EP3204168A1 - Buse de pulvérisation - Google Patents

Buse de pulvérisation

Info

Publication number
EP3204168A1
EP3204168A1 EP14784032.6A EP14784032A EP3204168A1 EP 3204168 A1 EP3204168 A1 EP 3204168A1 EP 14784032 A EP14784032 A EP 14784032A EP 3204168 A1 EP3204168 A1 EP 3204168A1
Authority
EP
European Patent Office
Prior art keywords
liquid
mixing chamber
channel
nozzle
gas
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.)
Granted
Application number
EP14784032.6A
Other languages
German (de)
English (en)
Other versions
EP3204168B1 (fr
Inventor
Jochen PAAL
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Spraying Systems Manufacturing Europe GmbH
Original Assignee
Spraying Systems Manufacturing Europe GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Spraying Systems Manufacturing Europe GmbH filed Critical Spraying Systems Manufacturing Europe GmbH
Publication of EP3204168A1 publication Critical patent/EP3204168A1/fr
Application granted granted Critical
Publication of EP3204168B1 publication Critical patent/EP3204168B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0491Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid the liquid and the gas being mixed at least twice along the flow path of the liquid
    • 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
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0441Spray 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
    • B05B7/0466Spray 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
    • 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
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0483Spray 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 gas and liquid jets intersecting in the mixing chamber
    • 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
    • B05B7/08Spray pistols; Apparatus for discharge with separate outlet orifices, e.g. to form parallel jets, i.e. the axis of the jets being parallel, to form intersecting jets, i.e. the axis of the jets converging but not necessarily intersecting at a point
    • B05B7/0892Spray pistols; Apparatus for discharge with separate outlet orifices, e.g. to form parallel jets, i.e. the axis of the jets being parallel, to form intersecting jets, i.e. the axis of the jets converging but not necessarily intersecting at a point the outlet orifices for jets constituted by a liquid or a mixture containing a liquid being disposed on a circle
    • 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
    • B05B7/10Spray pistols; Apparatus for discharge producing a swirling discharge

Definitions

  • the invention relates to an atomizer nozzle which can be used on spraying devices for spraying liquids.
  • the nebulizer nozzle may be arranged on mobile or stationary sprayers.
  • Atomizing nozzles are used for fine atomization of a liquid supplied to the atomizing nozzle, for example water , or a liquid mixture which may also contain additives, such as cleaning agents or the like.
  • a liquid supplied to the atomizing nozzle
  • a liquid mixture which may also contain additives, such as cleaning agents or the like.
  • the following is spoken of a liquid, wherein such liquid mixtures should also be included.
  • compressed gas is used which is mixed with the liquid ⁇ speed in a mixing chamber and the Zerstäu ⁇ bung supported.
  • the atomized by means of the compressed gas liquid is discharged as an atomized spray jet at least one outlet opening of the spray nozzle.
  • the spray nozzle can be used in various fürsbe ⁇ rich, for example, for the Versprü ⁇ hen of fertilizers, pesticides or fungicides in agriculture or for moistening or cooling of objects in industrial production, for spraying water and / or detergent or chemical Industry to facilitate the evaporation of liquid by atomizing.
  • the atomizer nozzle can be used wherever a very fine atomizing a Liquid is needed.
  • An atomizer nozzle is known, for example, from EP 0 714 706 B1.
  • the spray nozzle has a liquid ⁇ keitsan gleich and a gas port.
  • the liquid ⁇ keitsan gleich is fluidly connected to a liquid channel which extends coaxially along a nozzle axis and opens into a mixing chamber.
  • the liquid ⁇ keitsstrom flows as a jet along the nozzle axis in the mixing chamber.
  • Radially to the nozzle axis open into the mixing chamber several in etechnischskanäle which are fluidly connected to the gas port.
  • the axial liquid flow is atomized via the gas flowing transversely thereto and discharged downstream along the nozzle axis through an outlet opening to the outside.
  • the atomizer nozzle has a liquid port for supplying a liquid.
  • the liquid may be a single liquid or a liquid mixture.
  • the liquid connection is connected to a liquid channel through which the supplied liquid flows and which opens downstream into a ring mixing chamber.
  • the ring ⁇ mixing chamber encloses a nozzle axis of the atomizer nozzle annular and is arranged coaxially with the nozzle axis.
  • An end section opening directly into the ring mixing chamber expands toward the ring mixing chamber.
  • the outer diameter of the end portion becomes larger toward the ring mixing chamber. In this end portion may preferably be arranged a central part.
  • the nozzle axis may preferably penetrate the centering ⁇ ralteil center.
  • a flow layer is formed from the air passing through the end portion liquid vergiert of the nozzle axis away di ⁇ and preferably completely circumferentially about the due ⁇ senachse is closed annularly.
  • the strö ⁇ tion layer is directed obliquely away from the nozzle axis.
  • a hollow-conical or hollow-frustum-shaped flow layer which may also be referred to as a liquid ⁇ keitsfilm forms.
  • the ring mixing chamber connects.
  • the liquid of the flow ⁇ layer flows from the end portion in the ring mixing chamber.
  • any pressurized gas or gas ⁇ can as a pressurized gas mixture at any temperature and / or pressure every use, regardless of the saturation vapor pressure and / or the critical temperature of the gas or gas mixture.
  • Compressed gas can be used, for example, compressed air and / or nitrogen and / or hydrogen. Steam can also be used as compressed gas in some applications, for example water vapor.
  • To the gas line system includes at least one outer In ekomskanal and at least one inner In ekomskanal. Via the injection channels pressurized gas is introduced into the annular mixing chamber ⁇ .
  • the outer injection channel opens at an outer injection site and the inner Injetationska ⁇ nal opens at an inner injection site in the ring ⁇ mixing chamber.
  • the inner injection site is enclosed by the ring mixing chamber extending coaxially around the nozzle axis.
  • the gas flows from outside and inside into the ring ⁇ mixing chamber and meets there on the flow layer.
  • the pressurized gas is directed from the radially outer and radially inner ge ⁇ gen the hollow truncated cone-shaped flow layer.
  • the outer injection site and the inner injection site are in the extension direction of the ring mixing chamber offset from one another.
  • Under the ER of the annular mixing chamber stretch direction is the course of the center plane through the annular mixing chamber beginning at Endab ⁇ section of the liquid passage to the outer end of the annular mixing chamber in front of the at least one outlet opening to understand.
  • the extension direction of the ring mixing chamber therefore does not relate to its course in the circumferential direction about the nozzle axis, but at right angles thereto along the center plane.
  • the outer and inner Injekti ⁇ onsstelle can also be arranged opposite to each other in the extension direction of the ring mixing chamber.
  • the inner Injekti ⁇ onsstelle is disposed upstream in the direction of extension of the annular mixing chamber to the outer site of injection.
  • the supplied via the internal gas pressure injection site ⁇ it divides the flow of liquid towards a radial component and a component of flow to the outer site of injection.
  • pressurized gas is also supplied, whereby a further improved atomization is generated in small flues ⁇ stechniksp motherboard by at ⁇ motionless and the radially outwardly directed flow component.
  • gas streams may also include a shearing effect acting on the flow layer, which is particularly the case when the outer and inner injection site ⁇ in He stretch direction of the annular mixing chamber offset but are disposed close to each other .
  • a spatially close arrangement of the two injection sites is to be understood that the inflowing gas from one of the two injection sites at least partially directly to the other injection site or a directly adjacent to the other injection ⁇ onsstelle wall section impinges.
  • the inflowing gas from one of the two injection sites at least partially directly to the other injection site or a directly adjacent to the other injection ⁇ onsstelle wall section impinges.
  • the inflowing gas from one of the two injection sites at least partially directly to the other injection site or a directly adjacent to the other injection ⁇ onsstelle wall section impinges.
  • a preferred embodiment are in the ⁇ nere In ekomsstelle before a Hauptausströmraum which intersects the central plane of the annular mixing chamber at a first angle.
  • the outer injection ⁇ point specify a Hauptausströmraum intersecting the center plane of the annular mixing chamber at a second angle.
  • the amount of the second angle is smaller than the amount of the first angle.
  • the first angle may be, for example, in a range of 45 ° to 90 °, preferably between 60 ° and 90 °.
  • the second angle is for example less than 70 ° and preferably less than 45 °.
  • the gas line system fluidly connects the inner injection channel and the outer injection channel with the gas connection.
  • the compressed gas provided at the gas connection thus flows into both injection channels.
  • the gas ⁇ line system is designed such that the gas flow rate, which flows through the outer injection channel into the ring mixing chamber is greater than the gas flow rate, which flows through the inner injection channel into the ring mixing chamber.
  • the air flowing into the annular mixing chamber via the injection channel outer gas volume flow can be more than 50% and preferably up to 80% of the total gas volume ⁇ current that flows through the two injection ports in the annular mixing chamber.
  • gas volumetric flow rates of less than 50% or more than 80% may optionally also be selected.
  • Preferably, in the circumferential direction are distributed around the nozzle axis and, for example in accordance with the same peripheral portion distributed more outlet openings ⁇ present.
  • the outlet openings preferably each have a rotationally symmetrical shape and may, for example, be cylindrical and / or widening and / or designed as a Laval nozzle.
  • a further improvement of the atomization of the liquid is achieved in one embodiment, characterized in that the annular mixing chamber between the In edictionsstellen and the at least one outlet opening in the direction of the nozzle axis one or more times curved course ⁇ has.
  • the annular mixing chamber can, viewed in the direction of the nozzle axis, curve toward the nozzle axis and / or away from the nozzle axis.
  • the ring mixing chamber is in a preferred embodiment rotationally symmetrical to the nozzle axis out ⁇ leads.
  • the nebulizer nozzle may include a spin agent.
  • the swirl generating means is arranged to divide the air flowing into the liquid ⁇ keitskanal and in particular in the end portion of the flues ⁇ stechnikskanals liquid has a swirl to it ⁇ .
  • the swirl generating means may be formed, for example, in that a Einströmmündung for supplying the liquid into the liquid passage with respect to the nozzle axis radially offset and obliquely. Characterized the einströ ⁇ Mende in the liquid channel liquid is already helical flow with a swirl along the liquid channel.
  • the swirl generating means may comprise a swirl generator, which is arranged in the liquid channel and in particular upstream of the Endab ⁇ section of the liquid channel.
  • the swirl generator ⁇ is flown by the liquid and gives the liquid flow is twisted. This can be effected by inclined and / or helical guide surfaces and / or guide channels and / or by a rotor of the swirl generator, for example an impeller.
  • all known swirl generation means may be used alone or in combination ⁇ nation.
  • the swirler is located upstream at the end portion of remplisstechnikska ⁇ Nals subsequent swirl-generating portion of the liquid in a ⁇ keitskanals.
  • the swirl generating portion may be located upstream of and in close proximity to a transition portion of the liquid passage leading to the end portion and having a cross section or diameter tapering towards the end portion.
  • the standing of the liquid available Strömungsquerab ⁇ cut in the swirl generating section may in Strö ⁇ flow direction be substantially constant.
  • the Gas einssys ⁇ tem has a central channel which extends along the nozzle axis in the central part.
  • the central channel opens in the central part in the liquid channel.
  • Pressurized gas may be substantially out of the centering ⁇ ralkanal against the axial Flow direction component of the liquid immediately upstream of the end portion of the liquid passage ⁇ flow and there contribute to an improved design of the hollow cone-shaped flow layer.
  • the atomizer nozzle in one embodiment has a nozzle body in which the liquid channel and the ring mixing chamber are formed.
  • the nozzle body is preferably made integrally from a material without seam and joining ⁇ point .
  • it can be manufactured by so-called ⁇ additive manufacturing process such as 3D-printing process. It is also preferred if all fluid-carrying lines and channels are formed in this nozzle body.
  • the central part is an integral part of this nozzle body.
  • Figure 1 is a perspective view of an embodiment of an atomizing nozzle exporting approximately ⁇
  • FIG. 3 shows a schematic, block diagram-like schematic representation of the atomizer nozzle according to the invention.
  • a spray nozzle 10 is veran ⁇ illustrates.
  • Figures 1 and 2 show a preferred execution from ⁇ example, while Figure 3 shows the functional principle ver anschaubit ⁇ .
  • the atomizer nozzle 10 is used in a mobile or sta tionary ⁇ spray device and serves to atomize a liquid supplied to F using compressed gas L and the finely atomized liquid particles as a spray or S dispense spray.
  • the flowing liquid F is schematically illustrated by block arrows and the pressurized gas L by simple arrows.
  • the dot density is illustrated in Figure 3 shows schematically the fine atomization of the liquid F, wherein a lower dot density represents a fine ⁇ res sputtering.
  • the atomizing nozzle 10 has a nozzle housing 11. On the nozzle housing, a liquid port 12 for supplying the liquid F and a gas port 13 for supplying the compressed gas L is present.
  • the liquid connection 12 is arranged on a hollow cylindrical connecting piece 14 of the nozzle housing 11.
  • the connecting piece 14 is arranged coaxially to a nozzle axis A.
  • the gas connection 13 is arranged at ⁇ play according to ring around the connecting piece 14 coaxial with the nozzle axis A.
  • the number and arrangement of the gas connection 13 or of the liquid connection 12 can also be provided in a different arrangement and alignment with the nozzle housing 11, depending on the spray device on which the atomizer nozzle 10 is used.
  • the nozzle housing 11 has an approximately cylindrically contoured shape.
  • housing part IIa of which the connecting piece 14 of the nozzle housing 11 protrudes.
  • the housing portion IIa is arranged coaxially with the SI ⁇ senachse A.
  • the gas connection 13 is arranged coaxially around the connecting piece 14 in an end wall of the housing part IIa.
  • a Malawian ⁇ handle section IIb may be provided with one or more surfaces for a tool, for example, to rotate the atomizer nozzle 10 during its attachment to a spray device in the circumferential direction U about the nozzle axis A and mechanically and fluidly connect to the spray.
  • the nozzle housing 11 is, for example embodied as according ein Communityi ⁇ ger, integral nozzle body 15 and can for example be produced as 3D printing or by any other additive method of manufacture.
  • the nozzle body 15 is free of seams and joints and is made of a uniform material.
  • the fluid port 12 is fluidly connected to a fluid passage 19.
  • first portion 19a of the liquid passage 19 has a cylindrical shape and it ⁇ coaxially extends to the nozzle axis A.
  • first section 19a includes a Drallerzeugungsab ⁇ section 19b of the liquid channel 19 at.
  • a swirl generator 20 is angeord ⁇ net, of a swirl it divides the fluid F, which flows from the first section 19a in the swirl generating section 19b ⁇ .
  • the swirl generator 20 is formed in the embodiment by a swirler 21 which is arranged coaxially with the nozzle axis A in the swirler section 19b.
  • the swirl body 21 may have guide surfaces or guide channels in order to impart a spin to the liquid F. It is also possible to use a swirl generator 20 with a paddle wheel.
  • one or more suitable swirl generating means may be used to impart a twist to the liquid as it flows into the liquid channel 19 or while flowing in the liquid channel 19. It is also possible to use flow effects, such as the Co-anda effect for twisting. It is au ⁇ ßerdem possible, the inflow of the fluid F in the fluid passage 19 radially offset to the nozzle axis A, tan ⁇ gential perform to a channel wall 22 of the liquid passage 19 and inclined to the nozzle axis A, so that be ⁇ already achieved a swirling liquid flow becomes.
  • Swirl generator 20 a baffle body in the liquid channel 19 are arranged (not illustrated), which is suitable, for example. Substantially plate-shaped, so that upon impact of a liquid F on the baffle a thin, substantially plate-shaped liquid layer is generated, which also serves as a baffle referred to as.
  • transition section decreases in the flow direction. This is achieved by the diameter of the swirl-generating section 19b or transition section starting from the first section 19a decreasing.
  • ⁇ swirl generation is completed immediately before the transition section.
  • the diameter of the liquid channel 19 in the Drallerschiungsab may be omitted ⁇ section 19b constant and the tapered transition portion, which is by way of example schematically illustrated in the schematic diagram according to FIG. 3
  • an end portion 19c of the liquid passage 19 includes ge ⁇ optionally at about the transition portion.
  • the diameter of the channel ⁇ wall 22 increases from the swirl-generating portion 19 b away.
  • the liquid flowing along the channel wall 22 has a tendency to continue to flow along the channel wall 22, starting from the smallest channel wall diameter at the transition point between the swirl-generating portion 19b and the end portion 19c.
  • a flow layer FH of the liquid F forms in the end section, which has the shape of a hollow truncated cone.
  • the flow layer FH is formed coaxially with the nozzle axis A in the atomizer nozzle 10.
  • the flow layer FH is highly schematically in figure 3 by the block arrows and dots in the end portion 19c veran ⁇ illustrated.
  • a central part 25 is arranged in the end section 19c of the liquid channel, the diameter of which widens to form a ring mixing chamber 26, into which the liquid channel 19 opens.
  • the ring mixing chamber 26 directly adjoins the end section 19c of the liquid channel 19.
  • the central part 25 is penetrated centrally from the nozzle axis A. Due to the arrangement of the central part 25 and the widening channel cross section of the end portion 19 c, the end portion 19 c is designed as a coaxial with the nozzle axis A, in the circumferential direction U around the nozzle axis A annularly closed, hollow truncated cone-like channel.
  • the passage wall 22 of the liquid passage 19 is curved in the swirl generating portion 19b and the end portion 19c along the nozzle axis A.
  • Drallerzeugungsab ⁇ section 19b of the channel cross-section is thereby reduced and increased again at the end portion 19c.
  • the outer surface 27 of the central part 25 along the Dü ⁇ senachse A is also curved and, for example, concave ge ⁇ curved.
  • the outer surface 27 of the central part 25 is opposite the channel wall 22 and is preferably adapted to the profile of the channel wall, that the radial distance to the nozzle axis A between the outer surface 27 of the central part 25 remains substantially constant to the outer inner wall of the end portion 19c, wherein the annular flow cross-sectional area in the downstream direction increases with increasing distance to the nozzle axis A.
  • a hollow frustum-shaped flow layer FH is thus generated in front of the annular mixing ⁇ chamber 26, which flows into the annular mixing chamber 26.
  • a swirl-generating means and / or the widening end section 19c with the central part 25 arranged therein can be used. Example According to both measures are implemented ge ⁇ jointly.
  • the gas line system 28 includes an outer injection channel 29 which extends in the circumferential direction U around the nozzle axis A annularly around at least a portion of the liquid passage 19 around and at an outer In ekomsstelle 30 opens into the ring mixing chamber 26.
  • the outer injection point 30 is designed as an annular gap and arranged coaxially with the nozzle axis A.
  • annular connecting channel 31 of the embodiment Gas line system 28 disposed in the nozzle housing 11, which is fluidly connected via one or more passage openings 32 with a central gas passage 33 of the gas line system 28.
  • the central gas channel 33 extends along the nozzle axis A and is enclosed by the ring mixing chamber 26 in the circumferential direction U.
  • the inner In etechnischskanal 34 may be formed by a portion of the central gas channel 33 or separated by partitions branch off the central gas channel 33.
  • the inner injection channel 34 opens into an annular injection chamber 35 at an inner injection site 35.
  • the inner injection site 35 is provided as a preferably closed in the circumferential direction U about the nozzle axis A, mög ⁇ lichst performed uninterrupted annular gap.
  • a central channel 36 is fluidly connected to the central ⁇ eral gas passage 33 branched from the central gas channel 33 or may be formed by a section of the central gas duct 33rd
  • the central channel 36 opens into the liquid passage 19a upstream of the end portion 19c.
  • the mouth 37 of the central channel 36 is arranged coaxially with the nozzle axis A and oriented in the direction of the nozzle axis A from the end portion 19c and the annular mixing chamber 26 away.
  • the pressurized gas L flowing out there thus flows approximately counter to the liquid F and assists in the formation of the flow layer FH in the end section 19 c of the liquid channel 19.
  • the atomizing nozzle 10 has a plurality of, for example, 8 outlet openings 40 arranged distributed in the circumferential direction U around the nozzle axis A.
  • the at least one outlet ⁇ opening 40 may be designed as a cylindrical bore, as a slot or preferably in the form of a Laval nozzle.
  • least one outlet opening 40 ei ⁇ has conically widening in the direction of flow cross-section.
  • the longitudinal axis of each discharge port 40 is open ⁇ geninate the nozzle axis A inclined.
  • the angle of inclination of the bore axis of the outlet opening 40 to the nozzle axis A is preferably in the range between 10 ° and 30 °.
  • a spray jet S is generated which is directed away from the nozzle axis A (FIGS. 1 and 3).
  • the outlet openings 40 are arranged in tube pieces 41, which are fluidically connected to the annular mixing chamber 26. Between the pipe sections 41, the fürgangsöff ⁇ openings 32 are formed by the fact that in the circumferential direction U immediately adjacent pipe sections 41 are arranged at a distance from each other. As a result, a fluidic connection between the connecting duct 31 and the central gas duct 33 is formed between the pipe sections 41.
  • a partition wall 45 is provided, which directs the gas flow in the outer injection channel 29 to the outer injection site 30 out.
  • the direction of the flow of the compressed gas L is at a distance from the outer Injetechnischsstel ⁇ le 30 at least one communication port 46 in the
  • Partition wall 45 is provided, can flow through the compressed gas L, starting from the gas port 13 into the connecting channel 31.
  • both the outer In edictionskanal 29 and the inner In edictionskanal 34 is supplied via the gas port 13 with pressurized gas L.
  • the volume flows in the communication passage 31 to the central gas ⁇ channel 33 and the inner injection site 35 are via the communication port 46 on the one hand and by the outer injection port 29 and the outer Injek ⁇ tion site 30 on the other hand is determined according to requirements.
  • the ratio of the cross sectional area of the communication hole 46 is located to that of the outer injection site 30, for example in loading ⁇ range from about 20% to 40%, preferably about 30%.
  • the cross-sections may be required, selected in the gas conduit system 28 so that a larger gas volume flow flows over the outer In ⁇ jemieskanal 29 and the outer injection site 30 in the annular mixing chamber 26 and through the inner injection port 34 or in ⁇ nere injection site 35th
  • a larger gas volume flow flows over the outer In ⁇ jemieskanal 29 and the outer injection site 30 in the annular mixing chamber 26 and through the inner injection port 34 or in ⁇ nere injection site 35th
  • the area ratio is about 2: 1.
  • at least about two thirds of the gas flowing into the annular mixing chamber 26 can flow in via the outer injection point 30.
  • the area ratio between the inner injection ⁇ point 35 and the mouth 37 of the central channel 36 is in the embodiment about 1:10 to 1:15.
  • FIG. 2 schematically illustrates a center plane E of the ring mixing chamber 26, which also essentially corresponds to the center of the liquid jet in the ring mixing chamber 26.
  • the central liquid jet entering the ring mixing chamber 26 from the end section 19c is indicated by a dotted line.
  • the two are in etechnischsstellen 30, 35 offset from one another.
  • the first arrow schematically illustrates the first main outflow direction PI from the outer injection channel 29 into the annular mixing chamber 26.
  • This first main outflow direction PI which runs here for example approximately parallel to the nozzle axis A, cuts the central liquid jet at a first angle CC.
  • a second Schoausströmraum P2 for the compressed gas L from the inner injection channel 34 is indicative ⁇ net, which is to the nozzle axis A at an acute angle to ⁇ arranged and includes a second angle ß with the central liquid jet.
  • the second angle ⁇ is greater in magnitude than the first angle CC.
  • the first angle CC is in particular less than 45 °, while the second angle ⁇ is between 70 ° and 90 °.
  • the atomizer nozzle 10 works as follows:
  • a liquid F flows through the liquid channel 19.
  • a fluid is generated in the swirl-producing section 19b via a swirl-generating means and according to the swirl generator 20, for example.
  • an impact jet is generated by an impact body.
  • a hollow frustoconical flow layer FH is generated there, which flows into the ring mixing chamber 26 flows in.
  • annular mixing chamber 26 downstream of the two injection sites 30, 35, by one or more bends in the extension of the ring mixing chamber Further atomization and uniform distribution of the liquid particles in the liquid-gas mixture can be achieved towards the nozzle axis A and / or away from the nozzle axis A. The liquid particles are then discharged through the outlet openings 40 in the form of spray jets S.
  • the annular mixing chamber 26 curves downstream of the two In etationsstellen first to the nozzle axis A back and then back away from the nozzle axis A.
  • the invention relates to an atomizer nozzle 10 with egg ⁇ nem liquid channel 19, to the downstream of a ring ⁇ mixing chamber 26 is fluidly connected. Via a liquid connection 12, a liquid F is supplied to the liquid channel 19.
  • the atomizing nozzle 10 comprises, in addition to a ⁇ the gas connection 13 which is connected to a gas line system 28th
  • compressed gas L is directed to an outer injection channel 29 and an inner injection channel 34.
  • the two injection channels 29, 34 lead to an injection point 30, 35 in the Ringmischkam ⁇ mer 26 a.
  • the outer injection site 30 is with respect to a nozzle axis A, around which the annular mixing chamber 26 extends coaxially, on the radially outer mixing chamber wall and the inner injection point 35 on the radially inner mixing ⁇ chamber wall available.
  • the inflowing liquid can be finely atomized with a low compressed gas consumption in the annular mixing chamber 26 and downstream of the ring mixing chamber 26 via at least one outlet opening 40 are each discharged as a spray jet S.

Landscapes

  • Nozzles (AREA)

Abstract

L'invention concerne une buse de pulvérisation (10) qui comprend un conduit de fluide (19) avec lequel une chambre de mélange annulaire (26) est en communication fluidique en aval. Un liquide (F) est amené au conduit de liquide (19) par un raccord de liquide (12). La buse de pulvérisation (10) comprend en outre un raccord de gaz (13) qui est raccordé à un système de conduit de gaz (28). Du gaz sous pression (G) est amené à un conduit d'injection extérieur (29) et un conduit d'injection intérieur (34). Les deux conduits d'injection (29, 34) débouchent dans la chambre de mélange annulaire (26) en un seul point d'injection (30, 35). Le point d'injection extérieur (30) est prévu sur la paroi de chambre de mélange radialement extérieure et le point d'injection intérieur (35) est prévu sur la paroi de chambre de mélange radialement intérieure. Le liquide entrant peut donc être finement pulvérisé dans la chambre de mélange annulaire (26) avec peu de gaz sous pression (L) et peut être délivré sous forme d'un jet de pulvérisation (S) en aval de la chambre de mélange annulaire par au moins un orifice de sortie (40).
EP14784032.6A 2014-10-09 2014-10-09 Buse de pulvérisation Active EP3204168B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/EP2014/071689 WO2016055115A1 (fr) 2014-10-09 2014-10-09 Buse de pulvérisation

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EP3204168A1 true EP3204168A1 (fr) 2017-08-16
EP3204168B1 EP3204168B1 (fr) 2020-04-08

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EP14784032.6A Active EP3204168B1 (fr) 2014-10-09 2014-10-09 Buse de pulvérisation

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US (1) US10245602B2 (fr)
EP (1) EP3204168B1 (fr)
JP (1) JP6487041B2 (fr)
CN (1) CN107107080B (fr)
AU (1) AU2014408516B2 (fr)
CA (1) CA2963894C (fr)
ES (1) ES2788743T3 (fr)
WO (1) WO2016055115A1 (fr)

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JP6817583B2 (ja) * 2018-02-21 2021-01-20 パナソニックIpマネジメント株式会社 噴霧装置
CN108404693A (zh) * 2018-04-16 2018-08-17 凡吾科技(上海)有限公司 一种气液混合装置
CN108580153B (zh) * 2018-07-09 2024-04-09 中国船舶重工集团公司第七0三研究所 一种大流量超声精细雾化喷嘴
BE1026905B1 (nl) * 2018-12-20 2020-07-22 Soudal Verbeterde vulling van vloeistoffen in polyurethaan spuitbussen
CN109396454A (zh) * 2018-12-24 2019-03-01 南通金源智能技术有限公司 一种3d打印双级气雾化喷嘴
CN110326803A (zh) * 2019-07-18 2019-10-15 浙江省海洋水产研究所 一种水产饲料油剂喷涂装置
USD1016556S1 (en) * 2019-09-19 2024-03-05 TML Innovative Products, LLC Steam nozzle
US11925288B1 (en) 2019-09-19 2024-03-12 TML Innovative Products, LLC Nozzle structure for steaming milk
JP7345649B2 (ja) * 2019-11-04 2023-09-15 ルーマス テクノロジー エルエルシー 流動接触分解フィードインジェクター
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AU2014408516A1 (en) 2017-05-25
ES2788743T3 (es) 2020-10-22
AU2014408516B2 (en) 2020-05-14
CA2963894A1 (fr) 2016-04-14
CA2963894C (fr) 2021-07-27
EP3204168B1 (fr) 2020-04-08
WO2016055115A1 (fr) 2016-04-14
US10245602B2 (en) 2019-04-02
JP2017534443A (ja) 2017-11-24
CN107107080A (zh) 2017-08-29
JP6487041B2 (ja) 2019-03-20
CN107107080B (zh) 2019-11-12
US20170304851A1 (en) 2017-10-26

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