EP0615512A1 - Universelles system zum progressiven treiben und/oder aktiven versprühen von aersolen - Google Patents

Universelles system zum progressiven treiben und/oder aktiven versprühen von aersolen

Info

Publication number
EP0615512A1
EP0615512A1 EP93913136A EP93913136A EP0615512A1 EP 0615512 A1 EP0615512 A1 EP 0615512A1 EP 93913136 A EP93913136 A EP 93913136A EP 93913136 A EP93913136 A EP 93913136A EP 0615512 A1 EP0615512 A1 EP 0615512A1
Authority
EP
European Patent Office
Prior art keywords
propulsion
propulsion element
product
hole
joining
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Withdrawn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
EP93913136A
Other languages
English (en)
French (fr)
Inventor
Joseph Ferraye
Dante Mario Ferretti
Michel Ferraye
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.)
Individual
Original Assignee
Individual
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
Priority claimed from ITPN920048A external-priority patent/IT1263285B/it
Priority claimed from FR9303471A external-priority patent/FR2711972A1/fr
Application filed by Individual filed Critical Individual
Publication of EP0615512A1 publication Critical patent/EP0615512A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS 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
    • B65D83/00—Containers or packages with special means for dispensing contents
    • B65D83/14—Containers 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
    • B65D83/44—Valves specially adapted therefor; Regulating devices

Definitions

  • the present invention relates to a universal active propulsion and atomization system with its propulsion and atomization elements for, for example aerosols, comprising a housing (1) aerosol and a conventional propulsion nozzle (2); the new system comprises a conduit (3) joining the lower part (4) of the housing (1), allowing the product to be propelled and a nozzle (5) , joining the upper part (6) of the housing, allowing the propulsion of the gas; the system comprises a first propulsion element comprising for example a lower part (7) and an upper part (8); the lower part (7) having an inner diameter smaller than the upper part (8), forming for example by the difference a rim (9) inside the first propulsion element, making it possible to separate the upper part (8) and the lower part (7) of the first propulsion element, in two independent compartments by pressing on the propulsion end piece (2) acting on the second propulsion element; the upper part of the first propulsion element comprises also a border (00) making it possible to maintain the first propulsion element on the stopper and a flange (000
  • the invention comprises a second propulsion element comprising for example a lower part (10), making it possible to hold a spring (11) and an upper edge (12) making it possible to block the small seal (13) against the third.
  • element of propulsion (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 propelling gas.
  • the invention comprises a third propulsion element (17) comprising, for example a central milling (18) allowing the linear movement of the cylinder (14) forming part of the second propulsion element and an upper rim (19), blocking the large joint (20) against the plug;
  • the central milling of the third propulsion element (17) has an upper part, including a milling having a larger diameter (21) than its lower part, making it possible to accommodate a small spring (22) softer than the large one (11); the spring (22) pushes the third propulsion element against the flange (9) inside the first propulsion element, separating the upper part (8) and the lower part (7) of the first propulsion element in two parts
  • the spring (11) is stronger than the spring (22) allowing the spring (22) to be locked in the milling (21) when the propulsion stops.
  • the spring (11) acts on the second propulsion element ensuring the blocking of the two seals (20,13) and the holes (15,16) when the propulsion stops.
  • the first variant comprises the conduit (3) and the nozzle (5) as well as the inverted holes (15, 16).
  • the second propulsion element of the second variant comprises, for example a vertical slot (16p), or superimposed holes for the propulsion of the product and a vertical slot (15p), or superimposed holes for the propulsion of the gas , allowing by progressive support on the propulsion nozzle (2), acting on the second propulsion element, the progressive release of the slot (16p) joining the product and of the slot (15p) joining the gas and the propulsion progressive product.
  • the second propulsion element of the third variant comprises for example a notch (23s) comprising the large seal (20s) and the small seal (13s) superimposed; the small seal acting on the hole (16s) joining the product and the large seal acting on the hole (15s) joining the gas; pressing on the propulsion nozzle (2), acting on the second propulsion element, blocks the small seal (13s) against the flange (9s), at the inside the first propulsion element, separating the upper part (8) and the lower part (7) of the first propulsion element into two independent compartments, unlocking the two superimposed seals (20s, 13s) and the holes (15s, 16s) the gas propelled by the hole (15s) joining the upper part of the housing, mixes with the product propelled by the hole (16s) joining the lower part of the housing, in the terminal duct (0) activating the propulsion and atomization
  • the fourth variant includes a pet ite ring, or a small rim making
  • the fifth variant comprises, inside the first propulsion element, a conical milling (9c), allowing by pressing on the propulsion end piece (2), acting on the second propulsion element to block the small seal (13s) in the countersinking (9c) (replacing the flange (9) of the first ele ⁇ propulsion) and separating the upper portion (8) and the inferi part ⁇ eure (7) of the first propulsion element into two independent compartments, releasing the two superimposed seals (20s, 13s) and the superposed holes (15s, 16s); the first propulsion element also includes a nozzle (5), in the upper part allowing the direct arrival of gas in the ter ⁇ duct minimum (0) through the hole (15s); the gas propelled through the hole (15s), joining the upper part (6) of the housing mixes with the product propelled through the hole (16s), joining the lower part (4) of the housing in the terminal duct (0), activating the propulsion and
EP93913136A 1992-06-22 1993-06-16 Universelles system zum progressiven treiben und/oder aktiven versprühen von aersolen Withdrawn EP0615512A1 (de)

Applications Claiming Priority (13)

Application Number Priority Date Filing Date Title
ITPN920048 1992-06-22
ITPN920048A IT1263285B (it) 1992-06-22 1992-06-22 Dispositivo universale di aerosol a propulsione e dinamica attive
FR9303471 1993-03-22
FR9303471A FR2711972A1 (fr) 1993-03-22 1993-03-22 Système et éléments d'aérosol universel à propulsion et atomisation actives.
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 (fr) 1992-06-22 1993-06-16 Systeme universel de propulsion progressive et ou d'atomisation active pour aerosols

Publications (1)

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

Family

ID=27546410

Family Applications (1)

Application Number Title Priority Date Filing Date
EP93913136A Withdrawn EP0615512A1 (de) 1992-06-22 1993-06-16 Universelles system zum progressiven treiben und/oder aktiven versprühen von aersolen

Country Status (2)

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

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR84908E (fr) * 1963-04-04 1965-05-07 Commissaria A L En Atomique Perfectionnements apportés aux procédés de coulée, notamment de lingots, et en particulier de carbure d'uranium
US3391834A (en) * 1966-10-10 1968-07-09 Precision Valve Corp Valved closure for a pressurized dispenser
US4398654A (en) * 1978-12-26 1983-08-16 American Cyanamid Company Aerosol dispensing system
DE3623934A1 (de) * 1986-07-16 1988-01-21 Cebal Verpackungen Behaelter mit zahnpasta
EP0440855A1 (de) * 1990-02-08 1991-08-14 Deutsche Präzisions-Ventil GmbH Sprühventilanordnung
IT1243765B (it) * 1990-03-06 1994-06-28 Coster Tecnologie Speciali Spa Perfezionamenti alle valvole per l'erogazione nebulizzata di liquidi
DE9190042U1 (de) * 1990-03-23 1993-01-14 Hubacek, Hugo, Prof. Dr.
FR2674774B1 (fr) * 1991-04-08 1993-07-16 Oreal Dispositif de pulverisation d'un liquide comprenant un recipient pressurise muni d'une valve a prise de gaz additionnelle.
FR2684358B1 (fr) * 1991-12-02 1995-01-20 Oreal Dispositif aerosol pour distribuer une composition a viscosite relativement elevee.

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
WO1994000367A1 (fr) 1994-01-06

Similar Documents

Publication Publication Date Title
EP2139768B1 (de) Flugzeugmotorbefestigungspylon mit einer mit einer tonnenmutter versehenen hinteren motorbefestigung
EP2436601B1 (de) Vorrichtung zur Aufnahme der Schubkräfte eines Triebwerks mit drei in Reihe angeordneten Kugelgelenken
CA2613194C (fr) Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
EP1928739B1 (de) Verfahren zur montage eines fugzeugmotors auf einer starren strebenstruktur zur sicherung des motors
EP1928743B1 (de) Motoranordnung für ein flugzeug mit einem motor sowie einer motormontagestruktur für einen derartigen motor
EP1928742B1 (de) Motoranordnung für ein flugzeug mit einem motor sowie einer motormontagestruktur
EP1535838B1 (de) Aufhängung eines Triebwerks unter einer Flugzeugtragfläche
FR2755944A1 (fr) Suspension avant redondante pour turbomachine
WO2009147341A2 (fr) Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson
FR2887851A1 (fr) Mat d'accrochage de moteur pour aeronef
FR3040076A1 (fr) Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
USD947451S1 (en) Razor cartridge guard
CA2638143A1 (en) Conduit sleeve pass through for concrete construction
WO1999006745A8 (en) Improved retaining structure for a fuel tank mounted valve body
EP0615512A1 (de) Universelles system zum progressiven treiben und/oder aktiven versprühen von aersolen
EP1277516B1 (de) Ausgabekopf mit zwei Düsen
USD439876S1 (en) Supersonic aircraft with in-flight refueling system
USD914578S1 (en) Attendant module
USD296775S (en) Vehicle aerodynamic fairing
USD505204S1 (en) Nose, tail and wing tips for a jet airplane
USD974991S1 (en) Aircraft
US6843510B2 (en) System for coupling a fuel feed hose with the opening of equipment for filling a motor vehicle tank
EP0804964A3 (de) Feinmahlanlage mit Hochleistungsabscheider
USD978768S1 (en) Aircraft airframe
EP2352674B1 (de) Flugzeugmotor mit starrem modularem aufbau für einen montagemast

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB GR IE IT LI LU MC NL PT SE

17P Request for examination filed

Effective date: 19940630

RBV Designated contracting states (corrected)

Designated state(s): AT BE CH DE DK ES FR GB GR IE IT LI NL PT SE

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19951231