EP3771761B1 - Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric - Google Patents
Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric Download PDFInfo
- Publication number
- EP3771761B1 EP3771761B1 EP19189237.1A EP19189237A EP3771761B1 EP 3771761 B1 EP3771761 B1 EP 3771761B1 EP 19189237 A EP19189237 A EP 19189237A EP 3771761 B1 EP3771761 B1 EP 3771761B1
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- EP
- European Patent Office
- Prior art keywords
- filaments
- sheath
- core
- spunbond nonwoven
- nonwoven material
- Prior art date
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- 239000004745 nonwoven fabric Substances 0.000 title description 50
- 238000000151 deposition Methods 0.000 claims description 36
- 239000000463 material Substances 0.000 claims description 26
- -1 polyethylene Polymers 0.000 claims description 25
- 238000001816 cooling Methods 0.000 claims description 21
- 229920000728 polyester Polymers 0.000 claims description 13
- 239000004743 Polypropylene Substances 0.000 claims description 11
- 229920000098 polyolefin Polymers 0.000 claims description 11
- 229920001155 polypropylene Polymers 0.000 claims description 11
- 239000004698 Polyethylene Substances 0.000 claims description 10
- 229920000573 polyethylene Polymers 0.000 claims description 10
- 238000009987 spinning Methods 0.000 claims description 6
- 229920001634 Copolyester Polymers 0.000 claims description 5
- 238000007596 consolidation process Methods 0.000 description 34
- 238000005192 partition Methods 0.000 description 16
- 229920003023 plastic Polymers 0.000 description 12
- 239000004033 plastic Substances 0.000 description 12
- 229920000139 polyethylene terephthalate Polymers 0.000 description 10
- 239000005020 polyethylene terephthalate Substances 0.000 description 10
- 238000005299 abrasion Methods 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 229920000747 poly(lactic acid) Polymers 0.000 description 8
- 229920001707 polybutylene terephthalate Polymers 0.000 description 8
- 239000000203 mixture Substances 0.000 description 7
- 239000000306 component Substances 0.000 description 6
- 238000002788 crimping Methods 0.000 description 6
- 239000000835 fiber Substances 0.000 description 6
- 230000008018 melting Effects 0.000 description 6
- 230000007547 defect Effects 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 229920001577 copolymer Polymers 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000000178 monomer Substances 0.000 description 3
- 229920000642 polymer Polymers 0.000 description 3
- 229920005606 polypropylene copolymer Polymers 0.000 description 3
- 229920001169 thermoplastic Polymers 0.000 description 3
- 239000012815 thermoplastic material Substances 0.000 description 3
- 239000004416 thermosoftening plastic Substances 0.000 description 3
- 238000005253 cladding Methods 0.000 description 2
- 239000011258 core-shell material Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 239000000654 additive Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
Images
Classifications
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/005—Synthetic yarns or filaments
- D04H3/009—Condensation or reaction polymers
- D04H3/011—Polyesters
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D5/00—Formation of filaments, threads, or the like
- D01D5/22—Formation of filaments, threads, or the like with a crimped or curled structure; with a special structure to simulate wool
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D5/00—Formation of filaments, threads, or the like
- D01D5/28—Formation of filaments, threads, or the like while mixing different spinning solutions or melts during the spinning operation; Spinnerette packs therefor
- D01D5/30—Conjugate filaments; Spinnerette packs therefor
- D01D5/34—Core-skin structure; Spinnerette packs therefor
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/005—Synthetic yarns or filaments
- D04H3/007—Addition polymers
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/018—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the shape
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/14—Non-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 thermoplastic yarns or filaments produced by welding
- D04H3/147—Composite yarns or filaments
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2331/00—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
- D10B2331/04—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyesters, e.g. polyethylene terephthalate [PET]
Definitions
- the invention relates to a spunbond nonwoven fabric made from continuous filaments, in particular from crimped continuous filaments, the filaments being designed as bicomponent filaments or as multicomponent filaments.
- the invention further relates to a device for producing a spunbond nonwoven fabric from continuous filaments, in particular from crimped continuous filaments. It is within the scope of the invention that the continuous filaments and continuous filaments are made of thermoplastic material. Because of their quasi-endless length, continuous filaments differ from staple fibers, which have much shorter lengths of, for example, 10 mm to 60 mm.
- high-loft nonwovens are nonwovens that are relatively thick and at the same time relatively soft.
- the production of these nonwovens is not possible without any problems, however, since the nonwovens generally have to have sufficient strength and abrasion resistance at the same time. To this extent, there is a conflict of objectives.
- the setting of a higher strength or abrasion resistance is normally at the expense of the thickness and the softness of the nonwoven fabric.
- maintaining a large thickness and high softness usually leads to less strong and abrasion-resistant nonwovens. So far, there are hardly any known satisfactory solutions.
- a high thickness of nonwovens is usually produced with the help of curling or crimping fibers / filaments.
- bicomponent filaments with a side-by-side configuration or with an eccentric or asymmetrical core-sheath configuration are used in particular.
- Many of the previously known nonwovens made from crimping or crimping are characterized by a relatively high defect rate.
- undesired agglomerates are found in the nonwovens, which adversely affect the homogeneity.
- WO 2018/110523 discloses the use of bicomponent filaments having an eccentric core-sheath configuration for the manufacture of nonwovens.
- the invention is based on the technical problem of specifying a nonwoven fabric which has an optimal thickness and an optimal softness and at the same time has sufficient strength or tensile strength and sufficient abrasion resistance.
- the nonwoven should be as free as possible from defects and, in particular, as free as possible from agglomerates.
- the invention is also based on the technical problem of specifying a device for producing such a nonwoven fabric.
- the invention teaches a spunbond nonwoven fabric made from continuous filaments, in particular from crimped or crimped continuous filaments, the filaments being designed as bicomponent filaments or as multicomponent filaments and having an eccentric core-sheath configuration and wherein the sheath of the filaments in the filament cross-section has a constant thickness or an essentially constant thickness over at least 20%, in particular over at least 25%, preferably over at least 30%, preferably over at least 35% and very preferably over at least 40% of the filament circumference and wherein the thickness of the jacket in the region of its constant or substantially constant thickness d is 0.1 to 2 ⁇ m.
- the thickness of the sheath of the filaments is the mean thickness or mean sheath thickness, specifically preferably the mean sheath thickness in relation to a filament.
- the jacket thickness or the jacket thicknesses are expediently with Measured using a scanning electron microscope.
- the jacket thickness or the mean jacket thickness is measured on filaments or filament sections that are not involved in a thermal pre-consolidation or consolidation and are therefore in particular not part of bonding points or bonding points. In other words, the sheath thickness is measured on the filaments or on the filament sections outside the bonding points or bonding points.
- the continuous filaments of the nonwoven fabric consist or essentially consist of thermoplastic material.
- Crimped endless filaments in the context of the invention means in particular that the crimped filaments each have a crimp with at least 1.5, preferably with at least 2, preferably with at least 2.5 and very preferably with at least 3 loops per centimeter of their length.
- a recommended embodiment of the invention is characterized in that the continuous filaments of the spunbond nonwoven fabric according to the invention have a crimp of 1.8 to 3.2, in particular 2 to 3 loops per centimeter of their length.
- the number of crimped loops or crimped arcs (loops) per centimeter of length of the filaments is measured in particular according to the Japanese standard JIS L-1015-1981 by counting the crimps under a pretension of 2 mg / den in (1/10 mm) based on the unstretched length of the filaments. A sensitivity of 0.05 mm is used to determine the number of curling loops. The measurement is expediently carried out with a "Favimat” device from TexTechno, Germany. Reference is made to the publication "Automatic Crimp Measurement on Staple Fibers", Denkendorf Colloquium ",” Textile Mess- und expresstechnik ", November 9, 1999, Dr. Ulrich Mörschel (in particular p. 4, Fig. 4 ) referenced.
- the filaments are / is removed from the deposit or from the deposit belt as a filament ball before further solidification and the filaments are separated and measured.
- bicomponent filaments or multicomponent filaments with an eccentric core-sheath configuration are used for the spunbond nonwoven fabric. It is within the scope of the invention that the sheath of the filaments completely surrounds the core. Furthermore, it is within the scope of the invention that the material or the plastic of the jacket has a lower melting point than the material or the plastic of the core of the filaments.
- the invention is based on the knowledge that with the spunbond nonwoven fabric according to the invention, a great thickness and a high softness and nevertheless sufficient strength and abrasion resistance can be achieved without any problems.
- strength means, in particular, the strength of the nonwoven in the machine direction (MD). With the nonwoven fabric according to the invention, a completely satisfactory strength can be achieved without any appreciable loss of thickness.
- the invention is further based on the knowledge that due to the cross-sectional structure of the filaments according to the invention, an optimal crimp can be achieved and, above all, can also be easily adjusted by varying the parameters - whereby the desired thickness and the desired softness is achieved - and at the same time that via Sheath material encircling the entire filament circumference can be used effectively for thermal pre-consolidation.
- bonding points are produced between the filaments with the aid of the lower-melting sheath material of the filaments, and these bond points in the nonwoven fabric according to the invention with the filament properties according to the invention an optimal strength and abrasion resistance of the nonwoven fabric while still maintaining sufficient thickness and softness.
- the nonwovens according to the invention can be formed surprisingly free of defects and, above all, are largely free of troublesome agglomerates. As a result, a very homogeneous fiber layer or nonwoven layer can be achieved.
- a nonwoven fabric according to the invention is recommended to have a thickness of more than 0.5 mm, in particular of more than 0.55 mm and preferably a thickness of more than 0.6 mm. It is within the scope of the invention that the nonwovens according to the invention have a strength in the machine direction (MD) of more than 20 N / 5 cm, in particular of more than 25 N / 5 cm.
- MD machine direction
- the above thickness and strength values apply in particular to nonwovens with a basis weight of 10 to 50 g / m 2 , preferably with a basis weight of 15 to 40 g / m 2 and preferably with a basis weight of 18 to 35 g / m 2 .
- the core of the filaments takes up more than 40%, in particular more than 50%, preferably more than 60%, preferably more than 65% and very preferably more than 70% of the area of the filament cross-section of the filaments. According to one embodiment of the invention, the core of the filaments takes up more than 75% of the area of the filament cross-section of the filaments.
- the core of the filaments is designed in the shape of a segment of a circle when viewed in the filament cross-section and preferably has at least one, in particular a circular arc-shaped circumferential section or substantially circular arc-shaped circumferential section with regard to its circumference.
- the core of the filaments is recommended to have the Viewed filament cross-section, additionally at least one, in particular a linear or essentially linear, circumferential section.
- the core of the filaments, viewed in the filament cross section consists of an arcuate or essentially arcuate circumferential section and a linear or essentially linear circumferential section - expediently directly adjoining it.
- a proven embodiment of the invention is characterized in that the circular arc-shaped or essentially circular arc-shaped circumferential section of the core takes up over 40%, in particular over 50%, preferably over 60% and preferably over 65% of the circumference of the core.
- a recommended embodiment is characterized in that the sheath of the filaments - viewed in the filament cross-section - outside the sheath area with the constant or essentially constant thickness is formed in the shape of a segment of a circle or essentially in the shape of a segment of a circle.
- This circular segment expediently has at least one, in particular a circular arc-shaped or essentially circular arc-shaped, circumferential section and preferably at least one, in particular a linear or essentially linear, circumferential section with regard to its circumference.
- the jacket section in the form of a segment of a circle preferably consists of a circular arc-shaped or essentially circular arc-shaped circumferential section and a linear or essentially linear circumferential section — expediently directly adjoining it.
- the thickness of the jacket in the region of its constant or essentially constant thickness is less than 10%, in particular less than 8%, preferably less than 7% and preferably less than 3% of the filament diameter or the largest filament diameter.
- the thickness of the jacket in the region of its constant or essentially constant thickness is expediently at least 0.5%, in particular at least 1% and preferably at least 1.2% of the filament diameter or the largest filament diameter.
- the spinneret for producing the filaments is preferably selected or set up with the proviso that the filaments leaving the spinneret have the relative thickness values or percentage thickness values for the jacket given above and below in the not yet drawn state. However, it is also within the scope of the invention that these relative thickness values also apply to the sheath of the filaments in the finished spunbond nonwoven fabric.
- the thickness of the jacket in the region of its constant or essentially constant thickness in the finished spunbond nonwoven material is 0.15 to 1.5 ⁇ m and in particular 0.1 to 0.9 ⁇ m.
- the ratio of the mass of the core to the mass of the sheath in the filaments of the spunbond nonwoven fabric according to the invention is 90:10 to 40:60, preferably 90:10 to 60:40 and preferably 85:15 to 70:30.
- a particularly recommended embodiment of the invention is characterized in that, with regard to the filament cross section, the distance a of the centroid of the core from the centroid of the sheath is 5% to 38%, in particular 6% to 36% and preferably 6% to 34%, preferably 7% to 33% of the filament diameter or the largest filament diameter.
- a very preferred embodiment of the invention is characterized in that, with regard to the filament cross-section, the distance a of the centroids of the core and sheath with a core: sheath mass ratio of 85:15 to 70:30 is between 5% and 36% of the filament diameter or the largest Filament diameter is.
- the distance a between the centroids is preferably between 12% and 40% of the filament diameter or the largest filament diameter.
- the distance a between the centers of area of the core and sheath is recommended between 18% and 36%, in particular between 20% and 31% of the filament diameter or the largest filament diameter.
- a particularly recommended embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists or essentially consists of at least one polyolefin.
- “essentially consists” primarily means that the core and / or the jacket comprises at least 90% by weight, preferably at least 95% by weight and preferably at least 97% by weight of the respective plastic.
- both the core and the sheath of the filaments each consist of at least one polyolefin, in particular of a polyolefin or essentially of at least one polyolefin, in particular essentially of one Polyolefin.
- a very particularly preferred embodiment of the invention is characterized in that the sheath of the filaments consists or essentially consists of polyethylene and that the core of the filaments consists of polypropylene or essentially consists of polypropylene. It has already been stated above that it is within the scope of the invention that the sheath of the filaments consists or essentially consists of the lower-melting material or plastic compared to the core of the filaments.
- copolymers of the aforementioned polyolefins can also be used in the context of the invention, either alone in the core and / or in the shell or in a mixture with at least one homopolyolefin. Mixtures of homopolyolefins can also be used for the core and / or for the shell. Mixtures with other plastics are also possible.
- polypropylene is used or polypropylene is used for the core, it is preferably a polypropylene with a melt flow rate of more than 25 g / 10 min, in particular more than 40 g / 10 min, preferably more than 50 g / 10 min, preferably more than 55 g / 10 min and very preferably more than 60 g / 10 min.
- the melt flow rate (MFR) is measured in particular according to ASTM D1238-13 (condition B, 2.16 kg, 230 ° C).
- polyethylene is used as a component, in particular as a component for the jacket, it is expediently a polyethylene with a melt flow rate below 35 g / 10 min, in particular below 25 g / 10 min, preferably below 20 g / 10 min
- the melt flow rate is measured in particular according to ASTM D1238-13 at 190 ° C. / 2.16 kg.
- One embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists or essentially consists of at least one polyester and / or of at least one copolyester.
- a recommended embodiment is characterized in that the core of the filaments consists or essentially consists of at least one polyester, in particular a polyester, and that the sheath preferably consists of at least one, in particular a polyester and / or copolyester with a lower melting point than the core component exists or essentially exists. It is also possible that the core consists or substantially consists of at least one polyester and / or of at least one copolyester and that the jacket consists or substantially consists of at least one polyolefin.
- PET Polyethylene terephthalate
- Co-PET PET copolymer
- PBT polybutylene terephthalate
- PLA polylactide
- copolymers of these polyesters can also be used as polyester. It is moreover within the scope of the invention that mixtures or blends of polymers or the polymers mentioned can also be used for the core and / or for the sheath of the filaments.
- a proven embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists of at least one plastic from the group "polyolefin, polyolefin copolymer, in particular polyethylene, polypropylene, polyethylene copolymer, polypropylene copolymer; polyester, polyester -Copolymer, in particular polyethylene terephthalate (PET), PET copolymer, polybutylene terephthalate (PBT), PBT copolymer, polylactide (PLA), PLA copolymer "consists or essentially consists.
- PET polyethylene terephthalate
- PET PET copolymer
- PBT polybutylene terephthalate
- PBT PBT copolymer
- PLA copolymer polylactide
- the plastic of the jacket has a lower melting point than the plastic of the core.
- a recommended embodiment of the invention is characterized in that the core of the filaments consists of at least one plastic from the group "polypropylene, polypropylene copolymer, polyethylene terephthalate (PET), PET copolymer, polybutylene terephthalate (PBT), PBT copolymer, polylactide (PLA), PLA copolymer” or essentially consists.
- the sheath of the filaments consists of at least one plastic from the group "polyethylene, polyethylene copolymer, polypropylene, polypropylene copolymer".
- the titer of the filaments used for the spunbond nonwoven fabric according to the invention is between 1 and 12 den. According to a recommended embodiment, the titer of the filaments is between 1.0 and 2.5 den, in particular between 1.5 and 2.2 den, and preferably between 1.8 and 2.2 den. This titer or this filament diameter has proven particularly useful in terms of solving the technical problem according to the invention.
- a well-proven embodiment is characterized in that the spunbond nonwoven according to the invention is a thermally pre-bonded and / or thermally bonded nonwoven which has thermal bonding points or thermal bonding points between the filaments.
- the spunbond nonwoven according to the invention is a nonwoven thermally pre-bonded with hot air and / or thermally bonded nonwoven.
- the thermal pre-consolidation of the nonwoven fabric can in principle also be carried out by compacting rollers. It is also within the scope of the invention that a thermal pre-consolidation or consolidation of the nonwoven fabric is carried out with the aid of a calender.
- the invention is based on the knowledge that in the configuration according to the invention of the cross-sections of the filaments, an optimal pre-consolidation or thermal pre-consolidation of the spunbonded nonwovens is possible and nevertheless sufficient crimp and thus the desired thickness of the nonwoven fabric can be maintained. In this respect, an optimal compromise between sufficient crimp and thus sufficient thickness on the one hand and optimal consolidation of the nonwovens is possible.
- the crimp can be set in a targeted manner by varying the cross-sectional parameters of the filaments and it is also easy to ensure that the crimp does not become too large and that the desired thickness can be created precisely and functionally and, in addition, an effective pre-consolidation of the Nonwoven fabric can be carried out.
- the invention also teaches a device for producing a spunbond nonwoven fabric from continuous filaments, in particular from crimped continuous filaments, with at least one spinneret being present, the device or the spinneret being set up with the proviso that multicomponent filaments or bicomponent filaments with an eccentric core-sheath configuration, the sheath of the filaments seen in the filament cross-section over at least 20%, in particular over at least 25%, preferably over at least 30%, preferably over at least 35% and very preferably over at least 40% of the filament circumference has a constant thickness or a substantially constant thickness, the thickness of the jacket in the region of its constant or substantially constant thickness d being 0.1 to 2 ⁇ m and the filaments being deposited on a depositing device, in particular on a depositing screen belt.
- the device is a spunbond device. It is recommended that the device has a cooling device for cooling the filaments and a stretching device connected to it for stretching the filaments. Furthermore, the device is preferably equipped with at least one diffuser connected to the stretching device. - A particularly preferred one Embodiment of the invention is characterized in that the unit from the cooling device and the stretching device is designed as a closed unit and that apart from the supply of cooling air in the cooling device, no further air supply takes place from the outside into this unit.
- a thermal pre-consolidation of the fiber deposit or the nonwoven web can be carried out.
- at least one thermal pre-consolidation device is provided.
- a recommended embodiment of the invention is characterized in that the at least one thermal pre-consolidation device is designed as a hot-air pre-consolidation device.
- the thermal pre-consolidation device expediently has at least one hot air knife and / or at least one hot air oven.
- thermal pre-consolidation or consolidation can also be carried out with pressure rollers or compacting rollers and / or at least one calender can be used for pre-consolidation or consolidation.
- a thermal pre-consolidation of the deposited nonwoven web takes place first with the help of at least one hot air knife, in particular with the help of a hot air knife, and then a further thermal pre-consolidation takes place with the help of at least one hot air oven, in particular with the help of a hot air oven.
- a preferred embodiment of the invention is characterized in that the spunbond nonwoven is only pre-bonded with hot air and / or is only finally bonded with hot air.
- the invention is based on the knowledge that due to the filament cross-section according to the invention on the one hand the the entire filament circumference is available for thermal pre-consolidation and, on the other hand, through a targeted selection of parameters - in particular the thickness of the jacket - the thermal pre-consolidation or the extent of the thermal pre-consolidation can be specifically influenced, so that, on the one hand, an optimal consolidation of the nonwoven can be achieved and on the other hand, the crimp of the filaments is nevertheless not impaired too much in order to maintain a desired thickness of the nonwoven fabric.
- a very simple and targeted setting of the nonwoven properties - in particular with regard to thickness, softness and strength - is possible. Above all, with the invention, the crimp can be adjusted without any problems and can thus be controlled.
- the nonwovens according to the invention are characterized on the one hand by an optimal thickness and softness and on the other hand by a satisfactory strength or abrasion resistance.
- the crimping of the filaments can easily be kept within the desired limits due to the configuration of the filaments according to the invention, so that at the same time a controllable crimp or a controllable crimp is the result of the teaching according to the invention.
- optimal strength and abrasion resistance that are easy to set, a largely defect-free nonwoven fabric can also be achieved, which above all is essentially free of troublesome agglomerates.
- an optimal compromise between strength properties and thickness or softness properties of the nonwoven fabric can be achieved and this compromise can be achieved in a simple manner with a surprisingly homogeneous filament deposition.
- the Fig. 1 shows in comparison a section through a continuous filament 2 with a conventional eccentric core-sheath configuration ( Fig. 1a ) and by a continuous filament 2 with an eccentric core-sheath configuration according to the invention ( Figure 1b ).
- Bicomponent filaments with a first component made of thermoplastic in the sheath 3 and with a second component made of thermoplastic in the core 4.
- the component in the sheath 3 has a lower melting point than the component in the core 4.
- the sheath 3 of the filaments 2 preferably has a constant thickness d in the filament cross section and in the exemplary embodiment over more than 50% of the filament circumference.
- the core 4 of the filaments 2 takes up more than 65% of the area of the filament cross section of the filaments 2.
- the core 4 of the filaments 2 according to the invention - viewed in the filament cross section - is designed in the shape of a segment of a circle.
- the core 4 has an arcuate circumferential section 5 and a linear circumferential section 6 with respect to its circumference.
- the circular arc-shaped circumferential section of the core 4 takes up over 65% of the circumference of the core 4.
- the jacket 3 of the filaments 2 - viewed in the filament cross section - is designed in the shape of a segment of a circle outside the jacket area with the constant thickness d.
- This circular segment 7 of the jacket 3 has, as recommended and in the exemplary embodiment with regard to its circumference, a circular arc-shaped circumferential section 8 and a linear circumferential section 9.
- the thickness d or the mean thickness d of the jacket 3 is preferably 1% to 8%, in particular 2% to 10%, in the region of its constant thickness Filament diameter D.
- the thickness d of the jacket 3 in the region of its constant thickness may be 0.2 to 3 ⁇ m.
- the Fig. 2 shows the distance a of the centroid of the core 4 from the centroid of the sheath 3 of an endless filament 2 according to the invention.
- This distance a of the centroids of the core 4 and sheath 3 is at a given mass or area ratio of core and sheath material in the endless filaments 2 according to the invention regularly larger than with conventional continuous filaments 2 with an eccentric core-sheath configuration.
- the distance a of the centroid of the core 4 from the centroid of the sheath 3 in the filaments 2 according to the invention is preferably 5 to 40% of the filament diameter D or the largest filament diameter D.
- the 3 shows schematically for preferred embodiments of the invention the dependence of the distance a of the centroids of the core 4 and sheath 3 on the constant thickness d of the sheath 3 of the endless filaments 2 according to the invention.
- the dependence here is for an area proportion of the core 4 of 75%, of 67% and represented by 50%.
- the distance a and the constant jacket thickness d of the jacket 3 are each given in micrometers.
- the underlying endless filaments 2 according to the invention here have a filament diameter D of 18 ⁇ m.
- the table below shows the distances a between the centers of area of core 4 and sheath 3 for continuous filaments 2 with a filament diameter D of 18 ⁇ m for different core: sheath ratios (75:25, 67:33 and 50:50). In the table on the left, these distances are listed for a constant sheath thickness d of 1 ⁇ m in the case of the continuous filaments according to the invention with an eccentric core-sheath configuration (eC / S filaments according to the invention).
- the distance a of the centroids with the same filament diameter D and the same area ratio core: sheath in the endless filaments 2 according to the invention with an eccentric core-sheath configuration is greater or significantly greater than in the conventional continuous filaments 2 with an eccentric core Jacket configuration. Maintaining the distance a between the centers of area of the core 4 and cladding 3 is an essential feature of the invention, which is of particular importance.
- the distance between the centers of gravity is representative of the lever arm with which the crimping forces from the two materials act and thus an essential factor for the extent of the crimping.
- the core 4 of the filaments 2 according to the invention consists of polypropylene and the sheath 3 of the filaments 2 consists of polyethylene.
- the melting point of the thermoplastic material of the jacket 3 is lower than the melting point of the thermoplastic synthetic material of the core 4 of the continuous filaments 2 according to the invention.
- the continuous filaments 2 of a spunbond nonwoven fabric 1 according to the invention have a titer of 1.5 to 2.5 denier, preferably 1.5 to 2.2 denier and preferably 1.8 to 2.2 denier.
- This titer has proven to be particularly useful in terms of solving the technical problem.
- the spunbond nonwoven 1 according to the invention is a thermally pre-consolidated spunbond nonwoven, with thermal bonding points or bonding points between the continuous filaments 2.
- it is the spunbond nonwoven fabric 1 according to the invention by a spunbond nonwoven fabric 1 thermally pre-consolidated with hot air.
- Such a spunbond nonwoven fabric 1 has proven to be very useful in terms of solving the technical problem.
- the Fig. 4 shows a device according to the invention for producing a spunbond nonwoven fabric 1 according to the invention, which consists in particular of crimped continuous filaments 2.
- the spunbond device comprises a spinneret 10 or a spinnerette for spinning the continuous filaments 2.
- the spinning nozzle 10 or the device is designed so that the continuous filaments 2 are produced as multicomponent filaments or bicomponent filaments with an eccentric core-sheath configuration preferably as continuous filaments 2, in which the sheath 3, viewed in the filament cross-section, has a constant thickness d over at least 50% of the filament circumference.
- the spun continuous filaments 2 are introduced into a cooling device 11 with a cooling chamber 12.
- air supply cabins 13, 14 arranged one above the other are arranged on two opposite sides of the cooling chamber 12. Air of different temperatures is expediently introduced into the cooling chamber 12 from the air supply cabins 13, 14 arranged one above the other.
- a monomer suction device 15 is arranged between the spinneret 10 and the cooling device 11. With this monomer suction device 15, interfering gases occurring during the spinning process can be removed from the device. These gases can be, for example, monomers, oligomers or decomposition products and similar substances.
- a stretching device 16 for stretching the continuous filaments 2 is connected downstream of the cooling device 11 in the filament flow direction.
- the stretching device 16 has an intermediate channel 17 which connects the cooling device 11 to a stretching shaft 18 of the stretching device 16.
- the unit from the cooling device 11 and the stretching device 16 or the unit from the cooling device 11, the intermediate channel 17 and the stretching shaft 18 is designed as a closed unit and, apart from the supply of cooling air in the cooling device 11, there is no further air supply from the outside into this unit.
- a diffuser 19 through which the continuous filaments 2 are guided, adjoins the stretching device 16 in the filament flow direction.
- the endless filaments 2 are preferably deposited on a depositing device designed as a depositing screen belt 20 in the exemplary embodiment.
- the depositing screen belt 20 is preferred and, in the exemplary embodiment, is designed as a continuously revolving depositing screen belt 20. It is expediently designed to be air-permeable, so that suction from below through the screen belt 20 is possible.
- the diffuser 19 or the diffuser 19 arranged directly above the depositing screen belt 20 has two opposite diffuser walls, two lower diverging diffuser wall sections 21, 22 being provided, which are preferably designed asymmetrically with respect to the center plane M of the diffuser 19.
- the inlet-side diffuser wall section 21 forms a smaller angle ⁇ with the center plane M of the diffuser 19 than the outlet-side diffuser wall section 22.
- This preferred embodiment is of particular importance in the context of the invention and it has proven particularly in terms of solving the technical problem proven.
- the terms inlet side and outlet side relate here to the running direction of the depositing screen belt 20 or to the conveying direction of the nonwoven web.
- two opposite secondary air inlet gaps 24, 25 are provided at the inflow end 23 of the diffuser 19, each of which is arranged on one of the two opposite diffuser walls.
- a lower secondary air volume flow can preferably be introduced through the secondary air inlet gap 24 on the inlet side with respect to the conveying direction of the depositing screen belt 20 than through the secondary air inlet gap 25 on the outlet side this embodiment is of particular importance in the context of the invention.
- a suction device with which air or process air can be sucked through the depositing screen belt 20 in a main suction area 27 in the deposit area 26 of the filaments 2.
- the main suction area 27 is expediently delimited below the depositing screen belt 20 in an inlet area of the depositing screen belt 20 and in an outlet area of the depositing screen belt 20 by a suction partition 28.
- a second suction area 29 is connected downstream of the main suction area 27 in the conveying direction of the depositing screen belt 20, in which air or process air can be sucked through the depositing screen belt 20. It is recommended that the suction speed v 2 of the process air through the depositing screen belt 20 in the second suction area 29 is lower than the suction speed v H in the main suction area 27.
- a particularly preferred embodiment is characterized in that the end of a suction partition 28 facing the depositing screen belt 20 has a vertical distance A from the depositing screen belt 20 between 10 and 250 mm, in particular between 25 and 200 mm, preferably between 28 and 150 mm and preferably between 29 and 140 mm and very preferably between 30 and 120 mm.
- a partition section designed as a spoiler section 30 is connected in the area of this suction partition 28 facing the depositing screen belt 20, which includes the named end of the suction partition 28 facing the depositing screen belt 20.
- this spoiler section 30 facing the depositing screen belt 20 forms an imaginary extension of the remaining associated suction partition 28 has horizontal distance C, which corresponds to at least 80% of the vertical distance A.
- the distances A and C are not shown in the figures.
- a suction partition wall 28 on the screen belt side has a partition wall section which is angled from the rest of the suction partition wall 28 and is designed as a spoiler section 30.
- this spoiler section 30 is provided on the outlet-side suction partition wall 28 of the main suction area 27.
- the spoiler section 30 is more angled with respect to a vertical oriented perpendicular to the filing screen belt surface than a partition wall section of the further, opposite suction partition 28 facing the filing screen belt 20.
- the spoiler section 30, when projected onto the filing screen belt surface has a greater length than the corresponding one Projection of an angled or bent partition section of the further opposite suction partition 28 facing the depositing screen belt 20.
- the spoiler section 30 has a greater distance from the depositing screen belt 20 with respect to its end on the screen belt side than the end of the partition wall section of the further opposite suction partition 28 facing the depositing screen belt 20
- the embodiment with the spoiler section 30 ensures a very even and continuous transition of the suction speeds from the house ptabsaug Colour 27 to the area following in the conveying direction of the depositing screen belt 20 and in particular to the second suction area 29. Due to the arrangement of the spoiler section 30, a very continuous steady decrease in the suction speed can be achieved.
- defects in the nonwoven web or in the spunbond nonwoven fabric 1 according to the invention can be largely avoided, which can occur due to abrupt changes in the suction speed, for example due to backflow effects (so-called blow-back effects) in the Transition area between the main suction area 27 and the second suction area 29.
- the embodiment with the spoiler section 30 is therefore a very preferred embodiment which contributes to solving the technical problem of the invention.
- At least one thermal pre-consolidation device for thermal pre-consolidation of the nonwoven web is provided in the conveying direction of the nonwoven web after the depositing area 26.
- the thermal pre-consolidation device is preferably arranged on or above the second suction area 29.
- the thermal pre-consolidation device works with hot air and particularly preferably this thermal pre-consolidation device downstream of the main suction area 27 is a hot air knife 31.
- At least two thermal pre-consolidation devices are provided for pre-consolidation of the nonwoven web.
- the first thermal preconsolidation device in the conveying direction of the nonwoven web is expediently a hot air knife 31, and a second thermal preconsolidation device in the form of a hot air oven 32 is preferably connected downstream of this hot air knife 31 in the conveying direction of the depositing screen belt 20.
- air is sucked through the sieve belt 20 in the area of the hot air oven 32 as well.
- the suction speed of the air sucked off by the depositing screen belt 20 from Main suction area 27 decreases to further suction areas in the conveying direction of the depositing screen belt 20.
- Fig. 4 shows a spunbond device according to the invention with a spinneret 10 and thus with a spinning beam. It is also within the scope of the invention that a spunbond device according to the invention can be used in the context of a 2-beam system or a multi-beam system. According to one embodiment, several spunbond devices according to the invention can be used here one after the other.
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
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Description
Die Erfindung betrifft ein Spunbond-Vliesstoff aus Endlosfilamenten, insbesondere aus gekräuselten Endlosfilamenten, wobei die Filamente als Bikomponentenfilamente bzw. als Multikomponentenfilamente ausgebildet sind. Die Erfindung bezieht sich weiterhin auf eine Vorrichtung zur Erzeugung eines Spunbond-Vliesstoffes aus Endlosfilamenten, insbesondere aus gekräuselten Endlosfilamenten. Es liegt im Rahmen der Erfindung, dass es sich bei den Endlosfilamenten und Endlosfilamente aus thermoplastischem Kunststoff handelt. Endlosfilamente unterscheiden sich aufgrund ihrer quasi endlosen Länge von Stapelfasern, die viel geringere Längen von beispielsweise 10 mm bis 60 mm aufweisen.The invention relates to a spunbond nonwoven fabric made from continuous filaments, in particular from crimped continuous filaments, the filaments being designed as bicomponent filaments or as multicomponent filaments. The invention further relates to a device for producing a spunbond nonwoven fabric from continuous filaments, in particular from crimped continuous filaments. It is within the scope of the invention that the continuous filaments and continuous filaments are made of thermoplastic material. Because of their quasi-endless length, continuous filaments differ from staple fibers, which have much shorter lengths of, for example, 10 mm to 60 mm.
Für viele technische Anwendungen ist es wünschenswert, sogenannte High-Loft-Vliese herzustellen. Dabei handelt es sich um Vliesstoffe, die eine relativ große Dicke und zugleich eine relativ hohe Weichheit aufweisen. Die Erzeugung dieser Vliese ist aber nicht problemlos möglich, da die Vliese in der Regel zugleich eine ausreichende Festigkeit und Abriebsfestigkeit aufweisen müssen. Insoweit besteht ein Zielkonflikt. Die Einstellung einer höheren Festigkeit bzw. Abriebsfestigkeit geht normalerweise zu Lasten der Dicke und der Weichheit des Vliesstoffes. Umgekehrt führt eine Beibehaltung einer großen Dicke und einer hohen Weichheit in der Regel zu weniger festen und abriebsfesten Vliesstoffen. Befriedigende Lösungen sind hier bislang kaum bekannt. - Eine hohe Dicke von Vliesstoffen wird normalerweise mit Hilfe von kräuselnden bzw. crimpenden Fasern/Filamenten erzeugt. Dazu werden insbesondere Bikomponentenfilamente mit Seite-an-Seite-Konfiguration oder mit exzentrischer bzw. asymmetrischer Kern-Mantel-Konfiguration eingesetzt. Viele der bislang bekannten Vliesstoffe aus kräuselnden bzw. crimpenden Fasern zeichnen sich aber durch eine relativ hohe Defektrate aus. Insbesondere finden sich in den Vliesstoffen unerwünschte Agglomerate, die die Homogenität nachteilhaft beeinträchtigen. Auch insoweit besteht VerbesserungsbedarfFor many technical applications it is desirable to produce so-called high-loft nonwovens. These are nonwovens that are relatively thick and at the same time relatively soft. The production of these nonwovens is not possible without any problems, however, since the nonwovens generally have to have sufficient strength and abrasion resistance at the same time. To this extent, there is a conflict of objectives. The setting of a higher strength or abrasion resistance is normally at the expense of the thickness and the softness of the nonwoven fabric. Conversely, maintaining a large thickness and high softness usually leads to less strong and abrasion-resistant nonwovens. So far, there are hardly any known satisfactory solutions. - A high thickness of nonwovens is usually produced with the help of curling or crimping fibers / filaments. For this purpose, bicomponent filaments with a side-by-side configuration or with an eccentric or asymmetrical core-sheath configuration are used in particular. Many of the previously known nonwovens made from crimping or crimping However, fibers are characterized by a relatively high defect rate. In particular, undesired agglomerates are found in the nonwovens, which adversely affect the homogeneity. There is also a need for improvement in this regard
Der Erfindung liegt das technische Problem zugrunde, einen Vliesstoff anzugeben, der eine optimale Dicke und eine optimale Weichheit aufweist und zugleich eine ausreichende Festigkeit bzw. Zugfestigkeit sowie eine ausreichende Abriebsfestigkeit aufweist. Außerdem soll der Vliesstoff möglichst frei von Defekten und insbesondere möglichst frei von Agglomeraten sein. Der Erfindung liegt weiterhin das technische Problem zugrunde, eine Vorrichtung zur Herstellung eines solchen Vliesstoffes anzugeben.The invention is based on the technical problem of specifying a nonwoven fabric which has an optimal thickness and an optimal softness and at the same time has sufficient strength or tensile strength and sufficient abrasion resistance. In addition, the nonwoven should be as free as possible from defects and, in particular, as free as possible from agglomerates. The invention is also based on the technical problem of specifying a device for producing such a nonwoven fabric.
Zur Lösung des technischen Problems lehrt die Erfindung einen Spunbond-Vliesstoff aus Endlosfilamenten, insbesondere aus gekräuselten bzw. gecrimpten Endlosfilamenten, wobei die Filamente als Bikomponentenfilamente bzw. als Multikomponentenfilamente ausgebildet sind und eine exzentrische Kern-Mantel-Konfiguration aufweisen
und wobei der Mantel der Filamente im Filamentquerschnitt über zumindest 20 %, insbesondere über zumindest 25 %, vorzugsweise über zumindest 30 %, bevorzugt über zumindest 35 % und sehr bevorzugt über zumindest 40 % des Filamentumfanges eine konstante Dicke bzw. eine im Wesentlichen konstante Dicke aufweist und wobei die Dicke des Mantels im Bereich seiner konstanten bzw. im Wesentlichen konstanten Dicke d 0,1 bis 2 µm beträgt.To solve the technical problem, the invention teaches a spunbond nonwoven fabric made from continuous filaments, in particular from crimped or crimped continuous filaments, the filaments being designed as bicomponent filaments or as multicomponent filaments and having an eccentric core-sheath configuration
and wherein the sheath of the filaments in the filament cross-section has a constant thickness or an essentially constant thickness over at least 20%, in particular over at least 25%, preferably over at least 30%, preferably over at least 35% and very preferably over at least 40% of the filament circumference and wherein the thickness of the jacket in the region of its constant or substantially constant thickness d is 0.1 to 2 μm.
Es liegt im Rahmen der Erfindung, dass es sich bei der Dicke des Mantels der Filamente um die mittlere Dicke bzw. mittlere Manteldicke handelt, und zwar bevorzugt um die mittlere Manteldicke in Bezug auf ein Filament. Zweckmäßigerweise wird die Manteldicke bzw. werden die Manteldicken mit Hilfe eines Rasterelektronenmikroskopes gemessen. Weiterhin liegt es im Rahmen der Erfindung, dass die Manteldicke bzw. die mittlere Manteldicke an Filamenten bzw. Filamentabschnitten gemessen wird, die nicht in eine thermische Vorverfestigung bzw. Verfestigung involviert sind und somit insbesondere nicht Bestandteil von Bondingpunkten bzw. Bondingstellen sind. Mit anderen Worten erfolgt die Messung der Manteldicke an den Filamenten bzw. an den Filamentabschnitten außerhalb der Bondingpunkte bzw. Bondingstellen.It is within the scope of the invention that the thickness of the sheath of the filaments is the mean thickness or mean sheath thickness, specifically preferably the mean sheath thickness in relation to a filament. The jacket thickness or the jacket thicknesses are expediently with Measured using a scanning electron microscope. Furthermore, it is within the scope of the invention that the jacket thickness or the mean jacket thickness is measured on filaments or filament sections that are not involved in a thermal pre-consolidation or consolidation and are therefore in particular not part of bonding points or bonding points. In other words, the sheath thickness is measured on the filaments or on the filament sections outside the bonding points or bonding points.
Außerdem liegt es im Rahmen der Erfindung, dass die Endlosfilamente des Vliesstoffes aus thermoplastischem Kunststoff bestehen bzw. im Wesentlichen bestehen. Gekräuselte Endlosfilamente meint im Rahmen der Erfindung insbesondere, dass die gekräuselten Filamente jeweils einen Kräuselung mit mindestens 1,5, vorzugsweise mit mindestens 2, bevorzugt mit mindestens 2,5 und sehr bevorzugt mit mindestens 3 Schlingen (loops) pro Zentimeter ihrer Länge aufweisen. Eine empfohlene Ausführungsform der Erfindung zeichnet sich dadurch aus, dass die Endlosfilamente des erfindungsgemäßen Spunbond-Vliesstoffes eine Kräuselung von 1,8 bis 3,2, insbesondere 2 bis 3 Schlingen (loops) pro Zentimeter ihrer Länge aufweisen. Die Anzahl der Kräuselschlingen bzw. Kräuselbögen (loops) pro Zentimeter Länge der Filamente wird dabei insbesondere nach der japanischen Norm JIS L-1015-1981 gemessen, indem die Kräuselungen unter einer Vorspannung von 2 mg/den in (1/10 mm) gezählt werden, wobei die nicht ausgestreckte Länge der Filamente zugrunde liegt. Es wird eine Empfindlichkeit von 0,05 mm verwendet, um die Anzahl der Kräuselschlingen zu bestimmen. Die Messung wird zweckmäßigerweise durchgeführt mit einem "Favimat"-Gerät der Firma TexTechno, Deutschland. Dazu wird auf die Veröffentlichung "Automatic Crimp Measurement on Staple Fibres", Denkendorf Kolloquium", "Textile Mess- und Prüftechnik", 9.11.99, Dr. Ulrich Mörschel (insbesondere S. 4,
Die Filamente (bzw. die Filamentprobe) werden/wird hierzu als Filamentknäuel vor einer weiteren Verfestigung von der Ablage bzw. vom Ablageband abgenommen und die Filamente werden vereinzelt und gemessen.For this purpose, the filaments (or the filament sample) are / is removed from the deposit or from the deposit belt as a filament ball before further solidification and the filaments are separated and measured.
Erfindungsgemäß werden für den Spunbond-Vliesstoff Bikomponentenfilamente bzw. Multikomponentenfilamente mit exzentrischer Kern-Mantel-Konfiguration eingesetzt. Es liegt dabei im Rahmen der Erfindung, dass der Mantel der Filamente den Kern vollständig umgibt. Weiterhin liegt es im Rahmen der Erfindung, dass das Material bzw. der Kunststoff des Mantels einen geringeren Schmelzpunkt aufweist als das Material bzw. der Kunststoff des Kerns der Filamente.According to the invention, bicomponent filaments or multicomponent filaments with an eccentric core-sheath configuration are used for the spunbond nonwoven fabric. It is within the scope of the invention that the sheath of the filaments completely surrounds the core. Furthermore, it is within the scope of the invention that the material or the plastic of the jacket has a lower melting point than the material or the plastic of the core of the filaments.
Der Erfindung liegt die Erkenntnis zugrunde, dass bei dem erfindungsgemäßen Spunbond-Vliesstoff problemlos eine große Dicke sowie eine hohe Weichheit und nichtsdestoweniger eine ausreichende Festigkeit und Abriebsfestigkeit erzielt werden kann. Festigkeit meint im Rahmen der Erfindung insbesondere die Festigkeit des Vliesstoffes in Maschinenrichtung (MD). Bei dem erfindungsgemäßen Vliesstoff kann eine völlig zufriedenstellende Festigkeit ohne nennenswerten Dickenverlust realisiert werden. Der Erfindung liegt dabei weiterhin die Erkenntnis zugrunde, dass aufgrund der erfindungsgemäßen Querschnittsstruktur der Filamente eine optimale Kräuselung erzielt werden kann und vor allem durch Variierung der Parameter auch einfach eingestellt werden kann - wodurch die gewünschte Dicke und die gewünschte Weichheit erreicht wird - und zugleich das über den gesamten Filamentumfang umlaufende Mantelmaterial effektiv für eine thermische Vorverfestigung eingesetzt werden kann. Bei dieser thermischen Vorverfestigung werden mit Hilfe des niedrigerschmelzenden Mantelmaterials der Filamente Bondingpunkte zwischen den Filamenten hergestellt und diese bedingen bei dem erfindungsgemäßen Vliesstoff mit den erfindungsgemäßen Filamenteigenschaften eine optimale Festigkeit und Abriebsfestigkeit des Vliesstoffes wobei nichtsdestoweniger eine ausreichende Dicke und Weichheit erhalten bleiben kann. Zu betonen ist weiterhin, dass die erfindungsgemäßen Vliesstoffe überraschend defektfrei ausgebildet werden können und dabei vor allem weitgehend frei von störenden Agglomeraten sind. Im Ergebnis kann eine sehr homogene Faserlage bzw. Vliesstoffablage erzielt werden.The invention is based on the knowledge that with the spunbond nonwoven fabric according to the invention, a great thickness and a high softness and nevertheless sufficient strength and abrasion resistance can be achieved without any problems. In the context of the invention, strength means, in particular, the strength of the nonwoven in the machine direction (MD). With the nonwoven fabric according to the invention, a completely satisfactory strength can be achieved without any appreciable loss of thickness. The invention is further based on the knowledge that due to the cross-sectional structure of the filaments according to the invention, an optimal crimp can be achieved and, above all, can also be easily adjusted by varying the parameters - whereby the desired thickness and the desired softness is achieved - and at the same time that via Sheath material encircling the entire filament circumference can be used effectively for thermal pre-consolidation. During this thermal pre-consolidation, bonding points are produced between the filaments with the aid of the lower-melting sheath material of the filaments, and these bond points in the nonwoven fabric according to the invention with the filament properties according to the invention an optimal strength and abrasion resistance of the nonwoven fabric while still maintaining sufficient thickness and softness. It should also be emphasized that the nonwovens according to the invention can be formed surprisingly free of defects and, above all, are largely free of troublesome agglomerates. As a result, a very homogeneous fiber layer or nonwoven layer can be achieved.
Empfohlenermaßen weist ein erfindungsgemäßer Vliesstoff eine Dicke von mehr als 0,5 mm, insbesondere von mehr als 0,55 mm und vorzugsweise eine Dicke von mehr als 0,6 mm auf. Es liegt im Rahmen der Erfindung, dass die erfindungsgemäßen Vliesstoffe eine Festigkeit in Maschinenrichtung (MD) von mehr als 20 N/5 cm, insbesondere von mehr als 25 N/5 cm aufweisen. Die vorstehenden Dicken- und Festigkeitswerte gelten insbesondere für Vliesstoffe mit einem Flächengewicht von 10 bis 50 g/m2, vorzugsweise mit einem Flächengewicht von 15 bis 40 g/m2 und bevorzugt mit einem Flächengewicht von 18 bis 35 g/m2.A nonwoven fabric according to the invention is recommended to have a thickness of more than 0.5 mm, in particular of more than 0.55 mm and preferably a thickness of more than 0.6 mm. It is within the scope of the invention that the nonwovens according to the invention have a strength in the machine direction (MD) of more than 20 N / 5 cm, in particular of more than 25 N / 5 cm. The above thickness and strength values apply in particular to nonwovens with a basis weight of 10 to 50 g / m 2 , preferably with a basis weight of 15 to 40 g / m 2 and preferably with a basis weight of 18 to 35 g / m 2 .
Es liegt weiterhin im Rahmen der Erfindung, dass der Kern der Filamente mehr als 40 %, insbesondere mehr als 50 %, vorzugsweise mehr als 60 %, bevorzugt mehr als 65 % und sehr bevorzugt mehr als 70 % der Fläche des Filamentquerschnittes der Filamente einnimmt. Nach einer Ausführungsform der Erfindung nimmt der Kern der Filamente mehr als 75 % der Fläche des Filamentquerschnittes der Filamente ein.It is also within the scope of the invention that the core of the filaments takes up more than 40%, in particular more than 50%, preferably more than 60%, preferably more than 65% and very preferably more than 70% of the area of the filament cross-section of the filaments. According to one embodiment of the invention, the core of the filaments takes up more than 75% of the area of the filament cross-section of the filaments.
Es empfiehlt sich, dass der Kern der Filamente im Filamentquerschnitt gesehen kreissegmentförmig ausgebildet ist und vorzugsweise bezüglich seines Umfanges zumindest einen, insbesondere einen kreisbogenförmigen Umfangsabschnitt bzw. im Wesentlichen kreisbogenförmigen Umfangsabschnitt aufweist. Empfohlenermaßen weist der Kern der Filamente im Filamentquerschnitt gesehen zusätzlich zumindest einen, insbesondere einen linearen bzw. im Wesentlichen linearen Umfangsabschnitt auf. Gemäß besonders bevorzugter Ausführungsform der Erfindung besteht der Kern der Filamente im Filamentquerschnitt gesehen aus einem kreisbogenförmigen bzw. im Wesentlichen kreisbogenförmigen Umfangsabschnitt und einem - zweckmäßigerweise unmittelbar daran anschließenden - linearen bzw. im Wesentlichen linearen Umfangsabschnitt. Eine bewährte Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass der kreisbogenförmige bzw. im Wesentlichen kreisbogenförmige Umfangsabschnitt des Kerns über 40 %, insbesondere über 50 %, vorzugsweise über 60 % und bevorzugt über 65 % des Umfanges des Kerns einnimmt.It is recommended that the core of the filaments is designed in the shape of a segment of a circle when viewed in the filament cross-section and preferably has at least one, in particular a circular arc-shaped circumferential section or substantially circular arc-shaped circumferential section with regard to its circumference. The core of the filaments is recommended to have the Viewed filament cross-section, additionally at least one, in particular a linear or essentially linear, circumferential section. According to a particularly preferred embodiment of the invention, the core of the filaments, viewed in the filament cross section, consists of an arcuate or essentially arcuate circumferential section and a linear or essentially linear circumferential section - expediently directly adjoining it. A proven embodiment of the invention is characterized in that the circular arc-shaped or essentially circular arc-shaped circumferential section of the core takes up over 40%, in particular over 50%, preferably over 60% and preferably over 65% of the circumference of the core.
Eine empfohlene Ausführungsform zeichnet sich dadurch aus, dass der Mantel der Filamente - im Filamentquerschnitt gesehen - außerhalb des Mantelbereiches mit der konstanten bzw. im Wesentlichen konstanten Dicke kreissegmentförmig bzw. im Wesentlichen kreissegmentförmig ausgebildet ist. Dabei weist dieses Kreissegment zweckmäßigerweise bezüglich seines Umfanges zumindest einen, insbesondere einen kreisbogenförmigen bzw. im Wesentlichen kreisbogenförmigen Umfangsabschnitt auf sowie vorzugsweise zumindest einen, insbesondere einen linearen bzw. im Wesentlichen linearen Umfangsabschnitt auf. Bevorzugt besteht der kreissegmentförmige Mantelabschnitt aus einem kreisbogenförmigen bzw. im Wesentlichen kreisbogenförmigen Umfangsabschnitt und aus einem - zweckmäßigerweise unmittelbar daran anschließenden - linearen bzw. im Wesentlichen linearen Umfangsabschnitt.A recommended embodiment is characterized in that the sheath of the filaments - viewed in the filament cross-section - outside the sheath area with the constant or essentially constant thickness is formed in the shape of a segment of a circle or essentially in the shape of a segment of a circle. This circular segment expediently has at least one, in particular a circular arc-shaped or essentially circular arc-shaped, circumferential section and preferably at least one, in particular a linear or essentially linear, circumferential section with regard to its circumference. The jacket section in the form of a segment of a circle preferably consists of a circular arc-shaped or essentially circular arc-shaped circumferential section and a linear or essentially linear circumferential section — expediently directly adjoining it.
Es liegt im Rahmen der Erfindung, dass der Mantel der Filamente - im Filamentquerschnitt gesehen - über 45 %, insbesondere über 50 %, vorzugsweise über 55 % und bevorzugt über 60 % des Filamentumfanges eine konstante Dicke bzw. eine im Wesentlichen konstante Dicke aufweist. Gemäß bevorzugter Ausführungsform der Erfindung beträgt die Dicke des Mantels im Bereich seiner konstanten bzw. im Wesentlichen konstanten Dicke weniger als 10%, insbesondere weniger als 8%, vorzugsweise weniger als 7% und bevorzugt weniger als 3 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers. Zweckmäßigerweise beträgt die Dicke des Mantels im Bereich seiner konstanten bzw. im Wesentlichen konstanten Dicke mindestens 0,5 %, insbesondere mindestens 1 % und bevorzugt mindestens 1,2 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers. - Vorzugsweise wird die Spinndüse zur Erzeugung der Filamente mit der Maßgabe gewählt bzw. eingerichtet, dass die die Spinndüse verlassenden Filamente im noch nicht verstreckten Zustand die vorstehend und nachfolgend angegebenen relativen Dickenwerte bzw. prozentualen Dickenwerte für den Mantel aufweisen. Es liegt aber auch im Rahmen der Erfindung, dass diese relativen Dickenwerte ebenso für den Mantel der Filamente in dem fertigen Spunbond-Vliesstoff zutreffen.It is within the scope of the invention that the sheath of the filaments - seen in the filament cross section - over 45%, in particular over 50%, preferably over 55% and preferably over 60% of the filament circumference having a constant thickness or a substantially constant thickness. According to a preferred embodiment of the invention, the thickness of the jacket in the region of its constant or essentially constant thickness is less than 10%, in particular less than 8%, preferably less than 7% and preferably less than 3% of the filament diameter or the largest filament diameter. The thickness of the jacket in the region of its constant or essentially constant thickness is expediently at least 0.5%, in particular at least 1% and preferably at least 1.2% of the filament diameter or the largest filament diameter. The spinneret for producing the filaments is preferably selected or set up with the proviso that the filaments leaving the spinneret have the relative thickness values or percentage thickness values for the jacket given above and below in the not yet drawn state. However, it is also within the scope of the invention that these relative thickness values also apply to the sheath of the filaments in the finished spunbond nonwoven fabric.
Nach empfohlener Ausführungsform der Erfindung beträgt die Dicke des Mantels im Bereich seiner konstanten bzw. im Wesentlichen konstanten Dicke bei dem fertigen Spunbond-Vliestoff 0,15 bis 1,5 µm und insbesondere 0,1 bis 0,9 µm.According to a recommended embodiment of the invention, the thickness of the jacket in the region of its constant or essentially constant thickness in the finished spunbond nonwoven material is 0.15 to 1.5 μm and in particular 0.1 to 0.9 μm.
Es empfiehlt sich, dass das Verhältnis der Masse des Kerns zur Masse des Mantels in den Filamenten des erfindungsgemäßen Spunbond-Vliesstoffes 90:10 bis 40:60, vorzugsweise 90:10 bis 60:40 und bevorzugt 85:15 bis 70:30 beträgt. - Eine besonders empfohlene Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass bezüglich des Filamentquerschnittes der Abstand a des Flächenschwerpunktes des Kerns von dem Flächenschwerpunkt des Mantels 5 % bis 38 %, insbesondere 6 % bis 36 % und vorzugsweise 6 % bis 34 %, bevorzugt 7 % bis 33 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers beträgt. Weiterhin ist eine sehr bevorzugte Ausführungsform der Erfindung dadurch gekennzeichnet, dass bezüglich des Filamentquerschnittes der Abstand a der Flächenschwerpunkte von Kern und Mantel bei einem Massenverhältnis Kern:Mantel von 85:15 bis 70:30 zwischen 5 % und 36 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers beträgt. Vorzugsweise beträgt bei einem Massenverhältnis Kern:Mantel von 70:30 bis 60:40 der Abstand a der Flächenschwerpunkte zwischen 12 % und 40 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers. Empfohlenermaßen beträgt bei einem Massenverhältnis Kern:Mantel von 60:40 bis 45:55 der Abstand a der Flächenschwerpunkte von Kern und Mantel zwischen 18 % und 36 %, insbesondere zwischen 20 % und 31 % des Filamentdurchmessers bzw. des größten Filamentdurchmessers.It is recommended that the ratio of the mass of the core to the mass of the sheath in the filaments of the spunbond nonwoven fabric according to the invention is 90:10 to 40:60, preferably 90:10 to 60:40 and preferably 85:15 to 70:30. A particularly recommended embodiment of the invention is characterized in that, with regard to the filament cross section, the distance a of the centroid of the core from the centroid of the sheath is 5% to 38%, in particular 6% to 36% and preferably 6% to 34%, preferably 7% to 33% of the filament diameter or the largest filament diameter. Furthermore, a very preferred embodiment of the invention is characterized in that, with regard to the filament cross-section, the distance a of the centroids of the core and sheath with a core: sheath mass ratio of 85:15 to 70:30 is between 5% and 36% of the filament diameter or the largest Filament diameter is. With a core: sheath mass ratio of 70:30 to 60:40, the distance a between the centroids is preferably between 12% and 40% of the filament diameter or the largest filament diameter. With a core: sheath mass ratio of 60:40 to 45:55, the distance a between the centers of area of the core and sheath is recommended between 18% and 36%, in particular between 20% and 31% of the filament diameter or the largest filament diameter.
Eine besonders empfohlene Ausführungsform der Erfindung zeichnet sich dadurch aus, dass der Kern und/oder der Mantel der Filamente aus zumindest einem Polyolefin besteht bzw. im Wesentlichen besteht. Dass der Kern und/oder der Mantel "im Wesentlichen" aus einem Kunststoff beispielsweise besteht, meint im Rahmen der Erfindung insbesondere, dass außer diesem Kunststoff auch noch Additive in dem Kern und/oder dem Mantel vorhanden. "Im Wesentlichen besteht" meint im Rahmen der Erfindung vor allem, dass der Kern und/oder der Mantel mindestens 90 Gew.-%, vorzugsweise mindestens 95 Gew.-% und bevorzugt mindestens 97 Gew.-% des jeweiligen Kunststoffes aufweist. - Nach einer empfohlenen Ausführungsform der Erfindung besteht sowohl der Kern als auch der Mantel der Filamente jeweils aus zumindest einem Polyolefin, insbesondere aus einem Polyolefin bzw. im Wesentlichen aus zumindest einem Polyolefin, insbesondere im Wesentlichen aus einem Polyolefin. Eine ganz besonders bevorzugte Ausführungsform der Erfindung zeichnet sich dadurch aus, dass der Mantel der Filamente aus Polyethylen besteht bzw. im Wesentlichen besteht und dass der Kern der Filamente aus Polypropylen bzw. im Wesentlichen aus Polypropylen besteht. - Es wurde bereits weiter oben ausgeführt, dass es im Rahmen der Erfindung liegt, dass der Mantel der Filamente im Vergleich zu dem Kern der Filamente aus dem niedrigerschmelzenden Material bzw. Kunststoff besteht bzw. im Wesentlichen besteht. - Grundsätzlich können im Rahmen der Erfindung auch Copolymere der vorgenannten Polyolefine eingesetzt werden, und zwar entweder allein im Kern und/oder im Mantel oder in einer Mischung mit zumindest einem Homo-Polyolefin. Weiterhin können auch Mischungen von Homo-Polyolefinen für den Kern und/oder für den Mantel verwendet werden. Es sind auch Mischungen mit anderen Kunststoffen möglich.A particularly recommended embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists or essentially consists of at least one polyolefin. The fact that the core and / or the jacket "essentially" consists of a plastic, for example, means in the context of the invention in particular that, in addition to this plastic, additives are also present in the core and / or the jacket. In the context of the invention, “essentially consists” primarily means that the core and / or the jacket comprises at least 90% by weight, preferably at least 95% by weight and preferably at least 97% by weight of the respective plastic. According to a recommended embodiment of the invention, both the core and the sheath of the filaments each consist of at least one polyolefin, in particular of a polyolefin or essentially of at least one polyolefin, in particular essentially of one Polyolefin. A very particularly preferred embodiment of the invention is characterized in that the sheath of the filaments consists or essentially consists of polyethylene and that the core of the filaments consists of polypropylene or essentially consists of polypropylene. It has already been stated above that it is within the scope of the invention that the sheath of the filaments consists or essentially consists of the lower-melting material or plastic compared to the core of the filaments. In principle, copolymers of the aforementioned polyolefins can also be used in the context of the invention, either alone in the core and / or in the shell or in a mixture with at least one homopolyolefin. Mixtures of homopolyolefins can also be used for the core and / or for the shell. Mixtures with other plastics are also possible.
Wenn im Rahmen der Erfindung Polypropylen eingesetzt wird bzw. Polypropylen für den Kern eingesetzt, handelt es sich vorzugsweise um ein Polypropylen mit einer Schmelzflussrate von mehr als 25 g/10 min, insbesondere mehr als 40 g/10 min, vorzugsweise von mehr als 50 g/10 min, bevorzugt von mehr als 55 g/10 min und sehr bevorzugt von mehr als 60 g/10 min. Dabei wird die Schmelzflussrate (MFR) insbesondere nach ASTM D1238-13 gemessen (Bedingung B, 2,16 kg, 230°C). Wenn im Rahmen der Erfindung Polyethylen als Komponente verwendet wird, insbesondere als Komponente für den Mantel verwendet wird, handelt es sich zweckmäßigerweise um ein Polyethylen mit einer Schmelzflussrate unter 35 g/10 min, insbesondere unter 25 g/10 min, bevorzugt unter 20 g/10 min. Für Polyethylen wird die Schmelzflussrate insbesondere nach ASTM D1238-13 bei 190°C/2,16kg gemessen.If, in the context of the invention, polypropylene is used or polypropylene is used for the core, it is preferably a polypropylene with a melt flow rate of more than 25 g / 10 min, in particular more than 40 g / 10 min, preferably more than 50 g / 10 min, preferably more than 55 g / 10 min and very preferably more than 60 g / 10 min. The melt flow rate (MFR) is measured in particular according to ASTM D1238-13 (condition B, 2.16 kg, 230 ° C). If, in the context of the invention, polyethylene is used as a component, in particular as a component for the jacket, it is expediently a polyethylene with a melt flow rate below 35 g / 10 min, in particular below 25 g / 10 min, preferably below 20 g / 10 min For polyethylene, the melt flow rate is measured in particular according to ASTM D1238-13 at 190 ° C. / 2.16 kg.
Eine Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass der Kern und/oder der Mantel der Filamente aus zumindest einem Polyester und/oder aus zumindest einem Copolyester besteht bzw. im Wesentlichen besteht. Eine empfohlene Ausführungsform zeichnet sich dabei dadurch aus, dass der Kern der Filamente aus zumindest einem Polyester, insbesondere aus einem Polyester besteht bzw. im Wesentlichen besteht und dass vorzugsweise der Mantel aus zumindest einem, insbesondere aus einem gegenüber der Kernkomponente niedrigerschmelzenden Polyester und/oder Copolyester besteht bzw. im Wesentlichen besteht. Es ist auch möglich, dass der Kern aus zumindest einem Polyester und/oder aus zumindest einem Copolyester besteht bzw. im Wesentlichen besteht und dass der Mantel aus zumindest einem Polyolefin besteht bzw. im Wesentlichen besteht. - Als Polyester eignet sich insbesondere Polyethylenterephthalat (PET) und als Polyester-Copolymer insbesondere PET-Copolymer (Co-PET). Als Polyester kann aber auch Polybutylenterephthalat (PBT) oder Polylactid (PLA) eingesetzt werden oder Copolymere dieser Polyester. Es liegt im Übrigen im Rahmen der Erfindung, dass für den Kern und/oder für den Mantel der Filamente auch Mischungen bzw. Blends von Polymeren bzw. der genannten Polymere eingesetzt werden können. Eine bewährte Ausführungsform der Erfindung zeichnet sich dadurch aus, dass der Kern und/oder der Mantel der Filamente aus zumindest einem Kunststoff aus der Gruppe "Polyolefin, Polyolefin-Copolymer, insbesondere Polyethylen, Polypropylen, Polyethylen-Copolymer, Polypropylen-Copolymer; Polyester, Polyester-Copolymer, insbesondere Polyethylenterephthalat (PET), PET-Copolymer, Polybutylenterephthalat (PBT), PBT-Copolymer, Polylactid (PLA), PLA-Copolymer" besteht bzw. im Wesentlichen besteht. Für Kern und/oder Mantel können auch Mischungen bzw. Blends der vorgenannten Polymere eingesetzt werden. Es liegt dabei im Rahmen der Erfindung, dass der Kunststoff des Mantels einen geringeren Schmelzpunkt aufweist als der Kunststoff des Kerns. Eine empfohlene Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass der Kern der Filamente aus zumindest einem Kunststoff aus der Gruppe "Polypropylen, Polypropylen-Copolymer, Polyethylenterephthalat (PET), PET-Copolymer, Polybutylenterephthalat (PBT), PBT-Copolymer, Polylactid (PLA), PLA-Copolymer" besteht bzw. im Wesentlichen besteht. Der Mantel der Filamente besteht nach bevorzugter Ausführungsform aus zumindest einem Kunststoff aus der Gruppe "Polyethylen, Polyethylen-Copolymer, Polypropylen, Polypropylen-Copolymer".One embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists or essentially consists of at least one polyester and / or of at least one copolyester. A recommended embodiment is characterized in that the core of the filaments consists or essentially consists of at least one polyester, in particular a polyester, and that the sheath preferably consists of at least one, in particular a polyester and / or copolyester with a lower melting point than the core component exists or essentially exists. It is also possible that the core consists or substantially consists of at least one polyester and / or of at least one copolyester and that the jacket consists or substantially consists of at least one polyolefin. - Polyethylene terephthalate (PET) is particularly suitable as the polyester and PET copolymer (Co-PET) is particularly suitable as the polyester copolymer. However, polybutylene terephthalate (PBT) or polylactide (PLA) or copolymers of these polyesters can also be used as polyester. It is moreover within the scope of the invention that mixtures or blends of polymers or the polymers mentioned can also be used for the core and / or for the sheath of the filaments. A proven embodiment of the invention is characterized in that the core and / or the sheath of the filaments consists of at least one plastic from the group "polyolefin, polyolefin copolymer, in particular polyethylene, polypropylene, polyethylene copolymer, polypropylene copolymer; polyester, polyester -Copolymer, in particular polyethylene terephthalate (PET), PET copolymer, polybutylene terephthalate (PBT), PBT copolymer, polylactide (PLA), PLA copolymer "consists or essentially consists. Mixtures or blends of the aforementioned polymers can also be used for the core and / or shell. It is within the scope of the invention that the plastic of the jacket has a lower melting point than the plastic of the core. A recommended embodiment of the invention is characterized in that the core of the filaments consists of at least one plastic from the group "polypropylene, polypropylene copolymer, polyethylene terephthalate (PET), PET copolymer, polybutylene terephthalate (PBT), PBT copolymer, polylactide (PLA), PLA copolymer" or essentially consists. According to a preferred embodiment, the sheath of the filaments consists of at least one plastic from the group "polyethylene, polyethylene copolymer, polypropylene, polypropylene copolymer".
Es liegt im Rahmen der Erfindung, dass der Titer der für den erfindungsgemäßen Spunbond-Vliesstoff eingesetzten Filamente zwischen 1 und 12 den liegt. Gemäß einer empfohlenen Ausführungsform liegt der Titer der Filamente zwischen 1,0 und 2,5 den, insbesondere zwischen 1,5 und 2,2 den liegt und bevorzugt zwischen 1,8 und 2,2 den. Dieser Titer bzw. dieser Filamentdurchmesser hat sich im Hinblick auf die Lösung des erfindungsgemäßen technischen Problems besonders bewährt.It is within the scope of the invention that the titer of the filaments used for the spunbond nonwoven fabric according to the invention is between 1 and 12 den. According to a recommended embodiment, the titer of the filaments is between 1.0 and 2.5 den, in particular between 1.5 and 2.2 den, and preferably between 1.8 and 2.2 den. This titer or this filament diameter has proven particularly useful in terms of solving the technical problem according to the invention.
Eine sehr bewährte Ausführungsform ist dadurch gekennzeichnet, dass der erfindungsgemäße Spunbond-Vliesstoff ein thermisch vorverfestigter und/oder thermisch endverfestigter Vliesstoff ist, der thermische Bondingstellen bzw. thermische Bondingpunkte zwischen den Filamenten aufweist. Gemäß einer sehr bevorzugten Ausführungsform handelt es sich bei dem erfindungsgemäßen Spunbond-Vliesstoff um einen mit Heißluft thermisch vorverfestigten Vliesstoff und/oder thermisch endverfestigten Vliesstoff. Die thermische Vorverfestigung des Vliesstoffes kann grundsätzlich auch durch Kompaktierwalzen erfolgen. Es liegt auch im Rahmen der Erfindung, dass eine thermische Vorverfestigung bzw. Verfestigung des Vliesstoffes mit Hilfe eines Kalanders durchgeführt wird. - Der Erfindung liegt die Erkenntnis zugrunde, dass bei der erfindungsgemäßen Ausgestaltung der Querschnitte der Filamente eine optimale Vorverfestigung bzw. thermische Vorverfestigung der Spinnvliese möglich ist und nichtsdestoweniger eine ausreichende Kräuselung und somit die gewünschte Dicke des Vliesstoffes aufrechterhalten werden kann. Insoweit ist ein optimaler Kompromiss zwischen einer ausreichenden Kräuselung und somit einer ausreichenden Dicke einerseits und einer optimalen Verfestigung der Vliesstoffe möglich. Die Kräuselung kann durch Variierung der Querschnittsparameter der Filamente gezielt eingestellt werden und dabei kann auch problemlos darauf geachtet werden, dass die Kräuselung kein zu großes Ausmaß annimmt und dass vielmehr die gewünscht Dicke präzise und funktionssicher erzeugt werden kann und zusätzlich ohne großen Dickenverlust eine effektive Vorverfestigung des Vliesstoffes durchgeführt werden kann.A well-proven embodiment is characterized in that the spunbond nonwoven according to the invention is a thermally pre-bonded and / or thermally bonded nonwoven which has thermal bonding points or thermal bonding points between the filaments. According to a very preferred embodiment, the spunbond nonwoven according to the invention is a nonwoven thermally pre-bonded with hot air and / or thermally bonded nonwoven. The thermal pre-consolidation of the nonwoven fabric can in principle also be carried out by compacting rollers. It is also within the scope of the invention that a thermal pre-consolidation or consolidation of the nonwoven fabric is carried out with the aid of a calender. The invention is based on the knowledge that in the configuration according to the invention of the cross-sections of the filaments, an optimal pre-consolidation or thermal pre-consolidation of the spunbonded nonwovens is possible and nevertheless sufficient crimp and thus the desired thickness of the nonwoven fabric can be maintained. In this respect, an optimal compromise between sufficient crimp and thus sufficient thickness on the one hand and optimal consolidation of the nonwovens is possible. The crimp can be set in a targeted manner by varying the cross-sectional parameters of the filaments and it is also easy to ensure that the crimp does not become too large and that the desired thickness can be created precisely and functionally and, in addition, an effective pre-consolidation of the Nonwoven fabric can be carried out.
Zur Lösung des technischen Problems lehrt die Erfindung weiterhin eine Vorrichtung zur Erzeugung eines Spunbond-Vliesstoffes aus Endlosfilamenten, insbesondere aus gekräuselten Endlosfilamenten, wobei zumindest eine Spinndüse vorhanden ist, wobei die Vorrichtung bzw. die Spinndüse mit der Maßgabe eingerichtet ist, dass Multikomponentenfilamente bzw. Bikomponentenfilamente mit exzentrischer Kern-Mantel-Konfiguration erzeugt werden, wobei der Mantel der Filamente im Filamentquerschnitt gesehen über zumindest 20 %, insbesondere über zumindest 25 %, vorzugsweise über zumindest 30 %, bevorzugt über zumindest 35 % und sehr bevorzugt über zumindest 40 % des Filamentumfanges eine konstante Dicke bzw. eine im Wesentlichen konstante Dicke aufweist, wobei die Dicke des Mantels im Bereich seiner konstanten bzw. im Wesentlichen konstanten Dicke d 0,1 bis 2 µm beträgt und wobei die Filamente auf einer Ablagevorrichtung, insbesondere auf einem Ablagesiebband abgelegt werden. Es liegt im Rahmen der Erfindung, dass es sich bei der Vorrichtung um eine Spunbond-Vorrichtung handelt. Empfohlenermaßen weist die Vorrichtung eine Kühlvorrichtung zum Kühlen der Filamente sowie eine daran anschließende Verstreckeinrichtung zum Verstrecken der Filamente auf. Vorzugsweise ist die Vorrichtung fernerhin mit zumindest einem an die Verstreckeinrichtung anschließenden Diffusor ausgestattet. - Eine besonders bevorzugte Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass das Aggregat aus der Kühlvorrichtung und der Verstreckeinrichtung als geschlossenes Aggregat ausgebildet ist und dass außer der Zufuhr von Kühlluft in der Kühlvorrichtung keine weitere Luftzufuhr von außen in dieses Aggregat stattfindet.To solve the technical problem, the invention also teaches a device for producing a spunbond nonwoven fabric from continuous filaments, in particular from crimped continuous filaments, with at least one spinneret being present, the device or the spinneret being set up with the proviso that multicomponent filaments or bicomponent filaments with an eccentric core-sheath configuration, the sheath of the filaments seen in the filament cross-section over at least 20%, in particular over at least 25%, preferably over at least 30%, preferably over at least 35% and very preferably over at least 40% of the filament circumference has a constant thickness or a substantially constant thickness, the thickness of the jacket in the region of its constant or substantially constant thickness d being 0.1 to 2 μm and the filaments being deposited on a depositing device, in particular on a depositing screen belt. It is within the scope of the invention that the device is a spunbond device. It is recommended that the device has a cooling device for cooling the filaments and a stretching device connected to it for stretching the filaments. Furthermore, the device is preferably equipped with at least one diffuser connected to the stretching device. - A particularly preferred one Embodiment of the invention is characterized in that the unit from the cooling device and the stretching device is designed as a closed unit and that apart from the supply of cooling air in the cooling device, no further air supply takes place from the outside into this unit.
Es liegt im Rahmen der Erfindung, dass nach der Ablage der Endlosfilamente auf der Ablagevorrichtung bzw. auf dem Ablagesiebband eine thermische Vorverfestigung der Faserablage bzw. der Vliesbahn durchführbar ist. Dazu ist nach empfohlener Ausführungsform der Erfindung zumindest eine thermische Vorverfestigungseinrichtungs vorgesehen. Eine empfohlene Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass die zumindest eine thermische Vorverfestigungseinrichtung als Heißluft-Vorverfestigungseinrichtung ausgebildet ist. Dabei weist zweckmäßigerweise die thermische Vorverfestigungseinrichtung zumindest ein Heißluftmesser auf und/oder zumindest einen Heißluftofen auf. Nach einer anderen Ausführungsform der Erfindung kann im Rahmen der Erfindung eine thermische Vorverfestigung bzw. Verfestigung auch mit Andrückwalzen bzw. Kompaktierwalzen durchgeführt werden und/oder es kann zur Vorverfestigung bzw. Verfestigung zumindest ein Kalander eingesetzt werden. Nach einer empfohlenen Ausführungsform der erfindungsgemäßen Vorrichtung erfolgt zunächst eine thermische Vorverfestigung der abgelegten Vliesbahn mit Hilfe zumindest eines Heißluftmessers, insbesondere mit Hilfe eines Heißluftmessers und erfolgt anschließend eine weitere thermische Vorverfestigung mit Hilfe zumindest eines Heißluftofens, insbesondere mit Hilfe eines Heißluftofens. Eine bevorzugte Ausführungsform der Erfindung ist dadurch gekennzeichnet, dass der Spunbond-Vliesstoff lediglich mit Heißluft vorverfestigt ist und/oder lediglich mit Heißluft endverfestigt ist. - Der Erfindung liegt die Erkenntnis zugrunde, dass aufgrund des erfindungsgemäßen Filamentquerschnittes einerseits der gesamte Filamentumfang für eine thermische Vorverfestigung zur Verfügung steht und andererseits durch gezielte Wahl der Parameter - insbesondere der Dicke des Mantels- die thermische Vorverfestigung bzw. das Ausmaß der thermischen Vorverfestigung gezielt beeinflusst werden kann, sodass zum einen eine optimale Verfestigung des Vliesstoffes erzielt werden kann und zum anderen nichtsdestoweniger die Kräuselung der Filamente dabei nicht zu sehr beeinträchtigt wird, um eine gewünschte Dicke des Vliesstoffes aufrechtzuerhalten. Im Rahmen der Erfindung ist insbesondere aufgrund des erfindungsgemäßen Filamentquerschnittes eine sehr einfache und gezielte Einstellung der Vliesstoffeigenschaften - insbesondere im Hinblick auf Dicke, Weichheit und Festigkeit - möglich. Vor allem ist mit der Erfindung die Kräuselung problemlos einstellbar und somit beherrschbar.It is within the scope of the invention that after the filaments have been deposited on the depositing device or on the depositing screen, a thermal pre-consolidation of the fiber deposit or the nonwoven web can be carried out. For this purpose, according to the recommended embodiment of the invention, at least one thermal pre-consolidation device is provided. A recommended embodiment of the invention is characterized in that the at least one thermal pre-consolidation device is designed as a hot-air pre-consolidation device. The thermal pre-consolidation device expediently has at least one hot air knife and / or at least one hot air oven. According to another embodiment of the invention, thermal pre-consolidation or consolidation can also be carried out with pressure rollers or compacting rollers and / or at least one calender can be used for pre-consolidation or consolidation. According to a recommended embodiment of the device according to the invention, a thermal pre-consolidation of the deposited nonwoven web takes place first with the help of at least one hot air knife, in particular with the help of a hot air knife, and then a further thermal pre-consolidation takes place with the help of at least one hot air oven, in particular with the help of a hot air oven. A preferred embodiment of the invention is characterized in that the spunbond nonwoven is only pre-bonded with hot air and / or is only finally bonded with hot air. - The invention is based on the knowledge that due to the filament cross-section according to the invention on the one hand the the entire filament circumference is available for thermal pre-consolidation and, on the other hand, through a targeted selection of parameters - in particular the thickness of the jacket - the thermal pre-consolidation or the extent of the thermal pre-consolidation can be specifically influenced, so that, on the one hand, an optimal consolidation of the nonwoven can be achieved and on the other hand, the crimp of the filaments is nevertheless not impaired too much in order to maintain a desired thickness of the nonwoven fabric. Within the scope of the invention, in particular due to the filament cross section according to the invention, a very simple and targeted setting of the nonwoven properties - in particular with regard to thickness, softness and strength - is possible. Above all, with the invention, the crimp can be adjusted without any problems and can thus be controlled.
Die erfindungsgemäßen Vliesstoffe zeichnen sich einerseits durch eine optimale Dicke und Weichheit aus und andererseits durch eine zufriedenstellende Festigkeit bzw. Abriebsfestigkeit. Die Kräuselung der Filamente kann aufgrund der erfindungsgemäßen Ausgestaltung der Filamente problemlos in den gewünschten Grenzen gehalten werden, sodass gleichsam eine beherrschbare Kräuselung bzw. ein beherrschbarer Crimp das Resultat der erfindungsgemäßen Lehre ist. Bei einfach einzustellender optimaler Festigkeit und Abriebsfestigkeit kann zudem ein weitgehend defektfreier Vliesstoff erzielt werden, der vor allem im Wesentlichen frei von störenden Agglomeraten ist. Zusammenfassend kann festgestellt werden, dass im Rahmen der Erfindung ein optimaler Kompromiss zwischen Festigkeitseigenschaften und Dicken- bzw. Weichheitseigenschaften des Vliesstoffes erreicht werden kann und dieser Kompromiss kann bei einer überraschend homogenen Filamentablage auf einfache Weise erzielt werden.The nonwovens according to the invention are characterized on the one hand by an optimal thickness and softness and on the other hand by a satisfactory strength or abrasion resistance. The crimping of the filaments can easily be kept within the desired limits due to the configuration of the filaments according to the invention, so that at the same time a controllable crimp or a controllable crimp is the result of the teaching according to the invention. With optimal strength and abrasion resistance that are easy to set, a largely defect-free nonwoven fabric can also be achieved, which above all is essentially free of troublesome agglomerates. In summary, it can be stated that within the scope of the invention an optimal compromise between strength properties and thickness or softness properties of the nonwoven fabric can be achieved and this compromise can be achieved in a simple manner with a surprisingly homogeneous filament deposition.
Nachfolgend wird die Erfindung anhand einer lediglich ein Ausführungsbeispiel darstellenden Zeichnung näher erläutert. Es zeigen in schematischer Darstellung:
- Fig. 1
- einen Querschnitt durch ein Endlosfilament
- a)
- mit herkömmlicher exzentrischer Kern-Mantel-Konfiguration und
- b)
- mit erfindungsgemäßer exzentrischer Kern-Mantel-Konfiguration,
- Fig. 2
- einen Schnitt durch ein erfindungsgemäßes Endlosfilament im Detail,
- Fig. 3
- schematisch die Abhängigkeit des Abstandes a der Flächenschwerpunkte von Kern und Mantel eines erfindungsgemäßen Endlosfilamentes von der Dicke d des Mantels der Endlosfilamente im Bereich der konstanten Dicke d des Mantels und
- Fig. 4
- einen Vertikalschnitt durch eine erfindungsgemäße Vorrichtung zur Erzeugung eines erfindungsgemäßen Spunbond-Vliesstoffes.
- Fig. 1
- a cross section through a continuous filament
- a)
- with conventional eccentric core-shell configuration and
- b)
- with an eccentric core-shell configuration according to the invention,
- Fig. 2
- a section through a continuous filament according to the invention in detail,
- Fig. 3
- schematically, the dependence of the distance a of the centroids of the core and sheath of an endless filament according to the invention on the thickness d of the sheath of the continuous filaments in the region of the constant thickness d of the sheath and
- Fig. 4
- a vertical section through a device according to the invention for producing a spunbond nonwoven fabric according to the invention.
Die
Empfohlenermaßen und im Ausführungsbeispiel ist der Kern 4 der erfindungsgemäßen Filamente 2 - im Filamentquerschnitt gesehen - kreissegmentförmig ausgebildet. Zweckmäßigerweise und im Ausführungsbeispiel weist der Kern 4 bezüglich seines Umfanges einen kreisbogenförmigen Umfangsabschnitt 5 sowie einen linearen Umfangsabschnitt 6 auf. Bewährtermaßen und im Ausführungsbeispiel nimmt der kreisbogenförmige Umfangsabschnitt des Kerns 4 über 65 % des Umfanges des Kerns 4 ein. Zweckmäßigerweise und im Ausführungsbeispiel ist der Mantel 3 der Filamente 2 - im Filamentquerschnitt gesehen - außerhalb des Mantelbereiches mit der konstanten Dicke d kreissegmentförmig ausgebildet. Dieses Kreissegment 7 des Mantels 3 weist empfohlenermaßen und im Ausführungsbeispiel bezüglich seines Umfanges einen kreisbogenförmigen Umfangsabschnitt 8 sowie einen linearen Umfangsabschnitt 9 auf.Recommended and in the exemplary embodiment, the
Vorzugsweise beträgt die Dicke d bzw. die mittlere Dicke d des Mantels 3 im Bereich seiner konstanten Dicke 1 % bis 8 %, insbesondere 2 % bis 10 % des Filamentdurchmessers D. Im Ausführungsbeispiel mag die Dicke d des Mantels 3 im Bereich seiner konstanten Dicke 0,2 bis 3 µm betragen.The thickness d or the mean thickness d of the
Die
In der nachfolgenden Tabelle sind die Abstände a der Flächenschwerpunkte von Kern 4 und Mantel 3 für Endlosfilamente 2 mit einem Filamentdurchmesser D von 18 µm angegeben und zwar für unterschiedliche Flächenverhältnisse Kern:Mantel (75:25, 67:33 und 50:50). Links in der Tabelle sind diese Abstände für eine konstante Manteldicke d von 1 µm bei den erfindungsgemäßen Endlosfilamenten mit exzentrischer Kern-Mantel-Konfiguration (erfindungsgemäße eC/S-Filamente) aufgeführt. Rechts in der Tabelle sind die Abstände für eine Manteldicke d' von 1 µm an der Stelle des geringsten Abstandes zwischen Kern 4 und Außenoberfläche für die Endlosfilamente 2 mit herkömmlicher exzentrischer Kern-Mantel-Konfiguration (herkömmliche eC/S-Filamente). Der Abstand a der Flächenschwerpunkte ist hier jeweils absolut in µm aufgeführt sowie relativ zum Filamentdurchmesser D in %.
Aus der Tabelle ist ersichtlich, dass der Abstand a der Flächenschwerpunkte bei gleichem Filamentdurchmesser D und gleichem Flächenverhältnis Kern:Mantel bei den erfindungsgemäßen Endlosfilamenten 2 mit exzentrischer Kern-Mantel-Konfiguration jeweils größer bzw. deutlich größer ist als bei den herkömmlichen Endlosfilamenten 2 mit exzentrischer Kern-Mantel-Konfiguration. Bei der Einhaltung des Abstandes a der Flächenschwerpunkte von Kern 4 und Mantel 3 handelt es sich um ein wesentliches Merkmal der Erfindung, dem besondere Bedeutung zukommt. Der Abstand der Flächenschwerpunkte ist repräsentativ für den Hebelarm, mit dem die Kräuselkräfte aus den beiden Materialien wirken und so ein wesentlicher Faktor für das Ausmaß der Kräuselung.From the table it can be seen that the distance a of the centroids with the same filament diameter D and the same area ratio core: sheath in the
Bevorzugt und im Ausführungsbeispiel besteht der Kern 4 der erfindungsgemäßen Filamente 2 aus Polypropylen und besteht der Mantel 3 der Filamente 2 aus Polyethylen. Dabei handelt es sich um eine ganz besonders bevorzugte Ausführungsform, die sich im Rahmen der Erfindung sehr bewährt hat. Es liegt grundsätzlich im Rahmen der Erfindung, dass der Schmelzpunkt des thermoplastischen Kunststoffs des Mantels 3 geringer ist als der Schmelzpunkt des thermoplastischen Kunststoffes des Kerns 4 der erfindungsgemäßen Endlosfilamente 2.Preferably, and in the exemplary embodiment, the
Nach bevorzugter Ausführungsform der Erfindung haben die Endlosfilamente 2 eines erfindungsgemäßen Spunbond-Vliesstoffes 1 einen Titer von 1,5 bis 2,5 den, vorzugsweise von 1,5 bis 2,2 den und bevorzugt von 1,8 bis 2,2 den. Dieser Titer hat sich im Hinblick auf die Lösung des technischen Problems ganz besonders bewährt. - Es liegt weiterhin im Rahmen der Erfindung, dass es sich bei dem erfindungsgemäßen Spunbond-Vliesstoff 1 um einen thermisch vorverfestigten Spunbond-Vliesstoff handelt, und zwar mit thermischen Bondingstellen bzw. Bondingpunkten zwischen den Endlosfilamenten 2. Nach ganz besonders bevorzugter Ausführungsform handelt es sich bei dem erfindungsgemäßen Spunbond-Vliesstoff 1 um einen mit Heißluft thermisch vorverfestigten Spunbond-Vliesstoff 1. Ein solcher Spunbond-Vliesstoff 1 hat sich im Hinblick auf die Lösung des technischen Problems sehr bewährt.According to a preferred embodiment of the invention, the
Die
Bevorzugt und im Ausführungsbeispiel werden die ersponnenen Endlosfilamente 2 in eine Kühlvorrichtung 11 mit einer Kühlkammer 12 eingeführt.Preferably, and in the exemplary embodiment, the spun
Zweckmäßigerweise und im Ausführungsbeispiel sind an zwei gegenüberliegenden Seiten der Kühlkammer 12 übereinander angeordnete Luftzufuhrkabinen 13, 14 angeordnet. Aus den übereinander angeordneten Luftzufuhrkabinen 13, 14 wird zweckmäßigerweise Luft unterschiedlicher Temperatur in die Kühlkammer 12 eingeführt.Appropriately and in the exemplary embodiment,
Nach bevorzugter Ausführungsform und im Ausführungsbeispiel gemäß
In Filamentströmungsrichtung ist der Kühlvorrichtung 11 eine Verstreckeinrichtung 16 zum Verstrecken der Endlosfilamente 2 nachgeschaltet. Empfohlenermaßen und im Ausführungsbeispiel weist die Verstreckeinrichtung 16 einen Zwischenkanal 17 auf, der die Kühlvorrichtung 11 mit einem Verstreckschacht 18 der Verstreckeinrichtung 16 verbindet. Nach besonders bevorzugter Ausführungsform und im Ausführungsbeispiel ist das Aggregat aus der Kühlvorrichtung 11 und der Verstreckeinrichtung 16 bzw. das Aggregat aus der Kühlvorrichtung 11, dem Zwischenkanal 17 und dem Verstreckschacht 18 als geschlossenes Aggregat ausgebildet und außer der Zufuhr von Kühlluft in der Kühlvorrichtung 11 erfolgt keine weitere Luftzufuhr von außen in dieses Aggregat.A stretching
Empfohlenermaßen und im Ausführungsbeispiel schließt in Filamentströmungsrichtung an die Verstreckeinrichtung 16 ein Diffusor 19 an, durch den die Endlosfilamente 2 geführt werden. Nach Durchlaufen des Diffusors 19 werden die Endlosfilamente 2 vorzugsweise und im Ausführungsbeispiel auf einer als Ablagesiebband 20 ausgebildeten Ablagevorrichtung abgelegt. Das Ablagesiebband 20 ist bevorzugt und im Ausführungsbeispiel als endlos umlaufendes Ablagesiebband 20 ausgebildet. Zweckmäßigerweise ist es luftdurchlässig ausgeführt, sodass eine Absaugung von unten durch das Ablagesiebband 20 möglich ist.Recommended and in the exemplary embodiment, a
Gemäß empfohlener Ausführungsform und im Ausführungsbeispiel weist der Diffusor 19 bzw. der unmittelbar über dem Ablagesiebband 20 angeordnete Diffusor 19 zwei gegenüberliegende Diffusorwände auf, wobei zwei untere divergierende Diffusorwandabschnitte 21, 22 vorgesehen sind, die bevorzugt bezüglich der Mittelebene M des Diffusors 19 asymmetrisch ausgebildet sind. Zweckmäßigerweise und im Ausführungsbeispiel bildet der einlaufseitige Diffusorwandabschnitt 21 einen geringeren Winkel β mit der Mittelebene M des Diffusors 19 als der auslaufseitige Diffusorwandabschnitt 22. Dieser bevorzugten Ausführungsform kommt im Rahmen der Erfindung besondere Bedeutung zu und sie hat sich im Hinblick auf die Lösung des technischen Problems besonders bewährt. Die Begriffe einlaufseitig und auslaufseitig beziehen sich hier im Übrigen auf die Laufrichtung des Ablagesiebbandes 20 bzw. auf die Förderrichtung der Vliesbahn.According to the recommended embodiment and in the exemplary embodiment, the
Gemäß einer empfohlenen Ausführungsform der Erfindung sind an dem Einströmende 23 des Diffusors 19 zwei gegenüberliegende Sekundärlufteintrittsspalte 24, 25 vorgesehen, die jeweils an einer der beiden gegenüberliegenden Diffusorwände angeordnet sind. Vorzugsweise ist durch den in Bezug auf die Förderrichtung des Ablagesiebbandes 20 einlaufseitigen Sekundärlufteintrittsspalt 24 ein geringerer Sekundärluftvolumenstrom einführbar als durch den auslaufseitigen Sekundärlufteintrittsspalt 25. Auch dieser Ausführungsform kommt im Rahmen der Erfindung besondere Bedeutung zu.According to a recommended embodiment of the invention, two opposite secondary
Empfohlenermaßen und im Ausführungsbeispiel ist zumindest eine Absaugeinrichtung vorhanden, mit der im Ablagebereich 26 der Filamente 2 in einem Hauptabsaugbereich 27 Luft bzw. Prozessluft durch das Ablagesiebband 20 saugbar ist. Zweckmäßigerweise ist der Hauptabsaugbereich 27 unterhalb des Ablagesiebbandes 20 in einem Einlaufbereich des Ablagesiebbandes 20 und in einem Auslaufbereich des Ablagesiebbandes 20 jeweils durch eine Saugtrennwand 28 begrenzt. Vorzugsweise und im Ausführungsbeispiel ist dem Hauptabsaugbereich 27 in Förderrichtung des Ablagesiebbandes 20 ein zweiter Absaugbereich 29 nachgeschaltet, in dem Luft bzw. Prozessluft durch das Ablagesiebband 20 saugbar ist. Es empfiehlt sich, dass die Absauggeschwindigkeit v2 der Prozessluft durch das Ablagesiebband 20 in dem zweiten Absaugbereich 29 geringer ist als die Absauggeschwindigkeit vH in dem Hauptabsaugbereich 27.Recommended and in the exemplary embodiment, there is at least one suction device with which air or process air can be sucked through the
Eine besonders bevorzugte Ausführungsform ist dadurch gekennzeichnet, dass das dem Ablagesiebband 20 zugewandte Ende einer Saugtrennwand 28 einen vertikalen Abstand A zu dem Ablagesiebband 20 zwischen 10 und 250 mm, insbesondere zwischen 25 und 200 mm, vorzugsweise zwischen 28 und 150 mm und bevorzugt zwischen 29 und 140 mm und sehr bevorzugt zwischen 30 und 120 mm aufweist. Nach einer sehr empfohlenen Ausführungsform ist in dem dem Ablagesiebband 20 zugewandten Bereich dieser Saugtrennwand 28 ein als Spoilerabschnitt 30 ausgebildeter Trennwandabschnitt angeschlossen, der das genannte dem Ablagesiebband 20 zugewandte Ende der Saugtrennwand 28 umfasst. Es liegt im Rahmen der Erfindung, dass das dem Ablagesiebband 20 zugewandte Ende dieses Spoilerabschnittes 30 zu einer gedachten Verlängerung der übrigen zugeordneten Saugtrennwand 28 einen horizontalen Abstand C aufweist, der zumindest 80 % des vertikalen Abstandes A entspricht. Die Abstände A und C sind in den Figuren nicht eingezeichnet. - Gemäß einer - in
Zweckmäßigerweise und im Ausführungsbeispiel ist in Förderrichtung der Vliesbahn nach dem Ablagebereich 26 zumindest eine thermische Vorverfestigungseinrichtung zur thermischen Vorverfestigung der Vliesbahn vorgesehen. Vorzugsweise ist die thermische Vorverfestigungseinrichtung am bzw. über dem zweiten Absaugbereich 29 angeordnet. Gemäß besonders bevorzugter Ausführungsform arbeitet die thermische Vorverfestigungseinrichtung mit Heißluft und besonders bevorzugt handelt es sich bei dieser dem Hauptabsaugbereich 27 nachgeschalteten thermischen Vorverfestigungseinrichtung um ein Heißluftmesser 31. Mit der thermischen Vorverfestigungseinrichtung können Bondingpunkte zwischen den Filamenten 2 der Vliesbahn auf einfache Weise realisiert werden. Dabei kann der über den gesamten Umfang umlaufende Mantel 3 der erfindungsgemäßen Endlosfilamente 2 sehr effektiv zur Ausbildung der thermischen Bondingstellen eingesetzt werden.Appropriately and in the exemplary embodiment, at least one thermal pre-consolidation device for thermal pre-consolidation of the nonwoven web is provided in the conveying direction of the nonwoven web after the depositing
Nach einer Ausführungsform der Erfindung sind zumindest zwei thermische Vorverfestigungseinrichtungen zur Vorverfestigung der Vliesbahn vorgesehen. Zweckmäßigerweise handelt es sich bei der in Förderrichtung der Vliesbahn ersten thermischen Vorverfestigungseinrichtung um ein Heißluftmesser 31 und vorzugsweise ist diesem Heißluftmesser 31 in Förderrichtung des Ablagesiebbandes 20 eine zweite thermische Vorverfestigungseinrichtung in Form eines Heißluftofens 32 nachgeschaltet. Es liegt im Rahmen der Erfindung, dass auch im Bereich des Heißluftofens 32 Luft durch das Ablagesiebband 20 gesaugt wird. Weiterhin liegt es im Rahmen der Erfindung, dass die Absauggeschwindigkeit der durch das Ablagesiebband 20 abgesaugten Luft vom Hauptabsaugbereich 27 zu weiteren Absaugbereichen in Förderrichtung des Ablagesiebbandes 20 abnimmt.According to one embodiment of the invention, at least two thermal pre-consolidation devices are provided for pre-consolidation of the nonwoven web. The first thermal preconsolidation device in the conveying direction of the nonwoven web is expediently a
In
Claims (20)
- A spunbond nonwoven material (1) made of continuous filaments (2), in particular of crimped continuous filaments (2), wherein the filaments (2) are configured as bicomponent filaments or multicomponent filaments and have an eccentric core-sheath configuration, wherein the sheath (3) of the filaments (2) in the filament cross-section has a constant thickness d or substantially constant thickness d over at least 20 %, in particular over at least 25 %, preferably over at least 30 %, preferably over at least 35 % and very preferably over at least 40 % of the filament circumference and wherein the thickness of the sheath (3) in the region of its constant or substantially constant thickness d is 0.1 to 2 µm.
- The spunbond nonwoven material according to one of Claims 1 to 3, wherein the core (4) of the filaments (2) occupies more than 50 %, in particular more than 55 %, preferably more than 60 %, preferably more than 65 % and very preferably more than 70 % of the area of the filament cross-section of the filaments (2).
- The spunbond nonwoven material according to Claim 1 or 2, wherein the core (4) of the filaments (2) when viewed in the filament cross-section is configured to be circular-segment-shaped and in particular with regard to its circumference, has at least one, in particular one circular-arc-shaped circumferential section (5) or substantially circular-arc-shaped circumferential section (5) and at least one, in particular one linear or substantially linear circumferential section (6).
- The spunbond nonwoven material according to Claim 3, wherein the circular-arc-shaped circumferential section (5) of the core (4) occupies over 50 %, in particular over 55 %, preferably over 60 % and preferably over 65 % of the circumference of the core (4) .
- The spunbond nonwoven material according to one of Claims 1 to 4, wherein the sheath (3) of the filaments (2), when viewed in the filament cross-section, is configured in a circular segment shape outside the sheath region having the constant thickness d, wherein this circular segment (7) in relation to its circumference has at least one, in particular one circular-arc-shaped or substantially circular-arc-shaped circumferential section (8) and has at least one, in particular one linear or substantially linear circumferential section (9).
- The spunbond nonwoven material according to one of Claims 1 to 5, wherein the sheath (3) of the filaments (2), when viewed in the filament cross-section, has a constant thickness d or a substantially constant thickness d over 45 %, in particular over 50 %, preferably over 55 % and preferably over 60 % of the filament circumference.
- The spunbond nonwoven material according to one of Claims 1 to 6, wherein the thickness of the sheath (3) in the region of its constant or substantially constant thickness d is less than 10 %, in particular less than 8 % and preferably less than 7 % of the filament diameter D or the largest filament diameter D.
- The spunbond nonwoven material according to one of Claims 1 to 7, wherein the thickness of the sheath (3) in the region of its constant or substantially constant thickness d is 0.1 to 0.9 µm.
- The spunbond nonwoven material according to one of Claims 1 to 8, wherein the ratio of the mass of the core (4) to the mass of the sheath (3) is 90:10 to 50:50, preferably 90:10 to 60:40 and preferably 85:15 to 70:30.
- The spunbond nonwoven material according to one of Claims 1 to 9, wherein the distance a of the centroid of the area of the core (4) from the centroid of the area of the sheath (3) is 5 % to 45 %, in particular 6 % to 40 % and preferably 6 % to 36 % of the filament diameter D or the largest filament diameter D.
- The spunbond nonwoven material according to Claim 10, wherein the distance a of the centroids of the area with a core:sheath mass ratio of 85:15 to 70:30 is between 5 % and 45 % of the filament diameter D or of the largest filament diameter D and/or with a core:sheath mass ratio of 70:30 to 60:40 this distance is between 12 % and 40 % of the filament diameter or of the largest filament diameter D and/or with a core:sheath mass ratio of 60:40 to 45:55 this distance is between 18 % and 36 % of the filament diameter D or the largest filament diameter D.
- The spunbond nonwoven material according to one of Claims 1 to 11, wherein the core (4) and/or the sheath (3) of the filaments (2) consists or substantially consists of a polyolefin, wherein in particular both the core (4) and also the sheath (3) of the filaments (2) consist or substantially consist of at least one polyolefin and wherein preferably the sheath (3) consists or substantially consists of polyethylene and wherein preferably the core (4) consists of polypropylene or substantially consists of polypropylene.
- The spunbond nonwoven material according to one of Claims 1 to 12, wherein the core (4) and/or the sheath (3) of the filaments (2) consists or substantially consists of at least one polyester and/or copolyester, wherein in particular the core (4) consists or substantially consists of a polyester and wherein preferably the sheath (3) consists or substantially consists of a copolyester.
- The spunbond nonwoven material according to one of Claims 1 to 13, wherein the titre of the filaments is 1.5 to 2.5 den, in particular 1.7 to 2.3 den, preferably 1.8 to 2.2 den.
- The spunbond nonwoven material according to one of Claims 1 to 14, wherein the nonwoven material (1) is a thermally pre-consolidated and/or thermally finally consolidated nonwoven material (1) which has bonding positions or bonding points between the filaments.
- A device for producing a spunbond nonwoven material (1) made of continuous filaments (2), in particular of crimped continuous filaments (2), wherein at least one spinning nozzle (10) is provided, wherein the device or the spinning nozzle (10) is adapted with the proviso that multicomponent filaments or bicomponent filaments having an eccentric core-sheath configuration can be produced, wherein the sheath (3) of the filaments (2) when viewed in the filament cross-section has a constant thickness d or substantially constant thickness d over at least 20 %, in particular over at least 25 %, preferably over at least 30 %, preferably over at least 35 % and very preferably over at least 40 % of the filament circumference, wherein the thickness of the sheath (3) in the region of its constant or substantially constant thickness d is 0.1 to 2 µm and wherein the filaments (2) can be deposited on a depositing device, in particular on a depositing foraminous belt (20).
- The device according to Claim 16, wherein the device has a cooling device (11) for cooling the filaments (2) and an adjoining stretching device (16) for stretching the filaments (2) and preferably has at least one diffuser (19) adjoining the stretching device (16).
- The device according to Claim 17, wherein the unit consisting of cooling device (11) and stretching device (16) is configured as a closed unit and wherein apart from the supply of cooling air in the cooling device (11) no further supply of air from outside takes place.
- The device according to one of Claims 16 to 18, wherein at least one thermal pre-consolidating device is provided, by means of which the nonwoven web (1) made of the filaments (2) deposited on the depositing device or on the depositing foraminous belt (20) can be thermally pre-consolidated.
- The device according to Claim 19, wherein the thermal pre-consolidating device is configured as a hot air pre-consolidating device.
Priority Applications (20)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK19189237.1T DK3771761T3 (en) | 2019-07-30 | 2019-07-30 | Spunbond nonwoven fabric of endless filaments and device for the production of the spunbond nonwoven fabric |
EP19189237.1A EP3771761B1 (en) | 2019-07-30 | 2019-07-30 | Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric |
ES19189237T ES2887951T3 (en) | 2019-07-30 | 2019-07-30 | Continuous filament spunbonded nonwoven material and device for producing the spunbonded nonwoven material |
PL19189237T PL3771761T3 (en) | 2019-07-30 | 2019-07-30 | Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric |
CA3138612A CA3138612A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven fabric made of endless filaments and apparatus for making the spunbond nonwoven fabric |
AU2020322639A AU2020322639A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material |
MA54584A MA54584B1 (en) | 2019-07-30 | 2020-07-14 | Spunbonded nonwoven material consisting of continuous filaments and device for producing the spunbonded nonwoven material |
PE2021001596A PE20212355A1 (en) | 2019-07-30 | 2020-07-14 | SPUN-SPUN NON-WOVEN FABRIC MANUFACTURED WITH CONTINUOUS FILAMENTS AND APPARATUS FOR MANUFACTURING SPUN-SPUN NON-WOVEN FABRIC |
JP2021560393A JP2022542497A (en) | 2019-07-30 | 2020-07-14 | Nonwoven fabrics made of endless filaments and nonwoven spunbonds |
JOP/2022/0019A JOP20220019A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material |
MX2022001188A MX2022001188A (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material. |
TNP/2021/000211A TN2021000211A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material |
CN202080017576.2A CN113508199A (en) | 2019-07-30 | 2020-07-14 | Spunbonded nonwoven formed from continuous filaments and device for producing spunbonded nonwoven |
IL286980A IL286980B (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material |
US17/426,834 US20220251747A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven of continuous filaments and method of making sam3e |
BR112021015709-3A BR112021015709B1 (en) | 2019-07-30 | 2020-07-14 | TNT SPUNBOND WITH CONTINUOUS FILAMENTS AND DEVICE FOR GENERATING A TNT SPUNBOND WITH CONTINUOUS FILAMENTS |
KR1020217038218A KR20220037406A (en) | 2019-07-30 | 2020-07-14 | Spunbond Nonwoven Material Made of Continuous Filament and Apparatus for Producing Spunbond Nonwoven Material |
PCT/EP2020/069906 WO2021018574A1 (en) | 2019-07-30 | 2020-07-14 | Spunbond nonwoven material made of continuous filaments and device for producing the spunbond nonwoven material |
CONC2021/0012402A CO2021012402A2 (en) | 2019-07-30 | 2021-09-22 | Spunbond nonwoven fabric made from continuous filaments and apparatus for making spunbond nonwoven fabric |
CL2021002774A CL2021002774A1 (en) | 2019-07-30 | 2021-10-22 | Spunbond nonwoven fabric made from continuous filaments and apparatus for making spunbond nonwoven fabric |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19189237.1A EP3771761B1 (en) | 2019-07-30 | 2019-07-30 | Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric |
Publications (2)
Publication Number | Publication Date |
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EP3771761A1 EP3771761A1 (en) | 2021-02-03 |
EP3771761B1 true EP3771761B1 (en) | 2021-05-19 |
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EP19189237.1A Active EP3771761B1 (en) | 2019-07-30 | 2019-07-30 | Spunbond nonwoven fabric made from endless filaments and device for producing spunbond nonwoven fabric |
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US (1) | US20220251747A1 (en) |
EP (1) | EP3771761B1 (en) |
JP (1) | JP2022542497A (en) |
KR (1) | KR20220037406A (en) |
CN (1) | CN113508199A (en) |
AU (1) | AU2020322639A1 (en) |
BR (1) | BR112021015709B1 (en) |
CA (1) | CA3138612A1 (en) |
CL (1) | CL2021002774A1 (en) |
CO (1) | CO2021012402A2 (en) |
DK (1) | DK3771761T3 (en) |
ES (1) | ES2887951T3 (en) |
IL (1) | IL286980B (en) |
JO (1) | JOP20220019A1 (en) |
MA (1) | MA54584B1 (en) |
MX (1) | MX2022001188A (en) |
PE (1) | PE20212355A1 (en) |
PL (1) | PL3771761T3 (en) |
TN (1) | TN2021000211A1 (en) |
WO (1) | WO2021018574A1 (en) |
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CN115694776A (en) | 2021-07-27 | 2023-02-03 | 三星电子株式会社 | Storage device, storage system operation method and computing system |
DE102022115200A1 (en) | 2022-06-17 | 2023-12-28 | Reifenhäuser GmbH & Co. KG Maschinenfabrik | Nonwoven fabric and device for producing a nonwoven fabric |
DE102022115205A1 (en) * | 2022-06-17 | 2023-12-28 | Reifenhäuser GmbH & Co. KG Maschinenfabrik | Method and device for producing a nonwoven fabric |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1346103A (en) * | 1971-06-18 | 1974-02-06 | Ici Ltd | Apparatus for the manufacture of eccentric core/sheath cojugate filaments |
US5599420A (en) * | 1993-04-06 | 1997-02-04 | Kimberly-Clark Corporation | Patterned embossed nonwoven fabric, cloth-like liquid barrier material and method for making same |
CA2105026C (en) * | 1993-04-29 | 2003-12-16 | Henry Louis Griesbach Iii | Shaped nonwoven fabric and method for making the same |
US5512358A (en) * | 1993-09-22 | 1996-04-30 | Kimberly-Clark Corporation | Multi-component polymeric strands including a butene polymer and nonwoven fabric and articles made therewith |
WO1996021759A1 (en) * | 1995-01-09 | 1996-07-18 | Kanebo, Ltd. | Conjugated fiber and fiber structure containing the same |
JP2003013354A (en) * | 2001-06-26 | 2003-01-15 | Toray Ind Inc | Spun-bond nonwoven fabric |
US20040110442A1 (en) * | 2002-08-30 | 2004-06-10 | Hannong Rhim | Stretchable nonwoven materials with controlled retraction force and methods of making same |
ATE333528T1 (en) * | 2003-08-08 | 2006-08-15 | Reifenhaeuser Gmbh & Co Kg | SPUNNED WEB AND METHOD FOR PRODUCING A SPUNNED WEB |
DE102004040645A1 (en) * | 2004-08-20 | 2006-03-02 | REIFENHäUSER GMBH & CO. MASCHINENFABRIK | Apparatus for the continuous production of a spunbonded nonwoven web |
EP2034057A1 (en) * | 2007-09-10 | 2009-03-11 | ALBIS Spa | Elastic spunbonded nonwoven and elastic nonwoven fabric comprising the same |
TWI721037B (en) * | 2015-11-20 | 2021-03-11 | 美商纖維創新科技公司 | Multicomponent fibers, fabric, yarn and forming method thereof |
DE102016109115A1 (en) * | 2016-05-18 | 2017-11-23 | Reifenhäuser GmbH & Co. KG Maschinenfabrik | Spunbonded nonwoven made of continuous filaments |
MY193083A (en) * | 2016-12-14 | 2022-09-26 | Toray Industries | Eccentric core-sheath composite fiber and combined filament yarn |
-
2019
- 2019-07-30 EP EP19189237.1A patent/EP3771761B1/en active Active
- 2019-07-30 DK DK19189237.1T patent/DK3771761T3/en active
- 2019-07-30 ES ES19189237T patent/ES2887951T3/en active Active
- 2019-07-30 PL PL19189237T patent/PL3771761T3/en unknown
-
2020
- 2020-07-14 KR KR1020217038218A patent/KR20220037406A/en not_active Application Discontinuation
- 2020-07-14 JO JOP/2022/0019A patent/JOP20220019A1/en unknown
- 2020-07-14 MA MA54584A patent/MA54584B1/en unknown
- 2020-07-14 TN TNP/2021/000211A patent/TN2021000211A1/en unknown
- 2020-07-14 PE PE2021001596A patent/PE20212355A1/en unknown
- 2020-07-14 CN CN202080017576.2A patent/CN113508199A/en active Pending
- 2020-07-14 IL IL286980A patent/IL286980B/en unknown
- 2020-07-14 AU AU2020322639A patent/AU2020322639A1/en active Pending
- 2020-07-14 WO PCT/EP2020/069906 patent/WO2021018574A1/en active Application Filing
- 2020-07-14 US US17/426,834 patent/US20220251747A1/en active Pending
- 2020-07-14 CA CA3138612A patent/CA3138612A1/en active Pending
- 2020-07-14 BR BR112021015709-3A patent/BR112021015709B1/en active IP Right Grant
- 2020-07-14 JP JP2021560393A patent/JP2022542497A/en active Pending
- 2020-07-14 MX MX2022001188A patent/MX2022001188A/en unknown
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2021
- 2021-09-22 CO CONC2021/0012402A patent/CO2021012402A2/en unknown
- 2021-10-22 CL CL2021002774A patent/CL2021002774A1/en unknown
Non-Patent Citations (1)
Title |
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None * |
Also Published As
Publication number | Publication date |
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CO2021012402A2 (en) | 2021-12-10 |
CN113508199A (en) | 2021-10-15 |
CA3138612A1 (en) | 2021-02-04 |
JOP20220019A1 (en) | 2023-01-30 |
EP3771761A1 (en) | 2021-02-03 |
ES2887951T3 (en) | 2021-12-29 |
MA54584B1 (en) | 2022-10-31 |
CL2021002774A1 (en) | 2022-05-27 |
BR112021015709B1 (en) | 2024-01-09 |
US20220251747A1 (en) | 2022-08-11 |
PL3771761T3 (en) | 2021-11-02 |
IL286980B (en) | 2022-07-01 |
KR20220037406A (en) | 2022-03-24 |
MX2022001188A (en) | 2023-02-24 |
JP2022542497A (en) | 2022-10-04 |
PE20212355A1 (en) | 2021-12-17 |
AU2020322639A1 (en) | 2021-10-07 |
DK3771761T3 (en) | 2021-07-26 |
MA54584A1 (en) | 2022-02-28 |
TN2021000211A1 (en) | 2023-07-04 |
BR112021015709A2 (en) | 2022-02-08 |
WO2021018574A1 (en) | 2021-02-04 |
IL286980A (en) | 2021-12-01 |
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