WO1992022424A1 - Composite material and use and method for the production thereof - Google Patents
Composite material and use and method for the production thereof Download PDFInfo
- Publication number
- WO1992022424A1 WO1992022424A1 PCT/SE1992/000401 SE9200401W WO9222424A1 WO 1992022424 A1 WO1992022424 A1 WO 1992022424A1 SE 9200401 W SE9200401 W SE 9200401W WO 9222424 A1 WO9222424 A1 WO 9222424A1
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- WO
- WIPO (PCT)
- Prior art keywords
- composite material
- thermoplastic particles
- curable resin
- pressing
- impregnated
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/02—Layered 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 structural features of a fibrous or filamentary layer
- B32B5/022—Non-woven fabric
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/36—Feeding the material to be shaped
- B29C44/38—Feeding the material to be shaped into a closed space, i.e. to make articles of definite length
- B29C44/44—Feeding the material to be shaped into a closed space, i.e. to make articles of definite length in solid form
- B29C44/445—Feeding the material to be shaped into a closed space, i.e. to make articles of definite length in solid form in the form of expandable granules, particles or beads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/56—After-treatment of articles, e.g. for altering the shape
- B29C44/5609—Purging of residual gas, e.g. noxious or explosive blowing agents
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/58—Moulds
- B29C44/588—Moulds with means for venting, e.g. releasing foaming gas
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
- B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
- B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/58—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres
- B29C70/66—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres the filler comprising hollow constituents, e.g. syntactic foam
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/02—Layered 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 structural features of a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/02—Layered 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 structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/18—Layered 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/22—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/245—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it being a foam layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/22—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/242—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using metal fibres
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/244—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using glass fibres
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J9/00—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
- C08J9/22—After-treatment of expandable particles; Forming foamed products
- C08J9/228—Forming foamed products
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/16—Fillers
- B29K2105/165—Hollow fillers, e.g. microballoons or expanded particles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/30—Fillers, e.g. particles, powders, beads, flakes, spheres, chips
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/72—Cured, e.g. vulcanised, cross-linked
Definitions
- This invention is related to a composite material comprising a web shaped material, which is impregnated with curable resin and which contains thermoplastic particles distributed in the web shaped material.
- the invention relates to use of such a composite material for producing laminates by warm pressing and also a method for producing the composite mate ⁇ rial.
- thermoplastic particles have been present in the semi-manufacture in expanded state, and the resin has been present in B-stage.
- a curable resin which is in A-stage, is meltable, cross-linked to a small degree and soluble in acetone and other solvents.
- a resin in C-stage is unmeltable, entirely cross-linked and insoluble.
- the B-stage is a stage between the A- and C-stages.
- the web shaped material On production of the semi-manufacture the web shaped material is impregnated with the impregnation solution containing the curable resin and the thermoplastic particles.
- the semi-manu ⁇ facture is thereafter obtained by heat processing so that the same obtains the character of a foam composite material.
- This semi-manufacture is then pressed into a laminate in a final pressing operation.
- the heat processing to obtain the foam composite material that means the semi- anufacture, substantially simultaneous expansion of the thermoplastic particles and drying occur, which means that considerable volumes of solvent are evaporated from the impregnated web shaped material. Simultaneously there is also a change of the curable resin from A-stage to B-stage.
- thermoplastic particles involve the disadvantage that it is very difficult to achieve a good uniformity of the foam com ⁇ posite material and, accordingly, also of the final laminate. This is due to the fact that the expansion of the thermoplastic particles causes a disturbance and an irregularity as far as the solvent emission and the curing of the curable resin are concerned. Furthermore, it has been found that this prior art involves a great sensitivity to area weight variations since such variations in turn give rise to variations in the degree of curing of the curable resin.
- the simultaneous expansion of the thermoplastic particles and the solvent emission may, furthermore, give rise to web break due to the fact that the bonding of fibres to each other in the web shaped material may be broken locally. Also in the absence of such breakages, irregularities concerning the internal fibre bonding may easily cause an uneven expansion of the thermoplastic particles and, accordingly, an uneven structure of the foam composite mate ⁇ rial.
- the object of the present invention is to reduce the disadvan ⁇ tages indicated hereinabove.
- the composite material As far as the composite material is concerned, this is obtained by the thermoplastic particles being of an expandable type but being present in the composite material in substantially unexpanded form, and by the curable resin being in A- or B-stage.
- this composite material which has the character of a semi-manufacture to be suitable for use, in a subsequent warm pressing operation, for producing laminates, either by means of a plurality of like layers of the composite material or in combination with further lamination layers.
- the composite material in its capacity as a semi-manufacture contains solvent, for instance water, to a proportion of 2-40, in particular 5-25, percent by weight. Said solvent proportion is, accordingly, that which is present when the semi-manufacture is intended to be subjected to the final warm pressing to a laminate.
- the composite material present as a semi-manufacture has, in accordance with the present invention, the thermoplastic particles unexpanded a lower freight volume is obtained, and furthermore the material may be handled in coil form or otherwise without being broken. According to the prior art discussed by way of introduction, the semi-manufacture occurs in the form of a foamed composite having a rigid structure.
- the curable resin should be, in the composite material according to the invention, in A-stage or possibly in a somewhat, but not completely, cured stage, that is at most in B-stage.
- the expansion or foaming of the thermoplastic particles and the final curing of the curable resin occur by warm pressing when the laminate aimed at is obtained. Due to the remaining solvent contents in the compo ⁇ site material according to the invention the expansion of the thermoplastic particles will proceed very homogeneously thanks to efficient heating in vapour environment.
- the problems discussed by way of introduction do not occur since the remaining solvent proportion is relatively restricted, that is suitably not higher than 25 percent by weight and preferably not higher than 15 percent by weight.
- thermoplastic particles Such a relatively small solvent proportion does not cause any unacceptable irregularity of the final product due to the simultaneously occurring expansion of the thermoplastic particles.
- a good workability of the composite material by means of the pressing tools is obtained in accordance with the invention since shaping occurs simultaneously with or prior to the expansion of the thermoplastic particles. In accordance with the prior art discussed, the expansion of the thermoplastic particles occurs initially and thereafter the final shaping in a subsequent pressing operation.
- the composite material may for instance be produced in the following manner: A pre-condensate of . a waterbased curable resin is produced in a conventional manner and the water contents is regulated so that a dry content of 30-75 percent by weight is obtained.
- the solution obtained in this way is provided with unexpanded thermoplastic particles, so called microspheres, in such an amount that the weight proportion microspheres: resin in the pressed composite material varies between 4:1 and 1:50. It is preferable to allow the micro- spheres to be included in such an amount that they in an expanded state form 50-95, preferably 75-95, percent by volume of the web shaped material and the resin mixture.
- the web shaped material is impregnated with the mixture of resin and microspheres in a conventional manner, e.g. by moving the web down into a bath of the mixture or by spraying the mixture on to the web.
- the degree of impregnation of the impregnated web may be regulated e.g. by pressing with rolls.
- the curable resins which preferably come in question, are formed by so called formaldehyde-based resins with carbamide, phenol, resorcinol or melamine.
- curable resins may also be used more generally, such as polycondensated resins, e.g. polyimide and polyadded resins, e.g. polyurethane.
- the web shaped material may be formed by a woven or non-woven, organic or inorganic material, amongst which glass fibre, mineral fibre, cellulose fibre and polyester fibre may be mentioned in particular. It is also important that the web shaped material has a sufficient porosity to be able to be impregnated with the mixture of resin and microspheres in a satisfactory manner.
- the web shaped material In order to obtain good conditions for drying and handling the web shaped material, considered as an individual layer, it has suitably a thickness varying between 0.1 and 5 mm.
- a plurality of such individual composite material layers may, however, be combined mutually and with possible further layers and more specifically so that the thickness of the resulting laminate may be 40 mm or more.
- microspheres used on production of the composite material according to the invention have shells which may be formed by copolymers of vinyl chloride and vinylidene chloride, copoly- mers of vinyl chloride and acrylonitrile, copolymers of vinyl ⁇ idene chloride and acrylonitrile, and copolymers of styrene and acrylonitrile.
- copolymers of methyl methacrylate should be mentioned, which contain up to about 20 percent by weight styrene, copolymers of methyl methacrylate and up to about 50 percent by weight of combined monomers of ethyl methacrylate, copolymers of methyl methacrylate and up to about 70 percent by weight of orto chlorostyrene.
- the particle size of the unex ⁇ panded spheres and, accordingly, of the expanded spheres may vary within wide limits and is chosen with guidance of the properties, which are desired of the final product. As an example on particle sizes for unexpanded spheres one may mention 1 ⁇ m to 1 mm, preferably 2 ⁇ m to 0.5 mm and in particular 5 ⁇ m to 50 ⁇ m.
- the diameter of the microspheres increases on expansion with a factor 2-5.
- the unexpanded spheres contain volatile liquid expanding agents, which are evaporated on the application of heat. These expanding agents may be formed by freons, hydrocarbons, such as n-pentane, i-pentane, neopentane, butane, i-butane and other expanding agents, which conventionally are used in microspheres of the nature here defined.
- the expanding agent may suitably form 5-30 percent by weight of the microsphere.
- the microspheres may be added to the resin solution as dried particles or in a suspen ⁇ sion, e.g. in water or an alcohol, such as methanol.
- the proportion resin to microspheres in the impregnation solution may, as has previously been pointed out, vary within wide limits and this proportion affects the properties of the final product. Conversely, one can, accordingly, choose a suitable proportion resins to microspheres in the mixture starting from a certain field of use and certain desired properties of the final product. This proportion may easily be determined by preparatory experiments in laboratory scale.
- the mixture of resins and microspheres may, if so desired or required, be provided with various additives, such as stabi ⁇ lisers, coupling agents, fillers, fire retarding additives and/or pigments.
- thermoplastic particles occur in the composite material, considered in its capacity as a semi-manufacture, in unexpanded form and the curable resin occurs in A- or possibly B-stage.
- the composite material After drying to a solvent proportion of preferably 5-25 percent by weight the composite material may be prepared for the warm pressing to follow as a later operation. In that connection the composite material may for instance be coiled to coils for transportation or storage.
- a porous material layer may, if desired be placed on one side or on both sides of the web shaped material impregnated with the resin mixture. This includes that said porous material layer could be located between two material webs impregnated with the resin mixture.
- the term "porous" in connection with the material layer means that the layer should present such openings or cavities that it on one hand allows partial penetration of the resin mixture into the material layer when the thermoplastic particles expand, and on the other hand allows solvent emission along and/or through the material layer.
- the material layer may be formed by some kind of fibrous layer or fibrous web, for instance a woven or non-woven, organic or inorganic fibre material.
- fibre splinter mats or splinter mats for instance of glass or mineral
- glass fibre, mineral fibre, cellulose fibre and polyester fibre may be mentioned as examples of fibre material.
- Particularly advantageous alternatives in this respect are to prepare the porous layer of glass wool or mineral wool.
- the porous material layer may alternatively also be constituted of so called expanded metal, namely a net like metal structure formed by one single coherent metal piece.
- expanded metal there are connecting bridges which are more or less inclined in relation to the general plane of the expanded metal layer.
- the expanded metal layer has through openings.
- the expanded metal layer allows solvent emission through the openings of the expanded metal layer and furthermore, the solvent may leave parallel to the expanded metal layer due to the openings and cavities present in connec ⁇ tion with the expanded metal layer.
- a further alternative as a material layer is a foam layer, for instance of melamine foam or polyester foam.
- a foam layer may, when the method is carried out, be placed on one side of the impregnated web shaped material on the warm pressing so as to provide the laminate aimed at.
- Such a foam layer could for the rest also be placed between layers formed by the impreg ⁇ nated web shaped material on the warm pressing.
- foamed plastic it is preferable to choose a foamed plastic having a relatively soft character.
- density of the foamed plastic it is preferable to choose a foamed plastic having a relatively soft character.
- foamed plastic may for instance be chosen to about 200 kg/ or less. However, the density of the foamed plastic should pre-
- the density is preferably chosen to be somewhere between 5 500 aanndd 330000 kg/m 3, between 100 and 200 kg/m3 being particularly preferred.
- the combination of the composite material consisting of the impregnated web shaped material and said porous material layer may be placed in a warm press or the like and is there subjected to heat so that the remaining solvent proportion is evaporated and the thermoplastic particles are expanded.
- the material layer and the impregnated web shaped material are prepared or chosen so that a partial penetration of the resin mixture into the material layer occurs when the thermoplastic particles expand. In this way an excellent mutual connection between the resin mixture, the web shaped material and the porous material layer is obtained.
- the material layer is preferably chosen to have such a porous character that the remaining solvent to a substantial degree may leave along and/or through the material layer. In a normal press structure, the solvent is emitted to a major part towards the sides through that part of the porous material layer which is not occupied by resin mixture penetrating into the material layer.
- the curing of the curable resin occurs in one and the same stage in the warm press as the evaporation of the remaining solvent and the expansion of the thermoplastic particles, the order in time preferably being such that the evaporation of the solvent and the expansion of the thermoplastic particles occur approximately simultaneously whereas the final curing of the curable resin occurs thereafter in connection with the tempera ⁇ ture increase which results when the main part of the volume of the solvent has been emitted.
- the composite material of the impregnated web shaped material and possible further material layers is preferably placed in the warm press, which is then closed to a certain given press slot width.
- the expansion of the thermoplastic particles following thereafter gives rise to such a volume increase that a pressing function is obtained between the press surfaces without having to move the press surfaces towards each other.
- the temperature in the heating device, warm press or the like during the processing of the composite material may vary between 100 and 200°C, preferably 120-160°C. Good results have been achieved in experiments at about 140°C.
- the porous material layer may act, when it occurs, so that the solvent may leave along and/or through the material layer.
- the porous material layer may also have other functions. More specifically, it may simply act as a spacer layer in various sandwich-like composite materials and this independently of whether layers obtained by the impregnated web shaped material are present on both sides or only on one side of the material layer.
- the porous material layer may also have the character of a non-expensive filler material.
- the porous material layer, the impregnated web shaped material and the heat and press condi ⁇ tions are chosen so that the curable resin and/or the thermo- plast form connecting bridges through the porous material layer.
- the connecting bridges may, in such an embodi ⁇ ment, not become so extensive that they prevent solvent emis ⁇ sion along and/or through the material layer.
- Such connecting bridges between the layers obtained by the impregnated web shaped material and located on either sides of the porous material layer involve a more stable mutual connection of the layers obtained by means of the impregnated, web shaped mate ⁇ rial than the connection which could be provided by the porous material layer alone. In this way improved strength properties, for instance regarding rigidity of the composite material obtained but primarily in respect of the resistance to sputte ⁇ ring of the composite along the porous material layer, are achieved.
- the connecting bridges involve, furthermore, a higher degree of resistance to compression of the porous material layer in particular when easily compressible, porous material layers are involved.
- the connecting bridges are particularly preferable in such cases where the porous material layer is formed by foamed plastic or otherwise a material which is relatively soft or has a low density but where good strength properties are desirable despite such softness or low density.
- foamed plastic or otherwise a material which is relatively soft or has a low density but where good strength properties are desirable despite such softness or low density.
- Unexpanded thermoplastic particles are added to a formaldehyde based resin (for instance melamine, phenol) in an aqueous solution with a dry contents of 50% so as to obtain a dry contents proportion of 15%.
- a web shaped material in the form of a fibre web is impregnated with the mixture and dried to a residual moisture contents of 15 percent by weight.
- a glass fibre mat or an expanded metal layer is placed on one side or both sides of the impregnated fibre web.
- the combination is placed in a warm press having for instance a temperature of 140 ⁇ C with a given slot.
- a warm press having for instance a temperature of 140 ⁇ C with a given slot.
- the thermoplastic particles expand, a partial penetration of the resin mixture into the glass fibre mat or expanded metal layer is obtained.
- the residual moisture is expelled for the largest part towards the sides through that part of the glass fibre mat or expanded metal layer which is not filled by the resin mixture.
- approximately simultaneous drying and expansion occur with direct following successive curing of the curable resin.
- the expression "given slot” indicates that the slot of the press is not changed during the actual pressing operation. Instead, the pressing operation is obtained due to the expansion of the thermoplastic particles.
- the material between the press surfaces will expand to such a degree that a pressing operation will be obtained between the press surfaces. It follows from this that the starting slot width should be adapted to the expansion of the thermoplastic particles.
- Mats the dry weight of which were 350 g/m 2, and which had been impregnated with a mixture of a curable resin in a solvent and unexpanded thermoplastic particles were placed in a warm press on both sides of a porous material layer consisting of polyether foam having a thickness of 5 mm and a density of 30 kg/m 3.
- a porous material layer consisting of polyether foam having a thickness of 5 mm and a density of 30 kg/m 3.
- These i.mpregnated mats compri.sed on thei.r si.des faci.ng towards the foamed plastic layer, glass fibre splinters to an amount of 100 g/m 2.
- the mats were dried to a moisture contents of 20 percent by weight.
- the surface weight was 850 g/m .
- a glass fibre mat which was impregnated with a mixture of a curable resin in a solvent and unexpanded thermoplastic par-
- a glass fibre mat which had a surface weight of 350 g/m 2 and impregnated with a mixture of a curable resin in a solvent and unexpanded thermoplastic particles, and a mineral wool layer with a thickness of 15 mm and a density of 150 kg/m 3 were placed in a warm press.
- the resin mixture penetrates, on pressing, 1-2 mm into the mineral wool so that an intimate adhesion is obtained.
- a glass fibre mat having an area weight of 55 g per m 2 is impregnated with an impregnation solution containing a curable melamine resin and unexpanded thermoplastic particles.
- the impregnated mat (the composite material) is dried carefully to a residual moisture content of 15 percent by weight and an area weight of 200 g per m 2.
- Laminate pressing in a warm press of an arbitrary number of these impregnated glass fibre mats gave rise to high quality laminates.
- the method according to the invention is of course not only restricted to the examples cited here.
- the method by suitable selection of materials in the porous material layer and the impregnated web shaped material and suitable selection of heat processing or warm pressing conditions could cause solvent emission to occur during a considerable part of the process along and/or through the porous material layer but in the final stage of the manu ⁇ facturing process, the resin mixture could penetrate so almost entirely into the porous material layer that the latter would no longer give any porous impression but instead be substantially filled by the resin mixture, which would also be present on the surface of the material layer which was originally porous, independently of whether this surface was placed outermost towards the surroundings or formed an interface to a further layer comprised in the laminate. Also further modifications are possible within the scope of the invention.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Health & Medical Sciences (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Inorganic Chemistry (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Textile Engineering (AREA)
- Toxicology (AREA)
- Laminated Bodies (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK92913255T DK0647182T3 (en) | 1991-06-12 | 1992-06-12 | Composite material as well as its use and method of manufacture |
JP05500821A JP3091224B2 (en) | 1991-06-12 | 1992-06-12 | Method for producing composite materials and laminates |
DE69227847T DE69227847T2 (en) | 1991-06-12 | 1992-06-12 | COMPOSITE, ITS USE AND METHOD FOR THE PRODUCTION THEREOF |
EP92913255A EP0647182B1 (en) | 1991-06-12 | 1992-06-12 | Composite material and use and method for the production thereof |
AU20223/92A AU668867B2 (en) | 1991-06-12 | 1992-06-12 | Composite material and use and method for the production thereof |
Applications Claiming Priority (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9101791-3 | 1991-06-12 | ||
SE9101791A SE468546B (en) | 1991-06-12 | 1991-06-12 | Process for manufacturing a composite material |
SE9103460-3 | 1991-11-21 | ||
SE9103460A SE505843C2 (en) | 1991-02-05 | 1991-11-21 | Composite material prodn. |
SE9200674-1 | 1992-03-05 | ||
SE9200674A SE508051C2 (en) | 1991-06-12 | 1992-03-05 | Composite materials and their use and process for their preparation |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1992022424A1 true WO1992022424A1 (en) | 1992-12-23 |
Family
ID=27355628
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1992/000401 WO1992022424A1 (en) | 1991-06-12 | 1992-06-12 | Composite material and use and method for the production thereof |
PCT/SE1992/000402 WO1992022420A1 (en) | 1991-06-12 | 1992-06-12 | Method for the production of a composite material |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1992/000402 WO1992022420A1 (en) | 1991-06-12 | 1992-06-12 | Method for the production of a composite material |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP0647182B1 (en) |
JP (1) | JP3091224B2 (en) |
AT (1) | ATE174262T1 (en) |
AU (2) | AU2022492A (en) |
DE (1) | DE69227847T2 (en) |
DK (1) | DK0647182T3 (en) |
SE (1) | SE508051C2 (en) |
WO (2) | WO1992022424A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201700024675A1 (en) * | 2017-03-06 | 2018-09-06 | Tryonic Ltd | "Hot stamping method" |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4406039C1 (en) * | 1994-02-24 | 1995-03-30 | Erlenbach Gmbh & Co Kg | Moulding of composite material and process for producing such a composite material |
US5665295A (en) * | 1994-08-04 | 1997-09-09 | Teijin Limited | Process for the production of composite molded article |
TW354280B (en) * | 1994-08-04 | 1999-03-11 | Teijin Ltd | Material of a composite molded article of a fiber-reinforced resin of foamed core sandwichded layer and preparation thereof |
DE69839091T2 (en) | 1998-12-16 | 2009-01-29 | Lantor B.V. | Core material for closed molding systems |
DE10329727A1 (en) * | 2003-07-01 | 2005-02-03 | Evi Gmbh | Composite panel and method of making a composite panel |
WO2006080833A1 (en) * | 2005-01-31 | 2006-08-03 | Fits Holding Bv | Method of manufacturing a sandwich panel and a sandwich panel as such |
CN101374644B (en) * | 2006-01-30 | 2012-11-07 | 金斯潘控股有限公司 | A phenolic foam board |
SE529803C2 (en) | 2006-04-04 | 2007-11-27 | Andersson Composite Technologi | Semi-finished web or sheet-shaped, polymeric foam composite material and sheet and processes for making them |
US7981173B2 (en) * | 2008-04-28 | 2011-07-19 | Ali Industries, Inc. | Process of making a laminate and laminate formed thereby |
EP2233280A1 (en) * | 2009-03-23 | 2010-09-29 | Lantor B.V. | Conductive core material |
NL2005945C2 (en) | 2010-12-31 | 2012-07-03 | Holland Composites Innovations B V | Composite materials and shaped articles. |
DE102012105425B4 (en) * | 2012-06-22 | 2017-05-04 | Carcoustics Techconsult Gmbh | Semi-finished product and molded part of sheet-like fiber structures and binders and process for their preparation |
ITUA20161692A1 (en) * | 2016-03-15 | 2017-09-15 | Tryonic Ltd | "Method to stabilize the size of a printed object" |
KR102277768B1 (en) * | 2019-06-17 | 2021-07-15 | 주식회사 엘지화학 | Manufacturing method for composite material and the composite material |
Citations (2)
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---|---|---|---|---|
GB1427647A (en) * | 1973-07-20 | 1976-03-10 | Firet Bv | Process for producing fibrous fabrics for use in fibre-reinforced plastics |
EP0041054A2 (en) * | 1980-05-21 | 1981-12-02 | KemaNord AB | A foam composite material impregnated with resin |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US3676288A (en) * | 1970-05-04 | 1972-07-11 | Kendall & Co | Low-density bonded nonwoven fabrics and process therefor |
CH521849A (en) * | 1971-03-19 | 1972-04-30 | Alusuisse | Composite panel |
SE389696B (en) * | 1973-10-26 | 1976-11-15 | Kema Nord Ab | PROCEDURE FOR PAPER PAPER CONTAINING PLASTIC PARTICLES |
US4102721A (en) * | 1976-10-13 | 1978-07-25 | Minnesota Mining And Manufacturing Company | Barrier tape construction |
US4836871A (en) * | 1986-12-02 | 1989-06-06 | Mitsubishi Yuka Badische Co., Ltd. | Manufacturing method for an expanded laminated sheet |
-
1992
- 1992-03-05 SE SE9200674A patent/SE508051C2/en not_active IP Right Cessation
- 1992-06-12 WO PCT/SE1992/000401 patent/WO1992022424A1/en active IP Right Grant
- 1992-06-12 JP JP05500821A patent/JP3091224B2/en not_active Expired - Fee Related
- 1992-06-12 WO PCT/SE1992/000402 patent/WO1992022420A1/en active Application Filing
- 1992-06-12 AT AT92913255T patent/ATE174262T1/en not_active IP Right Cessation
- 1992-06-12 AU AU20224/92A patent/AU2022492A/en not_active Abandoned
- 1992-06-12 DE DE69227847T patent/DE69227847T2/en not_active Expired - Fee Related
- 1992-06-12 DK DK92913255T patent/DK0647182T3/en active
- 1992-06-12 EP EP92913255A patent/EP0647182B1/en not_active Expired - Lifetime
- 1992-06-12 AU AU20223/92A patent/AU668867B2/en not_active Ceased
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1427647A (en) * | 1973-07-20 | 1976-03-10 | Firet Bv | Process for producing fibrous fabrics for use in fibre-reinforced plastics |
EP0041054A2 (en) * | 1980-05-21 | 1981-12-02 | KemaNord AB | A foam composite material impregnated with resin |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201700024675A1 (en) * | 2017-03-06 | 2018-09-06 | Tryonic Ltd | "Hot stamping method" |
EP3372366A1 (en) * | 2017-03-06 | 2018-09-12 | Tryonic Ltd | Hot-molding method |
Also Published As
Publication number | Publication date |
---|---|
EP0647182A1 (en) | 1995-04-12 |
AU668867B2 (en) | 1996-05-23 |
ATE174262T1 (en) | 1998-12-15 |
JP3091224B2 (en) | 2000-09-25 |
SE9200674L (en) | 1992-12-13 |
DE69227847T2 (en) | 1999-08-05 |
WO1992022420A1 (en) | 1992-12-23 |
EP0647182B1 (en) | 1998-12-09 |
DE69227847D1 (en) | 1999-01-21 |
AU2022392A (en) | 1993-01-12 |
AU2022492A (en) | 1993-01-12 |
DK0647182T3 (en) | 1999-08-16 |
JPH06508310A (en) | 1994-09-22 |
SE9200674D0 (en) | 1992-03-05 |
SE508051C2 (en) | 1998-08-17 |
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