US3790086A - Atomizing nozzle - Google Patents

Atomizing nozzle Download PDF

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Publication number
US3790086A
US3790086A US00256372A US3790086DA US3790086A US 3790086 A US3790086 A US 3790086A US 00256372 A US00256372 A US 00256372A US 3790086D A US3790086D A US 3790086DA US 3790086 A US3790086 A US 3790086A
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Prior art keywords
gas
liquid
guide surface
flow
ejecting
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US00256372A
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English (en)
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T Masai
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Hitachi Ltd
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Hitachi Ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02—Spray pistols; Apparatus for discharge
    • B05B7/04—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02—Spray pistols; Apparatus for discharge
    • B05B7/04—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0441—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber
    • B05B7/0466—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber with means for deflecting the central liquid flow towards the peripheral gas flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02—Spray pistols; Apparatus for discharge
    • B05B7/04—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0441—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber
    • B05B7/0475—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of liquid surrounded by an external conduit of gas upstream the mixing chamber with means for deflecting the peripheral gas flow towards the central liquid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02—Spray pistols; Apparatus for discharge
    • B05B7/06—Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane
    • B05B7/062—Spray 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
    • B05B7/065—Spray 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02—Spray pistols; Apparatus for discharge
    • B05B7/10—Spray pistols; Apparatus for discharge producing a swirling discharge
    • 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
    • F23D11/10—Burners 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
    • F23D11/106—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
    • F23D11/107—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion

Definitions

  • Gas is gener- May 24, 1971 Japan 46/35757 comically swirled along the front face of a nozzle end while liquid is ejected into the gas flow, in combi- ⁇ g g 239/406 239/426 nation with means for preventing the recombination of I I u s s u s s u u s u [58] Flew of s g ig f g 2 4 adjacent the liquid ejection ports.
  • the recombination l is particularly prevented by gas ejection downstream from the liquid ejection and the downstream projec- [5 6] References C'ted tion of the recombination surface into the whirling gas UNITED STATES PATENTS flow.
  • the atomizer nozzle according to the present invention is particularly suitable for atomizing liquid fuel of low quality andhigh viscosity, such as heavy oil.
  • FIG. 1 is a longitudinal cross-sectional view taken from the flow access of an atomizing nozzle according to one embodiment of the present invention
  • FIG. 2 is a longitudinal cross-sectional view of the gas swirler of the embodiment according 'to FIG. 1;
  • FIG. 3 is a front view of the swirler shown in FIG. 2;
  • FIG. 4 is a longitudinal cross-sectional view of the nozzle body in FIG. 1;
  • FIG. 5 is a front view of the nozzle body shown in FIG. 4;
  • FIG. 6 is a longitudinal.cross-sectional view of the cap of FIG. 1;
  • FIG. 7 is a partial cross-sectional view showing a detail of a variation for the joints between the gas swirler and the nozzle body for forming a gas seal;
  • FIG. 8 is a longitudinal cross-sectional view through another embodiment of the present invention.
  • FIG. 9 is a longitudinal cross-sectional view of still a further embodiment of the present invention.
  • FIG. 10 is a longitudinal cross-sectional view of another embodiment of the present invention.
  • FIG. 11 is a longitudinal cross-sectional view of a still further embodiment of the present invention.
  • FIG. 12 is a variation of the embodiment according to FIG. 11;
  • FIG. 13 is a somewhat schematic view showing the gas flow within the gas passages of the atomizin g nozzle shown in FIG. 10;
  • FIG. 14 is a partial longitudinal cross-sectional view of a known atomizing nozzle showing the liquid recom bination phenomena.
  • FIG. 15 is a longitudinal cross-sectional view of the known nozzle according to.FIG. 14 after it has been in use, showing the buildup of carbon resulting from the recombination phenomena.
  • the nozzle body DETAILED DESCRIPTION OF THE DRAWING the nozzle body and in turn is surrounded or enclosed by'a cap 5, which is shown alone in FIG. 6.
  • the predominately cylindrical nozzle-body l' is provided with a central passage 10 for conducting liquid. from a source liquid under pressure to be atomized, which source is not shown in the drawing.
  • the nozzle body further has a plurality of peripherally spaced projections 11, which extend radially outwardly from its otherwise cylindricalouter surface.
  • the outermost portions of the projections 11 are provided with screw threads so that the gas swirler 3 may be threaded thereon, with the internal threads 30 of the gas swirler 3 engaging the external threads of the projections 11 on the nozzle body L
  • This construction forms a plurality of peripherally spaced openings or gas passages 21 defined by adjacent projections 11, the internal surface of the swirler 3, and the external surfaces 13 of the body 1 between projections 11.
  • These gas passages 21 communicate with an annular gas chamber 39 formed between the nozzle body 1 and the forward or down stream portion of the interior of the gas swirler 3.
  • the annular chamber 39 feeds gas under pressure to an annular gas reservoir 24 in the central portion 16 of the downstream end of the nozzle body 1 by means of a plurality of gas passages 19 formed in the nozzle body 1.
  • the annular gas reservoir 24 is defined by the central portion 16 of the nozzle body, the spacer collar or sleeve 4 that is telescopically assembled on the boss 18 of the nozzle body formed in the center of the central portion 16, and the tip 22 that is fixed to the boss 18 by means of welding or the like 25. In this manner, a gap or annular space 23 is formed between the conical face 17 of the down stream end of the nozzle body 1 and a correspondingly shaped face on the tip 22.
  • the size of the gap or space 23 is determined by the axiallength of the collar or spacer sleeve 4, and this space 23 functions as a gas ejecting port communicating with and receiving gas under pressure from the gas reservoir 24.
  • the outer tapered face 34 of the gas swirler 3 is provided with a plurality of radial and inclined veins, with respect to the axis of the nozzle, which axis lies within the plane of FIG. 1 and is further the axis of symetry for most of the nozzle portions.
  • These vanes 36 which may be of any conventional design form a plurality of gas passages that will eject gas in cooperation with the tapered face 51 of the cap 5, which ejected gas will be conically swirled as it moves axially to the left or downstream as shown in FIG.'1.
  • the cross section, in the flow direction, for the gas passages between adjacent vanes 36 of the swirler 3 will be made tapered so as to obtain the maximum flow velocity in the vicinity of the outlet of the vane part.
  • the gas passage cross-section between adjacent veins 36 will be made preferably convergent, at least for its downstream portion, to obtain the maximum flow velocity'at the outlet or the vicinity of the outlet of the vanes 36, the theory of which is known in nozzle design for subsonic and supersonic gas flow. These design criteria are highly desirable to obtain the maximum conversion of gas pressure into gas velocity to raise the atomization efficiency of the nozzle.
  • the present invention may be employed with a nozzle wherein the flow crosssection between the gas swirler vanes 36 may be uniform throughout its flow direction, that is unchanged, when such is necessary due to restrictions in working or construction. Further, rounded corners are very effective for the construction of these parts to prevent a contracted flow from occurring at the inlet of the vanes 36 of the swirler 3.
  • liquid ejecting ports or holes provided in the outer surface of the nozzle body 1, which ports 15 communicate with the high pressure liquid within the central passage 10.
  • the previously described gas ejection port 23 is located further downstream from the liquid ejecting ports 15, and projects through the same outer surface of the nozzle body 1.
  • the gas is highly compressed by means of a compressor or the like to supply high pressure gas to the gas chamber 7 between the nozzle body 1 and the cap 5, which will feed gas through the annular passage 71 de fined by the cap and the gas swirler 3 to the vanes 36.
  • the gas After travelling through the vanes 36, the gas is ejected in a conical and swirling flow with respect tothe axis of the nozzle body.
  • the liquid or fuel is supplied under pressure to the central passage 10 within nozzle body 1 to flow through the ejecting ports 15. In this manner,
  • the liquid flowing from the ports 15 is atomized by the velocity energy of the swirling gas immediately down stream from the outlet 38 of the vanes 36, so that the liquid is picked up by and swirled with the gas.
  • This swirling or vortex flow is then projected into the furnace 6 through an annular passage formed by the tapered face 53 of the cap 5 and the tapered face or surface 20 of the nozzle body 1, which surface 20 is immediately downstream from the liquid ejecting ports 15.
  • the liquid ejected to the air flow in the passage formed by an inner portion of the cap 5 d1 and outer portion of the swirler or nozzle body 3111 at least partially recombines downstream from the liquid ejecting port to adhere to the surface of the nozzle body downstream from the liquid ejecting port to become a liquid film, which grows in thickness as other previously atomized droplets recombine with the film; such as known as the recombination phenomena.
  • the above flow diversion for the prevention of the recombination phenomena is accomplished according to the embodiment of FIG. 1 of the present invention by directing high pressure gas from the passage 7, through the passages 21, through the annular space 39, through the passages 19, through the gas reservoir 24, and through the ejecting port 23.
  • the gas ejected through the port 23 into the vortex flow of mixed gas and lliquid will cause the vortex flow to swerve at its outer limits back from the nozzle axis so that the once atomized liquid will not recombine and adhere to the wall or surface downstream from the liquid ejecting ports 15, which surface is particularly formed by the nozzle body 1 and tip 22.
  • atomization of the liquid will be improved.
  • the tapered surfaces 52 and 53 at the downstream end of the cap 1 are conically formed with respect to the nozzle axis.
  • the inner oor upstream tapered surface 23 has two functions. When the velocity and force of the liquid ejected from the liquid ejecting ports 15 is very high, there is the undesirable possibility that the liquid will completely penetrate the main flow of gas from gas swirler and completely pass by the swirler 3 before it is atomized, leading to poor overall atomization.
  • One of the functions of the tapered surface 52 is to prevent this penetration of the ejected liquid by forming a blocking surface against which the liquid will strike to be diverted back into the gas flow.
  • the other function of the tapered surface 52 is to keep constant the maximum flow velocity of the main gas flow passing from the vanes 36 of the swirler 3 within the region of the inner taper 52 from the outlet 38 of the vanes 36 within the vicinity of the liquid ejecting ports to improve the effectiveness of the liquid atomization. Since stream lines of the main gas flow containing liquidparticles are turned outwards by the gas flow ejecting from the ejecting port 23, the outer tapered surfaceportion 53 of the cap 5 is divergent in shape, in the direction of fluid flow. If the surface 53 were no so formed, there would be the possibility that the recombination phenomena of the the liquid particles would occur on such a surface as 53 without the divergent shape.
  • the screw parts may be fixed by other methods, for example, by employing hook pins or by meshing the swirler 3 and the nozzle body 1 with each other.
  • the surfaces 13 form the bottom or inner portions of the gas passages 21 between adjacent projections 11 on the nozzle body 1.
  • FIG. 7 A variation of this gas-seal between the swirler 3 and nozzle body 1 is shown in FIG. 7, wherein a step construction is employed for the seal surface 35 and the adjacent surface of the nozzle body 1 to form a tortuous flow path seal.
  • air passages or spaces 21, particularly shown in FIGS. 1 and 5, are shown as slots as in a splined shaft, these flow passages 21 may also be formed by circular axial holes perforating the swirler 3 that would extend down to the nozzle body 1 0r perforating the projection 11 that would extend upwardly to the swirler 3 from the nozzle body 1.
  • the engaging tapered surfaces 31 of the swirler 3 and 14 of the nozzle body 1, for determining the axial position of the swirler 3 and nozzle body 1 maybe omitted in some instances.
  • FIG. 8 A second embodiment of the present invention is shown in FIG. 8 for atomizing liquid, and the above description will suffice except with respect to points of differences which will be described below.
  • the vanes 36a are constructed differently from the vanes'36 of FIG. I so that the tapered surface 52 of the first embodiment is not needed in the embodiment of FIG. 8; However, a similar result will be obtained with FIG. 8 in that the vanes extend over the direction of the liquid ejection from the liquid ports 15a.
  • the air passages 21 of the embodiment according to FIG. I are replaced by a plurality of radial air passages 21a as shown in FIG. 8 passing through the swirler 3a for supplying air to the annular space 39a.
  • the passages 21a will bleed off the boundary layer and air adjacent thereto flowing to the vanes 36 to provide a smooth redirecting of the main gas flow from the annular space corresponding to space 71 in FIG. 1 to the directional flow through the vane 36a.
  • FIG. 9 differs from the embodiment of FIG. 1 in that two annular gas ejecting ports 23b, and 2312 are provided downstream from the liquid ejecting ports 15b, instead of the provision of only one downstream gas ejecting port 23 as in FIG. 1.
  • the dimensions of the gas vortexes 94 produced downstream from the liquid ejecting ports 15c vary depending not only on the diameter of the liquid ejecting ports 15c, but also on the flow rates of the gas and liquid, that is, the running conditions.
  • FIG. 10 A further embodiment of the present invention is shown in FIG. 10, which differs from the embodiment of FIG. I in that gas is supplied to the annular gas space 390 by a plurality of gas sucking or bleed ports 210 between the vanes 36c and through the wall of the swirler 3c.
  • This construction differs from the construction of FIG. 8, in that the boundary layer and adjacent gases are sucked from the main gas stream as it flows between the vanes 360 instead of as it flows between the swirler 3a and cap 50 of FIG. 8 in the space corresponding to the space 71 of FIG. 1. In this manner, the deflecting effect of the main flow gas in the annular passage 71c that was brought out with respect to the description in the embodiment of FIG. 8, is further promoted.
  • FIG. 13c illustrates the difference between the velocity distribution 91 between the vanes and immediately donwstream therefrom in FIG. 1 and the veocity distribution 92 according to the embodiment of FIG. 10 due to the removal of the boundary layer by the bleed passages 21c.
  • a similar result would be obtained by removal of the boundary layer with the passages 21a in the embodiment of FIG. 8.
  • the atomization of the 2-fluid spray will be more effective, because the velocity of the gas flowing immediately adjacent or across the liquid ejecting ports will be higher and the velocity gradient from the wall will be greater.
  • FIG. 11 A further embodiment of the present invention is shown in FIG. 11 for diverting the gas liquid atomized mixture to prevent recombination. Again, only the differences from the previously described embodiments will be described in detail.
  • the nozzle body is provided with a liquid passage d that is eccentric with respect to the nozzle axis and a gas passage 7d, which is similarly eccentric.
  • the liquid passage 10d supplies high pressure liquid to the liquid reservoir 83 between the interior of the gas swirler 8 and the nozzle body, in front of the nozzle body.
  • Gas swirler 8 is provided with a plurality of gas ejecting vanes 36a to eject the gas, such as air, to the interior of the furnace 6 in a whirling conical fashion, in combination with liquid ejected from the liquid ejecting ports 81 communicating with the liquid reservoir 83.
  • the central portion of the gas swirler 8 is provided with an annular surface 82 parallel with the axis of the nozzle, which surface 82 could also be formed by a portion of the nozzle body.
  • the gas will flow from the gas passage 7d through the passage 21d to the annular gas reservoir 39d, where it is supplied to the vanes 36d.
  • the cap 5d is secured to the nozzle body by means of threads or the like 55d to form therewith the annular gas reservoir space 39d.
  • the compressed gas is ejected from the vanes 36d in a whirling conical path to atomize the liquid ejected from the liquid ejection ports 81.
  • the liquid film that would tend to appear on the outer surface of the gas swirler 8 downstream from the liquid ejecting ports 81 due to the recombination phenomena as described with respect to FIG. 14 at 96 is prevented from occurring by means of the parallel surface portion 82 at the downstream terminal end of the gas swirler 8.
  • the liquid film 96 that tned's to appear in the known nozzles as shown in FIG. 14 becomes'quite thick with highly viscous fuels such as heavy oil; However, it has been experimentally proved that making the boundary layer quite thin according to the embodiments of the present invention has a most desirable effect.
  • the parallel surface portion 82 of the swirler 8 in FIG. 11 will tend to divert the gas liquid boundary layer flow from the wall of the swirler toward the main gas flow.
  • a similar diversion of the gasliquid boundary layer flow is obtained according to the variation of the embodiment of FIG. 11 as shown in FIG. 12, wherein arcuate surface 82' at the front or terminal end of the swirler 8 will even moresharply direct the gas-liquid boundary layer flow back into'the main swirling gas flow.
  • the configuration of the ejecting part may be made concave to prevent the boundary layer of the ejected flow on the side of liquid ejecting ports from being developed.
  • FIG. 15 The resultsof the recombination phenomena for the known nozzles of FIG. 14 are shown in FIG. 15, wherein solid carbon 97 has developed on the front central section of the nozzle with a surface 98 as an extension of the surface on which the liquid film forms. Such a buildup of carbon is prevented with the present invention.
  • the boundary layer of relatively slow velocity fluid along the surface that has extending therethrough the liquid ejecting ports is considerably reduced in thickness as compared to the known nozzles by the various means including sucking off the boundary layer upstream of the liquid ejecting ports, blowing the boundary layer back into the main gas flow by ejecting air downstream of the liquid ejecting ports and providing a surface projection downstream of the liquid ejecting ports for turning the boundary layer back into the main gas flow.
  • the bleeding or sucking off of the boundary layer will produce a thinner, higher velocity boundary layer as shown in FIG.
  • An atomizing nozzle for atomizing liquid within a gas comprising:
  • said diverting means further including means for ejecting gas through said guide surface downstream from said means for ejecting liquid to divert the gas-liquid boundary layer away from said guide surface toward the main gas flow.
  • the atomizing nozzle according to claim 1 including common means for supplying gas under pressure to both said means for directing gas and said means for ejecting gas.
  • bleed passage means extending into said air passage up stream from said liquid ejecting means for. bleeding at least the gas boundary layer that would otherwise form along said guide surface and supplying it to said means for ejecting gas.
  • the atomizing nozzle according to claim 2 including a nozzle body having a central downstream conical surface forming at least in part said guide surface, a downstream opening annular recess concentrically inwardly of said conical surface, and a downstream projecting central member at least in part forming said annular recess; said nozzle body further having a second conical surface oppositely directed from said firstmentioned conical surface and extending between said first-mentioned conical surface and said annular recess; a spacer sleeve surrounding said projecting member within said annular recess for only a portion of the axial extent of said projectingmember; and a nozzle tip surrounding the remaining portion of said projecting member and tightly abutting said spacer sleeve; said nozzle tip having a conical surface complementary to and spaced from said nozzle body second conical surface to form therebetween an annular passage extending from said annular recess through said guide surface; and said common ,means including said annular recess.
  • said gas directing means includes a generally annular gas whirler mounted on said nozzle body to form therebetween an annular gas chamber, and having an annuar array of blades to project the gas flow in a whirling cone terminating at least closely adjacent said first mentioned nozzle body conical surface; a cap member surrounding said annular array of blades and being outwardly spaced from the remainder of said gas whirler and said nozzle body to form therebetween a main gas passage leading to the downstream end of said blades, which gas passage forms in part said common means; said common means further including gas passage means extending between said main gas passage and said annular gas chamber.
  • the atomizing nozzle according to claim 7, including threaded means between said gas whirler and said nozzle body; said gas whirler and nozzle body having complementary seal surfaces immediately adjacent the downstream end of said blades and upstream from said liquid ejecting means, and said seal surfaces having an interference fit and extending generally parallel to the axis of said threaded means.
  • An atomizing nozzle for atomizing liquid within a gas comprising:
  • the atomizing nozzle according to claim .12 wherein said gas directing means includes an annular array of blades to project the gas flow in a whirling cone along said guide surface upstream from said means for ejecting liquid; and said bleed passage means extending between said blades.
  • An atomizing nozzle for atomizing liquid within a gas comprising:
  • said diverting means including a projection from said guide surface downstream of said liquid ejecting means for'changing the direction of the fluid boundary layer moving along said surface to direct ittoward the main gas flow to be broken up thereby and to decrease the angle between the fluid boundary layer flow and the direction of flow for the liquid ejected by said liquid ejecting means;
  • said gas directing means including an annular array of blades forming an annular flow of main gas, and said liquid ejecting means being annular and projecting.
  • said liquid in an annular path having an axis of symmetry substantially concentric with the axis of symmetry of the main gas flow annular path; and said projection means having an annular surface generally parallel to said axes, and at its upstream end angularly joining said guide surface.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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US00256372A 1971-05-24 1972-05-24 Atomizing nozzle Expired - Lifetime US3790086A (en)

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JP46035757A JPS5141693B1 (US06486227-20021126-C00005.png) 1971-05-24 1971-05-24

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Cited By (59)

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US3887135A (en) * 1973-11-15 1975-06-03 Shigetake Tamai Gas-atomizing nozzle by spirally rotating gas stream
US3904119A (en) * 1973-12-05 1975-09-09 Avco Corp Air-fuel spray nozzle
US3963182A (en) * 1972-12-21 1976-06-15 Aqua-Chem, Inc. Burner
US4017253A (en) * 1975-09-16 1977-04-12 The United States Of America As Represented By The United States Energy Research And Development Administration Fluidized-bed calciner with combustion nozzle and shroud
US4111369A (en) * 1977-07-05 1978-09-05 General Motors Corporation Fuel nozzle
US4141505A (en) * 1976-06-07 1979-02-27 Reich Richard B Heavy fuel oil nozzle
FR2412352A1 (fr) * 1977-12-23 1979-07-20 Gema Ag Appareil pulverisateur de liquides
US4216174A (en) * 1977-12-31 1980-08-05 Osrodek Badawczo-Rozwojowy Samochodow Malolitrazowych "Bosmal" Method and apparatus for preparation and control of an air-fuel mixture
US4267979A (en) * 1979-11-19 1981-05-19 Howe-Baker Engineers, Inc. Dual-phase atomizer
WO1982000106A1 (en) * 1980-06-27 1982-01-21 Res Center Inc Adelphi Oil burner nozzle
US4347982A (en) * 1979-07-02 1982-09-07 Adelphi Research Center, Inc. Oil burner nozzle
US4368850A (en) * 1980-01-17 1983-01-18 George Szekely Dry aerosol generator
US4461425A (en) * 1982-07-13 1984-07-24 Respiratory Care, Inc. Nebulizer system
EP0128805A2 (en) * 1983-06-03 1984-12-19 Forney Engineering Company Twin fluid atomizer
US4498629A (en) * 1982-05-26 1985-02-12 Shell Oil Company Apparatus for vaporization of a heavy hydrocarbon feedstock with steam
EP0167049A2 (de) * 1984-06-29 1986-01-08 Linde Aktiengesellschaft Verfahren zum Verbrennen eines Brennstoffes
US4836453A (en) * 1988-02-22 1989-06-06 Outboard Marine Corporation Fuel injector with continuous air flow
EP0408801A1 (en) * 1988-01-29 1991-01-23 Ohkawara Kakohki Co., Ltd. Spray drying apparatus
US5227017A (en) * 1988-01-29 1993-07-13 Ohkawara Kakohki Co., Ltd. Spray drying apparatus equipped with a spray nozzle unit
US5228624A (en) * 1992-03-02 1993-07-20 Mensink Daniel L Swirling structure for mixing two concentric fluid flows at nozzle outlet
US5499768A (en) * 1989-05-31 1996-03-19 Ohkawara Kakohki Co., Ltd. Spray nozzle unit
US5641124A (en) * 1992-10-08 1997-06-24 Abb Flakt Ab Apparatus for cleaning gas
WO1998001705A1 (en) * 1996-07-08 1998-01-15 Corning Incorporated Gas-assisted atomizing device
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