the atomized oil.
  • the 7 interior of the housing is hollow for this purpose, and within this housing is supported the atomizing nozzle and its associated arts.
  • the wall of the housing 10 is provid with Ja recess 13 from which leads a pipe 14, de signed to deliver the pressure or* atomizing air to the burner.
  • the inlet end 15 of this pipe extends in the recess 13 and through an opening in this recess for connection with the outlet of a suitable air fan or blower (not shown), designed to deliver air atthe required pressure.
  • a suitable air fan or blower (not shown), designed to deliver air atthe required pressure.
  • To the forward end of the pipe 14 is ⁇ detachably connected a second pipe 16, the interior of which is in communication with the interior of the pipe 14.
  • the delivery end of the pipe 16. is threaded for engagement with the threaded socket 17 at the rear end of the atomizing nozzle 18.
  • the nozzlebody ⁇ is provided adjacent Fig. 1 is a sidel elevational view of an oil ⁇ its ⁇ forward end with a plurality of offset or stepped portionsQO, 21, 22 and 23, for a purpose hereinafter described. These portions, it will be understood, are annular in shape and extend entirely around the burner body, thepart 23 being threaded in order 1,00
  • a longitudinal oil assage or bore 24 is arranged in the nozzge which, at its inlet end, communicates with a threaded socket 25 to which may bel connected the oil pipe 26 leading from a source of fuel oil.
  • the oil passage 24 leads through the shoulder 26 between the stepped portions 20 and 21 of the nozzle.
  • An inner cap 27 is designed to be slipped upon the end of the nozzle body 18, this cap having a rear skirt portion 28, adapted to it closely upon the portion 21 of the nozzle and the rear end of which is adapted to lodge against the shoulder 29.
  • the skirt portion 28 is somewhat longer than the part 21 of the nozzle, so as to provide in front of the shoulder 26 an annular oil chamber 30 in communication with the oil inlet passage 24.
  • the inner diameter of the front portion 31 of the inner tip is slightly larger than the front portion 20 of the burner nozzle, so as to leave therebetween an annular oil passage 32.
  • the front end ofthe burner nozzle is beveled, as shown at 33, and the adjacent inner surface 34 of the inner tip is complementally beveled so that the delivery end of the passage between these parts is directed inwardly or toward the longitudinal axis of the nozzle and of the air passage 19. At its forward end, the tip is provlded with an.
  • opening 35 in line with and substantially the same size as the opening at the forward end of the air passa e 19.
  • An outer cap mem er or shell 36 is designed to be telescoped over the nozzle and over the inner cap member, and at itsrear end is providedwith internal threads 37 to engage the threads 23 on the nozzle member.
  • An outer cap mem er or shell 36 is designed to be telescoped over the nozzle and over the inner cap member, and at itsrear end is providedwith internal threads 37 to engage the threads 23 on the nozzle member.
  • For a considerable distance forwardly of the threaded end of the outer ca it is substantially cylindrical in shape and) of such a size as to leave an annular air passage 38 between its wall and the outer wall of the burner nozzle and the skirt portion 28 of the inner cap.
  • Forwardly of this rear cylindrical portion the wall of the outer cap or shell, is displaced inwardly, as shown at 39, to follow the shape of the inner cap, the latterl being provi ed with two or more lugs 39 against which the part 39 of the outer cap bears to hold the inner capin place.
  • the outer cap is larger than the inner ca so that the air passage 38 is continued etween these two members, which are of substantially the same shape throughout their lengths, the air from the passage 38 being delivered through the annular outlet 40 in a direction toward the axis of the burner, and just forwardly of the oil delivery outlet. At its extreme forward end, an opening 41 is provided in the outer cap.
  • openings 42 and 43 are provided between the longitudinal air passage 19 yand the annular air passage .38, so that a part ofthe air entering the passage 17 is diverted into the annular passage 38 to be delivered through the air outlet 40 between the inner and outer caps.
  • a web 44 extends across the passage 19, and is provided with an opening 45 to receive the stem 46 of an air tip 47, located at the mouth of the nozzle.
  • the stem 46 is provided with an enlarged collar 48, designed to be lodged against the forward end of the web 44, and a nut 49 threaded upon the rear end of the stem is designed to draw this collar in tight engagement with the web and hold the tip in place.
  • the Aside of this tip toward the burner is of conical shape, so as to cause the air and fuel impinging thereagainst to be deflected in an outward direction away from the longitudinal axis of the burner.
  • a number of openings 50 extend through the tip 47 in a direction longitudinally of the burner, so asv to permit part of the air from the passage 19 to pass therethrough.
  • the stem 52 'ofjan air'spreader 53 Threaded into the stem 46 of the tip, as shown at 5l, is the stem 52 'ofjan air'spreader 53, against which theair passing through the openings 50, is designed to impinge and be deflected ina direction transverse to the longitudinal axis of the nozzle.
  • This spreader is a substantially flat disk shaped member, and is spaced forwardly of the tip 47 so that the openings 50 will not be closed.
  • the air passing through these openings strikes the rear face of the spreader and is "defleeted in a lateral direction and caused to enter the stream of atomized vfuel in this dinection, so as to spread out this stream lateral y and prevent it.I from issuing from the' mouth of the nozzle in a narrow axially dir cted stream. Also, as it is directed th ough the atmozied oil, so to speak, it tends to urther break up and atomize the fuel.
  • an externalsh 1- de 54 which as lShown in Fig. 2, at the l was portion of the nozzle, substantially closes t e annular oil passage 32 so as to shut off c mmunication between this passage and the oi; ⁇ chamber 3(1).k shoulder 54 gradually diminishes toward the upper part of the nozzle until it merges into the wall 20, leaving the passage 32 at the upper slide of the burner entirely clear. This resultsin forcing the oil in its passage from the cha iber 30 to rise to the upper side of this lchagilber before itcan enter freely into the pas ge 32, so'that the last named passage As shown in ',Fig. 4, the
  • an air dctlector or diverter 55 Upon the outside of the outer cap 36 is placed an air dctlector or diverter 55, which is enclosed within a. cylindrical sleeve 56, open at its rear end and having a flaring mouth 57. 'Ihe air diverter 55 is provided p with a central opening within which the outer the housing.
  • This spray is also mixed with additional air issuing rom the passages 58 and-59 between the sleeve 56 and the wall of the housing 10, which air is directed inwardly toward the mixed fuel and air coming from the sleeve 56, by the inturned lips 60 and 61 of it becomes thoroughly mixed
  • the lower ⁇ inturned lip 61 provides a well 62 to receive from the pipe 63 any oil leakage which might occur and any oil caught by this well is consumed by the flame at the burner nozzle.
  • the pipe 63 leadsto the bed of the machine (not shown).
  • the operation of my device may be briefly described as follows.
  • the oil'pipe 26 is connected to a source of oil, which is preferably under no greater pressure than just a sufficient amount to deliver 1t at the burner tip.
  • This pressure may be obtained by gravity from the position ofthe oil'tank or other source of supply.
  • This oil passes through the passage 24 and into the chamber 30, where coming into contact with the shoulf'n-.r 54 it is caused to spread upwardly to fill the chamber 30, so as to pass into the upper part of the annular oil delivery passage 32, and be delivered at the mouth of this passage in an ⁇ annular stream directed inwardly toward the axis of the burner.
  • Air under a certain amount of pressure isjsupplied through the air tube 16, to the passage 19.
  • This com ined air and oil stream then passes forwardly, where it is deflected by the tip 47 in an outward direction to pass through the opening 41.
  • pressure air issuing from the mouth 40 of the outer air passage is delivered peripherally into and across this stream of 011 and air, so as to further break up the oil particles and effect a further atomization.
  • partially mixed oil and air issues through the openings 50 in the tip 47 to impinge against the rear surface of the spreader 53 and be defleet-ed outwardly across the atomized oil issuing fromV the opening 41. This' further breaks up the oil particles and completes the l atomization thereof, and at the same time, prevent its being projected from the nozzle inl an axially directed jet.
  • This spreading vjet of atomized fuel is then attacked by the whirling volume air passing through the diverter 55, within the sleeve 56.
  • This volume air is delivered into the housing 1() bythe fan 12, and is preferably under a very low pressure, say two to four ounces, or a pressure just sullicient to deliver the proper volume of air to support the combustion of the fuel.
  • This whirling, spreading spray of atomized oil andair is then thrown into theA furnace after being mixed with additional volume air issuing from the passages 58 and 59, when it will be in condition to be eiliciently and completely burned.
  • This ele- ⁇ loo ment comprises a central sleeve or collar 55a Y which is adapted to fit upon and embrace the outer cap member or shell 36 of the atomizing nozzle, collar and extending forwardly therefrom are spaced vanes 55b of spiral shape.
  • the vanes Viewed from the rear side thereof the vanes present air cups or pockets 55, which receive the volume 4air from' ⁇ the fan, 12 and deflect it spirally through the spaces 55d, between the vanes in a whirling movement.
  • Recesses 55e may be provided intwo of the vanes to allow the spark members 65 to project therethrough adjacent the front end of the atomizing nozzle. It willbe apparent that the volume air passing in the sleeve 56 will be caught Within the pockets 55 and be given a whirling moveas shown in Fig. 1. Attached to thisl ment as it passes through the diverter for the purpose already set forth.
  • the oil may be atomized with air at a very low pressure, as in the p resent burner, and also when the volume air is furnished at a very low pressure, the char e of mixed fuel and air is thrown into the urnace with a low velocity so that it may spread out quickly in all directions and not bethrown against the back of the furnace.
  • a liquid fuel burner nozzle a fuel chamber, a fuel passage leading into the chamber at lthe lower end thereof, an annular passage leading from said chamber, and an l abutment at the entrance of said last named passage to restrict the lower portion thereof to cause the fuel in said chamber to rise toi ward the top thereof before being admitted sesV to said annular passa e. ⁇ v
  • a fuel chamber means to sup ly fuel thereto, an annular passagefleading fiom the chamber, and a shoulder l formed o n the' wall of the passage and projecting thereinto to substantially close the same at the lower'sidethereof, and merging in'to the wall of the passage toward the up per side thereof.
  • an atomizing nozzle having an air passage to direct a stream of air longitudinally of the burner, a second air passage, means to direct a stream of air 'communication therefrom across the first air stream, at a point in advance of the outlet of the first passage, and means to deliver a supply of fuel between said air streams, and means to deliver a'supply of air with a whirling motion about the nozzle into the atomized fuel.
  • an atomizing nozzle having an air passage adapted to deliver an air stream longitudinally 'of the burner, a'fuel passage adapted to direct a jet of fuel across the outlet of said air passage, and a second air passage beyond the fuel passage and adapted to direct a jet of air across the stream of mixed air and fuel.
  • means providing a longitudinally disposed air passage having an open mouth
  • means providing a'fuel passage to deliver a jet of' fuel inwardly across the air stream issuing from said passage, and peripherally about the same, and a second air passage beyond the fuel passage and adapted to deliver a. stream of air across the jet of air and fuel from the first two passages, and peripherally about the same, and a tip arranged forwardly of said passages against which the air and oil is directed, said tip being provided with openings through which the mixed air and fuel passes, and a spreader member to deflect the air and fuel passing through said openings in a lateral direction.
  • An oil burner comprising a nozzle body having a longitudinal air opening therein, an annular oil passage surrounding said air pas ⁇ sage, an annular air passage surrounding said oil passage, means affording communication between said longitudinal air passage and said annular air passage, both of said annular passages and said longitudinal passage havmg delivery openings adjacent the front end of the nozzle body, a tip adjacent the outlet of said openings and being itself provided with axially directed openings, and a spreader member infront of the tip to deflect in a lateral direction the oil and air passing through the tip openings.
  • An atomizing nozzle for liquid fuel burners comprising a nozzle body having a longitudinal opening therethrough, a cap positioned telescopic'ally on said body and spaced therefrom to provide an annular passage therebetween, a second cap supported on said body and positioned about the first cap and spaced therefrom to provide a second annular passage between the caps, and limiting members between the first and second caps to secure them in properly spaced relation, and said annular passages having outlets in with the longitudinal passage.
  • An atomizing nozzle comprising a body member having a longitudinal passage therein, an outer cap received upon and supported by said body and spaced therefrom to leave an annular passage therebetween, an inner cap telescopically secured upon said bodywithin said annular passage and spaced bo from the wall of the body and from the outer cap to leave annular passages therebetween, and means affording communication between the longitudinal passage in the body and the annular passage between'the caps.
  • An atomizing nozzle comprising a body W member having a longitudinal passage therein', an outer cap received upon and supported by said body and spaced therefrom to leave an annular passage therebetween, an inner cap telescopleallv secured upon said body within said annular passage and spaced both from the wall of the body and Jfrom the outer cap to leave annular passages therebetween,

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Description

Jan. 28, 1930.
F. L. HAMMER `BURNER NOZZLE Filed April 21. 1927 2 Sheets-Sheet l v A., H 0
. 8 e .l 7 6 W 1 1 J 5 l i 2 0 2 nQ/UN 49 ll/ s ,4 l C 4 1. a@ m f e2 M a, u WW 2 6 im M 4 AIU. M uw .wo ma. M J 0 WJ :D 3 o 1U 2 M EW F ww 6 5 A. w -5 m fon /v www u w v N Z .I 7 O mbv lo 3 5 l 3 3 u. o YU u .M uw 3 Patented Jan. 28 1930 PATENT OFFICE FORRESTEB L. HAMMER, F BRANFOBD, CONNECTICUT BURNER NOZZLE Application iled April 21,
This invention relates to oil burners, and more especially tothat part of an oil burn# ing system which may be termed the burner proper, and which comprises the means for atomizing the liquid fuel and mixin a quantity of air, for the purpose o obtaining substantially complete combustion of the fuel. In the preferred formof my invention which I have illustrated in the drawings, the
liquid fuel or oil is first atomized by the im- 4. l pinging on a stream of air under a certain amount of pressure. During the atomizing process, this air is, of course, mixed with the oil and itself serves in part to support the combustion of the fuel, although as shown in the drawings, the atomizedoil is thereafter mixed with a quantity of what may be termed volume air or air under a low pressure, in order to supplyT the necessary amount of oxygen to assure substantially complete combustion of the fuel.` j
One object of my invention is to provide a more eilicient'oil burner than has been used heretofore. 4
Another object of my invention is to provide a burner wherein the atomized fuel and air is discharged therefrom in a rapidly spreading j et rather than in a straight stream which might be vdirected against the wall 3o of the furnace and result in uneven distribution of heat.
Another object of my invention is to provide an eiiicientoil burner of a type that may be used' economically in household furnaces.
A still further object of my invention is ,y the provision of an oil burner wherein the atomizing of the oil may be accomplished by a stream of air under a relatively low pressure. Y
To these and other ends, the invention consists in the novel features and combinations of parts to be hereinafter described and claimed; i,
In th`e accompanying drawings:
burner nozzle embodying my invention, the wall of the burner housing being shown in section to expose the interior parts:
2 is a sectional view through the atomizing nozzle;
it withv 1927. Serial N0. 185,616.
' Fig. 3 is a sectional view on line 3-3 of Fig. 2; n `ig. 4 is a transverse sectional view on line 4-4 of Fig. 2;
Fig. 5 is arear face view of the diverter surrounding the atomizing nozzle;
Fig. 6 is a side view of the same;
7 is a' sectional view on line VV7--7 of 'lo illustrate a preferred embodiment of my invention, I have shown a burner housing 10, the interior of which is in communicav tionwith the outlet 11 of a fan 12. The fan may be of any preferred type, and it isv not considered necessary to show the details thereof in this application. This fan is what may be termed the volume air fan and is designed to blow a considerable quantity of air through the interior of the housing 10 to support the combustion of the atomized oil. The 7 interior of the housing is hollow for this purpose, and within this housing is supported the atomizing nozzle and its associated arts. The wall of the housing 10 is provid with Ja recess 13 from which leads a pipe 14, de signed to deliver the pressure or* atomizing air to the burner. The inlet end 15 of this pipe extends in the recess 13 and through an opening in this recess for connection with the outlet of a suitable air fan or blower (not shown), designed to deliver air atthe required pressure. To the forward end of the pipe 14 is `detachably connected a second pipe 16, the interior of which is in communication with the interior of the pipe 14. The delivery end of the pipe 16. is threaded for engagement with the threaded socket 17 at the rear end of the atomizing nozzle 18.
This atomizing nozzle i-s shown in section in Fig. 2, and comprises a nozzle body having a longitudinal opening 19 extending entirely through the body and'communic ating at its'rear end withthe threaded opening 17. f The nozzlebody` is provided adjacent Fig. 1 is a sidel elevational view of an oil` its `forward end with a plurality of offset or stepped portionsQO, 21, 22 and 23, for a purpose hereinafter described. These portions, it will be understood, are annular in shape and extend entirely around the burner body, thepart 23 being threaded in order 1,00
' on. Below the air to secure the other parts of the nozzle therepassage 19, a longitudinal oil assage or bore 24 is arranged in the nozzge which, at its inlet end, communicates with a threaded socket 25 to which may bel connected the oil pipe 26 leading from a source of fuel oil. At its forward end, the oil passage 24 leads through the shoulder 26 between the stepped portions 20 and 21 of the nozzle.
An inner cap 27 is designed to be slipped upon the end of the nozzle body 18, this cap having a rear skirt portion 28, adapted to it closely upon the portion 21 of the nozzle and the rear end of which is adapted to lodge against the shoulder 29. The skirt portion 28 is somewhat longer than the part 21 of the nozzle, so as to provide in front of the shoulder 26 an annular oil chamber 30 in communication with the oil inlet passage 24. The inner diameter of the front portion 31 of the inner tip is slightly larger than the front portion 20 of the burner nozzle, so as to leave therebetween an annular oil passage 32. The front end ofthe burner nozzle is beveled, as shown at 33, and the adjacent inner surface 34 of the inner tip is complementally beveled so that the delivery end of the passage between these parts is directed inwardly or toward the longitudinal axis of the nozzle and of the air passage 19. At its forward end, the tip is provlded with an.
opening 35 in line with and substantially the same size as the opening at the forward end of the air passa e 19.
An outer cap mem er or shell 36 is designed to be telescoped over the nozzle and over the inner cap member, and at itsrear end is providedwith internal threads 37 to engage the threads 23 on the nozzle member. For a considerable distance forwardly of the threaded end of the outer ca it is substantially cylindrical in shape and) of such a size as to leave an annular air passage 38 between its wall and the outer wall of the burner nozzle and the skirt portion 28 of the inner cap. Forwardly of this rear cylindrical portion the wall of the outer cap or shell, is displaced inwardly, as shown at 39, to follow the shape of the inner cap, the latterl being provi ed with two or more lugs 39 against which the part 39 of the outer cap bears to hold the inner capin place. It will be ap arent that when the outer cap is threadldd .upon the nozzle, that the three parts of the burner above described, will be securelyheld in assembled relation andat the same time may be very readily dis-assembled if occasion requires. The outer cap is larger than the inner ca so that the air passage 38 is continued etween these two members, which are of substantially the same shape throughout their lengths, the air from the passage 38 being delivered through the annular outlet 40 in a direction toward the axis of the burner, and just forwardly of the oil delivery outlet. At its extreme forward end, an opening 41 is provided in the outer cap.
As shown in Figs. 2 and 3, openings 42 and 43 are provided between the longitudinal air passage 19 yand the annular air passage .38, so that a part ofthe air entering the passage 17 is diverted into the annular passage 38 to be delivered through the air outlet 40 between the inner and outer caps. A web 44 extends across the passage 19, and is provided with an opening 45 to receive the stem 46 of an air tip 47, located at the mouth of the nozzle. The stem 46 is provided with an enlarged collar 48, designed to be lodged against the forward end of the web 44, and a nut 49 threaded upon the rear end of the stem is designed to draw this collar in tight engagement with the web and hold the tip in place.
As clearly shown in Figs. 2 and 3 of the drawing, the Aside of this tip toward the burner is of conical shape, so as to cause the air and fuel impinging thereagainst to be deflected in an outward direction away from the longitudinal axis of the burner. A number of openings 50 extend through the tip 47 in a direction longitudinally of the burner, so asv to permit part of the air from the passage 19 to pass therethrough. Threaded into the stem 46 of the tip, as shown at 5l, is the stem 52 'ofjan air'spreader 53, against which theair passing through the openings 50, is designed to impinge and be deflected ina direction transverse to the longitudinal axis of the nozzle.` This spreader is a substantially flat disk shaped member, and is spaced forwardly of the tip 47 so that the openings 50 will not be closed. At the same time, the air passing through these openings strikes the rear face of the spreader and is "defleeted in a lateral direction and caused to enter the stream of atomized vfuel in this dinection, so as to spread out this stream lateral y and prevent it.I from issuing from the' mouth of the nozzle in a narrow axially dir cted stream. Also, as it is directed th ough the atmozied oil, so to speak, it tends to urther break up and atomize the fuel.
t the rear end of the portion 20 of the bu 'ner nozzle is provided an externalsh 1- de 54, which as lShown in Fig. 2, at the l wer portion of the nozzle, substantially closes t e annular oil passage 32 so as to shut off c mmunication between this passage and the oi;` chamber 3(1).k shoulder 54 gradually diminishes toward the upper part of the nozzle until it merges into the wall 20, leaving the passage 32 at the upper slide of the burner entirely clear. This resultsin forcing the oil in its passage from the cha iber 30 to rise to the upper side of this lchagilber before itcan enter freely into the pas ge 32, so'that the last named passage As shown in ',Fig. 4, the
will be substantially filled with oil, and the latter will be delivered at the mouth of the nozzle aboutthe entire periphery of the air passage 19. In View of the fact that the oil delivery tube 24 is at the lower side of the burner, if it were not for the provision of this shoulder, the upper part of the passage 32 might not receive the proper quantity of oil.
Upon the outside of the outer cap 36 is placed an air dctlector or diverter 55, which is enclosed within a. cylindrical sleeve 56, open at its rear end and having a flaring mouth 57. 'Ihe air diverter 55 is provided p with a central opening within which the outer the housing.
cap is received, and surrounding this opening are a plurality of vanesof spiralshape, so as to give the air passing therethrough, volume air in this instance, a whirling movement. 'lhis aircomes in contact with the atomized fuel, and due to the whirling moveand to the fact the spreader 53, with the fuel, and the entire charge of mixe fuel and air issues from the flaring mouth 57 of the sleeve 56 in a whirling, spreading spray. This spray is also mixed with additional air issuing rom the passages 58 and-59 between the sleeve 56 and the wall of the housing 10, which air is directed inwardly toward the mixed fuel and air coming from the sleeve 56, by the inturned lips 60 and 61 of it becomes thoroughly mixed The lower `inturned lip 61 provides a well 62 to receive from the pipe 63 any oil leakage which might occur and any oil caught by this well is consumed by the flame at the burner nozzle. The pipe 63 leadsto the bed of the machine (not shown).
The operation of my device may be briefly described as follows. The oil'pipe 26 is connected to a source of oil, which is preferably under no greater pressure than just a sufficient amount to deliver 1t at the burner tip.
This pressure may be obtained by gravity from the position ofthe oil'tank or other source of supply. This oil passes through the passage 24 and into the chamber 30, where coming into contact with the shoulf'n-.r 54 it is caused to spread upwardly to fill the chamber 30, so as to pass into the upper part of the annular oil delivery passage 32, and be delivered at the mouth of this passage in an `annular stream directed inwardly toward the axis of the burner. Air under a certain amount of pressure isjsupplied through the air tube 16, to the passage 19. W ith Vthe arrangement I have provided, it is not necessary to use a-high pressure for lthe atomizing air, a pressure of from six ounces to one pound being sufficient, and experience has shown that a pressure of sixounces .producesvery satisfactory results. A part of the 'air in the. passage 19 is diverted through the openings 42 and 43 to the annular passage 38. The red serves to spread the atomized oil to mainder of the air passing through the central passage 19 strikes the oil stream issuing at the mouth of the oil passage, and as this oil stream is directed inwardly across the air stream, the impact of the latter will 'cause the oil stream to be broken up into tine particles, so as to be prepared for thorough atomization. This com ined air and oil stream then passes forwardly, where it is deflected by the tip 47 in an outward direction to pass through the opening 41. At the same time pressure air issuing from the mouth 40 of the outer air passage is delivered peripherally into and across this stream of 011 and air, so as to further break up the oil particles and effect a further atomization. In the meanwhile, partially mixed oil and air issues through the openings 50 in the tip 47 to impinge against the rear surface of the spreader 53 and be defleet-ed outwardly across the atomized oil issuing fromV the opening 41. This' further breaks up the oil particles and completes the l atomization thereof, and at the same time, prevent its being projected from the nozzle inl an axially directed jet. This spreading vjet of atomized fuel is then attacked by the whirling volume air passing through the diverter 55, within the sleeve 56. This volume air is delivered into the housing 1() bythe fan 12, and is preferably under a very low pressure, say two to four ounces, or a pressure just sullicient to deliver the proper volume of air to support the combustion of the fuel. This whirling, spreading spray of atomized oil andair is then thrown into theA furnace after being mixed with additional volume air issuing from the passages 58 and 59, when it will be in condition to be eiliciently and completely burned.
Between the spiral fins of the diverter 55 are passed a pair of spark members 65, only Y one ofwhich is shown, these members being Figs. 5, 6 and 7 of the drawings. This ele-` loo ment comprises a central sleeve or collar 55a Y which is adapted to fit upon and embrace the outer cap member or shell 36 of the atomizing nozzle, collar and extending forwardly therefrom are spaced vanes 55b of spiral shape. Viewed from the rear side thereof the vanes present air cups or pockets 55, which receive the volume 4air from'` the fan, 12 and deflect it spirally through the spaces 55d, between the vanes in a whirling movement.` Recesses 55e may be provided intwo of the vanes to allow the spark members 65 to project therethrough adjacent the front end of the atomizing nozzle. It willbe apparent that the volume air passing in the sleeve 56 will be caught Within the pockets 55 and be given a whirling moveas shown in Fig. 1. Attached to thisl ment as it passes through the diverter for the purpose already set forth.
Under some conditions it has been found that the jet of mixed air and oil issuing within the collar 56 has a tendency to move in an upward direction and this tendency may be counteracted by closin the passage 59 below the collar 56, so that t e air issuing between this collar'and the` housingwill be above the flame or above the issuing jet of air and, oil, and will be directed thereinto in a downward direction. When the lower passage 59 is thus closed off the spray of mixed fuel and air is maintained at a lower point in the furnace, and in some instances, the operation of the burner is improved.
In the case of burners of small sizes, I have foundit sometimes desirable to omit the openings in the tip 47 and use this tip as a spreader for the oil and air, also, of course, omitting. the provision of the spreader 53. In other words, in the case of such burners, if the tip 47 is imperforate it will act to spread the iiame and the tip 53 may be omitted, thus simplifying the construction of the burner without affecting the efliciency thereof. p
It is to be noted that when the oil may be atomized with air at a very low pressure, as in the p resent burner, and also when the volume air is furnished at a very low pressure, the char e of mixed fuel and air is thrown into the urnace with a low velocity so that it may spread out quickly in all directions and not bethrown against the back of the furnace.
While I have shown and described a preferred embodiment of my invention, it wi ll bel understood that it is not to be limited to the details shown, but is capable of modification and variation which will lie within the spirit of the invention and the scope of the appended claims.
lVhat I claim is:
1. In a liquid fuel burner nozzle, a fuel chamber, a fuel passage leading into the chamber at lthe lower end thereof, an annular passage leading from said chamber, and an l abutment at the entrance of said last named passage to restrict the lower portion thereof to cause the fuel in said chamber to rise toi ward the top thereof before being admitted sesV to said annular passa e.` v
2. In a liquid fuel urner, a fuel chamber, means to sup ly fuel thereto, an annular passagefleading fiom the chamber, and a shoulder l formed o n the' wall of the passage and projecting thereinto to substantially close the same at the lower'sidethereof, and merging in'to the wall of the passage toward the up per side thereof.
3. In a liquid fuel burner, an atomizing nozzle having an air passage to direct a stream of air longitudinally of the burner, a second air passage, means to direct a stream of air 'communication therefrom across the first air stream, at a point in advance of the outlet of the first passage, and means to deliver a supply of fuel between said air streams, and means to deliver a'supply of air with a whirling motion about the nozzle into the atomized fuel.
4. In a liquid fuel burner, an atomizing nozzle having an air passage adapted to deliver an air stream longitudinally 'of the burner, a'fuel passage adapted to direct a jet of fuel across the outlet of said air passage, and a second air passage beyond the fuel passage and adapted to direct a jet of air across the stream of mixed air and fuel.
issuing from the first two passages, and means to deliver a supply of air with a whirling motion about the nozzle into the atomized fuel.
5. In a liquid fuel burner, means providing a longitudinally disposed air passage having an open mouth, means providing a'fuel passage to deliver a jet of' fuel inwardly across the air stream issuing from said passage, and peripherally about the same, and a second air passage beyond the fuel passage and adapted to deliver a. stream of air across the jet of air and fuel from the first two passages, and peripherally about the same, and a tip arranged forwardly of said passages against which the air and oil is directed, said tip being provided with openings through which the mixed air and fuel passes, and a spreader member to deflect the air and fuel passing through said openings in a lateral direction.
6. An oil burner, comprising a nozzle body having a longitudinal air opening therein, an annular oil passage surrounding said air pas` sage, an annular air passage surrounding said oil passage, means affording communication between said longitudinal air passage and said annular air passage, both of said annular passages and said longitudinal passage havmg delivery openings adjacent the front end of the nozzle body, a tip adjacent the outlet of said openings and being itself provided with axially directed openings, and a spreader member infront of the tip to deflect in a lateral direction the oil and air passing through the tip openings.
7 An atomizing nozzle for liquid fuel burners. comprising a nozzle body having a longitudinal opening therethrough, a cap positioned telescopic'ally on said body and spaced therefrom to provide an annular passage therebetween, a second cap supported on said body and positioned about the first cap and spaced therefrom to provide a second annular passage between the caps, and limiting members between the first and second caps to secure them in properly spaced relation, and said annular passages having outlets in with the longitudinal passage.
8. An atomizing nozzle, comprising a body member having a longitudinal passage therein, an outer cap received upon and supported by said body and spaced therefrom to leave an annular passage therebetween, an inner cap telescopically secured upon said bodywithin said annular passage and spaced bo from the wall of the body and from the outer cap to leave annular passages therebetween, and means affording communication between the longitudinal passage in the body and the annular passage between'the caps.
9. An atomizing nozzle, comprising a body W member having a longitudinal passage therein', an outer cap received upon and supported by said body and spaced therefrom to leave an annular passage therebetween, an inner cap telescopleallv secured upon said body within said annular passage and spaced both from the wall of the body and Jfrom the outer cap to leave annular passages therebetween,
and means affording communication between the longitudinal passage in the body and the annular passage between the caps, and limiting members positioned on one of the caps and engaging the other thereof to hold them in properly spaced relation.
In witness whereof, I have hereunto set my hand this 19th day of April, 1927.
' FORRESTER L. HAMMER.
US185616A 1927-04-21 1927-04-21 Burner nozzle Expired - Lifetime US1745329A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US185616A US1745329A (en) 1927-04-21 1927-04-21 Burner nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US185616A US1745329A (en) 1927-04-21 1927-04-21 Burner nozzle

Publications (1)

Publication Number Publication Date
US1745329A true US1745329A (en) 1930-01-28

Family

ID=22681725

Family Applications (1)

Application Number Title Priority Date Filing Date
US185616A Expired - Lifetime US1745329A (en) 1927-04-21 1927-04-21 Burner nozzle

Country Status (1)

Country Link
US (1) US1745329A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485244A (en) * 1947-09-26 1949-10-18 Sanborn Systems Inc Atomizing device for oil burners
US2760564A (en) * 1956-08-28 Fuel supply system for oil burners -
US2821976A (en) * 1954-11-29 1958-02-04 James L Fizzell Liquid fuel burner and hood
US3190342A (en) * 1964-02-17 1965-06-22 Hart Heat Inc Dribble vaporizer for an oil burner nozzle
US3376097A (en) * 1964-12-03 1968-04-02 Gulf Research Development Co Oil burning process
US4485968A (en) * 1982-09-07 1984-12-04 Columbia Chase Corporation Boiler nozzle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2760564A (en) * 1956-08-28 Fuel supply system for oil burners -
US2485244A (en) * 1947-09-26 1949-10-18 Sanborn Systems Inc Atomizing device for oil burners
US2821976A (en) * 1954-11-29 1958-02-04 James L Fizzell Liquid fuel burner and hood
US3190342A (en) * 1964-02-17 1965-06-22 Hart Heat Inc Dribble vaporizer for an oil burner nozzle
US3376097A (en) * 1964-12-03 1968-04-02 Gulf Research Development Co Oil burning process
US4485968A (en) * 1982-09-07 1984-12-04 Columbia Chase Corporation Boiler nozzle

Similar Documents

Publication Publication Date Title
US4203717A (en) Flat flame burner assembly
US1462395A (en) Construction of spraying nozzles or atomizers
US1594641A (en) Method of and apparatus for atomizing
US1745329A (en) Burner nozzle
US1817470A (en) Fuel burning apparatus and method
US1587249A (en) Method of and apparatus for burning oil
US2242797A (en) Method of and apparatus for burning fluid fuel
US2931430A (en) Combination oil and gas burner
US2274573A (en) Oil burner
US2111908A (en) Combustion apparatus
US1785802A (en) Atomizing jet nozzle
US1066161A (en) Oil-burner.
US1641017A (en) Liquid-fuel burner
US1428896A (en) Steam-atomizing fuel-oil burner
US1063913A (en) Oil-burner.
US1331376A (en) Oil-burner
US3038530A (en) Flame thrower
GB131175A (en) Improvements in or relating to Fuel Burners or Atomisers.
US2664703A (en) Preheater and vaporizer for gas turbine engines
US1785803A (en) Atomizing mixing nozzle
US2515494A (en) Liquid-fuel burner nozzle construction
US218619A (en) Improvement in hydrocarbon-burners
US2450418A (en) Oil burner
CN108286710A (en) A kind of kerosene oil-gas three uses burner
US710718A (en) Crude-oil burner.