GB2174644A - Production of a laminate - Google Patents

Production of a laminate Download PDF

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Publication number
GB2174644A
GB2174644A GB08611333A GB8611333A GB2174644A GB 2174644 A GB2174644 A GB 2174644A GB 08611333 A GB08611333 A GB 08611333A GB 8611333 A GB8611333 A GB 8611333A GB 2174644 A GB2174644 A GB 2174644A
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United Kingdom
Prior art keywords
sheets
resin material
liquid resin
assembly
laminate
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Granted
Application number
GB08611333A
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GB2174644B (en
GB8611333D0 (en
Inventor
James Arthur Albert Hickman
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Individual
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Individual
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Filing date
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Priority claimed from GB858511707A external-priority patent/GB8511707D0/en
Application filed by Individual filed Critical Individual
Publication of GB8611333D0 publication Critical patent/GB8611333D0/en
Priority claimed from EP86306959A external-priority patent/EP0259528A3/en
Publication of GB2174644A publication Critical patent/GB2174644A/en
Application granted granted Critical
Publication of GB2174644B publication Critical patent/GB2174644B/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C39/00Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
    • B29C39/02Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C39/12Making multilayered or multicoloured articles
    • B29C39/123Making multilayered articles
    • B29C39/126Making multilayered articles by casting between two preformed layers, e.g. deformable 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
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • 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
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/20Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • 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
    • B32B37/24Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer not being coherent before laminating, e.g. made up from granular material sprinkled onto a substrate
    • 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
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/006Degassing moulding material or draining off gas during moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2067/00Use of polyesters or derivatives thereof, as moulding material
    • B29K2067/06Unsaturated polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/02Aluminium
    • 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
    • B32B2311/00Metals, their alloys or their compounds
    • B32B2311/24Aluminium

Landscapes

  • Laminated Bodies (AREA)
  • Adhesives Or Adhesive Processes (AREA)

Abstract

A method of producing a laminate comprising forming an assembly of spaced apart first and second preformed sheets, at least one of which is metallic, the assembly having a barrier to passage of liquid resin material between the sheets around at least a lower part of the periphery of the assembly, pouring flowable, settable liquid resin material between the sheets through an upper peripheral edge of the assembly and allowing the introduced resin material to set to bond the sheets together.

Description

SPECIFICATION Production of a laminate This invention relates to a method of producing a laminate comprising forming an assembly of first and second preformed sheets which are spaced apart from each other to define a space therebetween and which have a barrier to passage of liquid resin material between the sheets around at least a lower part of the periphery of the assembly, pouring flowable, settable liquid resin material between the sheets through an upper peripheral edge of the assembly, arranging the assembly so that the introduced resin material flows into, and fills the space between, the sheets and allowing the introduced resin material to set thereby bonding the first and second preformed sheets together.Hereinafter such a method will be referred to as a "method of the kind referred to". The invention also relates to a laminate produced by such a method.
It is already known in GB-A-2,155,856 to produce a transparent or translucent glazing unit by a known method of the kind referred to. In this known method the first and second preformed sheets comprise glazing sheets, e.g. of glass and/or polycarbonate or acrylic material.
It is also known from US-A-3,560,285 to produce a metallic laminate by injecting foamable material, e.g. urethane, styrene or epoxy resin material, between thin, spaced apart aluminium facings. However, in this known method, the use of foamed adhesive presents certain problems since the facing aluminium sheets have to be well supported during injection and subsequent setting to prevent distortion of the laminate. Furthermore the presence of many gas bubbles in the foamed adhesive leads to a laminate having an interlayer which provides a relatively weak joint due to the presence of the many voids and interstices in the finished product. In addition it is often difficult to accurately control the injection of foamed material into narrow spaces to ensure consistency in the distribution of the injected material.
The present invention aims to provide a method of the kind referred to for producing a laminate in which at least one sheet is metallic.
According to one aspect of the present invention, a method of the kind referred to is characterised in that at least one of the said first and second preformed sheets is metallic.
The method according to the invention does not employ foamed material as a laminate interlayer but instead uses a curable liquid resin material which is poured between the spaced apart first and second preformed sheets. To ensure good flow, the viscosity of the liquid resin material when poured is comparatively low.
Conveniently both the first and second preformed sheets are metallic, e.g. aluminium.
Suitably the first and second preformed sheets are flat and are typically rectangular.
Typically each of the said sheets has a thickness of approximately 2 mm and the sheets of the said assembly are conveniently spaced up to 6 mm apart, preferably from 1 mm to 2 mm apart.
If the said assembly is flat it is preferably inclined to the horizontal at an angle, e.g. of from 150 to 65 , typically from 200 to 40 , during pouring of the settable liquid resin through an upper peripheral edge of the assembly.
Preferably the said barrier is provided by adhesive strip material which is sandwiched between the said sheets adjacent the periphery of the assembly. The strip material is preferably flexible, e.g. double-sided adhesive tape, and may be gas-permeable or non-permeable to gas.
Any suitable liquid resin material may be used to fill the space between the said sheets. Typically the liquid resin material comprises a pre-mixed liquid adhesive-catalyst system which may be room temperature curing or heat curing. The viscosity of the liquid resin material during pouring should be relatively low, e.g. no more than about 25 cSt, to ensure good flow of liquid material between the sheets during the pouring step. A particularly preferred resin material is obtained by mixing, e.g. hand mixing, "Naftolan Resin S696" or "Naftolan Resin 5700" with catalysts designated "K66", "K206" and "K73" (the designated resins and catalysts are manufactured by Degussa AG, Deschaftsbereich Chemie, Frankfurt, West Germany and distributed by Chemetall, Gesellschaft Technische Verfahren mbH Sparte Glas Reutervey 14, Frankfurt, West Germany.
There are substantial advantages in laminating together comparatively thin sheets to provide a relatively thick composite laminate. For example two flat, rectangular sheets of aluminium, each approximately 2 mm in thickness and either mill finished or anodised, may be bonded together with a resin interlayer of up to 6 mm to provide a composite laminate having an overall thickness of up to 10 mm.
A thick aluminium-resin-aluminium laminate (e.g. up to 10 mm thick) is considerably cheaper to produce than a similar thickness sheet of solid aluminium and can be cut and/or worked more easily. It is not, of course, essential for the laminated sheets to be flat and thus bent, curved or otherwise shaped metallic sheets can be laminated together to form relatively thick shaped forms which would otherwise have been costly and/or extremely difficult to produce in solid metal form.
Although the first and second preformed sheets are typically both metallic, e.g. alumi nium, it is also possible for one of the sheets to be metallic and the other sheet to be glass, polywarbonate, acrylic, any other preformed re sin based sheet material, or any other sheet material to which the liquid resin material will bond when set.
According to another aspect of the present invention, a laminate comprising spaced apart first and second preformed sheets, at least one of which is metallic, bonded together by a resin material poured in liquid form between an assembly of said first and second preformed sheets and allowed to set.
An embodiment of the invention will now be described, by way of example, with reference to the following Example.
EXAMPLE First and second rectangular sheets of anodised aluminium, typically each having a length of 1 m, a width of 1 m and a thickness of 2 mm, were thoroughly cleaned. The first aluminium sheet was then laid in a horizontal position to enable lengths of flexible, double-sided adhesive strip material to be applied thereto.
The strip material conveniently had pressuresensitive adhesive coatings on either of its sides covered by non-adhesive backing layers.
Prior to application of the adhesive strip material, one of these backing layers was removed to reveal one of the pressure-sensitive adhesive coatings. The strip material was then adhered to the upwardly facing surface of the first aluminium sheet around first, second, third and fourth peripheral'sides of the latter.
The opposite ends of the strip material applied to the second peripheral side were butt jointed to respective end portions of the strip material applied to the first and third peripheral sides. However, the opposite ends of the strip material applied to the fourth peripheral side were spaced slightly from the respective end portions of the strip material applied to the first and third peripheral sides to form a pair of spaced apart "air gaps" in the peripherally applied strip material.
The second aluminium sheet was then positioned above the first aluminium sheet, in face-to-face relationship therewith, and was carefully lowered onto the strip material adhered to the first aluminium sheet so that the adhesive strip material was sandwiched between the two aluminium sheets. The adhesive strip material thus served to space the first and second aluminium sheets apart a distance of approximately 2 mm. The other layer of backing paper was then removed from the adhesive strip material applied to the first, second and third peripheral sides (but not the fourth peripheral side) of the first aluminium sheet and the two aluminium sheets were firmly pressed together along these three sides.
The strip material applied along the first, second and third peripheral sides formed a continuous barrier to passage of liquid resin material. Any gap in this barrier was sealed, e.g. with mastic, at this stage.
The assembly of aluminium sheets was then raised into an inclined position with its unsealed edge (i.e. along the fourth peripheral side of the first aluminium sheet) uppermost.
Typically, the assembly was inclined at an angle of from 15 to 65', preferably from 20" to 40 , e.g. 30 , to the horizontal. The unsealed edge of the second aluminium sheet was carefully lifted from the underlying backing layer of the adhesive strip applied to the fourth peripheral side of the first aluminium sheet and a broad but thin spout of a funnel was inserted between the new slightly spaced apart second aluminium sheet and strip material to permit previously prepared flowable, settable liquid resin material, e.g. a premixed, liquid adhesive-catalyst system, to be poured through the funnel downwardly between the aluminium sheets.
The settable liquid resin material was prepared by a so-called hand mixing process invoving the hand mixing or stirring of a low viscosity liquid resin with at least one catalyst.
A particularly preferred resin material is methacrylate resin, e.g. obtained by mixing, typically hand mixing, "Naftolan Resin 5696" or "Naftolan Resin 5700" with catalysts designated "K66", "K206" and "K73". This provides a liquid resin material which is of extremely low viscosity compared with other known resin materials.
The volume of resin material required to bond the aluminium together was calculated by multiplying the surface area of one side of one of the aluminium sheets by the desired interlayer thickness. The calculated volume was adjusted slightly to allow for slight shrinkage during setting of the resin material.
The predetermined quantity of selected resin "5696" or "5700" was then measured out by being slowly poured into a measuring beaker and was allowed to degas sufficiently to ensure few micro bubbles were held in the basic resin, the actual rate of degassing being dependent on the temperature of the operating environment.
When the selected resin was clear, and had no or little trapped air therein, the catalysts were slowly poured into the resin and gently, but thoroughly, manually stirred, i.e. with the aid of a hand held stirrer. Care was taken to ensure adequate mixing without causing too many air micro bubbles to be generated. The stirred mixture was then allowed to stand to enable dispersion of bubbles generated during mixing.
Catalysts "K206" and "K66" were then added to the selected resin, suitably at a ratio of 100:1 by volume, and catalyst "K73" was added to the resin suitably at a ratio of 100:0.5 by volume. However, these ratios are only an approximate guide and can be substantially altered to affect clarity, strength and curing rate of the resin material.
The curing rate of the liquid resin material with hand mixing is influenced by the operating temperature, which should ideally be between 1 50C and 25 C. At temperatures under 1 50C the ratio of resin and catalyst must be altered to effect proper curing. At temperatures below 1 0C the hand mix ratio of resin and catalysts must be altered and further curing can only be effected by applying heat to the filled laminate for a minimum of 120 minutes.
By using liquid resin having a relatively low viscosity, a homogeneous mixture of liquid resin and catalyst(s) can be obtained by a hand mixing process-i.e. by the use of a hand held stirrer-and does not involve the use of expensive mixing machinery. This means that a laminate can be produced with minimal capital expenditure for machinery. Furthermore the relatively low viscosity of the resin/catalyst mixture enables at least most of the bubbles (e.g. micro bubbles) created by the hand mixing to dissipate freely without the use of additional degassing equipment (e.g. heating equipment or a vacuum pump).
The measured quantity of degassed resin and catalysts was then poured through the funnel between the inclined assembly of aluminium sheets care being taken to ensure a slow even pour into the centre of the interspace between the panels. The liquid resin material flowed downwardly and outwardly, with the upper corners of the interspace, in the region of the previously mentioned air gaps left substantially unfilled.
After the predetermined, measured amount of liquid resin material had been introduced into the interspace between the aluminium sheets, the funnel was withdrawn ensuring that little or no resin material dripped over the backing layer of the adhesive strip applied to the fourth peripheral side of the first aluminium sheet. Then the backing layer was carefully, manually, pulled away from this adhesive strip and the second aluminium sheet was pressed firmly against the revealed adhesive surface of the adhesive strip to ensure good adhesion thereto. At this stage the aluminium sheets bulged apart slightly, and the liquid resin material only partly filled the interspace therebetween.
The assembly of aluminium sheets was then lowered to a horizontal position and air in the sheet interspace was allowed to evacuate naturally through the air gaps. It was important to ensure that the assembly was positioned horizontally as soon as possible after the liquid resin material had been poured into the interspace between the aluminium sheets so that the resin material was still in a flowable state.
When the aluminium sheets were in the horizontal position, the weight of the upper sheet caused the liquid resin material to spread out to provide an even thickness interlayer between the sheets. Initially the liquid resin material flowed back over the lower aluminium sheet along a path of least liquid flow resistance, i.e. over the part of the sheet previously "wetted" or "lubricated" by the resin material as it was poured into the interspace.
After a short time the liquid resin material met the adhesive strip applied along the fourth peripheral side and then gradually spread outwardly towards the unfilled corners of the interspace thereby expelling air from the interspace through the air gaps. When the interspace was completely filled with an even thickness of resin material and the air was fully evacuated from between the aluminium sheets, typically after approximately 2 minutes, the air gaps were sealed, e.g. with mastic, and the resin material was allowed to cure (with the assembly still in a horizontal position) for approximately 3 to 6 hours at normal room temperature. In view of the thickness of the resin interlayer, it was found advisable to cool the sheet assembly, e.g. by air or water, during curing of the resin material.
An aluminium-resin-aluminium laminate was thus produced having a thickness of approximately 6 mm. The laminate was found to be easier to cut and work than a solid sheet of aluminium of the same thickness. The resin interlayer contained few voids and provided a strong joint.
It will be appreciated that, especially in the case of extra long aluminium sheets, it may be necessary to have a number of spaced apart filling points along the upper edge of the periphery of the aluminium sheets. For example two or more funnels could be employed for introducing liquid resin material into the interspace between the aluminium sheets.
In this case, however, it is necessary to provide at least one air gap in the peripheral seal between each pair of adjacent resin filling points.
In the above-described Example, the adhesive strip material sandwiched between the aluminium sheets around the periphery thereof spaces the sheets apart and blocks the passage of the liquid resin material therethrough when the latter is poured between the sheets and during the setting of the resin material.
The strip material may be impervious to gas at least to the extent that air expelled from between the aluminium sheets as the liquid resin material spreads between the sheets will not pass through the strip material but will be forced to pass out through the air gaps. A particularly suitable adhesive strip material is a polyurethane tape known as "Normount V2500" (a trade name of the U.S. company Norton Performance Plastics). However other types of strip material, e.g. gas-permeable strip material, may be employed.
It will be appreciated that, unlike forming laminated glass, in the formation of an opaque laminate, e.g. comprising two metallic sheets bonded together by a resin interlayer, it is not essential for the liquid resin material introduced between the spaced apart sheets to be entirely free of bubbles since the resin interlayer formed is not visible. It is important, however, that there are not a sufficient number of air bubbles present to weaken the interlayer.
It has been previously proposed to inject foamed adhesive between spaced apart sheets, the foamed adhesive expanding as it sets to produce an expanded foam interlayer.
The method described above differs from such known methods in that the introduced liquid resin material does not expand as it sets and thus produces an at least substantially noncellular sheet-bonding layer. This is advantageous in that it is strong, and does not force the sheets apart as it sets. Furthermore it is easy to calculate the volume of resin material to be introduced between the sheets as no expansion of the resin material occurs during curing.
Although methacrylate resin is a preferred liquid resin material for pouring between spaced apart sheets to be laminated together, it is possible to use other resin materials, such as polyester resins, in applications where attributes, such as lack of clarity and ultra violet stability, are not important. This may be the case, for example, in metal to metal laminates. The flowability of the liquid resin material during pouring is important and will be dependent, to some extent, on the spacing apart of the sheets to be laminated together.
However to ensure good flow characteristics, even when the sheets are spaced a small distance apart, the liquid resin material during pouring should have a relatively low kinematic viscosity-for example less than about 25 cSt (centistokes) at the pouring temperature (typically 20 C). Preferably the kinematic viscosity, at 20 C, should be no more than 15 cSt and acceptable results have been achieved with the liquid resin material having a kinematic viscosity of 14.2 cSt at 20 C. However, the best results have been achieved with a liquid resin material having a kinematic viscosity at 20-C of less than 5 cSt, typically 3.1 cSt.
The sheets may be positioned in a vertical position during application of the adhesive strip and/or during resin pouring. However, it is preferable for the resin material to set with the sheets in a lowered, e.g. horizontal, position.
As previously mentioned the adhesive strip may be in the form of gas-permeable tape or strip material. In this case air gaps need not be provided, air being expelled through the tape when the laminate assembly is lowered to its resin-setting position. A particularly suitable type of gas-permeable tape is marketed by 3M under the trade name "Scotchmount".
1. A method of producing a laminate comprising forming an assembly of first and second preformed sheets which are spaced apart from each other to define a space therebetween and which have a barrier to passage of liquid resin material between the sheets around at least a lower part of the periphery of the assembly, pouring flowable, settable liquid resin material between the sheets through an upper peripheral edge of the assembly, arranging the assembly so that the introduced liquid resin material flows into, and fills the space between, the sheets and allowing the introduced resin material to set thereby bonding the first and second preformed sheets together, characterised in that at least one of the said first and second preformed sheets is metallic.
2. A method according to claim 1, in which the sheets are spaced apart a distance of up to 6 mm.
3. A method according to claim 1 or 2, in which the sheets are spaced apart a distance of from 1 mm to 2 mm.
4. A method according to any of claims 1 to 3, in which both the first and second preformed sheets are metallic.
5. A method according to any of claims 1 to 3, in which one or both of the first and second preformed sheets is or are aluminium.
6. A method according to any of the preceding claims, in which the said assembly is inclined to the horizontal at an angle of from 150 to 65", preferably 20" to 40 , during pouring of the liquid resin material between the sheets.
7. A method according to any of claims 1 to 3, in which one of said sheets is nonmetallic.
8. A method according to any of the preceding claims, in which the said barrier is provided by adhesive strip material sandwiched between the said sheets adjacent the periphery of the assembly.
9. A method according to claim 8, in which the adhesive strip material is flexible.
10. A method according to claim 7 or 8, in which the adhesive strip material is at least substantially gas impermeable.
11. A method according to any of the preceding claims, in which the said resin material comprises methacrylate resin.
12. A method according to any of the preceding claims, in which the said liquid resin material has a kinematic viscosity of less than 25 cSt when it is poured between said sheets.
13. A method according to claim 12, in which the kinematic viscosity of said liquid resin material at 20-C is no more than 15 cSt, preferably no more than 5 cSt.
14. A method of producing a laminate substantially as herein described with reference to the foregoing Example.
15. A laminate produced by the method ac
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (16)

**WARNING** start of CLMS field may overlap end of DESC **. It will be appreciated that, unlike forming laminated glass, in the formation of an opaque laminate, e.g. comprising two metallic sheets bonded together by a resin interlayer, it is not essential for the liquid resin material introduced between the spaced apart sheets to be entirely free of bubbles since the resin interlayer formed is not visible. It is important, however, that there are not a sufficient number of air bubbles present to weaken the interlayer. It has been previously proposed to inject foamed adhesive between spaced apart sheets, the foamed adhesive expanding as it sets to produce an expanded foam interlayer. The method described above differs from such known methods in that the introduced liquid resin material does not expand as it sets and thus produces an at least substantially noncellular sheet-bonding layer. This is advantageous in that it is strong, and does not force the sheets apart as it sets. Furthermore it is easy to calculate the volume of resin material to be introduced between the sheets as no expansion of the resin material occurs during curing. Although methacrylate resin is a preferred liquid resin material for pouring between spaced apart sheets to be laminated together, it is possible to use other resin materials, such as polyester resins, in applications where attributes, such as lack of clarity and ultra violet stability, are not important. This may be the case, for example, in metal to metal laminates. The flowability of the liquid resin material during pouring is important and will be dependent, to some extent, on the spacing apart of the sheets to be laminated together. However to ensure good flow characteristics, even when the sheets are spaced a small distance apart, the liquid resin material during pouring should have a relatively low kinematic viscosity-for example less than about 25 cSt (centistokes) at the pouring temperature (typically 20 C). Preferably the kinematic viscosity, at 20 C, should be no more than 15 cSt and acceptable results have been achieved with the liquid resin material having a kinematic viscosity of 14.2 cSt at 20 C. However, the best results have been achieved with a liquid resin material having a kinematic viscosity at 20-C of less than 5 cSt, typically 3.1 cSt. The sheets may be positioned in a vertical position during application of the adhesive strip and/or during resin pouring. However, it is preferable for the resin material to set with the sheets in a lowered, e.g. horizontal, position. As previously mentioned the adhesive strip may be in the form of gas-permeable tape or strip material. In this case air gaps need not be provided, air being expelled through the tape when the laminate assembly is lowered to its resin-setting position. A particularly suitable type of gas-permeable tape is marketed by 3M under the trade name "Scotchmount".
1. A method of producing a laminate comprising forming an assembly of first and second preformed sheets which are spaced apart from each other to define a space therebetween and which have a barrier to passage of liquid resin material between the sheets around at least a lower part of the periphery of the assembly, pouring flowable, settable liquid resin material between the sheets through an upper peripheral edge of the assembly, arranging the assembly so that the introduced liquid resin material flows into, and fills the space between, the sheets and allowing the introduced resin material to set thereby bonding the first and second preformed sheets together, characterised in that at least one of the said first and second preformed sheets is metallic.
2. A method according to claim 1, in which the sheets are spaced apart a distance of up to 6 mm.
3. A method according to claim 1 or 2, in which the sheets are spaced apart a distance of from 1 mm to 2 mm.
4. A method according to any of claims 1 to 3, in which both the first and second preformed sheets are metallic.
5. A method according to any of claims 1 to 3, in which one or both of the first and second preformed sheets is or are aluminium.
6. A method according to any of the preceding claims, in which the said assembly is inclined to the horizontal at an angle of from 150 to 65", preferably 20" to 40 , during pouring of the liquid resin material between the sheets.
7. A method according to any of claims 1 to 3, in which one of said sheets is nonmetallic.
8. A method according to any of the preceding claims, in which the said barrier is provided by adhesive strip material sandwiched between the said sheets adjacent the periphery of the assembly.
9. A method according to claim 8, in which the adhesive strip material is flexible.
10. A method according to claim 7 or 8, in which the adhesive strip material is at least substantially gas impermeable.
11. A method according to any of the preceding claims, in which the said resin material comprises methacrylate resin.
12. A method according to any of the preceding claims, in which the said liquid resin material has a kinematic viscosity of less than 25 cSt when it is poured between said sheets.
13. A method according to claim 12, in which the kinematic viscosity of said liquid resin material at 20-C is no more than 15 cSt, preferably no more than 5 cSt.
14. A method of producing a laminate substantially as herein described with reference to the foregoing Example.
15. A laminate produced by the method ac
cording to any of the preceding claims.
16. A laminate comprising spaced apart first and second preformed sheets, at least one of which is metallic, bonded together by a resin material poured in liquid form between an assembly of said first and second preformed sheets and allowed to set.
GB08611333A 1985-05-09 1986-05-09 Production of a laminate Expired GB2174644B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB858511707A GB8511707D0 (en) 1985-05-09 1985-05-09 Laminate
EP86306959A EP0259528A3 (en) 1986-09-10 1986-09-10 Production of a laminate

Publications (3)

Publication Number Publication Date
GB8611333D0 GB8611333D0 (en) 1986-06-18
GB2174644A true GB2174644A (en) 1986-11-12
GB2174644B GB2174644B (en) 1989-02-01

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GB08611333A Expired GB2174644B (en) 1985-05-09 1986-05-09 Production of a laminate

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0259528A2 (en) * 1986-09-10 1988-03-16 James Arthur Albert Hickman Production of a laminate

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB979997A (en) * 1965-02-24 1965-01-06 Pittsburgh Plate Glass Co Polyurethane compositions producing process and laminated glass
GB1163002A (en) * 1966-05-06 1969-09-04 Kirk Optical Lens Co Inc Light transmitting element.
US3560285A (en) * 1967-02-06 1971-02-02 Kaiser Aluminium Chem Corp Processes for producing composite panels
GB1406235A (en) * 1971-08-19 1975-09-17 Bendix Home Systems Uk Ltd Panels
GB1454711A (en) * 1974-02-21 1976-11-03 Sod Detudes Des Tech Dindustri Process for producing constructional panels and to the panels obtained when carrying out the process
GB1512239A (en) * 1974-10-31 1978-05-24 Coldstream Prod Of Ca Ltd Method and apparatus for manufacturing sandwich panels
GB1537023A (en) * 1975-10-28 1978-12-29 British Steel Corp Panelled components suitable for use in buildings
GB2032844A (en) * 1978-10-31 1980-05-14 Langlands M Method of making frangible laminates
GB2155856A (en) * 1984-03-23 1985-10-02 Leith Glazing Company Limited Production of a laminate

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB979997A (en) * 1965-02-24 1965-01-06 Pittsburgh Plate Glass Co Polyurethane compositions producing process and laminated glass
GB1163002A (en) * 1966-05-06 1969-09-04 Kirk Optical Lens Co Inc Light transmitting element.
US3560285A (en) * 1967-02-06 1971-02-02 Kaiser Aluminium Chem Corp Processes for producing composite panels
GB1406235A (en) * 1971-08-19 1975-09-17 Bendix Home Systems Uk Ltd Panels
GB1454711A (en) * 1974-02-21 1976-11-03 Sod Detudes Des Tech Dindustri Process for producing constructional panels and to the panels obtained when carrying out the process
GB1512239A (en) * 1974-10-31 1978-05-24 Coldstream Prod Of Ca Ltd Method and apparatus for manufacturing sandwich panels
GB1537023A (en) * 1975-10-28 1978-12-29 British Steel Corp Panelled components suitable for use in buildings
GB2032844A (en) * 1978-10-31 1980-05-14 Langlands M Method of making frangible laminates
GB2155856A (en) * 1984-03-23 1985-10-02 Leith Glazing Company Limited Production of a laminate

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0259528A2 (en) * 1986-09-10 1988-03-16 James Arthur Albert Hickman Production of a laminate
EP0259528A3 (en) * 1986-09-10 1988-07-13 James Arthur Albert Hickman Production of a laminate

Also Published As

Publication number Publication date
GB2174644B (en) 1989-02-01
GB8611333D0 (en) 1986-06-18

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