US2374041A - Variable capacity atomizing device - Google Patents
Variable capacity atomizing device Download PDFInfo
- Publication number
- US2374041A US2374041A US428978A US42897842A US2374041A US 2374041 A US2374041 A US 2374041A US 428978 A US428978 A US 428978A US 42897842 A US42897842 A US 42897842A US 2374041 A US2374041 A US 2374041A
- Authority
- US
- United States
- Prior art keywords
- oil
- chamber
- liquid
- whirl chamber
- atomizing
- 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
Links
- 239000003921 oil Substances 0.000 description 96
- 239000007788 liquid Substances 0.000 description 57
- 230000001105 regulatory effect Effects 0.000 description 8
- 239000007921 spray Substances 0.000 description 6
- 238000000889 atomisation Methods 0.000 description 5
- 238000004891 communication Methods 0.000 description 5
- 230000003247 decreasing effect Effects 0.000 description 5
- 239000012530 fluid Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000003292 diminished effect Effects 0.000 description 3
- 230000001276 controlling effect Effects 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000000295 fuel oil Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 235000002020 sage Nutrition 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
- F23D11/26—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed
- F23D11/28—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed with flow-back of fuel at the burner, e.g. using by-pass
Definitions
- This invention relates to atomizing nozzles and relates more particularly to improvements in atomizing nozzles for fuel oil burners in which the volume of atomized oil can be varied over a wide range while maintaining a uniformly good atomization at different loads.
- One of the practices in the oil burner art, particularly in firing marine boilers, is to utilize a number of burners for each boiler and to operate each nozzle at a fixed optimum capacity. Variations in rate of firing are obtained by turning on or off a diii'erent number of burners.
- Variable volume fuel burner nozzles have been proposed heretofore and are desirable especially insmall installations where only one or a few burners are used and where accurate control is required. But none of the nozzles heretofore known has been capable of maintaining an entirely uniform type of atomization throughout a wide capacity range.
- One of the prior variable capacity nozzles includes a so-called whirl chamber having a discharge or atomizing orifice and tangentially disposed oil inlets which impart rotation to the oil in the whirl chamber.
- the back of the whirl chamber is provided with a plurality of oil escape passages communicating with a return pipe.
- the disadvantage of this type of nozzle is that the oil escape passages are in the path of the oil entering the whirl chamber through the tangential inlets. thereby permitting the oil to escape and lowering the pressure in the chamber as the amount of oil escaping through the passages increases, thereby decreasing the atomizing power of the nozzles.
- Another type of nozzle includes a whirl chamber provided with tangential oil inlets, an axial discharge or atomizing outlet and an axial oil escape passage of somewhat larger diameter than the discharge outlet.
- the oil entering the chamber tangentially will acquire a rotating motion which acts to atomize the oil flowing in the form of an annular stream over the edges of the discharge outlet.
- the oil escaping through the discharge passage also will have a rotating motion which is imparted to the column of oil being returned to the tank.
- the rotation of the long column of return oil absorbs energy and acts as a drag on the rotation of the oil in the chamber.
- extra power is required to supply'the oil and, under constant pressure feed conditions, variation in the amount of oil returned will vary the kinetic energy of the oil in the chamber, thereby varying the atomizing power of the nozzle.
- a whirl chamber including tangential inlets and an axial discharge outlet, is disposed behind a second chamber having an exit port in alignment with the discharge port of the whirl chamber.
- the second chamber is provided with oil return passages disposed radially outwardly of the exit port.
- oil is diverted from the annular stream discharged from the whirl chamber and is returned through an oil line to the supply tank.
- the volume of return oil is varied, greater or lesser amounts of the oil may be atomized through the exit port.
- the kinetic energy of the oil issuing from the exit port will vary depending upon the amount of energy absorbed by rotation of the oil in the second chamber.
- the oil will have the greatest amount of kinetic energy possible at the time it passes through the discharge port and cannot have energy added to it.
- the relatively small volume of oil passing across or through the second chamber supplies energy for rotating the body of oil in the second chamber and thus a portion of its atomizing power is lost and cannot be recovered.
- the amount 01' energy absorbed is increased or decreased with the result that the energy remaining in the oil passing through the exit port and the atomizing power of the nozzle varies at the different discharge rates.
- the present invention has as its principal object the provision of a nozzle which overcomes the defects of the nozzles described above in that. regardless of the volume of oil being atomized. the kinetic energy and tangential velocity of the oil in any' portion of the atomizing outlet will remain constant.
- Atomizing nozzles in accordance with the present invention may include an outer whirl chamber having at least one tangential oil inlet which causes the oil in the chamber to flow vortically, and coaxial atomizing and return ports in opposite sides of the whirl chamber.
- a second inner whirl chamber may be disposed rearwardly of through the tangential duct or ducts into the outer whirl chamber is given a vortical motion setting up a free vortex therein so that the oil attains an annular form having a hollow core.
- substantially all of the pressure head on the oil is converted into kinetic energy.
- the flow of oil through the atomizing port may be prevented by releasing the back pressure against the discharge or escape port and allowing the oil to flow freely therethrough with the whirling motion which it has acquired.
- This oil upon entering the inner whirl chamber tends to flow spirally outwardly in a manner substantially the reverse of the flow in the whirl chamher, but in the same direction of rotation with the result that the kinetic energy thereof is converted back into pressure.
- the construction is such that none of the pressure on the incoming oil is used for return of discharged oil prior to the conversion of the pressure into kinetic energy.
- the kinetic energy of the discharge oil is not absorbed or diminished by acting upon any other body of oil of substantial volume to impart a rotating motion thereto. Therefore, the atomizing effect of nozzles embodying the present invention is substantially the same on the oil being atomized regardless of the volume of oil being discharged.
- Figure 1 is a view in section of a typical form of nozzle embodying the present invention
- Figure 2 is an end view of the nozzle
- Figure 3 is a view in section taken on line 3-3 of Figure 1:
- Figure 4 is a view in section taken on line 4--4 of Figure 1;
- Figure 5 is a diagrammatic showing of the action of a nozzle of the type embodying the present invention.
- Figure 6 is a view in section on a reduced scale taken on the line 6-6 of Figure 5.
- a typical form of atomizing nozzle of the type embodying the present invention may include an elongated casing I having a bore I I therein through which oil may be supplied to the atomizing nozzle I2 by means of any suitable type of pump I3.
- the nozzle I! may include a threaded reduced portion II on one end of the casing t0 upon which is received a cap I that retains the various elements of the nozzle in fixed position adjacent to the end of the extension I 4.
- the outermost end of the extension H is provided with a recess I6 in which is mounted a disc-like member I'I having circular recesses or chambers I la and I'll: in
- the chambers are shown as cylindrical, but may be conical, hemispherical or any other desired shape. These chambers are connected by means of a bore or oil return port I'Ic.
- the disc member Il may have one or more of the tangential inlets Hit.
- the groove Mb communicates with the passageway It so that oil may flow therethrough into the openings He in the disc I! and thence into the chamber I'Ia through the tangential inlets IId.
- an atomizing disc I8 which is provided with an atomizing or discharge orifice l8c in the center thereof.
- the orifice I81: and the return port He may he the same or different in diameter, but I prefer to make the return port somewhat larger in order to obtain a wider range of control of the volume of oil atomized.
- the outer surface of the disc I 8 may be dished or have a concave recess 3b in order to decrease the effective thickness of the disc and permit unobstructed discharge of the oil.
- the cap I5 has an inwardly extending annular flange l5a which overlies the edges of the atomizing disc I8 and clamps it against the end of the extension I4.
- Oil may be returned from the atomizing nozzle through a passageway I9 extending along the casing III which terminates adjacent the disc (I in one or more narrower passages I9a which are so arranged that they communicate with the inner chamber I'Ib adjacent its periphery or eccentrically to the return port I To.
- the passage I9 adjacent its opposite end may have a rightangularly related passage 20 connected to a conduit having manually or automatically controlled valve 2i therein by means of which the flow of return oil may be regulated.
- oil is fed by the pump I3 into the passageway II and from the passageway into the opening Hc, through the tangential passage I'ld into the outer whirl chamber lia where the oil is given a whirling motion and the oil pressure is converted substantially completely into kinetic energy of rotation.
- tangential inlet I'Id and one tangential discharge passage I90. are shown in Figures 5 and 6.
- the outer whirl chamber Fla .and inner whirl chamber I 1b and inlets and outlets thus are identical, although rotated with respect to each other at about As the oil flows into the chamber Ila, it will be whirled in free vortical flow in the form of an annulus of gradually increasing width.
- valve If the valve is closed completely, or partially closed, so that oil enters the whirl chamber Ila faster than it is discharged through the passage IS, the hollow core of whirling vortex of oil in the whirl chamber I M will be reduced to a smaller diameter than the diameter of the orifice Na and oil will begin to flow into the discharge or atomizing orifice [8a and is thrown therefrom in the form of a conical spray, as shown in Figure 5.
- the amount of oil passing through the atomizing orifice We is dependent, of course, upon the amount of oil fed to the nozzles, less the amount returned through the passageway i 9.
- the whirl chamber l'lb in which the kinetic energy of the oil flowing through the opening port He is reconverted into pressure contains only a very small amount of oil even when full. This mass of oil will, at best, absorb only an inappreciable amount of energy and this energy is absorbed at a zone spaced from the oil passing through the discharge orifice I 8a.
- a nozzle has been provided by means of which uniform atomization can be obtained regardless of the volume of liquid atomized within the operating range of the nozzle.
- the form of nozzle described above is preferred, it will be understood that the number of tangential passageways for providing vortical movement of the liquid, the shape and disposition and number of liquid escape passageways communicating with the chamber llb can be varied and the size of the nozzle may a 3 be altered as may be desired without departing from the invention.
- the nozzle is not restricted to use in fuel oil burners. but may be used in water sprinkler systems and the like. Therefore, the above-described form of nozzle should be considered as illustrative only and not as limiting the scope of the following claims.
- An atomizing nozzle comprising means forming a pair of coaxial inner and outer circular chambers of substantially the same capacity, means for introducing a liquid substantially tangentially into said outer chamber, means forming a circular atomizing"orifieecommunicating with said outer chamber, means forming a circular liquid return port coaxial with, of smaller diameter than, and connecting said inner and outer chambers, means forming at least one passage communicating with said inner chamber at a point spaced from'the axis of said inner chamber a distance greater than the radius of said return port for withdrawing liquid from said inner chamber, and means for regulating the amount of liquid withdrawn from said inner chamber.
- An atomizin nozzle comprising meansforming a pair of coaxial inner and outer circular chambers of substantially the same capacity, means for introducing a liquid substantially tangentially into said outer chamber, means forming a circular atomizing orifice communicating and coaxial with said outer chamber, means forming a circular liquid return port coaxial with, of smaller diameter than, and connecting said inner and outer chambers, said atomizing orifice being of lesser diameter than said return port, means forming at least one passage communicating with said inner chamber at a point spaced from the axis of said inner chamber a distance greater than the radius of said return port for withdrawing liquid from said inner chamber, and means for regulating the amount of liquid withdrawn from said inner chamber.
- An atomizing nozzle comprising a casing, means in said casing forming a pair of coaxial spaced apart circular chambers of substantially the same capacity, means forming a port coaxial with, of smaller diameter than, and connecting said chambers, means forming an atomizing orifice in one end of said casing communicating and coaxial with one of said chambers, means for introducing liquid substantially tangentially into said one of said chambers, means forming in said casing at least one liquid return passage communicating with the other chamber tangentially to the periphery thereof at a distance from the axis of said other chamber greater than the radius of said port, and means for regulating the amount of liquid returned from said other chamber.
- a method of atomizing a liquid which cornprises introducing liquid under pressure into a whirl chamber to create a free vortex and convert the pressure of said liquid into kinetic energy, discharging liquid freely from the center zone of said vortex to atomize said liquid by the kinetic energy thereof, withdrawing liquid from the center zone or said vortex in a direction opposite to the direction of discharge of said liquid to control the volume of liquid atomized, forming an expanding vortex rotating in the same direction as said free vortex in said withdrawn liquid, and substantially immediately converting the kinetic energy of said liquid in said expanding vortex into pressure by withdrawing the liquid in the expanding vortex from adjacent its outer periphery.
- a method of controlling the rate of atomization of a liquid which comprises forcing a liquid under pressure tangentially to form a free vortex for converting the pressure into kinetic energy, discharging a portion of said liquid from the interior of the said vortex directly into a free space forming a spray, withdrawing the remaining portion of said liquid in the opposite direction,
- An atomizer having a supply conduit and a return conduit and a tip having a whirl chamber terminating in an orifice through which fluid is discharged for atomization, means including inlet ducts for supplying fluid from said supply conduit to said whirl chamber and for causing the fluid to rotate therein, said whirl chamber having a rear wall provided with an axial unobstructed return opening of smaller diameter than said whirl chamber and of a diameter at least as great as that of said orifice, said rear wall providing a smooth unbroken annular surface in contact with the whirling fluid in said whirl chamber, and an inner whirl chamber between said return opening and said return conduit of greater diameter than said return opening, said return opening and said inner whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return opening and said inner whirl chamber, whereby said return fluid can form an expanding vortex, said return conduit and said inner whirl chamber being con nected at a point spaced from
- An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second whirl chamber having a length not substantially exceeding the length of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber,
- An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, said return port being of greater diameter than said atomizing port, means introducing liquid intosaid chamberlto cause said liquid to form a free vortex, means forming a second whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to Provide direct and unobstructed communication between said return port and said second whirl chamber, means communieating with said second whirl chamber adjacent to the periphery thereof through which said liquid may escape from said second whirl chamber, and means for regulating the amount of liquid escap ing from said second whirl chamber.
- An atomizing nozzle comprising means forming a circular whirl chamber having atomlzing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second circular whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber, means communicating tangentially with said second whirl cham ber adjacent to the periphery thereof through which said liquid may escape, and means for regulating the amount of liquid escaping from said second whirl chamber.
- An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber, means communicating with said second whirl chamber eccentric to said return port for withdrawing liquid from said second whirl chamber, and means for regulating the amount of liquid escaping from said second whirl chamber.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
Description
A. P. SAHA VARIABLE CAPACITY ATOMIZING DEVICE April 17, 1945.
Filed Jan. 31, 1942 INVENTOR. Anna BSA/1,4
ATTORNEYS utant11.11545 VARIABLE cnracm a'romzmc navrca Aatto P, Saha, Staten Island, N. Y., assignor to General Furnaces Corporation, New York. N. Y., I a corporation of New York Application January 31, 1942, Serial No. 428,978 Claims. (Cl. 299-120) This invention relates to atomizing nozzles and relates more particularly to improvements in atomizing nozzles for fuel oil burners in which the volume of atomized oil can be varied over a wide range while maintaining a uniformly good atomization at different loads.
One of the practices in the oil burner art, particularly in firing marine boilers, is to utilize a number of burners for each boiler and to operate each nozzle at a fixed optimum capacity. Variations in rate of firing are obtained by turning on or off a diii'erent number of burners.
Variable volume fuel burner nozzles have been proposed heretofore and are desirable especially insmall installations where only one or a few burners are used and where accurate control is required. But none of the nozzles heretofore known has been capable of maintaining an entirely uniform type of atomization throughout a wide capacity range.
One of the prior variable capacity nozzles includes a so-called whirl chamber having a discharge or atomizing orifice and tangentially disposed oil inlets which impart rotation to the oil in the whirl chamber. The back of the whirl chamber is provided with a plurality of oil escape passages communicating with a return pipe.
The disadvantage of this type of nozzle is that the oil escape passages are in the path of the oil entering the whirl chamber through the tangential inlets. thereby permitting the oil to escape and lowering the pressure in the chamber as the amount of oil escaping through the passages increases, thereby decreasing the atomizing power of the nozzles.
Another type of nozzle includes a whirl chamber provided with tangential oil inlets, an axial discharge or atomizing outlet and an axial oil escape passage of somewhat larger diameter than the discharge outlet. The oil entering the chamber tangentially will acquire a rotating motion which acts to atomize the oil flowing in the form of an annular stream over the edges of the discharge outlet. The oil escaping through the discharge passage also will have a rotating motion which is imparted to the column of oil being returned to the tank. The rotation of the long column of return oil absorbs energy and acts as a drag on the rotation of the oil in the chamber. As a result, extra power is required to supply'the oil and, under constant pressure feed conditions, variation in the amount of oil returned will vary the kinetic energy of the oil in the chamber, thereby varying the atomizing power of the nozzle.
Expedients have been suggested for overcoming the disadvantages of the nozzles described above. In one suggested type of nozzle, a whirl chamber, including tangential inlets and an axial discharge outlet, is disposed behind a second chamber having an exit port in alignment with the discharge port of the whirl chamber. The second chamber is provided with oil return passages disposed radially outwardly of the exit port.
With this arrangement oil is diverted from the annular stream discharged from the whirl chamber and is returned through an oil line to the supply tank. As the volume of return oil is varied, greater or lesser amounts of the oil may be atomized through the exit port. However, the kinetic energy of the oil issuing from the exit port will vary depending upon the amount of energy absorbed by rotation of the oil in the second chamber. The oil will have the greatest amount of kinetic energy possible at the time it passes through the discharge port and cannot have energy added to it. However, the relatively small volume of oil passing across or through the second chamber supplies energy for rotating the body of oil in the second chamber and thus a portion of its atomizing power is lost and cannot be recovered. As the volume of oil passing through the second chamber varies, the amount 01' energy absorbed is increased or decreased with the result that the energy remaining in the oil passing through the exit port and the atomizing power of the nozzle varies at the different discharge rates.
The present invention has as its principal object the provision of a nozzle which overcomes the defects of the nozzles described above in that. regardless of the volume of oil being atomized. the kinetic energy and tangential velocity of the oil in any' portion of the atomizing outlet will remain constant.
Atomizing nozzles in accordance with the present invention may include an outer whirl chamber having at least one tangential oil inlet which causes the oil in the chamber to flow vortically, and coaxial atomizing and return ports in opposite sides of the whirl chamber. A second inner whirl chamber may be disposed rearwardly of through the tangential duct or ducts into the outer whirl chamber is given a vortical motion setting up a free vortex therein so that the oil attains an annular form having a hollow core. In setting up the vortical motion in the outer chamber, substantially all of the pressure head on the oil is converted into kinetic energy. When the oil escape port is of larger diameter than the atomizing port, the flow of oil through the atomizing port may be prevented by releasing the back pressure against the discharge or escape port and allowing the oil to flow freely therethrough with the whirling motion which it has acquired. This oil upon entering the inner whirl chamber tends to flow spirally outwardly in a manner substantially the reverse of the flow in the whirl chamher, but in the same direction of rotation with the result that the kinetic energy thereof is converted back into pressure.
As the flow of oil through the return pipe is diminished, as by closing or partially closing the valve therein, less oil can escape through the port between the outer and the inner whirl chambers with the result that the core which is free of oil becomes smaller and more oil can escape through the atomizing or discharge port.
By drawing the oil oil through the escape port or ports in the inner whirl chamber, any tendency for the escaping oil to rotate in the return pipe is completely eliminated and the returning column of oil cannot absorb kinetic energy to decrease the tangential velocity of the oil in the outer whirl chamber. Also, the construction is such that none of the pressure on the incoming oil is used for return of discharged oil prior to the conversion of the pressure into kinetic energy. Moreover, inasmuch as the discharged oil has attained maximum kinetic energy and escapes freely, the kinetic energy of the discharge oil is not absorbed or diminished by acting upon any other body of oil of substantial volume to impart a rotating motion thereto. Therefore, the atomizing effect of nozzles embodying the present invention is substantially the same on the oil being atomized regardless of the volume of oil being discharged.
For a better understanding of the present invention, reference may be had to the accompanying drawing in which:
Figure 1 is a view in section of a typical form of nozzle embodying the present invention;
Figure 2 is an end view of the nozzle;
Figure 3 is a view in section taken on line 3-3 of Figure 1:
Figure 4 is a view in section taken on line 4--4 of Figure 1;
Figure 5 is a diagrammatic showing of the action of a nozzle of the type embodying the present invention;
Figure 6 is a view in section on a reduced scale taken on the line 6-6 of Figure 5.
As shown particularly in Figure 1. a typical form of atomizing nozzle of the type embodying the present invention may include an elongated casing I having a bore I I therein through which oil may be supplied to the atomizing nozzle I2 by means of any suitable type of pump I3. The nozzle I! may include a threaded reduced portion II on one end of the casing t0 upon which is received a cap I that retains the various elements of the nozzle in fixed position adjacent to the end of the extension I 4. The outermost end of the extension H is provided with a recess I6 in which is mounted a disc-like member I'I having circular recesses or chambers I la and I'll: in
opposite sides thereof which are the outer and inner whirl chambers referred to heretofore. The chambers are shown as cylindrical, but may be conical, hemispherical or any other desired shape. These chambers are connected by means of a bore or oil return port I'Ic. Communicating with the whirl chamber Il'a, as best shown in Figure 3, are a pair of tangentially inclined grooves Ild which terminate in enlarged openings He that extend entirely through the disc-like member I! and communicate with an annular groove Mb in the end of the extension I4. The disc member Il may have one or more of the tangential inlets Hit. The groove Mb communicates with the passageway It so that oil may flow therethrough into the openings He in the disc I! and thence into the chamber I'Ia through the tangential inlets IId.
overlying the disc I! and retaining it in fixed position is an atomizing disc I8 which is provided with an atomizing or discharge orifice l8c in the center thereof. The orifice I81: and the return port He may he the same or different in diameter, but I prefer to make the return port somewhat larger in order to obtain a wider range of control of the volume of oil atomized. The outer surface of the disc I 8 may be dished or have a concave recess 3b in order to decrease the effective thickness of the disc and permit unobstructed discharge of the oil. The cap I5 has an inwardly extending annular flange l5a which overlies the edges of the atomizing disc I8 and clamps it against the end of the extension I4.
Oil may be returned from the atomizing nozzle through a passageway I9 extending along the casing III which terminates adjacent the disc (I in one or more narrower passages I9a which are so arranged that they communicate with the inner chamber I'Ib adjacent its periphery or eccentrically to the return port I To. The passage I9 adjacent its opposite end may have a rightangularly related passage 20 connected to a conduit having manually or automatically controlled valve 2i therein by means of which the flow of return oil may be regulated.
Referring now to Figure 5, in operation oil is fed by the pump I3 into the passageway II and from the passageway into the opening Hc, through the tangential passage I'ld into the outer whirl chamber lia where the oil is given a whirling motion and the oil pressure is converted substantially completely into kinetic energy of rotation. For simplicity, only one tangential inlet I'Id and one tangential discharge passage I90. are shown in Figures 5 and 6. The outer whirl chamber Fla .and inner whirl chamber I 1b and inlets and outlets thus are identical, although rotated with respect to each other at about As the oil flows into the chamber Ila, it will be whirled in free vortical flow in the form of an annulus of gradually increasing width. As the oil continues to flow into the chamber I'Ia the ho]- low core in the center of the annular whirling mass of oil will become narrower with the result that the oil will reach the edge of the escape port He and will tend to flow along this opening into the chamber Ilb as indicated by the dotted line in Figure 5. The oil leaving the opening I10 and entering the inner whirl chamber IIb will be rotating in the same direction and will flow outwardly in an expanding vortex so that its kinetic energy will be reconverted into pressure in the exact reverse of the manner in which the oil pressure was converted into kinetic energy in the whirl chamber Ila. The oil will flow through the passageway l9a under pressure and without rotation into the passage I 9 and thence through the valve 2|, if open, back into the supply tank. not shown. If the valve is closed completely, or partially closed, so that oil enters the whirl chamber Ila faster than it is discharged through the passage IS, the hollow core of whirling vortex of oil in the whirl chamber I M will be reduced to a smaller diameter than the diameter of the orifice Na and oil will begin to flow into the discharge or atomizing orifice [8a and is thrown therefrom in the form of a conical spray, as shown in Figure 5. The amount of oil passing through the atomizing orifice We is dependent, of course, upon the amount of oil fed to the nozzles, less the amount returned through the passageway i 9.
Irrespective of the amount of oil passing through the discharge orifice l8a, the amount of energy tending to throw the oil tangentially will remain the same for the reason that the fiow of oil through the discharge orifice l8a is unafiected by any other factors which would tend either to diminish the pressure of the oil, and hence its kinetic energy, which has reached a maximum at the discharge port I811, will be diminished only to the extent of losses through friction in passing through the discharge port.
The whirl chamber l'lb in which the kinetic energy of the oil flowing through the opening port He is reconverted into pressure contains only a very small amount of oil even when full. This mass of oil will, at best, absorb only an inappreciable amount of energy and this energy is absorbed at a zone spaced from the oil passing through the discharge orifice I 8a.
The only effect that an increase or decrease in the amount or oil escaping through the passageway will have is in the shape of the spray. An increase in the flow of liquid through the discharge orifice, by decreasing the fiow in the pas- .sage l9, will make the spray take the form of a narrow and long cone and a decrease in the fiow through the discharge orifice I8a will make the cone shorter and wider. This variation in the shape and the length of the cone spray is advantageous in that it permits a more efficient mixing of the atomized oil with the air that is fed for combustion purposes. The amount of air that is fed is usually substantially proportional to the amount of oil'that is atomized and thus the volume and velocity of the air are decreased when the amount of oil atomized is decreased. In order to cause thorough mixing of the oil and the air, the oil should be directed at such an angle to the direction of flow of the air that the spray will intersect and spread across the column of air.
When larger volumes of oil are to be burned, the air volume must be increased and, therefore, better mixing and more efiicient combustion can be obtained w th a longer flame. The narrower and longer cone obtainable by feeding a larger volume of oil, therefore, is most satisfactory for efilcient combustion at increased air velocities.
From the foregoingdescrip tion of typical forms of my invention, it will be clear that a nozzle has been provided by means of which uniform atomization can be obtained regardless of the volume of liquid atomized within the operating range of the nozzle. Although the form of nozzle described above is preferred, it will be understood that the number of tangential passageways for providing vortical movement of the liquid, the shape and disposition and number of liquid escape passageways communicating with the chamber llb can be varied and the size of the nozzle may a 3 be altered as may be desired without departing from the invention. Moreover, the nozzle is not restricted to use in fuel oil burners. but may be used in water sprinkler systems and the like. Therefore, the above-described form of nozzle should be considered as illustrative only and not as limiting the scope of the following claims.
Iclaim:
1. An atomizing nozzle comprising means forming a pair of coaxial inner and outer circular chambers of substantially the same capacity, means for introducing a liquid substantially tangentially into said outer chamber, means forming a circular atomizing"orifieecommunicating with said outer chamber, means forming a circular liquid return port coaxial with, of smaller diameter than, and connecting said inner and outer chambers, means forming at least one passage communicating with said inner chamber at a point spaced from'the axis of said inner chamber a distance greater than the radius of said return port for withdrawing liquid from said inner chamber, and means for regulating the amount of liquid withdrawn from said inner chamber.
2. An atomizin nozzle comprising meansforming a pair of coaxial inner and outer circular chambers of substantially the same capacity, means for introducing a liquid substantially tangentially into said outer chamber, means forming a circular atomizing orifice communicating and coaxial with said outer chamber, means forming a circular liquid return port coaxial with, of smaller diameter than, and connecting said inner and outer chambers, said atomizing orifice being of lesser diameter than said return port, means forming at least one passage communicating with said inner chamber at a point spaced from the axis of said inner chamber a distance greater than the radius of said return port for withdrawing liquid from said inner chamber, and means for regulating the amount of liquid withdrawn from said inner chamber.
3. An atomizing nozzle comprising a casing, means in said casing forming a pair of coaxial spaced apart circular chambers of substantially the same capacity, means forming a port coaxial with, of smaller diameter than, and connecting said chambers, means forming an atomizing orifice in one end of said casing communicating and coaxial with one of said chambers, means for introducing liquid substantially tangentially into said one of said chambers, means forming in said casing at least one liquid return passage communicating with the other chamber tangentially to the periphery thereof at a distance from the axis of said other chamber greater than the radius of said port, and means for regulating the amount of liquid returned from said other chamber.
4. A method of atomizing a liquid, which cornprises introducing liquid under pressure into a whirl chamber to create a free vortex and convert the pressure of said liquid into kinetic energy, discharging liquid freely from the center zone of said vortex to atomize said liquid by the kinetic energy thereof, withdrawing liquid from the center zone or said vortex in a direction opposite to the direction of discharge of said liquid to control the volume of liquid atomized, forming an expanding vortex rotating in the same direction as said free vortex in said withdrawn liquid, and substantially immediately converting the kinetic energy of said liquid in said expanding vortex into pressure by withdrawing the liquid in the expanding vortex from adjacent its outer periphery.
5. A method of controlling the rate of atomization of a liquid which comprises forcing a liquid under pressure tangentially to form a free vortex for converting the pressure into kinetic energy, discharging a portion of said liquid from the interior of the said vortex directly into a free space forming a spray, withdrawing the remaining portion of said liquid in the opposite direction,
forming in said remaining portion of said liquid a shallow expanding vortex rotating in the same direction as said free vortex for converting the kinetic energy thereof into pressure, and regulating the volume of the withdrawn portion by controlling the pressure of the withdrawn liquid.
6. An atomizer having a supply conduit and a return conduit and a tip having a whirl chamber terminating in an orifice through which fluid is discharged for atomization, means including inlet ducts for supplying fluid from said supply conduit to said whirl chamber and for causing the fluid to rotate therein, said whirl chamber having a rear wall provided with an axial unobstructed return opening of smaller diameter than said whirl chamber and of a diameter at least as great as that of said orifice, said rear wall providing a smooth unbroken annular surface in contact with the whirling fluid in said whirl chamber, and an inner whirl chamber between said return opening and said return conduit of greater diameter than said return opening, said return opening and said inner whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return opening and said inner whirl chamber, whereby said return fluid can form an expanding vortex, said return conduit and said inner whirl chamber being con nected at a point spaced from the axis of the chambers a greater distance than the radius of said return opening.
7. An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second whirl chamber having a length not substantially exceeding the length of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber,
means communicating with said second whirl chamber adjacent to the periphery thereof through which said liquid may escape from said second whirl chamber, and means for returning the escaping liquid to a zone of lower pressure than the pressure at said means for introducing liquid.
8. An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, said return port being of greater diameter than said atomizing port, means introducing liquid intosaid chamberlto cause said liquid to form a free vortex, means forming a second whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to Provide direct and unobstructed communication between said return port and said second whirl chamber, means communieating with said second whirl chamber adjacent to the periphery thereof through which said liquid may escape from said second whirl chamber, and means for regulating the amount of liquid escap ing from said second whirl chamber.
9. An atomizing nozzle comprising means forming a circular whirl chamber having atomlzing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second circular whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber, means communicating tangentially with said second whirl cham ber adjacent to the periphery thereof through which said liquid may escape, and means for regulating the amount of liquid escaping from said second whirl chamber.
10. An atomizing nozzle comprising means forming a whirl chamber having atomizing and liquid return ports of smaller diameter than said whirl chamber on opposite sides of and coaxial with said chamber, means for introducing a liquid into said chamber to cause said liquid to form a free vortex, means forming a second whirl chamber having a capacity not substantially greater than the capacity of said first mentioned whirl chamber and of greater diameter than said return port for receiving liquid escaping through said return port, said return port and said second whirl chamber being so constructed and connected as to provide direct and unobstructed communication between said return port and said second whirl chamber, means communicating with said second whirl chamber eccentric to said return port for withdrawing liquid from said second whirl chamber, and means for regulating the amount of liquid escaping from said second whirl chamber.
AA'IIO P. SAHA.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US428978A US2374041A (en) | 1942-01-31 | 1942-01-31 | Variable capacity atomizing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US428978A US2374041A (en) | 1942-01-31 | 1942-01-31 | Variable capacity atomizing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2374041A true US2374041A (en) | 1945-04-17 |
Family
ID=23701229
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US428978A Expired - Lifetime US2374041A (en) | 1942-01-31 | 1942-01-31 | Variable capacity atomizing device |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2374041A (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2549092A (en) * | 1943-10-19 | 1951-04-17 | Sulzer Ag | Burner for liquid fuels |
| US2561939A (en) * | 1948-12-30 | 1951-07-24 | A V Roe Canada Ltd | Dual spray nozzle for fuel burners |
| US2566532A (en) * | 1947-08-20 | 1951-09-04 | Delavan Mfg Company | Combustion spray nozzle |
| US2579215A (en) * | 1947-10-27 | 1951-12-18 | Shell Dev | Wide range liquid fuel burner and method for increasing adjustability r ge of whirl-type atomizing burners |
| US2578934A (en) * | 1945-08-01 | 1951-12-18 | Hendrik J J Janssen | Adjustable burner for liquid fuel |
| US2697636A (en) * | 1949-12-20 | 1954-12-21 | Dowty Equipment Ltd | Liquid fuel burner |
| US2715546A (en) * | 1949-09-10 | 1955-08-16 | Babcock & Wilcox Co | Atomizer |
| US2721765A (en) * | 1952-03-27 | 1955-10-25 | Hobson Ltd H M | Nozzles |
| US2757961A (en) * | 1950-09-07 | 1956-08-07 | Chrysler Corp | Regulated fuel system |
| US3228608A (en) * | 1961-04-26 | 1966-01-11 | Agfa Ag | Electrophotographic developer electrode |
| US3406911A (en) * | 1965-12-30 | 1968-10-22 | Valve Corp Of America | Spray discharge button for swirling spray |
| US3464630A (en) * | 1967-02-09 | 1969-09-02 | Burmeister & Wains Mot Mask | Pressure atomizing oil burner |
| US4186877A (en) * | 1976-06-25 | 1980-02-05 | Delavan Manufacturing Company | By-pass nozzles |
| US4535722A (en) * | 1982-12-01 | 1985-08-20 | Nihon Den-Netsu Keiki Co., Ltd. | Apparatus for applying molten wax onto printed circuit board |
| US5050799A (en) * | 1985-08-15 | 1991-09-24 | Ulrich Rohs | Injection nozzle for liquid media |
| US5067655A (en) * | 1987-12-11 | 1991-11-26 | Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt | Whirl nozzle for atomizing a liquid |
-
1942
- 1942-01-31 US US428978A patent/US2374041A/en not_active Expired - Lifetime
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2549092A (en) * | 1943-10-19 | 1951-04-17 | Sulzer Ag | Burner for liquid fuels |
| US2578934A (en) * | 1945-08-01 | 1951-12-18 | Hendrik J J Janssen | Adjustable burner for liquid fuel |
| US2566532A (en) * | 1947-08-20 | 1951-09-04 | Delavan Mfg Company | Combustion spray nozzle |
| US2579215A (en) * | 1947-10-27 | 1951-12-18 | Shell Dev | Wide range liquid fuel burner and method for increasing adjustability r ge of whirl-type atomizing burners |
| US2561939A (en) * | 1948-12-30 | 1951-07-24 | A V Roe Canada Ltd | Dual spray nozzle for fuel burners |
| US2715546A (en) * | 1949-09-10 | 1955-08-16 | Babcock & Wilcox Co | Atomizer |
| US2697636A (en) * | 1949-12-20 | 1954-12-21 | Dowty Equipment Ltd | Liquid fuel burner |
| US2757961A (en) * | 1950-09-07 | 1956-08-07 | Chrysler Corp | Regulated fuel system |
| US2721765A (en) * | 1952-03-27 | 1955-10-25 | Hobson Ltd H M | Nozzles |
| US3228608A (en) * | 1961-04-26 | 1966-01-11 | Agfa Ag | Electrophotographic developer electrode |
| US3406911A (en) * | 1965-12-30 | 1968-10-22 | Valve Corp Of America | Spray discharge button for swirling spray |
| US3464630A (en) * | 1967-02-09 | 1969-09-02 | Burmeister & Wains Mot Mask | Pressure atomizing oil burner |
| US4186877A (en) * | 1976-06-25 | 1980-02-05 | Delavan Manufacturing Company | By-pass nozzles |
| US4535722A (en) * | 1982-12-01 | 1985-08-20 | Nihon Den-Netsu Keiki Co., Ltd. | Apparatus for applying molten wax onto printed circuit board |
| US5050799A (en) * | 1985-08-15 | 1991-09-24 | Ulrich Rohs | Injection nozzle for liquid media |
| US5067655A (en) * | 1987-12-11 | 1991-11-26 | Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt | Whirl nozzle for atomizing a liquid |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2374041A (en) | Variable capacity atomizing device | |
| US5025989A (en) | Spray nozzle design | |
| US3790086A (en) | Atomizing nozzle | |
| US5251823A (en) | Adjustable atomizing orifice liquid fuel burner | |
| US3920187A (en) | Spray head | |
| US3747851A (en) | Swirl air nozzle | |
| US20120168538A1 (en) | Spin Annular Slit Spray Nozzle and Spray Apparatus Thereof | |
| US4526322A (en) | Flow-reversing nozzle assembly | |
| US2414459A (en) | Fluid fuel burner apparatus | |
| US2530206A (en) | Spray gun | |
| US4394965A (en) | Pulsating shower using a swirl chamber | |
| US4261517A (en) | Atomizing air metering nozzle | |
| US2999647A (en) | Mist and spray production method and nozzle designs for its usage | |
| US3702175A (en) | Flat spray fuel nozzle | |
| US3149783A (en) | Method of merging at least two streams of fluid into a single body of liquid | |
| US1593186A (en) | Atomizer for liquid fuel and the like | |
| US3537650A (en) | Two-stage sonic atomizing device | |
| CN108160359B (en) | Nozzle device capable of realizing multiple spraying functions | |
| US3968931A (en) | Pressure jet atomizer | |
| US2674493A (en) | Atomizer | |
| GB1210699A (en) | Two-stage sonic atomizing device | |
| US1750602A (en) | Device for vaporizing liquids | |
| US2650860A (en) | Improvement in hollow cone spray nozzle | |
| US2044091A (en) | Atomizer | |
| RU2039910C1 (en) | Nozzle for spraying viscose liquid |