GB2504012A - Reinforced laminate of porous material, curable material and veneer - Google Patents

Reinforced laminate of porous material, curable material and veneer Download PDF

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Publication number
GB2504012A
GB2504012A GB1315418.2A GB201315418A GB2504012A GB 2504012 A GB2504012 A GB 2504012A GB 201315418 A GB201315418 A GB 201315418A GB 2504012 A GB2504012 A GB 2504012A
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GB
United Kingdom
Prior art keywords
fibres
substrate
sheet
veneer
laminate
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.)
Granted
Application number
GB1315418.2A
Other versions
GB2504012A8 (en
GB201315418D0 (en
GB2504012B8 (en
GB2504012B (en
Inventor
Aldino Albertelli
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.)
Acell Industries Ltd Ireland
Original Assignee
Acell Industries Ltd Ireland
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
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Publication of GB201315418D0 publication Critical patent/GB201315418D0/en
Publication of GB2504012A publication Critical patent/GB2504012A/en
Application granted granted Critical
Publication of GB2504012B publication Critical patent/GB2504012B/en
Publication of GB2504012A8 publication Critical patent/GB2504012A8/en
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Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B32B21/00Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
    • B32B21/04Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B21/08Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood 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
    • B32B21/00Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
    • B32B21/14Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood board or veneer
    • 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
    • B32B27/065Layered 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 foam
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/18Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of discrete sheets or panels only
    • B32B37/182Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of discrete sheets or panels only one or more of the layers being plastic
    • 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
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/26Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
    • E04C2/284Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating
    • E04C2/296Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating composed of insulating material and non-metallic or unspecified sheet-material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0442Layered armour containing metal
    • F41H5/0457Metal layers in combination with additional layers made of fibres, fabrics or plastics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0471Layered armour containing fibre- or fabric-reinforced 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
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0012Mechanical treatment, e.g. roughening, deforming, stretching
    • B32B2038/0024Crushing
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    • 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
    • B32B2038/0052Other operations not otherwise provided for
    • B32B2038/0076Curing, vulcanising, cross-linking
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    • B32B2266/00Composition of foam
    • B32B2266/06Open cell foam
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    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/02Cellular or porous
    • B32B2305/022Foam
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/02Cellular or porous
    • B32B2305/026Porous
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/07Parts immersed or impregnated in a matrix
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/07Parts immersed or impregnated in a matrix
    • B32B2305/076Prepregs
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/08Reinforcements
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/72Cured, e.g. vulcanised, cross-linked
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/00Properties of the layers or laminate
    • B32B2307/10Properties of the layers or laminate having particular acoustical properties
    • B32B2307/102Insulating
    • 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
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
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    • B32B2307/3065Flame resistant or retardant, fire resistant or retardant
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    • B32B2307/308Heat stability
    • 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
    • B32B2307/402Coloured
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
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    • 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
    • B32B2307/40Properties of the layers or laminate having particular optical properties
    • B32B2307/414Translucent
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/546Flexural strength; Flexion stiffness
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/00Properties of the layers or laminate
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    • B32B2307/584Scratch resistance
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/714Inert, i.e. inert to chemical degradation, corrosion
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B2398/10Thermosetting resins
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
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    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/06Embossing

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Architecture (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Veneer Processing And Manufacture Of Plywood (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

A method of providing a laminate armoured or bullet-proof shield, the method comprising: applying a substrate 44 including a porous structure to a first surface of a layer comprising a sheet-form curable material 40; applying a veneer element 33 to a second surface of the sheet-form material; providing one or more reinforcement fibres selected from carbon fibres, glass fibres, aramid fibres (e.g KEVLAR RTM) and/or polyethylene fibres; and applying pressure to press the veneer element, the sheet-form material, the reinforcement fibres and the substrate together to form the laminate shield. Preferably, there is provided a metal frame 46, another porous material 48, curable material 52 and veneer 54. The veneer 33, 54 is preferably wood. Preferably, the thermosetting, curable, sheet moulding compound (SMC) 40, 52 flows into the veneer 33, 54 during the heating and pressing step. Preferably, gas or vapour is displaced from the porous, open cell foam 44, 48. The laminate can be used as a door, building panel, furniture, vehicle fitting, window or picture frame, or bowl. The pressing members can be flat 56 or structured 20

Description

-I-
Laminate products This invention relates to composite products, for example laminate products. Preferred aspects of the invention relate to laminate products comprising a foam substrate and a skin on a surface of the substrate. Preferred aspects of the invention relate to the production ot laminated panels, for example for use in building, in furniture and as architectural components, for example architectural mouldings, although the invention has wide application to a broad range of composite products. Aspects of the invention described relate to doors, windows and other panels, in particular those used in buildings and in furniture.
Doors, windows and panels, for example for buildings and furniture have traditionally been made from wood, and may be glazed or unglazed. However, unless specially treated, wood can warp if exposed to changes in temperature and/or humidity. This can be disadvantageous aesthetically and can also lead to difficulties in opening and closing the doors, windows and partitions. The latter are particular problems in the light of modern building safety regulations, where warped doors, windows and panels can constitute a fire hazard. Furthermore, wood can be relatively expensive to obtain and there are major environmental concerns in respect of the use of certain types of wood.
Over the last few decades there has therefore been a trend towards providing artificial doors, panels and windows. One type of artificial door, panel and window is a moulded article. Moulded article can be formed by a number of different methods.
Foam resin laminate panels of the kind comprising a foam resin layer and a skin are being employed increasingly in the building, decorating and furniture industries because of the wide range of useful properties achievable.
In a known method of forming panels, the panels comprise a pair of outer skins and an internal foam core. The skin or skins and the foam core are formed separately and may then bonded together by means of an adhesive or by heat. However, there are disadvantages with such panels, for example with delamination of the skin for example on failure of the adhesive.
In known systems, the skins may be formed by compression moulding of a sheet moulding compound (SMC). The SMC includes a thermosetting resin, for example a polyester resin, together with reinforcing fibres, for example glass fibres.
To make the formed skin, the sheet moulding may be folded to form a block of charge and placed into a preheated moulding cavity. The mould is closed and pressure is applied to press the moulding compound so that it spreads to all parts of the mould.
Heat and pressure is applied until the moulded material has cured. The mould is then opened and the formed skin is removed.
The shaped skins can then be secured to opposite sides of a frame, prior to injecting a foam into a cavity located between the skins. The foam acts as a filler and can assist in providing increased improved rigidity and insulation the door. The door can then be finished as appropriate.
In a further method described in UK Patent Application No. 0719343.6, the skins are bonded directly to a foam core during a moulding step. A layer of sheet-form SMC is provided on the mould surface, a foam core is placed on the layer of SMC, and pressure is applied to mould the components together. During the moulding step, the core and 5MG layer are moulded to the desired shape, and the SMC material becomes bonded to the core.
Such methods can give laminated products having good physical and chemical properties and good aesthetic finish, but their appearance is not thes?me as real wood. Thus the laminated products are not used for some applications where a real An object of aspects of the present invention is to solve or mitigate the above identified problems and/or other problems and/or to provide an improved composite product and method of forming a composite product.
According to an aspect of the invention, there is provided a method of forming a laminate product, the method comprising: providing a layer comprising a sheet-form material; providing a substrate including a porous structure; and providing a veneer element; the method including the step of applying the substrate to a first surface of the sheet-form material, applying the veneer element to a second surface of the sheet-form material, and applying pressure to press the veneer element, the sheet-form material and the substrate together to form the laminate product.
In this way, a laminate product comprising a veneer surface can be formed. The veneer can provide a desirable aesthetic finish to the product and/or desired physical and/or chemical surface properties of the product.
Preferably the term veneer is to be understood, where appropriate, to refer to a thin surface layer applied to the sheet-form material.
While it is envisaged that a broad range ol materials could be used in the veneer, in preferred arrangements, the veneer includes wood.
The veneer elernent.may include wood. The veneer may include two or more different woods, and/or other components in addition to wood. Such components may for example be include to enhance the physical and/or chemical properties of the veneer, and might for example include binders, stiffeners, hardeners, and/or other components.
Such other components may include for example polymer resins, tillers, varnishes and/or other suitable components. The veneer may include a surface pattern, arid/or may itself comprise a laminate material.
Alternatives are possible. For example theveneer might not include wood, The veneer may include a simulated wood surface, for example the veneer may include a polymer having a surface finish simulating wood or other material, for example stone. The surface of the veneer may be flat or may be provided with surface formations, for example for aesthetic reasons, for example to simulate a wood, stone or other surface.
Alternatively or in addition, surface formations may be provided on a surface 01 the veneer which will not be visible in the laminated product. For example, surface formations may be provided on the surface to be bonded to the sheet-form material, for example to improve the strength of the interface between the veneer and the sheet-form material.
The thickness of the veneer may be 5mm or less, preferably 3mm or less. The thickness of the veneer will depend on the application of the product, and the physical and aesthetic properties required.
Preferably the sheet-form material comprises a curable material, for example a thermoset.
Preferably the curable material flows into the veneer element during the pressing step.
Preferably at least some part of curable material flows into a surface of the veneer during pressing. Preferably the material is keyed into the veneer layer. In this way, a strong bond between the matrix and the veneer element can be obtained. Where the veneer element comprises wood, ills found that the curable material is pressed into spaces between the fibres of the wood to form a strong bond between the two layers.
Alternatively or in addition1 adhesive material may be applied between the sheet-form material and the veneer element to aid bonding.
The veneer element may extend over substantially all or only a part of the sheet-form material and/or the substrate area.
Preferably the configuration of the substrate is such that gas and/or vapour can be displaced from the pressing region. Preferably the pressing region is that area where the surface of the substrate and the sheet-form material are being pressed together, preferably in the region of the interface of the substrate and the material.
By removing gas or vapour that might otherwise remain and/or build up in that region, it has been found that the pressure required to form the composite product can be significantly reduced in some examples.
Preferably the nature of the surface of the substrate is such that the gas or vapour can escape from the pressing region. For example, a region at at least a part of the surface of the material is preferably porous to allow forthe displacement Of gas or vapour from the relevant areas.
Preferably the substrate is such that gas or vapour can escape from the pressing region in a direction having at least a component in a direction generally trsverse to the pressing direction in which the sheet-form material is pressed to the substrate.
Other formations (as an alternative or in addition) may be provided to assist the displacement of the gas. For example, grooves or channels could be formed in the substrate.
The configuration of the substrate which allows for the displacement of the gas may be inherent in that it arises from the nature of the composition of the substrate itself, and/or it may be provided by subsequent action, for example by machining the substrate or by chemical action on the substrate. Preferably the configuration of the substrate is such that it can release pressure in the pressing region.
Preferably the substrate includes a material having a cellular structure.
A cellular structure of the substrate can provide the necessary displacement of the gases in some arrangements. In preferred examples, the substrate comprises a material including a substantially open-celled structure. In this way, good movement of the gases away from the pressing region can be obtained in some examples. The substrate may comprise a foam material.
The substrate may comprise a loam material including a substantially open-celled structure.
It is envisaged that the substrate might not form part of the ultimate product being formed. For example after the pressing step, the substrate may be removed from the resin and veneer laminate. The laminate might then subsequently be used as a skin in 1 0 the production of other products, for example the panels and doors described above.
Preferably, however, the substrate becomes bonded to the sheet-form material during the pressing. Preferably the curable material extends into the surface of the substrate during the formation of the laminate so as to improve the mechanical bonding between the components. Alternatively, or in addition, an adhesive or other bonding agent may 1 5 be used between the substrate and sheet-form layer.
Thus in preferred arrangements, curable material moves into the laminate element and the substrate surface during the pressing.
By applying a sheet-form material to a substrate comprising an open-celled structure.
several advantages can be achieved. In particular, by using an open cell foam substrate1 air in the mould and gases produced during the moulding process can pass into and through the open cell structure of the foam so that the risk of the air and gases leading to flaws and other deformities in the skin are reduced.
Furthermore, by bonding the sheet-form material to the substrate and the veneer in the moulding process, efficiencies in manufacture of the laminate product can be achieved since in some examples, a further step to adhere the layers together might be avoided.
In preferred examples, the material of the sheet-form material passes into the cells or otherformations of the substrate material during the moulding process and provides a mechanical bond between the substrate and the moulded skin. This can reduce the risk of delamination of the skin from the substrate core, provide a stable product when exposed to heating/cooling cycles and provides a monolithic composite structure without the need for an adhesive to be applied or the assembly of parts.
The substrate can form a part of the final product, or it is envisaged that the substrate might be removed, for example by machining, after the skin has been formed.
Preferably the substrate forms a part of a final product derived from the composite product.
By providing the matrix in the form of a sheet, the use of liquid resin can be avoided.
This can give considerable time savings in the manufacture of the product, as well as benefits regarding the ease of use of the matrix material and a reduction in the manpower and equipment required to apply the matrix material or pre-polymer to the mould.
However, in other arrangements, liquid resin might be used. Therefore the invention further provides a method of forming a laminate product, the method comprising: providing a layer comprising a curable material; providing a substrate; and providing a veneer element; the method including the step of applying the curable material to the veneer, applying the substrate to a surface of the curable material, and applying pressure to press the veneer element, the curable material and the substrate together to form the laminate product.
In preterred examples, the sheet-form material forms a skin on the substrate, which is mechanically keyed into substrate giving a good bond between the skin and the substrate. In some cases it has been found that the bond achieved at the interface of the skin and the substrate is in fact stronger then the material of the substrate itself. A laminate product made by this method may fail within the substrate layer, and not at the interface.
The sheet-form material may include a sheet moulding compound (SMC). Preferably the SMC includes a thermosetting polymer, for example a resin, for example a polyester resin, together with reinforcing fibres, for example glass fibres.
The laminate product produced may comprise for example a core having one skin of SMC and veneer applied to a surface, or may comprise a core sandwiched between two skins. Other arrangements are possible. In some cases, for example, the product may comprise a core having a first skin including SMC and an outer layer of the veneer, and a second skin including just the SMG layer and no additional veneer. This arrangement might be preferred where different finishes were required on different surfaces of the product, for example for use as cupboard doors.
The core having two skins might be formed in a single pressing operation in which the required layers were arranged and then pressed together in a mould to bond the layers together.
The method may include the step of providing a second layer including a sheet-form material, applying the second layer at a surface of the substrate, the substrate being sandwiched between the first and second layers of sheet-form material, and pressing the second layer and the substrate together.
In this way it can be seen how a two-sided panel or door can be formed in a single IC pressing operation. Alternatively, two or more steps might be used. A further layer of veneer material can be provided at the second layer.
In some embodiments of the invention, the sheet-form material is applied directlyto the substrate. In other examples, one or more layers may be provided between the substrate and the sheet-form material, for example to enhance adhesion or bonding of IS the two parts. For example an adhesive might be applied between the parts.
The components will be pressed together between suitable moulds or plates. In preferred examples, at least one mould part is providedwhich includes a pattern to be taken by the components during the pressing or moulding step.
For example, where the laminate product is to be a door, a mould surface might include for example recessed regions and other surface features so that the moulded door might look more realistic compared with a traditional wooden door.
Preferably the veneer element has appropriate dimensions and is formed of a suitable material so that it can be moulded, as required.
Preferably the method includes the step of applying the layer of sheet-form material to a mould, the method further including the step of pressing the substrate to the sheet-form material to the mould.
Preferably the method includes the step of applying the veneer directly to a surface of a mould.
In some examples, one or more further layers might be appfled between the veneer andfor sheet-from material and the tool surface itself. In some examples, materials %4,* .fl:. ::-c;. ..,:",S.'to.J I *:... %...:.: .C?! might be applied to the tool surface, for example to assist moulding and/or release of the product from the mould.
A coating composition may be applied to the mould which forms a coating on the product after moulding. The composition may be coloured. The composition may be applied to the mould in the form of a powder, for example using an electrostatic method.
Preferably the method includes applying heat and pressure to the veneer and the sheet-form material. Preferably the sheet-form material is cured directly onto the veneer and substrate. This important feature may be provided independenuy. A broad aspect of the invention provides, curing a sheet of curable material directly onto the surface of a veneer and of a substrate, preferably a substrate configured to displace gas or vapour from the interface region, preferably the substrate comprising an open-cell foam.
Preferably the sheet-form material comprises a thermosetting material, the method including the step of causing or allowing the material to cure Preferably the method comprises a method of compressIon moulding.
Preferably the pressure and temperature and cycle time are chosen so that the sheet-form material sets in the mould.
Preferably the mould is profiled to produce the desired shape of skin.
A contoured surface of the composite product can be obtained. For example the surface of the product may include depressions formed during the pressing step as the components are pressed onto the mould. Thus moulded composite products can be formed.
It is envisaged that the methods of the present invention can be used to form products having no surface mouldings. for example flat panels. In this case, the substrate may comprise any suitable material. Preferably the substrate comprises a rigid material so that the pressing step can be carried oul most successfully and the substrate can provide desired mechanical properties to the product. Such a method may for example be used to form flat-fronted panels or doors as well as other articles, for example table tops and kitchen worktops.
:V:;:...bt.Gi:..::t;c..F j:.t' .:.f. ;.MtVS"'; ri f:cL::. t:tC::.?. .4 In some examples, where a contoured surface is required, the required contours or mouldings can be formed on the surface of the substrate. For example, the required shape may be formed in the substrate by machining, for example, a substrate block comprising polyurethane foam.
The shape of the mould is matched to the contours of the substrate so that when the components are pressed onto the mould surface, the resulting panel has the skin having the required contours bonded to the shaped substrate.
Preferably the substrate comprises a crushable material such that, during the application of pressure step, a surface of the substrate is moulded.
The substrate may comprise more than one material, for example the substrate may comprise regions of different materials or materials flaying different mechanical properties.
The substrate may comprise a frangible material. Such a material may be rigid and non-crushable in the normal use of the resulting product, but during the pressing step.
the substrate material can be crushed to mould the substrate. Where a mould surface is used, the substrate material can be crushed so that its surfaces facing the mould conform to the contours of the mould surface.
This method is particularly advantageous in some examples. In particular, it can remove the requirement to machine the required contours into a surface of the substrate before the application of the skin.
Simple blocks of the substrate can be used in the method to form shaped or nioulded products.
The moulding may provide surface contours of the product, and/or may provide the shape of the product itself. It is envisaged that shaped products could e formed using this method.
In examples described, the substrate comprises a plastics matedal, but other any other suitable material could be used.
It is envisaged that the invention might be applied where the substrate comprises a material which is rigid even on the application of pressure, but preferably the substrate comprises a material which can be controllably crushed during application of pressure * :,c:j""2.:'.... ft.: y... **.j:r:s. C 1.1:r:ñ::.t... .:.zf:.
so that a surface of the substrate can take on the contours of a part of the mould.
In this way, moulded laminated products can be efficiently produced in a single step from a sheet moulding material and a block of substrate material.
In examples of the present invention, the substrate material preferably comprises a rigid foam, for example a foam material obtained by causing or allowing a mixture of phenolic resole, acid hardener and finely divided particulate solid to cure under conditions in which foaming for the mixture is caused primarily or solely byvolatilisation of small molecules present in the resole or formed as a by-product of the curing reaction. The formation of an example of such foams is described in detail in EP 0010353 and foamed bodies comprising these foams can be obtained as ACELL loam from Acell Holdings Limited, UK.
Preferably the substrate material has a density in the range of 100 to 500 kglms, more preferably 120 to 400 kg/m3 and most preferably 120 to 250 kg/m3. It has been found that such foams can be caused to reproduce on aface thereof the detail of even quite fine and complex mould surfaces by the application 01 a suitable pressure the level of which depends on the nature and density of the foam material but can readil be determined by simple experiment.
Such a substrate has a substantially open-cell structure so that as the layer of sheet-form material is pressed into the cells or pores of the material, the gas or vapour therein can be readily displaced.
While any suitable material may be employed, aspects of the invention are particularly suitable for use with substantially rigid structural materials, for example foams, that is, preferably self-supporting foams which are resistant to deflection under load and do not collapse under moderate pressure. The physical properties of such foams, especially the compressive strength and deflection under load are believed to be related to (amongst otherfactors) cell wall thickness. In some examples, the cell size for suitable substrate material is found to be in the range of about 0.5mm to 5mm1 more preferably O.Sorl mmto2or3mm.
It is preferred for the substrate to include a filler material, for example a finely divided filler material. Foamed phenolic resin reinforced with a finely divided filler is particularly preferred in some arrangements because of the excellent combination of physical ;it!:t:tx... **.**: .y: ,.:.._;2::.t::::,...:.:.
properties and fire resistance that can be obtained for laminates formed from it.
Preferably at least some of the cells or pores of the foamed substrate are open to the surface of the face on which the layer of sheet-form material is to be applied, and preferably the open out below the surface to a greater width than the opening, thereby £ providing an undercut which can enhance the keying of the layer material to the substrate.
In some examples, the thickness of the layer of sheet-form material provided on the substrate will be at least 1 mm but thicknesses of less than 1 mm are also contemplated. If desired, the thickness of the layer of material may be reduced before orafter setting.
In some examples a further layer of sheet-form material is applied to an opposing surface of the substrate, the application of pressure sandwiching the substrate between the two layers of sheet-form material. In this case, a further veneer layer or other layer may or may not be provided on the surface of the other layer of sheet-form material.
In this way, a laminate product including a skin on two sides can be formed. For example, were the product comprises a door, both sides ofihe door can be formed in a single step.
The sheet form material preferably includes a thermoset. The material may include further components, for example components to enable the material to be handled in sheet-form.
The sheet-form material of aspects of the invention, may include any appropriate matrix composition. For example, the matrix may include one or more of a thermosetting polymer, for example an epoxy resin, a phenolic resin, a bismaleimide or polyimide, and/or any other suitable material. The material may include melwnine, which is useful as a fire retardant. The matrix materials may further include hardeners, accelerators, fillers. pigments, andtor any other components as required. The matrix may include a thermoplastic material.
The sheet-form material may comprise reinforcement, for example reinforcing fibres.
The sheet-form material may include glass fibres.
Preferably the layer of sheet-form material comprises SMC (sheet moulding compound).
::..eY:.Ct:. .. . The SMO may comprise two main components: a matrix and a reinforcement.
The matrix preferably comprises a resin which preferably includes polyester, but may include vinyl ester, epoxy, phenolic, or a polytmide, Prelerably the matrix comprises a thermosetting resin.
The matrix may further comprise additives, for exampre minerals, inert tillers, pigments, stabilizers, inhibitors, release agents, catalysts, thickeners, hydrating additives and/or other suitable materials.
The reintorcement preterably comprises glass fibres. The fibres may be cut, for example into lengths of 5 cm or less, or may be continuous. Other reinforcement materials could be used, for example carbon fibres.
There are benefits in using SIC. For example, SMC has low density but favourable mechanical properties compared with other materiats for example thermoplastics and also exhibits good thermal properties. Of particular importance for some applications, for example building applications, resistance to tire is good. SMC also shows good noise reduction qualities, also important where used as a building material and good chemical resistance.
The fibres may be short fibres, or may be longer fibres. The fibres may be loose, tor example, the fibres may be arranged in a uni-or multi-directional manner. The tibres may be part of a network, for example woven or knitted together in any appropriate manner. The arrangement of the fibres may be random or regular, and may comprise a fabric, mat, felt Or woven or other arrangement. The material may include short fibres.
Fibres may provide a continuous filament winding. More than one layer of fibres may be provided.
The fibres may include one or more materials. For example the fibres may include one or more of carbon fibres, glass fibres, aramid fibres and/or polyethylene fibres. Kevlar (RIM) fibres may be used. Products including such fibres could be used for protective devices and building products. For example, some products of the present invention may find application as armoured or bullet-proof products. For example, protective panels may be formed having Kevlar (RIM) fibre reinforcement.
The sheet-form material may comprie an impregnated fibre composite material.
Surprisingly, it has been found that sheet-form materials including long fibres can be used in the methods of the present invention, and also sheet-form materials including fibres which are woven together can be used. Without wishing to be bound by theory, it is thought that such materials having relatively long fibre reinforcements and/or including fibre mats or other networks or structures can be used because the movement of material in the mould in a direction along the mould surface is relatively low.
Alternatively or in addition to reinforcement being provided as an integral part of the sheet-form material, reinforcement may be provided as a separate layer, for example arranged between the sheet-lorm material and the substrate.
Where the separate layer of reinforcement is provided, it may be located across the whole of the substrate, or may for example be provided in only parts. For example, if there is a particular section of the product which is more susceptible to damage or attack, additional reinforcement can be provided in that region. For example, where the product is to be used in a door, additional reinforcement may be provided at regions of the door which are thinner than others for due to decorative moulding or other fealures and/or at regions of the door which are more susceptile to damage.
Thus the arrangement may include sheet-form material having integral reinforcement, for example short fibres an War longer fibres which may be arranged as fabrics or mats, for example. In addition, or alternatively, reinforcement may be provided as one or more layers separate from the sheet-form material. The additional layer of reinforcement may include short and/or long fibres, for example of materials mentioned above.
During the pressing or moulding, preferablythe matrix material, for example resin, flows into the structure of the fabric or other arrangement, to form a bond.
Preferably the layer of sheet-form material comprises a curable composition. In some examples of the invention, the sheet-form material might be settable other than by curing.
Preterably the pressure and heat is chosen such that the sheet-form material is moulded and then sets in the mould.
Preferablythe viscosity of the sheet-form material is reduced during the pressing step.
Preferably the sheet-form material is one that reduces in viscosity and or at least partially liquefies on the application of heat and/or pressure. In this way, some flow of the material in the mould can be achieved. This can lead to improved moulding of the material, more uniform thickness and/or reduction of moulding defects. Preferably, the material at least partly flows into cells of the substrate material during the pressing step.
Preferably the material and substrate are such that the material only partly flows into the substrate during the moulding step so that good bonding between the skin and the substrate is obtained while retaining a suitable skin thickness for the required mechanical and other properties of the laminate.
Preferablythe sheet-form material is applied asasingle thickness.
Preferably the material, for example the SMC is applied to the mould in unfolded form.
This leads to ease of manufacture, and also can reduce the pressure required for the moulding step. As discussed further herein, a plurality of single thickness layers may be provided, the layers preferably overlapping at the edges to reduce the risk of gaps beingformed in the skin, Preferably the sheet-form materialisapplied to substantially a whole mould surface.-Having the SMC extend substantially across the full area of a mould face has a number of advantages. For example, in some arrangements, the pressure required to complete the moulding step can be reduced by reducing the amount of lateral flow required of the material in the mould. Also, by reducing the amount of flow of material across the mould surface, abrasion and/or wear of the surface of the mould can be reduced. In this way, the material used for the mould can be selected from a wider range of candidate materials as discussed in more detail below.
The sheet-form material can be applied to the mould as a single piece of material.
Preferably a plurality of sheets of sheet-form material is applied to a mould surface, In some arrangements, for example because the mould surface is large, or to improve the ease of handling the sheet-form material, several pieces of sheet-form material can be applied to the mou'd and/or the substrate. Preferably an edge of one sheet overlaps with an edge of an adjacent sheet. In this way, the risk of gaps being formed in the skin on the substrate is reduced. The additional material at the overlapping region has been found not to lead to reduced quality of the finished product: any excess material in that region can, in some examples, into the substrate and/or laterally within the mould.
Thus in some examples, in particular where complex shapes are to be formed, several pieces of sheet-form material can be provided.
This feature is further advantageous because it can lead to a reduction in the amount of potentially waste sheet-form materiaJ. Smaller pieces of material, for example off cuts from larger pieces or cut outs (for example if a panel is to include a glazed section) need not be disposed of but can be used.
Preferably the pressure apphed is pressure is less than 200 tonnes, preferably less than about 100 tonnes.
As discussed above, traditional SMC manufacturing processes requires enormous pressure to evacuate the air trapped during the forming of the SMC product. By putting the foam substrate behind the SMC skin prior to pressing, the air can escape though the cellular structure of the foam reducing greatly the abrasion on the tool surface.
Also considerably lower pressures are required. Preferably the pressure is less than 500 tonnes, preferably less than 200 ton nes, preferably less than about 100 tonnes.
Preferably thasheet-form material is applied to a mould surfacecomprisingaluminium or aluminium alloy.
Where lower pressures are used, aluminium tools can be used. This can give rise to low cost tooling, flexible production and less downtime due to tool change over in view of the reduced weight of an aluminium mould and speed of heating or cooling an aluminium mould compared with a stainless steel mould. For example, the volume of an aluminium tool could be significantly smaller than that of a corresponding tool of steel, and this combined with the lower density of aluminium leads to considerable weight advantages when using aluminium moulds.
Where reference is made herein to components being made of or comprising aluminium, preferably the relevant component includes aluminium or an appropriate aluminium alloy or other material including aluminium.
The substrate may include surface formations on at least a part of the substrate surface, so that the material of the sheet-form material keys with the formations to bond the material to the substrate.
i:-.::c ?q-k''-'c, :. r.:....:.. *-.: According to a broad aspect of the invention there is provided a method of forming a laminate product, the method comprising the steps of: providing a sheet-form curable material; providing a substrate; providing a veneer; and pressing the sheet-form material between the substrate and the veneer to form the laminate product Preferably the sheet-form material includes a thermoset material, Preferably the surface of the substrate includes a plurality of pores or other surface formations so that the sheet-form material can flow so as to key mechanically to the substrate, for example as a result of the pores or formations. In this way, a strong interface between the skin and substrate of the resulting product can be achieved.
In some examples the substrate has a substantially open cell structure, The substrate may comprise an open cell foam material.
Preferably a single pressing step is used in the forming of the composite product.
Preferably the complete finished product is formed by a method in which only one pressing or moulding step is used.
Preferably the substrate comprises a rigid crushable material. In this way, depressed regions in the laminate product can be formed by using a shaped moulding tool.
Preferabtythe sheet-form material is provided on a surface of the tool, the substrate is provided on the sheet-form layer, and is pressed onto the tool surface.
The method may include the step of providing further components between the two layers being pressed together.
Other components may also be sandwiched between the skins during the moulding process. For example where the product is a door, the door frame components, glazing panels and other components might be arranged in the mould so that they can be formed into the product in a single moulding step. It is envisaged that a substantially complete product, for example a door, could be made in a single moulding operation using the present invention.
A broad aspect of the invention provides, a method of forming a laminated product, for example a panel or door, the method comprising the steps of providing first and second veneers, providing first and second layers of sheet-form material between the veneers, applying a substrate between the first and second layers of sheet-form material, optionally further applying an additional component between the first and second layers of material, and applying pressure to the layers to bond the layers to the substrate to form the product.
To give improved rigidity, in the finished product (door, window or panel), in general the skins will be spaced not only by a core but also bya frame or frame members such as stiles, rails, and/or mullions. The frame members may be of wood, metal (for example, aluminium) or plastics (such as uPVC) or a combination of these, e.g. metal-reinforced plastics. The plastics materIal may containfilier, it desired, to improve hardness and/or rigidity.
In a preferred embodiment, the core occupies substantially the entire volume or volumes within the frame; Le. substantially the whole space within the panel defined by the skins and the components of the frame. It is also preferred that the substrate is bonded to each skin over substantially the entire area of the substrate which is in contact with that skin, even when the skin includes one or more depressed zones, since this enhances the overall strength of the panel and the resistance to bowing.
In one preferred embodiment, the substrate is in the form of one or more blocks, for example rectangular blocks, held in a frame, at least one of the skins includes one or more depressed zones and the portion of the block or blocks behind each said zone conforms to the contours of said zone as a result of selective controlled crushing of the substrate in the area behind said zone.
The veneer layer may include more than one veneer elements. For example, the method may include the step of placing a plurality of veneer elements in the mould, applying SMC over the veneer elements, positioning the substrate on the SMC layer and compression moulding the layers to form the laminate product.
The flow of the SMC material into the surface of the veneer, and the subsequent curing can form a laminate product in which the separate elements of the veneer are rigidly bonded onto the surface of the cured SMC layer in the desired arrangement. This feature can be advantageous, for example because it allows smaller, and cheaper, elements of veneer to be used. Also, more complex shapes might be formed using elements of veneer, for example veneer might be applied around a corner of the laminate product as discussed below.
:..vf:&c%:.'.?.: : Vf. *.:.... . The elements may all have the same composition, for example may include the same wood, it is envisaged that different materials [or example woods, might be placed together as a veneer layer. Thus a panelled or marquetry effects can be obtained.
The invention also provides a product formed by a method as described herein and an S apparatus for use in a method as described herein.
Also provided by the invention is a product comprising a substrate and a skin of sheet form material bonded to a surface of the substrate, and further including a veneer bonded to a surface of the skin of sheet-form material.
Preferably the veneer comprises wood.
Preferably the material of the sheet-form material is mechanically keyed with the surface of the substrate and/or with the surface of the veneer.
The substrate may have formations on its surface, the material keying with the formations. The substrate may be substantially open-celled the material extending into cells of the open-cell substrate.
15.The.veneer may have tormalionsori its surface, the material keyed with the surface of the formations. The veneer may be an at least partially porous material, the material extending into the surface of the veneer. For example where the veneer comprises wood, the material extends into the wood between the fibres of the wood material.
There may be a bonding agent between the veneer and the sheet-form material. This may enhance bonding of the layers together.
Preferably the thickness of the veneer is less than 10mm, preferably less than 5mm, for
example 3mm or less.
A further aspect of the invention provides a laminate comprising a layer of sheet-form material (for example SMC), and further including a veneer bonded to a surface of the sheet-form material.
Such a laminate product may have one or more of the further features described herein.
The laminate product so formed may be used as a skin in the formation of a door, panel or other article.
: .c -. ...:....
For example, two such laminate products can be used as outer skins for a door. The skins are secured to opposite sides of a frame, prior to injecting a foam into a cavity located between the skins. The foam acts as a filler and provides increased rigidity and insulation in the door. Alternatively, one or more of the skins can be bonded to a preformed substrate by any appropriate method.
Where reference is made herein to for example the veneer, skin, layer or substrate being bonded to another element, it is to be understood that, preferably, at least a part of the veneer, skin, layer or substrate is so bonded. In some examples, the veneer, skin or layer or substrate will be attached over the whole of its interface withthe other element.
The invention extends to methods and/or apparatus substantially as herein described with reference to the accompanying drawings.
Any feature in one aspect of the invention may be applied to other aspects of the invention, in any appropriate combination. In particular, method aspects may be applied to apparatus aspects, and vice versa.
PfeferOdMatUie th prnt ihVéntidnWill ñOWb debed; example, with reference to the accompan\Ang drawings, in which: Figure 1 shows a schematic plan view of a mould used for forming a laminate product according an example 01 the present invention; Figure 2 shows a section taken on A-A of Figure 1 and showing schematically the veneer and moulding material; Figure 3 illustrates in perspective exploded view the moulding of a laminated composite; Figure 4 shows in schematic sectional view the components of a door.
Figure 1 shows schematically a plan view of an aluminium mould 20. The mould comprises a surface contour suitable for moulding a door panel. The moulding surface is rectangular and includes an outer frame section 22, a rectangular inner panel section 24 and a bead 26 between the panel section 24 and the outer frame 22. The mould is heated to a temperature of approximately 140 degrees C. Wood veneer elements are placed in the mould 20 as shown in the sectional view in Figure a In this case, a plurality of veneer elements are used. Frame element 32 is placed onto the outer frame section 22, panel element 34 on the panel section 24 and a bead element 36 in the bead 26 of the mould. Each of the veneer elements may comprise one or more components which may be joined prior to moulding or may be separate.
A sheet of sheet moulding compound 40 is applied to the upper surface of the mould veneer. The sheet 40 is sized so as to extend across the whole area of the mould surface 20.
Further elements for forming the laminate are shown in Figure 3. It will be appreciated that in Figure 3 and in other of the figures the shapes of the components are shown schematically. In particular, the relative thicknesses of the elements are not shown to scale. For example, the preferred thickness of veneers is about 3mm.
Onto the sheet 40 is placed a wooden frame 42 is positioned onto the sheet 40 (Figure 3) and a block of foam substrate 44 is inserted into the frame 42.
The substrate 44 may comprise afoam, for example as described in more detail below.
Such foam used is advantageously: -structural and has significant load bearing properties -frangible and can be formed under pressure and has no memory and therefore substantially retains its pressed form -open cell and therefore allows the migration of clues resins into the cells during door manufacture to create a truly monolithic composite structure.
In an example of the foam used, the cell size ranges from 0.5 to 3 mm and the density is 80 to 800 kg/ma.
The block of foam 44 is sized so as to be thicker than the frame so that the upper surface of the foam 44 extends above the frame 42 when the foam 44 is inserted in the aperture of the frame 42.
Downward pressure of about 100 tonnes is applied to the components (as arranged in Figure 3) using a pressure plate 50. The substrate 44 is pressed toward the lower moulding surface 20, crushing the foam and moulding the lower surface of the substrate to the shape of the mould surface 20. The SMC sheet 40 is also pressed -21 -between the veneer 32. 34, 36 and the substrate 44. Near the heated mould surface 20, the SMC begins to liquefy and flow into cells at the surface of the substrate 44 as well as into pores and other spaces at the surface of the veneers 32, 34, 36.
Air and other gases trapped between the SMC 40 and the substrate 44 passes through the open cell structure of the foam. The components are held in the mould with the application of pressure for a sufficient time for the SMC to cure for form a skin bound to the moulded substrate 44 and the veneer 32, 34, 36.
The resulting product is removed from the mould. The cycle time for moulding the product may be about 4 minutes.
It is seen that in this example, an upper mould portion Is not required. In this example, the components are pressed against a single heated platen.
Referring now to Figure 4, a method is described In which a moulded door having a veneer surface is formed in a single pressing step, A lower mould 20 is provided and placed on a heated platen 25 so that the mould reaches a temperature of about 140 degrees C. The lower moulding surface 21 of the lower mould 20 may be flat or may be contoured as here according to the surface shape of a panelled door A layer of veneer 33 is placed onto the moulding surface 21. The veneer layer 33 may include more than one element, for example as shown in Figure 2. The veneer elements comprise for example thin portions of oak wood.
A lower sheet 40 of curable material is applied to the veneer. The size of the lower sheet 40 is approximately the same as that of the lower moulding surface 21.
A foam block 44 comprising ACELL foam is applied to the upper surface of the lower sheet 40. A wooden frame 42 is placed around the lower foam block. Alternatively, the frame 42 could be applied first, and the block 44 inserted into the frame. A reinforcement sheet 46 comprising a metal grid is placed in the frame 42 onto the lower foam block 44. Onto the reinforcement sheet 46 and within the frame 421s placed an upper foam block 48 also comprising ACELL loam. A layer of adhesive may be applied between the two blocks 44,48 to aid bonding. Onto the upper foam block is placed the upper sheet 52 of curable material.
Optionally, onto the upper sheet of curable material 52 is placed further veneer * %..:, -I:-.:..C! elements 54. In some arrangements, it will be desired for the veneer to be present on both surfaces of the panel. In other arrangements, veneer on one surface of the door only will be required. In the latter case, it will be appreciated that the veneer may be arranged at the lower or the upper region of the moulded components.
An upper mould 56 is provided having an upper moulding surface 58 contoured according to the surface shape of a panelled door or flat as shown here. The upper mould 56 is heated to a temperature of about 140 degrees C. The upper mould 56 is lowered onto the other components and pressure of about 100 tonnes is applied to press the upper mould 56 towards the lower mould 20.
The upper block 48 and the lower block 44 comprise frangible foam and the surfaces of the blocks facing the adjacent mould surfaces 20 and 58 are crushed and moulded to the surface shape of the panelled door.
The curable material of the upper and lower sheets 40 and 52 flow into the adjacent foam blocks 44, 48 and also into the veneers 33, 54 to form a mechanical bond.
Curing of the curable material takes place in the heated mould so that the upper and lower sheets 40 and 52 form skins bonded to the upper and lower blocks.
Once cure is complete after a few minutes, the formed door is released from the mould.
Thus it can be seen how a door can be made in a single pressing operation.
In an alternative example, the lower block 44, the reinforcement 46 and the upper block 48 are provided as a single unit.
In other arrangements, the mould may be coated with a powder coating which then forms a coating on the product. This feature may be present in relation to any of the aspects of the invention. As an example, a powder coating can be applied electrostatically to the mould surface. Where the mould surface is heated, the powder coating melts or softens almost as soon as it is applied to the surface. For example the powder may include a polyester. The SMC or other rnalrix material (with or without integral reinforcing material) is then applied over the melted or softened powder coating. The melted or softened powder coating is then "sticky" on the surface of the mould and is thought to reduce movement of the matrix material during the moulding operation, which can in some cases give improved surface finish. In this example, the coating remains on the surface of the product, and provides a surface which is scratch -23 -and/or impact resistant. The powder coating can be coloured and thus provide a coloured coating to the product. The powder coating may be transparent or translucent and may have the appearance of a varnish on the surface of the product.
It will be understood that a very wide range of different composite products could be formed using methods as described herein. The application of the present invention is not restricted to the formation of, tar example, doors.
Example of Preparation of SMC The SMC comprises a curable matrix and reinforcement.
To prepare the SMC, the matrix is prepared by mixing, for example a polyester resin with minerals and additives, for example including calcium carbonate and titanium dioxide together with appropriale pigments.
The matrix in the form of the resin paste is then applied to a bottom film carrier. Glass fibres as the reinforcement are then applied to the upper surface of the resin paste on the film carrier. A further layer of the resin paste is applied to sandwich the fibres between the layers of matrix. A top film is applied to the upper layer of the matrh. The resulting layered composition is subsequently compressed using a series of rollers to form a sheet of the sheet moulding compound between the firm carriers. The material is rolled onto rollers and kept for at least 3 days at a regulated temperature of for example 23 to 27 degrees C. The resulting SMC can be compression moulded with heat. The shelf life of the 5MG before use is usually a few weeks. Foam
In some examples of the invention, the substrate comprises a foam having frangible cell walls. Preferably this term includes a foam for which under compression the foam crumbles by brittle fracture of the cell walls e.g. involving a clean fracture of the cell wall& Such a foam can retain a clear and substantially dimensionally accurate imprint in the crushed zone of an object through which the compressive force is applied. In general, it is preferred that the yield strength of the foam, which in this case means the minimum force required to cause the fracture of the cell walls and for the foam to crumble, is in the range of about 100 to 140 KPa (15 to 20 lbs/sq.in) more preferably at least 200 KPa (30 lbs/sq.in), since this provides useful impact resistance. In general, for a given foam composition, the greater the density, the greater the yield strength.
* .ç:-..---. :---ts'..--.,-*.i *:.. ,2::t-::'Y:..r'c'-'. -c----,----.:: -..: -: :t.t. .".. ..C. -.....
By using a substantially rigid plastics foam with frangible cell walls, mouldings with depressed zones of moulding detail can be readily formed by applying a layer to the foam core with sufficient pressure to cause the cell walls of the foam in the areas behind the depressed zones of the skin to be fractured whereby the foam is caused to conform to the contours of the skin in those zones by controlled localised crushing.
Thus, air gaps between the skin and the substrate can be avoided and it is not necessary to pre-form the substrate in the form of complicated shapes. This is particularly advantageous since the presence of such air gaps in prior art products has in some cases contributed to their inability to resist changes in temperature.
For such a method, it is advantageous to use an open cell foam having frangible walls as pressing into a conventional foamed core such as of polystyrene is in some cases not successfully achieved because the resilience of the foam may cause distortion of the skins when the pressure is released.
In some examples of the invention, plastics foam are preferred which are substantially open-cell and rigid. However, the foam is advantageously selected to be of a high density relative to the foamed polystyrene conventionally used, e.g. a density of 75 makes-ft-soundand handle more like a conventional wooden panel. However, foams having lower densities may also be selected. Where a higher density is desirable, the foam may contain a filler, more preferably a finely divided inert and preferably inorganic solid. The filler may be selected such that it contributes to the panels ability to resist changes in temperature. In a particularly preferred embodiment, the filler is capable of absorbing moisture, e.g. as water of crystallisation.
While particular reference is made in the examples to open celled frangible foams, any suitable foam may be used. In some examples of the invention, foams which are substantially open cell are preferred; for example, a polyurethane foam, but in some examples the foam might not be open celled. Preferably in such example, the structure of the substrate is such that gases can be released from the mould. Where the foam is open celled, a foam that has an open-cell configuration at production is particularly suitable. A foam that also has frangible cell walls is particularly preferred where the panel or other product to be formed has depressed areas, such as to provide a moulding effect. However, as described herein, the moulding of the substrate can be provided by other methods, for example machining.
Any foam can be used some aspects of the invention. In many examples, rigid foam materials are preferred. For example a rigid foam could be used to form a panel having a substantially flat (unmoulded) surface which may or may not include surface pattern as described herein.
Alternatively, or in addition, the surface of the foam may be contoured. The contours could for example be formed on the surface of a foam block, for example by machining or any other suitable method. In such cases, the foam neeci not for example be a frangible or compressible foam.
Where a foam having frangible cell walls is used, the cell wail will fracture as pressure is placed on the foam by the application of the depressed areas of the mould. This localised increase in pressure will increase the pressure inside the cell, which will cause the gases to travel through the foam, and the cell to collapse thereby accommodating the depressed area of the skin.
One suitable foam is a rigid filled phenolic foam. One particularly suitable foam is that produced by effecting a curing reaction between: (a) a liquid phenolic resole having a reactivity number (as defined below) of at least 1 and (b) a strong acid hardener for the resole, in the presence of: (c) a finely divided inert and insoluble particulate solid which is present in an amount of at least 5% by weight of the liquid resole and is substantially uniformly dispersed through the mixture containing resole and hardener; the temperature of the mixture containing resole and hardener due to applied heat not exceeding 85_C and the said temperature and the concentration of the acid hardener being such that compounds generated as by-products of the curing reaction are volatilised within the mixture before the mixture sets whereby a foamed phenolic resin product is produced.
By a phenolic resole is meant a solution in a suitable solvent of the acid-curable prepolymer composition obtained by condensing, usually in the presence of an alkaline catalyst such as sodium hydroxide, at least one phenolic compound with at least one aldehyde, in well-known manner. Examples of phenols that may be employed are phenol itself and substituted, usually alkyl substituted, derivatives thereof provided that *1.. \:.: j:x:Yk:..Cf -26 -the three positions on the phenolic benzene ring a-and p-to the phenolic hydroxyl group are unsubstituted. Mixtures of such phenols may also be used. Mixtures of one or more than one of such phenols with substituted phenols in which one of the ortho or para positions has been substituted may also be employed where an improvement in the flow characteristics of the resole is required but the cured products will be less highly cross-linked. However, in general, the phenol will be comprised mainly or entirely of phenol itself, for economic reasons.
The aldehyde will generally be formaldehyde although the use of higher molecular weight aldehydes is not excluded.
The phenol/aldehyde condensation product component of the resole is suitably formed by reaction of the phenol with at least 1 mole of formaldehyde per mole of the phenol the formaldehyde being generally provided as a solution in water. e.g. as formalin. It is preferred to use a molar ratio of formaldehyde to phenol of at least 1.25 to 1 but ratios above 2.5 to 1 are preferably avoided. The most preferred range is 1.4 to 2.0 to 1.
The mixture may also contain a compound having two active H atoms (dihydric compound) that will react with the phenoValdehyde reaction product of the resole during --the-curingstep-to-reduce-thedensityof-cross-Unkingr Preferred-thhydriccornpounds are dials, especially allcylene diols or diols in which the chain of atoms between the OH groups contains not only methylene and/or alkyl-substituted methylene groups but also one or more hetero atoms, especially oxygen atoms, e.g. ethylene glycol, propylene glycol, propane-i,3-diol, butane-i,4-diol and neopentyl glycol. Particularly preferred diols are poly-, especially di-, (alkylene ether) diols e.g. diethylene glycol and, especially, dipropylene glycol. Preferably the dihydric compound is present in an amount of from 0 to 35% by weight, more preferably 0 to 25% by weight, based on the weight of phenol/aldehyde condensation product. Most preferably, the dihydric compound, when used, is present in an amount of from S to 15% by weight based on the weight of phenol/aldehyde condensation product. When such resoles containing dihydric compounds are employed in the present process, products having a particularly good combination of physical properties, especially strength, can be obtained.
Suitably, the dihydric compound is added to the formed resole and preferably has 2-6 atoms between OH groups.
r..:.., -27 -The resole may comprise a solution of the phenol/aldehyde reaction product in water or in any other suitable solvent or in a solvent mixture, which may or may not include water. Where water is used as the sole solvent, it is preferred to be present in an amount of from 15 to 35% by weight of the resole, preferably 20 to 30%. CI course the water content may be substantially less if ii is used in conjunction with a cosolvent. e.g. an alcohol or one of the above-mentioned dihydric compounds where one is used.
As indicated above, the liquid resole (I.e. the solution of phenoValdehyde product optionally containing dihydric compound) must have a reactivity number of at least 1.
The reactivity number is 10/x where x is the time in minutes required to harden the resole using 10% by weight of the resole of a 66-67% aqueous solution of p-toluene sulfonic acid at 6odegreesC. The test involves mixing about 5m1 of the resole with the stated amount of the p-toluene sulfonic acid solution in a test tube, immersing the test tube in a water bath heated to 6odegreesC and measuring the time required for the mixture to become hard to the touch. The resole should have a reactivity number ot at least 1 for useful foamed products to be produced and preferably the resole has a reactivity number of at least 5, roost preferably at least 10.
--The-pHof-theresole1whichisrgenerally-alkaUneis-preferably-adju5tedto-abO ut7, if -*-----necessary, for use in the process, suitably by the addition of a weak organic acid such as lactic acid.
Examples of strong acid hardeners are inorganic acids such as hydrochloric acid, sulphuric acid and phosphoric acid, and strong organic acids such as aromatic sulphonic acids, e.g. toluene sulphonic acids, and trichloroacetic acid-Weak acids such as acetic acid and propionic acid are generally not suitabie. The preferred hardeners for the process of the invention are the aromatic sulfonic acids, especially toluene sulfonic acids.
The acid may be used as a solutiOn in a suitable solvent such as water.
When the mixture of resole, hardener and solid is to be poured, e.g. into a mould and in slush moulding applications, the amount of inert solid that can be added to the resole and hardener is determined by the viscosity of the mixture of resole and hardener in the absence of the sdid. For these applications, it is preferred that the hardener is provided in a form, e.g. solution, such that when mixed with the resole in the required amount yields a liquid having an apparent viscosity not exceeding about 50 poises at -28 -the temperature at which the mixture is to be used, and the preferred range is 5-20 poises. Below 5 Poises, the amount of solvent present tends to present difficulties during the curing reaction.
The curing reaction is exothermic and will therefore ot itself cause the temperature of the mixiure containing resole and acid hardener to be raised. The temperature of the mixture may also be raised by applied heat but the temperature to which said mixture may then be raised (that is, excluding the effect of any exotherm) must not exceed 85 degrees C. If the temperature of the mixture exceeds 85 degrees C before addition of the hardener, it is difficult or impossible thereafter to properly disperse the hardener through the mixture because of incipient curing. On the other hand, it is difficult, if not impossible, to uniformly heat the mixture above 85 degrees C after addition of the hardener.
Increasing the temperature towards 85 degrees C tends to lead to coarseness and non-uniformity of the texture of the foam but this can be offset at least to some extent at moderate temperatures by reducing the concentration of hardener. However at -----* temperatures-rnuekabove-75-degrees C-eve1he minimum amount of-hacdener -------required to cause the composition to set is generally too much to avoid these disadvantages. Thus, temperatures above 75 degrees C are preferably avoided and preferred temperatures for most applications are from ambient temperature to about 75 degrees C. The preferred temperature range appears to depend to some extant on the nature of the solid (c). For most solids it is from 25 to 65 degrees C but for some solids, in particular wood flour and grain flour, the preferred range is 25 to 75 degrees C. The most preferred temperature range is 30 to 50 degrees C. Temperatures below ambient. e.g. down to 10 degrees C can be used, if desired, but no advantage is gained thereby. In general, at temperatures up to 75 degrees C, increase in temperature leads to decrease in the density of the foam and vice versa.
The amount of hardener present also affects the nature of the product as well as the rate of hardening. Thus, increasing the amount of hardener not only has the effect of reducing the time required to harden the composition but above a certain level dependant on the temperature and nature of the resole it also tends to produce a less uniform cell structure. It also tends to increase the density of the foam because of the increase in the rate of hardening. In fact, if too high a concentration of hardener is *:r.k?.;.tc.: used, the rate of hardening may be so rapid that no foaming occurs at all and under some conditions the reaction can become explosive because of the build up of gas inside a hardened shell of resin. The appropriate amount of hardener will depend primarily on the temperature of the mixture of resole and hardener prior to the S commencement of the exotbermic curing reaction and the reactivity number of the resole and will vary inversely with the chosen temperature and the reactivity number.
The preferred range of hardener concentration is the equivalent of 2 to 20 parts by weight of p-toluene sulfonic acid per 100 parts by weight of phenol/aldehyde reaction product in the resole assuming that the resole has a substantially neutral reaction, i.e. a pH of about 7. By equivalent to p-toluene sulfonic acid, we mean the amount of chosen hardener required to give substantially the same setting time as the stated amount of p-toluene sulfonic acid. The most suitable amount for any given temperature and combination of resole and finely divided solid is readily determinable by simple experiment. Where the preferred temperature range is 25-75 degrees C and the resole has a reactivity number of at least 10, the best results are generally obtained with the use of hardener in amounts equivalent to 3 to 10 parts of p-toluene sulfonic acid per parts by weight of the phenol/aldehyde reaction product. For use with ---tempreratures below-25 degrees-C-orresoles-havir,g a reactivity-number-belowlO,-it ----may be necessary to use more hardener.
It may be necessary to make some adjustment of the hardener composition in accordance with the nature, especially shape and size, of the mould and this can be established by experiment.
By suitable control of the tern perature and of the hardener concentration, the time lapse between adding the hardener to the resole and the composition becoming hard (referred to herein as the setting time) can be varied at will from a few seconds to up to an hour or even more, without substantially affecting the density and cell structure of the product.
Another factor that controls the arnount of hardener required can be the nature of the inert solid. Very few are exactly neutral and if the solid has an alkaline reaction, even if only very slight, more hardener may be required because of the tendency of the filler to neutralize it. It is therefore to be understood that the preferred values for hardener concentration given above do not take into account any such effect of the solid. Any adjustment required because of the nature of the solid will depend on the amount of solid used and can be determined by simple experiment.
The exothermic curing reaction of the resole and acid hardener leads to the formation of by-products, particularly aldehyde and water, which are at least partially volatilised.
The curing reaction is effected in the presence of a finely divided inert and insoluble particulate solid which is substantially uniformly dispersed throughout the mixture of resole and hardener. Byan inert solid we mean that in the quantity it is used it does not prevent the curing reaction.
It is believed thatthe finelydivided particulate solid provides nuclei for the gas bubbles formed by the volatilisation of the small molecules, primarily CH2O and/or H20, present in the resole and/or generated by the curing action, and provides sites at which bubble formation is promoted, thereby assisting uniformity of pore size. The presence of the finely divided solid may also promote stabilization of the individual bubbles and reduce the tendency of bubbles to agglomerate and eventually cause likelihood of bubbre collapse prior to cure. The phenomenon may be similar to that of froth flotation employed in the concentration of low grade ores in metallurgy. In any event, the presence of the solid is essential to the formation of the product. To achieve the desired-effect -the solid-should-be presentin-an-amount of-not-less than-5%-by-weight------based on the weight of the resole, Any finely divided particulate solid that is insoluble in the reaction mixture is suitable, provided it is inert. The filters may be organic or inorganic (including metallic), and crystalline or amorphous. Even fibrous solids have been found to be effective, although not preferred. Examples include clays, clay minerals, talc, vermiculite, metal oxides, ref ractories, solid or hollow glass microspheres, fly ash, coal dust, wood tlour, grain flour, nut shell flour, silica, mineral fibres such as finely chopped glass fibre and finely divided asbestos, chopped fibres, finely chopped natural or synthetic fibres, ground plastics and resins whether in the form of powder or fibres, e.g. reclaimed waste plastics and resins, pigments such as powdered paint and carbon back, and starches.
Solids having more than a slightly alkaline reaction, e.g. silicates and carbonates of alkali metals, are preferably avoided because of their tendency to react with the acid hardener. Solids such as talc, however, which have a very mild alkaline reaction, in some cases because of contamination with more sirongly alkaline materials such as magnesite, are acceptable.
.%.....% .....n* *. .. *%X..%.* ctf:e.c:.tc Some materials, especially fibrous materials such as wood flour, can be absorbent and it may therefore be necessary to use generally larger amounts of these materials than non-f ibrous materials, to achieve valuable foamed products.
The solids preferably have a particle size in the range 0.5 to 800 microns. If the particle size is too great, the cell structure of the loam tends to become undesirably coarse. On the other hand, at very small particle sizes, the foams obtained tend to be rather dense.
The preferred range is ito 100 microns, most preferably 2 to 40 microns. Uniformity of cell structure appears to be encouraged by uniformity of particle size. Mixtures of solids may be used if desired.
If desired, solids such as finely divided metal powders may be included which contribute to the volume of gas or vapour generated during the process. If used alone, however, it be understood that the residues they leave after the gas by decomposition or chemical reaction satisfy the requirements of the inert and insoluble finely divided particulate solid required by the process of the invention.
Preferably, the finely divided solid has a density that is not greatly different from that of the resole, so as to reduce the possibility of the finely divided solid tending to accumulate towards the bottom of the mixture after mixing.
One preferred class of solids is the hydraulic cements, e.g. gypsum and plaster, but not Portland cement because of its alkalinity. These solids will tend to react with water present in the reaction mixture to produce a hardened skeletal structure within the cured resin product. Moreover, the reaction with the water is also exothermic and assists in the foaming and curing reaction. Foamed products obtained using these materials have particularly valuable physical properties. Moreover, when exposed to flame even for long periods of time they tend to char to a brick-like consistency that is still strong and capable of supporting loads. The products also have excellent thermal insulation and energy absorption properties. The preferred amount of inert particulate solid is from 20 to 200 parts by weight per 100 parts by weight of resole.
Another class of solids that is preferred because its use yields products having properties similar to those obtained using hydraulic cements comprises talc and fly ash.
The preferred amounts of these solids are also 20 to 200 parts by weight per 100 parts by weight of resole.
For the above classes of solid, the most preferred range is 50 to 150 parts per 100 parts of resole.
Thixotropic foam-forming mixtures can be obtained if a very finely dMded solid such as Aerosil (finely divided silica) is included.
If a finely divided metal powder is included, electrically conducting properties can be obtained. The metal powder is preferably used in amounts of from 50 to 250 parts per parts by weight of resole.
In general, the maximum amount of solid that can be employed is controlled only by the physical problem of inCorporating it into the mixture and handling the mixture. In general it is desired that the mixture is pourable but even at quite high solids concentrations1 when the mixture is like a dough or paste and cannot be poured, foamed products with valuable properties can be obtained.
In general, it is preferred to use the fibrous solids only in conjunction with a non-fibrous solid since otherwise the foam texture tends to be poorer.
Other additives may be included in the foam-forming mixture; e.g. surfactants, such as anionic materials e.g. sodium salts of long chain alkyl bonzene sulfonic acids, non-ionic materials such as those based on poly(ethylene oxide) or copolymers thereof, and cationic materials such as long chain quaternary amrnonium compounds or those based on polyacrylamides; viscosity modifiers such as alkyl cellulose especially methyl cellulose, and colorants such as dyes or pigments. Plasticisers for phenolic resins may also be included provided the curing and foaming reactions are not suppressed thereby, and polyfunctional compounds other than the dihydric compounds referred to above may be included which take part in the cross-linking reaction which occurs in curing; e.g. di-or poly-amines, di-or poly-isocyanates, di-or poly-carboxylic acids and aminoalcohols.
Polymerisable unsaturated compounds may also be included possibly together with free-radical pol\,lTlerisation initiators that are activated during the curing action e.g. acrylic monomers, so-called urethane acrylates, styrene, maleic acid and derivatives thereof, and mixtures thereof.
Other resins may be included e.g. as prepolymers which are cured during the foaming and curing reaction or as powders, emulsions or dispersions. Examples are polyacetals such as polyvinyl acetals, vinyl polymers, olef in polymers, polyesters.
acrylic polymers and styrene polymers, polyurethanes and prepolyrners thereof and polyester prepolymers, as well as melamine resins, phenolic novolaks, etc. Conventional blowing agents may also be included to enhance the foaming reaction, e.g. low boiling organic compounds or compounds which decompose or react to produce gases.
The foam-forming compositions may also contain dehydrators, if desired.
A preferred method of forming the foam-forming composition comprises lirst mixing the resole and inert tiller to obtain a substantially uniform dispersion of the filler in the resole, and thereafter adding the hardener. Uniform distribution of both the filler and the hardener throughout the composition is essential for the production of uniformly textured foam products and therefore thorough mixing is required.
If it is desired that the composition is at elevated temperature prior to commencement of the exothermic reaction, this can be achieved by heating the resole or first mixing the resole and the solid and then heating the mixture. Preferably the solid is added to the resole just before the addition of the hardener. Alternatively, the mixture of resole, solid and hardener may be prepared and the whole mixture then heated, e.g. by short wave irradiation, preferably after it has been charged to a mould. A conventional radiant heat mixture by this means.
Preferably, the foam has a density in the range 75 to 500 kg/rn3, more preferably 100 to 400 kg/rn3 and most preferably 100 to 250 kg/rn3. Foam cell size is also important because up to a limit the larger the size of the cell for a given density, the thicker will be the walls and hence the greater the physical strength of the foam. However if the cell size is too large, the strength begins to suffer. Preferably, the cell size is in the range of ito 3mm.
It will be understood that the present invention has been described above purely by way of example, and modification of detail can be made within the scope of the invention.
In particular, the examples above have been described in relation to the manufacture of panels, in particular the manufacture of doors. However, it should be appreciated that the invention has very wide application including other products. Indeed it is envisaged that an extremely wide range of products could be made in accordance with methods of the present invention. Many moulded products could be made using the methods of the present invention, even where those products may currently be manufactured using -.34 -different materials (for example wood, metal, porcelain) at present. In addition to building products, it is envisaged that for example, the invention could find application to vehicle parts and fittings, casings for electrical equipment and many household items of which furniture, picture frames, chairs, tables, lamp bases, vases, bowls are only a
few examples.
Each feature disclosed in the description, and (where appropriate) the claims and drawings may be provided independently or in any appropriate combination.

Claims (28)

  1. :c%.....%..÷..:r..,..., *..-**%%** ... *.......Claims 35 1. A method of providing a laminate armoured or bullet-proof shield, the method comprising: applying a substrate including a porous structure to a first surface of a layer comprising a sheet-form curable material; applying a veneer element to a second surface of the sheet-form material; providing one or more reinforcement fibres selected from carbon fibres, glass fibres, aramid fibres and/or polyethylene fibres; and applying pressure to press the veneer element, the sheet-form material, the reinforcement fibres and the substrate together to form the laminate shield.
  2. 2. A method according to claim 1, wherein the reinforcement fibres are provided as an integral part of the sheet-form material.
  3. 3. A method according to claim 1 or claim 2, wherein the reinforcement fibres are provided as a separate layer.
  4. 4. A method according to claim 3, wherein the reinforcement fibres are provided as one or more layers.
  5. 5. A method according to claim 3, wherein the reinforcement fibres are arranged between thesheet-formcurable-ma-terialancl-the-substrate. -------- 6. A method according to any preceding claim, wherein the fibres are short fibres.7. A method according to any of claims ito 5, wherein the fibres are long fibres.8. A method according to any preceding claim, wherein the fibres are arranged uni-or multi-directionally.9. A method according to any preceding claim, wherein the fibres are arranged in a fabric, mat, felt or woven arrangement.10. A method according to any preceding claim, wherein the fibres are Kevlar (RTM) fibres.ii. A method according to any preceding claim, wherein the fibres are located across the whole of the substrate.12. A method according to any preceding claim, wherein curable material flows into the veneer element during the pressing step.13. A method according to any preceding claim, wherein the configuration of the substrate is such that gas and/or vapour can be displaced from the pressing region.* . -. -. .... . --... 4.* .< .-*-..:.. .\C-. .t. ... ... -. -: . ... .-*. .. -.14. A method according to claim 13, wherein the substrate includes a material having an open-cell structure.15. A method according to any preceding claim) wherein the substrate is foamed phenolic resin.16. A method according to claim 15, wherein the substate comprises finely divided organic, inorganic or metallic particles.17. A method according to any preceding claim, wherein the substrate is a frangible material.18. A method according to any preceding claim, wherein the sheet-form material includes a sheet moulding compound (SMC).19. A method according to any preceding claim, wherein during pressing, the sheet-form curable material is mechanically keyed into the surface of the substrate.20. A method according to any of claims 1 to 18, wherein during pressing, the sheet-form curable material extends into the surface of the substrate.21. A method according to any preceding claim, wherein the sheet-form curable material is applied to substantially a whole mould surface.22. A method according to any preceding claim, wherein the method includes the step of ----providing a-condr incluthna-sheet-formmat-Erfaapplying thcond lafaUrce of the substrate, the substrate being sandwiched between the first and second layers of sheet-form material, and pressing the second layer and the substrate together.23. A method according to any preceding claim, wherein the thickness of the veneer is 5mm or less, preferably 3mm or less.24. A method according to any preceding claim, wherein a plurality of veneer elements are provided on the sheet material to form a veneer layer.25. A laminate armoured or bullet-proof shield made by a method of any of claims 1 to 24.26. A laminate armoured or bullet-proof shield comprising a porous substrate and a skin of sheet form material bonded to a surface of the substrate such that the sheet-form curable material extends into the surface of the substrate, further including a veneer bonded to a surface of the skin of sheet-form material, and additionally comprising one or more reinforcement fibres selected from carbon fibres, glass fibres, aramid fibres and/or polyethylene fibres.:.,7.: 27. A laminate according to claim 26, wherein the reinforcement fibres are provided as an integral part of the sheet-form material.28. A laminate according to claim 26 or claim 27, wherein the reinforcement fibres are provided as a separate layer.29. A laminate according to c laim 28, wherein the reinforcement fibres are arranged between the sheet-form curable material and the substrate 30. A method and/or laminate substantially as herein described with reference to the accompanying drawings.AMENDMENTS TO CLAIMS HAVE BEEN FILED AS FOLLOWSClaims 1. A method of providing a laminate armoured or bullet-proof shield, the method comprising: applying a substrate including a porous structure to a first surface of a layer comprising a sheet-form curable material; applying a veneer element to a second surface of the sheet-form material; providing one or more reinforcement fibres selected from carbon fibres, glass fibres, aramid fibres and/or polyethylene fibres; and applying pressure to press the veneer element, the sheet-form material, the reinforcement fibres and the substrate together to form the laminate shield.2. A method according to claim 1, wherein the reinforcement fibres are provided as an integral part of the sheet-form material.3. A method according to claim 1 or claim 2, wherein the reinforcement fibres are provided as a separate layer.4. A method according to claim 3, wherein the reinforcement fibres are provided as one r or more layers.(\,j 5. A method according to claim 3, wherein the reinforcement fibres are arranged between the sheet-form curable material and the substrate.
  6. 6. A method according to any preceding claim, wherein the fibres are arranged unidirectionally.
  7. 7. A method according to any of claims 1 to 5, wheiein the fibres are arranged multi-directionally.
  8. 8. A method according to any preceding claim, wherein the fibres are arranged in a fabric, mat, felt or woven arrangement.
  9. 9. A method according to any preceding claim, wherein the fibres are aramid fibres.
  10. 10. A method according to any preceding claim, wherein the fibres are located across the whole of the surface of the substrate.
  11. 11. A method according to any preceding claim, wherein curable material flows into the veneer element during the pressing step.
  12. 12. A method according to any preceding claim, wherein the configuration of the substrate is such that gas and/or vapour can be displaced from the pressing region.
  13. 13. A method according to claim 12, wherein the substrate includes a material having an open-cell structure.
  14. 14. A method according to any preceding claim, wherein the substrate is foamed phenolic resin.
  15. 15. A method according to claim 14, wherein the substrate comprises finely divided organic, inorganic or metallic particles.
  16. 16. A method according to any preceding claim, wherein the substrate is a frangible material.
  17. 17. A method according to any preceding claim, wherein the sheet-form material includes a sheet moulding compound (SMC).
  18. 18. A method according to any preceding claim, wherein the veneer element, the sheet-form material, the reinforcement fibres and the substrate are pressed together between moulds and wherein the sheet-form curable material is applied to substantially a whole r mould surface.
  19. 19. A method according to any preceding claim, wherein the method includes the step of providing a second layer including a sheet-form material, applying the second layer at a surface of the substrate, the substrate being sandwiched between the first and second layers of sheet-form material, and pressing the second layer and the substrate together.
  20. 20. A method according to any preceding claim, wherein the thickness of the veneer is 5mm or less.
  21. 21. A method according to any preceding claim, wherein the thickness of the veneer is 3mm or less.
  22. 22. A method according to any preceding claim, wherein a plurality of veneer elements are provided on the sheet material to form a veneer layer.
  23. 23. A laminate armoured or bullet-proof shield made by a method of any of claims 1 to 22.
  24. 24. A laminate armoured or bullet-proof shield comprising a porous substrate and a skin of sheet form material bonded to a surface of the substrate such that the sheet-form material extends into the surface of the substrate, further including a veneer bonded to a surface of the skin of sheet-form material, and additionally comprising one or more reinforcement fibres selected trom carbon fibres, glass fibres, aramid fibres and/or polyethylene fibres.
  25. 25. A laminate according to claim 24, wherein the reinforcement fibres are provided as an integral part of the sheet-form material.
  26. 26. A laminate according to claim 24 or claim 25, wherein the reinforcement fibres are provided as a separate layer.
  27. 27. A laminate according to claim 26, wherein the reinforcement fibres are arranged between the sheet-form material and the substrate.C')
  28. 28. A method and/or laminate substantially as herein described with reference to the accompanying drawings. r r
GB201315418A 2008-10-20 2008-10-20 Laminate Products Expired - Fee Related GB2504012B8 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016016621A1 (en) * 2014-07-31 2016-02-04 Ecotechnilin Ltd Layered composite structure

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2453308B (en) 2007-10-03 2012-07-25 Acell Group Ltd Composite products
GB2482030B (en) * 2010-07-16 2015-11-04 Acell Ind Ltd Composite materials and uses thereof
GB2491415B (en) * 2011-06-03 2018-02-07 Albertelli Aldino A modular building with a triangular profile
ITTV20130043A1 (en) * 2013-04-03 2014-10-04 Enrico Pillon METHOD OF PRODUCTION OF A BUFFER PANEL FOR SIMILAR DOORS AND WINDOWS
DE102013113125A1 (en) 2013-11-27 2015-05-28 Guido Schulte Floor, wall or ceiling panel and method of making the same
DE102013113109A1 (en) 2013-11-27 2015-06-11 Guido Schulte floorboard
DE102013113130B4 (en) 2013-11-27 2022-01-27 Välinge Innovation AB Method of manufacturing a floorboard
UA121544C2 (en) 2014-01-10 2020-06-25 Велінге Інновейшн Аб A method of producing a veneered element
WO2015174909A1 (en) 2014-05-12 2015-11-19 Välinge Innovation AB A method of producing a veneered element and such a veneered element
US11313123B2 (en) 2015-06-16 2022-04-26 Valinge Innovation Ab Method of forming a building panel or surface element and such a building panel and surface element
CA3185645A1 (en) 2016-04-25 2017-11-02 Valinge Innovation Ab A veneered element and method of producing such a veneered element
WO2019004952A1 (en) * 2017-06-29 2019-01-03 Karapinar Coskun Production of decorative and customized products using composite materials
CA3085983A1 (en) 2018-01-11 2019-07-18 Valinge Innovation Ab A method to produce a veneered element and a veneered element
WO2019139522A1 (en) 2018-01-11 2019-07-18 Välinge Innovation AB A method to produce a veneered element and a veneered element
WO2020145870A1 (en) 2019-01-09 2020-07-16 Välinge Innovation AB A method to produce a veneer element and a veneer element

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5142835A (en) * 1990-10-12 1992-09-01 Taylor Building Products Company Reaction injection molded door assembly
WO1999035364A1 (en) * 1998-01-08 1999-07-15 Acell Holdings Limited Weather resistant panels
EP1022400A1 (en) * 1997-09-26 2000-07-26 Ibiden Co., Ltd. Composite refractory building material, method of manufacturing the same, gypsum board, and resin composition
EP1110712A1 (en) * 1998-08-07 2001-06-27 Toho Rayon Co., Ltd. Reinforcing material for wood and reinforced wood

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60180823A (en) * 1984-02-29 1985-09-14 Sadao Nishibori Formation of wood-like decorative panel
JPH04103635A (en) * 1990-08-22 1992-04-06 Aica Kogyo Co Ltd Production of internal trim material
JP2854855B1 (en) * 1998-02-13 1999-02-10 親和ツキ板株式会社 Manufacturing method of natural wood decorative metal plate and natural wood decorative metal plate

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5142835A (en) * 1990-10-12 1992-09-01 Taylor Building Products Company Reaction injection molded door assembly
EP1022400A1 (en) * 1997-09-26 2000-07-26 Ibiden Co., Ltd. Composite refractory building material, method of manufacturing the same, gypsum board, and resin composition
WO1999035364A1 (en) * 1998-01-08 1999-07-15 Acell Holdings Limited Weather resistant panels
EP1110712A1 (en) * 1998-08-07 2001-06-27 Toho Rayon Co., Ltd. Reinforcing material for wood and reinforced wood

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016016621A1 (en) * 2014-07-31 2016-02-04 Ecotechnilin Ltd Layered composite structure
GB2529061B (en) * 2014-07-31 2017-06-14 Ecotechnilin Ltd Layered composite structure with veneer

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GB2464541A (en) 2010-04-28
GB201315418D0 (en) 2013-10-16
GB2464541B (en) 2014-02-19
GB0819212D0 (en) 2008-11-26
GB2504012B8 (en) 2014-08-27
GB2504012B (en) 2014-03-12

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