WO1983002423A1 - A method for the manufacture of packing containers and an arrangement for the realization of the method - Google Patents
A method for the manufacture of packing containers and an arrangement for the realization of the method Download PDFInfo
- Publication number
- WO1983002423A1 WO1983002423A1 PCT/SE1983/000009 SE8300009W WO8302423A1 WO 1983002423 A1 WO1983002423 A1 WO 1983002423A1 SE 8300009 W SE8300009 W SE 8300009W WO 8302423 A1 WO8302423 A1 WO 8302423A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- mandrel
- tube
- accordance
- portions
- laminate
- Prior art date
Links
- 238000012856 packing Methods 0.000 title claims abstract description 38
- 238000000034 method Methods 0.000 title claims abstract description 26
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000005030 aluminium foil Substances 0.000 claims abstract description 37
- 229920000728 polyester Polymers 0.000 claims abstract description 25
- 239000000463 material Substances 0.000 claims description 61
- 239000004033 plastic Substances 0.000 claims description 21
- 229920003023 plastic Polymers 0.000 claims description 21
- 239000007787 solid Substances 0.000 claims description 20
- 238000007789 sealing Methods 0.000 claims description 10
- 238000001125 extrusion Methods 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 3
- 239000002654 heat shrinkable material Substances 0.000 claims description 2
- 229920005644 polyethylene terephthalate glycol copolymer Polymers 0.000 claims 2
- 239000010410 layer Substances 0.000 description 62
- 239000012528 membrane Substances 0.000 description 8
- 235000013405 beer Nutrition 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 3
- 238000005304 joining Methods 0.000 description 3
- 238000004806 packaging method and process Methods 0.000 description 3
- 229920001824 Barex® Polymers 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 239000004372 Polyvinyl alcohol Substances 0.000 description 2
- 238000007664 blowing Methods 0.000 description 2
- 229910001882 dioxygen Inorganic materials 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229920002451 polyvinyl alcohol Polymers 0.000 description 2
- 239000002966 varnish Substances 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 150000001398 aluminium Chemical class 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 235000010210 aluminium Nutrition 0.000 description 1
- 235000013361 beverage Nutrition 0.000 description 1
- VQLYBLABXAHUDN-UHFFFAOYSA-N bis(4-fluorophenyl)-methyl-(1,2,4-triazol-1-ylmethyl)silane;methyl n-(1h-benzimidazol-2-yl)carbamate Chemical compound C1=CC=C2NC(NC(=O)OC)=NC2=C1.C=1C=C(F)C=CC=1[Si](C=1C=CC(F)=CC=1)(C)CN1C=NC=N1 VQLYBLABXAHUDN-UHFFFAOYSA-N 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000005033 polyvinylidene chloride Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D22/00—Producing hollow articles
- B29D22/003—Containers for packaging, storing or transporting, e.g. bottles, jars, cans, barrels, tanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
- B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/02—Thermal shrinking
- B29C61/025—Thermal shrinking for the production of hollow or tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/06—Making preforms having internal stresses, e.g. plastic memory
- B29C61/0608—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms
- B29C61/0616—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms layered or partially layered preforms, e.g. preforms with layers of adhesive or sealing compositions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/481—Non-reactive adhesives, e.g. physically hardening adhesives
- B29C65/4815—Hot melt adhesives, e.g. thermoplastic adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/66—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by liberation of internal stresses, e.g. shrinking of one of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1222—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a lapped joint-segment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1224—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a butt joint-segment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
- B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
- B29C66/2422—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical
- B29C66/24221—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical being circular
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/432—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms
- B29C66/4322—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms by joining a single sheet to itself
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/49—Internally supporting the, e.g. tubular, article during joining
- B29C66/494—Internally supporting the, e.g. tubular, article during joining using an inflatable core
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
- B29C66/5346—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
- B29C66/53461—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
- B29C66/5346—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
- B29C66/53461—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies
- B29C66/53462—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies joining substantially flat covers and substantially flat bottoms to open ends of container bodies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
- B29C66/7232—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a non-plastics layer
- B29C66/72321—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a non-plastics layer consisting of metals or their alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
- B29C66/7234—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a barrier layer
- B29C66/72341—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a barrier layer for gases
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7371—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable
- B29C66/73711—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable oriented
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7371—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable
- B29C66/73711—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable oriented
- B29C66/73713—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable oriented bi-axially or multi-axially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7371—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable
- B29C66/73715—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable heat-shrinkable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
- B29C66/5324—Joining single elements to the wall of tubular articles, hollow articles or bars said single elements being substantially annular, i.e. of finite length
- B29C66/53245—Joining single elements to the wall of tubular articles, hollow articles or bars said single elements being substantially annular, i.e. of finite length said articles being hollow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
- B29C66/542—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles joining hollow covers or hollow bottoms to open ends of container bodies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2067/00—Use of polyesters or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/02—Aluminium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0049—Heat shrinkable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/005—Oriented
- B29K2995/0053—Oriented bi-axially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1007—Running or continuous length work
- Y10T156/1008—Longitudinal bending
- Y10T156/1013—Longitudinal bending and edge-joining of one piece blank to form tube
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1328—Shrinkable or shrunk [e.g., due to heat, solvent, volatile agent, restraint removal, etc.]
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1355—Elemental metal containing [e.g., substrate, foil, film, coating, etc.]
- Y10T428/1359—Three or more layers [continuous layer]
Definitions
- the present invention relates to a method for the manufacture of a packing container from a web or a plane sheet or blank of a heat-shrinkable material comprising a laminate of orientation-stretched polyester, which has at least one surface coating of glycol-modi fied polyester (so-called PETG), the said web or sheet being formed to a tube in the first place in that two opposite edge zones of the web or sheet are joined together, and that thereafter parts of the tube formed are heated so that the material for the purpose of forming is made to shrink.
- PETG glycol-modi fied polyester
- the invention also relates to an arrangement for the realization of the method and to packing containers manufactured in accordance with the method.
- bottlelike packing containers can be manufactured by the plastic deforming of packing material in the form of a web or a blank. This is done e.g. by blowing of plastic bottles, but also by the shrink-forming of a previously orientation-stretched plastic material, which after heating is made to shrink over a mandrel. It has long been desirable to manufacture such containers with a gas-barrier layer, which is necessary if the contents are pressurized or sensitive to oxygen gas.
- a product is beer, which has to have a packing material, which does not give admission to oxygen gas from the atmosphere as this would have a detrimental effect on the quality of the beer, and which neither lets out the carbon dioxide in the beer package.
- plastic material which is formed by blowing or deepdrawing
- both acrylonitrile material e.g. a material which is marketed under the trade mark BAREX
- polyester material e.g. a material which is marketed under the trade mark BAREX
- the acrylonitrile material has the advantage that it has relatively good gas-tightness characteristics, but it has on the other hand inferior pressure, absorbing characteristics and is subject to a constant deformation, so-called creep, when it is exposed to pressure.
- Polyester material for its part has very good pressure absorbing characteristics, especially if it is orientation-stretched, whilst in return the gas-tightness is inferior.
- aluminium foil has very good gas barrier properties even if the aluminium foil is extremely thin (5 ⁇ m or less).
- the problem has been to create a plastic deformable laminate comprising aluminium foil.
- a laminate, which is containing a combination of aluminium foil and orientation stretched polyester should be an ideal packaging material, for instance beer, provided the laminate can be formed to a container or bottle.
- Fig. 1 is showing an enlarged cross-section of an orientation stretched packaging laminate
- Fig. 2, 3 and 4 are showing how a laminate, in accordance with fig. 1 in the form of a web or a sheet, is folded into a tube by joining the longitudinal edges of the web or sheet in an overlap joint.
- the figures are showing the overlap joint in an enlarged cross section.
- Fig. 2 is showing a conventional overlap joint
- Fig. 3 is showing an overlap joint, in which the aluminium foil layer has been cut out along one of the web edges, and
- Fig. 4 is showing an overlap joint with cut-out parts in the aluminium foil layer and with an intermediate sealing layer in the form of a string of plastic material.
- Fig. 5 is showing an expandable mandrel,
- Fig. 6 is showing the mandrel in accordance with fig. 5 after it has been expanded and a tube of packing laminate has been fitted over the mandrel
- Fig. 7 is showing a packing container manufac t ⁇ red in accordance with the invention.
- Fig. 8 is showing an expandable mandrel, on which two or more packing containers can be manufactured at the same time, and
- Fig. 9 a finished packing container in accordance with the invention.
- Fig. 10 is showing a variant of the method of manufacture, where the container is manufactured in two operations, the one shrunk-in end of the container being shrunk over a solid mandrel, whilst the other end, in a separate operation in accordance with fig. 11, is shrunk with the help of an expandable mandrel.
- Fig. 12 finally is showing an alternative embodiment of the laminate for the manufacture of containers in accordance with the invention.
- the material on the one hand, should be subjected to plastic form-processing and that, on the other hand, it should be joined together in sealing joints and that the material should be biaxially orientation-stretched and contain a gas barrier. It has been mentioned in the preamble that orientation-stretched polyester, which has very good tensile strength characteristics cannot be heat-sealed after the orientation stretching, since a crystalline structure has been imparted to the material.
- polyester can be co-extruded with a modified polyester, so-called glycol-modified polyester (PETG), and since these materials are very closely akin, they fuse together during the co-extrusion in a boundary area in such a manner that after the extrusion the materials cannot be separated from one another. It is possible, for example, in such a co-extrusion to have a central layer of PET and outer PETG layers on either side thereof. Such a laminate, after the extrusion operation, can be subjected to a joint orientation-stretching at a suitable temperature (approx.
- the central PET layer being molecular-oriented and given a crystalline structure, whilst the two outer PETG layers substantially retain their amorphous molecular structure and consequently their heatsealing capacity. If the material is stretched four times in two directions at right angles to one another the total stretching will be 16 times, that is to say the surface of the material increases 16 times. If the stretching becomes altogether too great (25 times), the PETG layers begin to crystallize more and more with the heat-sealing capacity dimi nishing to a corresponding degree. This means that the stretching of the material cannot be forced to an unlimited degree, but a stretching of the laminate to 20-25 times is quite possible whilst retaining the heat- sealing capacity of the outer layers.
- Such an orienta tion-stretched laminate has very great tensile strength and is thus suitable packing material for pressurized contents, e.g. beer, refreshing beverages etc.
- the gas-tightness generally is not sufficient and for this reason a layer providing gas-tightness has to be introduced into the laminate.
- a layer providing gas-tightness may consist of a gastightplastic e.g. polyvinyl alcohol (PVA), polyvinylidene chloride (PVDC) or of the type of acrylonitrile material, which comes on the market under the trade mark BAREX.
- a material with al together superior gas-tightness properties is metal foil and in particular aluminium foil, which even in thicknesses of 5 ⁇ , that is to say 5/1 000 mm is as good as completely gastight.
- a thin aluminium layer is very fragile and on the whole tolerates no tensile stresses whatever, whereas on the other hand it can be wrinkled together relatively readily if it is allowed to shrink together with a plastic material.
- the aforementioned, orientation-stretched laminate thus can be laminated with a thin aluminium foil, which is done with the help of a varnish, which fastens onto the aluminium foil surface as well as to the oriented polyester surface.
- Outside the aluminium foil may be placed a further layer of thermoplastic, e.g. polyethylene or PETG, which in the abovementioned material is advantageous, especially as the laminate is to be folded to a tube by joining together outside and inside of the laminate in an overlap join.
- a laminate which has been manufactured in such a manner that in the first place a PET layer 2 and a PETG layer 1 have been extruded jointly and have been subjected to orientation-stretching in two directions at right angles to each other.
- An aluminium foil layer 3 has been coated by an extrusion process with a PETG layer 1', whereupon the orientationstretched PET layer is varnish-laminated to the aluminium foil/PETG laminate.
- the laminate shown in fig. 1 thus contains two surface layers 1 and 1' of PETG (the one layer 1 having been orientation-stretched) and a central base layer 2 of biaxially orientation-stretched PET and an aluminium foil 3.
- the layer 1' is very thin and since the adhesion force in the varnish-lamination layer between the layer 1' and the aluminium foil layer 3 is considerably lower than the adhesion force between the layers 1 and 2 and the layers 1 and 1', as these are heat-sealed to one another, it is found that the sealing join cannot absorb particularly large tensile stresses, since all the tensile stresses will be concentrated on the layer 1' in the upper layer in the overlap join, since the other layers 1 and 2 cannot participate in the absorption of the forces, as they are separated from the layer 1' by the varnish-laminated aluminium foil layer 3.
- a solution of the problem is illustrated in fig. 4 and this solution implies that a strand 5 of molten PETG material is extruded onto both or just one of the edge regions, which are to be joined to one another in an overlap join, whereupon the edge regions are combined and pressed against one another whilst they are cooled from the outside of the material. It has been found that by regulating the temperature and volume of the extruded strand it is possible to regulate the heat content in the strand in such a manner that heat is transferred to the adjoining PETG layers to such a degree that these are melted in their surface regions so as to forma substantially homogeneous connection layer, which comprises the layers 1' and 1 situated in the overlap join as well as the extruded strand 5. If the heat content in the strand 5 is controlled correctly, the heat is consumed only to perform the seal without heating the remaining parts of the laminate in such a manner that shrinkage is occasioned or a loss of the orientation occurs.
- the tube or pipe of molecular-oriented PET/ PETG-laminate provided with aluminium foil now formed can be form-processed further by shrink-forming over a mandrel and some embodiments of such a shrink-forming will be described in the following.
- a tube manufactured from the abovementioned material, which has been sealed in a longitudinal join in the abovementioned manner, can be shrink-formed over a mandrel, and the following description will furnish several suggestions regarding methods and arrangements for the manufacture from a tube of shrinkable material of a bottlelike packing container of the laminate, which has been described earlier. Since the container aimed at is manufactured in such a manner that the end por brane material, inserted wires or "beams" so as to guide the appearance of the membrane when it is expanded.
- the mandrel 6 When a packing container is to be formed, the mandrel 6 is expanded in that compressed gas is supplied through the duct 12, the pressure being increased in the cutout space 9. Owing to the increased pressure in the space 9, the expandable membrane 10, which may be manufactured from a rubberlike material, will be expanded in the manner as shown in fig. 6. The expansion can be guided to a certain extent through the inserted wires or beams 13 so as to obtain a circular or at least less strongly curved portion of the expandable part of the mandrel. After the expansion of the mandrel the tube 14, which is manufactured from the aforementioned orientation-stretched laminate, is fitted, whereupon the end portions of the tube are heated so that the material is caused to shrink.
- the shrinkage may be forced very far and an accurate adhesion of the tube 14 to the mandrel 6 can be obtained. It should be noted that in this shrinkage the aluminium foil layer, which forms part of the laminate, will follow along without any breakages occurring in the aluminium foil layer. If the aluminium foil layer has good adhesion to the laminate moreover, the "shrinkage" of the aluminium foil layer will take place in the form of a very dense wrinkling or contraction.
- the "wrinkles" on the aluminium foil formed will be so small and dense that they can hardly be distinguished, but manifest themselves optically primarily through the disappearance of the gloss of the bare aluminium foil and through the shrunk portions of the laminate showing a "duller metallic lustre" derived from the aluminium foil laminate.
- the shrink-forming of the laminate however, no breakages occur in the aluminium foil layer, but the same stays intact and retains its gastight characteristics. If the aluminium foil layer is too thick and rigid, the shrinkage of the laminate may be rendered more difficult or be prevented, but it has been found that an aliminium foil layer of 5-10 ⁇ thickness
- the laminate tube 14 is shrunk so that it adheres to the expanded mandrel, which is marked by a broken line in the figure.
- the shrunk tube 14 is designated 16 in fig. 6, and as is evident from the figure the shrunk container 16 is provided with two cylindrical portions 15 of smaller dia meter, which are shrink-formed around the solid mandrel portions 7 and 8 and a cylindrical or "barrel-shaped" portion of larger diameter along the parts where the tube 14 adheres to the expanded part 10 of the mandrel 6.
- parts of the tube 14 may extend beyond the solid part of the mandrel 7.
- the duct 12 is connected to atmospheric pressure of a source of vacuum, which causes the membrane 10 to contract so that it assumes the position, which is shown in fig. 5.
- the container part 16 shown in fig. 7, as has been made evident, has an inward-turned flange 38 at the end, which terminates the neck-shaped part 19 of the container as well as an outward-turned flange 37 at the part, which is intended to constitute the bottom of the container. Furthermore, in fig.
- the bottom of the container 16 may be closed after the container has been filled in that a plastic or metal end wall 25 is provided over the outward-turned flange 37 and is beaded together with the said flange so as to form a tight end wall closure.
- the proportions shown in fig. 7 of the packing container have been chosen only in order to illustrate clearly the method of manufacture, and the proportions naturally can be altered, e.g. the neck and bottom portions shrunk over the solid mandrel portions may be made shorter in order to make better use of the material and it also may be appropriate to arrange the mandrel in such a manner that the solid portion 8 of the mandrel 6, around which the bottom part of the container is shrunk, has a substantially greater diameter than the portion 7 of the mandrel 6, around which neck part 19 is shrunk.
- This mandrel 6 is constructed in principle in the same manner as the mandrel, which has been described previously, but it has instead two expandable membranes 10 and three solid mandrel parts, namely two outer solid mandrel parts 8, around which the bottom of the containers is shrunk and a central solid mandrel part 7, around which the neck portions of the two containers facing one another are shrunk.
- the shrunk tube 14 is cut along the central line 23 around the shrunk portion of the tube.
- the parts of the shrunk tube 14 thus separated can be withdrawn subsequently from the mandrel 6, and in order to facilitate the withdrawal, especially if the solid parts 8 of the mandrel have a larger diameter than the central solid part 7 of the mandrel, the mandrel 6 should be dividable along the line 21 so that, after the separation of the shrunk tube 14 along the annular, line 23, the mandrel 6 is divided in that the mandrel halves are shifted in relation to each other, whereupon the shrink-formed container parts can be withdrawn from the mandrel parts after the expandable membranes have been returned to their starting position marked by a broken line.
- FIG. 9 is shown schematically a packing container in accordance with the invention, partly cut open and as is evident from the figure the container consists of a central, non-shrunk part 39 of large diameter and a shrunk neck part 40 and a similarly shrunk bottom part 41.
- the bottom part 41 is closed with a beaded-on end wall 25, e.g. of sheet-steel, whilst the top opening of the container is closed with the help of a weldedon end wall 26, which is fitted against the inward-turned flange of the container not shown here.
- a pouring opening is provided, e.g. in that a PETG strip 27 is welded onto the end wall 26, which moreover may be provided with weakening lines.
- a part of the end wall 26 is also torn off so as to form an emptying opening.
- the shrunk-in bottom portion of the bottle may be given a larger diameter than the neck portion, which implies having to make the end plate 25 somewhat larger.
- the packing container may also be manufactured in a different manner from that described here. For example, in accordance with fig.
- a pipe or a tube 31 of the type mentioned earlier comprising an alumi nium foil layer or a layer of gastight plastic is shrunk around a solid mandrel consisting of separable parts 28 and 29.
- the manufacture of the container is carried out in two stages, namely in the first place the tube 31 is fitted over the solid mandrels 28 and 29, whereafter the tube 31 is heated to shrinkage so that it accurately adheres to the profiled portions of the mandrels, the shrunk parts assuming the position shown in broken lines and marked 32.
- the shrunk in pipe or tube 31 is cut by means of an annular incision 33 to yield two formed halves.
- the mandrel portions 28 and 29 are separated from one another, whereupon the partly shrink-formed parts of the laminated tube are fitted onto a second mandrel 6, which shows great similarities to the expandable mandrel described in fig. 5.
- the mandrel 6 thus has a solid mandrel portion 42 and an expandable membrane 10, which is stretched over a recess or a cavity 9.
- the membrane 10 is expanded by supplying compressed gas through the duct 12 to the cavity 9.
- the partially shrunk package blank 32 is placed on the expanded mandrel 6 in the manner as shown in fig. 11, whereafter the non-shrunk part 34 of the tube blank 32 is heated to shrinkage.
- the expanded membrane 10 can be retracted by connecting the duct to atmospheric pressure or to a source of vacuum, where after the formed package can be withdrawn from the mandrel 6.
- the packing container manufactured in accordance with the said two-stage process can be provided in a similar manner to that mentioned earlier with an outward-turned flange at its bottom end and with an inward-turned flange at its opening for the arrangement of a pouring opening and, after it has been filled, a plastic or metal lid can be beaded on around the outward-flanged lower end wall.
- an alternative laminate combination consisting of a co-extruded three-layer material, comprising a central layer 2 of PET and outer layers 1 of PETG.
- a co-extruded three-layer material comprising a central layer 2 of PET and outer layers 1 of PETG.
- an aluminium foil layer 3 may be varnish-laminated or glued to one of the PETG layers 1 and a further, nonorientation-stretched PETG layer 36 may be laminated to the aluminium foil layer after the same has been primed with a varnish.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
- Tubes (AREA)
Abstract
A method for the manufacture by means of shrink-forming of a packing container of orientation-stretched laminate comprising polyester and aluminium foil, the laminate being formed to a tube (14) and subsequently being made to shrink over a mandrel (10, 28) to the intended shape.
Description
A METHOD FOR THE MANUFACTURE OF PACKING CONTAINERS AND AN ARRANGEMENT FOR THE REALIZATION OF THE METHOD
The present invention relates to a method for the manufacture of a packing container from a web or a plane sheet or blank of a heat-shrinkable material comprising a laminate of orientation-stretched polyester, which has at least one surface coating of glycol-modi fied polyester (so-called PETG), the said web or sheet being formed to a tube in the first place in that two opposite edge zones of the web or sheet are joined together, and that thereafter parts of the tube formed are heated so that the material for the purpose of forming is made to shrink. The invention also relates to an arrangement for the realization of the method and to packing containers manufactured in accordance with the method. It is known in the technology of packaging that bottlelike packing containers can be manufactured by the plastic deforming of packing material in the form of a web or a blank. This is done e.g. by blowing of plastic bottles, but also by the shrink-forming of a previously orientation-stretched plastic material, which after heating is made to shrink over a mandrel. It has long been desirable to manufacture such containers with a gas-barrier layer, which is necessary if the contents are pressurized or sensitive to oxygen gas. One example of such a product is beer, which has to have a packing material, which does not give admission to oxygen gas from the atmosphere as this would have a detrimental effect on the quality of the beer, and which neither lets out the carbon dioxide in the beer package. It is known that for this purpose plastic material can be used, which is formed by blowing or deepdrawing, and in this connection both acrylonitrile material, e.g. a material which is marketed under the trade
mark BAREX, has been used, but also polyester material. The acrylonitrile material has the advantage that it has relatively good gas-tightness characteristics, but it has on the other hand inferior pressure, absorbing characteristics and is subject to a constant deformation, so-called creep, when it is exposed to pressure. Polyester material for its part has very good pressure absorbing characteristics, especially if it is orientation-stretched, whilst in return the gas-tightness is inferior.
It is well known that aluminium foil has very good gas barrier properties even if the aluminium foil is extremely thin (5 μ m or less). However, the problem has been to create a plastic deformable laminate comprising aluminium foil. Up to now this has been impossible, owing to the fact that an aluminium foil will rupture when it is stretched already when the stretching only is a few per cent and this means that laminate comprising aluminium foil can not be blown or deep drawn in a normal way. A laminate, which is containing a combination of aluminium foil and orientation stretched polyester should be an ideal packaging material, for instance beer, provided the laminate can be formed to a container or bottle. Up to now it has not been possible to use aluminium foil as a gas barrier in a container, which has been produced by plastic deforming of a material, but the present invention is giving a teaching about a method and a device for producing such packaging containers, which characterizing features appear from the enclosed patent claims.
An embodiment of the method and device in accordance with the invention will in the following be described with references to the enclosed schematic drawing, in which: Fig. 1 is showing an enlarged cross-section of an orientation stretched packaging laminate,
Fig. 2, 3 and 4 are showing how a laminate, in accordance with fig. 1 in the form of a web or a sheet, is folded into a tube by joining the longitudinal edges of the web or sheet in an overlap joint. The figures are showing the overlap joint in an enlarged cross section.
Fig. 2 is showing a conventional overlap joint, Fig, 3 is showing an overlap joint, in which the aluminium foil layer has been cut out along one of the web edges, and
Fig. 4 is showing an overlap joint with cut-out parts in the aluminium foil layer and with an intermediate sealing layer in the form of a string of plastic material. Fig. 5 is showing an expandable mandrel,
Fig. 6 is showing the mandrel in accordance with fig. 5 after it has been expanded and a tube of packing laminate has been fitted over the mandrel, and Fig. 7 is showing a packing container manufac tύred in accordance with the invention.
Fig. 8 is showing an expandable mandrel, on which two or more packing containers can be manufactured at the same time, and
Fig. 9 a finished packing container in accordance with the invention.
Fig. 10 is showing a variant of the method of manufacture, where the container is manufactured in two operations, the one shrunk-in end of the container being shrunk over a solid mandrel, whilst the other end, in a separate operation in accordance with fig. 11, is shrunk with the help of an expandable mandrel.
Fig. 12 finally is showing an alternative embodiment of the laminate for the manufacture of containers in accordance with the invention. As mentioned earlier, it is the object of the present invention to provide methods and means for the
manufacture of a packing container from orientationstretched polyester and in particular a container, which in addition is gas-tight. It is a further pre-requisite for the invention that it shall be possible to furnish the material for the package as a web or plane blank and not, as is the case now, in the form of seamless extruded tubes or injection-moulded semi-finished products. Thus it is a condition for the manufacture of a container in accordance with the invention that the material, on the one hand, should be subjected to plastic form-processing and that, on the other hand, it should be joined together in sealing joints and that the material should be biaxially orientation-stretched and contain a gas barrier. It has been mentioned in the preamble that orientation-stretched polyester, which has very good tensile strength characteristics cannot be heat-sealed after the orientation stretching, since a crystalline structure has been imparted to the material. However, polyester (PET) can be co-extruded with a modified polyester, so-called glycol-modified polyester (PETG), and since these materials are very closely akin, they fuse together during the co-extrusion in a boundary area in such a manner that after the extrusion the materials cannot be separated from one another. It is possible, for example, in such a co-extrusion to have a central layer of PET and outer PETG layers on either side thereof. Such a laminate, after the extrusion operation, can be subjected to a joint orientation-stretching at a suitable temperature (approx. 70-80°C), the central PET layer being molecular-oriented and given a crystalline structure, whilst the two outer PETG layers substantially retain their amorphous molecular structure and consequently their heatsealing capacity. If the material is stretched four times in two directions at right angles to one another the total stretching will be
16 times, that is to say the surface of the material increases 16 times. If the stretching becomes altogether too great (25 times), the PETG layers begin to crystallize more and more with the heat-sealing capacity dimi nishing to a corresponding degree. This means that the stretching of the material cannot be forced to an unlimited degree, but a stretching of the laminate to 20-25 times is quite possible whilst retaining the heat- sealing capacity of the outer layers. Such an orienta tion-stretched laminate has very great tensile strength and is thus suitable packing material for pressurized contents, e.g. beer, refreshing beverages etc. However, the gas-tightness generally is not sufficient and for this reason a layer providing gas-tightness has to be introduced into the laminate. Such a layer providing gas-tightness may consist of a gastightplastic e.g. polyvinyl alcohol (PVA), polyvinylidene chloride (PVDC) or of the type of acrylonitrile material, which comes on the market under the trade mark BAREX. A material with al together superior gas-tightness properties, however, is metal foil and in particular aluminium foil, which even in thicknesses of 5 μ, that is to say 5/1 000 mm is as good as completely gastight. However, such a thin aluminium layer is very fragile and on the whole tolerates no tensile stresses whatever, whereas on the other hand it can be wrinkled together relatively readily if it is allowed to shrink together with a plastic material. The aforementioned, orientation-stretched laminate thus can be laminated with a thin aluminium foil, which is done with the help of a varnish, which fastens onto the aluminium foil surface as well as to the oriented polyester surface. Outside the aluminium foil may be placed a further layer of thermoplastic, e.g. polyethylene or PETG, which in the abovementioned material is advantageous, especially as the laminate is to be folded to a tube by joining together outside and inside of the
laminate in an overlap join.
In principle it is not necessary to apply PETG layers to both sides of the PET layer, but in the enclosed fig. 1 a laminate is shown, which has been manufactured in such a manner that in the first place a PET layer 2 and a PETG layer 1 have been extruded jointly and have been subjected to orientation-stretching in two directions at right angles to each other. An aluminium foil layer 3 has been coated by an extrusion process with a PETG layer 1', whereupon the orientationstretched PET layer is varnish-laminated to the aluminium foil/PETG laminate. The laminate shown in fig. 1 thus contains two surface layers 1 and 1' of PETG (the one layer 1 having been orientation-stretched) and a central base layer 2 of biaxially orientation-stretched PET and an aluminium foil 3.
As mentioned earlier it is possible, starting from this material in the form of a web or blank, to manufacture a pipe or tube by joining together opposite edges of the sheet or blank in an overlap join. In fig.2 is shown how the laminate in accordance with fig. 1 has been joined in such an overlap join, and it is possible to imagine that this join becomes a longitudinal sealing join in a pipe or a tube. For the sake of simplicity the different laminate layers in fig. 2, 3 and 4 have been provided with the same reference designations as in fig. 1. If fig. 2 is studied more closely it will be found that a material fusion and connection can be obtained between the layers 1 and 1'. However, the layer 1' is very thin and since the adhesion force in the varnish-lamination layer between the layer 1' and the aluminium foil layer 3 is considerably lower than the adhesion force between the layers 1 and 2 and the layers 1 and 1', as these are heat-sealed to one another, it is found that the sealing join cannot absorb particularly large tensile stresses, since all the tensile
stresses will be concentrated on the layer 1' in the upper layer in the overlap join, since the other layers 1 and 2 cannot participate in the absorption of the forces, as they are separated from the layer 1' by the varnish-laminated aluminium foil layer 3.
Thus if the laminate is to be used in packing containers for pressurized contents, a longitudinal join on the tube from which the package is to be made can not be manufactured in accordance with fig. 2. A better solution of the problem is provided by the sealing joints according to fig. 3 and 4. As is evident from fig. 3, the material edge, which is located uppermost in the overlap join, is provided with a cutout 4, wherein the aluminium foil layer 3 is not present. This cut out runs along the edge region and has a .width, which corresponds to ihe width of the overlap join. It has been found that by the introduction of such a recess the strong, orientation-stretched base layers 2 remain firmly anchored to each other in the overlap join by virtue of the PETG layers 1' and 1 having been made to fuse together with each other. Since a molecular oriented plastic material is made to shrink when it is heated to such a degree that the orientation stresses are released, it can be difficult to achieve an overlap join in accordance with fig. 3. If the layers only are heated, either the shrinking stresses can be released or the orientation too can be destroyed, which has the effect that the material loses its strength. This must not be allowed to happen, since the join must be equally strong as the remainder of the packing material, if it is to be possible for the internal pressure in the packing container to be absorbed. A solution of the problem is illustrated in fig. 4 and this solution implies that a strand 5 of molten PETG material is extruded onto both or just one of the edge regions, which are to be joined to one another in an overlap join,
whereupon the edge regions are combined and pressed against one another whilst they are cooled from the outside of the material. It has been found that by regulating the temperature and volume of the extruded strand it is possible to regulate the heat content in the strand in such a manner that heat is transferred to the adjoining PETG layers to such a degree that these are melted in their surface regions so as to forma substantially homogeneous connection layer, which comprises the layers 1' and 1 situated in the overlap join as well as the extruded strand 5. If the heat content in the strand 5 is controlled correctly, the heat is consumed only to perform the seal without heating the remaining parts of the laminate in such a manner that shrinkage is occasioned or a loss of the orientation occurs.
It has been found that by realising a longitudinal tube join according to fig. 4 and at the same time introducing a cutout 4 of the aluminium foil along one edge region of the laminate, a join can be obtained, which in respect of this strength is comparable with the rest of the material.
The tube or pipe of molecular-oriented PET/ PETG-laminate provided with aluminium foil now formed can be form-processed further by shrink-forming over a mandrel and some embodiments of such a shrink-forming will be described in the following.
A tube manufactured from the abovementioned material, which has been sealed in a longitudinal join in the abovementioned manner, can be shrink-formed over a mandrel, and the following description will furnish several suggestions regarding methods and arrangements for the manufacture from a tube of shrinkable material of a bottlelike packing container of the laminate, which has been described earlier. Since the container aimed at is manufactured in such a manner that the end por
brane material, inserted wires or "beams" so as to guide the appearance of the membrane when it is expanded.
When a packing container is to be formed, the mandrel 6 is expanded in that compressed gas is supplied through the duct 12, the pressure being increased in the cutout space 9. Owing to the increased pressure in the space 9, the expandable membrane 10, which may be manufactured from a rubberlike material, will be expanded in the manner as shown in fig. 6. The expansion can be guided to a certain extent through the inserted wires or beams 13 so as to obtain a circular or at least less strongly curved portion of the expandable part of the mandrel. After the expansion of the mandrel the tube 14, which is manufactured from the aforementioned orientation-stretched laminate, is fitted, whereupon the end portions of the tube are heated so that the material is caused to shrink. As the material has been orientation-stretched as much as 10 to 20 times, the shrinkage may be forced very far and an accurate adhesion of the tube 14 to the mandrel 6 can be obtained. It should be noted that in this shrinkage the aluminium foil layer, which forms part of the laminate, will follow along without any breakages occurring in the aluminium foil layer. If the aluminium foil layer has good adhesion to the laminate moreover, the "shrinkage" of the aluminium foil layer will take place in the form of a very dense wrinkling or contraction. The "wrinkles" on the aluminium foil formed will be so small and dense that they can hardly be distinguished, but manifest themselves optically primarily through the disappearance of the gloss of the bare aluminium foil and through the shrunk portions of the laminate showing a "duller metallic lustre" derived from the aluminium foil laminate. During the shrink-forming of the laminate, however, no breakages occur in the aluminium foil layer, but the
same stays intact and retains its gastight characteristics. If the aluminium foil layer is too thick and rigid, the shrinkage of the laminate may be rendered more difficult or be prevented, but it has been found that an aliminium foil layer of 5-10 μ thickness
"follows" the laminate during shrinkage without difficulty and retains its sealing characteristics.
In fig. 6, which shows the mandrel in accordance with fig. 5 in expanded state, the laminate tube 14 is shrunk so that it adheres to the expanded mandrel, which is marked by a broken line in the figure. The shrunk tube 14 is designated 16 in fig. 6, and as is evident from the figure the shrunk container 16 is provided with two cylindrical portions 15 of smaller dia meter, which are shrink-formed around the solid mandrel portions 7 and 8 and a cylindrical or "barrel-shaped" portion of larger diameter along the parts where the tube 14 adheres to the expanded part 10 of the mandrel 6. As can be seen in the figure, parts of the tube 14 may extend beyond the solid part of the mandrel 7. These are intended to form the "neck" or emptying opening of the packing container, where the material will shrink in over the end surface of the mandrel 6 to form an invard-turned flange 38, which may be shaped additionally with the help of a pressing tool, which is pressed against the end surface of the mandrel 6. In a similar manner the opposite part of the tube may be formed to an outward-turned flange 37 with the help of a tool, which flanges the material out and prevents it from shrinking down over the edge of the mandrel 6.
When the shrinking operation has been concluded, the duct 12 is connected to atmospheric pressure of a source of vacuum, which causes the membrane 10 to contract so that it assumes the position, which is shown in fig. 5. This means that the mandrel 6 and the container part 16 formed can be separated from each other
by withdrawing the container part 16 from the mandrel, and in fig. 7 is shown the withdrawn container part. The container part 16 shown in fig. 7, as has been made evident, has an inward-turned flange 38 at the end, which terminates the neck-shaped part 19 of the container as well as an outward-turned flange 37 at the part, which is intended to constitute the bottom of the container. Furthermore, in fig. 7 the longitudinal sealing join of the tube 14, wherein a cutout has been made in the aluminium foil layer in the manner described earlier, is designated 20 and a plastic disc welded against the inward-turned flange 38 is designated 17. In the plastic disc 17, which should be made of the same material as the rest of the packing container, may be provided an emptying opening of optional type, e.g. a hole covered by a tear-off cover strip or a tear-off indication provided in the plate 17. The bottom of the container 16 may be closed after the container has been filled in that a plastic or metal end wall 25 is provided over the outward-turned flange 37 and is beaded together with the said flange so as to form a tight end wall closure.
The proportions shown in fig. 7 of the packing container have been chosen only in order to illustrate clearly the method of manufacture, and the proportions naturally can be altered, e.g. the neck and bottom portions shrunk over the solid mandrel portions may be made shorter in order to make better use of the material and it also may be appropriate to arrange the mandrel in such a manner that the solid portion 8 of the mandrel 6, around which the bottom part of the container is shrunk, has a substantially greater diameter than the portion 7 of the mandrel 6, around which neck part 19 is shrunk. AS mentioned earlier, it may be advantageous to manufacture several packing containers simulta
neously in one shrinking operation. One of the advantages obtained by this, beside rationalization, is that the shrunk-in neck portions on the containers can be given a better defined length and edge than when the containers are shrunk individually. The reason for this is that a tube, which is shrunk around a mandrel, receives a somewhat uneven opening edge, which means that the edge has to be trimmed by cutting off a small amount. If on the other hand two containers facing one another are shrunk simultaneously, they can be separated readily by cut along the shrunk portion. This means that the two opening edges automatically will be well defined and uniform without anything having to be "trimmed off". In fig. 8 is shown how two packing containers are shrunk simultaneously on a "long" mandrel 6. This mandrel 6 is constructed in principle in the same manner as the mandrel, which has been described previously, but it has instead two expandable membranes 10 and three solid mandrel parts, namely two outer solid mandrel parts 8, around which the bottom of the containers is shrunk and a central solid mandrel part 7, around which the neck portions of the two containers facing one another are shrunk. After the shrink-forming around the expanded mandrel 6 in the manner as described above, the shrunk tube 14 is cut along the central line 23 around the shrunk portion of the tube. The parts of the shrunk tube 14 thus separated can be withdrawn subsequently from the mandrel 6, and in order to facilitate the withdrawal, especially if the solid parts 8 of the mandrel have a larger diameter than the central solid part 7 of the mandrel, the mandrel 6 should be dividable along the line 21 so that, after the separation of the shrunk tube 14 along the annular, line 23, the mandrel 6 is divided in that the mandrel halves are shifted in relation to each other, whereupon the shrink-formed container parts can be withdrawn from the mandrel parts
after the expandable membranes have been returned to their starting position marked by a broken line. In fig. 9 is shown schematically a packing container in accordance with the invention, partly cut open and as is evident from the figure the container consists of a central, non-shrunk part 39 of large diameter and a shrunk neck part 40 and a similarly shrunk bottom part 41. After filling, which preferably takes place through the open bottom part, the bottom part 41 is closed with a beaded-on end wall 25, e.g. of sheet-steel, whilst the top opening of the container is closed with the help of a weldedon end wall 26, which is fitted against the inward-turned flange of the container not shown here. In the end wall 26, which preferably may be made of plastic material, of PETG or a laminate of the same type as that from which the container is manufactured, a pouring opening is provided, e.g. in that a PETG strip 27 is welded onto the end wall 26, which moreover may be provided with weakening lines. When the strip 27 is torn away with the help of a free pull-lug, a part of the end wall 26 is also torn off so as to form an emptying opening. It is also possible to provide in an end wall a hole punched out in advance, which can be covered over with a tear-off strip or even realize the end wall with a hole having male or female thread so that it can be closed with a screw cap or a threaded plug. As mentioned earlier, the shrunk-in bottom portion of the bottle may be given a larger diameter than the neck portion, which implies having to make the end plate 25 somewhat larger. This is a certain advantage though as the supporting surface of the package will thereby be enlarged. If the supporting surface is considered to be insufficient, the package may be surrounded by an external sleeve 24, which is shown here in a partly cutopen condition. In most cases, however, the use of such a sleeve 24 will not be necessary.
The packing container may also be manufactured in a different manner from that described here. For example, in accordance with fig. 10, a pipe or a tube 31 of the type mentioned earlier comprising an alumi nium foil layer or a layer of gastight plastic is shrunk around a solid mandrel consisting of separable parts 28 and 29. In this case the manufacture of the container is carried out in two stages, namely in the first place the tube 31 is fitted over the solid mandrels 28 and 29, whereafter the tube 31 is heated to shrinkage so that it accurately adheres to the profiled portions of the mandrels, the shrunk parts assuming the position shown in broken lines and marked 32. After the shrunk-in portions have become stabilized by cooling, the shrunk in pipe or tube 31 is cut by means of an annular incision 33 to yield two formed halves. Now the man drel portions 28 and 29 are separated from one another, whereupon the partly shrink-formed parts of the laminated tube are fitted onto a second mandrel 6, which shows great similarities to the expandable mandrel described in fig. 5. The mandrel 6 thus has a solid mandrel portion 42 and an expandable membrane 10, which is stretched over a recess or a cavity 9. In the manner described earlier, the membrane 10 is expanded by supplying compressed gas through the duct 12 to the cavity 9. The partially shrunk package blank 32 is placed on the expanded mandrel 6 in the manner as shown in fig. 11, whereafter the non-shrunk part 34 of the tube blank 32 is heated to shrinkage. As a result it is formed around the expanded mandrel to assume a position 35, which is indicated by broken lines. After the material has been stabilized by cooling, the expanded membrane 10 can be retracted by connecting the duct to atmospheric pressure or to a source of vacuum, where after the formed package can be withdrawn from the mandrel 6.
The packing container manufactured in accordance with the said two-stage process can be provided in a similar manner to that mentioned earlier with an outward-turned flange at its bottom end and with an inward-turned flange at its opening for the arrangement of a pouring opening and, after it has been filled, a plastic or metal lid can be beaded on around the outward-flanged lower end wall. As mentioned earlier, laminated combinations other than those shown in fig. 1 and in the following figures will sometimes be used, and in fig. 12 an alternative laminate combination is shown consisting of a co-extruded three-layer material, comprising a central layer 2 of PET and outer layers 1 of PETG. To this co-extruded three-layer material may be imparted a biaxial orientation-stretching. Then an aluminium foil layer 3 may be varnish-laminated or glued to one of the PETG layers 1 and a further, nonorientation-stretched PETG layer 36 may be laminated to the aluminium foil layer after the same has been primed with a varnish.
It has been shown that it is possible with the method and the arrangement in accordance with the invention to manufacture a packing container, which is very thin-walled (for the sake of greater clarity the wall thickness in the enclosed figures has been exaggerated and the figures, in this respect, are not true to scale), which means that the consumption of plastic material for the packing containers can be kept extremely low, although the containers, thanks to the oriented polyester material, tolerate very high internal pressure and, thanks to the incorporated aluminium foil layer, possess very good gas-tightness. The packing containers manufactured in accordance with this method will be cheap to manufacture therefore and substantially surpass the containers known at present in respect of price, weight and gas-tightness.
Claims
1. A method for the manufacture of a packing container from a web or a plane sheet or blank of a heat-shrink able material comprising a laminate of orientation stretched polyester, which has at least one surface co ating of glycol-modified polyester (so-called PETG), the said web or sheet being formed to a tube in the first place in that two opposite edge zones of the web or sheet are joined together and that thereafter parts of the tube formed are heated so that the material for the purpose of forming is made to shrink, c h a r a c t e r i z e d i n that the tube formed is fitted over a mandrel comprising partly expandable portions and partly solid portions, that the tube is heated to shrinking so that it adheres to the outer contours of the said mandrel, that the expanded portions of the mandrel, after the shrunk plastic material has been stabilized through cooling, are made to assume a shape and a size, which correspond to the solid portions of the mandrel, that the container formed is withdrawn from the mandrel and is provided with a sealing end wall over one of the openings of the tube formed.
2. A method in accordance with claim 1, c h a r a ct e r i z e d i n that the laminate comprises a gastight layer, preferably aluminium foil and that a cutout of a width corresponding to the width of the overlap join is provided on forming of the tube in the said gastight layer along one of the longitudinal edges of the web or sheet.
3. A method in accordance with claim 1, c h a r a ct e r i z e d i n that a length of tube corresponding to two packing containers is arranged over a mandrel with two expandable portions, which are separated by a solid mandrel portion, and that the tube, after the shrinking operation over the mandrel, is separated in the portion, which has been formed through shrinkage against the said central solid portion of the mandrel so as to form two packing units, which are then withdrawn from the mandrel after the expandable portions of the mandrel have been made to contract to the cross-sectional area of the mandrel.
4. A method in accordance with claim 1, c h a r a ct e ri z e d i n that an inward-turned flange of the tube is formed against the end surface of the outer solid portion of the mandrel by shrinking in of the plastic material over the edge followed by a possible pressure-forming, the mandrel end serving as a holderup.
5. A method in accordance with claim 1, c h a r a ct e r i z e d i n that molten plastic material of modified polyester (PETG) is applied to one or both of the edge regions of the said web or sheet by means of extrusion before the edge regions are combined with each other to form the said tube.
6. An arrangement for the realization of the method in accordance with the preceding claims, c h a r a ct e r i z e d i n that a cylindrical mandrel is provided, whose diairteter corresponds to the inside diameter of the neck and bottom opening of the container produced and that the said mandrel has portions with cutouts or recesses, these portions being bridged over by a stretchable material, e.g. rubber or rubberlike plastics, which is fixed tightly in the mandrel in such a manner that the said stretchable bridge-over material does not exceed the contour of the mandrel, that ducts are provided in the mandrel, which can be connected to a source of compressed gas, the said ducts ending in the said cutout spaces or recesses so that the said fixed, stretchable material can be expanded with the help of compressed gas to form a body of an appreciable larger diameter than the diameter of the solid mandrel.
7. An arrangement in accordance with claim 6, c h a r a c t e r i z e d i n that the stretchable material is elastic so that when the said cutouts or recesses are connected to atmospheric pressure or to a source of vacuum it will contact to assume once more a position, which coincides with or is slightly smaller than the outer contour of the solid mandrel.
8. An arrangement in accordance with claim 6, c h a r a c t e r i z e d i n that the said material has varying thickness or expansion capacity with the object of controlling the outer shape of the expanded part of the mandrel.
9. A packing container manufactured in accordance with the method according to the invention, c h a r a ct e r i z e d i n that the one tubular end of the packing container is covered in a tight manner with a metal disc fitted on by means of beading.
10. A packing container manufactured in accordance with the method according to the invention, c h a r a ct e r i z e d i n that the one tubular end of the packing container is provided with an inward-turned flange, onto which a disc of the same material as the packing container is welded with the help of heat and pressure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE8383900445T DE3364793D1 (en) | 1982-01-20 | 1983-01-19 | A method for the manufacture of packing containers and a device for the realization of the method |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8200286A SE429626B (en) | 1982-01-20 | 1982-01-20 | SET FOR MEDIUM CRIMPING FORMING PACKAGING CONTAINERS ALSO DEVELOPING SET |
SE8200286-6820120 | 1982-01-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1983002423A1 true WO1983002423A1 (en) | 1983-07-21 |
Family
ID=20345775
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1983/000009 WO1983002423A1 (en) | 1982-01-20 | 1983-01-19 | A method for the manufacture of packing containers and an arrangement for the realization of the method |
Country Status (6)
Country | Link |
---|---|
US (2) | US4557888A (en) |
EP (1) | EP0099387B1 (en) |
JP (1) | JPS58502192A (en) |
DE (1) | DE3364793D1 (en) |
SE (1) | SE429626B (en) |
WO (1) | WO1983002423A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0189868B1 (en) * | 1985-01-25 | 1991-03-13 | Nippon Film Industrial Co., Ltd. | Packaging material and sealing cap |
US4942008A (en) * | 1985-07-10 | 1990-07-17 | Cahill John W | Process for molding a multiple layer structure |
US4753832A (en) * | 1985-09-10 | 1988-06-28 | The Procter & Gamble Company | Barrier laminates for the retention of essential oils, vitamins and flavors in citrus beverages and a method of making said laminate and leak-tight containers therefrom |
AU627689B2 (en) * | 1985-10-02 | 1992-09-03 | Robert Archibald Donald | Improved aseptic packaging |
US5071506A (en) * | 1987-10-09 | 1991-12-10 | Thiokol Corporation | Equipment for making composite tubes including an inflatable heated bladder and a composite mold having a negative coefficient of thermal expansion |
US5037178A (en) * | 1988-12-22 | 1991-08-06 | Kingston Technologies, L.P. | Amorphous memory polymer alignment device |
US5066091A (en) * | 1988-12-22 | 1991-11-19 | Kingston Technologies, Inc. | Amorphous memory polymer alignment device with access means |
FR2679821B1 (en) * | 1991-07-31 | 1993-10-22 | Rossignol Sa Skis | PROCESS FOR THE MANUFACTURE OF A COMPLEX MOLDED STRUCTURE, PARTICULARLY A SKI, AND COMPLEX MOLDED STRUCTURE THUS OBTAINED. |
SE517051C2 (en) | 1999-12-10 | 2002-04-09 | Tetra Laval Holdings & Finance | Continuous device in a distribution equipment |
US7217380B2 (en) * | 2002-07-22 | 2007-05-15 | Toyota Motor Sales, Usa, Inc. | Vibration apparatus and methods of vibration |
US20060091143A1 (en) * | 2004-11-03 | 2006-05-04 | Vinit Chantalat | Heat insulating covering for beverage containers |
US8783515B2 (en) | 2012-10-25 | 2014-07-22 | Sonoco Development, Inc. | Dispenser with fitment |
FR3006438B1 (en) * | 2013-06-04 | 2015-06-26 | Commissariat Energie Atomique | TEMPERATURE SENSOR |
KR102170841B1 (en) * | 2014-05-22 | 2020-10-27 | 뉴라이언 홀딩스 리미티드 | Handheld vaporizing device |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1481167A (en) * | 1974-06-27 | 1977-07-27 | Imp Metal Ind Kynoch Ltd | Mandrels |
SE413477B (en) * | 1978-09-06 | 1980-06-02 | Ekstrom & Co H A B | EXPANDABLE DORN FOR USE IN BUILDING OF Pipes |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2396635A (en) * | 1943-01-23 | 1946-03-19 | Bogoslowaky Boris | Collapsible tube |
US3032823A (en) * | 1960-05-26 | 1962-05-08 | Sherman Plastics Corp | Method of forming plastic articles |
US3347970A (en) * | 1964-08-19 | 1967-10-17 | Hercules Inc | Method of forming duplicate bottles by heat shrinking |
DE1778252A1 (en) * | 1968-04-11 | 1971-10-28 | Hoerauf M Maschinenfabrik | Method and device for the production of workpieces, preferably designed as cup-like containers tapering upwards or downwards |
US4129467A (en) * | 1974-10-18 | 1978-12-12 | Ab Ziristor | Method for making packing containers |
CH590760A5 (en) * | 1975-01-03 | 1977-08-31 | Rausing Anders Ruben | |
CH607969A5 (en) * | 1976-02-09 | 1978-12-15 | Tetra Pak Dev | |
US4085244A (en) * | 1976-02-10 | 1978-04-18 | Champion International Corporation | Balanced orientated flexible packaging composite |
US4121402A (en) * | 1976-03-10 | 1978-10-24 | Maryland Cup Corporation | Methods and means for manufacturing foam plastic containers and sidewall blanks for same |
US4054474A (en) * | 1976-03-18 | 1977-10-18 | Aluminum Company Of America | Shrink wrapping |
CH611833A5 (en) * | 1976-03-31 | 1979-06-29 | Tetra Pak Dev | |
US4312689A (en) * | 1977-02-22 | 1982-01-26 | The Procter & Gamble Company | Dispensing container and method of assembling it |
US4142630A (en) * | 1977-11-07 | 1979-03-06 | Ethyl Corporation | Collapsible dispensing tube |
JPS5677123A (en) * | 1979-11-29 | 1981-06-25 | Mitsubishi Chem Ind Ltd | Manufacture of food packing container |
JPS5944267B2 (en) * | 1979-12-14 | 1984-10-27 | 日本クラウンコルク株式会社 | Metal container lid with liner and manufacturing method thereof |
-
1982
- 1982-01-20 SE SE8200286A patent/SE429626B/en not_active IP Right Cessation
-
1983
- 1983-01-19 EP EP83900445A patent/EP0099387B1/en not_active Expired
- 1983-01-19 US US06/541,321 patent/US4557888A/en not_active Expired - Fee Related
- 1983-01-19 WO PCT/SE1983/000009 patent/WO1983002423A1/en active IP Right Grant
- 1983-01-19 DE DE8383900445T patent/DE3364793D1/en not_active Expired
- 1983-01-19 JP JP58500447A patent/JPS58502192A/en active Pending
-
1985
- 1985-09-20 US US06/778,073 patent/US4606954A/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1481167A (en) * | 1974-06-27 | 1977-07-27 | Imp Metal Ind Kynoch Ltd | Mandrels |
SE413477B (en) * | 1978-09-06 | 1980-06-02 | Ekstrom & Co H A B | EXPANDABLE DORN FOR USE IN BUILDING OF Pipes |
Also Published As
Publication number | Publication date |
---|---|
SE429626B (en) | 1983-09-19 |
JPS58502192A (en) | 1983-12-22 |
US4557888A (en) | 1985-12-10 |
EP0099387A1 (en) | 1984-02-01 |
DE3364793D1 (en) | 1986-09-04 |
US4606954A (en) | 1986-08-19 |
SE8200286L (en) | 1983-07-21 |
EP0099387B1 (en) | 1986-07-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0099387B1 (en) | A method for the manufacture of packing containers and a device for the realization of the method | |
US5009939A (en) | Composite paperboard and polymer package | |
AU660492B2 (en) | Paperboard bottle | |
EP1197438B1 (en) | Method of producing a packaging container | |
US4696840A (en) | Blown bag-in-box composite container and method and apparatus for making the same | |
US3717544A (en) | Lined plastic articles | |
US4983238A (en) | Method for manufacturing a thermoplastic container with a label | |
US4384440A (en) | Method for the continuous manufacture of packing containers | |
US5169470A (en) | Method of extrusion blow molding into paperboard inserts to form a composite package | |
GB2216090A (en) | Sealing end closures to container bodies | |
US4109813A (en) | Composite plastic container | |
EP0126575A2 (en) | Friction-welded barriered containers | |
US8945459B2 (en) | Container made from expanded plastic film | |
AU2002222028B2 (en) | Method for making heat-shrinkable skirt caps and resulting caps | |
US4898708A (en) | Method for shaping closed bottom of tubular container | |
EP0663278A1 (en) | Composite paperboard and plastic container | |
EP0244256B1 (en) | Method for producing tubular plastic containers | |
JPS61268426A (en) | Manufacture of oriented polyester container with resistance to heat shrinkage | |
JPS58177328A (en) | Method of composite molding of composite container of thermoplastic resin and paper | |
KR19980701626A (en) | How to make a packaging container | |
JPH0331716Y2 (en) | ||
EP0700333B1 (en) | A method of producing bottle or tube-like, capped packaging containers from a polymer material | |
GB2191730A (en) | A method of forming the head of a thermoplastic container | |
JPS6034331A (en) | Friction-welded can with barrier | |
JPS59134153A (en) | Composite vessel proper and its manufacture |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Designated state(s): JP US |
|
AL | Designated countries for regional patents |
Designated state(s): BE CH DE FR GB NL SE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1983900445 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 1983900445 Country of ref document: EP |
|
WWG | Wipo information: grant in national office |
Ref document number: 1983900445 Country of ref document: EP |