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US2929563A - Process for generating aerosol and apparatus therefor - Google Patents

Process for generating aerosol and apparatus therefor Download PDF

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US2929563A
US2929563A US632332A US63233257A US2929563A US 2929563 A US2929563 A US 2929563A US 632332 A US632332 A US 632332A US 63233257 A US63233257 A US 63233257A US 2929563 A US2929563 A US 2929563A
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annular
conduit
gas
orifice
aerosol
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US632332A
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Jones James Byron
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Aeroprojects Inc
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Aeroprojects Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/12Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/06Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane
    • B05B7/062Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane with only one liquid outlet and at least one gas outlet
    • B05B7/065Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane with only one liquid outlet and at least one gas outlet an inner gas outlet being surrounded by an annular adjacent liquid outlet

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  • the present invention relates to a process for generating aerosols and apparatus therefor, and more particularly to a process for generating aerosols within a selected particle size range, in which the distribution of various particle sizes is maintained within narrow limits; and to a nozzle for producing such aerosolized particles.
  • substantially all prior aerosol generators capable of handling liquids or slurries at a bulk liquid velocity in excess of about one milliliter per second are incapable of delivering such relatively large volumes in the form of aerosols having a major weight percentage of aerosolized droplets of a diameter of below ten microns.
  • Prior equipment has been developed by me capable of producing aerosol droplets having a particle size of ten microns diameter or less in high yield and within a relatively small size range distribution.
  • Such equipment comprises a multiple orifice nozzle having a barrier spaced from and facing at least the centermost orifice.
  • barrier type nozzle constitutes one of the most efficient forms of aerosol generators yet developed, if not the most efiicient aerosol generator yet developed, it suffers from certain handicaps in certain areas of use. These handicaps arise due to the necessity for positioning the barrier in respect to the orifices by means of struts which extend from the housing comprising the orifices to the barrier.
  • the struts adversely affect the resultant flame due to their action as impingement surfaces in respect to the aerosol droplets.
  • the struts serve as surfaces upon which coke or other carbonaceous materials deposit. These coke and carbonaceous materials act as secondary combustion centers and adversely affect the nature of the flame developed by the aerosol particles.
  • the presence of the struts within the combustion chamber frequently leads to the conflagrant or corrosive consumption of the struts with attendant shutdowns for repairs.
  • This invention has as an object the provision of a novel process for generating aerosols.
  • This invention has as another object the provision of a process for generating particles of liquids, or other aerosolizable substances, or slurries of a size difiicult to achieve by prior processes and apparatus.
  • This invention has as yet another object the provision of a process for producing aerosols in which at least a This invention has as a still further object the pro-' vision of a process for producing aerosols comprising small size particles having a narrow size range distribution.
  • This invention has as a difierent object the provision of a method for producing small size aerosol particles of liquid, or slurries, at a relatively rapid rate.
  • This invention has as yet a diflerent object the pr vision of apparatus for forming aerosol particles of small sizes.
  • This invention has as a further object the provision of apparatus for converting large amounts of a liquid, or slurry into aerosol particles at a relatively rapid rate.
  • This invention has as yet another object the provision of apparatus for producing aerosol particles of diameters less than ten microns.
  • This invention has as a still further object the provision of apparatus for producing small size aerosol particles within a relatively narrow size range.
  • Figure 4 is a longitudinal sectional view of another embodiment of the apparatus of the present invention.
  • the apparatus of the present invention is designated generally as 10.
  • the apparatus 10 comprises a nozzle which in accordance with the process of the present invention should discharge into the open atmosphere, or into a gaseous atmosphere, if the process is conducted under conditions where air or oxygen is to be excluded.
  • the aspiration of gas from the surrounding atmosphere through the material being aerosolized is desirable and preferable for the proper functioning of the apparatus 10.
  • the apparatus 10 includes a center conduit 12.
  • the outermost end portion of center conduit 12 is provided with internal splines 14 which segregate the interior of center conduit 12 into a plurality of channels 16, 18 and 26 (see, in particular, Figure 2). While three channels 16, 18, and 20 are shown in the drawings, it is to be understood that a larger or smaller number of such channels may be utilized.
  • the splines 14- are press-fitted into center conduit 12 and are preferably integral with a cap 22 which is longitudinally disposed to conduit 12.
  • the outer end of cap 22 is preferably streamlined, e.g. tapered or generally conical, to permit aspiration circulation of gas from the surrounding atmosphere, as will be more fully explained below.
  • the cap 22 faces and blocks the channels 16, 18 and 20.
  • An annular aperture 24 is positioned intermediate the free edge 26 of cap 22 and the free edge 28 of center conduit 12.
  • the annular aperture 24 should not varysubstantially
  • the centerconduit 12 is concentrically disposed within-a conduit 30 (see Figures 1 and 3).
  • the disposition of center conduit 12 in respect to conduit 30 is maintained by splines 32, which are external and which are for convenience'integral with conduit 12.
  • conduit 30 The interior of conduit 30 is provided with a plurality of -channels 34, 36, and 38 defined by splines 32. ' While threechannels 34, 36 and 38 are shown in the drawings, itis'j to be understood that a largeror smaller number of channels may be-utilizedwithin conduit 30.
  • the conduit 30 is provided with an inlet 40, preferably tangential as shown in the drawings, positioned in back (if-splines 32.
  • the rear portion 42 of conduit 30 extends radially: inwardly and is secured to center conduit 12.
  • Conduit 30 discharges forwardly through annular orifice 44 defined by an inwardly directed lip 46;
  • the dimensioning of annular orifice. 44 is critical and should, in all cases, be between 0.0005 and 0;030 inch.
  • the annular orifice 44 should.
  • conduit 30 not vary substantially about its360 degrees of circularity so, that an annular discharge of uniform configuration will be had.
  • the inwardly directed lip 46 of conduit 30 be provided at its innermost;.-edge 48 with as. narrow a land as possible, e.g.
  • the discharge orificefor conduit 50 comprises annular. orifice 56 defined by an inwardly. directed lip 58.
  • the annular orifice 56 is spaced tothe rear of annular orifice 44.
  • the size, of the opening of annular orifice 56 should becontrolled,: and the narrowest portion thereof should preferably be'within the range 0.0005 inch to about 0.050 inch. Asa general rule, for liquids of very low viscosity or low; surface tension the smaller size for orifice 56 is to be preferred, whereas for very viscous liquids the larger'size for orifice 56 is to be preferred.
  • the annular orifice-56 should not vary substantially about its 360 degrees of circularity so that an annular discharge of uniform-configuration will be had.
  • the innermost edge 60 of lip 58 should be maintained as small as possible, but as with the innermost edge 48, itis difiicult in practice to maintain an innermotslt edge havingdimensions of lessthan 0.008 to 0010 me The, outermostsurface of the lip 58. should; be curved,
  • the curvature of lip 46 should comprise a continuation of the curvature of lip 58 or a conical tangent thereto.
  • the curvature of the lips 46 and 58 in the manner set forth above provides for the facile passage of gas from the ambient atmosphere due to aspiration by the streams discharged from the annular orifice 44 and the annular aperture 24. I have found that the presence of a sharp corner intermediate the outer surface of conduit 50 and lip 58 or a discontinuous noncurved or irregular outer surface of'the lip 46 or lip 58"interferes with the optimum performance of the apparatus 10.
  • Propellant gas is introduced into center conduit 12 and from inlet 40 into conduit 30. It is essential for superior performance that at least one of the gas streams, namely the gas stream discharged from center conduit 12 or the gas stream discharged from conduit 30 be moving at a supersonic velocity when it' leaves the conduit. In. a preferred. embodiment, both the gas stream discharged from annular aperture 24 of center conduit 12 andthe gas. stream discharged from annular orifice 44 of conduit 30 are discharged at supersonic velocities.
  • the material to be aerosolized is preferably introduced through'inlet 54 into conduit 50 and discharged through annular orifice 56 of conduit 50.
  • the material intro Jerusalem through inlet 54 may comprise a liquid, or a slurry comprising finely divided solids dispersed within a liquid.
  • the gas discharged from annular aperture24 is directed. radially in the illustrated embodiment.
  • the form of pattern of the gasrdischarge may be varied, as to a radial pattern, or a more angularly deflected pattern.
  • the gas discharged from annular orifice 44 impinges upon the umbrella-like pattern from the annular aperture 24, which serves as a gaseous'barrier;
  • the material being aerosolized from conduit 50 passes over the outer surface of lip 46 within and about the gaseous sleeve issuingfrom on'fice 44 and is aspirated with the gas from conduit 30 along the outer surface of center conduitv 12 until.
  • the aspiration of gas w from the ambient atmosphere into and through the material from conduit 50 is aspirated into the material undergoing aerosolization from both sides of the pattern from annular aperture 24.
  • the streamlined shape of cap 22 and the rounded surfaces of lips '58 and'46 provide for ease of access of the aspirated gas to the material being aerosolized.
  • This aspirated gas acts to carry: the discharging aerosol away from its relatively diminutive zone of generation into a' greater volume, so that the formed aerosol particles are to reagglomerate I a
  • the subject apparatus and process permit a marked degree of control.
  • the velocity of the gas in the conduits 12 and 30 may be independently altered.
  • the shape of the pattern resulting from the combination of the discharges from annular aperture 24 and annular orifice 44 may be altered. This permits the subject apparatus and process to achieve resultant aerm solized particles of desired characteristics. Moreover, the shape of the pattern may be altered to conform to the shape of the container within which the apparatus is positioned. For a narrow container, a conical pattern is normally most advantageous; Whereas for a relatively broad container a pattern approximating a circular disc is advantageous. This control is also efiicacious when the nozzle is located within a moving gas stream.
  • Convenient adjustment of the pressures in conduits 12 and 40 can, for example, cause the discharging aerosol to mix thoroughyy with a gas moving axially of the nozzle in a duct or pipe, even to the extent when the gas is moving at velocities approaching the speed of sound.
  • the material to be aerosolized may be introduced into conduit 30 from inlet 40 and discharged from annular orifice 44 thereof, while aerosolizing gas is introduced from center conduit 12 to be discharged from annular aperture 24 thereof and further aerosolizing gas is introduced from inlet 54 into conduit 50 and discharged through annular orifice 56 thereof.
  • This mode of operation effects an exceptionally turbulent action in the zone of aerosolization.
  • the apparatus 10a generally resembles that of Figures 1, 2 and 3 except that the conduit 50 is eliminated, and the lip 46a has a rounded corner 47 to provide for facile aspiration of gas from the ambient atmosphere into the discharge from annular orifice 44a.
  • the material undergoing aerosolization such as the liquid, or slurry of finely dispersed particles is introduced along with gas through the conduit 30a.
  • the combined gas and material mixture is discharged from annular orifice 44a and impinges upon the pattern from annular aperture 24a.
  • either the gas I stream from annular aperture 24a or the mixture stream from annular orifice 44a, or preferably both such streams, should be moving at supersonic velocities at their time of discharge.
  • the dimensioning of the aperture 24a and the orifice 44a should conform to the dimensions heretofore set forth for annular aperture 24 and annular orifice 44, namely that the narrowest portion of annular aperture 24a should have a size of from 0.0005 inch to 0.030 inch and the narrowest portion of annular orifice 44a should have a size of from 0.0005 inch to 0.030 inch (the passage in each of these openings is substantially uniform about the entire 360 degrees of cicularity).
  • a minimal thickness of the land at the edge 48a of lip 46a is desirable, and the distance between annular orifice 44 and annular aperture 24 should be maintained for the annular orifice 44a and the annular aperture 24a.
  • the apparatus 10 shown in Figures 1, 2, and 3 is to be preferred over the apparatus 10a shown in Figure 4 because of the greater degree of control which may be efiected due to the regulation of the independent gas stream in the gas conduits 12 and 30. This permits greater regulation of size and shape of spray pattern, and control of aerosol particle sizes.
  • the aerosolized liquid material was aerosolized to particles having a size less than 8 microns, the particle size ranges being distributed entirely within the size range of somewhat below 1 micron to 8 microns, with 42 weight percent of the particles having a size of less than 4 microns.
  • the mean resultant aerosol particle size diameter was 4.6 microns.
  • a process for aerosolizing a material into very finely divided aerosol particles which comprises associating a rapidly moving annular stream of the material to be aerosolized with a first rapidly moving coaxial thin annular gas stream, the annular stream of the material to be aerosolized being of larger inside diameter than said first annular gas stream at the moment of association, impinging said mixed gas and material streams against an angularly directed rapidly moving annular gas stream, said angularly directed gas stream being angularly directed in respect to both the initial direction of movement of said first annular gas stream and also the initial direction of movement of the annular stream of material to be aerosolized, whereby aerosolized particles are formed, and minimizing the reagglomeration of the aerosolized particles by spacing such aerosolized particles away from each other through engagement with gas.
  • each of the streams in the process is initially moving at a supersonic velocity.
  • Apparatus for forming aerosolized particles comprising at least three concentric tubes, one end of the innermost tube projecting beyond the end of the next adjacent concentric tube, said one of said innermost tube having a smaller outer diameter along the entire portion of its length which projects beyond the end of the next adjacent concentric tube than the smallest inside diameter of the next adjacent concentric tube to said innermost tube, a cap juxtaposed to said one end of said innermost tube, said cap having a smaller outside diameter along its entire length than the smallest inside diameter of the next adjacent concentric tube to said innermost tube, cap supporting means extending through said innermost tube, said cap supporting means joining together the inner wall of said innermost tube and said cap, at least one channel in said cap supporting means, an annular aperture intermediate said one end of said innermost tube and said cap, said channel being in communication with the interior of said innermost tube: and said. annular aperttn'e,

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  • Chemical & Material Sciences (AREA)
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Description

March 22, 1960 J. B. JONES 9,
PROCESS FOR GENERATING AEROSOL AND APPARATUS THEREFOR Filed Jan. s. 1957 Fig.3
o 38 I I 36 l4 Fig. 4
Y 220 w E g g x \l I r v 0 A k we 4ou h 47 'L INVENTOR. JAMES BYRON JONES i M a. W
' ATTORNEY United States Patent PRDCESS F011 GENERATING AEROSOL AND APPARATUS THEREFOR James Byron Jones, West Chester, Pa., assignor to Aeroprojects, 1138., West Chester, Pa., a corporation of Pennsylvania Application January 3, 1957, Serial No. 632,332
8 tllaims. (Cl. 239-8) The present invention relates to a process for generating aerosols and apparatus therefor, and more particularly to a process for generating aerosols within a selected particle size range, in which the distribution of various particle sizes is maintained within narrow limits; and to a nozzle for producing such aerosolized particles.
A variety of processes for generating aerosols and aerosolization equipment have heretofore been suggested. It is, however, very difficult to produce aerosols in which substantially all of the particles are characterized by dimensions smaller than a diameter of about ten microns. Furthermore, it is most difficult with most prior processes and apparatus to obtain small size aerosol particles within a relatively narrow size distribution range.
In particular, substantially all prior aerosol generators capable of handling liquids or slurries at a bulk liquid velocity in excess of about one milliliter per second are incapable of delivering such relatively large volumes in the form of aerosols having a major weight percentage of aerosolized droplets of a diameter of below ten microns.
Prior equipment has been developed by me capable of producing aerosol droplets having a particle size of ten microns diameter or less in high yield and within a relatively small size range distribution. Such equipment comprises a multiple orifice nozzle having a barrier spaced from and facing at least the centermost orifice.
While the aforesaid barrier type nozzle constitutes one of the most efficient forms of aerosol generators yet developed, if not the most efiicient aerosol generator yet developed, it suffers from certain handicaps in certain areas of use. These handicaps arise due to the necessity for positioning the barrier in respect to the orifices by means of struts which extend from the housing comprising the orifices to the barrier.
For example, when the use of the generator is to erosolize a combustible liquid, as for example fuel oil or the like, which is to be burnt while in the aerosolized state, the struts adversely affect the resultant flame due to their action as impingement surfaces in respect to the aerosol droplets. Thus, the struts serve as surfaces upon which coke or other carbonaceous materials deposit. These coke and carbonaceous materials act as secondary combustion centers and adversely affect the nature of the flame developed by the aerosol particles. Moreover, the presence of the struts within the combustion chamber frequently leads to the conflagrant or corrosive consumption of the struts with attendant shutdowns for repairs.
This invention has as an object the provision of a novel process for generating aerosols.
This invention has as another object the provision of a process for generating particles of liquids, or other aerosolizable substances, or slurries of a size difiicult to achieve by prior processes and apparatus.
This invention has as yet another object the provision of a process for producing aerosols in which at least a This invention has as a still further object the pro-' vision of a process for producing aerosols comprising small size particles having a narrow size range distribution.
This invention has as a difierent object the provision of a method for producing small size aerosol particles of liquid, or slurries, at a relatively rapid rate.
This invention has as yet a diflerent object the pr vision of apparatus for forming aerosol particles of small sizes.
This invention has as a further object the provision of apparatus for converting large amounts of a liquid, or slurry into aerosol particles at a relatively rapid rate.
This invention has as yet another object the provision of apparatus for producing aerosol particles of diameters less than ten microns.
This invention has as a still further object the provision of apparatus for producing small size aerosol particles within a relatively narrow size range.
Other objects will appear hereinafter.
For the purpose of illustrating the invention there is shown in the drawings forms which are presently preferred; it being understood, however, that this invention is not limited to the precise arrangements and instru-' Figure 3 is a cross sectional view taken on line 33 of Figure 1.
Figure 4 is a longitudinal sectional view of another embodiment of the apparatus of the present invention.
Referring initially to Figures 1, 2 and 3, wherein the preferred embodiment of the present invention is shown, the apparatus of the present invention is designated generally as 10. The apparatus 10 comprises a nozzle which in accordance with the process of the present invention should discharge into the open atmosphere, or into a gaseous atmosphere, if the process is conducted under conditions where air or oxygen is to be excluded. Thus, as will be more fully explained below, the aspiration of gas from the surrounding atmosphere through the material being aerosolized is desirable and preferable for the proper functioning of the apparatus 10.
The apparatus 10 includes a center conduit 12. The outermost end portion of center conduit 12 is provided with internal splines 14 which segregate the interior of center conduit 12 into a plurality of channels 16, 18 and 26 (see, in particular, Figure 2). While three channels 16, 18, and 20 are shown in the drawings, it is to be understood that a larger or smaller number of such channels may be utilized.
The splines 14- are press-fitted into center conduit 12 and are preferably integral with a cap 22 which is longitudinally disposed to conduit 12. The outer end of cap 22 is preferably streamlined, e.g. tapered or generally conical, to permit aspiration circulation of gas from the surrounding atmosphere, as will be more fully explained below. As will be seen from Figure 1, the cap 22 faces and blocks the channels 16, 18 and 20.
An annular aperture 24 is positioned intermediate the free edge 26 of cap 22 and the free edge 28 of center conduit 12.
I have found that the size dimensioning of the annular Patented Mar. 22, 1960 v approximate a circular knife edge.
24 is critical ifsatisfactory aerosolization is to bis-accomplished. In particular, I have found that the narrowest part of the annular aperture 24 should be maintained within the size range 0.0005 to. 0.030 inch.
The annular aperture 24 should not varysubstantially The centerconduit 12 is concentrically disposed within-a conduit 30 (see Figures 1 and 3). The disposition of center conduit 12 in respect to conduit 30 is maintained by splines 32, which are external and which are for convenience'integral with conduit 12.
The interior of conduit 30 is provided with a plurality of - channels 34, 36, and 38 defined by splines 32. 'While threechannels 34, 36 and 38 are shown in the drawings, itis'j to be understood that a largeror smaller number of channels may be-utilizedwithin conduit 30.
The conduit 30 is provided with an inlet 40, preferably tangential as shown in the drawings, positioned in back (if-splines 32. The rear portion 42 of conduit 30 extends radially: inwardly and is secured to center conduit 12.
1 Conduit 30 discharges forwardly through annular orifice 44 defined by an inwardly directed lip 46; As with the annular aperture 24, the dimensioning of annular orifice. 44: is critical and should, in all cases, be between 0.0005 and 0;030 inch. The annular orifice 44 should.
not vary substantially about its360 degrees of circularity so, that an annular discharge of uniform configuration will be had. Moreover, it is desirable that the inwardly directed lip 46 of conduit 30 be provided at its innermost;.-edge 48 with as. narrow a land as possible, e.g.
Practical machining operations prevent a satisfactory edge 48 for most materials of less than 0.008 to 0.010 inch, but where possible, this;land dimension should not be exceeded.
'I:hej longitudinal spacing between the innermost edge 28.of,annular aperture24 and the innermost edge 48 of annular orifice 44 is critical to achieve optimum operation app ratus 10. I have found that with most, if not all materials, thisdistance between the land of 48 and the nearest edge of'annular orifice 24 should be in the range -of one-fifth to three times the diameter of lip 46 at the 4k conduit 50 is concentrically dispised in respect to conduit 30 and center conduit 12.. The. disposition of Conduit 50 in respect to conduit 30 is maintained by securing the rear portion 52 of conduit 50 to theouter surface of conduit30. The conduit 50 is providedwith an inlet 54, preferably a tangential inlet, as shown in the drawings.
The discharge orificefor conduit 50 comprises annular. orifice 56 defined by an inwardly. directed lip 58. The annular orifice 56 is spaced tothe rear of annular orifice 44. The size, of the opening of annular orifice 56 should becontrolled,: and the narrowest portion thereof should preferably be'within the range 0.0005 inch to about 0.050 inch. Asa general rule, for liquids of very low viscosity or low; surface tension the smaller size for orifice 56 is to be preferred, whereas for very viscous liquids the larger'size for orifice 56 is to be preferred. The annular orifice-56 should not vary substantially about its 360 degrees of circularity so that an annular discharge of uniform-configuration will be had. It is desirable that the innermost edge 60 of lip 58 should be maintained as small as possible, but as with the innermost edge 48, itis difiicult in practice to maintain an innermotslt edge havingdimensions of lessthan 0.008 to 0010 me The, outermostsurface of the lip 58. should; be curved,
surface of the lip 58. The curvature of lip 46 should comprise a continuation of the curvature of lip 58 or a conical tangent thereto.
The curvature of the lips 46 and 58 in the manner set forth above provides for the facile passage of gas from the ambient atmosphere due to aspiration by the streams discharged from the annular orifice 44 and the annular aperture 24. I have found that the presence of a sharp corner intermediate the outer surface of conduit 50 and lip 58 or a discontinuous noncurved or irregular outer surface of'the lip 46 or lip 58"interferes with the optimum performance of the apparatus 10.
The operation of the apparatus 10 of the present invention is as follows: 7 p
Propellant gas is introduced into center conduit 12 and from inlet 40 into conduit 30. It is essential for superior performance that at least one of the gas streams, namely the gas stream discharged from center conduit 12 or the gas stream discharged from conduit 30 be moving at a supersonic velocity when it' leaves the conduit. In. a preferred. embodiment, both the gas stream discharged from annular aperture 24 of center conduit 12 andthe gas. stream discharged from annular orifice 44 of conduit 30 are discharged at supersonic velocities. In order to achieve supersonic velocities forthe discharged gas stream in the apparatus 10, it is necessary that the gas from center conduit 12 and/or conduit 30 (depending upon whether one or both of the discharge streams from the conduits are moving at supersonic velocity) be pressurized at a pressure of 1.5 atmospheres or more within the conduit. f
The material to be aerosolized is preferably introduced through'inlet 54 into conduit 50 and discharged through annular orifice 56 of conduit 50. The material intro duced through inlet 54 may comprisea liquid, or a slurry comprising finely divided solids dispersed within a liquid.
The gas discharged from annular aperture24 is directed. radially in the illustrated embodiment. By varying the discharge nature of annular aperture 24, the form of pattern of the gasrdischarge may be varied, as to a radial pattern, or a more angularly deflected pattern. The gas discharged from annular orifice 44 impinges upon the umbrella-like pattern from the annular aperture 24, which serves as a gaseous'barrier; The material being aerosolized from conduit 50 passes over the outer surface of lip 46 within and about the gaseous sleeve issuingfrom on'fice 44 and is aspirated with the gas from conduit 30 along the outer surface of center conduitv 12 until. im-
achieved due to a number of means, such as the drawing of the liquid from the surface of lip 46 into and about the gaseous stream issuingfrom orifice 44, thereby maximizing the surface area of the liquid. Further, the impingement of the liquid now mixed with or embracing the gaseaus stream from orifice 44 upon the high-velocity gaseous umbrella issuing from aperture 24 disrupts the liquidlvolume which'has had its surface area maximized by embracement and mixing with thegas stream, issuing from orifice 44 into an exceedingly fine aerosol.
Of importance to the resulting aerosolization achieved by the" apparatus 10 of'the presentinvention is the aspiration of gas w from the ambient atmosphere into and through the material from conduit 50. Gas is aspirated into the material undergoing aerosolization from both sides of the pattern from annular aperture 24. The streamlined shape of cap 22 and the rounded surfaces of lips '58 and'46 provide for ease of access of the aspirated gas to the material being aerosolized. This aspirated gas acts to carry: the discharging aerosol away from its relatively diminutive zone of generation into a' greater volume, so that the formed aerosol particles are to reagglomerate I a The subject apparatus and process permit a marked degree of control. Thus, the velocity of the gas in the conduits 12 and 30 may be independently altered. In this manner, the shape of the pattern resulting from the combination of the discharges from annular aperture 24 and annular orifice 44 may be altered. This permits the subject apparatus and process to achieve resultant aerm solized particles of desired characteristics. Moreover, the shape of the pattern may be altered to conform to the shape of the container within which the apparatus is positioned. For a narrow container, a conical pattern is normally most advantageous; Whereas for a relatively broad container a pattern approximating a circular disc is advantageous. This control is also efiicacious when the nozzle is located within a moving gas stream. Convenient adjustment of the pressures in conduits 12 and 40 can, for example, cause the discharging aerosol to mix thoroughyy with a gas moving axially of the nozzle in a duct or pipe, even to the extent when the gas is moving at velocities approaching the speed of sound.
In some cases, where exceptionally turbulent action is desired between the gas streams and the material undergoing aerosolization, as for example, when chemical reaction between the gas streams and the material undergoing aerosolization is desired, the material to be aerosolized may be introduced into conduit 30 from inlet 40 and discharged from annular orifice 44 thereof, while aerosolizing gas is introduced from center conduit 12 to be discharged from annular aperture 24 thereof and further aerosolizing gas is introduced from inlet 54 into conduit 50 and discharged through annular orifice 56 thereof. This mode of operation effects an exceptionally turbulent action in the zone of aerosolization.
In the apparatus embodiment shown in Figure 4, the apparatus 10a generally resembles that of Figures 1, 2 and 3 except that the conduit 50 is eliminated, and the lip 46a has a rounded corner 47 to provide for facile aspiration of gas from the ambient atmosphere into the discharge from annular orifice 44a.
In the embodiment of Figure 4, the material undergoing aerosolization such as the liquid, or slurry of finely dispersed particles is introduced along with gas through the conduit 30a. The combined gas and material mixture is discharged from annular orifice 44a and impinges upon the pattern from annular aperture 24a.
The operation of the apparatus embodiment 10a is therefore generally similar to the operation of the apparatus embodiment shown in Figures 1, 2 and 3. In
the apparatus embodiment of Figure 4, either the gas I stream from annular aperture 24a or the mixture stream from annular orifice 44a, or preferably both such streams, should be moving at supersonic velocities at their time of discharge. Moreover, the dimensioning of the aperture 24a and the orifice 44a should conform to the dimensions heretofore set forth for annular aperture 24 and annular orifice 44, namely that the narrowest portion of annular aperture 24a should have a size of from 0.0005 inch to 0.030 inch and the narrowest portion of annular orifice 44a should have a size of from 0.0005 inch to 0.030 inch (the passage in each of these openings is substantially uniform about the entire 360 degrees of cicularity). In addition, a minimal thickness of the land at the edge 48a of lip 46a is desirable, and the distance between annular orifice 44 and annular aperture 24 should be maintained for the annular orifice 44a and the annular aperture 24a.
The apparatus 10 shown in Figures 1, 2, and 3 is to be preferred over the apparatus 10a shown in Figure 4 because of the greater degree of control which may be efiected due to the regulation of the independent gas stream in the gas conduits 12 and 30. This permits greater regulation of size and shape of spray pattern, and control of aerosol particle sizes.
An illustration of the results which may be achieved with the apparatus of the present invention, a mixture comprising 46 parts by weight of glycerol, 2 parts by weight of Brilliant Benzo blue dye (marketed by General Dyestufi Corporation, 123 South Second Street, Philadelphia, Penna), and 52 parts by weight of water was aerosolized using the apparatus of Figures 1, 2, and 3 with air being discharged from both the conduits 12 and 30 at supersonic velocities. The aerosolization was efiected with the temperature and humidity controlled so that the resultant aerosol particles would neither shrink in size nor grow in size on formation, and would thereby permit exact size measurement.
It was found that one hundred percent of the aerosolized liquid material was aerosolized to particles having a size less than 8 microns, the particle size ranges being distributed entirely within the size range of somewhat below 1 micron to 8 microns, with 42 weight percent of the particles having a size of less than 4 microns. The mean resultant aerosol particle size diameter was 4.6 microns.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof and, accordingly, reference should be made to the appended claims, rather than to the foregoing specification as indicating the scope of the invention.
I claim:
1. A process for aerosolizing a material into very finely divided aerosol particles which comprises associating a rapidly moving annular stream of the material to be aerosolized with a first rapidly moving coaxial thin annular gas stream, the annular stream of the material to be aerosolized being of larger inside diameter than said first annular gas stream at the moment of association, impinging said mixed gas and material streams against an angularly directed rapidly moving annular gas stream, said angularly directed gas stream being angularly directed in respect to both the initial direction of movement of said first annular gas stream and also the initial direction of movement of the annular stream of material to be aerosolized, whereby aerosolized particles are formed, and minimizing the reagglomeration of the aerosolized particles by spacing such aerosolized particles away from each other through engagement with gas.
2. A process in accordance with claim 1 in which the process is effected in a gaseous atmosphere and in which simultaneously with the deflection of the material to be aerosolized and the first annular gas stream upon the angularly directed gas stream substantial amounts of gas from the surrounding gaseous atmosphere are aspirated into the streams.
3. A process in accordance with claim 1 in which at least one of the streams is initially moving at supersonic velocity.
4. A process in accordance with claim 3 in which each of the streams in the process is initially moving at a supersonic velocity.
5. Apparatus for forming aerosolized particles comprising at least three concentric tubes, one end of the innermost tube projecting beyond the end of the next adjacent concentric tube, said one of said innermost tube having a smaller outer diameter along the entire portion of its length which projects beyond the end of the next adjacent concentric tube than the smallest inside diameter of the next adjacent concentric tube to said innermost tube, a cap juxtaposed to said one end of said innermost tube, said cap having a smaller outside diameter along its entire length than the smallest inside diameter of the next adjacent concentric tube to said innermost tube, cap supporting means extending through said innermost tube, said cap supporting means joining together the inner wall of said innermost tube and said cap, at least one channel in said cap supporting means, an annular aperture intermediate said one end of said innermost tube and said cap, said channel being in communication with the interior of said innermost tube: and said. annular aperttn'e,
with,- sa-id next adjacent concentric tube to the innermost tube: having an; annular discharge orificesurrounding the; outer surface of, said innermost tube, saidv annular dis'-- tric tube and discharging along the outer surface of said nextadjacent concentric tube parallel to the longitudinal axis of the innermosttube;
6! Apparatus in accordance with claim in which the outermost surface of the next adjacent concentric tubeto: the innermost tubeand the outermost surface of the concentric tube which is disposed about the next'adjacent concentric tube are both rounded inthe region of, their respective annular discharge orifice and annular-discharge opening with suchrounded surfaces being a continuation of each other. i
=7. Apparatus in accordance with claim 6 in which the annular discharge orifice of the next adjacent concentric.
8 tube in the annular dischargeopening oi the concentric tube which is; disposed about the next adjacent; conccn: tric tube are both'provided with inwardly directed: lips; whose outermost surfaces form, the curved surfaces de' finedtin claimS. I
j 8. Apparatus in accordance with claim 5 having tube support means joining together the inner wall of the next adjacentconcentric tube to the innermost tube and. the outer wall of the innermost tube with at least one channel extending through said tube support means.
References Cited in the file of this patent UNITED STATES PATENTS l,1 24; 789l Naudain Jan. 12,1915 1,321,358 Beck Nov. 11, 1919 13799551 Forney V Apr. 7, 1.931- '2;555 ,0,85 Goddard May 29, 1951 2,738,230 Pillard Mar. 13, 1956' 2770 5011 Coanda Nov.- 13, &
7 FOREIGN PATENTS 259,242 Switzerland June 16,1949 294,042. Germany Sept. 9,. 1916; 437,460 Italy July s, 1943. 499,641 Belgium Mar. 16, 1951'.
5968.38. Germany- May 11, 1934
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Publication number Priority date Publication date Assignee Title
US3112882A (en) * 1960-03-21 1963-12-03 Beckman Instruments Inc Pump for liquids
US3915384A (en) * 1975-03-13 1975-10-28 Richard E Diggs Combination irrigation and temperature control system for plants
US4271100A (en) * 1979-06-18 1981-06-02 Instruments S.A. Apparatus for producing an aerosol jet
CN106216129A (en) * 2016-08-23 2016-12-14 无锡市湖昌机械制造有限公司 Cleaning machine drip washing shower nozzle

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US1124789A (en) * 1914-02-17 1915-01-12 John E Naudain Oil-burner for heating.
US1321358A (en) * 1919-11-11 Burner
US1799551A (en) * 1929-04-01 1931-04-07 Forney Comb Engineering Compan Oil and steam burner nozzle
DE596838C (en) * 1931-10-08 1934-05-11 Karl Molnar Dipl Ing Atomizers for liquid fuels, especially for oil firing
CH259242A (en) * 1946-05-31 1949-01-15 Charbonnage Et De Combustibles Liquid fuel burner with spray effect.
US2555085A (en) * 1948-05-15 1951-05-29 Daniel And Florence Guggenheim Two-liquid feeding reflecting device for combustion chambers in propulsion apparatus
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US1321358A (en) * 1919-11-11 Burner
US1124789A (en) * 1914-02-17 1915-01-12 John E Naudain Oil-burner for heating.
US1799551A (en) * 1929-04-01 1931-04-07 Forney Comb Engineering Compan Oil and steam burner nozzle
DE596838C (en) * 1931-10-08 1934-05-11 Karl Molnar Dipl Ing Atomizers for liquid fuels, especially for oil firing
CH259242A (en) * 1946-05-31 1949-01-15 Charbonnage Et De Combustibles Liquid fuel burner with spray effect.
US2555085A (en) * 1948-05-15 1951-05-29 Daniel And Florence Guggenheim Two-liquid feeding reflecting device for combustion chambers in propulsion apparatus
US2738230A (en) * 1950-06-26 1956-03-13 Pillard Marcel Liquid fuel burners
US2770501A (en) * 1952-09-23 1956-11-13 Sebac Nouvelle Sa Means for the atomization of liquids

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3112882A (en) * 1960-03-21 1963-12-03 Beckman Instruments Inc Pump for liquids
US3915384A (en) * 1975-03-13 1975-10-28 Richard E Diggs Combination irrigation and temperature control system for plants
US4271100A (en) * 1979-06-18 1981-06-02 Instruments S.A. Apparatus for producing an aerosol jet
CN106216129A (en) * 2016-08-23 2016-12-14 无锡市湖昌机械制造有限公司 Cleaning machine drip washing shower nozzle

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