US20080006367A1 - Process for manufacturing a honeycomb composite material - Google Patents
Process for manufacturing a honeycomb composite material Download PDFInfo
- Publication number
- US20080006367A1 US20080006367A1 US11/860,081 US86008107A US2008006367A1 US 20080006367 A1 US20080006367 A1 US 20080006367A1 US 86008107 A US86008107 A US 86008107A US 2008006367 A1 US2008006367 A1 US 2008006367A1
- Authority
- US
- United States
- Prior art keywords
- web
- face
- honeycomb
- face sheet
- composite material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- 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
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
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- 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
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- 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
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- 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
- B29C66/438—Joining sheets for making hollow-walled, channelled structures or multi-tubular articles
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- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/834—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
- B29C66/8341—Roller, cylinder or drum types; Band or belt types; Ball types
- B29C66/83421—Roller, cylinder or drum types; Band or belt types; Ball types band or belt types
- B29C66/83423—Roller, cylinder or drum types; Band or belt types; Ball types band or belt types cooperating bands or belts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
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- 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
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- 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
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/4835—Heat curing adhesives
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- 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
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- 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
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- 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
- B29C66/72327—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 natural products or their composites, not provided for in B29C66/72321 - B29C66/72324
- B29C66/72328—Paper
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- 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
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- 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
- B29C66/725—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 hollow-walled or honeycombs
- B29C66/7252—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 hollow-walled or honeycombs hollow-walled
- B29C66/72521—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 hollow-walled or honeycombs hollow-walled comprising corrugated cores
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- 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
- B29C66/725—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 hollow-walled or honeycombs
- B29C66/7254—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 hollow-walled or honeycombs honeycomb structures
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- 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
- B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
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- 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
- B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
- B29K2023/04—Polymers of ethylene
- B29K2023/06—PE, i.e. polyethylene
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
- B29K2023/04—Polymers of ethylene
- B29K2023/08—Copolymers of ethylene
- B29K2023/083—EVA, i.e. ethylene vinyl acetate copolymer
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- B29K2311/00—Use of natural products or their composites, not provided for in groups B29K2201/00 - B29K2309/00, as reinforcement
- B29K2311/14—Wood, e.g. woodboard or fibreboard
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29K2711/00—Use of natural products or their composites, not provided for in groups B29K2601/00 - B29K2709/00, for preformed parts, e.g. for inserts
- B29K2711/14—Wood, e.g. woodboard or fibreboard
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
- B32B37/1207—Heat-activated adhesive
- B32B2037/1215—Hot-melt adhesive
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- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
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- 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
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- 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
- Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]
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- 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
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- 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
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- Y10T156/1084—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing of continuous or running length bonded web
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- 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
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- 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
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Definitions
- the present invention relates to the field of manufacturing composite materials and, more particularly, to a process for manufacturing a honeycomb composite material.
- the composite material can be used for packaging and building applications, for instance.
- Safe product delivery requires a strong and efficient packaging material which can hold up under tough conditions.
- selecting a packaging material one typically considers its weight, its recyclability, its mechanical properties, and its cost.
- Foam materials are widely used since they are inexpensive and lightweight. However they are typically not recognized as being environmentally friendly. Moreover, sometimes foam materials can generate static electricity when in contact with another object. Most paper honeycomb materials are fully recyclable, lightweight, and inexpensive. Honeycomb materials probably offer the best strength to weight ratio of packaging materials. However, they are characterized by a lower compressive strength in the plane of the material (edge compression resistance). Corrugated cardboards are also fully recyclable, lightweight, and inexpensive. However, important quantities of material are necessary to produce safe containers with corrugated cardboard, which increase the packaging cost. Moreover, corrugated cardboard having anti-static properties can be obtained.
- Mass production of packaging materials calls for cost efficient and continuous productions to be competitive with existing products. Furthermore, higher than average mechanical properties are sought, to allow reducing weight and lowering raw material cost.
- a process for a continuous production of a web of a composite material comprising the steps of: providing at least one web of face sheet material having a corrugated medium with a first face covered with a linerboard and an exposed second face, including unrolling the face sheet material from a roll; carrying said web of honeycomb material and said at least one web of face sheet material along a production line; and adhesively applying the exposed second face of the at least one web of face sheet material to one face of said honeycomb material while said honeycomb material is being conveyed through the production line and maintained in an expanded state.
- a packaging material manufactured with the process described hereinabove.
- an apparatus for a continuous production of a web of a composite material comprises at least one carrier for moving a web of honeycomb material along the apparatus; at least one carrier for moving at least one web of a face sheet material along the apparatus, the face sheet material having a corrugated medium with a linerboard on at least one face thereof; at least one laminator for adhesively applying the at least one web of the face sheet material to a face of the web of honeycomb material in an expanded state.
- paper is herein intended to means any wood fiber based material such as cardboard, kraft paper, recycled paper, medium, chipboard, bleached or not, and the like, for instance.
- FIG. 1 is a perspective view of a manually manufactured composite material according to the prior art
- FIG. 2 is an exploded perspective view of the composite material of FIG. 1 ;
- FIG. 3 is an exploded perspective view of a first embodiment of a composite material
- FIG. 4 is an exploded perspective view of a second embodiment of a composite material
- FIG. 5 is a schematic view of an example of a process for manufacturing a composite material in accordance with the first embodiment
- FIG. 6 is a schematic view of an example of a process for manufacturing a composite material in accordance with the second embodiment
- FIG. 7 is a top plan view of an apparatus for manufacturing a composite material.
- FIG. 8 is a side elevation view of the apparatus of FIG. 7 .
- the composite material 10 typically used in packaging applications is shown.
- the composite material 10 has a core portion 12 including an expanded honeycomb material 14 and two linerboards 16 laminated on the honeycomb material 14 .
- the linerboards 16 are used to maintain the honeycomb material 14 in an expanded state.
- a face sheet 18 is manually laminated on each linerboard 16 .
- the face sheet 18 has a corrugated medium 20 and two linerboards 22 , one laminated on each side of the corrugated medium 20 .
- the composite material 10 has satisfactory mechanical properties for some packaging applications. However, the operation of manually laminating the face sheets 18 on the core portion 12 results in relatively high manufacturing costs, and is known to limit the competitiveness of this product on the market.
- honeycomb composite material 10 a manufactured by a production line 30 such as shown in FIG. 5 .
- the composite material 10 a has a core portion 12 and two face sheets 18 laminated on the core portion 12 .
- the core portion 12 has a honeycomb material 14 in an expanded state.
- the honeycomb material 14 is not covered with linerboards 16 laminated on each side.
- the core portion 12 has two faces 34 a , 34 b .
- the cells of the honeycomb material 14 have an hexagonal shape, though any other suitable shape can be used.
- Each face sheet 18 includes a corrugated medium 20 having a first face 20 a with a linerboard 22 laminated thereon, and an exposed second face 20 b .
- the exposed second face 20 b of each face sheet 18 is directly laminated on the honeycomb material 14 forming the core portion 12 .
- the linerboard covered face 22 , of the face sheet material 18 can be directly laminated on the honeycomb material 14 , i.e. either face 22 or 20 b of the face sheet 18 can be applied to the honeycomb material 14 .
- the amount of raw material used is reduced as compared to the amount of raw material used in the composite material 10 shown in FIGS. 1 and 2 .
- the face sheets 18 can include a linerboard 22 laminated on a single side of the corrugated medium 20 , or alternately include a linerboard 22 laminated on each side of the corrugated medium.
- the composite material 10 b can also have a single face sheet 18 with a corrugated medium 20 applied thereon.
- the other face 34 b of the core portion 12 can be covered with a linerboard 22 or be left uncovered, for example.
- FIG. 5 an example of a production line 30 which can be used to manufacture the composite material 10 a ( FIG. 3 ) is shown.
- the production line 30 has a longitudinal axis 40 and a transversal axis 42 (visible in FIG. 7 ) which correspond to the longitudinal and transversal axis of the composite material 10 a .
- the faces sheets 18 are provided in webs. Two rolls 44 , 46 of face sheet material 18 are provided. In this example, the two rolls are similar.
- the corrugated medium has a first face covered with a linerboard, and a second face which is left exposed. The absence of a linerboard on the exposed, inner face, of the corrugated medium eases the rolling and unrolling of the face sheets into and from rolls.
- the face sheets 18 can be provided in rolls.
- the first face covered with a linerboard can be oriented either radially outwardly, or radially inwardly. Furthermore, either the covered face or the exposed face of the corrugated medium can be applied to the honeycomb material.
- the production line 30 can have only a single roll 44 . If the core portion 12 of the composite material 10 a has one face 34 a covered with a face sheet 18 including the corrugated medium 20 and the other face 34 b is covered with a linerboard 22 , a roll 48 ( FIG. 6 ) of linerboard 22 is provided instead of a roll 46 of face sheet 18 .
- the face sheet material can be provided in a web by unfolding from a stack of folded face sheet material, instead of unrolling from a roll.
- the face sheet material can have a corrugated medium 20 covered by a single linerboard, or covered by linerboards on both sides, for example.
- the production line 30 is continuously fed in face sheets 18 since the face sheets are provided in webs.
- a new roll 44 , 46 is supplied to the production line 30 when the face sheet web 18 of a previous roll 44 , 46 has been totally consumed.
- the face sheets 18 are carried along the production line 30 with carriers such as driven rolls, as it will be described in more detail below.
- the honeycomb material 14 is provided in a collapsed state to form the core portion 12 .
- the honeycomb material 14 is previously manufactured with a technology known by those skilled in the art.
- collapsed blocks 52 of honeycomb material 14 can be obtained by printing glue lines on a plurality of flat sheets (not shown). A stack of these sheets can be made, the glue be cured, and slices be cut from these blocks 52 .
- the sheets are pulled apart in the direction perpendicular to the planes of the constituent strips, i.e. in the expansion direction, thus expanding into an open cellular state having, usually, an hexagonal cell configuration.
- the honeycomb material 14 is provided in a collapsed state since it does not have linerboards 16 laminated thereon to maintain it in the expanded state. Webs of honeycomb material 14 are continuously supplied to the production line 30 .
- the web of honeycomb material 14 is provided in the collapsed state on pallets (not shown).
- the pallets carrying honeycomb material 14 are conveyed toward an hydraulic table 56 ( FIGS. 7 and 8 ) with a conveyor 58 ( FIGS. 7 and 8 ).
- the hydraulic table 56 moves vertically to adjust the height of the pallet.
- the hydraulic table 56 can tilt to a predetermined angle to facilitate the expansion of the honeycomb material 14 .
- the hydraulic table 56 is tilted to a 30-degree angle.
- the honeycomb material 14 is then expanded on an expanding table 60 ( FIGS. 7 and 8 ).
- the expanding table 60 is equipped with two expanding rolls 62 , which are preferably scored. Expanding rolls 62 are disposed on each side of the honeycomb material 14 . The height of the expanding rolls 62 can be adjusted according to the thickness of the honeycomb material 14 .
- the expanding table 60 also includes two curved guides 66 ( FIG. 7 ). While going through the curved guides 66 , the width of the honeycomb material 14 is reduced and, in combination with the expanding rolls 62 , the honeycomb material 14 is expanded. The expanding rolls 62 draw and expand to a predetermined degree the collapsed honeycomb material 14 .
- the expanding rolls 62 are preferably driven rolls and carry the web of honeycomb material 30 along the production line 30 . Expanding rolls 62 also supply the expanded honeycomb material 14 to a pair of adhesive rolls 68 disposed on each side of the honeycomb material 14 .
- the expanded honeycomb material 14 is then introduced between the two adhesive rolls 68 where an adhesive is applied on both faces 34 a , 34 b of the expanded honeycomb material 14 .
- Each adhesive roll 68 is continuously supplied in the adhesive to apply homogeneously a predetermined quantity of adhesive on each face 34 a , 34 b of the honeycomb material 14 .
- Any other technique known by those skilled in the art can be used to apply the adhesive on the faces 34 a , 34 b of the honeycomb material 14 . If the composite material 10 a includes only one face sheet 18 , the adhesive is applied on only one face 34 a of the expanded honeycomb material 14 and the face sheet 18 is applied on the face 34 a wherein the adhesive has previously been applied.
- the adhesive can be applied on a face 22 of the face sheets 18 , the face 22 that is in contact with the honeycomb material 14 , without departing from the scope of the invention.
- the quantity of adhesive required to bond the face sheets 18 on the core portion 12 is typically more important.
- the adhesive rolls 68 can be driven rolls to carry the web of honeycomb material 14 or the web of face sheets 18 along the production line 30 .
- Both face sheets 18 are carried close to the honeycomb material 14 after adhesive rolls 68 , one face sheet 18 on each side of the honeycomb material 14 .
- the face sheets 18 circulate parallel to the honeycomb material 14 .
- the face sheets 18 are carried along with a plurality of rolls 50 disposed at various positions (only one is shown). Some of the rolls 50 can be driven rolls.
- the face sheets 18 are laminated on the honeycomb material 14 with two insertion rolls 80 , one roll 80 disposed on each side of the honeycomb material 14 . As it is seen in FIG. 5 , each face sheet 18 is inserted between the insertion roll 80 and the honeycomb material 14 .
- the insertion roll 80 applies a slight pressure on the face sheet 18 and the honeycomb material 14 to create a link between both and produce the composite material 10 a without excessively compressing any of them. Insertion rolls 80 can also be driven rolls to carry the web of composite material 10 a along the production line 30 .
- the composite material 10 a can then circulate between two heating plates (not shown) wherein the adhesive is heated to activate its adhesive properties.
- the adhesive is heated to approximately 215° C.
- One heating plate can be disposed on each side of the composite material 10 a .
- the heating plates can be replaced by several heating systems and apparatus such as electric plates, steam plates, gas or electric infrared heaters, microwaves, and a warm air flow.
- the composite material 10 a goes between two compression conveyors 96 wherein the honeycomb material 14 and the face sheets 18 are maintained together permitting the adhesive to set.
- the composite material 10 a is maintained in the compression conveyors 96 until the adhesive is sufficiently dried and an adequate bond is formed between honeycomb material 14 and face sheets 18 .
- One compression conveyor 96 disposed on each side of the composite material 10 a .
- Each compression conveyor 96 has a rubber endless belt 98 mounted over a plurality of rolls 100 .
- the width of the compression conveyors 96 is preferably at least equal to the width of the composite material 10 a and they are sufficiently long to permit to the adhesive to set.
- the pressure applied by both two compression conveyors 96 is small in order to provide a composite material 10 a with a honeycomb material 14 that has not been excessively compressed. However, it is sufficient to maintain both face sheets 18 in continuous contact with the honeycomb material 14 to ensure an adequate adhesion of the composite material 10 a .
- the compression conveyors can also be carriers that carries the web of composite material 10 a along the production line 30 .
- any other appropriate system can be used such as flat presses or a plurality of rolls disposed on each side of the composite material 10 a .
- the system used to maintain the composite material 10 a together until the adhesive is set can be cooled down to accelerate the adhesive setting. Infrareds can also be used to accelerate the adhesive setting.
- the composite material 10 a is sent to a trim cutter unit 110 wherein the trims of the composite material 10 a are cut to obtain a composite material 10 a having a predetermined width. It is followed with a longitudinal cutter unit 112 wherein the composite material 10 a manufactured is cut longitudinally. If desired, it is also possible to cut grooves on-line to facilitate the folding of the composite material 10 a .
- a groove cutter unit 114 a saw (not shown) cuts one face sheet 18 along a predetermined length and a wheel (not shown) is used to bend the composite material 10 a at a predetermined angle, for instance 90°.
- transversal cutter unit 116 wherein pieces of the composite material 10 a having a predetermined length are produced by cutting transversally the composite material 10 a manufactured.
- the composite material 10 a can be cut on-line or off-line and the order of the cutting operations (trim cutter unit 110 , longitudinal cutter unit 112 , groove cutter unit 114 , and transversal cutter unit 116 ) can be interchanged.
- a continuous process as described hereinabove typically helps reducing manufacturing costs.
- the amount of raw material can also be reduced.
- FIG. 6 it will be seen another embodiment of a production line 130 used to manufacture the composite material 10 b ( FIG. 4 ) with a hot-melt adhesive process.
- a roll 44 of face sheet 18 having a corrugated medium 20 and one linerboard 22 laminated on one side of the corrugated medium 20 , is provided to cover a first face 34 a of the honeycomb material 14 .
- a roll 48 of linerboard 22 is also provided to cover the opposite face 34 b of the honeycomb material 14 .
- the production line 30 FIG. 5
- the face sheet 18 and the linerboard 22 can be fed to the production line 130 with driven rolls.
- Each of the face sheet 18 and the linerboard 22 are provided on one particular side of the honeycomb material 14 .
- the honeycomb material 14 is provided in a collapsed state to form the core portion 12 .
- the honeycomb material 14 is supplied, expanded, and the adhesive is applied in a similar manner than for the production line 30 .
- the adhesive applied is a hot melt adhesive that does not need to be activated with heat to have adhesive properties.
- the hot melt adhesive can be applied on both faces 34 a , 34 b of the expanded honeycomb material 14 .
- the face sheet 18 and the linerboard 22 are then applied on the expanded honeycomb material 14 .
- Two compression conveyors 96 are used to maintain the face sheet 18 and the linerboard 22 in contact with the honeycomb material 14 during only few seconds since the hot melt adhesive dries rapidly. Therefore, the length of the compression conveyors 96 of production line 130 ( FIG. 6 ) can be shorter than the length of the compression conveyors 96 used in the production line 30 ( FIG. 5 ).
- the composite material 10 a , 10 b can be sent to a trim cutter unit 110 , followed with a longitudinal cutter unit 112 , and a groove cutter unit 114 , where a saw cuts the face sheet 18 along a predetermined length and a wheel is used to bend the composite material 10 b at a predetermined angle, for instance 90°. Finally, the composite material 10 b is sent to a transversal cutter unit 116 . As mentioned earlier, one skilled in the art will appreciate that the composite material 10 a can be cut on-line or off-line and the order of the cutting operations (trim cutter unit 110 , longitudinal cutter unit 112 , groove cutter unit 114 , and transversal cutter unit 116 ) can be changed.
- FIGS. 7 and 8 there is shown an apparatus 230 for manufacturing the composite material 10 b ( FIG. 4 ), in accordance with the production line 130 schematically depicted in FIG. 6 .
- a roll 44 of face sheet 18 having a corrugated medium 20 and a linerboard laminated on one side of the corrugated medium 20 , is provided to cover a first face 34 a of the honeycomb material.
- a roll 48 of linerboard 22 is also provided to cover the opposite face 34 b of the honeycomb material (not shown).
- the face sheet 18 and the linerboard 22 are fed to the production line 30 with driven rolls.
- Each of the face sheet 18 and the linerboard 22 are provided on one respective side of the honeycomb material.
- the honeycomb material is provided in the collapsed state on pallets that are conveyed toward the hydraulic table 56 with the conveyor 58 .
- the honeycomb material is then expanded on the expanding table 60 .
- the expanding table 60 is equipped with two expanding rolls 62 disposed on each side of the honeycomb material and two curved guides 66 .
- the expanding table 60 draws and expands to a predetermined degree the collapsed honeycomb material.
- Expanding rolls 62 also supply the expanded honeycomb material to a pair of adhesive rolls 68 disposed on each side of the honeycomb material.
- the adhesive rolls 68 apply the adhesive on both faces 34 a , 34 b of the expanded honeycomb material.
- the face sheet 18 and the linerboard 22 are carried close to the honeycomb material after adhesive rolls 68 .
- the face sheet 18 and the linerboard 22 circulate parallel to the honeycomb material.
- the face sheet 18 and the linerboard 22 are carried along with a plurality of rolls 50 disposed at various positions (only one is shown). Some of the rolls 50 can be driven rolls.
- the face sheet 18 and the linerboard 22 are laminated on the honeycomb material with two insertion rolls 80 , one roll 80 disposed on each side of the honeycomb material. As it is seen in FIG. 5 , the face sheet 18 and the linerboard 22 are inserted between a respective insertion roll 80 and the honeycomb material 14 .
- the composite material 10 a can then circulate between two heating plates wherein the adhesive is heated to activate its adhesive properties.
- the composite material 10 a goes between two compression conveyors 96 wherein the honeycomb material and the face sheets 18 are maintained together permitting the adhesive to set.
- One compression conveyor 96 disposed on each side of the composite material 10 a .
- Each compression conveyor 96 has a rubber endless belt 98 mounted over a plurality of rolls 100 .
- the composite material 10 b is sent to cutter units (not shown) described above.
- honeycomb material 14 can be corrugated honeycomb without departing from the scope of the invention. Furthermore, one skilled in the art will understand that the adhesive can alternately be applied on the face sheets 18 .
- the composite material produced with either the hot melt production line 130 or the conventional production line 30 can consist in any combination of at least one face sheet 18 having at least one corrugated medium 20 laminated on a honeycomb material 14 .
- linerboards 16 , 22 or face sheets 18 can be laminated on the composite material 10 a , 10 b.
- the composite material can be used for packaging applications wherein at least a portion of a container is made of the composite material.
- the core portion 12 , the face sheets 18 , and the linerboard 22 are preferably made from material which may be readily recycled using commercially available technology such as wood fiber based materials (cardboard, kraft paper, recycled paper, medium, chipboard, bleached or not, and the like).
- the material can be impregnated with a resin to improve its resistance to water, grease or fire, its gas and vapor barrier properties, its non-slip properties, and the like.
- the choice of the adhesive to join together the various components of the composite material 10 a , 10 b can also be made on the basis of recyclability.
- the adhesive must ensure a good adhesion of the core portion 12 and the face sheets 18 or the linerboard 22 , remain on the top of the honeycomb material, and bond relatively rapidly.
- Adhesives such as polyvinyl alcohol (PVA), stamp glue, dextrin, and polyurethane can be used to assembly the composite material 10 .
- Hot melt adhesives such as polyolefin and ethylene vinyl acetate (EVA) can also be used.
- the composite material is wholly recyclable. It can be used as a packaging material due to its high strength for resisting stresses and strains.
- a portion or the entirety of the wood fiber based materials forming the composite material can be covered with a metallic foil, such as an aluminum foil, or a polymer, such as polyethylene.
- the composite material can be used in building applications such as for walls, doors, tableaux, etc. The scope of the invention is therefore intended to be limited solely by the scope of the appended claims.
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Abstract
The process relates to the continuous production of a web of a composite material, comprising: providing a web of honeycomb material; providing at least one web of face sheet material having a corrugated medium with a first face covered with a linerboard and an exposed second face, including unrolling the face sheet material from a roll; carrying said web of honeycomb material and said at least one web of face sheet material along a production line; and adhesively applying the exposed second face of the at least one web of face sheet material to one face of said honeycomb material while said honeycomb material is being conveyed through the production line and maintained in an expanded state.
Description
- This application is a continuation of U.S. patent application Ser. No. 10/879,199, entitled “Process and Apparatus for Manufacturing a Honeycomb Composite Material”, and which was filed Jun. 30, 2004 by applicants, the specification of which is hereby incorporated by reference.
- The present invention relates to the field of manufacturing composite materials and, more particularly, to a process for manufacturing a honeycomb composite material. The composite material can be used for packaging and building applications, for instance.
- Safe product delivery requires a strong and efficient packaging material which can hold up under tough conditions. When selecting a packaging material, one typically considers its weight, its recyclability, its mechanical properties, and its cost.
- Foam materials are widely used since they are inexpensive and lightweight. However they are typically not recognized as being environmentally friendly. Moreover, sometimes foam materials can generate static electricity when in contact with another object. Most paper honeycomb materials are fully recyclable, lightweight, and inexpensive. Honeycomb materials probably offer the best strength to weight ratio of packaging materials. However, they are characterized by a lower compressive strength in the plane of the material (edge compression resistance). Corrugated cardboards are also fully recyclable, lightweight, and inexpensive. However, important quantities of material are necessary to produce safe containers with corrugated cardboard, which increase the packaging cost. Moreover, corrugated cardboard having anti-static properties can be obtained.
- Mass production of packaging materials calls for cost efficient and continuous productions to be competitive with existing products. Furthermore, higher than average mechanical properties are sought, to allow reducing weight and lowering raw material cost.
- According to one aspect of the present invention, there is provided a process for a continuous production of a web of a composite material, the process comprising the steps of: providing at least one web of face sheet material having a corrugated medium with a first face covered with a linerboard and an exposed second face, including unrolling the face sheet material from a roll; carrying said web of honeycomb material and said at least one web of face sheet material along a production line; and adhesively applying the exposed second face of the at least one web of face sheet material to one face of said honeycomb material while said honeycomb material is being conveyed through the production line and maintained in an expanded state.
- According to another aspect of the present invention, there is provided a packaging material manufactured with the process described hereinabove.
- According to a further aspect of the present invention, there is provided an apparatus for a continuous production of a web of a composite material. The apparatus comprises at least one carrier for moving a web of honeycomb material along the apparatus; at least one carrier for moving at least one web of a face sheet material along the apparatus, the face sheet material having a corrugated medium with a linerboard on at least one face thereof; at least one laminator for adhesively applying the at least one web of the face sheet material to a face of the web of honeycomb material in an expanded state.
- According to another aspect of the present invention, there is provided a packaging material manufactured with the apparatus described hereinabove.
- The term paper is herein intended to means any wood fiber based material such as cardboard, kraft paper, recycled paper, medium, chipboard, bleached or not, and the like, for instance.
- Further features and advantages of the present invention will become apparent from the following detailed description, taken in combination with the appended drawings, in which:
-
FIG. 1 . is a perspective view of a manually manufactured composite material according to the prior art; -
FIG. 2 is an exploded perspective view of the composite material ofFIG. 1 ; -
FIG. 3 is an exploded perspective view of a first embodiment of a composite material; -
FIG. 4 is an exploded perspective view of a second embodiment of a composite material; -
FIG. 5 is a schematic view of an example of a process for manufacturing a composite material in accordance with the first embodiment; -
FIG. 6 is a schematic view of an example of a process for manufacturing a composite material in accordance with the second embodiment; -
FIG. 7 is a top plan view of an apparatus for manufacturing a composite material; and -
FIG. 8 is a side elevation view of the apparatus ofFIG. 7 . - It will be noted that throughout the appended drawings, like features are identified by like reference numerals.
- Referring to
FIGS. 1 and 2 , acomposite material 10 typically used in packaging applications is shown. Thecomposite material 10 has acore portion 12 including an expandedhoneycomb material 14 and twolinerboards 16 laminated on thehoneycomb material 14. Thelinerboards 16 are used to maintain thehoneycomb material 14 in an expanded state. On eachlinerboard 16, aface sheet 18 is manually laminated. Theface sheet 18 has acorrugated medium 20 and twolinerboards 22, one laminated on each side of thecorrugated medium 20. Thecomposite material 10 has satisfactory mechanical properties for some packaging applications. However, the operation of manually laminating theface sheets 18 on thecore portion 12 results in relatively high manufacturing costs, and is known to limit the competitiveness of this product on the market. - Referring to
FIG. 3 , there is shown an example of honeycombcomposite material 10 a manufactured by aproduction line 30 such as shown inFIG. 5 . Thecomposite material 10 a has acore portion 12 and twoface sheets 18 laminated on thecore portion 12. In this example, thecore portion 12 has ahoneycomb material 14 in an expanded state. As opposed to the material shown inFIGS. 1 and 2 , thehoneycomb material 14 is not covered withlinerboards 16 laminated on each side. Thecore portion 12 has twofaces honeycomb material 14 have an hexagonal shape, though any other suitable shape can be used. Eachface sheet 18 includes acorrugated medium 20 having afirst face 20 a with alinerboard 22 laminated thereon, and an exposedsecond face 20 b. In this embodiment, the exposedsecond face 20 b of eachface sheet 18 is directly laminated on thehoneycomb material 14 forming thecore portion 12. Alternately to the embodiment illustrated inFIG. 3 , it will be understood that the linerboard coveredface 22, of theface sheet material 18, can be directly laminated on thehoneycomb material 14, i.e. either face 22 or 20 b of theface sheet 18 can be applied to thehoneycomb material 14. As can be appreciated, the amount of raw material used is reduced as compared to the amount of raw material used in thecomposite material 10 shown inFIGS. 1 and 2 . - Further, the
face sheets 18 can include alinerboard 22 laminated on a single side of thecorrugated medium 20, or alternately include alinerboard 22 laminated on each side of the corrugated medium. For example, referring toFIG. 4 , thecomposite material 10 b can also have asingle face sheet 18 with acorrugated medium 20 applied thereon. Theother face 34 b of thecore portion 12 can be covered with alinerboard 22 or be left uncovered, for example. - Referring to
FIG. 5 , an example of aproduction line 30 which can be used to manufacture thecomposite material 10 a (FIG. 3 ) is shown. Theproduction line 30 has alongitudinal axis 40 and a transversal axis 42 (visible inFIG. 7 ) which correspond to the longitudinal and transversal axis of thecomposite material 10 a. Thefaces sheets 18 are provided in webs. Tworolls face sheet material 18 are provided. In this example, the two rolls are similar. The corrugated medium has a first face covered with a linerboard, and a second face which is left exposed. The absence of a linerboard on the exposed, inner face, of the corrugated medium eases the rolling and unrolling of the face sheets into and from rolls. Thus, when theface sheets 18 are constituted of acorrugated medium 20 and onelinerboard 22 laminated on one side of thecorrugated medium 20, theface sheets 18 can be provided in rolls. - In the roll, the first face covered with a linerboard can be oriented either radially outwardly, or radially inwardly. Furthermore, either the covered face or the exposed face of the corrugated medium can be applied to the honeycomb material.
- Moreover, if the
composite material 10 a includes only oneface sheet 18 including thecorrugated medium 20, theproduction line 30 can have only asingle roll 44. If thecore portion 12 of thecomposite material 10 a has oneface 34 a covered with aface sheet 18 including thecorrugated medium 20 and theother face 34 b is covered with alinerboard 22, a roll 48 (FIG. 6 ) oflinerboard 22 is provided instead of aroll 46 offace sheet 18. - It will be noted that in alternate embodiments, the face sheet material can be provided in a web by unfolding from a stack of folded face sheet material, instead of unrolling from a roll. When provided in a stack, the face sheet material can have a corrugated medium 20 covered by a single linerboard, or covered by linerboards on both sides, for example.
- The
production line 30 is continuously fed inface sheets 18 since the face sheets are provided in webs. Anew roll production line 30 when theface sheet web 18 of aprevious roll face sheets 18 are carried along theproduction line 30 with carriers such as driven rolls, as it will be described in more detail below. - The
honeycomb material 14 is provided in a collapsed state to form thecore portion 12. Thehoneycomb material 14 is previously manufactured with a technology known by those skilled in the art. For example, collapsedblocks 52 ofhoneycomb material 14 can be obtained by printing glue lines on a plurality of flat sheets (not shown). A stack of these sheets can be made, the glue be cured, and slices be cut from theseblocks 52. To expand thehoneycomb material 14, the sheets are pulled apart in the direction perpendicular to the planes of the constituent strips, i.e. in the expansion direction, thus expanding into an open cellular state having, usually, an hexagonal cell configuration. However, for theproduction line 30, thehoneycomb material 14 is provided in a collapsed state since it does not have linerboards 16 laminated thereon to maintain it in the expanded state. Webs ofhoneycomb material 14 are continuously supplied to theproduction line 30. - The web of
honeycomb material 14 is provided in the collapsed state on pallets (not shown). The pallets carryinghoneycomb material 14 are conveyed toward an hydraulic table 56 (FIGS. 7 and 8 ) with a conveyor 58 (FIGS. 7 and 8 ). The hydraulic table 56 moves vertically to adjust the height of the pallet. Furthermore, the hydraulic table 56 can tilt to a predetermined angle to facilitate the expansion of thehoneycomb material 14. In a preferred embodiment, the hydraulic table 56 is tilted to a 30-degree angle. - The
honeycomb material 14 is then expanded on an expanding table 60 (FIGS. 7 and 8 ). The expanding table 60 is equipped with two expandingrolls 62, which are preferably scored. Expanding rolls 62 are disposed on each side of thehoneycomb material 14. The height of the expanding rolls 62 can be adjusted according to the thickness of thehoneycomb material 14. The expanding table 60 also includes two curved guides 66 (FIG. 7 ). While going through the curved guides 66, the width of thehoneycomb material 14 is reduced and, in combination with the expanding rolls 62, thehoneycomb material 14 is expanded. The expanding rolls 62 draw and expand to a predetermined degree thecollapsed honeycomb material 14. The expanding rolls 62 are preferably driven rolls and carry the web ofhoneycomb material 30 along theproduction line 30. Expanding rolls 62 also supply the expandedhoneycomb material 14 to a pair ofadhesive rolls 68 disposed on each side of thehoneycomb material 14. - The expanded
honeycomb material 14 is then introduced between the twoadhesive rolls 68 where an adhesive is applied on bothfaces honeycomb material 14. Eachadhesive roll 68 is continuously supplied in the adhesive to apply homogeneously a predetermined quantity of adhesive on eachface honeycomb material 14. Any other technique known by those skilled in the art can be used to apply the adhesive on thefaces honeycomb material 14. If thecomposite material 10 a includes only oneface sheet 18, the adhesive is applied on only oneface 34 a of the expandedhoneycomb material 14 and theface sheet 18 is applied on theface 34 a wherein the adhesive has previously been applied. Moreover, one skilled in the art will appreciate that the adhesive can be applied on aface 22 of theface sheets 18, theface 22 that is in contact with thehoneycomb material 14, without departing from the scope of the invention. However, in that case, the quantity of adhesive required to bond theface sheets 18 on thecore portion 12 is typically more important. - The adhesive rolls 68 can be driven rolls to carry the web of
honeycomb material 14 or the web offace sheets 18 along theproduction line 30. - Both face
sheets 18 are carried close to thehoneycomb material 14 after adhesive rolls 68, oneface sheet 18 on each side of thehoneycomb material 14. Theface sheets 18 circulate parallel to thehoneycomb material 14. Theface sheets 18 are carried along with a plurality ofrolls 50 disposed at various positions (only one is shown). Some of therolls 50 can be driven rolls. - The
face sheets 18 are laminated on thehoneycomb material 14 with two insertion rolls 80, oneroll 80 disposed on each side of thehoneycomb material 14. As it is seen inFIG. 5 , eachface sheet 18 is inserted between theinsertion roll 80 and thehoneycomb material 14. Theinsertion roll 80 applies a slight pressure on theface sheet 18 and thehoneycomb material 14 to create a link between both and produce thecomposite material 10 a without excessively compressing any of them. Insertion rolls 80 can also be driven rolls to carry the web ofcomposite material 10 a along theproduction line 30. - The
composite material 10 a can then circulate between two heating plates (not shown) wherein the adhesive is heated to activate its adhesive properties. For example, for PVA, the adhesive is heated to approximately 215° C. One heating plate can be disposed on each side of thecomposite material 10 a. One skilled in the art will appreciate that the heating plates can be replaced by several heating systems and apparatus such as electric plates, steam plates, gas or electric infrared heaters, microwaves, and a warm air flow. - Thereafter, the
composite material 10 a goes between twocompression conveyors 96 wherein thehoneycomb material 14 and theface sheets 18 are maintained together permitting the adhesive to set. Thecomposite material 10 a is maintained in thecompression conveyors 96 until the adhesive is sufficiently dried and an adequate bond is formed betweenhoneycomb material 14 andface sheets 18. Onecompression conveyor 96 disposed on each side of thecomposite material 10 a. Eachcompression conveyor 96 has a rubberendless belt 98 mounted over a plurality ofrolls 100. The width of thecompression conveyors 96 is preferably at least equal to the width of thecomposite material 10 a and they are sufficiently long to permit to the adhesive to set. The pressure applied by both twocompression conveyors 96 is small in order to provide acomposite material 10 a with ahoneycomb material 14 that has not been excessively compressed. However, it is sufficient to maintain both facesheets 18 in continuous contact with thehoneycomb material 14 to ensure an adequate adhesion of thecomposite material 10 a. The compression conveyors can also be carriers that carries the web ofcomposite material 10 a along theproduction line 30. - One skilled in the art will appreciate that even if the
compression conveyors 96 are used to maintain thehoneycomb material 14 in contact with theface sheets 18, any other appropriate system can be used such as flat presses or a plurality of rolls disposed on each side of thecomposite material 10 a. The system used to maintain thecomposite material 10 a together until the adhesive is set can be cooled down to accelerate the adhesive setting. Infrareds can also be used to accelerate the adhesive setting. - Thereafter, the
composite material 10 a is sent to atrim cutter unit 110 wherein the trims of thecomposite material 10 a are cut to obtain acomposite material 10 a having a predetermined width. It is followed with alongitudinal cutter unit 112 wherein thecomposite material 10 a manufactured is cut longitudinally. If desired, it is also possible to cut grooves on-line to facilitate the folding of thecomposite material 10 a. In agroove cutter unit 114, a saw (not shown) cuts oneface sheet 18 along a predetermined length and a wheel (not shown) is used to bend thecomposite material 10 a at a predetermined angle, for instance 90°. It is followed with atransversal cutter unit 116 wherein pieces of thecomposite material 10 a having a predetermined length are produced by cutting transversally thecomposite material 10 a manufactured. As one skilled in the art will appreciate, thecomposite material 10 a can be cut on-line or off-line and the order of the cutting operations (trimcutter unit 110,longitudinal cutter unit 112,groove cutter unit 114, and transversal cutter unit 116) can be interchanged. - A continuous process as described hereinabove typically helps reducing manufacturing costs. The amount of raw material can also be reduced.
- Referring to
FIG. 6 , it will be seen another embodiment of aproduction line 130 used to manufacture thecomposite material 10 b (FIG. 4 ) with a hot-melt adhesive process. Aroll 44 offace sheet 18, having acorrugated medium 20 and onelinerboard 22 laminated on one side of thecorrugated medium 20, is provided to cover afirst face 34 a of thehoneycomb material 14. Aroll 48 oflinerboard 22 is also provided to cover theopposite face 34 b of thehoneycomb material 14. As for the production line 30 (FIG. 5 ), in theproduction line 130 ofFIG. 6 , theface sheet 18 and thelinerboard 22 can be fed to theproduction line 130 with driven rolls. Each of theface sheet 18 and thelinerboard 22 are provided on one particular side of thehoneycomb material 14. Thehoneycomb material 14 is provided in a collapsed state to form thecore portion 12. Thehoneycomb material 14 is supplied, expanded, and the adhesive is applied in a similar manner than for theproduction line 30. In this second example, the adhesive applied is a hot melt adhesive that does not need to be activated with heat to have adhesive properties. The hot melt adhesive can be applied on bothfaces honeycomb material 14. Theface sheet 18 and thelinerboard 22 are then applied on the expandedhoneycomb material 14. Twocompression conveyors 96 are used to maintain theface sheet 18 and thelinerboard 22 in contact with thehoneycomb material 14 during only few seconds since the hot melt adhesive dries rapidly. Therefore, the length of thecompression conveyors 96 of production line 130 (FIG. 6 ) can be shorter than the length of thecompression conveyors 96 used in the production line 30 (FIG. 5 ). - After processing, the
composite material trim cutter unit 110, followed with alongitudinal cutter unit 112, and agroove cutter unit 114, where a saw cuts theface sheet 18 along a predetermined length and a wheel is used to bend thecomposite material 10 b at a predetermined angle, for instance 90°. Finally, thecomposite material 10 b is sent to atransversal cutter unit 116. As mentioned earlier, one skilled in the art will appreciate that thecomposite material 10 a can be cut on-line or off-line and the order of the cutting operations (trimcutter unit 110,longitudinal cutter unit 112,groove cutter unit 114, and transversal cutter unit 116) can be changed. - Referring to
FIGS. 7 and 8 , there is shown anapparatus 230 for manufacturing thecomposite material 10 b (FIG. 4 ), in accordance with theproduction line 130 schematically depicted inFIG. 6 . Aroll 44 offace sheet 18, having acorrugated medium 20 and a linerboard laminated on one side of thecorrugated medium 20, is provided to cover afirst face 34 a of the honeycomb material. Aroll 48 oflinerboard 22 is also provided to cover theopposite face 34 b of the honeycomb material (not shown). Theface sheet 18 and thelinerboard 22 are fed to theproduction line 30 with driven rolls. Each of theface sheet 18 and thelinerboard 22 are provided on one respective side of the honeycomb material. - As for the
production lines conveyor 58. The honeycomb material is then expanded on the expanding table 60. The expanding table 60 is equipped with two expandingrolls 62 disposed on each side of the honeycomb material and two curved guides 66. The expanding table 60 draws and expands to a predetermined degree the collapsed honeycomb material. Expanding rolls 62 also supply the expanded honeycomb material to a pair ofadhesive rolls 68 disposed on each side of the honeycomb material. The adhesive rolls 68 apply the adhesive on bothfaces - The
face sheet 18 and thelinerboard 22 are carried close to the honeycomb material after adhesive rolls 68. Theface sheet 18 and thelinerboard 22 circulate parallel to the honeycomb material. Theface sheet 18 and thelinerboard 22 are carried along with a plurality ofrolls 50 disposed at various positions (only one is shown). Some of therolls 50 can be driven rolls. - The
face sheet 18 and thelinerboard 22 are laminated on the honeycomb material with two insertion rolls 80, oneroll 80 disposed on each side of the honeycomb material. As it is seen inFIG. 5 , theface sheet 18 and thelinerboard 22 are inserted between arespective insertion roll 80 and thehoneycomb material 14. Thecomposite material 10 a can then circulate between two heating plates wherein the adhesive is heated to activate its adhesive properties. - Thereafter, the
composite material 10 a goes between twocompression conveyors 96 wherein the honeycomb material and theface sheets 18 are maintained together permitting the adhesive to set. Onecompression conveyor 96 disposed on each side of thecomposite material 10 a. Eachcompression conveyor 96 has a rubberendless belt 98 mounted over a plurality ofrolls 100. Then, thecomposite material 10 b is sent to cutter units (not shown) described above. - The
honeycomb material 14 can be corrugated honeycomb without departing from the scope of the invention. Furthermore, one skilled in the art will understand that the adhesive can alternately be applied on theface sheets 18. - The composite material produced with either the hot
melt production line 130 or theconventional production line 30 can consist in any combination of at least oneface sheet 18 having at least onecorrugated medium 20 laminated on ahoneycomb material 14. - One skilled in the art will understand that any number of
linerboards face sheets 18 can be laminated on thecomposite material - The composite material can be used for packaging applications wherein at least a portion of a container is made of the composite material.
- The
core portion 12, theface sheets 18, and thelinerboard 22 are preferably made from material which may be readily recycled using commercially available technology such as wood fiber based materials (cardboard, kraft paper, recycled paper, medium, chipboard, bleached or not, and the like). The material can be impregnated with a resin to improve its resistance to water, grease or fire, its gas and vapor barrier properties, its non-slip properties, and the like. - The choice of the adhesive to join together the various components of the
composite material core portion 12 and theface sheets 18 or thelinerboard 22, remain on the top of the honeycomb material, and bond relatively rapidly. Adhesives such as polyvinyl alcohol (PVA), stamp glue, dextrin, and polyurethane can be used to assembly thecomposite material 10. Hot melt adhesives such as polyolefin and ethylene vinyl acetate (EVA) can also be used. - Preferably, the composite material is wholly recyclable. It can be used as a packaging material due to its high strength for resisting stresses and strains.
- The embodiments of the invention described above are intended to be exemplary only. For example, a portion or the entirety of the wood fiber based materials forming the composite material can be covered with a metallic foil, such as an aluminum foil, or a polymer, such as polyethylene. The composite material can be used in building applications such as for walls, doors, tableaux, etc. The scope of the invention is therefore intended to be limited solely by the scope of the appended claims.
Claims (20)
1. A process for a continuous production of a web of a composite material, the process comprising the steps of:
providing a web of honeycomb material;
providing at least one web of face sheet material having a corrugated medium with a first face covered with a linerboard and an exposed second face, including unrolling the face sheet material from a roll;
carrying said web of honeycomb material and said at least one web of face sheet material along a production line; and
adhesively applying one of said first face and second face of the at least one web of face sheet material to one face of said honeycomb material while said honeycomb material is being conveyed through the production line and maintained in an expanded state.
2. A process as claimed in claim 1 , further comprising the step of expanding said honeycomb material from a collapsed state to said expanded state while said honeycomb material is being conveyed through the production line.
3. A process as claimed in claim 1 , wherein the step of adhesively applying said at least one web of face sheet material to one face of said honeycomb material further comprises
applying an adhesive on one of at least one face of said web of honeycomb material and a face of each of said at least one web of face sheet material;
laminating said at least one web of face sheet material on said web of honeycomb material, said adhesive being located therebetween; and
permitting said adhesive to set to keep said at least one web of face sheet material laminated with said web of honeycomb material.
4. A process as claimed in claim 3 , wherein said adhesive is applied on at least one face of said web of honeycomb material.
5. A process as claimed in claim 3 , further comprising heating said adhesive.
6. A process as claimed in claim 1 , further comprising trimming said web of composite material.
7. A process as claimed in claim 1 , further comprising cutting one of said at least one face sheet material of said web of composite material and bending said web of composite material to a predetermined angle.
8. A process as claimed in claim 1 , further comprising cutting longitudinally said web of composite material.
9. A process as claimed in claim 1 , further comprising cutting transversally said web of composite material.
10. A process as claimed in claim 1 , wherein the step of adhesively applying includes adhesively applying the exposed second face of the face sheet material to the honeycomb.
11. A process for a continuous production of a web of a composite material, the process comprising the steps of:
unrolling a face sheet material from a roll, the face sheet having a corrugated medium with a first face covered with a linerboard and an exposed second face;
carrying said unrolled face sheet material along a production line;
expanding a web of honeycomb material into an expanded state; and
adhesively applying said face sheet material to the web of honeycomb material in the expanded state.
12. A process as claimed in claim 11 , further comprising expanding said honeycomb material from a collapsed state to said expanded state while said honeycomb material is being conveyed through the production line.
13. A process as claimed in claim 11 , wherein the step of adhesively applying said at least one web of face sheet material to one face of said honeycomb material further comprises
applying an adhesive on one of at least one face of said web of honeycomb material and a face of each of said at least one web of face sheet material;
laminating said at least one web of face sheet material on said web of honeycomb material, said adhesive being located therebetween; and
permitting said adhesive to set to keep said at least one web of face sheet material laminated with said web of honeycomb material.
14. A process as claimed in claim 13 , wherein said adhesive is applied on at least one face of said web of honeycomb material.
15. A process as claimed in claim 13 , farther comprising heating said adhesive.
16. A process as claimed in claim 11 , further comprising trimming said web of composite material.
17. A process as claimed in claim 11 , further comprising cutting one of said at least one face sheet material of said web of composite material and bending said web of composite material to a predetermined angle.
18. A process as claimed in claim 11 , further comprising cutting longitudinally said web of composite material.
19. A process as claimed in claim 11 , further comprising cutting transversally said web of composite material.
20. A process as claimed in claim 11 , wherein the step of adhesively applying includes adhesively applying the exposed second face of the face sheet material to the honeycomb.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/860,081 US20080006367A1 (en) | 2004-06-30 | 2007-09-24 | Process for manufacturing a honeycomb composite material |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/879,199 US7288164B2 (en) | 2004-06-30 | 2004-06-30 | Process and apparatus for manufacturing a honeycomb composite material |
US11/860,081 US20080006367A1 (en) | 2004-06-30 | 2007-09-24 | Process for manufacturing a honeycomb composite material |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US10/879,199 Continuation US7288164B2 (en) | 2004-06-30 | 2004-06-30 | Process and apparatus for manufacturing a honeycomb composite material |
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US20080006367A1 true US20080006367A1 (en) | 2008-01-10 |
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US10/879,199 Active 2025-08-24 US7288164B2 (en) | 2004-06-30 | 2004-06-30 | Process and apparatus for manufacturing a honeycomb composite material |
US11/851,696 Abandoned US20070295457A1 (en) | 2004-06-30 | 2007-09-07 | Process and apparatus for manufacturing a honeycomb composite material |
US11/860,081 Abandoned US20080006367A1 (en) | 2004-06-30 | 2007-09-24 | Process for manufacturing a honeycomb composite material |
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US10/879,199 Active 2025-08-24 US7288164B2 (en) | 2004-06-30 | 2004-06-30 | Process and apparatus for manufacturing a honeycomb composite material |
US11/851,696 Abandoned US20070295457A1 (en) | 2004-06-30 | 2007-09-07 | Process and apparatus for manufacturing a honeycomb composite material |
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Also Published As
Publication number | Publication date |
---|---|
US20060000547A1 (en) | 2006-01-05 |
US7288164B2 (en) | 2007-10-30 |
US20070295457A1 (en) | 2007-12-27 |
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