US2214568A - Fuel burner - Google Patents
Fuel burner Download PDFInfo
- Publication number
- US2214568A US2214568A US256919A US25691939A US2214568A US 2214568 A US2214568 A US 2214568A US 256919 A US256919 A US 256919A US 25691939 A US25691939 A US 25691939A US 2214568 A US2214568 A US 2214568A
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- Prior art keywords
- fuel
- burner
- fuels
- cup
- shaft
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- Expired - Lifetime
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- 239000000446 fuel Substances 0.000 title description 82
- 239000007788 liquid Substances 0.000 description 19
- 239000007921 spray Substances 0.000 description 13
- 238000002485 combustion reaction Methods 0.000 description 12
- 208000028659 discharge Diseases 0.000 description 11
- 230000001535 kindling effect Effects 0.000 description 11
- 230000000694 effects Effects 0.000 description 7
- 239000003921 oil Substances 0.000 description 7
- 239000012212 insulator Substances 0.000 description 4
- 241000239290 Araneae Species 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000007599 discharging Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000005192 partition Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/04—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action
Definitions
- This invention relates to fuel burners, and l particularly those capable of burning heavy fuels such as the less expensive hydrocarbon oils.
- Fig. l is a longitudinal section through a burner embodying the features of the present invention.
- Fig. 2 is a cross-section through the burner on the line 2-2 of Fig. 1.
- ⁇ Fig. 3 is a similar section on the line 3--3 o 0f Fig. 1.
- Fig. 4 is a rear elevational view of the burner.
- Fig. 5 is a detail perspective view oi' the parts of the rotary atomizing unit and actuating shaft shown in spaced relation to better illustrate the 5 construction thereof.
- Fig. 6 is a detail perspective view of the burner housing, particularly illustrating the air discharge nozzle.
- I designates a burner constructed in accordance with the present invention. and which inV cludes a housing 2, having a cylindrical body 3 forming a nozzle portion 4 and an air inlet chamber 5 which are separated by a spider-like diau phragm 6.
- the rear end of the air inlet chamber 5 is closed by a wall 'l having an axially arranged bearing housing 8 anda threaded opening 9 for mounting an igniting device Il), hereinafter described.
- the opposite end of the cylindrical body converges toform a central opening II, whereby 5 combustion supporting air passing from the inlet chamber 5 through a series of openings I2 arranged circumferentially of an axial opening I2' in the spider is directed toward the extended axis of the burner and in contact with the fuel as later l0 described.
- the airv is admitted under pressure tangentially of the chamber 5 through an opening I3 in the wall thereof by way of an air supply conduit I4 best shown in Fig. 2.
- an air directing nozzle I5 Supported by the spider-like diaphragm 6, co- 16 axially of the cylindrical body 3, is an air directing nozzle I5, also of cylindrical shape and of smaller diameter than the nozzle portion 4 to provide an annular air passageway I6 connected with the openings I2 in the spider.
- the forward 20 end of the nozzle I5 also converges toward the axis of the burner to form a constricted opening I1.
- the tip of the nozzle I5 projects beyond the nozzle portion of the housing, as shown in Fig. 1.
- the inner circumference of the air directing nozzle I5 is provided with a plurality of spirally arranged air directing fins I8 which extend from 30 the spider 5 to the tip of the nozzle, as clearly shown in Fig. 1.
- a peripheral flange I9 by which it is adapted to be mounted on the wall of a fire-box '20, with 35 the nozzle portion 4 ⁇ projecting through an opening' 2I therein, as shown in Fig. 1.
- the flange I9 is secured tothe fire-box wall by fastening devices, such as cap screws 22, extending through openings 23 in the flange and into threaded openings 24 of the fire-box wall.
- Mounted within ⁇ the bearing housing 8 is a pair of antifriction bearings 25 journalling a shaft 26.
- the shaft 26 has a collar 21 engaged between the inner races 28 of the respective bearings to anchor the shaft 5 against longitudinal movement upon manipulation of adjusting rings 29 and 30, which are threaded into the respective ends of the bearing housing and engage the outer races 3
- a driving pulley 32 whichA is actuated by a belt 33 driven by a suitable prime mover (not shown).
- the rear end of the shaft has a reduced extension 34 rotatably engaged within one 55 Y end of a bore 36 that is formed in a bearing 36 42 retained in sealing relation therewith by a cap nut 43 threadingly engaged with exterior threads on the bearing housing.
- the opposite end of the shaft extends within the nozzle I and is provided with a reduced threaded neck 44 for mounting a rotary atomizing unit 45 whereby the heavy viscous oil discharged through the channel is atomized and delivered into the fire-box in a conical spray, as indicated by the dotted lines 46,
- the vaporizing cup unit constitutes an imporatant part of the present invention as it adapts g5 the burner for operation with a heavy viscous fuel and permits of intermittent or thermostatic control of the burner throughignition of the vaporized heavy oil by the readily combustible fuel, which in turn is ignited by the ignition device I0, previously mentioned.
- the vaporizing unit includes an inner cup 48, including a hub portion 49 having an axially threaded bore 50 engaging the threaded neck of the actuating shaft, and which is provided with an annular recess 5I for engaginglyv receiving the shoulder portion 52 of the shaft, as shown in Fig. 1.
- the threaded portion of the bore terminates short of the inner face of the hub toaccommodate a pilot-like tip 53 on the terminal end of the'shaft, whereby the cup is securely locked on the shaft.
- the cup also includes an outwardly and forwardly aring wall portion 54 for receiving the oilA discharged from the central channel of the shaft and which effects centrifugal feed -of the oil in 1 the form of a conical, swirling spray into the fire-box, as indicated by the dotted line 46, the
- flare and length of the w'all portionof the cup l being such as toattain the desired spread and penetration of the fuel into the fire-box.
- the exterior portion of the hub has ways or grooves 55 for mounting an outer cup 56 thereon.
- the outer cup 56 includes a ring-like body 51, having inwardly directed radial'ribs 58 engaging within the ways 55.
- the inner circumference of the body 51 is of larger diameter than the outer circumference of the hub'49 so as to provide passageways 59 between the ribs 58.r
- the rear end of the body 51 curves inwardly over theshaft to form an annular fuel receiving chamber -or trough 60. through which a readily combustible fuel is discharged through the passageways 59, circumferentially of the inner cup, for centrifugal discharge against the interior aring-wall 6I of the outer cup 56.
- the annular lip 62 of the outer cup terminates Ashort of the lip 63 of the inner cup so that the fuel is discharged therefrom in rearwardly spaced relation with the discharge of the fuel from the inrer cup.r
- the spraysare thus -kept separated upon their initial entry into thev fire-box, so that the readily combustible fuel is ignited and in burning condition prior to contact thereof with the heavy fuel. This is important for the reason that should the fuels become blended prior to ignition of the light fuel, they would be dilcult to ignite by the ignition device and the blend would not burn properly.
- the ignition device I0 includes an insulator 68, carried by a fitting' 69 threaded into the opening 9, similar to a conventional spark plug. 'I'he insulator 68, however. is of sufficient length to project through the length of the burner housing where it terminates in an angular extension ,projecting through the nozzle-like opening of the outer air passageway. Carried within the insulator are electrodes 10 and.1I having the terminal ends thereof projecting from the insulator and forming a spark gap 12. adjacent the outer fuel spray. .
- One of theelectrodes may be grounded to the fitting 69, and the other electrode connected by a conductor 13 with a suitable current supply whereby a spark is caused to occur across the spark gap.
- combustion supporting air is delivered tangentially of the air inlet chamber under suflicient pressure so that it is caused to move in a spiral path through the outer passage.
- the kindling fuel moving in contact with the spark passing across the terminals of the igniting device is readily ignited to effect instantaneous combustion thereof, which in turn ignites the inner spray of less readily combustible fuel, so that the heavy fuel is kept vburning efficiently as long as the fuel valves are open;
- the iiow to the atomizing'cups is suspended to stop operation of the burner.
- the cups may be continually rotated'and the igniting device kept functioning so that when the fuels are again turned on through actuationof the automatic control, th burner is again started.
- a pair ofv coaxial cups having annular fuel discharge lips, means for feeding separate liquid fuels to said cups, means for rotating the cups to eil'ect centrifugal discharge of said fuels from said lips, and means initially igniting one of said fuels to kindle the other of said fuels.
- a pair of coaxial cups having annular fuel discharge lips one set in advance of the other, means for feeding separate liquid fuels to said cups, means forrotating the cups to eect centrifugal discharge of said fuels from said lips, and means initially igniting the fuel discharged from the rearmost lip to kindle the other of said fuels and maintain combustion thereof.
- separate centrifugal atomizing means means for feeding separate liquid fuels tosaid atomizing means for effecting centrifugal discharge of said fuels, means initially igniting one of said fuels to kindle the other of said fuels, and means for supplying combustion supporting air to the burner and having connection with said separate atomizing meansto direct a portion of the combustion supporting air through said atomizing means and between said liquid fuels to prevent ommingling thereof prior to ignition of said kindling fuel.
- a pair of coaxial cups having annular fuel discharge lips, means for feeding separate liquid fuels to said cups, means for rotating the cups to effect centrifugal discharge of said fuels from said lips, means initially igniting one of said fuels to kindle the other of said fuels, and means for discharging spirally converging streams of combustion supporting air around said cups.
- An oil burner including a housing having a nozzle portion, a hollow shaft rotatably'mounted in the housing, an atmoizing cup mounted on said shaft in the nozzle portion of said housing, means connected with the shaft for delivering a liquid fuel to said cup, a second cup mounted coaxially with the first cup, means for delivering a liquid kindling fuel to said second cup, means for rotating the shaft to effect centrifugal dis charge of the liquid fuel from said cups, means associated with the housing for initially igniting said kindling fuel, said cups being relatively supported with respect to each other and the housing to provide passages for combustion supporting air between and around said cups, and means for supplying combustion supporting air to said passages.
- An oil burner including a housing having a spider-like partition dividing the housing into a nozzle portion and an air inlet chamber,'a hollow shaft rotatably mounted in the housing, an atmoizing cup mounted on said shaft, means connected with the shaft for delivering a liquid fuel to said cup, a second cup mounted coaxially with the rst cup, means for delivering a liquid kindling fuel to said second cup, means for rotating the shaft to effect centrifugal discharge of the liquid fuel from said cups, means associated with the housing for initially igniting said kindling fuel, and an air directing nozzle encircling the cups and carried by said spider-like partition to effect discharge of combustion supporting air.
- centrifugal means for respectively discharging a liquid kindling fuel and a less combustible liquid fuel
- means supporting said centrifugal means for rotation about a common axis means for rotating said centrifugal means whereby said liquid fuels are discharged in coaxial conical sprays, and means for separately conveying the liquid fuels to said centrifugal means.
- centrifugal means for respectively discharging a liquid kindling fuel and a less combustible liquid fuel
- means supporting said centrifugal means for rotation about a common axis means for rotating said centrifugal means whereby said liquid fuels are discharged in coaxial conical sprays
- means for separately conveying the liquid fuels to said centrifugal means ignition means, and means supporting the ignition means in the zone of combustion of said kindling fuel spray.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Description
Sept. l0, 1940. F. s. THOMAS 2,214,568
FUEL BURNER Filed Feb. 17, 1939 2 Sheets-Sheet l SePtf 10, 1940. F. s, THOMAS 2,214,568
FUEL BURNER Filed Feb. 17, `1939 2 Sheets-Sheet'l 2 INVENTOR fra/M ,7770/7/05 BY nl M @mgm I A TOR'NEY Patented Sept. 10, 1940 UNITED "STATES FUEL BURNER Frank S. Thomas, Topeka, Kans., assignor of onehalf to Fred P, Martin, Topeka, Kans.,
Application February 171, 1939, Serial No. 256,919
8 Claims.
This invention relates to fuel burners, and l particularly those capable of burning heavy fuels such as the less expensive hydrocarbon oils.
It is well known that fuels of this character are economical and have a high B. t. u. content but their viscous character renders them dilcult to regulate and they willv not ignite readily. They are, therefore, not adapted for use in intermittently operated burners, or burners under automatic or thermostatic control.
It is, therefore, a principal object of the present invention to provide a burner constructed to operate efficiently usingl the less expensive viscous fuels, and which is adapted for automatic control responsive to variable heating requirements.
Other objects of the invention are to` provide a burner constructed with passageways that are not subject to clogging incidental to the use of heavy fuels; to provide a burner capable of .ac-
curate regulation of the fuel consumption proportionate to the heat desired; to provide a burner construction wherein the heavy fuel is discharged in a conical spray concentricaliy with a readily vaporizable fuel spray; and to provide a construction which insures ignition of the read ily vaporizable fuelprior to contact with the heavy fuel.
In accomplishing these and other objects of the invention, as hereinafter pointed out, I have provided improved details of structure, the preferred form of which is illustrated in the accompanying drawings, wherein: f
Fig. l is a longitudinal section through a burner embodying the features of the present invention.
Fig. 2 is a cross-section through the burner on the line 2-2 of Fig. 1.
` Fig. 3 is a similar section on the line 3--3 o 0f Fig. 1.
Fig. 4 is a rear elevational view of the burner.
Fig. 5 is a detail perspective view oi' the parts of the rotary atomizing unit and actuating shaft shown in spaced relation to better illustrate the 5 construction thereof.
Fig. 6 is a detail perspective view of the burner housing, particularly illustrating the air discharge nozzle.
Referring more in detail to the drawings:
I designates a burner constructed in accordance with the present invention. and which inV cludes a housing 2, having a cylindrical body 3 forming a nozzle portion 4 and an air inlet chamber 5 which are separated by a spider-like diau phragm 6. The rear end of the air inlet chamber 5 is closed by a wall 'l having an axially arranged bearing housing 8 anda threaded opening 9 for mounting an igniting device Il), hereinafter described. The opposite end of the cylindrical body converges toform a central opening II, whereby 5 combustion supporting air passing from the inlet chamber 5 through a series of openings I2 arranged circumferentially of an axial opening I2' in the spider is directed toward the extended axis of the burner and in contact with the fuel as later l0 described. The airv is admitted under pressure tangentially of the chamber 5 through an opening I3 in the wall thereof by way of an air supply conduit I4 best shown in Fig. 2.
Supported by the spider-like diaphragm 6, co- 16 axially of the cylindrical body 3, is an air directing nozzle I5, also of cylindrical shape and of smaller diameter than the nozzle portion 4 to provide an annular air passageway I6 connected with the openings I2 in the spider. The forward 20 end of the nozzle I5 also converges toward the axis of the burner to form a constricted opening I1. The tip of the nozzle I5 projects beyond the nozzle portion of the housing, as shown in Fig. 1.
In order to assure spiral movement of the air so 25 as to effect thorough mixture with the atomized fuel and complete penetration of the flame, the inner circumference of the air directing nozzle I5 is provided with a plurality of spirally arranged air directing fins I8 which extend from 30 the spider 5 to the tip of the nozzle, as clearly shown in Fig. 1.
'I'he burner housing thus described is provided with a peripheral flange I9 by which it is adapted to be mounted on the wall of a fire-box '20, with 35 the nozzle portion 4`projecting through an opening' 2I therein, as shown in Fig. 1. The flange I9 is secured tothe lire-box wall by fastening devices, such as cap screws 22, extending through openings 23 in the flange and into threaded openings 24 of the fire-box wall. Mounted within` the bearing housing 8 is a pair of antifriction bearings 25 journalling a shaft 26. The shaft 26 has a collar 21 engaged between the inner races 28 of the respective bearings to anchor the shaft 5 against longitudinal movement upon manipulation of adjusting rings 29 and 30, which are threaded into the respective ends of the bearing housing and engage the outer races 3| of the bearings. I'he rear end of the shaft projects 50 from the bearing housing a sufficient distance to mount a driving pulley 32, whichA is actuated by a belt 33 driven by a suitable prime mover (not shown). The rear end of the shaft has a reduced extension 34 rotatably engaged within one 55 Y end of a bore 36 that is formed in a bearing 36 42 retained in sealing relation therewith by a cap nut 43 threadingly engaged with exterior threads on the bearing housing. The opposite end of the shaft extends within the nozzle I and is provided with a reduced threaded neck 44 for mounting a rotary atomizing unit 45 whereby the heavy viscous oil discharged through the channel is atomized and delivered into the fire-box in a conical spray, as indicated by the dotted lines 46,
and whereby an igniting fuel is discharged in a similar conical spray circumferentially of the spray 46, as indicated by the dotted line 41.
The vaporizing cup unit constitutes an imporatant part of the present invention as it adapts g5 the burner for operation with a heavy viscous fuel and permits of intermittent or thermostatic control of the burner throughignition of the vaporized heavy oil by the readily combustible fuel, which in turn is ignited by the ignition device I0, previously mentioned. -The vaporizing unit includes an inner cup 48, including a hub portion 49 having an axially threaded bore 50 engaging the threaded neck of the actuating shaft, and which is provided with an annular recess 5I for engaginglyv receiving the shoulder portion 52 of the shaft, as shown in Fig. 1. The threaded portion of the bore terminates short of the inner face of the hub toaccommodate a pilot-like tip 53 on the terminal end of the'shaft, whereby the cup is securely locked on the shaft. The cup also includes an outwardly and forwardly aring wall portion 54 for receiving the oilA discharged from the central channel of the shaft and which effects centrifugal feed -of the oil in 1 the form of a conical, swirling spray into the fire-box, as indicated by the dotted line 46, the
flare and length of the w'all portionof the cup l being such as toattain the desired spread and penetration of the fuel into the fire-box.
The exterior portion of the hub has ways or grooves 55 for mounting an outer cup 56 thereon. The outer cup 56 includes a ring-like body 51, having inwardly directed radial'ribs 58 engaging within the ways 55. The inner circumference of the body 51 is of larger diameter than the outer circumference of the hub'49 so as to provide passageways 59 between the ribs 58.r The rear end of the body 51 curves inwardly over theshaft to form an annular fuel receiving chamber -or trough 60. through which a readily combustible fuel is discharged through the passageways 59, circumferentially of the inner cup, for centrifugal discharge against the interior aring-wall 6I of the outer cup 56. The annular lip 62 of the outer cup terminates Ashort of the lip 63 of the inner cup so that the fuel is discharged therefrom in rearwardly spaced relation with the discharge of the fuel from the inrer cup.r The spraysare thus -kept separated upon their initial entry into thev fire-box, so that the readily combustible fuel is ignited and in burning condition prior to contact thereof with the heavy fuel. This is important for the reason that should the fuels become blended prior to ignition of the light fuel, they would be dilcult to ignite by the ignition device and the blend would not burn properly. l
The readily combustible or delivered by way of a pipe 64, extending through an opening 66 in the bottom of the air inlet chamber to a point adjacent the shaft where it terminates in a lateral spout 66 projecting through the opening 61 that is formed between the shaft and the inwardly curved portion of the outer cup.
The ignition device I0 includes an insulator 68, carried by a fitting' 69 threaded into the opening 9, similar to a conventional spark plug. 'I'he insulator 68, however. is of sufficient length to project through the length of the burner housing where it terminates in an angular extension ,projecting through the nozzle-like opening of the outer air passageway. Carried within the insulator are electrodes 10 and.1I having the terminal ends thereof projecting from the insulator and forming a spark gap 12. adjacent the outer fuel spray. .One of theelectrodes may be grounded to the fitting 69, and the other electrode connected by a conductor 13 with a suitable current supply whereby a spark is caused to occur across the spark gap.
In operating a burner constructed and assembled as described, combustion supporting air is delivered tangentially of the air inlet chamber under suflicient pressure so that it is caused to move in a spiral path through the outer passage.
way I6, and in a similar path through the inner passageway circumferentially of the cups by aid of the spirally arranged vanes I8. Primary air is simultaneously delivered to the atomizing cup 56 through the opening 61 for mixture with the ,kindling fuel. The kindling fuel is delivered through thepipe 64, vand the heavy fuel is-delivered through the pipe 40 under control of them outwardly at high velocity and discharges them in atomized form from the lips of the cups, as indicated by the dotted lines 46 and 41. The kindling fuel moving in contact with the spark passing across the terminals of the igniting device, is readily ignited to effect instantaneous combustion thereof, which in turn ignites the inner spray of less readily combustible fuel, so that the heavy fuel is kept vburning efficiently as long as the fuel valves are open; When the fuel is shut o, the iiow to the atomizing'cups is suspended to stop operation of the burner. The cups may be continually rotated'and the igniting device kept functioning so that when the fuels are again turned on through actuationof the automatic control, th burner is again started.
It is thus appaxelt that. I have provided a burner which is capa le of automatic control and intermittent operation, and which is adapted to use the heavy, inexpensive fuels. The amount of light fuel required is relatively small in that it is only used tokindle and maintain combustion of the heavy fuel. The coaxial arrangement of kin'dnng fuel n the sprays, with the heavy fuel forming the inner spray, assures instantaneous ignition of the heavy fuel with a minimum amount of the lighter fuel.
What I claim and desire to secure by Letters Patent is:
1. In a burner of the character described, a pair ofv coaxial cups having annular fuel discharge lips, means for feeding separate liquid fuels to said cups, means for rotating the cups to eil'ect centrifugal discharge of said fuels from said lips, and means initially igniting one of said fuels to kindle the other of said fuels.
2. In an oil burner of the character described, a pair of coaxial cups having annular fuel discharge lips one set in advance of the other, means for feeding separate liquid fuels to said cups, means forrotating the cups to eect centrifugal discharge of said fuels from said lips, and means initially igniting the fuel discharged from the rearmost lip to kindle the other of said fuels and maintain combustion thereof.
3. In a burner of the character described, separate centrifugal atomizing means, means for feeding separate liquid fuels tosaid atomizing means for effecting centrifugal discharge of said fuels, means initially igniting one of said fuels to kindle the other of said fuels, and means for supplying combustion supporting air to the burner and having connection with said separate atomizing meansto direct a portion of the combustion supporting air through said atomizing means and between said liquid fuels to prevent ommingling thereof prior to ignition of said kindling fuel.
4. In an oil burner of the character described, a pair of coaxial cups having annular fuel discharge lips, means for feeding separate liquid fuels to said cups, means for rotating the cups to effect centrifugal discharge of said fuels from said lips, means initially igniting one of said fuels to kindle the other of said fuels, and means for discharging spirally converging streams of combustion supporting air around said cups.
5. An oil burner including a housing having a nozzle portion, a hollow shaft rotatably'mounted in the housing, an atmoizing cup mounted on said shaft in the nozzle portion of said housing, means connected with the shaft for delivering a liquid fuel to said cup, a second cup mounted coaxially with the first cup, means for delivering a liquid kindling fuel to said second cup, means for rotating the shaft to effect centrifugal dis charge of the liquid fuel from said cups, means associated with the housing for initially igniting said kindling fuel, said cups being relatively supported with respect to each other and the housing to provide passages for combustion supporting air between and around said cups, and means for supplying combustion supporting air to said passages.
6. An oil burner including a housing having a spider-like partition dividing the housing into a nozzle portion and an air inlet chamber,'a hollow shaft rotatably mounted in the housing, an atmoizing cup mounted on said shaft, means connected with the shaft for delivering a liquid fuel to said cup, a second cup mounted coaxially with the rst cup, means for delivering a liquid kindling fuel to said second cup, means for rotating the shaft to effect centrifugal discharge of the liquid fuel from said cups, means associated with the housing for initially igniting said kindling fuel, and an air directing nozzle encircling the cups and carried by said spider-like partition to effect discharge of combustion supporting air.
7. In a burner, separate centrifugal means for respectively discharging a liquid kindling fuel and a less combustible liquid fuel, means supporting said centrifugal means for rotation about a common axis, means for rotating said centrifugal means whereby said liquid fuels are discharged in coaxial conical sprays, and means for separately conveying the liquid fuels to said centrifugal means.
8. In a burner, separate centrifugal means for respectively discharging a liquid kindling fuel and a less combustible liquid fuel, means supporting said centrifugal means for rotation about a common axis, means for rotating said centrifugal means whereby said liquid fuels are discharged in coaxial conical sprays, means for separately conveying the liquid fuels to said centrifugal means, ignition means, and means supporting the ignition means in the zone of combustion of said kindling fuel spray.
FRANK S. THOMAS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US256919A US2214568A (en) | 1939-02-17 | 1939-02-17 | Fuel burner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US256919A US2214568A (en) | 1939-02-17 | 1939-02-17 | Fuel burner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2214568A true US2214568A (en) | 1940-09-10 |
Family
ID=22974145
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US256919A Expired - Lifetime US2214568A (en) | 1939-02-17 | 1939-02-17 | Fuel burner |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2214568A (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2559792A (en) * | 1947-08-13 | 1951-07-10 | Pietri Francois | Rotary atomizing liquid fuel burner |
| US2560866A (en) * | 1944-06-06 | 1951-07-17 | Shell Dev | Rotating atomizing cup burner |
| US2566692A (en) * | 1947-02-27 | 1951-09-04 | Edward F Chandler | Oil feeding device for oil burners |
| US2578422A (en) * | 1946-10-22 | 1951-12-11 | Guillot Etienne Jean Francois | Burner for liquid fuel operating under low air and fuel pressures |
| US2638974A (en) * | 1947-01-24 | 1953-05-19 | Ralph C Brierly | Fuel burner diffuser |
| US2685168A (en) * | 1948-01-02 | 1954-08-03 | Phillips Petroleum Co | Combustion chamber |
| US2715813A (en) * | 1952-04-14 | 1955-08-23 | Frederick T Holmes | Fuel injector and flame holder |
| US2715816A (en) * | 1950-10-27 | 1955-08-23 | Ruston & Hornsby Ltd | Combustion chamber for use with internal combustion turbines |
| US2916877A (en) * | 1954-05-12 | 1959-12-15 | Worthington Corp | Pressure fluid generator |
| US2922278A (en) * | 1948-11-30 | 1960-01-26 | Szydlowski Joseph | Coaxial combustion products generator and turbine |
| US3892206A (en) * | 1972-03-23 | 1975-07-01 | Toyoda Chuo Kenkyusho Kk | Combustion device for heat motors |
| US4478045A (en) * | 1980-03-07 | 1984-10-23 | Solar Turbines Incorporated | Combustors and gas turbine engines employing same |
| US5078321A (en) * | 1990-06-22 | 1992-01-07 | Nordson Corporation | Rotary atomizer cup |
| US6079976A (en) * | 1996-05-22 | 2000-06-27 | Toyota Jidosha Kabushiki Kaisha | Structure for supply of fuel and pilot air |
| US20060257807A1 (en) * | 2002-12-23 | 2006-11-16 | Robert Hicks | Combustion device |
| US20120017595A1 (en) * | 2009-04-06 | 2012-01-26 | Kexin Liu | Swirler, combustion chamber, and gas turbine with improved swirl |
-
1939
- 1939-02-17 US US256919A patent/US2214568A/en not_active Expired - Lifetime
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2560866A (en) * | 1944-06-06 | 1951-07-17 | Shell Dev | Rotating atomizing cup burner |
| US2578422A (en) * | 1946-10-22 | 1951-12-11 | Guillot Etienne Jean Francois | Burner for liquid fuel operating under low air and fuel pressures |
| US2638974A (en) * | 1947-01-24 | 1953-05-19 | Ralph C Brierly | Fuel burner diffuser |
| US2566692A (en) * | 1947-02-27 | 1951-09-04 | Edward F Chandler | Oil feeding device for oil burners |
| US2559792A (en) * | 1947-08-13 | 1951-07-10 | Pietri Francois | Rotary atomizing liquid fuel burner |
| US2685168A (en) * | 1948-01-02 | 1954-08-03 | Phillips Petroleum Co | Combustion chamber |
| US2922278A (en) * | 1948-11-30 | 1960-01-26 | Szydlowski Joseph | Coaxial combustion products generator and turbine |
| US2715816A (en) * | 1950-10-27 | 1955-08-23 | Ruston & Hornsby Ltd | Combustion chamber for use with internal combustion turbines |
| US2715813A (en) * | 1952-04-14 | 1955-08-23 | Frederick T Holmes | Fuel injector and flame holder |
| US2916877A (en) * | 1954-05-12 | 1959-12-15 | Worthington Corp | Pressure fluid generator |
| US3892206A (en) * | 1972-03-23 | 1975-07-01 | Toyoda Chuo Kenkyusho Kk | Combustion device for heat motors |
| US4478045A (en) * | 1980-03-07 | 1984-10-23 | Solar Turbines Incorporated | Combustors and gas turbine engines employing same |
| US5078321A (en) * | 1990-06-22 | 1992-01-07 | Nordson Corporation | Rotary atomizer cup |
| US6079976A (en) * | 1996-05-22 | 2000-06-27 | Toyota Jidosha Kabushiki Kaisha | Structure for supply of fuel and pilot air |
| US20060257807A1 (en) * | 2002-12-23 | 2006-11-16 | Robert Hicks | Combustion device |
| US20120017595A1 (en) * | 2009-04-06 | 2012-01-26 | Kexin Liu | Swirler, combustion chamber, and gas turbine with improved swirl |
| US9222666B2 (en) * | 2009-04-06 | 2015-12-29 | Siemens Aktiengesellschaft | Swirler, combustion chamber, and gas turbine with improved swirl |
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