EP0615512A1 - Universal gradual propulsion and/or active spraying system for aerosols - Google Patents

Universal gradual propulsion and/or active spraying system for aerosols

Info

Publication number
EP0615512A1
EP0615512A1 EP19930913136 EP93913136A EP0615512A1 EP 0615512 A1 EP0615512 A1 EP 0615512A1 EP 19930913136 EP19930913136 EP 19930913136 EP 93913136 A EP93913136 A EP 93913136A EP 0615512 A1 EP0615512 A1 EP 0615512A1
Authority
EP
Grant status
Application
Patent type
Prior art keywords
propulsion
element
part
product
upper
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP19930913136
Other languages
German (de)
French (fr)
Inventor
Joseph Ferraye
Michel Ferraye
Dante Mario Ferretti
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
FERRAYE Joseph
FERRAYE Michel
FERRETTI Dante Mario
Original Assignee
FERRAYE, Joseph
FERRAYE, Michel
FERRETTI, Dante Mario
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date

Links

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
    • B65D83/44Valves specially adapted therefor; Regulating devices

Abstract

L'invention concerne un système universel de propulsion et d'atomisation actives avec ses éléments de propulsion et d'atomisation pour par exemple les aérosols, comprenant un boîtier (1) et un embout de propulsion classiques, comportant un conduit (3), joignant la partie inférieure (4) du boîtier (1), permettant la propulsion du produit et une tuyère (5) joignant la partie supérieure (6) du boîtier, permettant la propulsion du gaz; The invention relates to a universal propulsion system and active atomization with its propulsion elements and atomization for example aerosols, comprising a housing (1) and a conventional propulsion nozzle comprising a conduit (3), joining the lower part (4) of the housing (1), allowing the propulsion of the product and a nozzle (5) joining the upper part (6) of the housing, allowing the propulsion gas; le système comporte un premier élément de propulsion, comprenant une partie inférieure (7) et une partie supérieure (8); the system includes a first propulsion unit, comprising a lower part (7) and an upper part (8); la partie inférieure (7) ayant un diamètre intérieur plus petit que la partie supérieure (8), formant par exemple par la différence un rebord (9) à l'intérieur du premier élément de propulsion (17), permettant de séparer la partie supérieure (8) et la partie inférieure (7), en deux compartiments indépendants par l'appui sur l'embout de propulsion (2) agissant sur le deuxième élément de propulsion; the lower part (7) having an inner diameter smaller than the upper part (8), forming, for example by the difference a flange (9) inside the first propulsion member (17) for separating the upper portion (8) and the lower part (7) into two separate compartments by pressing the propulsion nozzle (2) acting on the second drive member; la partie supérieure comporte aussi une bordure (00), permettant de maintenir le premier élément de propulsion sur le bouchon et un rebord (000) permettant de bloquer le joint contre le bouchon (20); the upper part also has a border (00) for maintaining the first drive member on the stopper and a flange (000) for locking the gasket against the plug (20); le gaz propulsé par le trou (15) se mélange avec le produit propulsé par le trou (16) dans le conduit terminal (0) activant la propulsion et l'atomisation du produit. gas powered by the hole (15) mixes with the product propelled through the hole (16) into the terminal conduit (0) activating the propulsion and atomization of the product.

Description

DESCRIPTION SYSTEM PROGRESSIVE PROPULSION AND UNIVERSAL OR SPRAY AEROSOLS FOR ACTIVE The present invention relates to a universal propulsion and active atomization with atomizing and propelling member system to, for ex¬ xample aerosols, comprising a housing (1) and a spray tip propul¬ sion (2) classics, the new system includes a conduit (3) joining the bottom (4) of the housing (1), allowing the propulsion of the product and a nozzle (5) , joining the upper part (6) of the housing, allowing the propulsion gas; the system includes a first propulsion element com¬ taking for example a lower part (7) and an upper part (8), the lower part (7) having an inner diameter smaller than the su¬ périeure part (8), forming, for example by the difference a flange (9) at the Eur intéri¬ the first drive member, for separating the supéri¬ eure part (8) and lower portion (7) of the first propulsion element, into two separate compartments by pressing the propulsion nozzle (2) acting on the second drive element, the upper portion of the first drive element also has a border (00 ) for holding the pre¬ Mier propulsion element on the cap and a flange (000) for locking the seal (20) against the plug and the gas propelled through the hole (15) mixes with the product powered by the hole (16) into the terminal conduit (0), and activating the propulsion 1'atomisation the product.

The invention includes a second drive member comprising for example a lower portion (10) for holding a spring (11) and a re¬ upper edge (12) for locking the small gasket (13) against the sth troi¬ propulsion member (17); the upper portion of the second propulsion member is extended by a cylinder (1A), comprising the terminal conduit (0), comprising, for example, a hole (16) for propulsion of the * product and a hole (15) for the propulsion of the gas.

The invention comprises a third drive member (17) having, e.g., a central milled (18) for linear movement of the cylinder (14) forming part of the second propulsion member and an upper rim (19), blocking the large o (20) against the plug and the central cutting of the third drive member (17) comprises an upper part, compre¬ ing a milling having a larger diameter (21) than its lower part for accommodating a small spring (22) softer than the large (11), the spring (22) pushes the third propulsion member against the flange (9) inside the first propulsion element, separating the upper portion (8) and the lower part (7) the first propulsion element in two corn-

SUBSTITUTE SHEET

ISA / EP independent compartments by pressing on the propulsion piece (2) and the downward movement of the second drive element, the spring (11) is stronger than the spring (22) for locking the spring (22 ) in the milling (21) for stopping the propulsion.

Pressing the propulsion nozzle (2) acting on the second propulsion member, unlocks the third drive member and the spring (22) agis¬ sant on the third drive member (17), the blocks against the flange (9) inside the first propulsion element, separating the inféri¬ eure part (7) and the upper part (8) of the first propulsion element into two independent compartments and releasing the seals (20,13) and the holes (15,16), the small gasket (13) is interposed between the third element of propul¬ sion (17) and the flange (9) of the first propulsion element and the gas powered by the hole (15) is mixed with the product propelled through the hole (16) into the terminal conduit (0), activating the propulsion and atomization of the product. The spring (11) acts on the second drive element ensuring the bloca¬ ge of the two joints (20,13) and holes (15,16) for stopping the propulsion. The first variant comprises the duct (3) and the nozzle (5) and the holes (15,16) reversed.

The second propulsion element of the second embodiment includes, for pho exem¬ a slit (16p) vertical, or overlapping holes for propulsion of the product and a slit (15p) vertical, or superimposed holes for gas propul¬ sion allowing the progressive supported on the propulsion piece (2), acting on the second drive element, the gradual release of the slit (16p) joining the product and of the slot (15p) connecting the gas and propulsion progressive product.

The second propulsion element of the third variant includes exem¬ ple by a notch (23s) having the larger seal (20s) and the small seal (13s) superposed and the small O acting on the hole (16s) joining the product and great seal acting on the hole (15s) joining the gas pressing the propulsion EMBOU (2), acting on the second drive element, blocks the small seal (13s) against the flange (9s), to within the first propulsion element, separating the upper portion (8) and the lower part (7) of the first propulsion element into two independent compartments, releasing the two seals (20s, 13s) superimposed and the holes (15s, 16s) ; gas propelled through the hole (15s) joining the upper housing part is mixed with the product propelled through the hole (16s) joining the lower part of the housing in the terminal conduit (0) activating the propulsion and atomization the off Product the fourth variant has a pet ite ring, or a small ledge making

REPLACEMENT FELILLE portion of the second propulsion member between the joints (20s, 13s) superimposed. The fifth embodiment comprises, inside the first propulsion element a countersinking (9c), allowing the support on the propulsion piece (2), acting on the second drive element of the small block seal (13s) in the countersinking (9c) (replacing the flange (9) of the first ele ¬ propulsion) and separating the upper portion (8) and the part inferi ¬ eure (7) of the first propulsion element into two independent compartments, releasing the two joints (20s, 13s) superimposed and the holes (15s, 16s) super¬ layered, the first drive element also comprises a nozzle (5) in the upper portion allowing the direct flow of gas in the conduit ter¬ minal (0) through the hole (15s), the gas powered by the hole (15s), joining the upper part (6) of the housing mixes with the product propelled through the hole (16s), joining the bottom (4) of the housing in the conduit ter¬ minal (0), activating the propulsion and atomization of the product. DESCRIBED THE SYSTEMS AND DRAWINGS SEALS ARE EXAMPLES AND DO NOT RESTRICT THE PROCESSES FOR CARRYING OUT THE INVENTION.

DRAWING I. REPRESENTS THE UNIVERSAL BOOSTER ACTIVA I. EXECUTIVE DRAWING II. UNIVERSAL ACTIVA II. EXECUTIVE

DRAWING III. p UNIVERSAL QUARTZ III. EXECUTIVE DRAWING IV. p UNIVERSAL ACTIVA IV. EXECUTIVE DRAWING V. UNIVERSAL s QUARTZ V. EXECUTIVE DRAWING VI. is UNIVERSAL ACTIVA VI. EXECUTIVE

Claims

01) universal propulsion system and active atomization with its propulsion element and atomization for example aerosols, comprising a housing and a conventional propulsion nozzle characterized in that it leads you compor¬ a joining part lower (4) of the housing for the pro¬ pulsion of product and a nozzle joining the upper part of the housing per putting the propulsion gas; the system comprises a first member of propu sion, for example comprising a lower portion and an upper portion; the lower part having such an inner diameter smaller than the upper portion, forming, for example by the difference a flange on the insid eur the first propulsion element for separating the re supérieu part (8) and the lower part (7 ) of the first propulsion element into two independent compartments by pressing on the propulsion piece (2) agissan on the second propulsion member; the upper part also comprises pa example an edge, for keeping the first drive element the cap and a flange, for locking the seal (20) against the bo chon; gas propelled through the hole (15) mixes with the propelled product pa the hole (16) into the terminal conduit, activating the propulsion and 'atomisatio product.
02) System according to claim 1, characterized in that it comprises a deu xth propulsion element, for example comprising a lower portion (10 for holding a spring and an upper rim (12), for locking the small seal, against the lower part of a third drive member, the upper portion of the second propulsion member is hold key by a cylinder comprising the terminal conduit, comprising for example a hole for propulsion of the product and a hole for the propulsion of the gas.
03) System according to claims 1 and 2, characterized in that it comprises a third drive member comprising for example a central milling permitting linear movement of the cylinder of the second propulsio member and an upper flange for locking the large seal against the cap central milling third propulsion element, comprises an upper part comprising a milling having a larger than its lower part diameter for accommodating a small spring softer than the large and the small spring acts on the third propulsion element , blocking it against the edge (9) inside the first propulsion element, by separating the lower tie (7) and the upper part (8), the first element of propul¬ sion into two independent compartments (7,8 ) by pressing the tip of pro drive (2), acting on the second drive member, the mainspring is stronger than the small Ressor t, for locking the small spring in the upper third milling propulsion member to the judgment of the propulsion.
04) System according to claims 1, 2 and 3, characterized in that the ap¬ pui on the propulsion piece (2) acting on the second element of pro¬ pulsion unlocks the third drive member and the small spring acting ¬ sant on the third propulsion element, the blocks against the flange (9) inside the first propulsion element, separating the supérieu¬ portion re and the lower portion of the first propulsion element in two independent and unlocking buildings compar¬ the largest ring and small O and propulsion holes of the product and the gas, the small gasket (13) interposed between the third drive member and the flange (9) inside the first propulsion member; the gas powered by the hole (15) mixes with the product propelled through the hole (16) into the terminal conduit (0), ac- tivant propulsion and atomization of the product.
05) System according to claims 1, 2, 3 and 4, characterized in that the mainspring acts on the second drive element, ensuring the locking of the two gaskets and holes (15,16) for stopping the propulsion .
06) System according to claims 1, 2, 3, 4 and 5, characterized in that the first variant includes the conduit and the nozzle and the two holes (15,16) reversed.
07) System according to claims 1, 2, 3, 4, 5 and 6, characterized in that the second propulsion member of the second embodiment comprises, for example a vertical slot or overlapping holes for propulsion of the product and a vertical slot or superposed holes for the propulsion gas, as by the gradual permet¬ supported on the propulsion piece, the release progres¬ sif of the slot joining the product and of the slot joining the gas and the pro¬ pulsion of the progressive product.
08) System according to claims 1, 2, 3, 4, 5, 6 and 7, characterized in that the second propulsion member of the third embodiment comprises, for example a notch having the general joint and the small superimposed joint; the small seal hole ioignant acts on the product and the great seal acts on the joining hole gas; 1'appui
SUBSTITUTE SHEET ISA / EP on the propulsion piece (2) acting on the second drive element, blocks the small seal (13s) against the flange (9s) inside the first ele ment propulsion, separating the part upper (8) and the lower part (7) of the first propulsion element into two independent compartments and dé¬ blocking two seals (20s, 13s) and at least one hole (16s) joining the pro¬ Duit and the hole (15s ) joining the gas, the gas powered by the hole (15s) joi¬ Gnant the upper housing part, mixes with the product propelled through the hole (16s) joining the lower part of the housing in the conduit ended (00) activating the propulsion and atomization of the product.
09) System according to claims 1, 2, 3, 4, 5, 6, 7 and 8, characterized in that the fourth embodiment has a small ring or a small flange fai sant portion of the second propulsion member between the two seals bunk (20s, 13s).
10) System according to claims 1, 2, 3, 4, 5, 6, 7, 8 and 9, characterized in that the first propulsion element of the fifth embodiment comprises, inside a countersinking (9c) for by pressing the propulsion nozzle (2) acting on the second drive element, to block the small seal (13s) in the countersinking (9c) within the first élé¬ ment propulsion, separating the part upper (8) and the lower part (7) of the first propulsion element into two independent compartments and dé¬ blocking two seals (20s, 13s) superimposed and at least one hole (16s) joi¬ Gnant the product and the hole ( 15s) joining the gas, the upper part of the first-mentioned drive element also comprises a nozzle (5) for the direct flow of gas into the terminal conduit (0) through the hole (15s), by joining the upper tie housing ; gas propelled through the hole (15s) joining the upper part (6) of the housing ( 1), is mixed with the product propelled through the hole (16s) joining the bottom (4) of the housing (1) into the conduit ended (0), activating the propulsion and atomization of the product.
SUBSTITUTE SHEET
! SA / i: c
EP19930913136 1992-06-22 1993-06-16 Universal gradual propulsion and/or active spraying system for aerosols Withdrawn EP0615512A1 (en)

Priority Applications (13)

Application Number Priority Date Filing Date Title
ITPN920048 1992-06-22
ITPN920048 1992-06-22
FR9303471 1993-03-22
FR9303471A FR2711972A1 (en) 1993-03-22 1993-03-22 Universal aerosol elements and system with active propulsion and atomization
FR9306340 1993-05-21
FR9306340 1993-05-21
FR9306392 1993-05-24
FR9306392 1993-05-24
FR9306547 1993-05-26
FR9306547 1993-05-26
FR9307108 1993-06-08
FR9307108 1993-06-08
PCT/FR1993/000581 WO1994000367A1 (en) 1992-06-22 1993-06-16 Universal gradual propulsion and/or active spraying system for aerosols

Publications (1)

Publication Number Publication Date
EP0615512A1 true true EP0615512A1 (en) 1994-09-21

Family

ID=27546410

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19930913136 Withdrawn EP0615512A1 (en) 1992-06-22 1993-06-16 Universal gradual propulsion and/or active spraying system for aerosols

Country Status (2)

Country Link
EP (1) EP0615512A1 (en)
WO (1) WO1994000367A1 (en)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR84908E (en) * 1963-04-04 1965-05-07 Commissaria A L En Atomique Improvements to casting processes, including ingots, and in particular uranium carbide
US4398654A (en) * 1978-12-26 1983-08-16 American Cyanamid Company Aerosol dispensing system
DE3623934C2 (en) * 1986-07-16 1991-01-24 Cebal Verpackungen Gmbh & Co Kg, 8500 Nuernberg, De
EP0440855A1 (en) * 1990-02-08 1991-08-14 Deutsche Präzisions-Ventil GmbH Spray valve assembly
DE69012790D1 (en) * 1990-03-06 1994-10-27 Coster Tecnologie Speciali Spa Valves for liquid atomizer.
DE9190042U1 (en) * 1990-03-23 1993-01-14 Hubacek, Hugo, Prof. Dr.
FR2674774B1 (en) * 1991-04-08 1993-07-16 Oreal Device for spraying a liquid comprising a pressurized container fitted with a valve has additional gas intake.
FR2684358B1 (en) * 1991-12-02 1995-01-20 Oreal Aerosol device for dispensing a composition has relatively high viscosity.

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9400367A1 *

Also Published As

Publication number Publication date Type
WO1994000367A1 (en) 1994-01-06 application

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