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EP2444161B1 - Ajutage d'atomisation binaire - Google Patents

Ajutage d'atomisation binaire Download PDF

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Publication number
EP2444161B1
EP2444161B1 EP11195368.3A EP11195368A EP2444161B1 EP 2444161 B1 EP2444161 B1 EP 2444161B1 EP 11195368 A EP11195368 A EP 11195368A EP 2444161 B1 EP2444161 B1 EP 2444161B1
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EP
European Patent Office
Prior art keywords
annular gap
compressed gas
atomizing nozzle
mixing chamber
inlet
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EP11195368.3A
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German (de)
English (en)
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EP2444161A1 (fr
Inventor
Dieter Wurz
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Individual
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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
    • 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
    • B05B7/0458—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 the gas and liquid flows being perpendicular just upstream the mixing chamber

Definitions

  • the invention relates to a two-component atomizing nozzle for spraying a liquid with the aid of a compressed gas having a mixing chamber, a liquid inlet opening into the mixing chamber, a compressed gas inlet opening into the mixing chamber and an outlet opening downstream of the mixing chamber, wherein an annular gap surrounding the outlet opening is provided for the exit of compressed gas and wherein the outlet opening is formed by means of a circumferential wall, whose extreme end forms an outlet edge, and wherein the annular gap is arranged in the region of the outlet edge.
  • a two-fluid nozzle is known in which first a tubular flow profile is to be formed within the nozzle, wherein in the interior of the tubular airfoil, the air is guided.
  • the tubular flow profile is achieved by introducing a partial flow into the liquid passage of the nozzle, said partial flow of the air after generating the tubular flow profile is then guided into its interior.
  • Compressed gas should escape from an annular space in the region of the outlet opening, which then breaks up the walls of the tube-like flow profile produced in drops.
  • the two-fluid nozzle described thus represents a two-fluid nozzle with external mixing, since a decomposition of the drops takes place only outside the nozzle.
  • FIG. 1 shows a dual-fluid nozzle with internal mixing according to the prior art.
  • a fundamental problem with such nozzles results from the fact that the walls of the mixing chamber 7 are wetted with liquid.
  • the liquid which wets the wall in the mixing chamber 7 is driven by the shear stress and pressure forces as liquid film 20 to the nozzle mouth. It is plausible to assume that the walls are blown dry towards the nozzle mouth due to high flow velocity of the gas phase and that only very fine droplets are formed from the liquid film.
  • the theoretical and experimental work of one of the inventors see the attached bibliography, has shown that liquid films on walls can still exist as stable films without dripping even when the gas flow which drives the liquid films to the nozzle orifice reaches supersonic speed. And this is also the reason why it is possible to use liquid film cooling in rocket thrusters.
  • a liquid is introduced parallel to a central longitudinal axis 24 in the direction of arrow 1.
  • the liquid is passed through a lance tube 2 extending concentrically to the central longitudinal axis 24 and enters a mixing chamber 7 at a liquid inlet 10.
  • the lance tube 2 and the mixing chamber 7 are concentrically surrounded by an annular chamber 6, which is formed by means of a further lance tube 4 for the supply of the compressed gas to the two-fluid nozzle.
  • this annular chamber 6 compressed gas is introduced according to the arrow 15.
  • a with respect to the central longitudinal axis 24 radial peripheral wall of the mixing chamber 7 has a plurality of compressed gas inlets 5, which are arranged radially to the central longitudinal axis 24. Through these compressed gas inlets 5, compressed gas can enter the mixing chamber 7 at right angles to the liquid jet entering through the liquid inlet 10, so that a liquid / air mixture is formed in the mixing chamber 7.
  • Adjoining the mixing chamber 7 is a frusto-conical constriction 3, which forms a convergent outlet section, followed by a frustum-shaped extension 9 after a narrowest cross section 14, which forms a divergent outlet section.
  • the frusto-conical enlargement 9 ends at the outlet opening or the nozzle mouth 8.
  • a Zweistoffzerstäubungsdüse be provided, in which a uniformly fine droplet spectrum can be achieved both in the edge region and in the jet core.
  • a two-component atomizing nozzle for spraying a liquid with the aid of a compressed gas with a mixing chamber, a liquid inlet opening into the mixing chamber, a pressurized gas inlet opening into the mixing chamber and an outlet opening downstream of the mixing chamber, an annular gap surrounding the outlet opening for exiting high-pressure compressed gas Speed is provided, with the outlet opening is formed by a circumferential wall, the extreme end of which forms an outlet edge and wherein the annular gap is arranged in the region of the outlet edge, wherein the mixing chamber, the liquid inlet and the compressed gas inlet are formed and arranged such that a liquid film on the wall of the nozzle mouth exists and the Annular gap and the trailing edge are formed so that the compressed gas exits directly in the region of the trailing edge at high speed from the annular gap and the liquid film at the trailing edge to a very thin liquid lamella and then breaks this up into fine droplets.
  • the volume of a drop having a diameter reduced by a factor of three is only one-seventeenth of a large drop. Without entering into the well-known relationships, it should be clear to the person skilled in the art that this results in considerable advantages in terms of the required construction volume of evaporative coolers or resulting from sorption eg for the flue gas cleaning. With the additional annular gap atomization, therefore, a much finer droplet spectrum can be generated with the same expenditure of energy.
  • the annular gap air quantity 10% to 40% of the total atomizing air quantity.
  • the total pressure of the air in the annular gap is advantageously 1.5 bar to 2.5 bar absolute.
  • the total pressure of the air in the annular gap would advantageously have to be so high that, when expanding to the pressure level in the vessel, approximately sound velocity is achieved.
  • the compressed gas emerging from the annular gap at high speed can escape directly in the region of the outlet edge and thereby reliably ensure that a liquid film is drawn out at the nozzle mouth to form a very thin liquid lamella, which is then divided into fine droplets.
  • the annular gap is formed between the outlet edge and an outer annular gap wall.
  • annular gap wall edge is formed by an annular gap wall edge and the annular gap wall edge is arranged in the outflow direction after the trailing edge.
  • the annular gap wall edge is arranged between 5% and 20% of the diameter of the outlet opening to the outlet edge.
  • control means and / or at least two compressed gas sources are provided, so that a pressure of the compressed gas supplied to the annular gap and a pressure of the compressed gas opening into the mixing chamber through the compressed gas inlet can be set independently of one another.
  • Separate pipes for pressurizing the mixing chamber and for pressurizing the annular gap with compressed gas offer advantages in that the pressure in a gap air chamber upstream of the annular gap is then independent of the pressure of the atomizing gas, which is supplied to the mixing chamber, can be specified. This is then in view of the own energy requirement of importance when compressors with different back pressure or steam networks with matching different pressures in a system are available. In general, however, only a compressed gas network with a single pressure will be available. In this case, for example, pressure reducers can be used.
  • the annular gap air volume is adjusted via separate valves, regardless of the core jet air quantity, which is introduced into the mixing chamber.
  • the mixing chamber is at least partially surrounded by an annular chamber for supplying the compressed gas, and a gap air chamber connected upstream of the annular gap is in flow communication with the annular chamber.
  • the configuration of the two-component atomizing nozzle can then be simplified by removing the atomizing gas supplied to the annular gap from the annular space from which the mixing chamber is supplied with atomizing gas.
  • the flow connection is formed, for example, by means of bores in a partition wall between annular chamber and gap air chamber, which are suitable to be dimensioned in cross-section, also in relation to the bores forming a compressed gas inlet into the mixing chamber.
  • an outlet opening and the annular gap at least partially surrounding Schleierluftdüse is provided.
  • Schleierluftdüse leads to a further improvement of the spray pattern of the Zweistoffzerstäubungsdüse according to the invention, in particular backflow vortex can be avoided by which drops and dust-containing gas are mixed together and lead to disturbing deposits on the nozzle mouth.
  • the veiling air nozzle has a void air ring gap surrounding the outlet opening and the annular gap, whose outlet area is much larger than an exit area of the annular gap.
  • the Schleierluftdüse is fed with compressed gas, the pressure of which is substantially lower than a pressure of the annular gap supplied compressed gas.
  • means are provided for imparting a twist about a central longitudinal axis of the nozzle to a mixture of compressed gas and liquid in the mixing chamber.
  • the compressed gas inlet has at least one first inlet bore opening into the mixing chamber, which is oriented tangentially to a circle about a central longitudinal axis of the nozzle in order to generate a twist in a first direction.
  • a swirl can be generated in the mixing chamber in a simple and less clog-sensitive manner.
  • a plurality of, in particular four, first inlet bores are provided in a first plane perpendicular to the central longitudinal axis and spaced apart in the circumferential direction.
  • At least one second inlet bore which is aligned tangentially to a circle about the central longitudinal axis of the nozzle to generate a twist in a second direction, is provided parallel to the central longitudinal axis of the first inlet bore.
  • a plurality of, in particular four, second inlet bores are provided in a second plane perpendicular to the central longitudinal axis and spaced apart in the circumferential direction.
  • At least three planes spaced apart parallel to the central longitudinal axis are provided with inlet bores, the inlet bores of successive planes generating an oppositely directed twist.
  • FIG. 2 shows a Zweowoffzerstäubungsdüse 30 according to the invention according to a first preferred embodiment.
  • the Zweistoffzäubäubdüse 30 according to the invention at least as regards the introduction of the liquid and the compressed gas into the mixing chamber and the shape of the nozzle subsequent to the mixing chamber, similar to the known nozzle according to Fig. 1 built up.
  • a liquid to be atomized is fed in the direction of an arrow 32 via an inner lance tube 34 running parallel to a central longitudinal axis 36 of the nozzle 30 and reaches a liquid inlet 38, which has a reduced cross-section with respect to the tube 34.
  • the liquid After passing through the liquid inlet 38, the liquid then passes in the form of a concentric to the central longitudinal axis 36 extending liquid jet in the cylindrical and concentric with the central longitudinal axis 36 arranged mixing chamber 40.
  • the tube 34 and the mixing chamber 40 are surrounded by an annular chamber 42, which through the gap between a outer lance tube 43 and the inner lance tube 34 is formed and in the direction of an arrow 44 pressurized gas, such as compressed air, is introduced.
  • a concentric with the central longitudinal axis 36 extending peripheral wall of the mixing chamber 40 has a plurality of inlet openings 46a, 46b, 46c, all together form a compressed gas inlet into the mixing chamber 40, so for supplying the so-called core air.
  • the compressed gas inlet openings 46 are arranged offset in the direction of the central longitudinal axis 36 as well as in the circumferential direction. As a result, compressed gas is introduced into the mixing chamber 40 in different layers. The exact arrangement of the compressed gas inlet openings 46 will be described below with reference to the Fig. 4 to 7 explained.
  • a frusto-conical constriction 48 is provided, which forms a convergent outlet part and which, after passing through a narrowest cross-section, again merges into a frusto-conical enlargement with a smaller opening angle, which forms a divergent outlet part.
  • the divergent exit part terminates at an exit opening 52 or a nozzle mouth.
  • the outlet opening 52 is formed by a peripheral outlet edge 54, which forms the downstream end of the outlet part.
  • the frustoconical constriction 48 and the frusto-conical extension 50 are surrounded by a funnel-like component 56, so that an annular gap air chamber 58 is formed between the funnel-like component 56 and an outer wall of the outlet part.
  • This annular gap air chamber 58 is supplied by means of a plurality of inlet bores 60 from the annular chamber 42 with compressed gas.
  • the lower end of the funnel-shaped component 56 is formed by an annular gap wall edge 62, which runs around the outlet opening 52. Between the annular gap wall edge 62 and the outlet edge 54, an annular gap 64 surrounding the outlet opening 52 is formed, which thus annularly surrounds the outlet opening 52.
  • annular gap 64 in the representation of the Fig. 2a shown enlarged again, compressed gas exits at high speed.
  • a liquid film 66 which forms on an inner wall of the conical enlargement 50, is drawn out at the exit opening 52 of this divergent nozzle exit part into a very thin liquid lamella 68, which disintegrates into small drops.
  • Experimental investigations by the inventors have shown that in this way the maximum droplet size of the two-component atomizing nozzle 30 in relation to the nozzle according to the prior art Fig. 1 same energy consumption can be reduced to about one third.
  • the annular gap air quantity is between 10% and 40% of the total atomizing air quantity.
  • the annular gap outlet edge 62 protrudes slightly in the flow direction with respect to the outlet edge 54.
  • the annular gap outlet edge 62 protrudes beyond the outlet edge 54 by 5% to 20% of the diameter of the outlet opening 52.
  • the annular gap air chamber 58 can be supplied with compressed gas from a separate line.
  • the holes 60 are closed and compressed gas is introduced from a separate line directly into the annular gap air chamber 58.
  • FIG. 3 shows another binary atomizing nozzle 70 according to a second preferred embodiment of the invention.
  • the two-component atomizing nozzle 70 with the exception of an additional Schleierluftdüse 72 is equal to the Zweistoffzäubungsdüse 30 of Fig. 2 so that on an in depth explanation of the basic operation is omitted and the same components are provided with the same reference numerals.
  • the funnel-shaped component 56 is surrounded in the two-component atomizing nozzle 70 by a further component 74, which is constructed in principle tubular, forms a further lance tube and narrows in the direction of the outlet opening 52 to a funnel-like.
  • a Schleierluftringspalt 76 is formed between the component 74 and the component 56.
  • the Schleierluftspalt 76 ends approximately at the height of the outlet opening 52 and a lower, circumferential edge of the component 74 is disposed at the same height as the annular gap wall edge 62.
  • a cross-sectional area of the Schleuf Kunststoffspalts formed thereby is significantly larger than the annular gap 64, so that in the Schleierlufteintechnischtechnisch, can be.
  • the nozzle nozzle or the outlet opening 52 annularly enclosing Schleierluftdüse 72 can be energetically charged with low pressure air, which is supplied according to an arrow 78.
  • the two-component atomizing nozzle 30 and the two-component atomizing nozzle 70 of the Fig. 2 or 3 can be arranged at the lower end of a so-called sputtering lance, which projects into a process space.
  • FIG. 4 shows a sectional sectional view of the two-component atomizing nozzle 30 of Fig. 2 .
  • sectional planes which are designated I, II and III.
  • the bores for forming the compressed gas inlet openings 46a, 46b, 46c are each aligned tangentially to a circle around the central longitudinal axis 36 of the nozzle.
  • the thus twisted beam is centered thereby in the mixing chamber 40 and in the convergent outlet part and in the divergent outlet part of the nozzle 30, 70 automatically.
  • the tangential orientation of the compressed gas inlet openings 46a is based on the sectional view of Fig. 5 to recognize more precisely.
  • four holes in the plane I are uniformly spaced from each other in the circumferential direction, which form a flow connection of the annular chamber 42 in the mixing chamber 40. All of these bores are arranged tangentially to an imaginary circle 80 about the central longitudinal axis 36 of the nozzle.
  • an imaginary circle 80 about the central longitudinal axis 36 of the nozzle.
  • the presentation of the Fig. 6 shows the arrangement of four holes to form the Druckgaseinlassö réelleen 46 b in the plane II.
  • the Druckgaseinlouö réelleen 46 b are also arranged tangentially to a circle about the central longitudinal axis 36 of the nozzle, but such that in the plane II, a flow about the central longitudinal axis 36 in the clockwise direction results.
  • the pressurized gas inlet ports 46c in the plane III are as Fig. 7 can be seen, again arranged equal to the compressed gas inlet openings 46a in the plane I, so that in the plane III again a flow around the central longitudinal axis 36 results in the counterclockwise direction.
  • the invention is therefore intended to impose counter-rotating swirl directions in the different planes I, II, III of the supply air bores.
  • the first inlet air bore plane I counted from the liquid inlet is left-handed
  • the second bore plane II is right-handed
  • the third bore plane is again left-handed. Due to the opposite directions of twist in the different planes I, II, III, strongly pronounced shear layers are produced in the mixing chamber 40, which contribute to the formation of particularly fine drops.
  • the two-component atomizing nozzles 30, 70 can be optimized in that the massive liquid jet entering the mixing chamber is split even before the interaction with the atomizing air. This can be done in a different, conventional manner, for example by providing impact plates, swirl inserts and the like.

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  • Nozzles (AREA)

Claims (15)

  1. Ajutage d'atomisation binaire destiné à la pulvérisation d'un liquide avec l'aide d'un gaz sous pression, avec une chambre de mélange (40), une entrée de liquide (38) débouchant dans la chambre de mélange (40), une entrée de gaz sous pression (46a, 46b, 46c) débouchant dans la chambre de mélange (40) et une ouverture de sortie (52) disposée en aval de la chambre de mélange (40), caractérisé en ce que la chambre de mélange (40), l'entrée de liquide (38) et l'entrée de gaz sous pression (46a, 46b, 46c) sont réalisées et disposées de telle sorte qu'un film de liquide existe au niveau de la paroi de l'embouchure de l'ajutage, une fente annulaire (64) entourant l'ouverture de sortie (52) pour la sortie de gaz sous pression étant prévue, l'ouverture de sortie (52) étant formée au moyen d'une paroi périphérique dont l'extrémité la plus extérieure forme une arête de sortie (54), la fente annulaire (64) étant située dans la région de l'arête de sortie (54), et la fente annulaire (64) et l'arête de sortie (54) étant réalisées et disposées de telle sorte que le gaz sous pression sorte directement dans la région de l'arête de sortie (54) à grande vitesse hors de la fente annulaire (64) et aspire le film de liquide au niveau de l'arête de sortie (54) pour former une lamelle de liquide très mince et divise celle-ci alors en fines gouttes.
  2. Ajutage d'atomisation binaire selon la revendication 1, caractérisé en ce que la fente annulaire (64) est formée entre l'arête de sortie (54) et une paroi extérieure de la fente annulaire.
  3. Ajutage d'atomisation binaire selon la revendication 2, caractérisé en ce qu'une extrémité extérieure de la paroi de la fente annulaire est formée par une arête de paroi de fente annulaire (62) et en ce que l'arête de paroi de fente annulaire (62), considérée dans la direction de l'écoulement de sortie, est disposée après l'arête de sortie (54).
  4. Ajutage d'atomisation binaire selon la revendication 3, caractérisé en ce que l'arête de paroi de fente annulaire (62) est disposée entre 5 % et 20 % du diamètre de l'ouverture de sortie (52) en aval de l'arête de sortie (54).
  5. Ajutage d'atomisation binaire selon au moins une des revendications précédentes, caractérisé en ce qu'il est prévu des moyens de commande et/ou au moins deux sources de gaz sous pression, de telle manière qu'une pression du gaz sous pression fourni à la fente annulaire et une pression du gaz sous pression débouchant dans la chambre de mélange par l'entrée de gaz sous pression puissent être réglées indépendamment l'une de l'autre.
  6. Ajutage d'atomisation binaire selon au moins une des revendications précédentes, caractérisé en ce que la chambre de mélange (40) est entourée au moins en partie par une chambre annulaire (42) destinée à l'introduction du gaz sous pression et en ce qu'une chambre à air d'atomisation (58) disposée en amont de la fente annulaire (64) est en communication d'écoulement avec la chambre annulaire (42).
  7. Ajutage d'atomisation binaire selon au moins une des revendications précédentes, caractérisé en ce qu'il est prévu un ajutage d'air de gainage (72) entourant au moins en partie l'ouverture de sortie (52) et la fente annulaire (64).
  8. Ajutage d'atomisation binaire selon la revendication 7, caractérisé en ce que l'ajutage d'air de gainage (72) présente une fente annulaire à air de gainage entourant l'ouverture de sortie (52) et la fente annulaire (64), et dont la section de sortie est plus grande qu'une section de sortie de la fente annulaire.
  9. Ajutage d'atomisation binaire selon la revendication 7 ou 8, caractérisé en ce que des moyens de commande et/ou au moins deux sources de gaz sous pression sont prévus, de telle manière qu'une pression du gaz sous pression acheminé à l'ajutage à air de gainage (72) soit sensiblement plus faible qu'une pression du gaz sous pression acheminé à la fente annulaire (64).
  10. Ajutage d'atomisation binaire selon au moins une des revendications précédentes, caractérisé en ce qu'il est prévu des moyens (46a, 46b, 46c) pour imprimer à un mélange de gaz sous pression et de liquide dans la chambre de mélange (40) une rotation autour d'un axe longitudinal central (36) de l'ajutage (30; 70).
  11. Ajutage d'atomisation binaire selon la revendication 10, caractérisé en ce que l'entrée de gaz sous pression (46a, 46b, 46c) présente au moins un premier alésage d'entrée débouchant dans la chambre de mélange (40), qui est orienté tangentiellement à un cercle (80) autour de l'axe longitudinal central (36) de l'ajutage (30; 70) pour la production d'une rotation dans un premier sens.
  12. Ajutage d'atomisation binaire selon la revendication 11, caractérisé en ce qu'il est prévu dans un premier plan (I), perpendiculairement à l'axe longitudinal central (36) et à distance l'un de l'autre en direction périphérique, plusieurs, en particulier quatre, premiers alésages d'entrée.
  13. Ajutage d'atomisation binaire selon la revendication 11 ou 12, caractérisé en ce qu'il est prévu, à distance du premier alésage d'entrée parallèlement à l'axe longitudinal central (36), au moins un deuxième alésage d'entrée, qui est orienté tangentiellement à un cercle autour de l'axe longitudinal central (36) de l'ajutage (30; 70) pour la production d'une rotation dans un deuxième sens.
  14. Ajutage d'atomisation binaire selon la revendication 13, caractérisé en ce qu'il est prévu dans un deuxième plan (II), perpendiculairement à l'axe longitudinal central (36) et à distance l'un de l'autre en direction périphérique, plusieurs, en particulier quatre, deuxièmes alésages d'entrée.
  15. Ajutage d'atomisation binaire selon au moins une des revendications 11 à 14, caractérisé en ce qu'il est prévu au moins trois plans (I, II, III) espacés l'un de l'autre parallèlement à l'axe longitudinal central, avec des alésages d'entrée, dans lequel les alésages d'entrée de plans successifs (I, II, III) produisent une rotation orientée en sens contraire.
EP11195368.3A 2005-10-07 2006-10-06 Ajutage d'atomisation binaire Active EP2444161B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005048489A DE102005048489A1 (de) 2005-10-07 2005-10-07 Zweistoffdüse mit Ringspaltzerstäubung
EP06792384.7A EP1931478B1 (fr) 2005-10-07 2006-10-06 Ajutage d'atomisation binaire

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP06792384.7A Division EP1931478B1 (fr) 2005-10-07 2006-10-06 Ajutage d'atomisation binaire
EP06792384.7A Division-Into EP1931478B1 (fr) 2005-10-07 2006-10-06 Ajutage d'atomisation binaire

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EP2444161A1 EP2444161A1 (fr) 2012-04-25
EP2444161B1 true EP2444161B1 (fr) 2015-12-16

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EP06792384.7A Active EP1931478B1 (fr) 2005-10-07 2006-10-06 Ajutage d'atomisation binaire

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US (1) US8028934B2 (fr)
EP (2) EP2444161B1 (fr)
CN (1) CN101287555B (fr)
DE (1) DE102005048489A1 (fr)
ES (1) ES2421923T3 (fr)
PL (1) PL1931478T3 (fr)
RU (1) RU2441710C2 (fr)
WO (1) WO2007042210A1 (fr)

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DE102006009147A1 (de) 2006-02-24 2007-08-30 Wurz, Dieter, Prof. Dr.-Ing. Zweistoffdüse mit Weitwinkelstrahl
JP5337029B2 (ja) * 2006-06-27 2013-11-06 コーニンクレッカ フィリップス エヌ ヴェ 口の洗浄に使用するためのガスアシスト（ｇａｓ−ａｓｓｉｓｔｅｄ）液滴噴霧作成用スプレーヘッド装置
DE102007044272A1 (de) * 2007-09-17 2009-04-02 Wurz, Dieter, Prof. Dr.-Ing. Vielloch- oder Bündelkopfdüse ohne und mit Druckluftunterstützung
US7731100B2 (en) * 2008-08-12 2010-06-08 Walsh Jr William Arthur Joining the mixing and variable gas atomizing of reactive chemicals in flue gas cleaning systems for removal of sulfur oxides, nitrogen oxides and mercury
DE102008057295A1 (de) 2008-11-14 2010-05-20 Venjakob Maschinenbau Gmbh & Co. Kg Ringspaltdüse
DE102010030195B4 (de) 2009-06-20 2020-09-10 Werner & Pfleiderer Lebensmitteltechnik Gmbh Kühlvorrichtung für Lebensmittel sowie Düseneinrichtung hierfür
CN101940900B (zh) * 2009-07-09 2012-05-30 中国石油化工股份有限公司 一种冲击式气液分布器
CN101940897B (zh) * 2009-07-09 2012-05-30 中国石油化工股份有限公司 一种气液分布器
US8336788B2 (en) * 2009-08-07 2012-12-25 Nelson Irrigation Corporation Dripless rotary sprinkler and related method
DE102010015497A1 (de) * 2010-04-16 2011-10-20 Dieter Wurz Außen mischende Mehrstoffdüse für minimalen inneren Wärmeübergang
CN102019252B (zh) * 2010-06-01 2013-02-20 陈尚文 一种气能雾化喷涂设备
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PL1931478T3 (pl) 2013-10-31
DE102005048489A1 (de) 2007-04-19
EP2444161A1 (fr) 2012-04-25
WO2007042210A1 (fr) 2007-04-19
ES2421923T3 (es) 2013-09-06
US20090166448A1 (en) 2009-07-02
EP1931478A1 (fr) 2008-06-18
CN101287555B (zh) 2013-09-18
RU2441710C2 (ru) 2012-02-10
EP1931478B1 (fr) 2013-05-15
RU2008117344A (ru) 2009-11-20
US8028934B2 (en) 2011-10-04

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