US20030148096A1 - Composite material - Google Patents

Composite material Download PDF

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Publication number
US20030148096A1
US20030148096A1 US10/220,193 US22019302A US2003148096A1 US 20030148096 A1 US20030148096 A1 US 20030148096A1 US 22019302 A US22019302 A US 22019302A US 2003148096 A1 US2003148096 A1 US 2003148096A1
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United States
Prior art keywords
composite material
endless filaments
recited
nonwoven fabric
bonded
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
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US10/220,193
Inventor
Robert Groten
Matthias Schuster
Georges Riboulet
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Carl Freudenberg KG
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Individual
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Assigned to CARL FREUDENBERG KG reassignment CARL FREUDENBERG KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GROTEN, ROBERT, RIBOULET, GEORGES, SCHUSTER, MATTHIAS
Publication of US20030148096A1 publication Critical patent/US20030148096A1/en
Abandoned 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
    • 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
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • 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
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/14Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
    • B29C45/14778Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles the article consisting of a material with particular properties, e.g. porous, brittle
    • B29C45/14786Fibrous material or fibre containing material, e.g. fibre mats or fibre reinforced 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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/02Layered products comprising a layer of synthetic resin in the form of fibres or filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/34Layered products comprising a layer of synthetic resin comprising polyamides
    • 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
    • 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0809Fabrics
    • B29K2105/0818Fleece
    • 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0854Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns in the form of a non-woven mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3005Body finishings
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2904Staple length fiber

Definitions

  • the invention relates to a composite material, made from a microfilament nonwoven fabric having masses per unit area of 50 to 200 g/m 2 , which is bonded with a thermoplastic synthetic material directly, using an injection-molding process.
  • Paneling parts for automobile interiors are known from the document EP 0 968 806, whereby a microfiber nonwoven fabric is placed into a mold and bonded to a thermoplastic synthetic material by an injection-molding process.
  • Such injection-molding or “direct injection molding” (DIM) processes permit efficient production of paneling parts in the automobile interior sector.
  • the microfiber nonwoven fabric is preferably made from polyester fibers that function as a binding layer for a decorative layer that is applied subsequently.
  • the paneling parts used in the interior of the automobile are supposed to demonstrate attractive optical and sensory properties of the decor.
  • the parts are supposed to be capable of recycling, to possess a very high level of resistance to color fading, especially under the effects of black-panel temperatures, a low tendency to become dirty, a high level of friction wear resistance, moisture resistance, fire resistance, cleanability, a low tendency or no tendency to emit gases, and low costs.
  • efficient, cost-effective production methods for the production of the paneling parts are aimed at.
  • the invention has set itself the task of indicating a composite material, as well as a method for its production, that take into account the stated requirements.
  • the task is accomplished by a composite material that is made from a microfilament nonwoven fabric having a mass per unit area of 50 to 200 g/m 2 , the nonwoven fabric being made from melt-spun, drawn multi-component endless filaments having a titer of 1.5 to 5 dtex and directly laid up to form a fibrous web, and the multi-component endless filaments, optionally after prebonding, being split up to at least 80% to form micro-endless filaments having a titer of 0.1-1.2 dtex, and bonded, and then bonded to a thermoplastic synthetic material using an injection-molding process.
  • the composite material demonstrates a high level of specific fiber surface at a comparatively low mass per unit area, as well as high opacity.
  • the fineness of the filaments permits good printability and embossability, and thereby decorative structuring of the nonwoven fabric used for the production of the composite material according to the invention.
  • the thermoplastic synthetic material does not impregnate the nonwoven fabric.
  • the composite material is one in which the nonwoven fabric is made from melt-spun, aerodynamically stretched multi-component endless filaments having a titer of 1.5 to 3 dtex and directly laid up to form a fibrous web, and the multi-component endless filaments are split up to at least 80% to form micro-endless filaments having a titer of 0.1 to 0.3 dtex, and bonded.
  • the composite material demonstrates an isotropic filament distribution in the web, making further processing relatively independent of the machine running direction and thereby very advantageous for material utilization.
  • the composite material is one in which the multi-component endless filament is a bicomponent endless filament made from two incompatible polymers, particularly a polyester and a polyamide.
  • a bicomponent endless filament demonstrates good splittability into micro-endless filaments and results in an advantageous ratio of strength to mass per unit area.
  • the composite material according to the invention is very easy to clean and wipe down, because of the polymers used and their filament structure, and demonstrates a high level of wear resistance, i.e. it is easy to take care of.
  • the composite material is one in which the multi-component endless filaments have a cross-section having an orange-like multi-segment structure, also called a “pie” structure, the segments alternately containing one of the two incompatible polymers in each case.
  • a “side-by-side” (s/s) segment arrangement of the incompatible polymers in the multi-component endless filaments is also possible, which arrangement is preferably used for the production of crimped filaments.
  • Such segment arrangements of the incompatible polymers in the multi-component endless filament have proven to be very easy to split.
  • the nonwoven fabric used for the production of the composite material according to the invention possesses a good deep drawing capacity, or deformability, which is expressed in the average strength values at a high expansion capacity and comparatively low modulus values.
  • the composite material is furthermore one in which at least one of the incompatible polymers forming the multi-component endless filament contains an additive, such as color pigments, permanently acting anti-statics, flame retarding agents and/or additives that influence the hydrophobic properties, in amounts up to 10 percent by weight.
  • an additive such as color pigments, permanently acting anti-statics, flame retarding agents and/or additives that influence the hydrophobic properties, in amounts up to 10 percent by weight.
  • Static charges can be reduced or prevented with the additives, and the lightfastness of the surfaces visible in the automobile interior on exposure to a high black-panel temperature can be improved.
  • values for lightfastness under black-panel temperatures of ⁇ 6 have been achieved, determined according to DIN EN 20105-A02.
  • the method according to the invention for the production of a composite material, is made up of the steps that multi-component endless filaments are spun from the melt, stretched, and directly laid up to form a web, that prebonding takes place, and that the nonwoven fabric is bonded using high-pressure fluid jets, and, at the same time, split into micro-endless filaments having a titer of 0.1 to 1.2 dtex, and bonded to a thermoplastic synthetic material by an injection-molding process.
  • the composite material obtained in this way can be produced in very short cycle times. The cycle times can be reduced from approximately 50 to 2 to 5 seconds, as compared with known composite components.
  • the method for the production of the composite material is carried out in such a manner that the multi-component endless filaments are bonded and split in that the nonwoven fabric, which has been prebonded if necessary, is impacted at least once on each side with high-pressure water jets, and placed into an injection-molding mold after a drying process, and backed with a thermoplastic synthetic material by injection-molding.
  • the composite material demonstrates a good surface and a degree of splitting of the multi-component endless filaments >80%.
  • the nonwoven fabric used in the composite material according to the invention is subjected to spot calandering in order to increase its friction wear resistance.
  • the split and bonded nonwoven fabric is passed through heated rollers, at least one of which has elevations that result in melt-bonding of the filaments to one another at certain points.
  • the nonwoven fabric used for producing the composite material according to the invention is suited for the production of door, pillar, and/or trunk linings, rear window shelves, car roof linings, dashboards, as well as wheel house liners.
  • a filament sheet having a mass per unit area of 134 g/m 2 is produced from a side-by-side (s/s) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.3 dtex and a weight ratio of PES/PA6.6 of 60/40, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides.
  • the bicomponent endless filaments have a titer of 1.0 dtex and a thickness of 0.51 mm after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time. Values of 372 N in the machine running direction and 331 N in the crosswise direction were determined for the tear strength.
  • a filament sheet having a mass per unit area of 137 g/m 2 is produced from a side-by-side (s/s) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 1.8 dtex and a weight ratio of PES/PA6.6 of 50/50, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides.
  • the bicomponent endless filaments have a titer of 1.0 dtex and a thickness of 0.52 mm after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time. Values of 457 N in the machine running direction and 373 N in the crosswise direction were determined for the tear strength.
  • a filament sheet having a mass per unit area of 105 g/m 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.4 dtex and a weight ratio of PES/PA6.6 of 55/45, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides.
  • the bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.48 mm after a final smoothing process. Values of 302 N in the machine running direction and 303 N in the crosswise direction were determined for the tear strength.
  • a filament sheet having a mass per unit area of 244 g/m 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.1 dtex and a weight ratio of PES/PA6.6 of 70/30, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides.
  • the bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.90 mm after a final smoothing process. Values of 763 N in the machine running direction and 739 N in the crosswise direction were determined for the tear strength.
  • a filament sheet having a mass per unit area of 131 g/m 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.0 dtex and a weight ratio of PES/PA6.6 of 70/30, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides.
  • the bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.53 mm after a final smoothing process. Values of 309 N in the machine running direction and 284 N in the crosswise direction were determined for the tear strength.

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

Abstract

The invention relates to a composite material, made from a microfilament nonwoven fabric having a mass per unit area of 40 to 200 g/m2, in which a nonwoven fabric, which is made from melt-spun, drawn, multi-component endless filaments having a titer of 1.5 to 5 dtex and directly laid up to form a fibrous web, and in which the multi-component endless filaments, optionally after prebonding, are split at least to 80% to form micro-endless filaments having a titer of 0.1 to 1.2 dtex and bonded, is bonded to a thermoplastic synthetic material using an injection-molding process.

Description

  • The invention relates to a composite material, made from a microfilament nonwoven fabric having masses per unit area of 50 to 200 g/m[0001] 2, which is bonded with a thermoplastic synthetic material directly, using an injection-molding process.
  • Paneling parts for automobile interiors are known from the document EP 0 968 806, whereby a microfiber nonwoven fabric is placed into a mold and bonded to a thermoplastic synthetic material by an injection-molding process. Such injection-molding or “direct injection molding” (DIM) processes permit efficient production of paneling parts in the automobile interior sector. The microfiber nonwoven fabric is preferably made from polyester fibers that function as a binding layer for a decorative layer that is applied subsequently. [0002]
  • In the course of ever greater requirements in the automobile industry, new demands are being made on the suppliers. For example, the paneling parts used in the interior of the automobile are supposed to demonstrate attractive optical and sensory properties of the decor. The parts are supposed to be capable of recycling, to possess a very high level of resistance to color fading, especially under the effects of black-panel temperatures, a low tendency to become dirty, a high level of friction wear resistance, moisture resistance, fire resistance, cleanability, a low tendency or no tendency to emit gases, and low costs. Furthermore, efficient, cost-effective production methods for the production of the paneling parts are aimed at. [0003]
  • The invention has set itself the task of indicating a composite material, as well as a method for its production, that take into account the stated requirements. [0004]
  • According to the present invention, the task is accomplished by a composite material that is made from a microfilament nonwoven fabric having a mass per unit area of 50 to 200 g/m[0005] 2, the nonwoven fabric being made from melt-spun, drawn multi-component endless filaments having a titer of 1.5 to 5 dtex and directly laid up to form a fibrous web, and the multi-component endless filaments, optionally after prebonding, being split up to at least 80% to form micro-endless filaments having a titer of 0.1-1.2 dtex, and bonded, and then bonded to a thermoplastic synthetic material using an injection-molding process. The composite material demonstrates a high level of specific fiber surface at a comparatively low mass per unit area, as well as high opacity. The fineness of the filaments permits good printability and embossability, and thereby decorative structuring of the nonwoven fabric used for the production of the composite material according to the invention. In this connection, the thermoplastic synthetic material does not impregnate the nonwoven fabric.
  • Preferably, the composite material is one in which the nonwoven fabric is made from melt-spun, aerodynamically stretched multi-component endless filaments having a titer of 1.5 to 3 dtex and directly laid up to form a fibrous web, and the multi-component endless filaments are split up to at least 80% to form micro-endless filaments having a titer of 0.1 to 0.3 dtex, and bonded. The composite material demonstrates an isotropic filament distribution in the web, making further processing relatively independent of the machine running direction and thereby very advantageous for material utilization. [0006]
  • Preferably, the composite material is one in which the multi-component endless filament is a bicomponent endless filament made from two incompatible polymers, particularly a polyester and a polyamide. Such a bicomponent endless filament demonstrates good splittability into micro-endless filaments and results in an advantageous ratio of strength to mass per unit area. At the same time, the composite material according to the invention is very easy to clean and wipe down, because of the polymers used and their filament structure, and demonstrates a high level of wear resistance, i.e. it is easy to take care of. [0007]
  • Preferably, the composite material is one in which the multi-component endless filaments have a cross-section having an orange-like multi-segment structure, also called a “pie” structure, the segments alternately containing one of the two incompatible polymers in each case. In addition to this orange-like multi-segment structure of the multi-component endless filaments, a “side-by-side” (s/s) segment arrangement of the incompatible polymers in the multi-component endless filaments is also possible, which arrangement is preferably used for the production of crimped filaments. Such segment arrangements of the incompatible polymers in the multi-component endless filament have proven to be very easy to split. The nonwoven fabric used for the production of the composite material according to the invention possesses a good deep drawing capacity, or deformability, which is expressed in the average strength values at a high expansion capacity and comparatively low modulus values. [0008]
  • Preferably, the composite material is furthermore one in which at least one of the incompatible polymers forming the multi-component endless filament contains an additive, such as color pigments, permanently acting anti-statics, flame retarding agents and/or additives that influence the hydrophobic properties, in amounts up to 10 percent by weight. Static charges can be reduced or prevented with the additives, and the lightfastness of the surfaces visible in the automobile interior on exposure to a high black-panel temperature can be improved. Using overdyed products, values for lightfastness under black-panel temperatures of ≧6 have been achieved, determined according to DIN EN 20105-A02. [0009]
  • The method according to the invention, for the production of a composite material, is made up of the steps that multi-component endless filaments are spun from the melt, stretched, and directly laid up to form a web, that prebonding takes place, and that the nonwoven fabric is bonded using high-pressure fluid jets, and, at the same time, split into micro-endless filaments having a titer of 0.1 to 1.2 dtex, and bonded to a thermoplastic synthetic material by an injection-molding process. The composite material obtained in this way can be produced in very short cycle times. The cycle times can be reduced from approximately 50 to 2 to 5 seconds, as compared with known composite components. [0010]
  • It is advantageous that the method for the production of the composite material is carried out in such a manner that the multi-component endless filaments are bonded and split in that the nonwoven fabric, which has been prebonded if necessary, is impacted at least once on each side with high-pressure water jets, and placed into an injection-molding mold after a drying process, and backed with a thermoplastic synthetic material by injection-molding. As a result, the composite material demonstrates a good surface and a degree of splitting of the multi-component endless filaments >80%. [0011]
  • Advantageously, the nonwoven fabric used in the composite material according to the invention is subjected to spot calandering in order to increase its friction wear resistance. For this purpose, the split and bonded nonwoven fabric is passed through heated rollers, at least one of which has elevations that result in melt-bonding of the filaments to one another at certain points. [0012]
  • Because of its properties, such as good printability, a high level of friction wear resistance, as well as its good lightfastness under black-panel temperatures, and its haptic properties, the nonwoven fabric used for producing the composite material according to the invention is suited for the production of door, pillar, and/or trunk linings, rear window shelves, car roof linings, dashboards, as well as wheel house liners.[0013]
  • EXAMPLE 1
  • A filament sheet having a mass per unit area of 134 g/m[0014] 2 is produced from a side-by-side (s/s) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.3 dtex and a weight ratio of PES/PA6.6 of 60/40, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides. The bicomponent endless filaments have a titer of 1.0 dtex and a thickness of 0.51 mm after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time. Values of 372 N in the machine running direction and 331 N in the crosswise direction were determined for the tear strength.
  • EXAMPLE 2
  • A filament sheet having a mass per unit area of 137 g/m[0015] 2 is produced from a side-by-side (s/s) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 1.8 dtex and a weight ratio of PES/PA6.6 of 50/50, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides. The bicomponent endless filaments have a titer of 1.0 dtex and a thickness of 0.52 mm after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time. Values of 457 N in the machine running direction and 373 N in the crosswise direction were determined for the tear strength.
  • EXAMPLE 3
  • A filament sheet having a mass per unit area of 105 g/m[0016] 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.4 dtex and a weight ratio of PES/PA6.6 of 55/45, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides. The bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.48 mm after a final smoothing process. Values of 302 N in the machine running direction and 303 N in the crosswise direction were determined for the tear strength.
  • EXAMPLE 4
  • A filament sheet having a mass per unit area of 244 g/m[0017] 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.1 dtex and a weight ratio of PES/PA6.6 of 70/30, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides. The bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.90 mm after a final smoothing process. Values of 763 N in the machine running direction and 739 N in the crosswise direction were determined for the tear strength.
  • EXAMPLE 5
  • A filament sheet having a mass per unit area of 131 g/m[0018] 2 is produced from a 16 segment (pie) polyester-polyamide 6.6 (PES-PA6.6) bicomponent endless filament having a titer of 2.0 dtex and a weight ratio of PES/PA6.6 of 70/30, and is subjected to water-jet needlepunching at pressures up to 230 bar, on both sides. The bicomponent endless filaments have a titer of 0.1 dtex after the water-jet needlepunching process, which results in splitting of the starting filaments at the same time, and a thickness of 0.53 mm after a final smoothing process. Values of 309 N in the machine running direction and 284 N in the crosswise direction were determined for the tear strength.

Claims (10)

What is claimed is:
1. A composite material made from a microfilament nonwoven fabric having masses per unit area of 50 to 200 g/m2, the nonwoven fabric being made from melt-spun, drawn, multi-component endless filaments having a titer of 1.5 to 5 dtex and directly laid up to form a fibrous web, and in which the multi-component endless filaments, optionally after prebonding, are split at least to 80% to form micro-endless filaments having a titer of 0.1 to 1.2 dtex and bonded, and is bonded to a thermoplastic synthetic material using an injection-molding process.
2. The composite material as recited in claim 1, wherein the nonwoven fabric is made from melt-spun, aerodynamically stretched multi-component endless filaments having a titer of 1.5 to 3 dtex and directly laid up to form a fibrous web, and the multi-component endless filaments, optionally after prebonding, are split to at least 80% to form micro-endless filaments having a titer of 0.1 to 0.3 dtex, and bonded
3. The composite material as recited in claim 1 or 2, wherein the multi-component endless filament a bicomponent endless filament made from two incompatible polymers, particularly a polyester and a polyamide.
4. The composite material as recited in one of claims 1 through 3, wherein the multi-component endless filaments have a cross-section having an orange-like multi-segment structure, the segments in each case alternately containing one of the two incompatible polymers and/or having a “side-by-side” structure.
5. The composite material as recited in one of claims 1 through 4, wherein at least one of the incompatible polymers forming the multi-component endless filament contains an additive, such as color pigments, permanently acting anti-statics, flame retarding agents and/or additives that influence the hydrophobic properties, in amounts up to 10 percent by weight.
6. A method for producing a composite material as recited in one of claims 1 through 5, wherein multi-component endless filaments are spun from the melt, stretched, and directly laid up to form a web, prebonding is optionally carried out, and the nonwoven fabric is bonded using high-pressure fluid jets, and, at the same time, split into micro-endless filaments having a titer of 0.1 to 1.2 dtex, and bonded to a thermoplastic synthetic material using an injection-molding process.
7. The method as recited in claim 6, wherein the multi-component endless filaments are bonded and split in that the nonwoven fabric, which has been prebonded if necessary, is impacted at least once on each side with high-pressure fluid jets.
8. The method as recited in claim 6 or 7, wherein the multi-component endless filaments are dyed by spin-dyeing and/or overdyeing.
9. The method as recited in one of claims 6 through 8, wherein the nonwoven fabric for the production of the composite material is spot-calandered.
10. The composite material as recited in one of claims 1 to 9, wherein it is used for the production of door, pillar, and/or trunk linings, rear window shelves, car roof linings, dashboards, as well as wheel house liners.
US10/220,193 2000-02-28 2001-01-17 Composite material Abandoned US20030148096A1 (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030220034A1 (en) * 2002-05-22 2003-11-27 Dr. Ing. H.C.F. Porsche Aktiengesellschaft. Wheel house shell for a vehicle and method of making same
US20040131836A1 (en) * 2003-01-02 2004-07-08 3M Innovative Properties Company Acoustic web
US20040231914A1 (en) * 2003-01-02 2004-11-25 3M Innovative Properties Company Low thickness sound absorptive multilayer composite
US20040231915A1 (en) * 2003-01-02 2004-11-25 3M Innovative Properties Company Sound absorptive multilayer composite
EP1543934A1 (en) * 2003-12-17 2005-06-22 Intier Automotive Eybl GmbH (Ebergassing) & Co. OHG Part with textile decoration
US20060065482A1 (en) * 2004-09-30 2006-03-30 Schmidft Richard J Acoustic material with liquid repellency
US20060166583A1 (en) * 2004-11-10 2006-07-27 O'regan Terry Stretchable nonwovens
EP1775110A1 (en) * 2005-10-11 2007-04-18 ISE Intex GmbH Plastic molded part with a non-woven layer partially impregnated by a plastic material and with a textile surface and method of producing the same
US20080261471A1 (en) * 2004-10-22 2008-10-23 Dow Global Technologies Inc. Polyolefinic Materials for Plastic Composites
US20080257641A1 (en) * 2005-04-04 2008-10-23 Gabriele Tocchi Sealed Thin-Multi-Layer Sound Absorber
CN100577259C (en) * 2004-09-27 2010-01-06 卡尔弗罗伊登柏格两合公司 Structure arrangement of plate type filter element in gas filtering device housing
US10737876B2 (en) 2015-07-13 2020-08-11 K-Fee System Gmbh Filter element having a cut-out
US11045035B2 (en) 2015-09-18 2021-06-29 K-Fee System Gmbh Adapter for a single serve capsule
US11084650B2 (en) 2015-06-10 2021-08-10 K-Fee System Gmbh Portion capsule with a three-ply nonwoven fabric

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE60122501T2 (en) * 2000-05-16 2007-02-01 Polymer Group, Inc. METHOD FOR PRODUCING A NONWOVEN FABRIC WITH FISSILE FIBERS
PL2705754T3 (en) * 2012-09-11 2017-07-31 Hans-Martin Rolf Baked good holder with non-woven fabric surface
DE102012018852B4 (en) * 2012-09-25 2016-01-07 Carl Freudenberg Kg Use of microfiber nonwovens for the production of decorative laminates
SG11201610117QA (en) 2014-06-12 2017-01-27 K Fee System Gmbh Single serve capsule with a calendered fibrous material

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4186235A (en) * 1975-04-24 1980-01-29 Imperial Chemical Industries Limited Thermoplastics articles having a surface fused to cloth
US4229397A (en) * 1976-12-10 1980-10-21 Agency Of Industrial Science & Technology Method for forming fiber-reinforced composite material
US5204170A (en) * 1991-08-01 1993-04-20 Basf Corporation High density structural reaction injection molded composite containing a fabric of nonwoven spunbonded fibers made of a polyester core sheathed in a polyamide skin embedded in a polyurethane matrix
US5456976A (en) * 1993-01-05 1995-10-10 The Haartz Corporation Resiliently padded laminate construction and injection molded thermoplastic articles faced therewith
US5759926A (en) * 1995-06-07 1998-06-02 Kimberly-Clark Worldwide, Inc. Fine denier fibers and fabrics made therefrom
US5783503A (en) * 1996-07-22 1998-07-21 Fiberweb North America, Inc. Meltspun multicomponent thermoplastic continuous filaments, products made therefrom, and methods therefor
US5965084A (en) * 1996-10-29 1999-10-12 Chisso Corporation Process for producing non-woven fabrics of ultrafine polyolefin fibers
US5969084A (en) * 1997-04-14 1999-10-19 Mitsubishi Gas Chemical Company Process for producing polycarbonate resin with high flowability
US6200669B1 (en) * 1996-11-26 2001-03-13 Kimberly-Clark Worldwide, Inc. Entangled nonwoven fabrics and methods for forming the same
US6706652B2 (en) * 2000-01-22 2004-03-16 Firma Carl Freudenberg Cleaning cloth

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE59902625D1 (en) * 1998-07-02 2002-10-17 Intier Automotive Eybl Ges M B Method for producing multilayer components
DE19934442C2 (en) * 1999-07-26 2001-09-20 Freudenberg Carl Fa Process for producing a nonwoven and nonwoven for producing cleanroom protective clothing

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4186235A (en) * 1975-04-24 1980-01-29 Imperial Chemical Industries Limited Thermoplastics articles having a surface fused to cloth
US4229397A (en) * 1976-12-10 1980-10-21 Agency Of Industrial Science & Technology Method for forming fiber-reinforced composite material
US5204170A (en) * 1991-08-01 1993-04-20 Basf Corporation High density structural reaction injection molded composite containing a fabric of nonwoven spunbonded fibers made of a polyester core sheathed in a polyamide skin embedded in a polyurethane matrix
US5456976A (en) * 1993-01-05 1995-10-10 The Haartz Corporation Resiliently padded laminate construction and injection molded thermoplastic articles faced therewith
US5456976B1 (en) * 1993-01-05 1998-06-30 Haartz Corp Resiliently padded laminate construction and injection molded thermoplastic articles faced therewith
US5759926A (en) * 1995-06-07 1998-06-02 Kimberly-Clark Worldwide, Inc. Fine denier fibers and fabrics made therefrom
US5783503A (en) * 1996-07-22 1998-07-21 Fiberweb North America, Inc. Meltspun multicomponent thermoplastic continuous filaments, products made therefrom, and methods therefor
US5965084A (en) * 1996-10-29 1999-10-12 Chisso Corporation Process for producing non-woven fabrics of ultrafine polyolefin fibers
US6200669B1 (en) * 1996-11-26 2001-03-13 Kimberly-Clark Worldwide, Inc. Entangled nonwoven fabrics and methods for forming the same
US5969084A (en) * 1997-04-14 1999-10-19 Mitsubishi Gas Chemical Company Process for producing polycarbonate resin with high flowability
US6706652B2 (en) * 2000-01-22 2004-03-16 Firma Carl Freudenberg Cleaning cloth

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030220034A1 (en) * 2002-05-22 2003-11-27 Dr. Ing. H.C.F. Porsche Aktiengesellschaft. Wheel house shell for a vehicle and method of making same
US20040131836A1 (en) * 2003-01-02 2004-07-08 3M Innovative Properties Company Acoustic web
US20040231914A1 (en) * 2003-01-02 2004-11-25 3M Innovative Properties Company Low thickness sound absorptive multilayer composite
US20040231915A1 (en) * 2003-01-02 2004-11-25 3M Innovative Properties Company Sound absorptive multilayer composite
US20060237130A1 (en) * 2003-01-02 2006-10-26 3M Innovative Properties Company Acoustic web
US20080073146A1 (en) * 2003-01-02 2008-03-27 3M Innovative Properties Company Sound absorptive multilayer composite
EP1543934A1 (en) * 2003-12-17 2005-06-22 Intier Automotive Eybl GmbH (Ebergassing) & Co. OHG Part with textile decoration
CN100577259C (en) * 2004-09-27 2010-01-06 卡尔弗罗伊登柏格两合公司 Structure arrangement of plate type filter element in gas filtering device housing
US7500541B2 (en) 2004-09-30 2009-03-10 Kimberly-Clark Worldwide, Inc. Acoustic material with liquid repellency
US20060065482A1 (en) * 2004-09-30 2006-03-30 Schmidft Richard J Acoustic material with liquid repellency
US20110114215A1 (en) * 2004-10-22 2011-05-19 Dow Global Technologies Inc. Composite pipes and method making same
US7887660B2 (en) 2004-10-22 2011-02-15 Dow Global Technologies Inc. Composite pipes and method making same
US20080265457A1 (en) * 2004-10-22 2008-10-30 Mcleod David G Plastic Composite Articles and Methods of Making Same
US20080265464A1 (en) * 2004-10-22 2008-10-30 D Hooghe Edward L Apparatus and Process for Manufacturing Shaped Plastic Reinforced Composite Articles
US20080261471A1 (en) * 2004-10-22 2008-10-23 Dow Global Technologies Inc. Polyolefinic Materials for Plastic Composites
US9227346B2 (en) 2004-10-22 2016-01-05 Dow Global Technologies Llc Plastic composite articles and methods of making same
US8685514B2 (en) 2004-10-22 2014-04-01 Dow Global Technologies Llc Composite pipes and method making same
US8043696B2 (en) 2004-10-22 2011-10-25 Dow Global Technologies Llc Microlayer structures and methods
US20060166583A1 (en) * 2004-11-10 2006-07-27 O'regan Terry Stretchable nonwovens
US20080257641A1 (en) * 2005-04-04 2008-10-23 Gabriele Tocchi Sealed Thin-Multi-Layer Sound Absorber
US7677358B2 (en) * 2005-04-04 2010-03-16 Rieter Technologies, AG Sealed thin-multi-layer sound absorber
EP1775110A1 (en) * 2005-10-11 2007-04-18 ISE Intex GmbH Plastic molded part with a non-woven layer partially impregnated by a plastic material and with a textile surface and method of producing the same
US11084650B2 (en) 2015-06-10 2021-08-10 K-Fee System Gmbh Portion capsule with a three-ply nonwoven fabric
US10737876B2 (en) 2015-07-13 2020-08-11 K-Fee System Gmbh Filter element having a cut-out
US11498750B2 (en) 2015-07-13 2022-11-15 Gcs German Capsule Solution Gmbh Filter element having a cut-out
US11045035B2 (en) 2015-09-18 2021-06-29 K-Fee System Gmbh Adapter for a single serve capsule

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EP1259366A1 (en) 2002-11-27
WO2001064416A1 (en) 2001-09-07

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