Method and apparatus for releasing additional ingredients in a pressurized container

• US 4,518,103 A
• Filed: 09/09/1981
• Issued: 05/21/1985
• Est. Priority Date: 09/09/1981
• Status: Expired due to Fees

• Current Assignee: Aerosol Services Co., Inc. (Kronos Acquisition Holdings, Inc.)
• Original Assignee: Aerosol Services Co., Inc. (Kronos Acquisition Holdings, Inc.)
• Inventors: Lim, Walter K., Krause, Arthur A.
• Primary Examiner(s): Rolla, Joseph J.
• Assistant Examiner(s): HUPPERT, MICHEAL
• Application Number:
  US06/300,506
• Time in Patent Office: 1,350 Days
• Field of Search: 222/399, 222/394, 222/145, 222/1, 222/94, 222/135, 222/136, 222/389, 222/402.1, 222/386.5, 222/129, 222/251, 222/402.24, 222/405, 222/464
• US Class Current: 222/135
• CPC Class Codes: B65D 83/663 at least a portion of the propellant being separated from the product and incrementally released by means of a pressure regulator

Abstract

A method and apparatus are disclosed for delayed release of additional ingredients including additional propellant within a pressurized dispensing container. A reserve container within the primary product container is constructed to open or rupture as a result of a predetermined degree of depressurization of the primary container to release its contents and repressurize the primary container to enable subsequent ejection of product. A catalytic activation system is disclosed as one possible application of this invention.

Claims

1. A dispensing container comprising:

a primary container pressurized by an initial supply of propellant including a first liquified propellant and a gaseous propellant and containing a first substance to be expelled therefrom under pressure;

valve means communicating only with said primary container for dispensing the contents of said primary container; and

a secondary container within said primary container closed against said gaseous propellant and pressurized by a reserve supply of liquified propellant having a characteristic head pressure higher than said first liquified propellant, and containing a second substance to be added to said first substance, said secondary container being constructed to open and release said second substance into said primary container only upon establishment of a predetermined pressure differential between the interior of said primary container and the interior of said secondary container by discharge of said gaseous propellant from said primary container through said valve means.

2. The apparatus of claim 1 wherein said secondary container is a tube of relatively thin material sealed at its two ends, said thin material being selected to rupture at a desired differential between the interior pressure in said secondary container and the pressure within said primary container.

3. The apparatus of claim 1 wherein said secondary container is a vial closed by means of a stopper, said stopper being adapted to be ejected from said vial at a predetermined pressure differential between the interior of said vial and the interior of said primary container.

4. The apparatus of claim 1 wherein one of said first and second substances is a catalyst for activating the other of said substances prior to use.

5. The dispensing container of claim 1 wherein said secondary container is a tube having a closed end and an open end and provided with a stopper adapted to fit into said open end in friction fit engagement with said tube.

6. The dispensing container of claim 1 wherein said secondary container is loosely contained within said primary container.

7. The dispensing container of claim 1 wherein said reserve propellant is soluble in said second substance thereby to expel and disperse said second substance into said primary container upon its release.

8. The dispensing container of claim 1 wherein said reserve propellant is emulsifiable with said second substance thereby to expel said second substance when said secondary container is opened.

9. A method for separately storing ingredients in a pressurized dispensing container such that the ingredients may be admixed by partial depressurization of the container just prior to use, said method comprising the steps of:

introducing a first ingredient in a primary container and a second ingredient in a detached sealable secondary container, said secondary container being constructed to open and release its contents only at a predetermined pressure differential between its internal pressure and the pressure in said primary container;

introducing a reserve supply of liquified propellant into said detached secondary container;

closing said secondary container to seal said second ingredient and said reserve liquified propellant therein and to seal said secondary container against an overpressurizing propellant in said primary container;

introducing said secondary container into said primary container; and

pressurizing said primary container with a first liquified propellant and a second gaseous propellant, said first propellant having a characteristic head space pressure sufficiently lower than said reserve propellant to cause said secondary container to open within said primary container, said second propellant overpressurizing only the primary container to prevent such opening of the secondary container until the second propellant is released from the primary container.

10. The method of claim 9 wherein said first propellant is soluble in said first ingredient and said second propellant is insoluble in said first ingredient.

11. The method of claim 9 further comprising the step of partially depressurizing said primary container to cause said secondary container to open and discharge the second ingredient into the primary container.

12. The method of claim 9 wherein said second propellant is selected from the group comprised of air and nitrogen.

13. The method of claim 9 wherein said first propellant suffices to fully eject said ingredients from said primary container.

14. The method of claim 9 further comprising the step of refrigerating said secondary container prior to its introduction into said primary container to thereby maintain said reserve propellant in a liquid state pending pressurization of the primary container.

15. The method of claim 9 wherein said reserve propellant is soluble or emulsifiable with said second ingredient such that the reserve propellant also expels the second ingredient upon opening of the secondary container.

16. A method for filling a pressurized dispensing container comprising the steps of:

providing a primary container including an open end and a valve assembly attachable to said primary container for sealing said open end;

providing a sealable secondary container dimensioned to fit into said primary container through said open end, said secondary container being constructed to open only at a predetermined differential between its internal and external pressure so as to release its contents including liquids into said primary container;

introducing a liquified propellant into said secondary container;

refrigerating said secondary container to a sufficiently low temperature to keep said propellant in a liquid state at atmospheric pressure;

introducing a second substance into said secondary container;

closing said secondary container such that its contents are sealed therein and said secondary container is sealed against an overpressurizing gaseous propellant in said primary container;

introducing said secondary container into said primary container;

attaching said valve assembly to seal said primary container;

filling said primary container with a product to be dispensed therefrom under pressure; and

pressurizing said primary container with a first liquified propellant and a second gaseous propellant, said liquified propellant having a characteristic head space pressure sufficiently lower than said reserve propellant to cause said secondary container to open within said primary container, said gaseous propellant overpressurizing only said primary container to prevent opening of said secondary container until said primary container is partially depressurized by releasing said second propellant.

17. The method of claim 16 wherein the first propellant is a liquified propellant soluble in the product filling the primary container, and the second propellant is a gaseous propellant insoluble in said product.

18. The method of claim 16 wherein said first propellant suffices to fully eject said product from said primary container.