US20100297403A1 - Laminate material - Google Patents

Laminate material Download PDF

Info

Publication number
US20100297403A1
US20100297403A1 US12/779,840 US77984010A US2010297403A1 US 20100297403 A1 US20100297403 A1 US 20100297403A1 US 77984010 A US77984010 A US 77984010A US 2010297403 A1 US2010297403 A1 US 2010297403A1
Authority
US
United States
Prior art keywords
laminate
product
resin
polyester
acrylic
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
Application number
US12/779,840
Inventor
Geoffrey Charles Thorpe
Kevin Joseph Black
Gavin Blair Watson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nu Cleer Systems Ltd
Original Assignee
Nu Cleer Systems Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from NZ54745206A external-priority patent/NZ547452A/en
Application filed by Nu Cleer Systems Ltd filed Critical Nu Cleer Systems Ltd
Assigned to NU CLEER SYSTEMS LIMITED reassignment NU CLEER SYSTEMS LIMITED ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BLACK, KEVIN JOSEPH, THORPE, GEOFFREY CHARLES, WATSON, GAVIN BLAIR
Publication of US20100297403A1 publication Critical patent/US20100297403A1/en
Priority to US13/720,722 priority Critical patent/US9168693B2/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/005Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor characterised by the choice of material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • B29C51/002Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor characterised by the choice of material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • B29C53/04Bending or folding of plates or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/308Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising acrylic (co)polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/36Layered products comprising a layer of synthetic resin comprising polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0012Mechanical treatment, e.g. roughening, deforming, stretching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • B29C51/14Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor using multilayered preforms or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/033 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/24All layers being polymeric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/40Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/40Properties of the layers or laminate having particular optical properties
    • B32B2307/412Transparent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/554Wear resistance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/718Weight, e.g. weight per square meter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/738Thermoformability
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2419/00Buildings or parts thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2479/00Furniture
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/12Ships
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1043Subsequent to assembly
    • Y10T156/1044Subsequent to assembly of parallel stacked sheets only
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495Thickness [relative or absolute]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495Thickness [relative or absolute]
    • Y10T428/24967Absolute thicknesses specified
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/26Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/269Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension including synthetic resin or polymer layer or component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31786Of polyester [e.g., alkyd, etc.]
    • Y10T428/31797Next to addition polymer from unsaturated monomers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

A self supporting curved laminate product resulting from curving of a planar precursor, wherein the planar precursor is a self supporting laminate of two sheets of an acrylic thermoplastic, or of sheets including an acrylic thermoplastic, spaced by, but attaching to, an interposed thermoset polyester system, and wherein curving has involved heating of the laminate sufficient to allow its curving without any substantial degradation of the lamination or its component layers.

Description

    CROSS REFERENCE TO RELATED APPLICATIONS
  • This application is a continuation of International Application PCT/NZ2007/000123, filed on May 22, 2007, which is incorporated by reference herein in its entirety. This application entered the National Phase in the U.S. on Nov. 21, 2008 as application Ser. No. 12/302,009.
  • FIELD OF THE INVENTION
  • The present invention relates to a laminate material and the method by which it is produced. More particularly but not exclusively it relates to a laminate material having one or more internal layers of polyester resin, and its method of preparation and shaping.
  • BACKGROUND OF THE INVENTION
  • In one aspect the invention relates to the technology of building materials. Glass is a very common such material. Although it has a number of advantages, transparency being an obvious one, it has a number of disadvantages. Glass is heavy, breakable and can be difficult to manufacture and to form. The problems associated with glass include the weight, lack of insulating and sound proofing properties.
  • We propose the use of an acrylic. Many variations and types are used, mainly in signage, walkways building canopies and skylights, for example. It has medium to high impact resistance, and has good resistance to scratching. However it is still inferior to glass in a number of areas. Greater thickness is required over certain dimensions and spans in comparison to glass.
  • Any discussion of documents, acts, materials, devices, articles or the like which has been included in the present specification is solely for the purpose of providing a context for the present invention. It is not to be taken as an admission that any or all of these matters form part of the prior art base or were common general knowledge in the field relevant to the present invention, as it existed before the priority date.
  • It is an object of the present invention to provide a laminate material of self-supporting character and preferably having one or more superior properties over glass, particularly when used as a construction or manufacturing material.
  • Additionally or alternatively it is an object of the present invention to provide a laminate material, which can be shaped or formed.
  • Additionally or alternatively it is an object of the present invention to provide a novel method of preparing a laminate material.
  • Additionally or alternatively it is an object of the present invention to provide a laminate material that at least provides the public with a useful choice.
  • Other objects of the invention may become apparent from the following description, which is given by way of example only.
  • SUMMARY OF THE INVENTION
  • In an aspect the invention consists in a self supporting curved laminate product resulting from curving of a planar precursor,
  • wherein the planar precursor is a self supporting laminate of two sheets of an acrylic thermoplastic, or of sheets including an acrylic thermoplastic, spaced by, but attaching to, an interposed thermoset polyester system,
  • and wherein curving has involved heating of the laminate sufficient to allow its curving without any substantial degradation of the lamination or its component layers.
  • Preferably said heating has been into the range of from 105° C. to 120° C.
  • Preferably one or both sheets is of an acrylic plastic or is at least primarily acrylic plastic.
  • Preferably said polyester system has been prepared at least in part from (A) carboxylic acid(s) or dicarboxylic acid(s) with (B) a component or components providing (a) hydroxyl(s) and/or dihydroxyl(s).
  • Preferably said polyester system involves a co-reactive monomer.
  • A preferred co-reactive monomer is styrene or a styrene derivative or analogue.
  • Preferably the co-reactive monomer is styrene or a styrene analogue that is present in the polyester system in a quantity from 30-55% w/w and most preferably, if styrene, 35-45% w/w.
  • Preferably the system when cured has an elongation at break greater than 150% (preferably greater than 170%).
  • Preferably the unsaturated polyester resin containing ethylenic unsaturation is present in the range of from 45-70% w/w.
  • Preferably the polyester system is or has been catalysed by free radical initiators, eg; a chemical initiator not reliant upon UV light. Alternatively, it can have been catalysed by a UV initiator of free radicals.
  • Preferably the polyester system has included or includes a metal salt provider to speed gel time upon initiation. This is particularly the case if a peroxide free radial initiator such as a MEKP is utilised (Methyl Ethyl Ketone Peroxide).
  • Preferably the level of said metal salt promoter is of the same order of or is less than the level of inclusion of any such initiator.
  • Preferably the level of any such initiator is no more than about 2% w/w of the system prior to the thermoset.
  • Preferably the level of such an initiator is less than 1% w/w of the thermoset system.
  • Preferably the lamination of the cursor laminate has involved the laying between the sheets, or the laying on one sheet and subsequent placement of the second sheet, of a liquid polyester system and thereafter allowing its thermoset.
  • Preferably the polyester resin system was a mix of:
      • 45-70% w/w unsaturated polyester resin containing ethylenic unsaturation,
      • 30-55% w/w styrene,
      • less than 2% w/w catalyst (eg; MEKP), and
      • less than 2% w/w initator (eg; metal salt provider).
  • Preferably the polyester resin system was mixed in the temperature range 18 to 22° C. (preferably about 20° C.). Preferably the polyester resin system sets at temperature(s) in the range 20° C. to 24° C. (preferably 22° C.).
  • Preferably the polyester resin system was mixed at a humidity in the range 57% to 67% (preferably about 62%). Preferably the resin is allowed to thermoset as a result of chemical initiation and its exothermicity at a humidity in the range of from 57% to 75% (preferably 62% to 73%) (eg; about 67%).
  • Preferably that surface of the acrylic plastic which is to interface with the polyester system is a clean face, ie; free of release agents and/or migrating materials from any removed cover sheet.
  • Preferably the surface of the sheets has been subjected to cleaning with a solvent.
  • Preferably said sheets have had the surface thereof to be presented to the polyester system, prior to its thermoset, cleaned with isopropyl alcohol.
  • Preferably said “without any substantial degradation” has involved some deformation of each layer but has not lead to any substantial detachment of the polyester system attachment to each said sheet.
  • Preferably throughout the curving process the interposed polyester system has remained non liquid, ie; has stretched, deformed, slipped and/or otherwise changed in shape without manifesting liquid characteristics, eg; as if it were a rubber or like material.
  • Preferably said interposed thermoset polyester system is of an unsaturated polyester system containing ethylenic unsaturation that has been linked with a coreactive monomer.
  • Preferably the polyester system is one which (without wishing to be limited to a theory) provides an attachment to each sheet as a result of either or both
      • cross linking with any free unsaturation in the acrylic material
      • free monomer solvation of the acrylic material.
  • Preferably there is both chemical, (ie; said cross linking) and physical adhesive (ie; free monomer solvation of the acrylic material) attachment.
  • Preferably said polyester system has thermoset to a non tacky form at its interface with the acrylic material and it is only where there is air access to the material that there is a residual tackiness. Preferably the material has a pliable physical character at ambient temperatures.
  • Optionally the polyester system includes one or more of pigmentation(s), fire retardant additive(s) and filler(s).
  • Preferably the laminate is transparent.
  • Preferably the acrylic sheet(s) have been mixed and/or cured at about 20° C. and/or about 65% humidity.
  • In another aspect the invention consists in a self supporting laminate product comprising or including two sheets of an acrylic thermoplastic, or of sheets including an acrylic thermoplastic, spaced by, but attaching to, an interposed thermoset polyester system, the interposed polyester system being of some or all of, or at least,
  • Preferably one or both sheets is of an acrylic plastic or is at least primarily acrylic plastic.
  • Preferably styrene is present at 35-45% w/w.
  • Preferably the system when cured has an elongation at break greater than 150% (preferably greater than 170%).
  • Preferably the polyester system is or has been catalysed by free radical initiators, eg; a chemical initiator not reliant upon UV light. Alternatively, it can have been catalysed by a UV initiator of free radicals.
  • The polyester system has preferably included or includes a metal salt provider to speed gel time upon initiation. This is particularly the case if a peroxide free radial initiator such as a MEKP is utilised (Methyl Ethyl Ketone Peroxide).
  • Preferably the level of said metal salt promoter is of the same order of or is less than the level of inclusion of any such initiator.
  • Preferably the level of any such initiator is no more than about 2% w/w of the system prior to the thermoset.
  • Preferably the level of such an initiator is less than 1% w/w of the thermoset system.
  • Preferably the lamination of the cursor laminate has involved the laying between the sheets, or the laying on one sheet and subsequent placement of the second sheet, of a liquid polyester system and thereafter allowing its thermoset.
  • Preferably the polyester resin system was a mix of:
      • 45-70% w/w unsaturated polyester resin containing ethylenic unsaturation,
      • 30-55% w/w styrene,
      • less than 2% w/w catalyst (eg; MEKP), and
      • less than 2% w/w initator (eg; metal salt provider).
  • Preferably the polyester resin system was mixed in the temperature range 18 to 22° C. (preferably about 20° C.). Preferably the polyester resin system sets at temperature(s) in the range 20° C. to 24° C. (preferably 22° C.).
  • Preferably the polyester resin system was mixed at a humidity in the range 57% to 67% (preferably about 62%). Preferably the resin is allowed to thermoset as a result of chemical initiation and its exothermicity at a humidity in the range of from 57% to 75% (preferably 62% to 73%) (eg; about 67%).
  • Preferably that surface of the acrylic plastic which is to interface with the polyester system is a clean face, i.e.; free of release agents and/or migrating materials from any removed cover sheet.
  • Preferably the surface of the sheets has been subjected to cleaning with a solvent.
  • Preferably said sheets have had the surface thereof to be presented to the polyester system, prior to its thermoset, cleaned with isopropyl alcohol.
  • Preferably said “without any substantial degradation” has involved some deformation of each layer but has not lead to any substantial detachment of the polyester system attachment to each said sheet.
  • Preferably the laminate can be subjected to a curving process under non destructive heating during which the interposed polyester system remains non liquid, i.e.; can stretch, deform, slip and/or otherwise change in shape without manifesting liquid characteristics, eg; as if it were a rubber or like material.
  • Preferably the polyester system is one which (without wishing to be limited to a theory) provides an attachment to each sheet as a result of either or both
      • cross linking with any free unsaturation in the acrylic material
      • free monomer solvation of the acrylic material.
  • Preferably there is both chemical, (i.e.; said cross linking) and physical adhesive (i.e.; free monomer solvation of the acrylic material) attachment.
  • Preferably said polyester system has thermoset to a non tacky form at its interface with the acrylic material and it is only where there is air access to the material that there is a residual tackiness. Preferably the material has a pliable physical character at ambient temperatures.
  • Optionally the polyester system includes one or more of pigmentation(s), fire retardant additive(s) and filler(s).
  • Preferably the laminate is transparent.
  • Preferably the acrylic sheet(s) have been mixed and/or cured at about 20° C. and/or about 65% humidity.
  • In another aspect the invention is a self supporting transparent laminate able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form, the laminate being of a transparent polyester system interposed and attaching to flanking transparent thermoplastic layers (the same or different), which thermoplastic layers attach to the polyester system by both
      • cross linking with any free unsaturation in the acrylic material
      • free monomer solvation of the acrylic material.
  • In another aspect the invention is a self supporting transparent laminate able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form, the laminate being of a transparent polyester system interposed and attaching to flanking transparent acrylic thermoplastic layers (the same or different).
  • In another aspect the invention is a self supporting transparent laminate greater than 3 mm thick able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form, the laminate being of a transparent polyester system interposed and attaching to flanking transparent thermoplastic layers (the same or different), the polyester system being at least 0.5 mm thick.
  • The polyester system can account for from 5% to 40% of overall laminate thickness.
  • Preferably in any of the foregoing laminates the polyester system layer is at least 1 mm thick (preferably from 1 to 3 mms thick, eg; about 2 mm)
  • Preferably the acrylic sheet(s) is (are) at least 0.5 mm thick. More preferably from 0.5 to 5 mm thick (eg; about 2 mm)
  • The laminates can be symmetric as to pairing of the acrylic layers (thickness and/or material), or not. They can be asymmetric.
  • The laminates can also, or instead, be symmetric three, five, seven or more layered panels, or not. A five layer laminate would have two polyester system layers.
  • In another aspect the invention is a self supporting transparent planar laminate (preferably able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form), the laminate being of a transparent polyester system interposed and attaching to flanking transparent acrylic thermoplastic layers (the same or different) (ie; a symmetric three layer system where the acrylic layers are symmetric with each other and, also preferably of the same thickness as the polyester, the laminate system having a performance related to a notional variant having acrylic layers 2 mm thick on the outside and a polyester system 2 mm thick, being able without fracture and/or delamination to withstand a challenge loading in excess of 40 tonnes into its edges, on its minor axis if notionally a rectangle of 960×470 mms.
  • By way of example a polyester resin system in the form of
      • 45-70% w/w unsaturated polyester resin containing ethylenic unsaturation,
      • 30-55% w/w styrene,
      • less than 2% w/w catalyst (eg; MEKP), and
      • less than 2% w/w initator (eg; metal salt provider), and
      • a thickness of 2 mm, 2 mm and 2 mm through the three layer laminate, when a rectangular panel of 960×470 mm squeezed on its minor axis can withstand without delamination between 60 and 80 tonnes.
  • The present invention therefore envisages laminates analogous to such performing laminates whether to be used in a planar form or in a curved form.
  • In another aspect the invention is a transparent laminate of at least three layers to an overall thickness of greater than 3 mm wherein a polyester resin system as a layer attaches to each of two acrylic layers the polyester resin system interposes.
  • In another aspect the invention is a transparent laminate of at least three layers to an overall thickness of greater than 3 mm wherein a polyester resin system as a layer attaches to each of two acrylic layers the polyester resin system interposes, the laminate being able to be curved under non destructive heating to a curved self supporting transparent form.
  • In another aspect the invention is a transparent laminate of at least three layers to an overall thickness of greater than 3 mm wherein a polyester resin system as a layer attaches to each of two acrylic layers the polyester resin system interposes, wherein the laminate is of any of the kinds previously defined.
  • In another aspect the invention is the use or methods of use and resulting structures of any planar and/or curved laminates as aforesaid.
  • In another aspect of the invention there is provided a laminate comprising:
      • a) a first thermoplastic layer,
      • b) a second thermoplastic layer, and
      • c) a thermoset resin layer intermediate between the first and second layers, wherein the thermoset layer is bonded to both layers and wherein there is a degree of cross linked bonding between the resin and the thermoplastic layers.
  • Preferably the thermoset resin is an unsaturated polyester resin. More preferably the thermoset resin, prior to curing, is a solution of a polyester in a monomer. Preferably the cross linked bonding is between the monomer and unsaturated sites available for bonding in the thermoplastic layers.
  • Preferably the monomer is styrene.
  • Preferably the resin has 30-45% styrene content.
  • Preferably the resin has an elongation at break of >150%; more preferably it has an elongation at break of around 170%. Preferably the resin has a glass transition temperature less than ambient temperature.
  • Preferably the styrene of the resin softens the surface of the thermoplastic layers allowing some degree of penetration of the resin into the thermoplastic layers.
  • In one embodiment at least one or both of the thermoplastic layers is polyethylene terphthalate glycol. In an alternative embodiment at least one or both of the thermoplastic layers is acrylic.
  • Preferably when the thermoplastic layer(s) is/are acrylic there is cross linking between unsaturated methyl methacrylate in the acrylic with the styrene monomer of the resin.
  • Preferably the resin has been catalysed by the addition of a free radical inhibitor; more preferably by the addition of a methylethyl ketone peroxide catalyst.
  • Preferably the acrylic is Polymethyl methacrylate (PMMA) or poly(methyl 2-methylpropenoate); preferably it is SHINKOLITE™ acrylic from Mitsubishi Rayon Japan.
  • Preferably the thermoplastic layer(s) have a degree of styrene resistance; preferably a high degree of styrene resistance. Alternatively or additionally the thermoplastic layer(s) have a styrene resistant surface coating.
  • Optionally the thermoplastic sheet(s) may be treated with one or more of the following:
      • a mar resistant coating
      • solar protective additives (added after preparation or in its resin state upon preparation)
      • texturing/etching/embossing/paint
      • applied photographic imagery, transfers or reflective mirror coatings
      • vinyls and metallic materials such as aluminium can be bonded and pressed onto outer surfaces
      • an annealing process
  • Optionally the thermoset resin may include or be treated with one or more of the following:
      • pigmentation
      • fire retardant additives
      • filler materials.
  • Preferably the laminate of the invention is substantially transparent with a TV (rating total visible light) close to 100%.
  • Preferably when the thermoplastic sheet(s) is/are acrylic, they have been mixed under the pour conditions of around 20° C. temperature and around 65% humidity, and cured at around 20° C. and around 65% humidity.
  • In another aspect of the invention there is provided a method of preparing a laminate comprising the steps of:
      • providing resin precursor materials,
      • adding a catalyst the resin precursor materials to give a catalysed thermoset resin,
      • inserting a layer of the catalysed thermoset resin between two thermoplastic layers, and
      • allowing the catalysed thermoset resin (the resin) to bond to the two thermoplastic layers,
  • wherein the step of allowing the resin to bond to the thermoplastic layers includes allowing the resin to cross link with the thermoplastic layers.
  • Preferably the catalysted thermoset resin formed in the first step is an unsaturated polyester resin; more preferably of a polyester in styrene monomer. Preferably the resin has 30-45% by weight styrene content. Preferably the resin has an elongation at break of >150%. Preferably the resin has a glass transition temperature less than ambient temperature.
  • Preferably the step of bonding includes cross linking between the thermoplastic layers and the styrene monomer of the resin. Preferably the step of bonding further includes softening of the surface of the thermoplastic layers by the styrene and a degree of penetration of the resin into the thermoplastic layers.
  • In one preferred form the thermoplastic layers are acrylic layers and the step of bonding includes cross linking between the styrene monomer of the resin with unsaturated methyl methacrylate sites of the acrylic.
  • In one embodiment the method is a batch process and the step of inserting a layer of the resin between two thermoplastic layers comprises pouring liquid (prior to gelation or curing) resin between two supported thermoplastic sheets and allowing to cure.
  • In an alternative embodiment the method is a continuous process and the step of inserting a layer of the resin between two thermoplastic sheets comprises advancing a first sheet or layer of the resin through a laminating station where at least one or preferably two of the thermoplastic layers contact the sheet or layer of resin.
  • In one form of the embodiment the resin is in a pre-gel state.
  • In another form of the embodiment the resin is in a gel-like state, at or near gelation of the resin.
  • In another form of the embodiment the resin is in a cured state and the step of advancing the resin may include heating the resin and/or one or both of the thermoplastic sheets to at least soften the resin and/or one or both of the thermoplastic sheets, prior to, or at about the same location as, or after, the laminating station.
  • In a further aspect there is provided a laminate material prepared according the above method.
  • In a further aspect of the invention there is provided a method of producing a curved laminate material comprising the steps of:
      • providing a laminate as hereinbefore described or produced according to the abovementioned method, wherein the thermoset resin has an elongation at break of >150% and a glass transition temperature less than ambient temperature,
      • heating a shaping region of the laminate to a shaping temperature,
      • shaping the laminate to the desired curvature,
      • cooling the laminate,
  • wherein the step of heating the shaping zone of the laminate comprises heating substantially through all layers (including the thermoset and thermoplastic layers) of the laminate in the shaping zone.
  • Preferably the step of heating the shaping region comprises applying heat to the shaping region from both a top surface of the laminate in the shaping region, and a bottom surface of the laminate in the shaping region.
  • Preferably the conditions of the heating step, including one or both of the shaping temperature and the duration of the heating, is/are not sufficient to result in annealing of any of the layers of the laminate in the heating region.
  • Preferably the step of cooling the shaping region comprises allowing the laminate to cool to ambient temperature.
  • Preferably the step of shaping the laminate comprises placing the substrate over a mould or template and applying pressure (which may simply be gravity) to one or more regions of the laminate adjacent the shaping region.
  • In a further aspect there is provided a curved laminate material or article incorporating a region of curved laminate prepared according the above method.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The invention will now be described by way of example only and with reference to the drawings in which:
  • FIG. 1 illustrates a perspective end view showing a transparent laminate constructed with principles of the present invention;
  • FIG. 2 illustrates a perspective end view showing a transparent multiple ply constructed with principles of the present;
  • FIG. 3 illustrates the molecular characteristics of the unsaturated polyester resin before the laminated sheet is thermoformed into shape;
  • FIG. 4 illustrates the molecular characteristics of the unsaturated polyester resin when the laminated sheet is thermoformed into one desired shape;
  • FIG. 5 illustrates the use of fire retardant and foamed resin materials;
  • FIG. 6 preferred thermoforming heating process;
  • FIGS. 7 a, 7 b, 7 c illustrates side views of the jig of Example 3;
  • FIGS. 8 a and 8 b illustrates part of the process of Example 3;
  • FIG. 9 illustrates delamination; due to absorption of resin into incorrect rubber type dam seal;
  • FIG. 10 illustrates light travel in the laminate of the invention;
  • FIG. 11 illustrates one form of continuous manufacturing.
  • DEFINITIONS
  • As used herein the term “and/or” means “and” or “or”, or both.
  • As used herein “(s)” following a noun means the plural and/or singular forms of the noun.
  • “The term “comprising” as used in this specification and claims means “consisting at least in part of”; that is to say when interpreting statements in this specification and claims which include “comprising”, features, other than those prefaced by this term in each statement, can also be present. Related terms such as “comprise” and “comprised” are to be interpreted in similar manner.”
  • As used herein is apparent that the term “thermoset” in respect of the polyester system encompasses a chemical initiated and/or UV light initiated polymerisation between the unsaturated polyester resin with its ethylenic unsaturation and the coreactive monomer(s). Once there has been such a thermoset, even if still to a pliable form (preferably non-tacky when excluded from ambient air), the material nonetheless can be deformed at the elevated temperature (i.e.; above ambient) required or chosen for reshaping of the thermoset acrylic material sheets without any substantial degradation of the laminate including the attachment of the polyester system to the acrylic material.
  • As used herein the term “curving” (and any derivative thereof eg; “curve” or “curved”) encompasses any mechanical manipulation of the precursor laminate that provides a three dimensional out come from the planar laminate eg; a curve of any shape, any bulge, any fold, etc. and includes part only of the overall precursor laminate sheet or all of it.
  • As referred to herein the term “laminate” preferably refers to a planar or curved sheet where the outer sheets (eg; of thermoplastic) and the interposed material of the polyester system is substantially coextensive. In some applications however this need not be the case, i.e.; there can, if desired, be unmatching of the outer sheets with respect to each other and/or one or both of the outer sheets with respect to the extent of the interposed polyester system, eg; if desired, some parts of an overall laminate could have direct fixing of one outer sheet to the other whilst other regions thereof have the polyester system interposed between such sheets.
  • As used herein, the term “forming” refers to any process by which the shape of a sheet is altered and includes, but is not limited to, bending, shaping, stretching, compressing, curving or arching a sheet.
  • As used herein, the term “styrene resistance” refers to the ability of the thermoplastic sheet(s) to resist the corrosive effect/attack of styrene. It is likely to relate to the resistance of the sheet to solubilisation by or in styrene. Styrene is present for example in one preferred thermoplastic resin.
  • As used herein, the term “transparency” refers to allowing of light to pass through the glazing without causing distortion, loss of clarity, or altering light transmission.
  • As used herein, the term “haze” refers to dullness or cloudiness. This can occur due to incompatibility of a resin with the outer sheets. For example the inner surface of the sheet becomes stressed and can react by separating its surface, and in severe cases complete delamination.
  • “Elongation” or “Elongation at break” is a standard measure for the amount a sample can stretch as a percentage of original length before it fails or breaks.
  • “Glass transition temperature” in respect of the resin means the temperature at which a reversible change occurs in the resin to undergo a rather sudden transition from a hard, glassy, or brittle condition to a flexible or elastomeric condition.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
  • This invention relates to a laminate material comprising a layer of thermoset resin inserted between two or more thermoplastic sheets. The preferred thermoplastic sheets are of acrylic, or polyethylene terphthalate glycol (P.E.T.G.).
  • FIG. 1 illustrate such a laminate, with outer sheets 1, of acrylic, or P.E.T.G. and an inner layer 2 of resin. The thickness of the laminate when complete can vary depending on the thickness of the resin inserted between the thermoplastic sheets and also to the number and thickness of thermoplastic sheets and resin employed. FIG. 2 illustrates such a multi-ply laminate.
  • There have been several attempts to provide laminates using various forms of plastic sheets and protective coverings. Although this invention was initially developed as an alternative to glass for use in the building and construction industry, the invention has wide reaching applications as a result of the lightweight, extreme strength and formability of the laminate panel. For example, the panel can be formed or worked to construct boat hulls, vehicle construction including monocoque assembly and outside panels, furniture, household appliances and a wide variety of manufactured goods. It should therefore be regarded as a construction and manufacturing material.
  • The simplest embodiment of the laminate material of the invention is a single layer of thermoset polyester resin sandwiched between two layers of thermoplastic acrylic, or P.E.T.G. (as illustrated in FIG. 1).
  • One preferred method of preparing the laminate sheet is a continuously manufactured process by which the two sheets are brought together and injected with the unsaturated polyester resin at the correct temperature and humidity required for the resin curing process. The resin is bonded with the outer sheets. One alternative method of preparation is a batch process involving assembling the two outer sheets in a parallel arrangement in a jig or equivalent, and pouring or injecting the resin between the sheets.
  • Another alternative is to manufacture the resin to the required thickness in sheet form, or in continuous form. The continuous resin can be then rolled and stored onto a drum ready for introduction to manufacturing process. When ready the two outer thermoplastic sheets can be heated and pressed either side of the solidified resin (which may have been heated) to create a solid ply. The bonding between the resin and sheets must be controlled accordingly.
  • One further aspect of the invention relates to a method of forming or shaping the laminate and the ability of the laminate to be formed. Once prepared the laminate is then heated to a temperature, at which the laminate can be formed or shaped, and then forming or shaping the laminate to a desired curvature and configuration. This invention includes the forming of a laminate in both single and complex curvatures. For example, a curvature shape, a corrugation shape and a 90° angle are achievable with the present invention after a thermoforming procedure.
  • a) Thermoplastic Sheets
  • The preferred outer sheets of the laminate can be of acrylic or P.E.T.G. sheeting.
  • By acrylic we mean a material composed of various clear, thermoplastic resins obtained from acrylic acid and its derivatives, and from raw natural sources such as petroleum and natural gas. moulded, and thermoformed. By P.E.T.G. we mean glycol-modified terephthalate glycol.
  • All of the above preferably have inherent chemical resistance to the styrene as one preferred thermoset resin contains styrene. Sheets that have insufficient styrene resistance (i.e. are likely to dissolve in or disintegrate upon contact with, styrene) are subject to poor adhesion, break down of the sheet surface due to the corrosive reaction build up on the contact face to be bonded.
  • An alternative approach to the styrene resistance requirement is the use of a styrene resistant coating on the sheeting prior to exposure to the resin. This is a protective coating acting as a barrier between the sheeting and the resin, as would be contemplated by one skilled in the art.
  • Standard acrylic plastic sheet is a more cost effective material with good optical properties, and less resistant to scratching in comparison to P.E.T.G. Further, the less cross linked the acrylic structure, the more suitable for the laminate of the invention as the free methyl methacrylate sites can cross link with the resin as discussed below. However, all materials are employed within the scope of the invention. The laminate can contain two (or more) layers of acrylic; or two (or more) layers of P.E.T.G.
  • b) The Resin Material
  • As would be known by one skilled in the art there are a number of thermoset resins which are capable of bonding two thermoplastic sheets together. However the resin suitable for the laminate of the invention must have the following characteristics—
      • An unsaturated polyester resin
      • Elongation at break characteristics sufficient to allow thermoforming of the laminate. Preferably an elongation over 150%; more preferably an elongation of around 170% or higher.
      • A low glass transition temperature, which is less than ambient temperature.
      • The preferred use of styrene as the monomer. Preferred styrene content is in the range 40-45%. Most polyester resins are viscous, pale coloured liquids consisting of a solution of a polyester in a monomer. The addition of styrene in amounts of up to 50% helps to make the resin easier to handle by reducing its viscosity. The styrene also performs the vital function of enabling the resin to cure from a liquid to a solid by ‘cross-linking’ the molecular chains of the polyester, without the evolution of any by-products. In the case of the current laminate invention we believe the styrene also has the role of softening the thermoplastic layers of the outer sheeting thereby assisting in the bonding process. In the case of acrylic sheeting the styrene may also be cross linking with unsaturated methyl methacrylate sites.
      • For use in moulding, a polyester resin can benefit from the addition of several ancillary products. In particular a catalyst is required in the invention. The catalyst is added to the resin system shortly before use to initiate the polymerisation reaction. The catalyst does not take part in the chemical reaction but simply activates the process. Accelerators may also be used to speed up the curing process.
  • Upon addition of the catalyst, in the presence of the styrene, the styrene cross-links the polymer chains in a polymerisation process, to form a complex three-dimensional network. This is the curing process.
  • Care is needed in the preparation of the resin mix prior to moulding. The resin and any additives must be carefully stirred to disperse all the components evenly before the catalyst is added. This stirring must be thorough as any air introduced into the resin mix affects the quality of the final moulding. This is especially so when laminating with layers of reinforcing materials as air bubbles can be formed within the resultant laminate which can weaken the structure. It is also important to add the accelerator (if any) and catalyst in carefully measured amounts to control the polymerisation reaction to give the best material properties. Too much catalyst will cause too rapid a gelation time, whereas too little catalyst will result in under-cure.
  • An alternative monomer to styrene is methyl methacrylate. This is also within the scope of the invention.
  • Preferred Resin
  • One preferred resin we use is NC007 resin. This is a flexible, low viscosity, clear unsaturated polyester resin in styrene monomer. It is preferably prepromoted (i.e. pre-mixed together and batched prior to the introduction of the catalyst). We recommend that it should be gelled and cured with between 0.75 and 2% of a medium reactivity MEKP catalyst. MEKP (Methyl Ethyl Ketone Peroxide, a free radical initiator) is the catalyst added to polyester resins and vinyl ester resins. As the catalyst mixes with the resin, a chemical reaction occurs (as mentioned previously), creating heat, which cures (hardens) the resin.
  • NC007 TYPICAL LIQUID PROPERTIES:
    Viscosity @ 25° C. 1.5 ps
    Gel time @ 25° C. 1% MEKP 45 minutes
    Volatile content 36%
    Appearance Clear pale pink
  • NC007 TYPICAL PHYSICAL PROPERTIES:
    % elongation at break 170%
    Tensile strength 3.2 mPa
  • The performance and characteristics of this resin during thermoforming is crucial to the success of the laminate.
  • Our preferred resin has an elongation percentage capacity of around or above 150%. This particular resin has an elongation at break of around 170%. It must be worked at between 105° C. and 120° C. At these temperatures we observe increased malleability allowing the molecules to stretch, settle, and when cooled hold their elongation and adhesion to the sheet surface. This can be shown in FIGS. 3 and 4. FIG. 3 shows the laminate structure prior to forming including resin 41 and thermoplastic layers 42.
      • (a) During the heating process the molecules of the resin begin to change shape and expand as the laminate product becomes more malleable. When the heating process begins prior to the forming and shaping process, the molecular structure of the internal resin within the laminate changes shape from being circular and honey combed to a more elongated state and stretches along the laminate surface as it is bent into shape.
      • (b) When the temperature of all layers reach the desired forming temperature of between 105° C. and 120° C. forming is commenced. The time that the temperature takes to produce the penetration required will depend on the thickness of the ply being formed. FIG. 4 illustrates the change in structure of the resin 41 and thermoplastic layers 42 upon heating.
  • The fact that the product can be laminated, then put through a thermo-forming process which involves the heating of the finished product, bending or forming into any shape, and when cooled retains its form without delamination and loss of tensile strength is a surprising outcome. The controlled environment and the factors necessary to ensure that the forming process is successful allow the laminate product to change in molecular structure at exactly the right time and effect to produce a successful and different structural outcome.
  • Catalyst for Resin Curing
  • As mentioned above, a catalyst is required to cure the resin. It acts as an initiator for curing the resin. The general catalyst type suitable for the invention is a free radical inhibitor, preferably a MEKP (methylethyl ketone peroxide catalyst). One catalyst we have used successfully is our F00826 coded Catalyst (MEKP 40%) QC. It is a MEKP catalyst, with the following components:
  • Dimethyl phthalate/dipropylene glycol phlegmatiser 30-70% 
    Methyl ethyl ketone peroxide 30%
    Methyl ethyl ketone 0-10%
    2,4-pentanedione peroxide 0-10%
  • It has a self-accelerating decomposition temperature (SADT) of approximately 60° C.
  • Gel and Cure Times; Procedure
  • Gel time refers to the point at which the catalyst and resin have crossed from an unstable liquid state to a state of at least semi hardness, or state of stability. If the early part of the curing or bonding (to the outer sheets) is disturbed then this could result in ultimate delamination. However, there is a time during the gel stage, before full cure, when the sheet may be manoeuvred, cut, and stored for a full cure time. It is important not to lift, bend or stress the sheet but rather to slide and manoeuvre the sheet along an aerated flat bed surface or flat belt feed table/conveyer.
  • The set time—refers to the point in time in which catalyst and resin complete cure and full adhesion to the sheet surfaces has occurred.
  • The time of complete cure and set will depend on the manufacturing process being used. By maximising the amount of catalyst and or accelerators and heating the NC007 system will dramatically accelerate the cure time. However whatever process is used a recommended period of 12 hours in storage prior to use.
  • c) Preparation of the Laminate
  • As mentioned previously, there are 3 main ways like laminate or the invention can be prepared. A batch process, (e.g. using a jig to hold sheets in place), a continuous process whereby the resin is poured or inserted between the sheets in a manufacturing line or alternatively using three solid sheets (two thermoplastic with the resin) and placing in contact with heating. The batch process is illustrated in the Examples. Typically in the batch process an amount of resin is mixed with the corresponding amount of catalyst using a mechanically assisted paddle. It is stirred for 2 minutes, allowed to stand for 2 minutes, or vibrated to allow excess air bubble removal. The formula is then poured directly into the cavity sample held within the cradle, a fine brass meshed funnel is used to further assist mixing and aiding in further removal of trapped air bubbles.
  • One form of continuous process could be as illustrated in FIG. 11. This involves applying two outer thermoplastic sheets to pre-mixed resin. The variants of this include using simply pre-mixed (still runny) resin; semi-set (jelly-like) resin and fully set resin which is then heated to soften and applied. The Figure illustrates a semi-set resin 121 and rolls of outer skin 122. The laminate proceeds through press rollers 123 to a mobile caterpillar pressure plate 124. An outer edge dam rubber or caterpillar rotating outer edge seal is optional (to prevent overflow of liquefied resin during manufacture).
  • It should be noted that often thermoplastic sheeting is supplied from the manufacturer with a protective plastic or paper. This can be on one or both side(s). It should be removed prior to laminate preparation.
  • d) The Bond Between the Acrylic/P.E.T.G and the Resin
  • As mentioned previously, the bond between the resin is an important feature of the invention. In the preferred embodiment the resin includes 30-45% styrene content. This styrene plays an important role in the preferred bond formation. Without being bound by the following theory we believe the presence of the styrene can soften the surfaces of the outer thermoplastic layers and allow some penetration of the resin. Further we believe it is able to cross link with the outer thermoplastic layers to create the bonding. For example with acrylic outer sheets, the styrene monomer of the resin is able to cross link with any residual methyl methacrylate sites of the acrylic.
  • e) Bending/Forming the Laminate
  • The thermoforming or shaping process is one preferred forming method. It involves forming the flat laminate sheets into the desired shape by concentrating the required heat, in and onto a particular area rather than the system of having the whole sheet oven heated. Thus a particular area of the sheet may be bent/shaped at a temperature which the acrylic, or P.E.T.G softens and the unsaturated polyester resin changes consistency such as will allow the panel or sheet to be formed into the desired shape.
  • Commonly in the art forming occurs via strip forming. This involves heating a sheet from one side, relying on one radiated heat source to pass through the entire sheet prior to bending.
  • The single side heating approach is efficient and acceptable for normal and standard non-ply sheet. However it is not preferred for our laminate (but is still possible under certain conditions).
  • The temperature and time need to penetrate our ply sheet samples is critical as an undesired annealing process can take place if the temperature is too high for too long. The time and temperature required to penetrate our ply sheet with a single heat strip forming bar/heating from one side may result in an annealing effect of the heat exposed side of the sheet resulting in crazing, shattering or snapping the outer sheet to splitting the core ply and delamination during the forming process. We use a process of directing a heat source from both top and bottom, allowing a deeper more even penetration meeting toward the core of the ply. For a particular laminate structure there will be a desired temperature and time period to bring about correct malleability and prevent an annealing of the sheet surface and delamination a and fault. It is therefore important to not exceed the correct forming temperature and time period.
  • f) Optional Features
  • i) Mar Coating
  • An optional mar coating can be used to enhance resistance to abrasive or chemical attack. While two-side coated laminate (i.e. on the outer sides of the laminate) provides maximum protection, one-sided coated laminate offers economical advantages for application where only one side of the sheet is exposed.
  • ii) UV Protection
  • We can include UV inhibitors within the thermoset resin in order to enhance the UV resistance of the laminate. The UV resistance enhances the properties of the laminate as a building material (by protecting what is inside the building) but also increases the longevity of the laminate itself.
  • iii) Colour/Tinted/Clear
  • It is possible to provide a colouring/tinting finish to the laminate by use of coloured or tinted thermoplastic sheeting. Both opaque and translucent laminates can be prepared by appropriate selection of the sheets. Alternatively transparent thermoplastic sheeting can be used and we can tint or colour the thermo set resin as would be known by one skilled in the art. Colouring of the resin mix can be carried out with pigments. The choice of a suitable pigment material, even though only added at about 3% resin weight, must be carefully considered as it is easy to affect the curing reaction and degrade the final laminate by use of unsuitable pigments.
  • iv) Fire Retardant
  • As shown in FIG. 5, fire retardant materials can be added to the thermoset resin 60, which is sandwiched between the outer thermoplastic sheets 42. It is likely a drop in transparency will be the result of this however.
  • v) Fillers
  • We can also use filler materials within the resin for a variety of reasons including:
      • To reduce the cost of the moulding
      • To facilitate the moulding process
      • To impart specific properties to the moulding
  • Fillers are often added in quantities up to 50% of the resin weight although such addition levels will affect the flexural and tensile strength of the laminate. The use of fillers can be beneficial in the laminating or casting of thick components where otherwise considerable exothermic heating can occur. Addition of certain fillers can also contribute to increasing the fire-resistance of the laminate.
  • vi) Other Possibilities
  • Other vinyls, metallic panels, such as aluminium, and fire retardant materials may be bonded and pressed to the outer layer of the resin sheet for requirements and cosmetics in the building industry. We can also place transfers, articles, and objects such as solar pick up panels within the resin formula within the cavity creating a solar glazing panel.
  • g) Advantages of the Laminate of the Invention
  • One preferred embodiment of the laminate sheet of the invention provides one or more of the following advantages when compared to glass:
      • Improved optical clarity
      • Ease of fabrication
      • Abrasion resistance
      • Lightweight—half weight of glass
      • Chemical resistance
      • Strength—improved impact strength compared with glass
      • Improved acoustic resistance
      • Workable—skill saw cutting, drill and router
      • Thermal resistance
      • Thermoform ability
    h) Blue Effect/Hazing
  • At times the product laminate can have hazing or blue lining. This tends to be due to one of three causes:
      • 1) the effect of refraction due to the fibre optic effect of the sheet and formula eg; the edge of the sheet when exposed to light absorbs the light and allows light to travel the length of the sheet (see FIG. 10). At cure if there is a significant distortion in the outer sheet surface, or detour of the line of light travel, internal reflection may result, giving the appearance of a light blue, smoke haze.
      • 2) The incorrect catalyst mix can cause the inner cavity formula to appear cloudy rather than having the same light refraction as the acrylic sheet, again causing internal reflection.
      • 3) There is the possibility that the inner cavity sheet surface has been slightly tainted due to the percentage of non-styrene resistance.
  • Remedy for blue hazing:
      • The outer edge of the sheet can been sealed to prevent light travel;
      • Ensure the jig or other setting apparatus results in a flat surface for curing;
      • Ensure the correct catalyst mix percentage
      • Ensure the correct sheet/styrene percentage
      • Use a range of translucent tints.
    EXPERIMENTAL Example 1 One Preferred Formulation
  • The tests samples 300 mm×300 mm of continuous and cell cast acrylic called Shinkolite™ of Mitsubish Rayon, Japan were used. They were set in place in the jig to prevent distortion and set at 30° angle for pouring so any air bubbles may rise. Vibration can be applied to speed the release of any air.
  • The mixture of resin and Catalyst were as follows
  • Resin NC007 500 grms
  • Catalyst NA1 5 grms
  • Mix time 2 min
  • Mix temp 20°
  • Mix humidity 62%
  • Setting temp 22°
  • Humidity 67%
  • The sample pour can remain in upright in the jig during the cure process in a hot box. Alternatively the entry hole (used for the filling) can be plugged and then sample laid flat for curing in the hot box.
  • Generally samples should be left at least 8 hours before handling. In order to speed this up post-curing can be used.
  • Post curing can be a matter of preparing the catalyst within the resin some time prior to the pour so as the gel time can be due at introduction to the cavity rather than the gel time being to long within the sheet on the table therefore slowing down production. Ideally while the process is continually on the move the sheet should be at gel stage after five or so meters ready for cutting to length and storage. More catalyst and the heating of the sheet and resin during pour would speed up the cure time dramatically also. We can also add a gel accelerator.
  • Example 2 Cleaning and Preparing Cavity Side of Sheet
  • This can be necessary due to possible contamination from the various adhesives used with protective plastic wrap, which can be applied by some manufacturers. Simply, the adhesive glue is removed with an appropriate cleaner. We have used methylated spirits (both industrial and household) but find iso propyl Alcohol is the most preferred. The preferred cleaner will depend upon the different wraps used by the different manufacturers.
  • Alternatively we use the acrylic, or P.E.T.G. sheeting provided as a sheet or roll without the protective coating, or used on one side only. The protective coating would be left on the outside of the laminate sheets (i.e. not on the side of the sheets in contact with the resin).
  • Example 3 Pour Conditions
  • One preferred resin used in the laminate manufacture is our NC007 resin. It is a dissolved styrene unsaturated Polyester Resin.
  • The following Table B presents our investigations of pour conditions of the P.E.T.G. and acrylic sheeting with this resin.
  • Mix Mix Box Box Resin Cat Set
    Sample Date temp hum temp hum g g time Result
    Taiwan cast 16 Oct. 2005 20° C. 62 22° C. 67 500 g 5 g 8 hrs Good
    Acrylic 1% no crazing
    Taiwan cast 17 Oct. 2005 21° C. 58 32° C. 67 500 g 5 g 8 hrs Not good
    Acrylic 1% crazing
    Taiwan cast 18 Oct. 2005 21° C. 63 36° C. 65 550 g 4 g 8 hrs Not good
    Acrylic 0.75 crazing
    Taiwan cast 19 Oct. 2005 22° C. 64 22° C. 58 550 4 g 6 hrs Good
    Acrylic 0.75 no crazing
    Asia Poly cast 20 Oct. 2005 21° C. 65 22° C. 58 500 g 5 g 6 hrs Good
    Acrylic 1% no crazing
    Asia Poly cast 21 Oct. 2005 23° C. 63 36° C. 65 550 g 4 g 8 hrs Not good
    Acrylic 0.75 crazing
    Asia Poly cast 22 Oct. 2005 21° C. 67 18° 58 550 g 4 g 8 hrs Good
    Acrylic 0.75 no crazing
    Mitsub Japan 23 Oct. 2005 18° C. 64 18° C. 58 550 g 4 g 8 hrs Slight
    C/cast Acrylic 0.75 crazing
    Mitsub Japan 24 Oct. 2005 20° C. 64 22° C. 58 500 g 5 g 8 hrs Slight
    C/cast Acrylic 1% crazing
    Australia High 25 Oct. 2005 22° C. 65 18° C. 58 550 g 4 g 8 hrs Slight
    Impact Acrylic 0.75 crazing
    Australia High 26 Oct. 2005 19° C. 66 18° C. 58 500 g 5 g 8 hrs Slight
    Impact extruded 1% crazing
    Acrylic
    PTEG Blue 27 Oct. 2005 20° C. 64 18° C. 58 500 g 5 g 8 hrs Translucent
    non UV 1% Hazy
    PETG Blue 28 Oct. 2005 18° C. 66 18° C. 64 550 g 4 g 8 hrs Translucent
    non UV 0.75 Hazy
    Size: 300 mm × 300 mm × 2 mm thick
    Temperature, mix, and times of test sample sheets
    (All samples methylated spirit cleaned)
  • FIG. 8 a illustrates the end view of the pour apparatus. The outer edge seal/dam rubber is made up of a closed cell pvc foam sealing tape 25 mm in width with a single adhesive side 91. After the 300 mm×300 mm sample sheet (of acrylic or PETG) 92 is prepared and cleaned the tape is laid out and cut to length, protective tape removed from one side exposing the adhesive. The tape 91 is then placed adhesive side down around outer inside edge of the sheet 92. Joins in the tape 93 at the corners need to be sealed with Soudal High Tak sealant or equivalent polyester compatible sealant. Then Soudal High Tak sealant was applied to the exposed top surface of the pvc sealant tape giving adhesive seal for the top sheet.
  • A gap 94 at the two top corners is essential for the filling of resin and escape of air. The dam rubber must be compatible with the resin formula, if not the resin will seep into the dam seal drawing resin away from the sheet along the outer edges, causing delamination as illustrated in FIG. 9. FIG. 9 shows delamination and air gap 98 due to resin soaking into the rubber dam seal 99.
  • At the time of mixing care needs to be taken not to allow over speed of mixing machinery as this can over aerate the formula, if this happens a period of time is needed to allow the bubbles to surface otherwise vibration of the curing frame is necessary.
  • Small amounts of air may enter the formula while pouring, while rising to the surface the outer edge bubbles can at times cling to the side edges of the rubber this is not a problem as the edge is cut away after cure air bubbles within the sheet do not cause delamination or contamination but rather a cosmetic nuisance.
  • With reference to FIGS. 7 a, b and c (cross sectional, side and perspective views) a jig apparatus 80 was prepared for use with all samples. This enabled the sheets 81 to be held parallel whilst the resin was poured from above.
  • The jig was engineered from 15 mm thick Acrylic sheet 81 and braced horizontally with 10 mm ribbing 82 and held in place using nuts 83. It was important not to over-tighten the outer edge of the jig as a concave appearance will show on the final product resulting in visual distortion to the sample.
  • Example 4 Annealing
  • As discussed previously, styrene resistance of the outer thermoplastic sheeting is an important feature of the invention. Our preferred invention uses sheeting which has an inherent styrene resistance. However it is also possible to anneal the sheeting prior to incorporation into the laminate in order to impart styrene resistance.
  • The following Table A relates to annealing Sample plates of Acrylic and PETG sheet sourced from various plastic sheet manufacturers, Samples sheet size, 3 mm Thick×150 long×75 mm wide, these where then cleaned with isopropyl-alcohol, placed into a cool oven on a flat non stick surface. Some samples were placed between sheets to prevent blistering or distortion. They were heated to the stated conditions and allowed to cool down over a period of 1 hour.
  • Samples were then re-cleaned, a dam rubber applied to the outer inner edge sealed and poured (under specific humidity and temperature conditions) with the resin formulation NC007 then placed into a preset temperature and humidity controlled environment for completion of cure.
  • TABLE A
    Sample Time in oven Temp ° C. Results Comments after pour
    2 mm Asia Poly Cast 1 Hour 80-90° C. Good Slight bow Slight blistering Not poured due to blistering,
    Meth cleaned Lamp only would give false readings
    2 mm Asia Poly cast 1 Hour 80-90° C. Good slight bow Slight blistering As above
    Non Meth cleaned Lamp only
    1 mm PTGE (blue) I Hour 80-85° C Severe blistering and curling As above
    Meth cleaned Lamp only
    1 mm PTGE (blue) 45 Min 50-60° C Blistering and curling As above
    Meth cleaned Lamp only
    1 mm PTGE (blue) 45 Min 70-80° C Placed between sheets of glass Slight hazing but translucent
    Meth cleaned Excellent result colour could be added
    Good bonding
    1 mm PTGE (red) UV protected
    Meth cleaned Test to be carried out plus
    comparison between results of
    blue non-UV PETG
    1 mm PTGE (blue) 2 Hours 75-80° C Placed between sheets of glass Slight hazing but translucent
    Meth cleaned Excellent result colour could be added
    Good bonding
    2 mm Asia Poly Cast/ 1.5 Hours 95-98° C. Placed on heat proof paper No crazing
    Meth Cleaned Good bonding
    2 mm Asia Poly Cast 1.5 Hours 95-98° C. Placed on heat proof paper As above
    Non Meth Cleaned
    2 mm Taiwan Continues 1.5 Hours 95-98° C. Placed on heat proof paper As above
    Cast Meth Cleaned
    Taiwan Continues Cast 1.5 Hours 95-98° C. Placed on heat proof paper As above
    Non Meth Cleaned
    2 mm Japanese Continues 1.5 Hours 95-98° C. Placed on heat proof paper As above
    Cast Meth Cleaned
    2 mm Japanese Continues 1.5 Hours 95-98° C. Placed on heat proof paper As above
    Cast Meth Cleaned
    Preferred sheet Shinkolite from Mitsubishi Rayon Japan
  • In general there was much improvement in the crazing of the samples. Results of the annealing studies showed styrene resistance can be imparted. However this is an inefficient and costly method of doing so. Thus whilst being within the scope of the invention, it is not a preferred step or characteristic.
  • Example 5 Forming/Folding of the Laminate
  • We tested a number of different combinations for their ability to thermoform. One preferred laminate consisted of two opposite outer layers of 2 mm acrylic sheet with an inner cavity barrier layer of 2 mm resin formula, forming an overall 6 mm sandwich or ply material for testing. The acrylic sheet used was Shinkolite (Mitsubishi Rayon Japan) though other suppliers can also provide suitable acrylics. The inner cavity material consisted of unsaturated polyester resin formula with 0.75 w/w (weight for weight) catalyst, e.g. 7.5 grams per litre of resin formula forming the said sandwich/ply sample, with an overall thickness of 6 mm.
  • Four samples of 300 mm×300 mm×6 mm thick were prepared. The pre poured sheet was poured at a room temperature of 20° C. and a humidity of 65% with curing time 6 hours, gel set time 1 hour. The sheets were placed in sealed controlled atmosphere, temperatures pre set to 20° C. Humidity 65%.
  • We attempted to pinpoint an optimum temperature for the maximum achievable curvature through a process of thermoforming.
  • Apparatus: Flat bed fan oven with an internal flat floor layer of Teflon mesh to prevent possible adhesion of test product to oven interior, having also a sealed glass inspection door for viewing.
  • Method: Place sample face down onto the Teflon oven base, the preheated oven temperature being 110° C., for a period of 10-12 minutes.
  • The sample sheet is then corner test lifted by a cotton-gloved hand. When the edge is at a stage of malleability the ply sheet is then removed by sliding a flat spatula underneath to prevent pre distortion and unnecessary exaggerated movement.
  • Forming method: Various Formed structures of ply MDF sheet curvature were prepared prior to sheet extraction from oven to a bench top so there is limited chance of movement as the sheet is clamped and manipulated over the chosen shape. To maximize the stress and to identify failure point of the experiment, a 45° angle with various degrees of sharpness at curvature was used.
  • The hot sheet was then directly placed over the mould and manipulated by hand to form and take the general shape of the mould, then at the latter stage clamped, secured and set in place to re cure. This is illustrated in FIG. 6. The heat source 71 is a double sided heat source applied to the laminate 70. Single sided heating is not ideal for our laminates.
  • Results of forming:
      • No crazing
      • Delaminating centrally and along outer edging only occurred when the sample sheet was left to form and hold the intended shape without pressure and forced forming.
  • Results: We found that in all cases using severe curvature (45 degrees or more) it is necessary to have a complete marrying of the ply forms equal to outer e.g. having the sample sheet pressed between equal outer curvatures therefore the sample sheet becomes a cavity between the outer moulds, a pressure of 2 kilos is sufficient. It is preferably to allow a time of between 12 to 15 minutes before release.
  • Where in the foregoing description reference has been made to elements or integers having known equivalents, then such equivalents are included as if they were individually set forth.
  • Although the invention has been described by way of example and with reference to particular embodiments, it is to be understood that modifications and/or improvements may be made without departing from the scope or spirit of the invention.
  • In addition, where features or aspects of the invention are described in terms of Markush groups, those skilled in the art will recognise that the invention is also thereby described in terms of any individual member or subgroup of members of the Markush group.

Claims (41)

1. A self supporting curved laminate product resulting from curving of a planar precursor,
wherein the planar precursor is a self supporting laminate of two sheets of an acrylic thermoplastic, or of sheets including an acrylic thermoplastic, spaced by, but attaching to, an interposed thermoset polyester system,
and wherein curving has involved heating of the laminate sufficient to allow its curving without substantial degradation of the lamination or its component layers.
2. A product of claim 1 wherein said heating has been into the range of from 105° C. to 120° C.
3. A product of claim 1 wherein one or both sheets is of an acrylic plastic or is at least primarily acrylic plastic.
4. A product of claim 1 wherein said polyester system has been prepared at least in part from (A) carboxylic acid(s) or dicarboxylic acid(s) with (B) a component or components providing (a) hydroxyl(s) and/or dihydroxyl(s).
5. A product of claim 4 wherein said polyester system involves a co-reactive monomer.
6. A product of claim 5 wherein co-reactive monomer is styrene or a styrene derivative or analogue.
7. A product of claim 6, wherein the co-reactive monomer is styrene or a styrene analogue that is present in the polyester system in a quantity from 30-55% w/w.
8. A product of claim 7 wherein styrene is present in a quantity or/from 35-45% w/w.
9. A product of claim 1 wherein the polyester system when cured has an elongation at break greater than 150%.
10. A product of claim 9 wherein said elongation at break is greater than 170%).
11. A product of claim 1 wherein the polyester system is of a polyester resin containing ethylenic unsaturation is present in the range of from 45-70% w/w.
12. A product of claim 1 wherein the polyester system is or has been catalysed by free radical initiators.
13. A product of claim 12 wherein a peroxide free initiator is used.
14. A product of claim 13 wherein the initiator is MEKP (Methyl Ethyl Ketone Peroxide).
15. A product of claim 13 wherein a metal salt promoter is present.
16. A product of claim 12 wherein the level of any such initiator is no more than about 2% w/w of the polyester system prior to the thermoset.
17. A product of claim 16 wherein the level of such an initiator is less than 1% w/w of the thermoset system.
18. A product of claim 1 wherein the lamination of the precursor laminate has involved the laying between flat sheets, or the laying on one flat sheet and subsequent placement of the second flat sheet, of a liquid polyester system and thereafter allowing its thermoset.
19. A product of claim 18 wherein the polyester resin system was a mix of:
45-70% w/w unsaturated polyester resin containing ethylenic unsaturation,
30-55% w/w styrene,
less than 2% w/w catalyst, and
less than 2% w/w initator.
20. A product of claim 1 wherein the polyester resin system was mixed in the temperature range 18 to 22° C.
21. A product of claim 1 wherein the polyester resin system set at temperature(s) in the range 20° C. to 24° C.
22. A product of claim 1 wherein the polyester resin system was mixed at a humidity in the range 57% to 67%.
23. A product claim 1 wherein the resin system is allowed to thermoset at a humidity in the range of from 57% to 75%.
24. A product of claim 1 wherein that surface of the acrylic plastic which is to interface with the polyester system is a clean face substantially free of release agents and/or migrating materials from any removed cover sheet.
25. A product of claim 24 wherein the surface of the sheet(s) has been subjected to cleaning with a solvent.
26. A product of claim 25 wherein said sheet(s) has had the surface thereof to be presented to the polyester system, prior to its thermoset, cleaned with isopropyl alcohol.
27. A product of claim 1, wherein said curving is without any substantial detachment of the polyester system attachment to each said sheet.
28. A product of claim 1 wherein throughout the curving process the interposed polyester system has remained non liquid.
29. A product of claim 1, wherein the product is transparent.
30. A product of claim 1 wherein the polyester system layer is at least 0.5 mm thick and accounts for from 5% to 40% of overall laminate thickness.
31. A product of claim 30 which is at least 1 mm thick.
32. A self supporting transparent laminate able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form, the laminate being of a transparent polyester system interposed and attaching to flanking transparent thermoplastic layers, which thermoplastic layers attach to the polyester system by both
cross linking with free unsaturation in acrylic material,
free monomer solvation of acrylic material,
and wherein each thermoplastic layer comprises an acrylic or PETG.
33. A self supporting transparent laminate able to be curved when all layers of the laminate are heated to a temperature or temperatures unable to melt any layer to a liquid form, the laminate being of a transparent polyester system interposed and attaching to flanking transparent acrylic thermoplastic layers.
34. The self supporting transparent laminate of claim 33, wherein the laminate is greater than 3 mm thick.
35. The self supporting transparent laminate of claim 34, wherein the polyester system is at least 0.5 mm thick and each thermoplastic layer comprises an acrylic or PETG.
36. The laminate of claim 35 wherein the polyester system can account for from 5% to 40% of overall laminate thickness.
37. A laminate of claim 33 wherein the polyester system layer is at least 1 mm thick.
38. The laminate of claim 33, the laminate having a performance related to a notional symmetric variant having acrylic layers 2 mm thick on the outside with a core of a polyester system 2 mm thick, the notional variant being able without fracture and/or delamination to withstand a challenge loading in excess of 40 tonnes into its edges, on its minor axis if notionally a rectangle of 960×470 mms.
39. A laminate of claim 38 wherein the polyester resin system was in the form of:
45-70% w/w unsaturated polyester resin containing ethylenic unsaturation,
30-55% w/w styrene,
less than 2% w/w catalyst, and
less than 2% w/w initator, and
when of a thickness of 2 mm, 2 mm and 2 mm through a three layer laminate and when a rectangular panel of 960×470 mm squeezed on its minor axis, it can withstand without delamination between 60 and 80 tonnes.
40. A method of producing a curved laminate material comprising the steps of:
providing a laminate of substantially flat sheets of an acrylic and/or PETG thermoplastic having a thermoset polyester resin therebetween, wherein the thermoset resin has an elongation at break of >150% and a glass transition temperature less than ambient temperature,
heating a shaping region of the laminate to a shaping temperature,
shaping the laminate to the desired curvature,
cooling the laminate,
wherein the step of heating the shaping zone of the laminate comprises heating substantially through all layers of the laminate in the shaping zone.
41. A method of claim 39 wherein the step of heating the shaping region comprises applying heat to the shaping region from both surfaces of the laminate in the shaping region.
US12/779,840 2006-05-23 2010-05-13 Laminate material Abandoned US20100297403A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/720,722 US9168693B2 (en) 2006-05-23 2012-12-19 Laminate material

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
NZ54745206A NZ547452A (en) 2006-05-23 2006-05-23 Self supporting curved laminate made from acrylic thermoplastic and thermoset polyester
NZ547452 2006-05-23
NZ55196306 2006-12-08
NZ551963 2006-12-08
PCT/NZ2007/000123 WO2007136282A2 (en) 2006-05-23 2007-05-22 Laminate material

Related Parent Applications (3)

Application Number Title Priority Date Filing Date
NAPCT/NA2007/000123 Continuation 2007-05-22
PCT/NZ2007/000123 Continuation WO2007136282A2 (en) 2006-05-23 2007-05-22 Laminate material
US12302009 Continuation 2007-05-22

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US13/720,722 Division US9168693B2 (en) 2006-05-23 2012-12-19 Laminate material

Publications (1)

Publication Number Publication Date
US20100297403A1 true US20100297403A1 (en) 2010-11-25

Family

ID=38723715

Family Applications (2)

Application Number Title Priority Date Filing Date
US12/779,840 Abandoned US20100297403A1 (en) 2006-05-23 2010-05-13 Laminate material
US13/720,722 Active US9168693B2 (en) 2006-05-23 2012-12-19 Laminate material

Family Applications After (1)

Application Number Title Priority Date Filing Date
US13/720,722 Active US9168693B2 (en) 2006-05-23 2012-12-19 Laminate material

Country Status (7)

Country Link
US (2) US20100297403A1 (en)
EP (1) EP2026955B1 (en)
JP (1) JP4918645B2 (en)
CN (1) CN103552289B (en)
AU (1) AU2007252345B2 (en)
CA (1) CA2687792C (en)
WO (1) WO2007136282A2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130076178A1 (en) * 2011-09-22 2013-03-28 Minebea Motor Manufacturing Corporation Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US20140199525A1 (en) * 2009-05-13 2014-07-17 3Form, Inc. Structured-core laminate panels and methods of forming the same
USD810961S1 (en) 2009-05-13 2018-02-20 3Form, Llc Structured-core laminate panel
US20210323746A1 (en) * 2018-06-05 2021-10-21 Anheuser-Busch Inbev S.A. Composite Transport Container for Beverages
US11762416B2 (en) * 2019-01-03 2023-09-19 Boe Technology Group Co., Ltd. Transparent laminated film, display device and method for manufacturing transparent laminated film

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2939716B1 (en) * 2008-12-11 2012-11-16 Essilor Int METHOD FOR OBTAINING A CURVED MULTILAYER STRUCTURE
FR3026982B1 (en) * 2014-10-14 2020-02-28 Airbus Group Sas THERMOPLASTIC / THERMOSETTING MULTILAYER COMPOSITE MATERIAL
JP7236554B2 (en) * 2019-10-09 2023-03-09 帝人株式会社 Method for manufacturing curved member, and polycarbonate resin laminate with hard coat layer for thermal bending

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3700546A (en) * 1971-02-17 1972-10-24 American Cyanamid Co High impact weatherable rigidified structures
US3707434A (en) * 1970-11-30 1972-12-26 Federal Huber Co Rigidified resinous laminate
US4648925A (en) * 1984-08-01 1987-03-10 Corning Glass Works Method of making transparent polarizing laminated glasses
US4936936A (en) * 1988-08-30 1990-06-26 E. I. Du Pont De Nemours And Company Method of making thermoplastic acrylic polymer coated composite structure
US5055346A (en) * 1988-08-30 1991-10-08 Frank Rohrbacher Thermoplastic acrylic polymer coated composite structure
US5705275A (en) * 1995-08-31 1998-01-06 Shin-Etsu Polymer Co., Ltd. Thermosetting resin composition and two-parts composite body thereof with silicone rubber
US20010041251A1 (en) * 1997-07-15 2001-11-15 Jean-Louis Bravet Plastic glazing, in particular for motor car and method for making same
US6476111B1 (en) * 2001-08-01 2002-11-05 E. I Du Pont De Nemours And Company Extrudable highly filled thermoplastic sheet composition
US20030021986A1 (en) * 2001-07-24 2003-01-30 Zuoxing Yu Moisture crosslinkable thermoplastics in the manufacture of vehicle weather strips
US20030130414A1 (en) * 2000-12-29 2003-07-10 Charles Brandenburg Alpha-methylene lactone homopolymer and copolymer compositions, sheets and articles made therefrom and the process for their manufacture
US20030194540A1 (en) * 2002-04-12 2003-10-16 Fusco Luciano A. Decorated panel and process for making the same
US20040161611A1 (en) * 2001-07-26 2004-08-19 Klaus Mueller Laminated composite material and method for the production thereof
US6811857B1 (en) * 1998-06-19 2004-11-02 Saint-Gobain Glass France Plastic glazing sheet with added overmoulded plastic material

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2917783A (en) 1954-10-21 1959-12-22 Fed Tool Corp Method for forming thermoplastic materials
GB1140743A (en) 1966-03-19 1969-01-22 Mealia Res And Dev Inc O Improvements relating to the manufacture of windows
US3810815A (en) * 1969-07-10 1974-05-14 Mc Donnell Douglas Corp Transparent laminate
US3993828A (en) 1973-02-16 1976-11-23 Akzona Incorporated Polyester, fiberglass-reinforced composite laminate
FR2325505A1 (en) * 1975-09-24 1977-04-22 Altulor LAMINATED POLYACRYLATE AND POLYESTER COMPLEX PRODUCT, ITS MANUFACTURING PROCESS AND ITS APPLICATIONS
DE2606569A1 (en) * 1976-02-19 1977-08-25 Degussa PROCESS FOR THE PRODUCTION OF BULLET-RESISTANT COMPOSITE (GLASS) PANELS
FR2547768B1 (en) 1983-06-24 1986-01-10 Ugine Kuhlmann THERMOPLASTIC POLYMER LIGHT THERMOSETTING POLYMER COMPOSITE MATERIAL AND METHODS OF MANUFACTURE
FR2679044B1 (en) 1991-07-12 1994-06-10 Corning Inc COMPOSITE OPHTHALMIC LENS.
JPH06149167A (en) 1992-11-09 1994-05-27 Morinaga Kenchiku Sekkei Jimusho:Kk Water wall unit
JPH06200643A (en) 1992-11-09 1994-07-19 Morinaga Kenchiku Sekkei Jimusho:Kk Wall structure for water
EP0622386B1 (en) 1993-04-26 1998-01-28 Gencorp Inc. Conductive in-mold coatings
US6475608B2 (en) * 1998-11-16 2002-11-05 Engelhard Corporation Multi-layer iridescent films
US6558784B1 (en) * 1999-03-02 2003-05-06 Adc Composites, Llc Composite footwear upper and method of manufacturing a composite footwear upper
US6291370B1 (en) 1999-09-01 2001-09-18 Harodite Industries, Inc. Chopped fiberglass laminate for automotive headliners and method of fabrication
WO2006092288A1 (en) * 2005-03-01 2006-09-08 Cfs Germany Gmbh Device for producing deep packaging trays comprising a cooled lower mould section
US20060272766A1 (en) * 2005-06-03 2006-12-07 Hebrink Timothy J Optical bodies and method of making optical bodies including acrylate blend layers

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3707434A (en) * 1970-11-30 1972-12-26 Federal Huber Co Rigidified resinous laminate
US3700546A (en) * 1971-02-17 1972-10-24 American Cyanamid Co High impact weatherable rigidified structures
US4648925A (en) * 1984-08-01 1987-03-10 Corning Glass Works Method of making transparent polarizing laminated glasses
US4936936A (en) * 1988-08-30 1990-06-26 E. I. Du Pont De Nemours And Company Method of making thermoplastic acrylic polymer coated composite structure
US5055346A (en) * 1988-08-30 1991-10-08 Frank Rohrbacher Thermoplastic acrylic polymer coated composite structure
US5705275A (en) * 1995-08-31 1998-01-06 Shin-Etsu Polymer Co., Ltd. Thermosetting resin composition and two-parts composite body thereof with silicone rubber
US20010041251A1 (en) * 1997-07-15 2001-11-15 Jean-Louis Bravet Plastic glazing, in particular for motor car and method for making same
US6811857B1 (en) * 1998-06-19 2004-11-02 Saint-Gobain Glass France Plastic glazing sheet with added overmoulded plastic material
US20030130414A1 (en) * 2000-12-29 2003-07-10 Charles Brandenburg Alpha-methylene lactone homopolymer and copolymer compositions, sheets and articles made therefrom and the process for their manufacture
US20030021986A1 (en) * 2001-07-24 2003-01-30 Zuoxing Yu Moisture crosslinkable thermoplastics in the manufacture of vehicle weather strips
US20040161611A1 (en) * 2001-07-26 2004-08-19 Klaus Mueller Laminated composite material and method for the production thereof
US6476111B1 (en) * 2001-08-01 2002-11-05 E. I Du Pont De Nemours And Company Extrudable highly filled thermoplastic sheet composition
US20030194540A1 (en) * 2002-04-12 2003-10-16 Fusco Luciano A. Decorated panel and process for making the same

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140199525A1 (en) * 2009-05-13 2014-07-17 3Form, Inc. Structured-core laminate panels and methods of forming the same
USD810961S1 (en) 2009-05-13 2018-02-20 3Form, Llc Structured-core laminate panel
US20130076178A1 (en) * 2011-09-22 2013-03-28 Minebea Motor Manufacturing Corporation Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US9590463B2 (en) * 2011-09-22 2017-03-07 Minebea Co., Ltd. Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US10298106B2 (en) 2011-09-22 2019-05-21 Minebea Co., Ltd. Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US10778074B2 (en) 2011-09-22 2020-09-15 Minebea Mitsumi Inc. Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US10790735B2 (en) 2011-09-22 2020-09-29 Minebea Mitsumi Inc. Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US11336164B2 (en) 2011-09-22 2022-05-17 Minebea Mitsumi Inc. Vibration generator moving vibrator by magnetic field generated by coil and holder used in vibration-generator
US20210323746A1 (en) * 2018-06-05 2021-10-21 Anheuser-Busch Inbev S.A. Composite Transport Container for Beverages
US11762416B2 (en) * 2019-01-03 2023-09-19 Boe Technology Group Co., Ltd. Transparent laminated film, display device and method for manufacturing transparent laminated film

Also Published As

Publication number Publication date
EP2026955B1 (en) 2018-02-07
WO2007136282A3 (en) 2008-01-24
CN103552289B (en) 2016-01-20
JP2009538242A (en) 2009-11-05
EP2026955A2 (en) 2009-02-25
JP4918645B2 (en) 2012-04-18
EP2026955A4 (en) 2012-06-13
CA2687792A1 (en) 2008-11-29
AU2007252345A1 (en) 2007-11-29
US20130105070A1 (en) 2013-05-02
AU2007252345B2 (en) 2012-06-14
US9168693B2 (en) 2015-10-27
CA2687792C (en) 2015-03-24
CN103552289A (en) 2014-02-05
WO2007136282A2 (en) 2007-11-29

Similar Documents

Publication Publication Date Title
US9168693B2 (en) Laminate material
US9718996B2 (en) Composition and method for temporarily fixing member using same
JP2009517539A (en) Pre-preg and in-situ hardened surfaces prepared therefrom
KR20140001983A (en) Decorative sheet, and decorative resin-molded article employing same
KR20160042813A (en) Adhesive agent composition, adhesive agent composition for polarizing plate, adhesive agent for polarizing plate, and polarizing plate manufactured using said adhesive agent
NZ547452A (en) Self supporting curved laminate made from acrylic thermoplastic and thermoset polyester
JP5351597B2 (en) Vacuum forming sheet
JP2002522620A (en) Adhesives for the production of composite glass
TWI798747B (en) coating film
JP5651337B2 (en) Artificial marble molded product and manufacturing method of artificial marble molded product
JP6175338B2 (en) Method for producing optical laminate sheet
CN108300385A (en) Adhesive sheet, display body and their manufacturing method
JP2001287313A (en) Composite material and method for manufacturing the same
JPH04166311A (en) Manufacture of molded object
JPH10235771A (en) Highly clear decorative sheet
JP2001288230A (en) Curable resin composition for producing gel coat sheet
JPH09314684A (en) Resin molded article
WO2001034386A1 (en) Transparent plastic film having hard coat layer
KR101314832B1 (en) High-glossy decorative sheet having EVA pattern layer and the method of fabrication thereof
JP2002070434A (en) Storage door
JPH0542930B2 (en)
TW202402525A (en) Sheet, product, decorative sheet, decorative material and curable composition
JPS6134390B2 (en)
KR20200046234A (en) Composition for forming hard coating layer having 3D shape and protective film using the same
JP2004275263A (en) Counter having bowl with high designability

Legal Events

Date Code Title Description
AS Assignment

Owner name: NU CLEER SYSTEMS LIMITED, NEW ZEALAND

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:THORPE, GEOFFREY CHARLES;BLACK, KEVIN JOSEPH;WATSON, GAVIN BLAIR;SIGNING DATES FROM 20100702 TO 20100707;REEL/FRAME:024757/0471

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION