[go: up one dir, main page]

WO1998035086A1 - Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites - Google Patents

Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites Download PDF

Info

Publication number
WO1998035086A1
WO1998035086A1 PCT/IB1997/000078 IB9700078W WO9835086A1 WO 1998035086 A1 WO1998035086 A1 WO 1998035086A1 IB 9700078 W IB9700078 W IB 9700078W WO 9835086 A1 WO9835086 A1 WO 9835086A1
Authority
WO
WIPO (PCT)
Prior art keywords
fibers
mat
fiber strands
composite body
mat according
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.)
Ceased
Application number
PCT/IB1997/000078
Other languages
German (de)
English (en)
Inventor
Bernd-Uwe Wulf
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.)
Mitsubishi Chemical Advanced Materials Composites AG
Original Assignee
Symalit AG
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
Application filed by Symalit AG filed Critical Symalit AG
Priority to EP97900719A priority Critical patent/EP0958420A1/fr
Priority to PCT/IB1997/000078 priority patent/WO1998035086A1/fr
Publication of WO1998035086A1 publication Critical patent/WO1998035086A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

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
    • 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
    • B32B5/02Layered 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
    • B32B5/08Layered 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 the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous 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
    • B29C70/086Fibrous 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 and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/12Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • 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
    • B32B5/02Layered 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
    • B32B5/022Non-woven fabric
    • 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
    • B32B5/02Layered 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
    • B32B5/06Layered 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 characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H1/00Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
    • D04H1/40Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
    • D04H1/42Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties characterised by the use of certain kinds of fibres insofar as this use has no preponderant influence on the consolidation of the fleece
    • D04H1/4209Inorganic fibres
    • D04H1/4218Glass fibres
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H1/00Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
    • D04H1/40Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
    • D04H1/54Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties by welding together the fibres, e.g. by partially melting or dissolving
    • D04H1/542Adhesive fibres
    • D04H1/544Olefin series
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H13/00Other non-woven fabrics
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/10Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H5/00Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
    • D04H5/12Glass fibres
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • 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
    • B32B2264/00Composition or properties of particles which form a particulate layer or are present as additives
    • B32B2264/02Synthetic macromolecular particles
    • B32B2264/0214Particles made of materials belonging to B32B27/00
    • B32B2264/0257Polyolefin particles, e.g. polyethylene or polypropylene homopolymers or ethylene-propylene copolymers
    • 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
    • B32B2305/10Fibres of continuous length
    • B32B2305/20Fibres of continuous length in the form of a non-woven mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/003Interior finishings

Definitions

  • the present invention relates to a mat which has fibers made of different materials and to a thermally deformable composite body produced from this mat. It further relates to a method for producing such a mat, a method for producing such a composite body and a method for producing a component from such a composite body.
  • Composite bodies in particular made of a fiber-reinforced plastic, are used for the longer to replace materials such as wood and metal.
  • Parts of road vehicles in which, for example, parts of the seats, dashboards, parts of the bumpers, etc. are made from fiber-reinforced thermoplastic materials can be mentioned as a non-exhaustive example. Specifically, for example, glass fiber reinforced polypropylene.
  • the glass fibers should be soaked with polypropylene, for example, so that every single fiber is completely covered by the thermoplastic material, so that the glass fibers are firmly embedded in the polypropylene and the polypropylene is distributed homogeneously in the respective component.
  • polypropylene for example, so that every single fiber is completely covered by the thermoplastic material, so that the glass fibers are firmly embedded in the polypropylene and the polypropylene is distributed homogeneously in the respective component.
  • the known composite bodies made of fiber-reinforced thermoplastic are successful and satisfactory, there is a desire for an even less impregnation of the glass fibers, an even better covering of the same by the polypropylene, for an even more homogeneous distribution of the plastic in the composite. body, and also after an even more rational manufacture of the composite body.
  • the aim of the invention is to show a mat made of fibers, which is composed of first fibers made of a first material and second fibers made of a second material, at least some of the fibers being in the form of fiber strands made of fibers made of the first material and made of Fibers made of the second material are present, and which, when processed into a composite body, enables an extremely complete impregnation of the fibers made of the first material with the second material, and allows the first fibers to be properly encased by the second material, which second material is completely homogeneous in the Composite body is distributed.
  • the mat according to the invention is characterized by the features of claim 1.
  • the thermally deformable composite body produced from at least one mat is characterized by the features of claim 14.
  • a method for manufacturing the mat is characterized by the features of claim 9 and a method for manufacturing the thermally deformable composite body by the features of claim 16.
  • a method for producing a component from the thermally deformable composite body is characterized by the features of claim 18.
  • FIG. 2 is a view of part of a mat formed from fiber strands
  • FIG. 3 shows a view of a composite body produced from the mat according to FIG. 2
  • FIG. 4 shows a mat formed from fiber strands and additional individual fibers
  • 5 shows a mat with a carrier layer formed from fibers
  • FIG. 6 shows a mat with a carrier layer formed from a film
  • FIG. 7 schematically shows a device for producing the composite body according to FIG. 3,
  • FIG. 8 shows a production variant
  • FIG. 9 schematically shows a molding tool for producing a component from a blank cut out of the composite body according to FIG. 4.
  • first fibers 1 shows a cross section through a fiber strand 3 which has a multiplicity of first fibers 1 made of a first material, for example glass, and a multiplicity of second fibers 2 made of a second material, for example polypropylene.
  • the first fibers 1 can alternatively consist of carbon, aramid, boron, steel, PEEK (polyether ether ketone), PAN (high-strength polyacrylonitrile), flax, hemp, salis, jute, ramie, coconut and kenaf, this list is not final.
  • the second fibers 2 can alternatively consist of thermoplastics, such as PP (polypropylene), PE (polyethylene), PA (polyamide), PET (polyethylene terephthalate) and / or mixtures of these thermoplastics. This list is also not exhaustive.
  • Fiber strands 3 which contain fibers 1 made of, for example, glass and fibers 2 made of, for example, polypropylene, are freely available on the market and therefore do not have to be described in detail.
  • a coherent mat is formed from a large number of the fiber strands 3 mentioned above.
  • the fiber strands are placed in an endless or cut form on a flat surface. The underlying surface is laid and connected and solidified with one another in such a way that a mat is created.
  • connection can be made by means of a needle known per se, with which a form-fitting connection of the individual fiber strands 3 is achieved to form a mat-shaped random fleece.
  • chemical or thermal bonding is also provided. Only the fibers of one material have to be connected. It is assumed that the material of the second individual fibers 2 is a thermoplastic, e.g. Is polypropylene.
  • the melting point of this second material is much lower than the melting point of the first material.
  • bonding in particular with thermal bonding, only the second material is heated and thus brought into a molten state, and thus the molten polypropylene fibers, for example, melt together at their contact points.
  • the glass fibers are not affected in any way. If an individual fiber strand is approximately rectilinear or only slightly curved, the individual glass fibers can be pulled out very easily, since they are arranged so as to be slidable relative to the polypropylene fibers in the fiber strand. In the finally formed mat, the glass fibers can still be pulled out individually, but this would be necessary due to this. the many strong curvatures of a greater application of force, so that the glass fibers practically do not shift during further processing to form the composite body, although there is no actual bond between the glass fibers.
  • the glass fibers are preferably connected to one another at their contact points, and the same conditions apply to the polypropylene fibers that were described above in connection with the thermal bonding for the glass fibers.
  • a section of the mat 4 (for example in the form of a random fleece) is shown schematically in FIG. 2. This mat 4 consists exclusively of fiber strands 3 held together. This mat 4 can now, for example when rolled up, be transported very easily and can be entered into corresponding devices in the form of webs in processing plants.
  • FIG. 7 schematically shows parts of a plant for producing a composite body from at least one mat 4 made of fiber strands 3.
  • the mat 4 is fed in a continuous processing process in the direction of arrow A to a first zone of the plant, which has, for example, a double belt press 5. Pressure and temperature are exerted on the mat 4 in this double belt press 5.
  • the thermoplastic material e.g. PP melted and penetrates the other fibers, e.g.
  • thermoplastic material is not from the outside, i.e. penetrate into the mat from the two main surfaces, but must be more or less evenly distributed within the mat, respectively. is arranged in the individual fiber strands of the mat, there is an excellent distribution of the thermoplastic material in the mat.
  • the mat is solidified under cooling and pressure to form a compact, here web-shaped composite body 7. This composite body 7 is shown schematically in FIG.
  • Fig. 3 shown. It has glass fibers 1 arranged in a tangled arrangement in a matrix 8 made of plastic are arranged so that there is now a thermally deformable composite body 7.
  • the thickness of this composite body 7 is smaller than the thickness of the original mat 4.
  • glass fibers are placed on a respective base and processed into a mat 4.
  • the processing can be done by means of needles or cohesive connection techniques.
  • Such a mat 4 which is needled as an example, is shown in FIG. 4. It therefore has fiber strands 3 made of glass and PP fibers and additionally fibers 10 made of glass, that is glass fibers.
  • the additional fibers 10 consist of PP.
  • the glass fibers are advantageously deposited in the form of known glass rovings and the PP fibers in the form of multifilaments.
  • additional polypropylene can be added to the mat 4 only immediately before it enters the double belt press.
  • This variant is drawn in FIG. 8.
  • additional polypropylene is fed in the form of one (or more) film web (s) 15, or also in the form of (at least) a melt film.
  • film web (s) 15 or also in the form of (at least) a melt film.
  • Needling should therefore be reduced to a minimum.
  • the mat that is ultimately to be processed into a composite body must still be able to be handled and be transportable.
  • the fiber strands 3 are placed on a tangled nonwoven 13 (also called nonwoven in technical terminology) made of PP (that is, not needled to one another) and only fixed on the tangled nonwoven 13 with the minimum number of needle sticks required for the subsequent handling, as drawn in FIG. 5.
  • a tangled nonwoven 13 also called nonwoven in technical terminology
  • PP that is, not needled to one another
  • a thin PP film web 14 a PP film
  • the connection between the fiber strands 3 and the film web 14 takes place by means of minimal needling.
  • the random fleece 13 can also consist of glass fibers, that is to say the first material.
  • the composite body 7 can now be made into final components, e.g. for road vehicles. Reference is made to FIG. 9.
  • Blanks 9 corresponding to the component to be manufactured are produced from the composite body 7. Depending on the subsequent processing, only a single blank 9 or multiple blanks are used together in the form of a blank structure.
  • the blank structure consisting of a blank 9 or more blanks corresponds in weight to the weight of the finished part of the component to be manufactured.
  • the blanks 9 are reheated in a known manner in a continuous manner in heaters, for example infrared ovens, so that the thermoplastic component of the blank structure from one or more blanks 9 again becomes flowable. Then a respective heated blank structure or blank 9 is inserted into a molding tool, which has, for example, a female mold 11 and a male mold 12, and the molding tool is closed, as indicated by the arrow B. The blank is pressed under pressure in the molding tool and then cooled, so that the component to be produced is finally shaped.
  • heaters for example infrared ovens

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Inorganic Chemistry (AREA)
  • Nonwoven Fabrics (AREA)
  • Laminated Bodies (AREA)

Abstract

On forme par aiguilletage ou par liage thermique une natte (4) constituée d'écheveaux de fibres (1) qui contiennent des fibres de verre (1) et des fibres (2) de matières thermoplastiques. On façonne avec cette natte sous l'effet de la pression et de la chaleur un corps composite (7) qui contient des fibres de verre (1) dans une matrice homogène (8) de matière thermoplastique. Ce corps composite peut à son tour être façonné pour former des éléments en matière plastique renforcée par des fibres de verre.
PCT/IB1997/000078 1997-02-05 1997-02-05 Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites Ceased WO1998035086A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP97900719A EP0958420A1 (fr) 1997-02-05 1997-02-05 Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites
PCT/IB1997/000078 WO1998035086A1 (fr) 1997-02-05 1997-02-05 Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB1997/000078 WO1998035086A1 (fr) 1997-02-05 1997-02-05 Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites

Publications (1)

Publication Number Publication Date
WO1998035086A1 true WO1998035086A1 (fr) 1998-08-13

Family

ID=11004524

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB1997/000078 Ceased WO1998035086A1 (fr) 1997-02-05 1997-02-05 Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites

Country Status (2)

Country Link
EP (1) EP0958420A1 (fr)
WO (1) WO1998035086A1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002062563A1 (fr) * 2001-02-08 2002-08-15 Quadrant Plastic Composites Ag Procede pour fabriquer un semi-produit thermoplastiquement malleable et renforce par des fibres
WO2002076711A1 (fr) * 2001-03-24 2002-10-03 Quadrant Plastic Composites Ag Procede de fabrication d'un demi-produit epais renforce par fibres a deformabilite thermoplastique
WO2003038175A1 (fr) * 2001-10-17 2003-05-08 Saertex Wagener Gmbh & Co. Kg Armature textile comportant au moins une couche de couverture et une couche de non-tisse volumineuse
WO2008139423A1 (fr) * 2007-05-15 2008-11-20 Gilbert Chomarat Armature textile de renforcement et son procede de realisation
WO2011021133A1 (fr) * 2009-08-21 2011-02-24 Gilbert Chomarat Armature textile a fils de verre continus
US8540830B2 (en) 2003-10-24 2013-09-24 Quadrant Plastic Composites, AG Method of producing a thermoplastically moldable fiber-reinforced semifinished product
EP3039060A4 (fr) * 2013-08-30 2017-04-26 Continental Structural Plastics, Inc. Surmoulage avec des fibres non-orientées
FR3155838A1 (fr) * 2023-11-24 2025-05-30 Chomarat Textiles Industries Etoffe textile non-tissee, adaptee pour former une couche de renfort mecanique dans un materiau composite

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3242033A (en) * 1962-02-21 1966-03-22 Fiber Glass Ind Inc Glass fiber mat
US3623935A (en) * 1965-12-28 1971-11-30 Celanese Corp Fluid-entangled nonwoven fabric
US3920879A (en) * 1971-11-01 1975-11-18 Allied Chem Glass fiber filled polyamide composites
EP0296970A1 (fr) * 1987-06-26 1988-12-28 Vetrotex Saint-Gobain Procédé et matériel d'aiguilletage de mat de verre et produit composite réalisé à partir dudit mat
EP0417827A1 (fr) * 1989-08-31 1991-03-20 Dsm N.V. Tissu de fibres thermoplastiques et fibre continue de renforcement
EP0465917A1 (fr) * 1990-07-02 1992-01-15 Ppg Industries, Inc. Procédé et appareil pour fabriquer d'une manière continue des mattes renforcées de faisceaux de fibres de verres
WO1995012701A1 (fr) * 1993-11-05 1995-05-11 Owens Corning Produit isolant en fibre de verre a deux composants

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3242033A (en) * 1962-02-21 1966-03-22 Fiber Glass Ind Inc Glass fiber mat
US3623935A (en) * 1965-12-28 1971-11-30 Celanese Corp Fluid-entangled nonwoven fabric
US3920879A (en) * 1971-11-01 1975-11-18 Allied Chem Glass fiber filled polyamide composites
EP0296970A1 (fr) * 1987-06-26 1988-12-28 Vetrotex Saint-Gobain Procédé et matériel d'aiguilletage de mat de verre et produit composite réalisé à partir dudit mat
EP0417827A1 (fr) * 1989-08-31 1991-03-20 Dsm N.V. Tissu de fibres thermoplastiques et fibre continue de renforcement
EP0465917A1 (fr) * 1990-07-02 1992-01-15 Ppg Industries, Inc. Procédé et appareil pour fabriquer d'une manière continue des mattes renforcées de faisceaux de fibres de verres
WO1995012701A1 (fr) * 1993-11-05 1995-05-11 Owens Corning Produit isolant en fibre de verre a deux composants

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002062563A1 (fr) * 2001-02-08 2002-08-15 Quadrant Plastic Composites Ag Procede pour fabriquer un semi-produit thermoplastiquement malleable et renforce par des fibres
WO2002076711A1 (fr) * 2001-03-24 2002-10-03 Quadrant Plastic Composites Ag Procede de fabrication d'un demi-produit epais renforce par fibres a deformabilite thermoplastique
US7132025B2 (en) 2001-03-24 2006-11-07 Quadrant Plastic Composites Ag Method of producing a thick, thermoformable, fiber-reinforced semi-finished product
WO2003038175A1 (fr) * 2001-10-17 2003-05-08 Saertex Wagener Gmbh & Co. Kg Armature textile comportant au moins une couche de couverture et une couche de non-tisse volumineuse
US8540830B2 (en) 2003-10-24 2013-09-24 Quadrant Plastic Composites, AG Method of producing a thermoplastically moldable fiber-reinforced semifinished product
WO2008139423A1 (fr) * 2007-05-15 2008-11-20 Gilbert Chomarat Armature textile de renforcement et son procede de realisation
FR2916208A1 (fr) * 2007-05-15 2008-11-21 Gilbert Chomarat Armature textile de renforcement et son procede de realisation.
US20110151231A1 (en) * 2007-05-15 2011-06-23 Gilbert Chomarat Reinforcement textile armature and method for making same
CN101680144B (zh) * 2007-05-15 2013-01-23 吉尔伯特·肖马拉 加强织物骨架及其制造方法
FR2916209A1 (fr) * 2007-05-15 2008-11-21 Gilbert Chomarat Armature textile de renforcement et son procede de realisation
WO2011021133A1 (fr) * 2009-08-21 2011-02-24 Gilbert Chomarat Armature textile a fils de verre continus
FR2949238A1 (fr) * 2009-08-21 2011-02-25 Gilbert Chomarat Armature textile a fils de verre continus
CN102482820A (zh) * 2009-08-21 2012-05-30 吉尔伯特·肖马拉 具有连续玻璃纤维的织物芯
CN102482820B (zh) * 2009-08-21 2015-09-02 吉尔伯特·肖马拉 具有连续玻璃纤维的织物芯
EP3039060A4 (fr) * 2013-08-30 2017-04-26 Continental Structural Plastics, Inc. Surmoulage avec des fibres non-orientées
US9718932B2 (en) 2013-08-30 2017-08-01 Continental Structural Plastics, Inc. Overmolding with non-oriented fibers
FR3155838A1 (fr) * 2023-11-24 2025-05-30 Chomarat Textiles Industries Etoffe textile non-tissee, adaptee pour former une couche de renfort mecanique dans un materiau composite

Also Published As

Publication number Publication date
EP0958420A1 (fr) 1999-11-24

Similar Documents

Publication Publication Date Title
EP1060069B1 (fr) Agencement de structure a fibres et procede pour la production d'une ebauche
DE69321549T2 (de) Verformbarer verbundvliesstoff und herstellverfahren hierfür
EP0657281B1 (fr) Elément de construction multicouche
EP0542186B1 (fr) Procédé pour la fabrication d'un matériau en couches par recyclage des déchets en plastique, et matériau en couches rigidifié contenant des déchets en plastique
EP2797729B1 (fr) Procédé ainsi que dispositif pour fabriquer un matériau composite fibreux sous la forme d'au moins une large bande de fibres imprégnée d'un polymère
EP2903794B1 (fr) Procédé de réalisation d'un semi-produit destiné à la fabrication d'une pièce composite
EP0597074A1 (fr) Structure plate contenant un materiau pelliculaire et son procede de fabrication.
EP2846986B1 (fr) Procédé de consolidation au moins par endroits d'une préforme servant à fabriquer une pièce façonnée dans un outil de façonnage
EP0956193B1 (fr) Corps composite thermoplastiquement deformable
WO1998035086A1 (fr) Natte en fibres de materiaux divers, corps composite forme de cette natte et procede de fabrication d'un element constitue de ces corps composites
EP3463825B1 (fr) Procédé pour la fabrication d'un élément en matériau composite à base de fibres
EP2737987B1 (fr) Procédé et dispositif de fabrication d'une pièce d'habillage intérieur
EP2447401B1 (fr) Produit semi-fini textile fixé partiellement
DE102015012537B3 (de) Verfahren zum Herstellen endlosfaserverstärkter Kunststoffe und eine entsprechende Vorrichtung
EP2794220A1 (fr) Procédé de production d'un matériau composite renforcé par des fibres, matériau composite renforcé par des fibres produit selon ce procédé et dispositif pour la mise en uvre de ce procédé
DE10258630A1 (de) Verfahren zu Herstellung langfaserverstärkter, thermoplastischer Bauteile
EP3877171B1 (fr) Procédé de fabrication d'un demi-produit plan renforcé par des fibres pouvant être déformé de manière thermoplastique
DE4412376C2 (de) Halbzeug
DE102013218143B4 (de) Verfahren zum Herstellen eines verstärkten Faserhalbzeugs und verstärktes Faserhalbzeug
EP2762295A1 (fr) Procédé et demi-produit pour la fabrication d'une pièce de formage composite en fibres et pièce de formage composite en fibres
EP0400766B1 (fr) Procédé pour fabriquer des nattes en fibres contenant un agent liant
DE102014119529A1 (de) Verfahren zur Herstellung von faserverstärkten Halbzeugen
DE102007028872A1 (de) Verfahren zur Herstellung eines flächigen Strukturverbundbauteils
DE9421206U1 (de) Mehrlagiges Bauelement
EP3680097A1 (fr) Procédé de fabrication d'un demi-produit plan renforcé par des fibres pouvant être déformé de manière thermoplastique

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): BR JP KR US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 1997900719

Country of ref document: EP

NENP Non-entry into the national phase

Ref country code: CA

WWP Wipo information: published in national office

Ref document number: 1997900719

Country of ref document: EP

NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 1998534025

Format of ref document f/p: F

WWR Wipo information: refused in national office

Ref document number: 1997900719

Country of ref document: EP

WWW Wipo information: withdrawn in national office

Ref document number: 1997900719

Country of ref document: EP