Multi-component synthetic closure and method of manufacture

• US 9,314,953 B2
• Filed: 11/14/2008
• Issued: 04/19/2016
• Est. Priority Date: 11/16/2007
• Status: Expired due to Fees

• Current Assignee: Nomacorc, LLC
• Original Assignee: Nomacorc, LLC
• Inventors: Lauer, Edouard, Kirch, Marco Josef Otto
• Primary Examiner(s): Khare, Atul P.
• Application Number:
  US12/291,880
• Publication Number:
  US 20090130350A1
• Time in Patent Office: 2,713 Days
• Field of Search: 264/132, 264/148, 264/448, 264/173.12, 264/173.16, 264/173.18, 264/45.9, 264/135, 264/171.1, 264/171.13
• US Class Current: 1/1
• CPC Class Codes: B29C 2793/0027 Cutting off
• CPC Class Codes: B29C 2795/007 after shaping
• CPC Class Codes: B29C 48/0022 combined with cutting
• CPC Class Codes: B29C 48/0023 combined with printing or marking
• CPC Class Codes: B29C 48/06 Rod-shaped
• CPC Class Codes: B29C 48/154 Coating solid articles, i.e. non-hollow articles
• CPC Class Codes: B29C 48/304 specially adapted for bringing together components, e.g. melts within the die
• CPC Class Codes: B29D 99/0096 Producing closure members for containers, e.g. closure caps or stoppers
• CPC Class Codes: B29L 2031/565 for containers
• CPC Class Codes: B65D 2203/00 Decoration means, markings, information elements, contents indicators
• CPC Class Codes: B65D 39/0058 from natural or synthetic cork, e.g. for wine bottles or the like
• CPC Class Codes: Y10T 428/13 Hollow or container type article [e.g., tube, vase, etc.]

Abstract

In the present invention, a manufacturing process is provided in which a complete multi-component synthetic closure is achieved which incorporates printed indicia formed thereon, in a continuous, in-line manufacturing operation. In the preferred embodiment of the present invention, the core member of the synthetic closure is formed by a continuous extrusion process which enables the core to be manufactured as an elongated, continuous length of material. As the continuous elongated length of extruded material forming the central core is advanced from the extruder towards an outer skin forming station, the central core passes through a printing station for forming any desired indicia on the outer surface of the central core prior to the application of the outer skin layer.

Claims

1. A method for mass-producing a plurality of multi-component thermoplastic closures for use in sealing fluid products in a container having a portal forming a neck of the container, said method comprising the steps of:

A. extruding a continuous, elongated, substantially cylindrically shaped length of material to form a central core member, said central core member comprising a continuous elongated form with a continuous length equivalent to a combined length of the plurality of multi-component thermoplastic closures, and said central core member being devoid of a skin layer or covering layer;

B. passing the central core member being devoid of a skin layer or covering layer through a printer system that repeatedly prints pre-determined, desired ink-based indicia directly on an outer cylindrical surface of said central core member;

C. separately extruding a visually transparent, separate and independent layer of plastic material in intimate bonded engagement with the central core member, said separate and independent layer of plastic material consisting of a single layer of material, peripherally surrounding and substantially enveloping the outer cylindrical surface of the central core member and being in overlying relationship with the indicia repeatedly printed on the outer cylindrical surface of said central core member, thereby forming a dual component product; and

D. repeatedly cutting the dual component product in a plane substantially perpendicular to a central axis of the central core member, thereby forming the plurality of multi-component thermoplastic closures, with each multi-component thermoplastic closure having a desired length for insertion and retention in the portal of the neck of the container, and with each multi-component thermoplastic closure having a core with the desired indicia contained thereon and visible through the separate and independent layer of plastic material.

2. The method defined in claim 1, wherein the central core member is further defined as comprising medium density or low density, closed cell plastic material comprising at least one material selected from the group consisting of inert polymers, homopolymers, and copolymers.

3. The method defined in claim 2, wherein said closed cell plastic material is further defined and as comprising closed cell foam plastic comprising at least one material selected from the group consisting of polyethylenes, metallocene catalyst polyethylenes, polybutanes, polybutylenes, polyurethanes, silicones, vinyl-based resins, thermoplastic elastomers, polyesters, ethylenic acrylic copolymers, ethylene-vinyl-acetate copolymers, ethylene-methyl-acrylate copolymers, ethylene-butyl-acrylate copolymers, ethylene-propylene-rubber, styrene butadiene rubber, ethylene-ethyl-acrylic copolymers, ionomers, polypropylenes, and copolymers of polypropylene and copolymerizable ethylenically unsaturated commoners.

4. The method defined in claim 3, wherein said separate and independent layer of plastic material is further defined as comprising at least one material selected from the group consisting of polyethylenes, metallocene catalyst polyethylenes, polybutanes, polybutylenes, polyurethanes, silicones, vinyl-based resins, thermoplastic elastomers, polyesters, ethylenic acrylic copolymers, ethylene-vinyl-acetate copolymers, ethylene-methyl-acrylate copolymers, ethylene-butyl-acrylate copolymers, ethylene-propylene-rubber, styrene butadiene rubber, ethylene-ethyl-acrylic copolymers, ionomers, polypropylenes, and copolymers of polypropylene and copolymerizable ethylenically unsaturated commoners.

5. The method defined in claim 1, wherein the step of extruding the separate and independent layer of plastic material in intimate bonded engagement with the central core member is further defined as being performed using cross-head extrusion equipment.

6. The method defined in claim 1, wherein the printer system is further defined as comprising one item selected from the group consisting of printing equipment constructed for providing one or more methods selected from the group consisting of printing, marking, labeling, decorating, laser marking, hot stamping, inkjet printing, hot melt inkjet printing, engraving, offset printing, dry offset printing, direct gravure printing, and tampon printing.

7. The method defined in claim 1, wherein the indicia printed on the outer cylindrical surface of the central core member is further defined as comprising at least one item selected from the group consisting of graphics, symbols, codes, numbers, designations, data matrix codes, linear barcodes, generic printed patterns, custom printed patterns, traceability numbers, labels, generic artwork, specific artwork, invisible marks, covert marks, and the like.

8. The method defined in claim 1, wherein the method further comprises the step of pretreating the outer cylindrical surface of the central core member prior to passage of the central core member through the printer system.

9. The method defined in claim 8, wherein said pretreatment is further defined as comprising at least one item selected from the group consisting of corona treatment, flame treatment, plasma treatment, UV light exposure, and infrared heat exposure.

10. The method defined in claim 1, wherein the method comprises the additional step of providing continuous movement of the central core member through the steps A-D.

11. The method defined in claim 10, wherein said continuous movement is provided by passing the central core member through a puller assembly.

12. The method defined in claim 1, wherein the printer system comprises an inkjet printer system.

13. The method defined in claim 12, wherein the inkjet printer system utilizes a UV curable inkjet ink.

14. The method defined in claim 1, wherein the method further comprises the step of curing the printed indicia after passage of the central core member through the printer system.

15. The method defined in claim 1, wherein the method further comprises the step of post treating the outer cylindrical surface of the central core member after passage of the central core member through the printer system.

16. The method defined in claim 1, wherein the method further comprises the step of printing additional pre-determined, desired indicia on a surface of said separate and independent layer of plastic material.

17. The method defined in claim 1, wherein said separate and independent layer of plastic material is further defined as comprising a lubricant in order to impart a lubrication function into said layer.

18. The method defined in claim 17, wherein said lubricant is selected from the group consisting of mineral oils, silicone oils, and lubricant polymers.

19. The method defined in claim 1, wherein the indicia are repeatedly printed in side to side spaced intervals directly on said central core member.

20. The method defined in claim 1, wherein the printer system comprises a laser printing system.

21. A method for mass-producing a plurality of multi-component thermoplastic closures for use in sealing fluid products in a container having a portal forming a neck of the container, said method comprising the steps of:

A. extruding a continuous, elongated, substantially cylindrically shaped length of material to form a central core member, said central core member comprising a continuous elongated form with a continuous length equivalent to a combined length of the plurality of multi-component thermoplastic closures, and said central core member being devoid of a skin layer or covering layer;

B. passing the central core member being devoid of a skin layer or covering layer through a printer system that repeatedly prints pre-determined, desired ink-based indicia directly on an outer cylindrical surface of said central core member;

C. separately extruding a visually transparent, separate and independent layer of plastic material in intimate bonded engagement with the central core member, peripherally surrounding and substantially enveloping the outer cylindrical surface of the central core member and being in overlying relationship with the indicia repeatedly printed on the outer cylindrical surface of said central core member, thereby forming a dual component product; and

D. repeatedly cutting the dual component product in a plane substantially perpendicular to a central axis of the central core member, thereby forming the plurality of multi-component thermoplastic closures, with each multi-component thermoplastic closure having a desired length for insertion and retention in the portal of the neck of the container, and with each multi-component thermoplastic closure having a core with the desired indicia contained thereon and visible through the separate and independent layer of plastic material,

wherein said manufacturing process operates as a continuous formation process with all steps being performed in-line, with virtually no manual intervention and with a fully produced final product being achieved.

22. The method defined in claim 21, wherein the printer system comprises a laser printing system.

23. The method defined in claim 21, wherein the indicia are repeatedly printed in side to side spaced intervals directly on said central core member.