EP1750922A1 - Preform assembly, container assembly, and method of manufacture - Google Patents

Preform assembly, container assembly, and method of manufacture

Info

Publication number
EP1750922A1
EP1750922A1 EP20050731258 EP05731258A EP1750922A1 EP 1750922 A1 EP1750922 A1 EP 1750922A1 EP 20050731258 EP20050731258 EP 20050731258 EP 05731258 A EP05731258 A EP 05731258A EP 1750922 A1 EP1750922 A1 EP 1750922A1
Authority
EP
European Patent Office
Prior art keywords
preform
finish ring
assembly
container
finish
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Withdrawn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
EP20050731258
Other languages
German (de)
French (fr)
Inventor
Keith J. Barker
Bassam M. Kalmouni
Brian A. Lynch
Nikhil Mani
Thomas E. Nahill
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.)
Graham Packaging Pet Technologies Inc
Original Assignee
Graham Packaging Pet Technologies Inc
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
Application filed by Graham Packaging Pet Technologies Inc filed Critical Graham Packaging Pet Technologies Inc
Publication of EP1750922A1 publication Critical patent/EP1750922A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/071Preforms or parisons characterised by their configuration, e.g. geometry, dimensions or physical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/06Making preforms by moulding the material
    • B29B11/12Compression moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • 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
    • B65D1/00Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
    • B65D1/02Bottles or similar containers with necks or like restricted apertures, designed for pouring contents
    • B65D1/0223Bottles or similar containers with necks or like restricted apertures, designed for pouring contents characterised by shape
    • B65D1/023Neck construction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/06Making preforms by moulding the material
    • B29B11/08Injection moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/0715Preforms or parisons characterised by their configuration the preform having one end closed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/072Preforms or parisons characterised by their configuration having variable wall thickness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/072Preforms or parisons characterised by their configuration having variable wall thickness
    • B29C2949/0722Preforms or parisons characterised by their configuration having variable wall thickness at neck portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/073Preforms or parisons characterised by their configuration having variable diameter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/073Preforms or parisons characterised by their configuration having variable diameter
    • B29C2949/0731Preforms or parisons characterised by their configuration having variable diameter at neck portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/073Preforms or parisons characterised by their configuration having variable diameter
    • B29C2949/0733Preforms or parisons characterised by their configuration having variable diameter at body portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/076Preforms or parisons characterised by their configuration characterised by the shape
    • B29C2949/0768Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform
    • B29C2949/077Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform characterised by the neck
    • B29C2949/0772Closure retaining means
    • B29C2949/0773Threads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/076Preforms or parisons characterised by their configuration characterised by the shape
    • B29C2949/0768Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform
    • B29C2949/077Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform characterised by the neck
    • B29C2949/0777Tamper-evident band retaining ring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/079Auxiliary parts or inserts
    • B29C2949/08Preforms made of several individual parts, e.g. by welding or gluing parts together
    • B29C2949/0801Finish neck ring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/22Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at neck portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/24Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at flange portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/26Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at body portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/28Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at bottom portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3008Preforms or parisons made of several components at neck portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3008Preforms or parisons made of several components at neck portion
    • B29C2949/3009Preforms or parisons made of several components at neck portion partially
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3012Preforms or parisons made of several components at flange portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3016Preforms or parisons made of several components at body portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/302Preforms or parisons made of several components at bottom portion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3024Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
    • B29C2949/3026Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3024Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
    • B29C2949/3026Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components
    • B29C2949/3028Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3024Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
    • B29C2949/3026Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components
    • B29C2949/3028Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components
    • B29C2949/303Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components having more than three components
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3032Preforms or parisons made of several components having components being injected
    • B29C2949/3034Preforms or parisons made of several components having components being injected having two or more components being injected
    • B29C2949/3036Preforms or parisons made of several components having components being injected having two or more components being injected having three or more components being injected
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3032Preforms or parisons made of several components having components being injected
    • B29C2949/3034Preforms or parisons made of several components having components being injected having two or more components being injected
    • B29C2949/3036Preforms or parisons made of several components having components being injected having two or more components being injected having three or more components being injected
    • B29C2949/3038Preforms or parisons made of several components having components being injected having two or more components being injected having three or more components being injected having more than three components being injected
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3056Preforms or parisons made of several components having components being compression moulded
    • B29C2949/3058Preforms or parisons made of several components having components being compression moulded having two or more components being compression moulded
    • B29C2949/306Preforms or parisons made of several components having components being compression moulded having two or more components being compression moulded having three or more components being compression moulded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3056Preforms or parisons made of several components having components being compression moulded
    • B29C2949/3058Preforms or parisons made of several components having components being compression moulded having two or more components being compression moulded
    • B29C2949/306Preforms or parisons made of several components having components being compression moulded having two or more components being compression moulded having three or more components being compression moulded
    • B29C2949/3062Preforms or parisons made of several components having components being compression moulded having two or more components being compression moulded having three or more components being compression moulded having more than three components being compression moulded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/18Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/06PE, i.e. polyethylene
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/08Copolymers of ethylene
    • B29K2023/086EVOH, i.e. ethylene vinyl alcohol copolymer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/10Polymers of propylene
    • B29K2023/12PP, i.e. polypropylene
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2067/00Use of polyesters or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2001/00Articles provided with screw threads
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352Polymer or resin containing [i.e., natural or synthetic]
    • Y10T428/1397Single layer [continuous layer]

Definitions

  • the present invention is directed to preform assemblies for blow molding plastic container assemblies, to plastic container assemblies blow molded from such preform assemblies, and to methods of making such preform assemblies and container assemblies.
  • Background of the Invention hi the manufacture of plastic containers, it is conventional to injection mold or compression mold a container preform -having a body and a neck finish with one or more external threads or other closure attachment means.
  • the preform neck finish typically is molded to its final geometry, while the body of the preform subsequently is blow molded to the desired geometry of the container body.
  • the preform may be of monolayer construction, or may be of multilayer construction in which one or more intermediate layers in the preform body may or may not extend into the neck finish of the preform.
  • Patents 4,609,516, 4,710,118 and 4,954,376 illustrate injection molding of multilayer container preforms.
  • Molding the neck finish portion of a container as part of the container preform presents a number of problems.
  • the plastic material typically is inj ected into a mold cavity at the closed end of the preform body, so that the material must flow along the sides of the preform mold cavity into the area in which the neck finish is molded.
  • the neck finish typically requires more accurate and stable dimensioning than the body of the preform, which can limit the cycle time of the preform molding process.
  • the neck finish of the preform is of the same material as a monolayer preform body, and of the same material as at least the outer layers of a multilayer preform b ody, which limits the ability to obtain the most desirable material characteristics at the neck finish.
  • the preform is of polyester construction, such as polyethylene terephthalate (PET)
  • PET polyethylene terephthalate
  • the neck finish of the preform can be wholly or partially crystallized to improve the operating characteristics of the neck finish area, particularly in hot-fill container applications.
  • the requirement that the neck finish be of the same material as at least the outer layers of a multilayer preform body still limits the design capabilities of preform manufacture.
  • a method of making a preform assembly in accordance with one aspect of the present invention includes providing a plastic finish ring on a core pin of a compression mold, and compression molding a plastic preform onto the finish ring in the mold.
  • a preform assembly for blow molding a container assembly which includes a molded plastic finish ring and a plastic preform compression molded to the finish ring such that a neck portion of the plastic preform radially interengages the finish ring.
  • FIG. 1 illustrates a side elevational view of a. preform assembly according to one exemplary embodiment of the present invention
  • FIG. 2 illustrates a side elevational view of a container assembly, blow-molded from the preform assembly of FIG.
  • FIG. 3 illustrates a side elevational view of a finish ring for the preform and container assemblies of FIGS. 1 and 2;
  • FIG. 4 illustrates a top view of the finish rirxg of FIG. 3;
  • FIG. 5 illustrates a cross-sectional view of t_he finish ring of FIG. 3, taken along line 5-5;
  • FIG. 6A illustrates a compression molding apparatus for use in accordance with an exemplary method of the present invention, wherein the app aratus is shown in an open position in which a charge of preform material is located within a mold cavity and a pre- made finish ring is loaded to a core pin;
  • FIG. 6B illustrates the compression molding apparatus of FIG.
  • FIG. 1 illustrates a preform assembly 20 in accordance with one presently preferred embodiment of the invention as comprising a preform 22 and a separate finish ring 24 secured thereover.
  • the preform 22 may be injection molded, but is preferably produced by compression molding as will be discussed in greater detail below.
  • the preform 22 is composed of any suitable plastic material such as monolayer polyethylene terephthalate (PET) or the like, or multilayer PET or the like in which matrix layers of PET, for example, are alternated with one or more layers of a barrier resin material such as ethylene vinyl alcohol (EVOH), nylon or the like.
  • the finish ring 24 is injection or compression molded or the like, and is composed of any desired material such as PET, post consumer resin (PCR), process regrind (REG), polypropylene (PP), polyethylene (PE), polyethylene napthalate (PEN), or the like.
  • FIG. 2 illustrates a container assembly 120 that is blow molded from the preform assembly 20 of FIG. 1 in accordance with another presently preferred embodiment of the present invention, and includes the finish ring 24 secured to a container 122 in a manner that is in all significant respects identical to that of the preform assembly 20 from which the container assembly 120 is blow-molded. Accordingly, such securement details will not be repeated for this embodiment.
  • FIG. 2 illustrates a container assembly 120 that is blow molded from the preform assembly 20 of FIG. 1 in accordance with another presently preferred embodiment of the present invention, and includes the finish ring 24 secured to a container 122 in a manner that is in all significant respects identical to that of the preform assembly 20 from which the container assembly 120 is blow-molded. Accordingly, such securement details will not be repeated for this embodiment.
  • FIG. 1 illustrates a container assembly 120 that is blow molded from the preform assembly 20 of FIG. 1 in accordance with another presently preferred embodiment of the present invention, and includes the finish ring 24 secured to a container
  • the preform 22 includes a closed lower end 26 and e-xtends upwardly therefrom in the form of a body 28 that terminates in a cylindrical neck 30 that is integrally molded with the body 26.
  • Directional words such as “upper” and “lower” are employed by way of description and not limitation with respect to the upright orientation of the preform assemblies and components illustrated in the dra ⁇ wings.
  • Directional words such as “radial” and “circumferential” are employed by way of description and not limitation with respect to the axis of the preform neck or finish -ring as appropriate.
  • the finish ring 24 is circumfer&ntially continuous and includes an annular cylindrical wall 32 having one or more external threads or thread segments 34.
  • a circumferential bead 36 extends around the outer surface of the wall 32 beneath the threads 34 for cooperating with a tamper-indicating mechanism on a closure (not shown) to be secured to the finish portion of the final container.
  • a capping or support fla ⁇ nge 38 extends radially outwardly from the lower end of the wall 32, giving the finish ring 24 a generally L-shaped lateral cross section in the illustrated embodiments of the invention.
  • the finish ring 24 includes a cylindrical internal surface 40 and a tapered internal surface 42 extending between top and bottom ends 44, 46.
  • A-_nnular grooves 48 are provided in the tapered internal surface 42, as will be further described in reference to FIGS.
  • FIGS. 6A-8 there is illustrated a compression molding apparatus 50 for use in accordance with an exemplary method of the present invention.
  • the apparatus 50 includes a core pin 52 positioned above a compression mold 54.
  • the compression mold 54 includes a closed bottom end. 56, a body portion 58, and a partial finish portion 60 that together define a mold cavity 6-2.
  • the apparatus 50 occupies an open position in FIG. 6A, in which a charge of preform -material 64 is introduced into the compression mold cavity 62 and the pre-made finish rin.g 24 is placed on to the compression core pin 52, as shown.
  • the charge 64 is soft or molten, and thereby conforms to and fills the lower end of the mold cavity 62.
  • the core pin 52, with the finish ring 24 mounted thereto, and the mold 54 are positioned in vertical alignment. [0011] As shown in FIG. 6B, the core pin 52 and finish ring 24 are then moved into the mold 54 to compression overmold the charge 64 partially witb-in the finish ring 24.
  • the term "overmold” is a term of art and, as used herein, means to mold one component from a soft or molten state to another component in a solid or finished state.
  • the molten preform material charge 64 flows in an upward or forward direction between the core pin 52 and mold 54.
  • the preform 22 is formed including the closed bottom end 26, the body 28 and the neck 30. More significantly, however, the preform assembly 20 is formed from the overmolding of the preform 22 to t ie finish ring 24. Thereafter, and as shown in FIG. 7, the core pin 52 is retracted with the preform assembly 20, including the preform 22 and finish ring 24, mounted thereto. [0012] As shown in FIG. 8, the preform assembly 20 includes the preform 22 compression molded partially within a portion of the finish ring 24.
  • the neck 30 of the preform 22 includes an upper portion 66 having annular projections 68 that extend into the annular grooves 48 of the finish ring 24 so as to positively radially interlock or interengage the finish ring 24 to the preform 22.
  • the annular grooves 48 in the finish ring 24 can also be referred to as radial recesses or radial interengagement features.
  • the radial interengagement between the preform 22 and finish, ring 24 provides positive resistance to any axially applied force tending to separate the components 22, 24.
  • the preform 22 also includes a tapered or conical external surface 70 tlxat corresponds to the tapered or conical internal surface 42 of the finish ring 24.
  • the tapered internal surface 42 of the finish ring 24 is greater in diameter than the corresponding portion of the core pin 52. Accordingly, a small gap 72 is provided between the cozre pin 52, tapered internal surface 42 of the finish ring 24, and a leading edge 74 of the preform 22.
  • the gap 72 is provided between a trarLsition point 76 of the finish ring 24 and the forward edge 74 of the preform 22, wherein the transition point 76 is defined by the intersection of the cylindrical or straight internal surface 40 and the tapered internal surface 42.
  • the gap 72 is intentionally provided to accommodate within- tolerance variation of the size, volume or weight of the molten preform charge.
  • gap 72 should always be present under ma-ximum material conditions of both the preform 22 and the finish ring 24, to ensxire a proper fit therebetween without any distortion due to overpacking of the preform material into the finish ring 24.
  • overpack is a term of art and, as used herein, refers to a condition where an excessive amount of molten polymer is compression molded s nd tends to lead to difficulties in ejecting the finished formed part or parts from the compression molding apparatus. Overpacking also tends to lead to warpage of, a id residual stress within, the finished part or parts.
  • the present invention facilitates producti on of preform assemblies and container assemblies wherein a finish ring is composed o_f a material different from that of a preform or container to which the finish ring is radially interengaged.
  • the present invention facilitates application of finish rings of various sizes and/or materials, to a common size preform and/or container.
  • the present invention enables a decrease in the cycle time required to produce a preform because the constraint of the process - forming the neck finish portion - can " be subordinated to a separate, parallel production process for producing just finish rings.
  • the present invention enables a reduction in the piece price of ea_ch preform because the mold tooling can be simplified, and reduced in cost, to omit the complex thread split features typically required for the threaded finish portion of the preform.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Manufacturing & Machinery (AREA)
  • Ceramic Engineering (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)

Abstract

A method of making a preform assembly (20) including providing a finish ring (24) of plastic construction, placing the finish ring onto a core pin (52), introducing a preform polymer (64)into a mold cavity that includes the core pin, and compression molding the preform polymer (64) to the finish ring. A resulting preform assembly, and container assembly blow-molded from the preform assembly, are also disclosed.

Description

PREFORM ASSEMBLY, CONTAINER ASSEMBLY, AND METHOD OF MANUFACTURE
Technical Field [001 ] The present invention is directed to preform assemblies for blow molding plastic container assemblies, to plastic container assemblies blow molded from such preform assemblies, and to methods of making such preform assemblies and container assemblies. Background of the Invention [002] hi the manufacture of plastic containers, it is conventional to injection mold or compression mold a container preform -having a body and a neck finish with one or more external threads or other closure attachment means. The preform neck finish typically is molded to its final geometry, while the body of the preform subsequently is blow molded to the desired geometry of the container body. The preform may be of monolayer construction, or may be of multilayer construction in which one or more intermediate layers in the preform body may or may not extend into the neck finish of the preform. U.S. Patents 4,609,516, 4,710,118 and 4,954,376 illustrate injection molding of multilayer container preforms. [003] Molding the neck finish portion of a container as part of the container preform presents a number of problems. For example, when the preforms are formed by inj ection molding, the plastic material typically is inj ected into a mold cavity at the closed end of the preform body, so that the material must flow along the sides of the preform mold cavity into the area in which the neck finish is molded. The neck finish typically requires more accurate and stable dimensioning than the body of the preform, which can limit the cycle time of the preform molding process. Furthermore, the neck finish of the preform is of the same material as a monolayer preform body, and of the same material as at least the outer layers of a multilayer preform b ody, which limits the ability to obtain the most desirable material characteristics at the neck finish. When the preform is of polyester construction, such as polyethylene terephthalate (PET), the neck finish of the preform can be wholly or partially crystallized to improve the operating characteristics of the neck finish area, particularly in hot-fill container applications. However, the requirement that the neck finish be of the same material as at least the outer layers of a multilayer preform body still limits the design capabilities of preform manufacture. Summary of the Invention [004] A method of making a preform assembly in accordance with one aspect of the present invention includes providing a plastic finish ring on a core pin of a compression mold, and compression molding a plastic preform onto the finish ring in the mold. [005] In accordance with a second aspect of the present invention, there is provided a preform assembly for blow molding a container assembly, which includes a molded plastic finish ring and a plastic preform compression molded to the finish ring such that a neck portion of the plastic preform radially interengages the finish ring. [006] In accordance with a third aspect o_f the invention, there is provided a container assembly blow molded from a preform assembly which is produced from compression molding a preform to a molded plastic finish ring. The container assembly includes the molded plastic finish ring, and a plastic container having a neck portion thereof radially interengaging said finish ring. Brief Description of the Drawings The invention, together with additional objects, features, advantages and aspects thereof, will be best understood from the following description, the appended claims and the accompanying drawings, in which: FIG. 1 illustrates a side elevational view of a. preform assembly according to one exemplary embodiment of the present invention; FIG. 2 illustrates a side elevational view of a container assembly, blow-molded from the preform assembly of FIG. 1 , according to another exemplary embodiment of the present invention; FIG. 3 illustrates a side elevational view of a finish ring for the preform and container assemblies of FIGS. 1 and 2; FIG. 4 illustrates a top view of the finish rirxg of FIG. 3; FIG. 5 illustrates a cross-sectional view of t_he finish ring of FIG. 3, taken along line 5-5; FIG. 6A illustrates a compression molding apparatus for use in accordance with an exemplary method of the present invention, wherein the app aratus is shown in an open position in which a charge of preform material is located within a mold cavity and a pre- made finish ring is loaded to a core pin; FIG. 6B illustrates the compression molding apparatus of FIG. 6A wherein the apparatus is shown in a closed position in which the preform, material is compression molded within a portion of the pre-made finish ring; FIG. 7 illustrates a fragmentary cross-sectional view of a portion of the compression molding apparatus of FIGS. 6 A and 6B and a cross-sectional view of the resulting preform assembly, wherein the preform assembly has been retracted and is carried on the compression core pin; and FIG. 8 illustrates an enlarged cross-sectional view of the preform assembly of FIG. 7, taken from circle 8 thereof. Detailed Description [007] FIG. 1 illustrates a preform assembly 20 in accordance with one presently preferred embodiment of the invention as comprising a preform 22 and a separate finish ring 24 secured thereover. The preform 22 may be injection molded, but is preferably produced by compression molding as will be discussed in greater detail below. The preform 22 is composed of any suitable plastic material such as monolayer polyethylene terephthalate (PET) or the like, or multilayer PET or the like in which matrix layers of PET, for example, are alternated with one or more layers of a barrier resin material such as ethylene vinyl alcohol (EVOH), nylon or the like. The finish ring 24 is injection or compression molded or the like, and is composed of any desired material such as PET, post consumer resin (PCR), process regrind (REG), polypropylene (PP), polyethylene (PE), polyethylene napthalate (PEN), or the like. Preferably, however, the finish ring 24 is composed of a material different than that of the preform 22, such as amorphous PET for preform 2 and crystalized PET for finish ring 24. [008] FIG. 2 illustrates a container assembly 120 that is blow molded from the preform assembly 20 of FIG. 1 in accordance with another presently preferred embodiment of the present invention, and includes the finish ring 24 secured to a container 122 in a manner that is in all significant respects identical to that of the preform assembly 20 from which the container assembly 120 is blow-molded. Accordingly, such securement details will not be repeated for this embodiment. [009] In FIG. 1, the preform 22 includes a closed lower end 26 and e-xtends upwardly therefrom in the form of a body 28 that terminates in a cylindrical neck 30 that is integrally molded with the body 26. (Directional words such as "upper" and "lower" are employed by way of description and not limitation with respect to the upright orientation of the preform assemblies and components illustrated in the dra~wings. Directional words such as "radial" and "circumferential" are employed by way of description and not limitation with respect to the axis of the preform neck or finish -ring as appropriate.) As also shown in FIGS. 3-5, the finish ring 24 is circumfer&ntially continuous and includes an annular cylindrical wall 32 having one or more external threads or thread segments 34. hi the preferred embodiment illustrated in the dra rings, a circumferential bead 36 extends around the outer surface of the wall 32 beneath the threads 34 for cooperating with a tamper-indicating mechanism on a closure (not shown) to be secured to the finish portion of the final container. A capping or support flaαnge 38 extends radially outwardly from the lower end of the wall 32, giving the finish ring 24 a generally L-shaped lateral cross section in the illustrated embodiments of the invention. As best shown in FIG. 5, the finish ring 24 includes a cylindrical internal surface 40 and a tapered internal surface 42 extending between top and bottom ends 44, 46. A-_nnular grooves 48 are provided in the tapered internal surface 42, as will be further described in reference to FIGS. 6A-8 below. [0010] Referring now in general to FIGS. 6A-8, there is illustrated a compression molding apparatus 50 for use in accordance with an exemplary method of the present invention. In FIG. 6A, the apparatus 50 includes a core pin 52 positioned above a compression mold 54. The compression mold 54 includes a closed bottom end. 56, a body portion 58, and a partial finish portion 60 that together define a mold cavity 6-2. The apparatus 50 occupies an open position in FIG. 6A, in which a charge of preform -material 64 is introduced into the compression mold cavity 62 and the pre-made finish rin.g 24 is placed on to the compression core pin 52, as shown. The charge 64 is soft or molten, and thereby conforms to and fills the lower end of the mold cavity 62. The core pin 52, with the finish ring 24 mounted thereto, and the mold 54 are positioned in vertical alignment. [0011] As shown in FIG. 6B, the core pin 52 and finish ring 24 are then moved into the mold 54 to compression overmold the charge 64 partially witb-in the finish ring 24. The term "overmold" is a term of art and, as used herein, means to mold one component from a soft or molten state to another component in a solid or finished state. The molten preform material charge 64 flows in an upward or forward direction between the core pin 52 and mold 54. As a result, the preform 22 is formed including the closed bottom end 26, the body 28 and the neck 30. More significantly, however, the preform assembly 20 is formed from the overmolding of the preform 22 to t ie finish ring 24. Thereafter, and as shown in FIG. 7, the core pin 52 is retracted with the preform assembly 20, including the preform 22 and finish ring 24, mounted thereto. [0012] As shown in FIG. 8, the preform assembly 20 includes the preform 22 compression molded partially within a portion of the finish ring 24. I ore specifically, the neck 30 of the preform 22 includes an upper portion 66 having annular projections 68 that extend into the annular grooves 48 of the finish ring 24 so as to positively radially interlock or interengage the finish ring 24 to the preform 22. The annular grooves 48 in the finish ring 24 can also be referred to as radial recesses or radial interengagement features. The radial interengagement between the preform 22 and finish, ring 24 provides positive resistance to any axially applied force tending to separate the components 22, 24. The preform 22 also includes a tapered or conical external surface 70 tlxat corresponds to the tapered or conical internal surface 42 of the finish ring 24. The tapered internal surface 42 of the finish ring 24 is greater in diameter than the corresponding portion of the core pin 52. Accordingly, a small gap 72 is provided between the cozre pin 52, tapered internal surface 42 of the finish ring 24, and a leading edge 74 of the preform 22. In terms of the preform assembly 20, the gap 72 is provided between a trarLsition point 76 of the finish ring 24 and the forward edge 74 of the preform 22, wherein the transition point 76 is defined by the intersection of the cylindrical or straight internal surface 40 and the tapered internal surface 42. The gap 72 is intentionally provided to accommodate within- tolerance variation of the size, volume or weight of the molten preform charge. In other words, at least some gap 72 should always be present under ma-ximum material conditions of both the preform 22 and the finish ring 24, to ensxire a proper fit therebetween without any distortion due to overpacking of the preform material into the finish ring 24. The term "overpack" is a term of art and, as used herein, refers to a condition where an excessive amount of molten polymer is compression molded s nd tends to lead to difficulties in ejecting the finished formed part or parts from the compression molding apparatus. Overpacking also tends to lead to warpage of, a id residual stress within, the finished part or parts. [0013] With one or more of the embodiments described above, the present invention provides a number of advantages. The present invention facilitates producti on of preform assemblies and container assemblies wherein a finish ring is composed o_f a material different from that of a preform or container to which the finish ring is radially interengaged. Likewise, the present invention facilitates application of finish rings of various sizes and/or materials, to a common size preform and/or container. Moreover, the present invention enables a decrease in the cycle time required to produce a preform because the constraint of the process - forming the neck finish portion - can "be subordinated to a separate, parallel production process for producing just finish rings. In the same vein, the present invention enables a reduction in the piece price of ea_ch preform because the mold tooling can be simplified, and reduced in cost, to omit the complex thread split features typically required for the threaded finish portion of the preform. [0014] There have thus been described preform assemblies for blow moldi-ng plastic container assemblies, plastic container assemblies blow molded from su-ch preform assemblies, and methods of making such preform assemblies and container assemblies. The present invention has been disclosed in conjunction with presently preferred embodiments thereof, and a number of modifications and variations have be en discussed. Other modifications and variations will readily suggest themselves to persons of ordinary skill in the art in view of the foregoing description. Indeed, the invention- is intended to embrace all modifications and variations as fall within the scope of t e appended claims.

Claims

Claims
1. A method of making a preform assembly comprising: providing a plastic finish ring on a core pin of a compression mold; and compression molding a plastic preform onto the finish ring in the mold.
2. The method of claim 1, wherein the method includes providing a charge of preform material in the mold, and wherein at least a portion of the preform material flows betv een the finish ring and core pin during the compression molding step.
3. The method of claim 2, wherein the finish ring includes an interengagement feature, and wherein at least a portion of the preform material flows into the interengagerrxent feature during the compression molding step.
4. The method of claim 1, wherein the finish ring has an internal engagement surface greater in diameter than the core pin, and wherein at least a portion of the molded preform is formed between the engagement surface and the core pin.
5. The method of claim 1, wherein a gap is provided between an internal engagem_ent surface of the finish ring and the core pin, and wherein the gap is not completely fiLled during the compression molding step.
6. The method of claim 1, wherein a charge of preform material is provided in the mold, and the core pin and finish ring are moved into the mold allowing the preform material to flow into engagement with an internal surface of the finish ring.
7. The prefonn assembly produced by the method of claim 1, comprising the preform and finish ring.
8. A method of making a container assembly, including blow molding the preform of claim 1 to form a container.
9. A container assembly produced by the method of claim 8, comprising the container and finish ring.
10. A preform assembly for blow molding a container assembly, which includes: a molded plastic finish ring, and a plastic preform which is compression molded to the finish ring such that a neck portion of the plastic preform radially interengages the finish ring.
11. The preform assembly of claim 10, wherein the finish ring has at least one radial interengagement feature formed therein, and wherein the neck portion of the plastic preform engages with the at least one radial interengagement feature.
12. The preform assembly of claim 10, wherein the finish ring includes an internal surface having a lower tapered surface, an upper straight surface, and a transition point therebetween, and wherein an open gap exists between the transition point and. a forward edge of the neck portion of the plastic preform.
13. A container assembly comprising: a molded plastic finish ring, and a plastic container blow-molded from a preform assembly, the preform assembly including a preform having a neck portion compression molded to the finish ring.
14. The container assembly of claim 13, wherein the finish ring has at least one internal radial interengagement feature, and wherein the neck portion of the plastic container engages with the at least one radial interengagement feature.
15. The container assembly of claim 14, wherein the finish ring includes an internal surface having a lower tapered surface, an upper straight surface, and a transition point therebetween, and wherein an open gap exists between the transition point and a forward edge of the neck portion of the plastic container.
EP20050731258 2004-04-01 2005-03-31 Preform assembly, container assembly, and method of manufacture Withdrawn EP1750922A1 (en)

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US10/816,500 US20050218103A1 (en) 2004-04-01 2004-04-01 Preform assembly, container assembly, and method of manufacture
PCT/US2005/010614 WO2005097453A1 (en) 2004-04-01 2005-03-31 Preform assembly, container assembly, and method of manufacture

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