DK151045B - SUSPENSION VALUES FOR DELIVERING A UNDERPRESSED LIQUID BASKET - Google Patents

SUSPENSION VALUES FOR DELIVERING A UNDERPRESSED LIQUID BASKET Download PDF

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Publication number
DK151045B
DK151045B DK340378AA DK340378A DK151045B DK 151045 B DK151045 B DK 151045B DK 340378A A DK340378A A DK 340378AA DK 340378 A DK340378 A DK 340378A DK 151045 B DK151045 B DK 151045B
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Denmark
Prior art keywords
nozzle according
channels
chamber
nozzle
spray nozzle
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Application number
DK340378AA
Other languages
Danish (da)
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DK340378A (en
DK151045C (en
Inventor
Winfried Jean Werding
Original Assignee
Werding Winfried J
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Priority claimed from CH960777A external-priority patent/CH618355A5/en
Priority claimed from CA288,724A external-priority patent/CA1077001A/en
Priority claimed from CH202478A external-priority patent/CH646619A5/en
Application filed by Werding Winfried J filed Critical Werding Winfried J
Publication of DK340378A publication Critical patent/DK340378A/en
Publication of DK151045B publication Critical patent/DK151045B/en
Application granted granted Critical
Publication of DK151045C publication Critical patent/DK151045C/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D83/00Containers or packages with special means for dispensing contents
    • B65D83/14Containers or packages with special means for dispensing contents for delivery of liquid or semi-liquid contents by internal gaseous pressure, i.e. aerosol containers comprising propellant for a product delivered by a propellant
    • B65D83/16Containers or packages with special means for dispensing contents for delivery of liquid or semi-liquid contents by internal gaseous pressure, i.e. aerosol containers comprising propellant for a product delivered by a propellant characterised by the actuating means
    • B65D83/20Containers or packages with special means for dispensing contents for delivery of liquid or semi-liquid contents by internal gaseous pressure, i.e. aerosol containers comprising propellant for a product delivered by a propellant characterised by the actuating means operated by manual action, e.g. button-type actuator or actuator caps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/34Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
    • B05B1/3405Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
    • B05B1/341Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
    • B05B1/3421Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber
    • B05B1/3431Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves
    • B05B1/3436Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves the interface being a plane perpendicular to the outlet axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/34Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
    • B05B1/3405Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
    • B05B1/341Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
    • B05B1/3421Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber
    • B05B1/3431Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves
    • B05B1/3442Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber the channels being formed at the interface of cooperating elements, e.g. by means of grooves the interface being a cone having the same axis as the outlet
    • 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
    • B05B7/0425Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid without any source of compressed gas, e.g. the air being sucked by the pressurised liquid
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D83/00Containers or packages with special means for dispensing contents
    • B65D83/0055Containers or packages provided with a flexible bag or a deformable membrane or diaphragm for expelling the contents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B1/00Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
    • B05B1/34Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
    • B05B1/3405Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
    • B05B1/341Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet
    • B05B1/3421Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl before discharging the liquid or other fluent material, e.g. in a swirl chamber upstream the spray outlet with channels emerging substantially tangentially in the swirl chamber

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Nozzles (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Fire-Detection Mechanisms (AREA)

Description

! 151045! 151045

OISLAND

Opfindelsen angår en forstøverdyse til afgivelse af en under overtryk stående væske i tågeform, hvilken dyse omfatter i det mindste en første og en anden del, som ligger mod hinanden med endeflader, der er tværstil-5 lede i forhold til aksen (MA) gennem en udløbsåbning i den første del, og 'der mellem delene er udformet strømningsveje, som har et centralt udløbskammer med flere i forhold til aksen (MA) i hovedsagen tangentialt deri udmundende kanaler fra i det mindste et omgivende ring-10 kammer, hvorhos der i kanalerne i hovedsagen vinkelret på disse udmunder andre, i aksial retning forløbende kanaler, gennem hvilke den under tryk stående væske ude fra kan ledes til strømningsvejene.BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to a nebulizer nozzle for dispensing a misty liquid in the overpressure form, said nozzle comprising at least a first and second portions adjacent to each other with end faces transverse to the axis (MA) through outlet port in the first portion, and flow paths are formed between the portions which have a central outlet chamber having several relative to the axis (MA), substantially tangentially therein, opening channels therein from at least one surrounding ring chamber 10, wherein the channels generally perpendicular to these, other, axially extending channels through which the pressurized liquid can be directed outwardly flow to the flow paths.

Fra beskrivelsen til fransk patent nr. 2.325.434 15 kendes en forstøverdyse af denne art, med et sprøjtehoved, der indeholder ringkanaler og et centralt hvirvelkammer til finest mulig opspaltning af produktet, som skal forstøves. Dette sprøjtehoved har imidlertid flere ulemper, især den at hvirvelkammeret tillader en ukontrolleret 20 strømning af produktet. Desuden er der ingen indretninger til at forøge strømningshastigheden af produktet i retning mod udløbet. Dette sprøjtehoved er derfor ikke egnet til at afgive fint forstøvede produkter, som er opbevaret under et kun relativt ringe tryk og uden drivgas.From the specification of French Patent No. 2,325,434, a nebulizer nozzle of this kind is known, with a syringe head containing ring ducts and a central vortex chamber for the finest possible splitting of the product to be atomized. However, this spray head has several drawbacks, especially that the swirl chamber allows an uncontrolled flow of the product. In addition, there are no devices for increasing the flow rate of the product towards the outlet. Therefore, this spray head is not suitable for dispensing finely atomized products which are stored under only relatively low pressure and without propellant gas.

25 Fra beskrivelsen til USA-patent nr. 3.652.018 kendes endvidere en forstøverdyse, som anvendes til mekanisk opbrydning af en væskestrøm under dannelse af en tåge af fine dråber. Denne kendte dyse er lettere at fremstille end en dyse med lignende trask, som kendes fra beskrivelsen til 30 USA-patent nr. 3.083.917. Tilførselskanalerne ved dysen ifølge USA-patent nr. 3.652.018 er indbyrdes adskilte ved skilleelementer, f.eks. afbøjningsplader, og tilførselskanalerne udgår fra et fælles ydre ringkammer og er afsluttet i en fælles, central udløbsåbning.Further, from the disclosure of U.S. Patent No. 3,652,018, there is known a nebulizer nozzle which is used for the mechanical breaking of a liquid stream to form a mist of fine droplets. This known nozzle is easier to manufacture than a nozzle with similar trench known from the specification of U.S. Patent No. 3,083,917. The supply channels at the nozzle of U.S. Patent No. 3,652,018 are spaced apart by separating elements, e.g. deflection plates, and the supply ducts exit from a common outer ring chamber and are terminated in a common central outlet opening.

35 2 151045 o35 2 151045 o

Et arrangement omfattende fire tilførselskanaler, der udgående fra et ydre ringkammer udmunder tangentialt i væggen af et centralt, cylindrisk blandekammer for at udvirke en forbedret forstøvning af væskematerialet, er 5 også kendt fra beskrivelsen til USA patent nr. 1.594.641.An arrangement comprising four supply ducts projecting from an outer annulus tangentially into the wall of a central cylindrical mixing chamber to effect an improved atomization of the liquid material is also known from U.S. Patent No. 1,594,641.

Disse kendte forstøverdyser tilfredsstiller imidlertid ikke fuldt ud de krav, som må opfyldes ved en række nutidige, til forstøvning bestemte produkter, f.eks. hårlak, deodoranter, luftopfriskere eller insektdræbende mid-10 ler. Den forstøvede tåge må således indeholde dråber med en størrelse på mellem 5 og lO^u, hvilket f.eks. er særlig betydningsfuldt i forbindelse med hårlak, med henblik på at opnå en hurtig fordampning, så at håret ikke sammenfiltres, når frisuren bringes på plads efter påføringen.However, these known nebulizer nozzles do not fully satisfy the requirements that must be met by a number of contemporary nebulizing products, e.g. hair lacquer, deodorants, air fresheners or insecticides. Thus, the atomized mist must contain droplets of between 5 and 100 µm, e.g. is particularly important in the case of hair varnish, in order to obtain a rapid evaporation so that the hair does not become entangled when the hairstyle is put in place after application.

15 Luftopfriskere og insektdræbende midler må fordampe hur tigt eller strømme ud i luften, så at de ikke beskadiger møbler, vægge, tapeter eller parketgulve. Samtidig med at der skal opnås en meget fin partikel-eller dråbestørrelse må det forstøvede produkt tillige være i besiddelse af en 20 tilstrækkelig stærk, kollisionskraft, hvis der er tale om hårlak, idet denne ikke alene skal ligge oven på håret, men tillige trænge ind i dette, hvilket sikrer en luftig frisure. Hvis der er tale om luftopfriskere og insektdræbende midler, må den forstøvede tåge kunne gennemtrænge 25 det til behandling bestemte luftrum i så vid udstrækning som mulig.15 Air fresheners and insecticides may evaporate rapidly or escape into the air so as not to damage furniture, walls, wallpaper or parquet floors. While obtaining a very fine particle or droplet size, the nebulized product must also possess a sufficiently strong collisional force in the case of hair lacquer, which must not only lie on top of the hair but also penetrate in this, ensuring an airy hairstyle. In the case of air fresheners and insecticides, the nebulized mist must be able to penetrate the airspace designated for treatment as widely as possible.

Kommercielt tilgængelige forstøverdyser, f.eks. at den art, der anvendes ved aerosoldåser eller pumpeforstøvere, nødvendiggør et tryk på i det mindste 6 ato for frembring-30 else af tåger med den Ønskede kvalitet, når de anvendes uden en til væskeform omdannet gaskomponent, eller omkring 3 ato, hvis en sådan komponent er til stede, idet et drivmiddel bestående af en til væske omdannet gas som bekendt trykaflastes i kontakt med den omgivende luft for derefter 35 afgørende at bidrage til dannelsen af fine dråber i den forstøvede tåge.Commercially available nebulizer nozzles, e.g. that the species used in aerosol cans or pump atomizers requires a pressure of at least 6 ato to produce fogs of the desired quality when used without a liquid component, or about 3 ato if such component is present, as a propellant consisting of a gas converted to liquid, as is known, is pressure-relieved in contact with the ambient air and then decisively contributes to the formation of fine droplets in the atomized mist.

OISLAND

3 1510453 151045

Idet en i overensstemmelse med opfindelsen udformet forstøverdyse fortrinsvis skal anvendes i forbindelse med en trykforstøvning uden til væske omdannet gas samt uden en luftpumpe og uden andre drivmidler (dvs. i såkaldte 5 drivgasfrie uddelingsaggregater), hvor der er tilstræbt et maksimalt tryk på 2,4 ato eller endog mindre tryk, i afhængighed af oplagringstiden, er det tilstræbt at konstruere dysen på en sådan måde, at den ved et forholdsvis lavt tryk er i stand til at tilvejebringe den nødven-10 dige tågekvalitet, samtidig med at den er enkel og derfor økonomisk at fremstille, idet det yderligere er forudset, at dersom til væske omdannet gas er til stede i produktet og trykkene er tilsvarende højere, skal der kunne opnås en hidtil ukendt, væsentligt forøget finhed af partiklerne 15 i den ved hjælp af en dyse ifølge opfindelsen tilvejebragte, forstøvede tåge.Preferably, a nozzle designed in accordance with the invention is to be used in connection with a pressure atomization without gas-converted gas and without an air pump and without other propellants (ie in so-called 5 propellant-free dispensing assemblies) where a maximum pressure of 2.4 is sought. Ato or even less pressure, depending on the storage time, it is sought to construct the nozzle in such a way that, at a relatively low pressure, it is able to provide the necessary fog quality while being simple and therefore economically prepared, further provided that if liquid-converted gas is present in the product and the pressures are correspondingly higher, a new, substantially increased fineness of the particles 15 in the nozzle according to the invention can be obtained. provided, atomized fog.

Dette er ifølge opfindelsen opnået med en forstøverdyse af den indledningsvis nævnte art, som er ejendommelig ved det i krav l's kendetegnende del angivne. Specielle udfø-20 relsesformer for forstøverdysen ifølge opfindelsen fremgår af underkravene.This is achieved according to the invention with a nebulizer nozzle of the kind mentioned initially, which is characterized by the characterizing part of claim 1. Specific embodiments of the nebulizer nozzle according to the invention are set forth in the subclaims.

Opfindelsen skal i det følgende forklares nærmere under henvisning til tegningen, på hvilken fig. 1 viser et længdesnit gennem et forstøverhoved 25 med en todelt forstøverdyse ifølge opfindelsen, fig. 2 et tværsnit gennem en dysekerne, som udgør en første del af en udførelsesform for forstøverdysen ifølge opfindelsen efter linien II-II i fig. 1 og i større målestok (det i fig. 1 viste snit er i fig. 2 antydet ved snit-30 pilene I-I), fig. 3 et længdesnit gennem den i fig. 2 viste dysekerne langs linien III-III i fig. 2, fig. 4 et længdesnit gennem et dysehus, der udgør en første del af en udførelsesform for forstøverdysen, som pas-35 ser til den i fig. 2 og 3 viste dysekerne,The invention will now be explained in more detail with reference to the drawing, in which: 1 shows a longitudinal section through a nebulizer head 25 with a two-part nebulizer nozzle according to the invention; FIG. 2 is a cross-section through a nozzle core forming a first part of an embodiment of the nebulizer nozzle according to the invention along line II-II of FIG. 1 and on a larger scale (the section shown in figure 1 is indicated in figure 2 by the arrows I-I in figure 2); 3 is a longitudinal section through the embodiment of FIG. 2 shows the nozzles along line III-III in FIG. 2, FIG. 4 is a longitudinal section through a nozzle housing constituting a first part of an embodiment of the nebulizer nozzle which conforms to that of FIG. 2 and 3 show the nozzles,

OISLAND

4 151045 fig. 5 et længdesnit gennem et midterområde af en forstøverdyse, som er sammensat af de i fig. 3 og 4 viste dele og i større målestok, fig. 6 et tværsnit gennem en udførelsesform i lig-5 hed med den i fig. 2-5 viste, men forsynet med seks tilførselskanaler , fig. 7 et tværsnit gennem en yderligere udførelsesform for en dysekerne, der er forsynet med tre turbulenstrin, 10 fig. 8 et længdesnit gennem en del af den i fig. 7 viste dysekerne, fig. 9 et tværsnit gennem en dysekerne svarende til den i fig. 2 viste, men forsynet med yderligere tilførselskanaler for indføring af et andet medium, 15 fig. 10 et længdesnit gennem en forstøverdyse, der er forsynet med en dysekerne ifølge fig. 9 og med en tilførselsventil samt tilførselskanaler for et andet medium, fig. 11 set forfra og delvis i snit en udførelsesform for en forstøverdyse, der er forsynet med et dyse-20 udløb, en ringsugekanal og en reguleringsventil som vist i fig. 10, fig. 12 viser en forstøverdyse svarende til den i fig. 11 viste, men forsynet med simple sugeåbninger for et andet medium, og 25 fig. 13 et aksialt længdesnit gennem en anden ud førelsesform for et forstøverhoved indeholdende en forstøverdyse ifølge opfindelsen.FIG. 5 is a longitudinal section through a central region of a nebulizer nozzle composed of those of FIG. 3 and 4 on a larger scale; FIG. 6 is a cross-section through an embodiment similar to that of FIG. 2-5, but provided with six supply channels; FIG. 7 is a cross-section through a further embodiment of a nozzle core provided with three turbulence stages; 8 is a longitudinal section through a portion of the embodiment of FIG. 7; FIG. 9 is a cross-section through a die core similar to that of FIG. 2, but provided with additional supply channels for introducing another medium; FIG. 10 is a longitudinal section through a nebulizer nozzle provided with a nozzle core according to FIG. 9 and with a supply valve and supply channels for another medium; FIG. 11 is a front elevational view, partly in section, of one embodiment of an atomizer nozzle provided with a nozzle outlet, an annulus and a control valve as shown in FIG. 10, FIG. 12 shows a nebulizer nozzle similar to that of FIG. 11 but provided with simple suction openings for another medium, and FIG. 13 is an axial longitudinal section through another embodiment of an atomizer head containing an atomizer nozzle according to the invention.

I fig. i er i længdesnit vist et aktiveringshoved 30, som i sin sidevæg 30a har en reces 31, hvori er an-30 bragt en foretrukken udførelsesform for forstøverdysen ifølge opfindelsen. Forstøverdysen består af en første del i form af et bægerformet dysehus 33 og en anden del i form af en dysekerne 32, som er optaget i en reces 33a, der er udformet i den indre endevæg i dysehuset 33.In FIG. is shown in longitudinal section an actuation head 30 which has in its side wall 30a a recess 31, in which is arranged a preferred embodiment of the atomizer nozzle according to the invention. The nebulizer nozzle consists of a first portion in the form of a cup-shaped nozzle housing 33 and a second portion in the form of a nozzle core 32 which is accommodated in a recess 33a formed in the inner end wall of the nozzle housing 33.

35 Dysekernen 32 bærer fordybninger, som er udformet i den 5 151045The nozzle core 32 carries recesses formed in it

OISLAND

forreste endeflade 32a, som er i tætnende kontakt med recessen 33a's bund 33b og vender mod en udløbsåbning 41, ligesom der er udformet fordybninger i dysekernens perifere væg 32b, der er i tæt kontakt med recessen 33a1s sidevæg 5 33c, hvilke fordybninger danner det indre dysehulrum, som omfatter ringkamre og kanaler, når dysen er fremstillet ved samling af dysekernen 32 og dysehuset (dysekappen) 33.the front end surface 32a which is in sealing contact with the bottom 33b of the recess 33a and faces an outlet opening 41, as well as recesses formed in the peripheral wall 32b of the nozzle core which are in close contact with the recess 33a1's sidewall 5 33c, which recesses form the inner nozzle cavity which comprises annular chambers and ducts when the nozzle is made by joining the nozzle core 32 and the nozzle housing (nozzle cap) 33.

De nævnte fordybninger er navnlig vist i den i fig.The recesses mentioned are particularly shown in the embodiment of FIG.

2 og 3 afbildede dysekerne 32.2 and 3 depict the nozzles 32.

10 Aktiveringshovedet 30 bærer på sin underside en bøs ning eller halsdel 34, der er åben nedad, og hvori ventilakselen fra en aerosoldåse kan være monteret på kendt måde.The actuation head 30 carries on its underside a sleeve or neck portion 34 which is open downwards and wherein the valve shaft from an aerosol can be mounted in known manner.

Det indre af bøsningen 34 danner en hovedtilførselskanal 27, fra hvis øvre endeområde der i aktiveringshovedet 30 forløber fire forsyningskanaler 35, der er udformet som langsgående noter i dysekernen 32's perifere væg 32b og forløber i aksialretningen i forhold til dysens midterakse MA og udmunder vinkelret i fordybninger i endefladen 32a, der danner dysens turbulenssystem. Turbulenssystemet omfat-20 ter, således som det fremgår af fig. 2, fire tilførselskanaler 36, der ved deres tilførselsåbninger 36a er forbundet med den forreste ende af en af de aksiale forsyningskanaler 35, og som alle forløber skævt i forhold til dysens midterakse i et plan, der skærer denne akse under 25 en ret vinkel, og som indmunder tangentialt i et fælles første yderste ringkammer 37, hvorhos deres mundinger eller udløbsåbninger 36b er symmetrisk fordelt anbragt omkring den ydre periferivæg 37a i ringkammeret 37 (fig. 2) og sammen med den nævnte perifere væg danner styreranden 30 36c.The interior of the sleeve 34 forms a main supply channel 27, from whose upper end region extends four supply channels 35 in the actuating head 30, formed as longitudinal grooves in the peripheral wall 32b of the nozzle core 32 and extending in the axial direction relative to the central axis of the nozzle and terminating perpendicular to the grooves. in the end surface 32a forming the turbulence system of the nozzle. The turbulence system comprises as shown in FIG. 2, four supply channels 36 connected at their supply openings 36a to the front end of one of the axial supply channels 35, all of which extend skewed to the center axis of the nozzle in a plane which intersects this axis at a right angle; and which tangentially opens into a common first outer annular chamber 37, wherein their orifices or outlet openings 36b are symmetrically spaced about the outer peripheral wall 37a of the annular chamber 37 (Fig. 2) and together with said peripheral wall the guide rim 30 36c forms.

Fra ringkammeret 37 forløber fire kanaler 38 hørende til det næste turbulenstrin indad og ind i dysen i et andet, indre ringkammer 39, som omgiver et taplignende afbøjningsfremspring 40, der rager op fra det plan, der er bestemt af tilførselskanalerne 36's bundflader 36d (fig. 3) og frem til i det væsentlige nær tilførslen til dysens udløbsåbning 41.From the annulus 37, four channels 38 of the next turbulence stage extend inwardly and into the nozzle of a second, inner annulus 39 which surrounds a pin-like deflection projection 40 which protrudes from the plane determined by the bottom surfaces 36d of the supply ducts 36 (FIG. 3) up to substantially near the inlet to the nozzle outlet opening 41.

3535

OISLAND

6 1510456 151045

Som det fremgår af fig. 3, er ringkamrene og kanalerne hermetisk dækkede eller i det mindste væsketæt dækkede af bundfladen 33b i recessen 33a. En under tryk stående væske, der strømmer gennem dysens indre hulrum, kan så-5 ledes kun bevæge sig gennem kanalerne og de ringformede kamre i retning frem mod dysens udløbsåbning 41.As shown in FIG. 3, the annular chambers and channels are hermetically or at least fluid tightly covered by the bottom surface 33b of recess 33a. Thus, a pressurized liquid flowing through the inner cavity of the nozzle can only move through the channels and annular chambers in the direction towards the nozzle outlet opening 41.

Den bedste koniske udformning af tilførselskanalerne 36 opnås, hvis der trækkes en tangent fra kanalsiden 35a frem til ringkammeret 27's periferi og samtidig en ret li-10 nie fra kanalsiden 35b gennem skæringspunktet 37a mellem tangenten og ringkammeret 37. Det har vist sig fordelagtigt at vælge bredden af ringkammeret 37 på en sådan måde, at den er lig med bredden af mundingerne 36b i tilførselskanalerne 36 i ringkammeret 37. Denne opbygning muliggør at den 15 under tryk fra forsyningskanalerne 35 strømmende væske ac-celeres på grund af indsnævringen af tilførselskanalerne 36 frem mod disses udmunding i ringkammeret 37, ligesom der tilvejebringes en centrifugalkraftkomponent i væsken ved hjælp af den drejebevægelse, som væsken udsættes for i ring-20 kammeret 37. Desuden frembringes en sugevirkning i ringkammeret 37 ved hver munding 36b i en tilførselskanal 36. Den optimale anbringelse af randen 38d i tilførselsåbningen 38a for de indre tantiale kanaler 38 i det andet turbulenstrin opnås ved fra det første kontaktpunkt på randen 36c 25 mellem den rette linie 35B-37A og ringkammervæggen 37a at trække en tangent til det andet ringkammer 39's periferi, medens den optimale bredde af tilførselsåbningerne 38a for de indre kanaler 38 opnås ved at trække en ret linie fra det punkt 39A, hvor denne tangent berører det andet ring-30 kammer 39 og frem til punktet 35A på forsyningskanalen 35's siderand 35a. Det har vist sig fordelagtigt at lade bredden af ringkammeret 39 have en sådan størrelse, at den er lig med summen af bredden af indmundingerne af de indre tangentiale kanaler 38 i ringkammeret, hvorved dia-35 meteren af det taplignende fremspring 40 ligeledes er be-The best conical design of the supply channels 36 is obtained if a tangent is drawn from the channel side 35a to the periphery of the annular chamber 27 and at the same time a straight line from the channel side 35b through the intersection point 37a between the tangent and the annular chamber 37. It has been found advantageous to choose the width of the annulus 37 in such a manner that it is equal to the width of the orifices 36b of the supply ducts 36 of the annulus 37. This structure allows the fluid flowing under pressure from the supply ducts 35 to accelerate due to the narrowing of the supply ducts 36 towards them. orifice in the annulus 37, as well as providing a centrifugal force component in the liquid by the pivotal movement to which the liquid is subjected in the annulus 37. In addition, a suction effect in the annulus 37 is produced at each orifice 36b in a supply channel 36. The optimal placement of the rim 38d in the supply opening 38a for the inner tantial ducts 38 in the second turbulence stage ridge by drawing a tangent to the periphery of the second ring chamber 39 from the first contact point on the rim 36c 25 between the straight line 35B-37A and the annular wall 37a, while obtaining a straight line the optimum width of the supply openings 38a for the inner channels 38 from the point 39A where this tangent touches the second ring 30 chamber 39 to the point 35A on the lateral edge 35a of the supply channel 35. It has been found advantageous to allow the width of the annular chamber 39 to be such that it is equal to the sum of the width of the orifices of the inner tangential channels 38 of the annular chamber, whereby the diameter of the pin-like projection 40 is likewise measured.

OISLAND

7 151045 stemt. Højden af de ydre tangentiale tilførselskanaler 36 i aksialretningen forbliver -uændret, medens de indre kanaler 38 derimod ikke blot i sideretningen, men også i højden indsnævres fra deres tilførselsåbninger 38a mellem 5 de to aksiale vægrande 38c og 38d og frem til deres mundinger 38b i ringkammeret 39. Denne indsnævring er ikke kontinuerlig, men er afbrudt ved et afbøjningsfremspring 23, der danner en forhindring, som genererer en mekanisk opbrydning og en turbulensdannelse allerede under accele- 10 reringen af væsken (fig. 2 og 3). Den rundtgående rand omkring fremspringet 40's forreste flade, der fortrinsvis har en fordybning 40a (fig. 5fører ligeledes til turbulensdannelse i den gennem de indre kanaler 38 strømmende væske. En yderligere tubulensdannelse frembringes 15 ved en ringformet vulst 42, som er anbragt på indersiden af dysehuset 33 omkring dysens udløbsåbning 41 (fig. 4).7 151045 voted. The height of the outer tangential supply channels 36 in the axial direction remains unchanged, while the inner channels 38, on the other hand, not only narrow in the lateral direction but also in height from their supply openings 38a between the two axial wall edges 38c and 38d and up to their orifices 38b in the annulus 39. This constriction is not continuous, but is interrupted by a deflection projection 23 which forms an obstacle which generates a mechanical break-up and turbulence formation already during the acceleration of the liquid (Figs. 2 and 3). The circumferential rim around the front face of the projection 40, preferably having a recess 40a (Fig. 5 also leads to turbulence in the liquid flowing through the inner channels 38. A further tubular formation is provided by an annular bead 42 disposed on the inside of the nozzle housing. 33 around the nozzle outlet opening 41 (Fig. 4).

I en forstøverdyse ifølge opfindelsen accelereres en under tryk stående væske, bringes i rotation og op-hvirvles på reguleret måde, hvilket fører til bedst mulig 20 udnyttelse af den forhåndenværende udstrålingskraft. Vo- ' luminet af hovedtilførselskanalen 27 er forholdsvis stort sammenlignet med de henholdsvis aksiale og tangentiale kanaler, som er tilsluttet hovedtilførselskanalen 27.In a nebulizer nozzle according to the invention, a pressurized fluid is accelerated, rotated and swirled in a controlled manner, leading to the best possible utilization of the existing radiating power. The volume of the main supply channel 27 is relatively large compared to the axial and tangential channels connected to the main supply channel 27, respectively.

Dennes i forhold til de efterfølgende kanaler overdimen-25 sionerede volumen er på den anden side nødvendig for at den forhåndenværende trykkraft, som væsken påføres, ubegrænset bringes til at virke frem til kanalerne 35, medens de aksiale og tangentiale kanaler forbliver frie, selv når en væske, som hurtigt tørrer, som følge af en langsom 30 fordampning af en forholdsvis stor mængde væske er oplagret i hovedtilførselskanalen 27.On the other hand, its oversized volume relative to the subsequent channels is necessary in order for the existing compressive force applied to the liquid to be unrestricted to act on the channels 35, while the axial and tangential channels remain free even when a liquid which dries quickly as a result of a slow evaporation of a relatively large amount of liquid is stored in the main supply duct 27.

Sprøjteydelsen af forstøverdysen ifølge opfindelsen kan tilpasses til en bestemt viskositet af væsken ved passende ændring af tværsnittet af de aksiale kanaler 35 og 35 tillige af tværsnittet af rummene 36, 37, 38 og 39 i dy-The spraying performance of the nebulizer nozzle according to the invention can be adapted to a particular viscosity of the liquid by appropriately changing the cross-section of the axial channels 35 and 35 as well as the cross-section of the compartments 36, 37, 38 and 39 of the die.

OISLAND

8 151045 sens indre. En større viskositet af væsken kræver selvsagt et større tværsnitsareal end en væske med lav viskositet.8 151045 sens inside. Of course, a higher viscosity of the liquid requires a larger cross-sectional area than a low viscosity liquid.

Størrelsen af dråberne i tågen kan indstilles ved at ændre afstanden mellem det taplignende fremspring 40 5 og en ringribbe 42 på dysehuset 33. Desto mindre afstand, desto mindre dråbestørrelse. Afstanden må naturligvis ikke gøres for lille, idet noget sådant ville reducere udstrålingshastigheden og derfor forøge udstrålingsvinklen af den forstøvede tåge, med mindre disse virkninger er ønsket ved 10 et bestemt produkt. Tågens udstrålingsvinkel afhænger tillige af længden af dysens udløbsåbning 41 i dysehuset 33.The size of the droplets in the fog can be adjusted by changing the distance between the pin-like projection 40 5 and a ring rib 42 on the nozzle housing 33. The less distance, the smaller the droplet size. Of course, the distance must not be made too small, as such would reduce the rate of radiation and therefore increase the angle of radiation of the atomized mist, unless such effects are desired for a particular product. Also, the angle of radiation of the fog depends on the length of the nozzle outlet opening 41 in the nozzle housing 33.

Desto længere udløbsåbning 41, desto mindre er denne vinkel.The longer the outlet opening 41, the smaller this angle is.

I fig. 4 og 5 er der vist en yderligere fordelagtig udførelsesform for forstøverdysen ifølge opfindelsen. Dyse-15 kernen 32 svarer til den i fig. 1-3 viste dysekerne 32, med undtagelse af, at der i stedet for det andet ringkammer 39 er tilvejebragt et turbulenskammer 45, som er udformet ved at fremspringet 40 bærer en aksial fremspringende ringflange 44. Den inden for flangen dannede fordybning 40 i 20 fremspringets forreste endeflade begrænser turbulenskammeret 45 indad, medens recessen 33a's bundflade 33b i udsparinger 33a i dysehuset 33 begrænser dette kammer udad, hvorhos ringvulsten 42, hvis ydre diamter er en smule mindre end den indre diameter af ringflangen 44, rager en smule 25 ind i turbulenskammeret 45. Der er således tilvejebragt en ringspalte 46 mellem ringflangen 44 og ringvulsten 42, hvilken spalte giver anledning til en betydelig stigning i turbulensen i turbulenskammeret 45, navnlig hvis den øvre rand af ringvulsten 42 rager frem til planet for ringflan- 30 gen 44's øvre rand eller ud over dette plan og ind i turbulenskammeret 45's indre (fig. 5).In FIG. 4 and 5 there is shown a further advantageous embodiment of the nebulizer nozzle according to the invention. The nozzle core 32 is similar to that of FIG. 1-3, except that in the second annular chamber 39, a turbulence chamber 45 is formed which is formed by the projection 40 carrying an axially projecting annular flange 44. The indentation 40 formed within the flange of the protrusion 20 the front end surface restricts turbulence chamber 45 inwardly, while the bottom surface 33b of recess 33a in recesses 33a of nozzle housing 33 confines this outwardly, wherein annular bead 42, whose outer diameter is slightly smaller than the inner diameter of annular flange 44, extends slightly 25 into turbulence chamber 45 Thus, a ring gap 46 is provided between the ring flange 44 and the ring bead 42, which gives rise to a significant increase in the turbulence of the turbulence chamber 45, especially if the upper edge of the ring bead 42 projects to the plane of the upper edge of the ring flange 44 or beyond this plane and into the interior of the turbulence chamber 45 (Fig. 5).

Ved den i fig. 4 viste udførelsesform er dysehuset 33 på sin indre rand, der omgiver recessen 33a, forsynet med en ringformet flange eller sikke 28, som ligger så tæt anIn the embodiment shown in FIG. 4, the nozzle housing 33 on its inner edge surrounding the recess 33a is provided with an annular flange or socket 28 which is so close to

QfTQFT

mod en tilsvarende reces 28a i aktiveringshovedet 30, at 0 9 151045 dysen ikke kan udkastes fra aktiveringshovedet 30, selv ved en væske, der er under meget højt tryk.against a corresponding recess 28a in the actuating head 30, that the nozzle cannot be ejected from the actuating head 30, even at a fluid under very high pressure.

Fig. 6 viser en yderligere udførelsesform for en dysekerne 32, der har seks forsyningskanaler 35, som fører 5 frem til seks tilførselskanaler 36 og udmunder i et fælles ringkammer 37, hvorfra seks tangentiale kanaler 38 fører frem til et fælles indre ringkammer 39, der er begrænset af det taplignende afbøjningsfremspring 40.FIG. 6 shows a further embodiment of a nozzle core 32 having six supply channels 35 leading 5 to six supply channels 36 and ending in a common ring chamber 37, from which six tangential channels 38 lead to a common inner ring chamber 39 limited by the pin-like deflection projection 40.

Fig. 7 viser en yderligere udførelsesform, hvori for-10 støverdysen ifølge opfindelsen kan være forsynet ikke alene med to, men tillige med tre eller flere efter hinanden følgende turbulenstrin, idet dysekernen 6 ud over kanalerne og ringkamrene 36, 37, 38 og 39 også kan indeholde tangentiale kanaler 48, og ringkammeret 49 kan være forsynet med 15 et turbulenskammer 45 oven over fremspringet 40. Antallet af efter hinanden følgende turbulenstrin kan naturligvis også afhænge af det tilgængelige væsketryk, så at væskestrømmen ikke udnødigt opbremses af en betydelig friktion. Desto højere tryk, som væsken udsættes for, jo flere turbu-20 lenstrin kan der være tilvejebragt. Ved den i fig. 7 viste udførelsesform er højden af tilførselskanalerne og passagerne ikke reduceret konisk, men trinvist i retning frem t mod turbulenskammeret 45. I dette tilfælde danner hvert trin en forhindring, som giver anledning til hvirveldannelse, 25 og den tilvejebragte indsnævring af passagerne er en faktor, der giver anledning til· en accelerering af væskestrømmen (fig. 8).FIG. 7 shows a further embodiment in which the atomizer nozzle according to the invention may be provided not only with two, but also with three or more successive turbulence steps, the nozzle core 6, in addition to the channels and annulus 36, 37, 38 and 39, may also contain tangential channels 48, and annulus 49 may be provided with a turbulence chamber 45 above the projection 40. Of course, the number of successive turbulence stages may also depend on the available fluid pressure so that the fluid flow is not unnecessarily slowed down by a significant friction. The higher the pressure to which the liquid is subjected, the more turbulent steps may be provided. In the embodiment shown in FIG. 7, the height of the supply channels and passageways is not reduced tapered, but incrementally towards the turbulence chamber 45. In this case, each step forms an obstacle causing vortex formation, and the narrowing of the passageways is a factor which gives rise to an acceleration of fluid flow (Fig. 8).

Fig. 9 viser endnu en udførelsesform for en dysekerne 32, hvori denne ud over de tangentiale kanaler 36 og 38 til-30 lige er forsynet med tilførselskanaler 29, hvis tilførselsåbninger 29a ikke er forsat langs periferien af dysekernen 32, men i retning mod kernens midte, og som er forsynet med passager 26, der forløber aksialt ud fra den forreste flade 33c i dysehuset 33 og gennem dysekernen. Tilførselska-35 nalerne 29 er anbragt.på en sådan måde, at de åbner ud i:FIG. 9 shows yet another embodiment of a nozzle core 32 in which, in addition to the tangential channels 36 and 38, it is also provided with supply channels 29, whose supply openings 29a are not positioned along the periphery of the nozzle core 32 but towards the center of the core, and which is provided with passageways 26 extending axially from the front face 33c of the nozzle housing 33 and through the nozzle core. The supply channels 29 are arranged in such a way that they open into:

OISLAND

10 151045 ringkammeret 37 tangentialt med den ydre sidevæg i kammeret ved områder, som giver anledning til en sugning mellem mundingerne 36b for hvert par op til hinanden grænsen-de tangentiale kanaler 36.The ring chamber 37 is tangentially to the outer side wall of the chamber at regions which give rise to suction between the orifices 36b for each pair of adjacent tangential channels 36.

5 Med henblik på at frembringe en yderligere sugevirk ning i tilførselskanalerne 29 er ringkammeret 37's ydervæg ikke fuldstændig cirkulær, men indsnævres netop før mundingerne 29b i tilførselskanalerne 29 set i strømningsretningen. Den væske, som strømmer ind fra en tilførsels-10 kanal 36, og som allerede er blevet accelereret, drives derpå ind i den efterfølgende indsnævring af ringkammeret 37, hvor den atter accelereres, så at den frembringer en sugning, når den strømmer forbi mundingen 29b af en passage 29, hvilket giver anledning til en forøgelse af effekten, 15 idet denne munding 29b er anbragt en smule bag tilførselsområdet 38a for en passage 38, dvs. foran i strømningsretningen, gennem hvilken passage 38 væsken strømmer frem til dyseudløbet 41. Tilførselskanaler 29 er tilvejebragt med henblik på at indsuge et andet medium, f.eks. luft, og med 20 henblik på at blande dette medium med den væske, som strømmer gennem dysens indre.5 In order to produce a further suction effect in the supply channels 29, the outer wall of the annular chamber 37 is not completely circular, but narrows just before the orifices 29b in the supply channels 29 seen in the flow direction. The liquid flowing in from a supply channel 36, which has already been accelerated, is then driven into the subsequent narrowing of the annulus 37 where it is again accelerated to produce a suction as it flows past the mouth 29b. of a passageway 29, which gives rise to an increase in power, 15 this opening 29b being located slightly behind the supply area 38a of a passageway 38, i.e. forward in the direction of flow, through which passage 38 the liquid flows to the nozzle outlet 41. Supply channels 29 are provided for sucking in another medium, e.g. air, and for the purpose of mixing this medium with the liquid flowing through the interior of the nozzle.

Idet en i overensstemmelse med opfindelsen udformet forstøverdyse er indrettet til fortrinsvis at blive anvendt til uddeling af et produkt, der ikke indeholder gas, og navn-25 lig ikke en drivgas, er det, hvis der skal afgives et skumdannende produkt, f.eks. barberskum, i skumform, hvilket ofte kræver tilstedeværelsen af et gasformig medium for at danne skummen, nødvendigt tillige at indføre en gasfase til barberskummets væskefase. Dette kan opnås, hvis den grund-30 læggende væske, samtidig med at den strømmer gennem de ydre · tangentiale kanaler 36, ringkammeret 37 og de indre, tangentiale kanaler 38, er indrettet til at indsuge luft gennem åbningerne 29a for tilførselskanalerne 29, idet luften derpå danner barberskummet, når den blandes med væsken (fig.Since a nebulizer nozzle designed in accordance with the invention is arranged to be preferably used for dispensing a product which does not contain gas, and in particular not a propellant gas, it is if a foam forming product is to be dispensed, e.g. shaving foam, in foam form, which often requires the presence of a gaseous medium to form the foam, is also necessary to introduce a gas phase to the shaving foam liquid phase. This can be achieved if the basic liquid, while flowing through the outer tangential ducts 36, the annular chamber 37 and the inner tangential ducts 38, is arranged to draw air through the openings 29a of the supply ducts 29, the air being then the shaving foam forms when mixed with the liquid (fig.

35 9-12) .35 9-12).

OISLAND

U 151045U 151045

Idet der i et gasfrit alternativ til aerosoldåser også er muligt at påfylde olie i tillæg til de skumdannende emulsioner, hvilket imidlertid ligeledes nødvendiggør tilstedeværelsen af et gasformigt medium med henblik 5 på at fremtræde som en støvsky eller tåge efter afgivningen fra en forstøverdyse, er det muligt at indsuge dette gas-formige medium (luft) via tilførselskanalerne 29 ved hjælp af forstøverdysen ifølge opfindelsen. Tværsnitsarealet af tilførselskanalerne 29 afhænger af den ønskede mængde 10 luft, som er nødvendig ved blandingen, og luftmængden må således tilpasses fra gang til gang. Fig. 11 og 12 viser en forstøverdyse, der omfatter et forstøverhus 33 og en dysekerne 32, som er anbragt i huset, og hvori fire åbninger 29a, gennem hvilke et andet medium kan indsuges via 16 tilførselskanalerne 29, er indbyrdes forbundet via passagen 26a og en ringformet kanal 26b, der i fig. 11 er vist med stiplede linier, og som munder ud i dysehuset 33 og er forbundet med en tilførselsventil 22, ved hjælp af hvilken mængden af det indsugede andet medium kan reguleres. Ud 20 over et gasformig medium kan der ved hjælp af en på denne måde udformet dåse endvidere indsuges andre væske- eller luftformige medier, f.eks. væsker eller pulvere, hvilket er beskrevet nærmere i det følgende.While in a gas-free alternative to aerosol cans, it is also possible to add oil in addition to the foam-forming emulsions, which, however, also necessitates the presence of a gaseous medium in order to appear as a dust cloud or mist after the discharge from a nebulizer nozzle. suctioning this gaseous medium (air) through the supply ducts 29 by means of the nebulizer nozzle of the invention. The cross-sectional area of the supply ducts 29 depends on the desired amount of 10 air required for mixing, and thus the amount of air must be adjusted from time to time. FIG. 11 and 12 show a nebulizer nozzle comprising a nebulizer housing 33 and a nozzle core 32 disposed in the housing, in which four openings 29a through which another medium can be sucked in via the 16 supply channels 29 are interconnected via the passage 26a and an annular channel 26b, which in FIG. 11 is shown in broken lines, which open into the nozzle housing 33 and are connected to a supply valve 22, by means of which the amount of the second suction medium can be controlled. In addition to a gaseous medium, other liquid or gaseous media, e.g. liquids or powders, which are described in more detail below.

Fig. 13 viser et længdesnit gennem et aktiverings-25 hoved, hvori der er anbragt en anden hensigtsmæssig udførelsesform for forstøverdysen ifølge opfindelsen. I dette tilfælde er de forskellige kanaler, passager og ringkamre påformet eller eroderet ind i et indre dyselegeme 52 på den forreste flade 52a og en perifer væg 52b i dette legeme 30 og er dækket ved hjælp af et dysehus af den i fig. 4 viste art. Dyselegemet 52 er fortrinsvis støbt ud i et med aktiver ingshovedet 50 og rager frem fra bunden 51b af recessen 51a i sidevæggen 51 i en sådan højdeudstrækning, at der tilbagestår et tilstrækkeligt spillerum ovenover og om- qr kring dyselegemet til at opnå en fast, tæt anbringelseFIG. 13 shows a longitudinal section through an actuating head in which another suitable embodiment of the atomizer nozzle according to the invention is arranged. In this case, the various channels, passageways and annular chambers are formed or eroded into an inner nozzle body 52 on the front face 52a and a peripheral wall 52b of this body 30 and covered by a nozzle housing of the embodiment shown in FIG. 4. The nozzle body 52 is preferably molded into one with the actuating head 50 and protrudes from the bottom 51b of the recess 51a in the sidewall 51 to such a height as to leave sufficient clearance above and around the nozzle body to obtain a firm, tight placement.

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12 151045 af dysehuset 53 i sidevæggen 51 for aktiveringshovedet 50.12 of the nozzle housing 53 in the side wall 51 of the actuating head 50.

En sådan udførelsesform er kun mulig, hvis dyselegemet 52's diameter tillader tilvejebringelsen af fire aksiale forsyningskanaler 35 ved sprøjtestøbningsteknik, dvs., 5 at hvis diameteren er for stor, vil kanalerne 35 blive for lange. Da kanalerne 35 skal have et meget lille tværsnitsareal, svarende til en diameter på mellem 0,3 og 0,6 mm i afhængighed af viskositeten af produktet, må kanalerne holdes så korte som muligt. Forsøg har vist, at 10 den mest hensigtsmæssige øvre grænse for den samlede diameter af dyselegemet 52 udgør omkring 16 mm i denne udførelsesform. Hvis diameteren skal være større af en eller anden grund er det tilrådeligt at vælge den i fig. 1 viste udførelsesform. Hovedtilførselskanalen 54 har en afkortet 15 kanaldel 56 ved den indre endevæg 52c af dyselegemet 52 og en resterende, indsnævret kanaldel 57, som fører længere ind i aktiveringshovedet 50. Desuden må vinklen β mellem den blinde ende 57a af den indsnævrede kanaldel 57 og dysens midterakse være fladere end den tilsvarende vinkel a, 20 som er dannet mellem midteraksen og den blinde ende 56a af den afkortede kanaldel 56. Disse med en indbyrdes vinkel anbragte blinde ender 56a og 57a tjener som afbøjningsflader eller dæmpningsflader for den væske, som strømmer i hovedtilførselskanalen 54, og som tilbagekastes ved hjælp 25 af disse afbøjningsflader med et mere eller mindre kraftigt tryk i de aksiale tilførselskanaler 35. Hvis hovedtilførselskanalen 54 havde været cylindrisk, ville der opstå et opstemningstryk ved den blinde ende af kanalen, hvilket tryk ville kaste væsken tilbage under et højere tryk via 30 de øvre tilførselskanaler 35 end via de nedre tilførselskanaler 35. Ifølge opfindelsen er dette undgået, idet tilbagekastningsfladen 56a rager ind i hovedtilførselskanalen 54's område oven over de nedre kanaler 35, og tilbagekastningsfladens hældningsvinkel og overflade er valgt på 35 en sådan måde, at det returtryk, som dannes i de under- i3 151045Such an embodiment is only possible if the diameter of the nozzle body 52 allows the provision of four axial supply channels 35 by injection molding technique, i.e., that if the diameter is too large, the channels 35 will be too long. Since the channels 35 must have a very small cross-sectional area, corresponding to a diameter of between 0.3 and 0.6 mm, depending on the viscosity of the product, the channels must be kept as short as possible. Tests have shown that the most convenient upper limit for the overall diameter of the nozzle body 52 is about 16 mm in this embodiment. If the diameter is to be larger for any reason, it is advisable to select the one shown in FIG. 1. The main supply channel 54 has a truncated channel portion 56 at the inner end wall 52c of the nozzle body 52 and a residual narrowed channel portion 57 which leads further into the activation head 50. In addition, the angle β between the blind end 57a of the narrowed channel portion 57 and the center axis of the nozzle must be flattened than the corresponding angle α, 20 formed between the center axis and the blind end 56a of the truncated channel portion 56. These mutually disposed blind ends 56a and 57a serve as deflection or damping surfaces for the fluid flowing in the main supply channel 54, and which are thrown back by these deflecting surfaces with a more or less strong pressure in the axial supply ducts 35. If the main supply duct 54 had been cylindrical, a thrusting pressure would occur at the blind end of the duct, which would throw the liquid back under a higher pressure via the upper supply channels 35 than via the lower supply channels 35. According to the invention this is avoided as the throwing surface 56a projects into the area of the main supply channel 54 above the lower channels 35, and the angle of inclination and surface of the throwing surface is selected in such a way that the return pressure formed in the sub-channels

OISLAND

liggende kanaler 35, er identisk med trykket i de øvre kanaler 35. Hvis de fire kanaler 35 har en ujævn tryk-fordeling, vil den udsendte tåge være usymmetrisk. Af de fire kanaler 35 er kun vist de to, som ligger i snit- 5 planet.lying channels 35 are identical to the pressure in the upper channels 35. If the four channels 35 have an uneven pressure distribution, the emitted fog will be asymmetrical. Of the four channels 35, only the two located in the section plane are shown.

Dysen ifølge opfindelsen overflødiggør brugen af en pumpe, som ikke alene kræver et gentaget tryk for udsendelse af produktet, men som tillige pumper omgivende luft og dermed oxygen ind i produktbeholderen, hvilket natur-10 ligvis medfører en uønsket oxidering af produktet.The nozzle of the invention eliminates the use of a pump which not only requires repeated pressure to dispense the product, but also pumps ambient air and thus oxygen into the product container, which naturally results in undesirable oxidation of the product.

Med henblik på at illustrere nyttevirkningen af en forstøverdyse ifølge opfindelsen, skal det nævnes, at laboratorieforsøg har vist, at det er muligt at spare op til 75% af drivmiddelgassen i aerosoldåser ved hjælp af 15 en dyse ifølge opfindelsen.In order to illustrate the usefulness of a nebulizer nozzle according to the invention, it should be mentioned that laboratory experiments have shown that it is possible to save up to 75% of the propellant gas in aerosol cans by means of a nozzle according to the invention.

Sammenfattende kan fordelene ved en forstøverdyse ifølge opfindelsen udtrykkes i følgende punkter; (a) Forstøverdysen ifølge opfindelsen er i stand til at udstråle en væske, som alene er under et rent me-20 kanisk tryk på omkring 2 ato med samme tågekvalitet, som opnås ved de i dag kommercielt tilgængelige forstøver-dys^r, der blot arbejder ved et tryk på 6 ato.In summary, the advantages of a nebulizer nozzle according to the invention can be expressed in the following points; (a) The nebulizer nozzle of the invention is capable of radiating a liquid which is only under a purely mechanical pressure of about 2 ato with the same fog quality achieved by the commercially available nebulizer nozzles which are merely works at a pressure of 6 ato.

j (b) Ved aerosoldåser betyder dette, at drivgassen ikke længere behøver at tjene som både udsendelsesenergi 25 og udstrålingsfaktor som følge af trykfaldet i den omgi- i vendb luft, men nu alene skal tilvejebringe et tryk, som netop er tilstrækkelig til fuldt ud at anvende de mekaniske opbrydningsegenskaber ved forstøverdysen ifølge opfindelsen.j (b) For aerosol cans, this means that the propellant no longer has to serve as both emission energy 25 and radiation factor due to the pressure drop in the ambient air, but must now only provide a pressure sufficient to fully apply the mechanical breaking properties of the nebulizer nozzle of the invention.

30 (c) Dette medfører atter, at det ikke lasngere er nød vendigt at anvende en drivgasblanding, f.eks. Freon 11 og Freon 12, som hidtil har været nødvendig for dels at frembringe en tilstrækkelig stor mængde gas, der tjener som udstrålingsfaktor, dels at ændre udsendelsestrykket ved hjælp 35 af forskellige mængder af en eller anden komponent af gas-(C) This again means that it is no longer necessary to use a propellant mixture, e.g. Freon 11 and Freon 12, which have heretofore been necessary to produce a sufficiently large amount of gas serving as a radiating factor, and partly to change the emission pressure by different amounts of some component of the gas.

OISLAND

14 151045 blandingen, på grund af de i blandingen indgåede komponenters forskellige kogepunkter, idet der ved anvendelse af forstøverdysen ifølge opfindelsen blot anvendes den drivmiddelgas, som har det laveste kogepunkt, og kun i en så-5 dan mængde, at et overskydende tryk på omkring 2 ato opnås i aerosoldåsen.The mixture, due to the various boiling points of the mixture contained in the mixture, uses only the propellant gas having the lowest boiling point, and only in such an amount that an excess pressure of about 2 ato is obtained in the aerosol can.

(d) Forsøg har vist, at f.eks. i forbindelse med hårlak, skal der blot påfyldes 19% Freon 12 svarende til et tryk på 1,7 ato på aerosoldysen, når der anvendes en for-10 støverdyse ifølge opfindelsen, hvor det tidligere var nødvendigt at anvende 77% gasblanding af Freon 11 og 12 svarende til et tryk på 3,8 ato med henhlik på at opnå tilsvarende strålekvaliteter. Forstøverdysen ifølge opfindelsen arbejder tillige ved et tryk på 1,7 ato eller endog 15 alt efter den krævede dråbestørrelse, ned til 0,8 ato, hvis dette tryk frembringes af en drivgas. Dette forhold kan forklares derved, at drivgassen når den har udfyldt sin mission som udsendelsesenergikilde, afspændes, selv om det.også kun sker i mindre udstrækning 20 i kontakt med den omgivende luft, og således som udstrålingsfaktor kompenserer for den ovenfor omtalte ned til 2 ato manglende trykandel.(d) Experiments have shown that e.g. in the case of hair varnish, only 19% Freon 12 must be filled, corresponding to a pressure of 1.7 ato on the aerosol nozzle, when using a pre-spray nozzle according to the invention, where it was previously necessary to use 77% gas mixture of Freon 11 and 12 corresponding to a pressure of 3.8 ato with the aim of obtaining similar radiation qualities. The atomizer nozzle according to the invention also operates at a pressure of 1.7 ato or even 15 depending on the required droplet size, down to 0.8 ato if this pressure is produced by a propellant gas. This relationship can be explained by the fact that when the gas has fulfilled its mission as a source of emission energy, the propellant is relaxed, although it also only occurs to a lesser extent 20 in contact with the ambient air, and thus as the emission factor compensates for the above-mentioned down to 2 ato. lack of pressure proportion.

Forsøg har endvidere vist, at som følge af de mekaniske opbrydningsegenskaber i forstøverdysen ifølge op-25 findelsen vil væsker, som tvinges gennem dysen under et højt tryk, kunne blive bragt til at fordampe som følge af den friktionsvarme, der opstår.Furthermore, tests have shown that due to the mechanical breaking up properties of the nebulizer nozzle according to the invention, liquids forced through the nozzle under a high pressure could be caused to evaporate as a result of the frictional heat generated.

Claims (17)

1. Forstøverdyse til afgivelse af en under overtryk stående væske i tågeform, hvilken dyse omfatter i det 5 mindste en første (33) og en anden del (32) , som ligger mod hinanden med endeflader, der er tværstillede i forhold til aksen (MA) gennem en udløbsåbning (41) i den første del (33), og der mellein delene (32, 33) er udformet strømningsveje (35^36, 37, 38, 39), som har et 10 centralt udløbskammer (45) med flere i forhold til aksen (MA) i hovedsagen tangentialt deri udmundende kanaler (36, 38) fra i det mindste et omgivende ringkammer (37, 39), hvorhos der i kanalerne (36) i hovedsagen vinkelret på disse udmunder andre, i aksial retning forløbende 15 kanaler (35), gennem hvilke den under tryk stående væske (139) ude fra kan ledes til strømningsvejene, kendetegnet ved, at et taplignende afbøjningsfremspring (40) er anbragt centralt i udløbskammeret (45) over for udløbsåbningen (41) og strækker sig næsten helt 20 hen til denne, og/eller at der i mindst én af de tangen- tiale kanaler (36) findes et afbøjningsfremspring (23).A nebulizer nozzle for dispensing a pressurized mist in liquid form, said nozzle comprising at least a first (33) and a second portion (32) which are opposed to each other with end faces transverse to the axis (MA). ) through an outlet opening (41) in the first portion (33) and between the portions (32, 33), flow paths (35 ^ 36, 37, 38, 39) having a central outlet chamber (45) having several relative to the axis (MA), substantially tangentially opening therein (36, 38) therefrom from at least one surrounding annular chamber (37, 39), whereas in the channels (36) substantially perpendicular thereto, other axially extending 15 channels (35) through which the pressurized liquid (139) can be routed from the outside to the flow paths, characterized in that a pin-like deflection projection (40) is arranged centrally in the outlet chamber (45) opposite the outlet opening (41) and extends almost 20 to this, and / or that at least one of the tangents can a deflection projection (23) is provided (36). 2. Forstøverdyse ifølge krav 1, kendetegnet ved, at den første del (33) med udløbsåbningen (41) er udformet som et bægerformet hus, i hvilket den anden del 25 (32) er indstukket som en prop.Spray nozzle according to claim 1, characterized in that the first part (33) with the outlet opening (41) is formed as a cup-shaped housing, in which the second part 25 (32) is inserted as a plug. 3. Forstøverdyse ifølge krav 1, hvilken forstøverdyse har et ydre (37) og et indre ringkammer (39), kendetegnet ved, at det ydre ringkammer (37) med tangentialt udefra indmundende tilførselskanaler (36) 30 tjener til væsketilførsel af de til det indre r.tinukammer (39) førende tangentiale kanaler (38).A nebulizer nozzle according to claim 1, which has an outer (37) and an inner annulus (39), characterized in that the outer annulus (37) with tangentially exterior supply channels (36) 30 serves to supply the liquid to the interior. r.tinuc chamber (39) leading tangential channels (38). 4. Forstøverdyse ifølge krav 1 eller 3, kende -tegnet ved, at hver tangentialt til det ydre ringkammer (37) førende kanal (36) udmunder et kort stykke 35 ovenstrøms for en indløbsåbning (38a) til en kanal, der fører ud fra samme ringformede kammer. Ο 1β 151045 loSpray nozzle according to claim 1 or 3, characterized in that each channel (36) leading tangentially to the outer annular chamber (37) opens a short distance 35 upstream of an inlet opening (38a) to a channel leading from the same annular chamber. Ο 1β 151045 lo 5. Forstøverdyse ifølge et af de foregående krav, kendetegnet ved, at tværsnittet af de tangen-tiale kanaler (36, 38) aftager i strømningsretningen i det mindste i deres udløbsområder (36b, 38b).Spray nozzle according to one of the preceding claims, characterized in that the cross-section of the tangential channels (36, 38) decreases in the flow direction at least in their outlet areas (36b, 38b). 6. Forstøverdyse ifølge krav 5, kendeteg net ved, at tværsnittet af de tangentiale kanaler (36, 38) aftager kontinuerligt fra kanalernes indløbsåbninger (36a, 38a) til deres udløbsområder (36b, 38b).Spray nozzle according to claim 5, characterized in that the cross-section of the tangential channels (36, 38) decreases continuously from the inlet openings (36a, 38a) of the channels to their outlet areas (36b, 38b). 7. Forstøverdyse ifølge krav 1 eller 3, kende- 10 tegnet ved, at det ydre ringkammer (37) har et større tværsnit end det indre ringkammer (39).Spray nozzle according to claim 1 or 3, characterized in that the outer ring chamber (37) has a larger cross-section than the inner ring chamber (39). 8. Forstøverdyse ifølge krav 1-7, kendetegnet ved, at udmundingstværsnittet af hver tangential kanal (36, 38) ved indmundingsstedet (36b, 38b) i et 15 ringkammer (37, 39) højest andrager en trediedel af tværsnittet af det ringformede kammer (37, 39).Nebulizer nozzle according to claims 1-7, characterized in that the orifice cross-section of each tangential channel (36, 38) at the orifice (36b, 38b) of a ring chamber (37, 39) is at most a third of the cross-section of the annular chamber ( 37, 39). 9. Forstøverdyse ifølge krav 1-8, kendetegnet ved, at de tangentiale kanaler (36, 38), ringkamrene (37, 39) og udløbskammeret (45) er udformede som 20 fordybninger i forsiden af den som en prop udformede anden del (32).Nebulizer nozzle according to claims 1-8, characterized in that the tangential channels (36, 38), the annular chambers (37, 39) and the outlet chamber (45) are formed as 20 recesses in the front of the second portion (32) formed as a plug. ). 10. Forstøverdyse ifølge krav 9, hvor der er afbøjningsfremspring (23} i flere tangentiale kanaler (36), kendetegnet ved, at afbøjningsfremspringet 25 eller -fremspringene (23) er udformet som trin i bunden af nævnte fordybninger.Spray nozzle according to claim 9, wherein there are deflection projections (23} in several tangential channels (36), characterized in that the deflection projections 25 or projections (23) are formed as steps at the bottom of said recesses). 11. Forstøverdyse ifølge krav 1-9, kendetegnet ved, at afbøjningsfremspringene (23) befinder sig i området ved indløbsåbningen og/eller i en tangential 30 kanals (38) indgangsmunding i henholdsvis afgangsmunding fra et ringkammer (39).Spray nozzle according to claims 1-9, characterized in that the deflection projections (23) are in the region of the inlet opening and / or in a tangent 30 channel (38) entrance orifice respectively of a ring chamber (39). 12. Forstøverdyse ifølge et af de foregående krav, kendetegnet ved, at en kravelignende ringribbe (42), der omgiver udløbsåbningen (41) , strækker sig 35 ind mod udløbskammeret (45). i7 151045 OSpray nozzle according to one of the preceding claims, characterized in that a collar-like ring rib (42) surrounding the outlet opening (41) extends 35 towards the outlet chamber (45). i7 151045 O. 13. Forstøverdyse ifølge et af de foregående krav, kendetegnet ved, at den aksiale afstand mellem forsiden af det taplignende afbøjningsfremspring (40) og indgangen til udløbsåbningen (41) højest er 5 0,1 mm.Spray nozzle according to one of the preceding claims, characterized in that the axial distance between the front of the pin-like deflection projection (40) and the entrance to the outlet opening (41) is at most 0.1 mm. 14. Forstøverdyse ifølge et af kravene 1-13, kendetegnet ved, at det taplignende afbøjningsfremspring (40) har en central fordybning (40a).Spray nozzle according to one of claims 1-13, characterized in that the pin-like deflection projection (40) has a central recess (40a). 15. Forstøverdyse ifølge krav 14, kende- 10 tegnet ved, at den aksiale afstand mellem ende fladen af det taplignende afbøjningsfremspring (40) og endekanten af ringribben (42) højest er 0,05 mm.A nebulizer nozzle according to claim 14, characterized in that the axial distance between the end face of the pin-like deflection projection (40) and the end edge of the annular rib (42) is at most 0.05 mm. 16. Forstøverdyse ifølge et af de foregående krav, kendetegnet ved, at dysen har tilførsels- 15 kanaler (29) for et andet medium, hvilke kanaler for løber i hovedsagen tangentialt udefra til det yderste ringkammer (37).A nebulizer nozzle according to one of the preceding claims, characterized in that the nozzle has supply channels (29) for another medium, which channels for running substantially tangentially from the outside to the outer ring chamber (37). 17. Forstøverdyse ifølge krav 16, kendetegnet ved, at ringkammeret (37) indsnævres således 20. strømningsretningen før indmundingen af hver til førselskanal (29), at indmundingen befinder sig i det af indsnævringen fremkaldte sugeområde.Nebulizer nozzle according to claim 16, characterized in that the annulus (37) narrows so that the flow direction 20 before the mouth of each of the guide ducts (29) is located in the suction area caused by the constriction.
DK340378A 1977-08-02 1978-08-01 SUSPENSION VALUES FOR DELIVERING A UNDERPRESSED LIQUID BASKET DK151045C (en)

Applications Claiming Priority (6)

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CH960777A CH618355A5 (en) 1977-08-02 1977-08-02 Diffuser container
CH960777 1977-08-02
CA288,724A CA1077001A (en) 1976-10-21 1977-10-14 Appliance for discharging gaseous liquid or pasty product, and process of its manufacture
CA288724 1977-10-14
CH202478A CH646619A5 (en) 1977-10-14 1978-02-24 Spray nozzle
CH202478 1978-02-24

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DK151045B true DK151045B (en) 1987-10-19
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Also Published As

Publication number Publication date
ATA519478A (en) 1990-07-15
FR2399282B1 (en) 1988-06-10
NO151649C (en) 1985-05-15
IT7822318A0 (en) 1978-04-14
IE48169B1 (en) 1984-10-17
DK340378A (en) 1979-02-03
IN150150B (en) 1982-07-31
IT1094411B (en) 1985-08-02
NO782630L (en) 1979-02-05
BR7804953A (en) 1979-03-06
FI782247A (en) 1979-02-03
ES470662A1 (en) 1979-02-16
PT68370A (en) 1978-09-01
AT392044B (en) 1991-01-10
DE2826784C2 (en) 1988-10-13
AU3810378A (en) 1980-01-24
IE781548L (en) 1979-04-14
DD140713A5 (en) 1980-03-26
EP0000688A3 (en) 1979-02-21
FR2399282A1 (en) 1979-03-02
NO151649B (en) 1985-02-04
JPS5459613A (en) 1979-05-14
IL55155A0 (en) 1978-09-29
EP0000688B1 (en) 1984-01-11
FI64331C (en) 1983-11-10
DK151045C (en) 1988-03-14
FI64331B (en) 1983-07-29
EP0000688A2 (en) 1979-02-07
JPS6312664B2 (en) 1988-03-22
AU521493B2 (en) 1982-04-08
DE2826784A1 (en) 1979-02-15
AR219333A1 (en) 1980-08-15

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