WO2021096008A1 - Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn - Google Patents

Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn Download PDF

Info

Publication number
WO2021096008A1
WO2021096008A1 PCT/KR2020/006160 KR2020006160W WO2021096008A1 WO 2021096008 A1 WO2021096008 A1 WO 2021096008A1 KR 2020006160 W KR2020006160 W KR 2020006160W WO 2021096008 A1 WO2021096008 A1 WO 2021096008A1
Authority
WO
WIPO (PCT)
Prior art keywords
yarn
core
elastic
composite elastic
filaments
Prior art date
Application number
PCT/KR2020/006160
Other languages
French (fr)
Korean (ko)
Inventor
김기림
정현기
강연수
김문선
Original Assignee
효성티앤씨 주식회사
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to US17/766,399 priority Critical patent/US20240011200A1/en
Application filed by 효성티앤씨 주식회사 filed Critical 효성티앤씨 주식회사
Priority to BR112022007993A priority patent/BR112022007993A2/en
Priority to CN202080074607.8A priority patent/CN114599829B/en
Priority to EP20888510.3A priority patent/EP4060103A4/en
Publication of WO2021096008A1 publication Critical patent/WO2021096008A1/en

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/32Elastic yarns or threads ; Production of plied or cored yarns, one of which is elastic
    • D02G3/328Elastic yarns or threads ; Production of plied or cored yarns, one of which is elastic containing elastane
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/32Elastic yarns or threads ; Production of plied or cored yarns, one of which is elastic
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/32Elastic yarns or threads ; Production of plied or cored yarns, one of which is elastic
    • D02G3/324Elastic yarns or threads ; Production of plied or cored yarns, one of which is elastic using a drawing frame
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01DMECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
    • D01D5/00Formation of filaments, threads, or the like
    • D01D5/28Formation of filaments, threads, or the like while mixing different spinning solutions or melts during the spinning operation; Spinnerette packs therefor
    • D01D5/30Conjugate filaments; Spinnerette packs therefor
    • D01D5/34Core-skin structure; Spinnerette packs therefor
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G1/00Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics
    • D02G1/16Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics using jets or streams of turbulent gases, e.g. air, steam
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/02Yarns or threads characterised by the material or by the materials from which they are made
    • D02G3/04Blended or other yarns or threads containing components made from different materials
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/36Cored or coated yarns or threads
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/38Threads in which fibres, filaments, or yarns are wound with other yarns or filaments, e.g. wrap yarns, i.e. strands of filaments or staple fibres are wrapped by a helically wound binder yarn
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02JFINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
    • D02J1/00Modifying the structure or properties resulting from a particular structure; Modifying, retaining, or restoring the physical form or cross-sectional shape, e.g. by use of dies or squeeze rollers
    • D02J1/08Interlacing constituent filaments without breakage thereof, e.g. by use of turbulent air streams
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02JFINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
    • D02J11/00Combinations, not covered by any one of the preceding groups, of processes provided for in such groups; Plant for carrying-out such combinations of processes
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/20Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
    • D03D15/208Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads cellulose-based
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/20Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
    • D03D15/233Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads protein-based, e.g. wool or silk
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/20Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
    • D03D15/283Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads synthetic polymer-based, e.g. polyamide or polyester fibres
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/40Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the yarns or threads
    • D03D15/47Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the yarns or threads multicomponent, e.g. blended yarns or threads
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/50Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the properties of the yarns or threads
    • D03D15/56Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the properties of the yarns or threads elastic
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2201/00Cellulose-based fibres, e.g. vegetable fibres
    • D10B2201/01Natural vegetable fibres
    • D10B2201/02Cotton
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2201/00Cellulose-based fibres, e.g. vegetable fibres
    • D10B2201/01Natural vegetable fibres
    • D10B2201/04Linen
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2201/00Cellulose-based fibres, e.g. vegetable fibres
    • D10B2201/20Cellulose-derived artificial fibres
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2201/00Cellulose-based fibres, e.g. vegetable fibres
    • D10B2201/20Cellulose-derived artificial fibres
    • D10B2201/22Cellulose-derived artificial fibres made from cellulose solutions
    • D10B2201/24Viscose
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2211/00Protein-based fibres, e.g. animal fibres
    • D10B2211/01Natural animal fibres, e.g. keratin fibres
    • D10B2211/02Wool
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2211/00Protein-based fibres, e.g. animal fibres
    • D10B2211/01Natural animal fibres, e.g. keratin fibres
    • D10B2211/04Silk
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2321/00Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D10B2321/02Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds polyolefins
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/02Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyamides
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/04Fibres 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]
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/10Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyurethanes
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2401/00Physical properties
    • D10B2401/06Load-responsive characteristics
    • D10B2401/061Load-responsive characteristics elastic
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2501/00Wearing apparel

Definitions

  • the present invention relates to a method of manufacturing a composite elastic yarn, an elastic fabric, and a composite elastic yarn, and more particularly, a puckering in the form of a fabric using a low adhesion elastic yarn having a low adhesion between filaments as a core yarn of the composite elastic yarn. It relates to a composite elastic yarn, an elastic fabric, and a method of manufacturing a composite elastic yarn that solved the problem.
  • spandex is woven into composite elastic yarns used as core yarns.
  • the composite elastic yarn is composed of a core section and a sheath section covering the core section.
  • the core yarn of the composite elastic yarn in the denim fabric is used as a single-core or dual-core elastic yarn to give elasticity to the denim fabric.
  • one elastic yarn is applied as core yarn
  • dual core elastic yarn and two polyester bicomponent fibers are applied as core yarn.
  • U.S. Patent No. 8,093,160 discloses an elastic core yarn comprising a core portion composed of at least one elastic core filament and at least one inelastic core filament, and a sheath portion of short fibers arranged in a manner surrounding the core portion in a longitudinal direction.
  • an elastic denim containing a core yarn Disclosed is an elastic denim containing a core yarn.
  • the stretchable denim obtained by this technique does not provide an appropriate level of stretchability, and there is a limit to the thickness of the yarn that can be used in the sheath portion including short fibers.
  • Composite elastic yarn and its manufacturing method are well known.
  • composite elastic yarns in which the elastic fiber core is covered with inelastic fibers are described in U.S. Patent Nos. 4,470,250 4,998,403, 7,134,265, 6,848,151.
  • the present invention is to solve the problems of the prior art described above, one object of the present invention is by applying an elastic yarn having a low adhesion between filaments to the core portion of the composite elastic yarn, puckering occurring on the surface of the denim fabric. ) To solve the problem.
  • Another object of the present invention is to provide a composite elastic yarn having high elasticity and remarkably improved elastic recovery property of a fabric in which the core yarn is used by forming a core portion of two or more elastic yarns supplied from a single bobbin.
  • Another object of the present invention is to improve the quality of the product and improve the feel of use by solving the problem of perkering occurring in the final product of the stretchable fabric.
  • a composite elastic yarn comprising a core part composed of an elastic core filament and a sheath part composed of short fibers surrounding the core part, wherein the elastic core filament has an adhesive force between the filaments in the range of 9 to 198 mg as measured by ASTM D3822 method. It relates to a composite elastic yarn, characterized in that it has a low adhesion property.
  • the elastic core filament has an inter-filament adhesion of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness.
  • the core portion may be composed of polyurethane, polyurethane-urea, or a blend of polyurethane and polyurethane-urea, and the sheath portion is wool, linen, silk, polyester, nylon, olefin, cotton, tencel, modal, poly It may be composed of hard yarn selected from the group consisting of viscose (poly-viscose) and combinations thereof.
  • the fineness of the core yarn may be 40 to 120 denier.
  • Another aspect of the present invention includes a composite elastic yarn in which at least one of the warp and weft yarns includes a core portion composed of an elastic core filament and a sheath portion composed of short fibers surrounding the core portion, wherein the elastic core filament is ASTM It relates to a fabric characterized in that it has a low adhesion property in the range of 9 to 198 mg of adhesion between the filaments as measured by the D3822 method.
  • the fabric of the present invention can be used for denim or non-denim.
  • the first interlacing is performed so that the bonding force between the filaments is 500 to 1500 mg, followed by secondary interlacing so that the bonding force between the filaments is 9 to 198 mg.
  • the first interlacing is performed so that the bonding force between the filaments is 500 to 1500 mg, followed by secondary interlacing so that the bonding force between the filaments is 9 to 198 mg.
  • the air flow rate is set to 3 to 4 L/min, and the temperature is set to 35 to 30°C for the first interlacing, and in the second interlacing step, the air flow rate is set to 1 to 2 L/min.
  • Interlacing can be performed by setting the temperature to 15 ⁇ 20°C.
  • the present invention applies the core yarn of the composite elastic yarn as a single elastic yarn, but by using the elastic yarn with low adhesion between the filaments as the core yarn, which occurs on the surface of the denim fabric when a general single-core yarn or dual-core yarn is applied as a core yarn. There is an excellent effect of the present invention in that the perkering problem is solved.
  • the spinning process in which the primary and secondary air entanglement processes are added by the spinning process in which the primary and secondary air entanglement processes are added, the bonding force between the filament strands in the yarn without deterioration and filamentation of the yarn properties of the composite elastic yarn occurs.
  • This low adhesion spandex yarn can be produced.
  • the fabric of the present invention improves the quality of the surface by improving the perkering problem occurring on the fabric surface, thereby providing a user with a comfortable feeling of use.
  • the final product obtained by using the low bonding core yarn of the present invention has high elastic properties, remarkably improved elastic recovery properties, and shape retention properties.
  • FIG. 1 is a schematic diagram of an apparatus for manufacturing a core yarn of a composite elastic yarn according to an embodiment of the present invention.
  • FIG. 2 is a schematic diagram of an apparatus for manufacturing a composite elastic yarn according to an embodiment of the present invention.
  • filament means long fiber strands
  • staple fiber means a limited or short length fiber strand
  • elastic core filament refers to a filament having an elongation at break of more than 100%, and a preferred example is a spandex fiber.
  • composite elastic yarn refers to a core-spun yarn made by covering fibers around an elastic core filament.
  • the "bonding force between filaments” means that one filament in the yarn is separated by a length of 1 cm or more, and then the ends of the separated filaments are hung on a bonding force measuring device (Lenzing Instruments GmbH & Co. KG, Vibrodyn 400). Means the value (mg) measured according to ASTM D3822-07 method (Standard test methods for tensile properties of single textile fibers") by stretching at a constant elongation rate. do.
  • the composite elastic yarn of one aspect of the present invention is a composite elastic yarn comprising a core part composed of an elastic core filament and a sheath part composed of short fibers surrounding the core part, wherein the elastic core filament is measured by the ASTM D3822 method. It has a low adhesion property in which the adhesion force is in the range of 9 to 198 mg.
  • the elastic core filament may be a low adhesion elastic core filament having a low adhesion of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness.
  • the adhesive force between the filaments of the spandex 80D yarn, which is commonly used is at the level of 700 to 900 mg
  • the low adhesion elastic core filament according to the present invention is the sum of about 9 mg to 198 mg of the filaments in the case of 80D. Have a good fit.
  • the bonding force between the filaments of the core yarn is less than 1.5% of the bonding force of the general-purpose spandex of the same fineness, a filamentation phenomenon in which the filaments in the yarn are separated due to excessively low bonding force may occur.
  • the bonding force between the filaments of the core yarn exceeds 22% of the bonding strength of the general-purpose spandex of the same fineness, it is not possible to provide a sufficient surface area to be fused by contact with the cotton yarn, which is the sheath part, during the covering process, so it is manufactured in the form of a fabric. There is a risk of perkering.
  • the core portion may be composed of an elastic core filament composed of polyurethane, polyurethane-urea, or a blend of polyurethane and polyurethane-urea.
  • the sheath portion may be a natural fiber such as cotton, wool, linen, silk, tencel, or modal.
  • the sheath portion may be a single component staple synthetic fiber.
  • the sheath portion may be a fiber selected from the group consisting of polyester, nylon, olefin, poly-viscose, acrylic, modacrylic, rayon, and any combination thereof.
  • the sheath portion preferably includes cotton yarn.
  • the core yarn has a fineness of 40 denier to 120 denier.
  • the fineness of the core yarn is less than 40 denier, a thin denim fabric is formed compared to the general fabric used for denim, and the effect of correcting the body when worn is insignificant and the appearance of the clothing is poor.
  • the fineness of the core yarn exceeds 120 denier, a thick denim fabric is formed compared to a general fabric for denim use, and the feeling of wearing clothes is deteriorated due to a stiff and heavy feeling.
  • Another aspect of the present invention relates to a method of manufacturing an elastic composite yarn.
  • the first interlacing is performed so that the bonding force between the filaments is 500 to 1500 mg
  • the second interlacing is performed so that the bonding force between the filaments is 9 to 198 mg
  • the low bonding core is wound.
  • a composite elastic yarn can be produced by preparing a yarn, and then coating the obtained low-adhesion core yarn with a short fiber roving yarn and spinning it.
  • the composite elastic yarn of the present invention is produced by spinning core yarn and sheath by ring spinning or open-end spinning in a spinning machine.
  • Spandex yarn is generally produced by dry spinning at high temperatures in a spinning barrel. At this time, the spandex yarn is heated after spinning, resulting in a lower modulus and an appropriate temperature for imparting twist to the yarn. In the drawing process, the spandex yarn passes through an air interlaced nozzle to impart adhesion between the filaments to perform winding. If you want to produce yarns with low adhesion to solve the perkering problem in denim fabrics, you can produce yarns with low adhesion by lowering the pressure applied from the air interlacing nozzle during the yarn spinning process.
  • the air interlaced nozzle (hereinafter referred to as “interlace nozzle”) that imparts adhesion in the spinning process of the core yarn is used as the first and second capable of imparting adhesion in two steps in the spinning process using one existing interlaced nozzle.
  • interlace nozzle By applying the second interlaced nozzle to the spinning process, it is possible to solve the problem of perkering in the final fabric.
  • the first interlaced nozzle 14 controls the pressure and temperature in the same way as the spinning process of the existing spandex, and passes the yarn through the air.
  • the flow rate of air in the general interlaced nozzle is 3 to 4 L/min, and the temperature is 35 to 30° C., and the air flow rate and temperature of the first interlaced nozzle 14 according to the present invention were the same as the above-mentioned existing conditions.
  • the yarn is adjusted so that it can be bonded to two large filament strands.
  • the second interlaced nozzle 15 finally produces a low adhesion elastic core filament having a low adhesion by passing the yarn strands passing through the first interlaced nozzle while applying low temperature and low pressure air. More specifically, the yarn that has passed through the first interlaced nozzle 14 exists in a form of largely bonded to two filament strands, and the yarn is fed from the second interlaced nozzle 15 at a flow rate of 1 to 2 L/min and It is produced to give very low adhesion between two filament strands by passing it through air at a temperature of 15 ⁇ 20°C.
  • the low bonding elastic core filament 21 is obtained by the core yarn manufacturing apparatus 10, and the composite elastic yarn 40 is obtained by the complex elastic yarn spinning apparatus 30.
  • the core yarn manufacturing apparatus 10 used to obtain the low bonding elastic core filament 21 is basically a dry spinning unit 11, a guide cylinder 12 continuously provided to the dry spinning unit 11 ), an oil pickup roller 13, a take-up device 16, and a bobbin 17 associated with the take-up device 16.
  • the polyurethaneurea polymer is first spun in the form of an elastic yarn 20 in the dry spinning unit 11. Subsequently, the obtained elastic yarn 20 passes through the oil pickup roller 13, passes through the first interlace nozzle 14 and the second interlace nozzle 15 by the guide cylinder 12, and is transferred to the take-up device 16. The oil pickup roller 13 transfers the elastic yarn 20 without oscillation and vibration in order to properly wind the elastic yarn 20. The elastic yarn 20 transmitted to the take-up device 16 is wound on the bobbin 17.
  • the composite elastic yarn spinning device 30 is basically a low-cohesion elastic core filament obtained from a roving yarn 31, a yarn drawing cylinder 32 through which the roving yarn 31 passes, a thin roving yarn 31, and a bobbin 17. It includes a guide front cylinder 33 supplied with 21, a yarn guide 34 provided continuously with the guide front cylinder 33, and a spinning unit 35.
  • the spinning unit 35 includes a ring 351, a moving unit 352 and a cop 353.
  • the roving yarn 31 Passing the roving yarn 31 between the yarn drawing cylinders 32, supplying the low bonding elastic core filament 21 from the bobbin 17 to the guiding front cylinder 33, and combining with the drawn roving yarn 31 ,
  • the thin roving yarn 31 and the low adhesion elastic core filament 21 are supplied from the yarn guide 34 to provide a smooth flow, and the spinning unit 35 is oriented, and the spinning unit 35 to the ring 351
  • the thin roving yarn 31 is wound on the low bonding elastic core filament 21, and the composite elastic yarn 40 can be manufactured by spinning and winding on the cob 353. .
  • the composite elastic yarn obtained by this process has a structure in which the roving yarn 31 is covered on the low adhesion elastic core filament 21.
  • the elastic yarn 20 used in the core portion is made of two-end or more elastic yarns supplied from a single bobbin. In this way, when a plurality of ends containing elastic yarns such as spandex provided from a single bobbin are used in the core portion, elasticity and elastic recovery rate can be improved in a final product such as a fabric in which the core yarn is used.
  • the elastic yarn 20 included in the core yarn structure is supplied from an individual bobbin, a difference in tension between the spandex is caused, thereby forming an uneven core yarn structure.
  • high elasticity is achieved by a component of a plurality of elastic yarns 20 provided from a single bobbin 17 of the core portion to a plurality of ends. Therefore, it is possible to obtain a core yarn with high uniformity.
  • the fabric of the present invention includes a composite elastic yarn in which at least one of the warp and weft yarns includes a core portion composed of an elastic core filament and a sheath portion composed of short fibers surrounding the core portion, wherein the elastic core filament is the ASTM D3822 method It is characterized in that it has a low adhesion property in the range of 9 to 198 mg of adhesion between filaments when measured as.
  • the fabric of the present invention can be used as a fabric for denim or non-denim.
  • the composite elastic yarn of the present invention may be used in the manufacture of fabrics, knitted fabrics, non-woven fabrics, and the like, and may be preferably used in stretch fabrics for denim.
  • the fabric can be made in a variety of weaving patterns including plain weave, poplin, twill, oxford, dobby, satin, satin, and combinations thereof.
  • the stretchable fabric of the present invention may have an elongation of 20-50% and an elongation recovery of 90-97%.
  • the fabric may exhibit only weft-elasticity, or may exhibit elasticity in both directions, where useful stretch and resilience properties appear in both warp and weft yarns.
  • the spandex yarn used as the core yarn of the composite elastic yarn was prepared by the following method. Due to the high temperature in the spinning barrel, the spandex yarn is heated after spinning, and is brought out at an appropriate temperature to impart twist to the yarn. At this time, air is imparted while passing through the first interlace nozzle, and the bonding force between the filaments of the spandex yarn is 870 mg, which falls within the range of the 80D universal spandex bonding force value.
  • the bonding force between the filaments of the spandex yarn was measured to be 40 mg, which is a 5% value of 800 mg, which is the bonding force value of the general-purpose spandex of 80D, by applying low-temperature and low-pressure air while passing through the second air interlace nozzle during the winding process.
  • the DR degree of elongation
  • the fabric was woven using 11 pure cotton yarn for warp.
  • the composite elastic yarn was introduced as weft yarn, and the yarn used for the warp was beamed without additional elongation.
  • the average width of the fabric before washing with water was 144 to 149 cm, and the width of the fabric after washing with water was found to be 120 to 125 cm.
  • the fabric was prepared as a sample through a dyeing process in a conventional method after fabrication by the above process.
  • the bonding force between the filaments of the spandex yarn after passing through the first interlaced nozzle is 880 mg, which falls within the range of the 80D universal spandex bonding force value
  • the bonding force between the filaments of the spandex yarn after passing through the second air interlacing nozzle is It was measured as 14 mg, which is a 2% value of 700 mg, which is the adhesion value of the universal spandex of 80D.
  • the composite elastic yarn and fabric were prepared in the same manner as in Example 1, except that the core yarn was different as described above, and then the physical properties were evaluated and the results are shown together in Table 1.
  • the bonding force between the filaments of the spandex yarn after passing through the first interlace nozzle is 870 mg, which is within the range of the 80D universal spandex bonding force value, and after passing through the second air interlace nozzle, the bonding force between the filaments of the spandex yarn is It was measured as 198 mg, which is a 22% value of 900 mg, which is the adhesion value of the universal spandex of 80D.
  • the composite elastic yarn and fabric were prepared in the same manner as in Example 1, except that the core yarn was different as described above, and then the physical properties were evaluated and the results are shown together in Table 1.
  • Composite elastic yarns and fabrics were prepared in the same manner as in Example 1, except that 50D inelastic fibers and 70D spandex dual-core yarns (120D) were applied as core yarns of the composite elastic yarn, and then the physical properties were evaluated and the results were evaluated. It is shown together in Table 1.
  • the bonding force between the filaments of the spandex yarn after passing through the first interlaced nozzle is 870 mg, which is within the range of the 80D universal spandex bonding force value, and the bonding force between the filaments of the spandex yarn after passing through the second air interlacing nozzle is 80D.
  • Composite elastic yarns and fabrics were prepared in the same manner as in Example 1, except that the adhesive strength of spandex was set to 7 mg, which is a 1% value of 700 mg, and then the physical properties were evaluated and the results are shown in Table 1.
  • the bonding force between the filaments of the spandex yarn is 890 mg, which is within the range of the 80D universal spandex bonding force value, and after passing through the second air interlaced nozzle, the bonding force between the filaments of the spandex yarn is 80D.
  • a composite elastic yarn and a fabric were prepared in the same manner as in Example 1, except that 230 mg, which is a 25.5% value of 900 mg, which is an adhesion value of spandex, and then the physical properties are evaluated, and the results are shown together in Table 1.
  • the bonding force between the filaments in the composite elastic yarn obtained in the examples was measured using a bonding force measuring device (manufactured by Lenzing Instruments GmbH & Co. KG, Vibrodyn 400) according to ASTM D3822-07.
  • the measuring method is a measuring device that measures the tensile strength of one fiber by separating one filament from the yarn with a fingertip and measuring the tensile strength of one fiber by measuring the separated filament and each end of the filaments remaining unseparated. Hang it on Vibrodyn-400, manufactured by Co., Ltd., and measure the force (mg) when the separated filament and the remaining filaments are separated by elongation by stretching at a constant rate of 1,000%/min.
  • the strength and elongation between the filaments in the yarn were measured using an automatic elongation measuring device (manufacturer: Textechno, model name: MEL) with a load cell of 32cN, a sample length of 10 cm, and a tensile speed of 100 cm/min. At this time, the strength and elongation values at break were measured.
  • an automatic elongation measuring device manufactured by Textechno, model name: MEL

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Woven Fabrics (AREA)

Abstract

The present invention relates to: a composite elastic yarn which comprises a core portion composed of elastic core filaments and a sheath portion composed of short fibers and covering the core portion, wherein the elastic core filaments have a low adhesion characteristics in which inter-filament adhesion is in the range of 9 to 198 mg, as measured according to the ASTM D3822 method; fabric; and a method for manufacturing a composite elastic yarn. According to the present invention, the problem of puckering occurring on the surface of a denim fabric can be resolved, thereby providing improved feel and improving the quality of an end product.

Description

복합 탄성사, 신축성 직물, 및 복합 탄성사의 제조방법Composite elastic yarn, stretch fabric, and manufacturing method of composite elastic yarn
본 발명은 복합 탄성사, 신축성 직물, 및 복합 탄성사의 제조방법에 관한 것으로, 더욱 상세하게는 복합 탄성사의 코어사로서 필라멘트 간 합착력이 낮은 저합착 탄성사를 사용하여 원단 형태에서의 퍼커링(puckering) 문제를 해결한 복합 탄성사, 신축성 직물, 및 복합 탄성사의 제조방법에 관한 것이다. The present invention relates to a method of manufacturing a composite elastic yarn, an elastic fabric, and a composite elastic yarn, and more particularly, a puckering in the form of a fabric using a low adhesion elastic yarn having a low adhesion between filaments as a core yarn of the composite elastic yarn. It relates to a composite elastic yarn, an elastic fabric, and a method of manufacturing a composite elastic yarn that solved the problem.
데님용으로 사용되는 신축성 원단의 경우 스판덱스가 코어사로 사용되는 복합 탄성사로 제직된다. 복합 탄성사는 코어부(core section)와 코어부를 커버하는 쉬스부(sheath section)로 구성된다. 일반적으로 데님용 원단 내 복합 탄성사의 코어사는 싱글코어 혹은 듀얼코어 탄성사가 사용되어 데님 직물에 신축성을 부여한다. 싱글 코어는 탄성사 한 가닥이 코어사로 적용되고, 듀얼 코어는 탄성사와 폴리에스테르 이성분 섬유 두 가닥이 코어사로 적용된다. In the case of stretch fabrics used for denim, spandex is woven into composite elastic yarns used as core yarns. The composite elastic yarn is composed of a core section and a sheath section covering the core section. In general, the core yarn of the composite elastic yarn in the denim fabric is used as a single-core or dual-core elastic yarn to give elasticity to the denim fabric. For single core, one elastic yarn is applied as core yarn, and for dual core, elastic yarn and two polyester bicomponent fibers are applied as core yarn.
일례로 미국 특허 제8,093,160호는 탄성 코어사가 하나 이상의 탄성 코어 필라멘트와 하나 이상의 비탄성 코어 필라멘트로 구성된 코어부 및 코어부를 종방향으로 둘러싸는 방식으로 배열된 단섬유의 쉬스부를 포함하는 탄성 코어사와 이러한 탄성 코어사를 포함하는 신축성 데님을 개시하고 있다. 그러나 이러한 기술에 의해 수득되는 신축성 데님은 적절한 수준의 신축성을 제공하지 못하며 단섬유를 포함하는 쉬스부에 사용될 수 있는 사의 두께에 한계가 존재한다.For example, U.S. Patent No. 8,093,160 discloses an elastic core yarn comprising a core portion composed of at least one elastic core filament and at least one inelastic core filament, and a sheath portion of short fibers arranged in a manner surrounding the core portion in a longitudinal direction. Disclosed is an elastic denim containing a core yarn. However, the stretchable denim obtained by this technique does not provide an appropriate level of stretchability, and there is a limit to the thickness of the yarn that can be used in the sheath portion including short fibers.
복합 탄성사 및 그의 제조방법은 널리 공지되어 있다. 예를 들어, 탄성 섬유 코어가 비탄성 섬유로 커버링된 복합 탄성사는 미국 특허 제4,470,250호 제4,998,403호, 제7,134,265호, 제6,848,151호에 기재되어 있다. Composite elastic yarn and its manufacturing method are well known. For example, composite elastic yarns in which the elastic fiber core is covered with inelastic fibers are described in U.S. Patent Nos. 4,470,250 4,998,403, 7,134,265, 6,848,151.
종래의 복합 탄성사로 데님 직물을 제작할 경우에, 얇은 면사가 코어부를 완전하게 덮지 못하고, 쉬스부인 면사와 코어사 간 융착할 수 있는 표면적이 적어 코어사와 면사가 서로 충분히 융착되지 못하는 문제점이 존재한다. 이는 이후 데님 원단 제직 및 가먼트로 제작된 후 복합 탄성사의 코어사가 쉬스부와 분리되어 빠져버리는 슬리피지(slippage) 현상을 유발한다. 슬리피지 현상에 의해 원단 내 탄성을 갖는 코어사가 빠지게 되면, 원단은 표면이 울퉁불퉁하게 오그라진 형태인 퍼커링(puckering) 문제가 발생한다. 데님 직물 표면의 퍼커링 현상은 가먼트 형태의 외관을 저해하여 제품 불량을 야기할 수 있는 요소이므로 데님 원단의 제직 시 퍼커링 문제의 해결이 요구된다.In the case of fabricating a denim fabric with a conventional composite elastic yarn, there is a problem in that the thin cotton yarn does not completely cover the core portion, and the surface area that can be fused between the cotton yarn and the core yarn, which is a sheath portion, is small, so that the core yarn and the cotton yarn cannot be sufficiently fused to each other. This causes a slippage phenomenon in which the core yarn of the composite elastic yarn is separated from the sheath part and then falls out after being made of denim fabric and garment. When the core yarn having elasticity in the fabric is lost due to the slippage phenomenon, the fabric has a puckering problem in which the surface of the fabric is unevenly constricted. The perkering phenomenon on the surface of denim fabric is a factor that can cause product defects by impairing the appearance of the garment, so it is required to solve the perkering problem when weaving denim fabrics.
아직까지 복합 탄성사를 이용한 신축성 원단의 퍼커링 문제를 해결하기 위한 원사 및 직물 생산 기술은 시도된 바가 없다. So far, no attempt has been made to produce yarns and fabrics to solve the problem of perkering of stretchable fabrics using composite elastic yarns.
본 발명은 상술한 종래 기술의 문제를 해소하기 위한 것으로, 본 발명의 하나의 목적은 필라멘트 간 합착력이 낮은 탄성사를 복합 탄성사의 코어부에 적용함으로써, 데님 직물의 표면에 발생하는 퍼커링(puckering) 문제를 해결하는 것이다. The present invention is to solve the problems of the prior art described above, one object of the present invention is by applying an elastic yarn having a low adhesion between filaments to the core portion of the composite elastic yarn, puckering occurring on the surface of the denim fabric. ) To solve the problem.
본 발명의 다른 목적은 코어부를 하나의 단일 보빈으로부터 공급되는 2 가닥 이상의 탄성사로 형성함으로써, 코어사가 사용되는 직물의 높은 신축성 및 현저하게 향상된 탄성회복성을 갖는 복합 탄성사를 제공하는 것이다. Another object of the present invention is to provide a composite elastic yarn having high elasticity and remarkably improved elastic recovery property of a fabric in which the core yarn is used by forming a core portion of two or more elastic yarns supplied from a single bobbin.
본 발명의 또 다른 목적은 신축성 직물의 최종 제품에서 발생하는 퍼커링 문제를 해결하여 제품의 품위를 향상시키고 사용 촉감을 향상시키는 것이다. Another object of the present invention is to improve the quality of the product and improve the feel of use by solving the problem of perkering occurring in the final product of the stretchable fabric.
상술한 과제를 해결하기 위한 본 발명의 하나의 양상은, One aspect of the present invention for solving the above-described problem,
탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사로서, 여기서 탄성 코어 필라멘트는 ASTM D3822 방법으로 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는 것을 특징으로 하는 복합 탄성사에 관한 것이다.A composite elastic yarn comprising a core part composed of an elastic core filament and a sheath part composed of short fibers surrounding the core part, wherein the elastic core filament has an adhesive force between the filaments in the range of 9 to 198 mg as measured by ASTM D3822 method. It relates to a composite elastic yarn, characterized in that it has a low adhesion property.
상기 탄성 코어 필라멘트는 동일한 섬도의 범용 탄성 코어 필라멘트 대비 1.5% 내지 22%의 필라멘트간 합착력을 갖는다.The elastic core filament has an inter-filament adhesion of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness.
상기 코어부는 폴리우레탄, 폴리우레탄-우레아, 또는 폴리우레탄과 폴리우레탄-우레아의 블렌드로 구성될 수 있고, 상기 쉬스부는 양모, 린넨, 실크, 폴리에스테르, 나일론, 올레핀, 면, 텐셀, 모달, 폴리비스코스(poly-viscose) 및 그의 조합으로 이루어진 군으로부터 선택된 경질사로 구성될 수 있다. 본 발명에서 코어사의 섬도가 40 데니어 내지 120 데니어일 수 있다. The core portion may be composed of polyurethane, polyurethane-urea, or a blend of polyurethane and polyurethane-urea, and the sheath portion is wool, linen, silk, polyester, nylon, olefin, cotton, tencel, modal, poly It may be composed of hard yarn selected from the group consisting of viscose (poly-viscose) and combinations thereof. In the present invention, the fineness of the core yarn may be 40 to 120 denier.
본 발명의 다른 양상은, 경사 및 위사 가운데 하나 이상이, 탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사를 포함하고, 여기서 상기 탄성 코어 필라멘트는 ASTM D3822 방법으로 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는 것을 특징으로 하는 직물에 관한 것이다. 본 발명의 직물은 데님용 또는 비데님용으로 이용될 수 있다.Another aspect of the present invention includes a composite elastic yarn in which at least one of the warp and weft yarns includes a core portion composed of an elastic core filament and a sheath portion composed of short fibers surrounding the core portion, wherein the elastic core filament is ASTM It relates to a fabric characterized in that it has a low adhesion property in the range of 9 to 198 mg of adhesion between the filaments as measured by the D3822 method. The fabric of the present invention can be used for denim or non-denim.
본 발명의 또 다른 양상은, 탄성 코어 필라멘트사의 방사 후에 필라멘트간 합착력이 500 내지 1500 mg이 되도록 1차 인터레이싱하고, 이어서 필라멘트간 합착력이 9 내지 198 mg이 되도록 2차 인터레이싱한 후 권취하여 저합착 코어사를 제조하는 단계; 및 전단계에서 수득된 저합착 코어사를 단섬유 로빙사로 피복하여 방적하는 단계를 포함하는 복합 탄성사의 제조방법에 관한 것이다. In another aspect of the present invention, after spinning the elastic core filament yarn, the first interlacing is performed so that the bonding force between the filaments is 500 to 1500 mg, followed by secondary interlacing so that the bonding force between the filaments is 9 to 198 mg. Taking and producing a low adhesion core yarn; And it relates to a method for producing a composite elastic yarn comprising the step of spinning by coating the low-adhesion core yarn obtained in the previous step with a short fiber roving yarn.
상기 1차 인터레이싱 단계에서는 공기 유량을 3~4 L/min로 하고, 온도를 35~30℃로 하여 1차 인터레이싱하고, 2차 인터레이싱 단계에서는 공기 유량을 1~2 L/min로 하고, 온도를 15~20℃로 하여 인터레이싱할 수 있다. In the first interlacing step, the air flow rate is set to 3 to 4 L/min, and the temperature is set to 35 to 30°C for the first interlacing, and in the second interlacing step, the air flow rate is set to 1 to 2 L/min. , Interlacing can be performed by setting the temperature to 15~20℃.
본 발명은 복합 탄성사의 코어부 원사를 단일의 탄성`사로 적용하되, 필라멘트 간 합착력이 낮은 탄성사를 코어사로 사용함으로써, 일반적인 싱글코어사 혹은 듀얼코어사를 코어사로 적용 시 데님 직물 표면에 발생하는 퍼커링 문제를 해결하였다는 점에서 본 발명의 우수한 효과가 있다.The present invention applies the core yarn of the composite elastic yarn as a single elastic yarn, but by using the elastic yarn with low adhesion between the filaments as the core yarn, which occurs on the surface of the denim fabric when a general single-core yarn or dual-core yarn is applied as a core yarn. There is an excellent effect of the present invention in that the perkering problem is solved.
또한 본 발명의 제조방법에 의하면 1차 및 2차 공기 교락 공정이 추가된 방사 공정에 의하여, 복합 탄성사의 원사의 물성 저하 및 필라멘테이션(filamentation)이 발생하지 않으면서 원사 내 필라멘트 가닥 간의 합착력이 낮은 저합착 스판덱스 원사를 제조할 수 있다.In addition, according to the manufacturing method of the present invention, by the spinning process in which the primary and secondary air entanglement processes are added, the bonding force between the filament strands in the yarn without deterioration and filamentation of the yarn properties of the composite elastic yarn occurs. This low adhesion spandex yarn can be produced.
본 발명의 직물은 직물 표면에 발생하는 퍼커링 문제가 개선되어 표면 품위가 향상되고, 그에 따라 사용자에게 쾌적한 사용감을 제공한다. 아울러, 본 발명의 저합착 코어사를 사용해서 얻어지는 최종 제품은 높은 탄성 특성, 현저히 개선된 탄성회복성 특성 및 형상유지 특성을 갖는다.The fabric of the present invention improves the quality of the surface by improving the perkering problem occurring on the fabric surface, thereby providing a user with a comfortable feeling of use. In addition, the final product obtained by using the low bonding core yarn of the present invention has high elastic properties, remarkably improved elastic recovery properties, and shape retention properties.
도 1은 본 발명의 일 실시예에 의한 복합 탄성사의 코어사 제조장치의 개략도이다. 1 is a schematic diagram of an apparatus for manufacturing a core yarn of a composite elastic yarn according to an embodiment of the present invention.
도 2는 본 발명의 일 실시예에 의한 복합 탄성사 제조장치의 개략도이다. 2 is a schematic diagram of an apparatus for manufacturing a composite elastic yarn according to an embodiment of the present invention.
이하에서 첨부 도면을 참조하여 본 발명을 더욱 구체적으로 설명한다.Hereinafter, the present invention will be described in more detail with reference to the accompanying drawings.
본원 및 첨부된 특허청구범위에 사용된 바와 같이, 하기 용어는 하기 정의된다:As used herein and in the appended claims, the following terms are defined below:
본원에서 "필라멘트"는 긴 섬유 가닥을 의미하고, "단섬유(staple fiber)"는 한정된 또는 짧은 길이의 섬유 가닥을 의미한다. As used herein, "filament" means long fiber strands, and "staple fiber" means a limited or short length fiber strand.
본원에서 "탄성 코어 필라멘트"는 100%를 초과하는 파단 연신율을 갖는 필라멘트를 의미하며, 바람직한 예는 스판덱스 섬유이다. As used herein, "elastic core filament" refers to a filament having an elongation at break of more than 100%, and a preferred example is a spandex fiber.
본원에서 사용되는 용어 "복합 탄성사”는 탄성 코어 필라멘트 주위로 섬유를 커버함으로써 제조된 코어-스펀 얀("core-spun yarn")을 의미한다. The term "composite elastic yarn" as used herein refers to a core-spun yarn made by covering fibers around an elastic core filament.
본 발명에서 “필라멘트간 합착력”은 원사 내의 하나의 필라멘트를 1 cm 이상의 길이로 분리한 후 분리된 필라멘트들의 단부를 합착력 측정장치(Lenzing Instruments GmbH & Co. KG사 제품, Vibrodyn 400)에 걸고 일정한 신장률로 신장시켜 섬유의 파단 강도를 ASTM D3822-07 방법(단일 직물 섬유의 인장 성질의 표준 시험 방법(Standard test methods for tensile properties of single textile fibers)")에 따라서 측정한 값(mg)을 의미한다. In the present invention, the "bonding force between filaments" means that one filament in the yarn is separated by a length of 1 cm or more, and then the ends of the separated filaments are hung on a bonding force measuring device (Lenzing Instruments GmbH & Co. KG, Vibrodyn 400). Means the value (mg) measured according to ASTM D3822-07 method (Standard test methods for tensile properties of single textile fibers") by stretching at a constant elongation rate. do.
본 발명의 하나의 양상의 복합 탄성사는 탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사로서, 여기서 탄성 코어 필라멘트는 ASTM D3822 방법으로 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는다. The composite elastic yarn of one aspect of the present invention is a composite elastic yarn comprising a core part composed of an elastic core filament and a sheath part composed of short fibers surrounding the core part, wherein the elastic core filament is measured by the ASTM D3822 method. It has a low adhesion property in which the adhesion force is in the range of 9 to 198 mg.
상기 탄성 코어 필라멘트는 동일한 섬도의 범용 탄성 코어 필라멘트 대비 1.5% 내지 22%의 낮은 합착력을 갖는 저합착 탄성 코어 필라멘트일 수 있다. 예를 들어, 범용적으로 사용되는 스판덱스 80D 원사의 필라멘트 간 합착력은 700~900 mg 수준인데 비해서, 본 발명에 따른 저합착 탄성 코어 필라멘트는 80D의 경우에 약 9 mg 내지 198 mg의 필라멘트간 합착력을 갖는다.The elastic core filament may be a low adhesion elastic core filament having a low adhesion of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness. For example, the adhesive force between the filaments of the spandex 80D yarn, which is commonly used, is at the level of 700 to 900 mg, whereas the low adhesion elastic core filament according to the present invention is the sum of about 9 mg to 198 mg of the filaments in the case of 80D. Have a good fit.
본 발명에서 코어사의 필라멘트간 합착력이 동일 섬도의 범용 스판덱스의 합착력 대비 1.5% 미만인 경우, 과도하게 낮은 합착력으로 인해 원사 내 필라멘트가 분리되는 필라멘테이션 현상이 발생할 수 있다. 한편, 코어사의 필라멘트 간 합착력이 동일 섬도의 범용 스판덱스의 합착력 대비 22%를 초과하는 경우에는, 커버링 공정 중 쉬스부인 면사와 접촉하여 융착될 수 있는 충분한 표면적이 부여되지 못하므로 원단 형태로 제조 시 퍼커링 현상이 발생할 우려가 있다. In the present invention, when the bonding force between the filaments of the core yarn is less than 1.5% of the bonding force of the general-purpose spandex of the same fineness, a filamentation phenomenon in which the filaments in the yarn are separated due to excessively low bonding force may occur. On the other hand, if the bonding force between the filaments of the core yarn exceeds 22% of the bonding strength of the general-purpose spandex of the same fineness, it is not possible to provide a sufficient surface area to be fused by contact with the cotton yarn, which is the sheath part, during the covering process, so it is manufactured in the form of a fabric. There is a risk of perkering.
상기 코어부는 폴리우레탄, 폴리우레탄-우레아, 또는 폴리우레탄과 폴리우레탄-우레아의 블렌드로 구성되는 탄성 코어 필라멘트로 구성될 수 있다. The core portion may be composed of an elastic core filament composed of polyurethane, polyurethane-urea, or a blend of polyurethane and polyurethane-urea.
상기 쉬스부는 천연 섬유, 예컨대, 면, 양모, 린넨, 실크, 텐셀, 모달일 수 있다. 대안으로 쉬스부는 단일 성분의 스테이플 합성섬유일수 있다. 일례로 상기 쉬스부는 폴리에스테르, 나일론, 올레핀, 폴리비스코스(poly-viscose), 아크릴, 모드아크릴, 레이온 및 이들의 임의의 조합으로 이루어진 군으로부터 선택된 섬유일 수 있다. 본 발명에서 쉬스부는 바람직하게 면사를 포함한다. The sheath portion may be a natural fiber such as cotton, wool, linen, silk, tencel, or modal. Alternatively, the sheath portion may be a single component staple synthetic fiber. For example, the sheath portion may be a fiber selected from the group consisting of polyester, nylon, olefin, poly-viscose, acrylic, modacrylic, rayon, and any combination thereof. In the present invention, the sheath portion preferably includes cotton yarn.
본 발명의 복합 탄성사에서 상기 코어사는 섬도가 40 데니어 내지 120 데니어이다. 코어사의 섬도가 40 데니어 미만일 경우, 데님 용도의 일반적인 직물에 비하여 얇은 데님 직물이 형성되어 착용 시 몸매 보정 효과가 미미하고 의복의 태가 좋지 못하다. 한편, 코어사의 섬도가 120 데니어를 초과하는 경우에는, 데님 용도의 일반적인 직물에 비해 두꺼운 데님 직물이 형성되어 뻣뻣하고 무거운 느낌으로 인해 의복 착용감이 저하된다.In the composite elastic yarn of the present invention, the core yarn has a fineness of 40 denier to 120 denier. When the fineness of the core yarn is less than 40 denier, a thin denim fabric is formed compared to the general fabric used for denim, and the effect of correcting the body when worn is insignificant and the appearance of the clothing is poor. On the other hand, when the fineness of the core yarn exceeds 120 denier, a thick denim fabric is formed compared to a general fabric for denim use, and the feeling of wearing clothes is deteriorated due to a stiff and heavy feeling.
본 발명의 다른 양상은 복합 탄성사의 제조방법에 관한 것이다. 본 발명에서는 탄성 코어 필라멘트사의 방사 후에 필라멘트간 합착력이 500 내지 1500 mg이 되도록 1차 인터레이싱하고, 이어서 필라멘트간 합착력이 9 내지 198 mg이 되도록 2차 인터레이싱한 후, 권취하여 저합착 코어사를 제조하고, 이어서 수득된 저합착 코어사를 단섬유 로빙사로 피복하여 방적함으로써 복합 탄성사를 제조할 수 있다.Another aspect of the present invention relates to a method of manufacturing an elastic composite yarn. In the present invention, after spinning the elastic core filament yarn, the first interlacing is performed so that the bonding force between the filaments is 500 to 1500 mg, and then the second interlacing is performed so that the bonding force between the filaments is 9 to 198 mg, and then the low bonding core is wound. A composite elastic yarn can be produced by preparing a yarn, and then coating the obtained low-adhesion core yarn with a short fiber roving yarn and spinning it.
본 발명의 복합 탄성사는 코어사와 쉬스가 방적 장치에서 링 정방(ring spinning) 또는 오픈엔드 정방(open-end spinning)에 의해 방적되어 제조된다.The composite elastic yarn of the present invention is produced by spinning core yarn and sheath by ring spinning or open-end spinning in a spinning machine.
스판덱스 원사는 일반적으로 방사통 내 높은 온도에서 건조 방사에 의해 생산된다. 이 때 스판덱스 원사는 방사 후 열을 받은 상태가 되어 모듈러스가 낮아지고 원사에 꼬임을 부여하기 적절한 온도가 되고, 인출 공정에서 공기 인터레이스 노즐을 통과하여 필라멘트간 합착력을 부여하여 권취를 진행한다. 데님 직물 원단 내 퍼커링 문제를 해결하기 위해 합착력이 낮은 원사를 생산코자 한다면, 원사 방사 공정 중 공기 인터레이스 노즐 에서 부여하는 압력을 낮추어 저합착력의 원사를 생산할 수 있다. 그러나, 위 방사 공정에 의해 원사의 합착력을 낮추게 되면 생산된 원사의 물성 중 강도 저하 문제가 발생하며, 원사 내 필라멘트 가닥들이 분리되는 필라멘테이션(filamentation) 현상이 발생하여 원사 불량 문제를 초래한다.Spandex yarn is generally produced by dry spinning at high temperatures in a spinning barrel. At this time, the spandex yarn is heated after spinning, resulting in a lower modulus and an appropriate temperature for imparting twist to the yarn. In the drawing process, the spandex yarn passes through an air interlaced nozzle to impart adhesion between the filaments to perform winding. If you want to produce yarns with low adhesion to solve the perkering problem in denim fabrics, you can produce yarns with low adhesion by lowering the pressure applied from the air interlacing nozzle during the yarn spinning process. However, when the bonding force of the yarn is lowered by the above spinning process, a problem of strength reduction occurs among the physical properties of the produced yarn, and a filamentation phenomenon occurs in which the filament strands in the yarn are separated, resulting in a yarn defect problem. .
본 발명에서는 코어사의 방사 공정 내 합착력을 부여하는 공기 인터레이스 노즐(이하 “인터레이스 노즐”이라 함)을 기존 하나의 인터레이스 노즐을 사용하는 방사 공정에서 2단계로 합착력을 부여할 수 있는 제1 및 제2 인터레이스 노즐을 방사 공정에 적용함으로써 최종 원단에서의 퍼커링 문제를 해결할 수 있다. In the present invention, the air interlaced nozzle (hereinafter referred to as “interlace nozzle”) that imparts adhesion in the spinning process of the core yarn is used as the first and second capable of imparting adhesion in two steps in the spinning process using one existing interlaced nozzle. By applying the second interlaced nozzle to the spinning process, it is possible to solve the problem of perkering in the final fabric.
제1 인터레이스 노즐(14)은 기존 스판덱스의 방사 공정과 동일한 방법으로 압력과 온도를 조절하여 공기로 원사를 통과시킨다. 일반적인 인터레이스 노즐 공기의 유량은 3~4 L/min, 온도는 35~30℃이며, 본 발명에 의한 제1 인터레이스 노즐(14)의 공기 유량 및 온도는 상기 언급한 기존 조건과 동일하였다. 제1 인터레이스 노즐(14)에서 공기를 부여할 때에는 원사는 크게 두 가닥의 필라멘트 가닥들로 합착될 수 있도록 조절한다.The first interlaced nozzle 14 controls the pressure and temperature in the same way as the spinning process of the existing spandex, and passes the yarn through the air. The flow rate of air in the general interlaced nozzle is 3 to 4 L/min, and the temperature is 35 to 30° C., and the air flow rate and temperature of the first interlaced nozzle 14 according to the present invention were the same as the above-mentioned existing conditions. When air is supplied from the first interlace nozzle 14, the yarn is adjusted so that it can be bonded to two large filament strands.
본 발명에서 제2 인터레이스 노즐(15)은 제1 인터레이스 노즐을 통과한 원사 가닥을 저온 및 저압의 공기를 부여한 채 통과시킴으로써 저합착력을 갖는 저합착 탄성 코어 필라멘트를 최종적으로 생산하게 된다. 보다 구체적으로, 제1 인터레이스 노즐(14)을 통과한 원사는 크게 두 가닥의 필라멘트 가닥들로 합착된 형태로 존재하며, 이 원사를 제2 인터레이스 노즐(15)에서 유량 1~2 L/min 및 온도 15~20℃의 공기로 통과시켜 두 개의 필라멘트 가닥 간 매우 낮은 합착력을 부여하도록 생산된다. 예를 들어, 80 데니어/6 필라멘트의 제품의 경우, 제1 인터레이스 노즐(14)을 통과한 뒤 40 데니어/3 필라멘트 두 가닥이 되고, 제2 인터레이스 노즐(15)에서 저온 및 저압의 공기를 통과하면서 두 가닥 간 낮은 합착력이 부여된다. 상기 설명한 1차 및 2차에 걸친 공기 인터레이스 노즐이 포함된 방사 공정에 의하여, 스판덱스 원사의 물성 저하 및 필라멘테이션이 발생하지 않으면서 원사 내 필라멘트 가닥 간의 합착력이 낮은 저합착 스판덱스 원사가 제조될 수 있다.In the present invention, the second interlaced nozzle 15 finally produces a low adhesion elastic core filament having a low adhesion by passing the yarn strands passing through the first interlaced nozzle while applying low temperature and low pressure air. More specifically, the yarn that has passed through the first interlaced nozzle 14 exists in a form of largely bonded to two filament strands, and the yarn is fed from the second interlaced nozzle 15 at a flow rate of 1 to 2 L/min and It is produced to give very low adhesion between two filament strands by passing it through air at a temperature of 15~20℃. For example, in the case of an 80 denier/6 filament product, after passing through the first interlaced nozzle 14, it becomes two 40 denier/3 filaments, and passes through low-temperature and low-pressure air through the second interlace nozzle 15. While doing so, low adhesion is imparted between the two strands. By the spinning process including the first and second air interlaced nozzles described above, a low adhesion spandex yarn having low adhesion between filament strands in the yarn without deterioration of properties and filamentation of the spandex yarn will be produced. I can.
저합착 탄성 코어 필라멘트(21)는 코어사 제조장치(10)에 의해 얻어지며, 복합 탄성사(40)는 복합 탄성사 방적장치(30)에 의해 얻어진다.The low bonding elastic core filament 21 is obtained by the core yarn manufacturing apparatus 10, and the composite elastic yarn 40 is obtained by the complex elastic yarn spinning apparatus 30.
도 1은 본 발명의 일 실시예의 복합 탄성사의 코어사 제조장치를 개략적으로 도시한 것이다. 도 1을 참조하면, 저합착 탄성 코어 필라멘트(21)를 얻기 위해 사용되는 코어사 제조장치(10)는 기본적으로 건식 방사 유닛(11), 건식 방사 유닛(11)에 연속하여 제공된 안내 실린더(12), 오일 픽업 롤러 (13), 권취장치(16), 및 상기 권취장치(16)와 관련된 보빈(17)을 포함한다. 1 schematically shows an apparatus for manufacturing a core yarn of a composite elastic yarn according to an embodiment of the present invention. Referring to FIG. 1, the core yarn manufacturing apparatus 10 used to obtain the low bonding elastic core filament 21 is basically a dry spinning unit 11, a guide cylinder 12 continuously provided to the dry spinning unit 11 ), an oil pickup roller 13, a take-up device 16, and a bobbin 17 associated with the take-up device 16.
저합착 탄성 코어 필라멘트(21)를 제조하기 위해서는 먼저 건식방사유닛(11)에서 폴리우레탄우레아 중합체를 탄성사(20) 형태로 방사한다. 이어서 얻어진 탄성사(20)는 오일 픽업 롤러(13)를 통과하여 안내 실린더(12)에 의해 제1 인터레이스 노즐(14)과 제2 인터레이스 노즐(15)을 통과하여 권취장치(16)로 전달된다. 오일 픽업 롤러(13)는 탄성사(20)를 적절하게 권취하기 위해 발진 및 진동 없이 탄성사(20)를 전달한다. 권취장치(16)로 전달되는 탄성사(20)는 보빈(17)에 권취된다.In order to manufacture the low-adhesion elastic core filament 21, the polyurethaneurea polymer is first spun in the form of an elastic yarn 20 in the dry spinning unit 11. Subsequently, the obtained elastic yarn 20 passes through the oil pickup roller 13, passes through the first interlace nozzle 14 and the second interlace nozzle 15 by the guide cylinder 12, and is transferred to the take-up device 16. The oil pickup roller 13 transfers the elastic yarn 20 without oscillation and vibration in order to properly wind the elastic yarn 20. The elastic yarn 20 transmitted to the take-up device 16 is wound on the bobbin 17.
이어서 저합착 탄성 코어 필라멘트(21)가 권취된 보빈(17)은, 도 2에 개략적으로 도시한 바와 같이, 복합 탄성사 방적장치(30)에 공급된다. 복합 탄성사 방적장치(30)는 기본적으로 로빙사(31), 상기 로빙사(31)이 통과하는 사 인출 실린더(32), 얇은 로빙사(31) 및 보빈(17)으로부터 얻어진 저합착 탄성 코어 필라멘트(21)이 함께 공급되는 안내 전방 실린더(33), 상기 안내 전방 실린더(33)와 연속하여 제공되는 사 가이드(34) 및 방사 유닛(35)을 포함한다. 상기 방사 유닛(35)은 링(351), 이동 유닛(352) 및 콥(cop, 353)을 포함한다. 사 인출 실린더(32) 사이로 로빙사(31)을 통과시키고, 저합착 탄성 코어 필라멘트(21)를 보빈(17)으로부터 안내 전방 실린더(33)로 공급하고, 인출된 로빙사(31)과 결합하고, 사 가이드(34)로부터 얇은 로빙사(31)와 저합착 탄성 코어 필라멘트(21)를 공급하여 원활한 흐름을 제공하고, 방사 유닛(35)으로 배향하고, 방사 유닛(35)에서 링(351)과 사 이동 유닛(352)을 함께 작동시켜 얇은 로빙사(31)를 저합착 탄성 코어 필라멘트(21)에 권취하며, 콥(353) 상에 방사 및 권취하여 복합 탄성사(40)를 제조할 수 있다. Subsequently, the bobbin 17 on which the low bonding elastic core filament 21 is wound is supplied to the composite elastic yarn spinning device 30, as schematically shown in FIG. 2. The composite elastic yarn spinning device 30 is basically a low-cohesion elastic core filament obtained from a roving yarn 31, a yarn drawing cylinder 32 through which the roving yarn 31 passes, a thin roving yarn 31, and a bobbin 17. It includes a guide front cylinder 33 supplied with 21, a yarn guide 34 provided continuously with the guide front cylinder 33, and a spinning unit 35. The spinning unit 35 includes a ring 351, a moving unit 352 and a cop 353. Passing the roving yarn 31 between the yarn drawing cylinders 32, supplying the low bonding elastic core filament 21 from the bobbin 17 to the guiding front cylinder 33, and combining with the drawn roving yarn 31 , The thin roving yarn 31 and the low adhesion elastic core filament 21 are supplied from the yarn guide 34 to provide a smooth flow, and the spinning unit 35 is oriented, and the spinning unit 35 to the ring 351 By operating the yarn moving unit 352 together, the thin roving yarn 31 is wound on the low bonding elastic core filament 21, and the composite elastic yarn 40 can be manufactured by spinning and winding on the cob 353. .
이러한 과정에 의해서 코어-쉬스 구조의 복합 탄성사를 수득할 수 있다. 이러한 과정에 의해서 수득되는 복합 탄성사는 저합착 탄성 코어 필라멘트(21) 상에 로빙사(31)가 커버되는 구조이다. 본 발명에서는 코어부에 사용되는 탄성사(20)는 단일의 보빈에서 공급되는 2-엔드 이상의 탄성사로 제조된다. 이와 같이 코어부에 단일의 보빈으로부터 제공된 스판덱스와 같은 탄성사를 함유하는 복수의 엔드를 사용하면, 코어사가 사용되는 직물과 같은 최종 제품에서 탄성 및 탄성회복률이 향상될 수 있다. Through this process, a composite elastic yarn having a core-sheath structure can be obtained. The composite elastic yarn obtained by this process has a structure in which the roving yarn 31 is covered on the low adhesion elastic core filament 21. In the present invention, the elastic yarn 20 used in the core portion is made of two-end or more elastic yarns supplied from a single bobbin. In this way, when a plurality of ends containing elastic yarns such as spandex provided from a single bobbin are used in the core portion, elasticity and elastic recovery rate can be improved in a final product such as a fabric in which the core yarn is used.
높은 탄성을 제공하기 위해 개별적인 보빈으로부터 코어사 구조에 포함되는 탄성사(20)를 공급하게 되면 스판덱스 사이에 장력 차이가 유발되며, 이에 따라 불균일한 코어사 구조가 형성된다. 본 발명에 따라 개시된 코어사에서 높은 탄성이 코어부의 단일 보빈(17)으로부터 다수의 엔드로 제공된 다수의 탄성사(20) 성분에 의해 달성된다. 따라서, 높은 균일성이 있는 코어사를 얻는 것이 가능하다.In order to provide high elasticity, when the elastic yarn 20 included in the core yarn structure is supplied from an individual bobbin, a difference in tension between the spandex is caused, thereby forming an uneven core yarn structure. In the core yarn disclosed according to the present invention, high elasticity is achieved by a component of a plurality of elastic yarns 20 provided from a single bobbin 17 of the core portion to a plurality of ends. Therefore, it is possible to obtain a core yarn with high uniformity.
본 발명의 또 다른 양상은 신축성 직물에 관한 것이다. 본 발명의 직물은 경사 및 위사 가운데 하나 이상이, 탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사를 포함하고, 여기서 상기 탄성 코어 필라멘트는 ASTM D3822 방법으로 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는 것을 특징으로 한다. 본 발명의 직물은 데님용 또는 비데님용 직물로 용도 전개가 가능하다. Another aspect of the present invention relates to an elastic fabric. The fabric of the present invention includes a composite elastic yarn in which at least one of the warp and weft yarns includes a core portion composed of an elastic core filament and a sheath portion composed of short fibers surrounding the core portion, wherein the elastic core filament is the ASTM D3822 method It is characterized in that it has a low adhesion property in the range of 9 to 198 mg of adhesion between filaments when measured as. The fabric of the present invention can be used as a fabric for denim or non-denim.
본 발명의 복합 탄성사는 직물, 편물, 부직포 등의 제작에 이용될 수 있는데, 바람직하게 데님용 신축성 직물에 이용될 수 있다. 여기서 직물은 평직, 포플린(poplin), 트윌(twill), 옥스포드(oxford), 도비(dobby), 새틴(sateen), 사틴(satin) 및 그의 조합을 포함하는 다양한 직조 패턴으로 제조될 수 있다. The composite elastic yarn of the present invention may be used in the manufacture of fabrics, knitted fabrics, non-woven fabrics, and the like, and may be preferably used in stretch fabrics for denim. Here, the fabric can be made in a variety of weaving patterns including plain weave, poplin, twill, oxford, dobby, satin, satin, and combinations thereof.
본 발명의 신축성 직물은 신장율이 20∼50%이고, 신장회복율이 90∼97%일 수 있다. 직물은 위사-신축성만을 나타낼 수 있거나, 또는 양방향으로 신축성을 나타낼 수 있고, 여기서 유용한 신축성 및 탄성회복성 특성은 경사 및 위사 양방향 모두에서 나타난다.The stretchable fabric of the present invention may have an elongation of 20-50% and an elongation recovery of 90-97%. The fabric may exhibit only weft-elasticity, or may exhibit elasticity in both directions, where useful stretch and resilience properties appear in both warp and weft yarns.
이하, 실시예를 들어 본 발명에 대해서 상세히 설명한다. 이러한 실시예들은 단지 본 발명을 예시하기 위한 것으로, 이하의 실시예들은 본 발명의 범위를 제한하는 것으로 해석되어서는 안 된다. Hereinafter, the present invention will be described in detail by way of examples. These examples are for illustrative purposes only, and the following examples should not be construed as limiting the scope of the present invention.
실시예Example
실시예Example 1 One
복합 탄성사의 코어사로 사용된 스판덱스 원사를 아래의 방법으로 제조하였다. 방사통 내 높은 온도에 의해 스판덱스 원사는 방사 후 열을 받은 상태가 되어, 원사에 꼬임을 부여하기 적절한 온도가 되어 인출된다. 이 때, 제1 인터레이스 노즐을 통과하면서 공기를 부여하고, 스판덱스 원사의 필라멘트 간 합착력은 80D 범용 스판덱스 합착력 값의 범위에 속하는 870 mg이 형성된다. 이후 권취 과정 중 제2 공기 인터레이스 노즐을 통과하면서 저온 및 저압의 공기를 부여하여 스판덱스 원사의 필라멘트 간 합착력은 80D의 범용 스판덱스의 합착력 값인 800 mg의 5% 값인 40 mg으로 측정되었다.The spandex yarn used as the core yarn of the composite elastic yarn was prepared by the following method. Due to the high temperature in the spinning barrel, the spandex yarn is heated after spinning, and is brought out at an appropriate temperature to impart twist to the yarn. At this time, air is imparted while passing through the first interlace nozzle, and the bonding force between the filaments of the spandex yarn is 870 mg, which falls within the range of the 80D universal spandex bonding force value. Thereafter, the bonding force between the filaments of the spandex yarn was measured to be 40 mg, which is a 5% value of 800 mg, which is the bonding force value of the general-purpose spandex of 80D, by applying low-temperature and low-pressure air while passing through the second air interlace nozzle during the winding process.
경질사로 면사 16 수 원사를 사용하고, 위에서 제조된 저합착 탄성 코어 필라멘트를 코어사로 사용하였다. 복합 탄성사 중 위사에 사용된 복합 탄성사를 제조하기 위한 스판덱스의 DR(신장 정도)은 3.5 배로 제조되었다. 16 cotton yarn was used as the hard yarn, and the low adhesion elastic core filament prepared above was used as the core yarn. Among the composite elastic yarns, the DR (degree of elongation) of the spandex for manufacturing the composite elastic yarn used for the weft was 3.5 times.
경사는 순면 11수 방적사를 사용하여 원단을 제직하였다. 해당 복합 탄성사를 이용하여 원단 제직 시 복합 탄성사는 위사로 투입되었으며, 경사에 투입하는 방적사는 별도의 신장 없이 비밍(beaming)하여 사용하였다. 상기 복합 탄성사를 사용하여 능직 원단 제조 후, 원단의 수세 전 직물의 폭은 평균 144 ~ 149 cm, 수세 후 직물의 폭은 120 ~ 125 cm로 확인되었다. 원단은 위 공정으로 원단 제조 후 통상의 방법으로 염색 공정을 거쳐 샘플로 준비하였다. The fabric was woven using 11 pure cotton yarn for warp. When weaving the fabric using the composite elastic yarn, the composite elastic yarn was introduced as weft yarn, and the yarn used for the warp was beamed without additional elongation. After the twill fabric was manufactured using the composite elastic yarn, the average width of the fabric before washing with water was 144 to 149 cm, and the width of the fabric after washing with water was found to be 120 to 125 cm. The fabric was prepared as a sample through a dyeing process in a conventional method after fabrication by the above process.
복합 탄성사의 코어사의 원사 특성 및 원단 형태에서의 퍼커링 발생 여부를 평가하여 하기 표 1에 나타내었다. The properties of the core yarn of the composite elastic yarn and the occurrence of perkering in the fabric form were evaluated and shown in Table 1 below.
실시예Example 2 2
데님 직물 제조를 위한 복합 탄성사의 코어사로 필라멘트 간 합착력이 낮은 탄성사를 적용하였다. 이 때, 제1 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 범용 스판덱스 합착력 값의 범위에 속하는 880 mg이고, 제2 공기 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 의 범용 스판덱스의 합착력 값인 700 mg의 2% 값인 14 mg으로 측정되었다.An elastic yarn with low adhesion between filaments was applied as the core yarn of the composite elastic yarn for the fabrication of denim fabric. At this time, the bonding force between the filaments of the spandex yarn after passing through the first interlaced nozzle is 880 mg, which falls within the range of the 80D universal spandex bonding force value, and the bonding force between the filaments of the spandex yarn after passing through the second air interlacing nozzle is It was measured as 14 mg, which is a 2% value of 700 mg, which is the adhesion value of the universal spandex of 80D.
위와 같이 코어사를 달리한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. The composite elastic yarn and fabric were prepared in the same manner as in Example 1, except that the core yarn was different as described above, and then the physical properties were evaluated and the results are shown together in Table 1.
실시예Example 3 3
데님 직물 제조를 위한 복합 탄성사의 코어사로 필라멘트 간 합착력이 낮은 탄성사를 적용하였다. 이 때, 제1 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 범용 스판덱스 합착력 값의 범위에 속하는 870 mg이고, 제2 공기 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 의 범용 스판덱스의 합착력 값인 900 mg의 22% 값인 198 mg으로 측정되었다.An elastic yarn with low adhesion between filaments was applied as the core yarn of the composite elastic yarn for the fabrication of denim fabric. At this time, the bonding force between the filaments of the spandex yarn after passing through the first interlace nozzle is 870 mg, which is within the range of the 80D universal spandex bonding force value, and after passing through the second air interlace nozzle, the bonding force between the filaments of the spandex yarn is It was measured as 198 mg, which is a 22% value of 900 mg, which is the adhesion value of the universal spandex of 80D.
위와 같이 코어사를 달리한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. The composite elastic yarn and fabric were prepared in the same manner as in Example 1, except that the core yarn was different as described above, and then the physical properties were evaluated and the results are shown together in Table 1.
비교예Comparative example 1 One
데님 직물 제조를 위한 복합 탄성사의 코어사로 제1, 제2 공기 인터레이스 노즐을 거치지 않고 제1 인터레이스 노즐만을 통과하여 제조되는 범용 스판덱스 80D를 사용한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. Composite elastic yarn and composite elastic yarn in the same manner as in Example 1, except that the general-purpose spandex 80D manufactured by passing only the first interlaced nozzle without passing through the first and second air interlacing nozzles was used as the core yarn of the composite elastic yarn for the fabrication of denim fabric. After preparing the fabric, the physical properties were evaluated and the results are shown together in Table 1.
비교예Comparative example 2 2
복합 탄성사의 코어사로 50D의 비탄성 섬유와 70D의 스판덱스의 듀얼코어사(120D)를 적용한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. Composite elastic yarns and fabrics were prepared in the same manner as in Example 1, except that 50D inelastic fibers and 70D spandex dual-core yarns (120D) were applied as core yarns of the composite elastic yarn, and then the physical properties were evaluated and the results were evaluated. It is shown together in Table 1.
비교예Comparative example 3 3
제1 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 범용 스판덱스 합착력 값의 범위에 속하는 870 mg이고, 제2 공기 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D의 범용 스판덱스의 합착력 값인 700 mg의 1% 값인 7 mg로 한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. The bonding force between the filaments of the spandex yarn after passing through the first interlaced nozzle is 870 mg, which is within the range of the 80D universal spandex bonding force value, and the bonding force between the filaments of the spandex yarn after passing through the second air interlacing nozzle is 80D. Composite elastic yarns and fabrics were prepared in the same manner as in Example 1, except that the adhesive strength of spandex was set to 7 mg, which is a 1% value of 700 mg, and then the physical properties were evaluated and the results are shown in Table 1.
비교예Comparative example 4 4
제1 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D 범용 스판덱스 합착력 값의 범위에 속하는 890 mg이고, 제2 공기 인터레이스 노즐을 통과한 뒤 스판덱스 원사의 필라멘트 간 합착력은 80D의 범용 스판덱스의 합착력 값인 900 mg의 25.5% 값인 230 mg으로 한 것을 제외하고는 실시예 1과 동일하게 실시하여 복합 탄성사 및 직물을 제조한 후, 물성을 평가하여 그 결과를 표 1에 함께 나타내었다. After passing through the first interlaced nozzle, the bonding force between the filaments of the spandex yarn is 890 mg, which is within the range of the 80D universal spandex bonding force value, and after passing through the second air interlaced nozzle, the bonding force between the filaments of the spandex yarn is 80D. A composite elastic yarn and a fabric were prepared in the same manner as in Example 1, except that 230 mg, which is a 25.5% value of 900 mg, which is an adhesion value of spandex, and then the physical properties are evaluated, and the results are shown together in Table 1.
시험예Test example
실시예 및 비교예에서 수득된 복합 탄성사 및 원단의 물성을 아래와 같은 방법으로 평가하였다. 측정 범위 오차를 고려하여 20개의 샘플을 각각 측정하고 최고값과 최저값을 제외한 중간값들의 평균값을 구하였다. 이때 각 시험편은 23℃ 및 65% 상대적 습도에서 14 시간 동안 컨디셔닝 후에 평가하였다. The physical properties of the composite elastic yarn and fabric obtained in Examples and Comparative Examples were evaluated in the following manner. Each of the 20 samples was measured in consideration of the measurement range error, and the average value of the median values excluding the highest and lowest values was calculated. At this time, each test piece was evaluated after conditioning at 23° C. and 65% relative humidity for 14 hours.
[섬유의 합착력 평가 방법][Method of evaluating the adhesion of fibers]
실시예에서 수득된 복합 탄성사 내 필라멘트 간 합착력은 ASTM D3822-07에 준하여 합착력 측정장치(Lenzing Instruments GmbH & Co. KG사 제품, Vibrodyn 400)를 이용하여 측정하였다. 측정 방법은 원사에서 손끝으로 하나의 필라멘트를 분리하여 약 1cm 이상의 길이가 되면, 분리된 한 가닥의 필라멘트와 분리되지 않고 남아 있는 필라멘트들의 각 끝을 하나의 섬유의 인장강도를 측정하는 측정기기 (LENZING사제, Vibrodyn- 400)에 걸어, 1,000%/분의 일정한 속도로 신장시켜 분리된 한 가닥의 필라멘트와 남아있는 필라멘트들이 신장에 의하여 분리될 때 힘(mg)을 측정한다.The bonding force between the filaments in the composite elastic yarn obtained in the examples was measured using a bonding force measuring device (manufactured by Lenzing Instruments GmbH & Co. KG, Vibrodyn 400) according to ASTM D3822-07. The measuring method is a measuring device that measures the tensile strength of one fiber by separating one filament from the yarn with a fingertip and measuring the tensile strength of one fiber by measuring the separated filament and each end of the filaments remaining unseparated. Hang it on Vibrodyn-400, manufactured by Co., Ltd., and measure the force (mg) when the separated filament and the remaining filaments are separated by elongation by stretching at a constant rate of 1,000%/min.
[섬유의 강도 및 신도 평가 방법][Fiber strength and elongation evaluation method]
원사 내 필라멘트 간 강도 및 신도를 자동 강신도 측정장치(제조사: Textechno, 모델명: MEL)를 이용하여 load cell 32cN, 시료 길이 10cm, 인장속도 100 cm/min로 하여 측정하였다. 이때, 파단 시의 강도와 신도 값을 측정하였다. The strength and elongation between the filaments in the yarn were measured using an automatic elongation measuring device (manufacturer: Textechno, model name: MEL) with a load cell of 32cN, a sample length of 10 cm, and a tensile speed of 100 cm/min. At this time, the strength and elongation values at break were measured.
[퍼커링 발생 유무][Presence or absence of percussion]
원단 제직 후 육안으로 퍼커링의 발생 여부를 평가하였다. After weaving the fabric, it was evaluated whether perkering occurred with the naked eye.
[규칙 제91조에 의한 정정 18.06.2020] 
Figure WO-DOC-TABLE-1
[Amendment 18.06.2020 pursuant to Rule 91]
Figure WO-DOC-TABLE-1
상기 표 1의 결과를 통해서 확인되는 바와 같이, 본 발명의 복합 탄성사를 적용한 경우에는 원단에서 퍼커링이 발생하지 않았고, 탄성회복률도 우수하였다. 이에 비해서 비교예 1, 2 및 4의 경우에는 퍼커링이 발생하였고, 비교예 3에서는 원사의 사절이 다수 발생하여 직물 제조 및 물성 평가가 불가능하였다. As can be seen from the results of Table 1, when the composite elastic yarn of the present invention was applied, perkering did not occur in the fabric, and the elastic recovery rate was also excellent. On the contrary, in Comparative Examples 1, 2 and 4, perkering occurred, and in Comparative Example 3, many yarn threading occurred, making fabric manufacturing and physical property evaluation impossible.
이상에서 본 발명의 바람직한 구현예에 대해서 상세하게 설명하였으나, 이러한 설명은 단지 예시를 위한 것으로, 통상의 기술자들은 본 발명의 취지를 벗어남 없이 변형 및 변경이 이루어질 수 있다는 것을 인지할 것이며, 이러한 모든 변형 및 변경은 본 발명의 진정한 권리범위에 속하는 것으로 포함되도록 의도된다.Although the preferred embodiments of the present invention have been described in detail above, these descriptions are for illustrative purposes only, and those skilled in the art will recognize that modifications and changes can be made without departing from the spirit of the present invention, and all such modifications And changes are intended to be included as belonging to the true scope of the present invention.

Claims (10)

  1. 탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사로서, 여기서 탄성 코어 필라멘트는 ASTM D3822 방법에 준하여 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는 것을 특징으로 하는 복합 탄성사. A composite elastic yarn comprising a core part composed of an elastic core filament and a sheath part composed of short fibers surrounding the core part, wherein the elastic core filament has a bonding force between the filaments in the range of 9 to 198 mg when measured according to ASTM D3822 method. Composite elastic yarn, characterized in that it has low adhesion resistance.
  2. 제1항에 있어서, 상기 탄성 코어 필라멘트는 동일한 섬도의 범용 탄성 코어 필라멘트 대비 1.5% 내지 22%의 필라멘트간 합착력을 갖는 것을 특징으로 하는 복합 탄성사. The composite elastic yarn of claim 1, wherein the elastic core filament has an inter-filament bonding force of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness.
  3. 제1항에 있어서, 상기 코어부는 폴리우레탄, 폴리우레탄-우레아, 또는 폴리우레탄과 폴리우레탄-우레아의 블렌드로 구성되는 것을 특징으로 하는 복합 탄성사.The composite elastic yarn according to claim 1, wherein the core part is composed of polyurethane, polyurethane-urea, or a blend of polyurethane and polyurethane-urea.
  4. 제1항에 있어서, 상기 쉬스부는 양모, 린넨, 실크, 폴리에스테르, 나일론, 올레핀, 면, 텐셀, 모달, 폴리비스코스(poly-viscose) 및 그의 조합으로 이루어진 군으로부터 선택된 것인 복합 탄성사.The composite elastic yarn of claim 1, wherein the sheath portion is selected from the group consisting of wool, linen, silk, polyester, nylon, olefin, cotton, tencel, modal, poly-viscose, and combinations thereof.
  5. 제1항에 있어서, 상기 코어사의 섬도가 40 데니어 내지 120 데니어인 것을 특징으로 하는 복합 탄성사.The composite elastic yarn according to claim 1, wherein the core yarn has a fineness of 40 denier to 120 denier.
  6. 제1항에 있어서, 상기 탄성 코어 필라멘트는 권취되기 전에 2차례 인터레이싱 되고, 2차 인터레이싱에서 1차 인터레이싱 단계보다 적은 압력 및 낮은 온도에서 공기 교락하여 제조되는 것임을 특징으로 하는 복합 탄성사. The composite elastic yarn according to claim 1, wherein the elastic core filaments are interlaced twice before being wound, and are produced by interlacing air at a lower pressure and lower temperature than in the first interlacing step in the second interlacing.
  7. 경사 및 위사 가운데 하나 이상이, 탄성 코어 필라멘트로 구성되는 코어부와 상기 코어부를 감싸는 단섬유로 구성되는 쉬스부를 포함하는 복합 탄성사를 포함하고, 여기서 상기 탄성 코어 필라멘트는 ASTM D3822 방법에 준하여 측정 시에 필라멘트간 합착력이 9 내지 198 mg의 범위 내인 저합착 특성을 갖는 것을 특징으로 하는 직물. At least one of the warp and weft includes a composite elastic yarn including a core portion composed of an elastic core filament and a sheath portion composed of short fibers surrounding the core portion, wherein the elastic core filament is measured according to ASTM D3822 method. A fabric, characterized in that it has low adhesion properties in the range of 9 to 198 mg of adhesion between filaments.
  8. 탄성 코어 필라멘트사의 방사 후에 필라멘트간 합착력이 500 내지 1500 mg이 되도록 1차 인터레이싱하고, 이어서 필라멘트간 합착력이 9 내지 198 mg이 되도록 2차 인터레이싱한 후, 권취하여 저합착 코어사를 제조하는 단계; 및 전단계에서 수득된 저합착 코어사를 단섬유 로빙사로 피복하여 방적하는 단계를 포함하는 복합 탄성사의 제조방법. After spinning the elastic core filament yarn, the first interlacing was performed so that the bonding force between the filaments was 500 to 1500 mg, followed by secondary interlacing so that the bonding force between the filaments was 9 to 198 mg, and then wound to produce a low bonding core yarn. The step of doing; And coating and spinning the low-adhesion core yarn obtained in the previous step with a short fiber roving yarn.
  9. 제8항에 있어서, 상기 방법은 공기 유량을 3~4 L/min로 하고, 온도를 35~30℃로 하여 제1 인터레이스 노즐에서 1차 인터레이싱하고, 이어서 공기 유량을 1~2 L/min로 하고, 온도를 15~20℃로 하여 제2 인터레이스 노즐에서 2차 인터레이싱하는 단계를 포함하는 것을 특징으로 하는 복합 탄성사의 제조방법. The method according to claim 8, wherein the air flow rate is 3 to 4 L/min, the temperature is 35 to 30°C, and the first interlacing is performed at the first interlacing nozzle, and then the air flow rate is 1 to 2 L/min. And performing secondary interlacing in a second interlaced nozzle at a temperature of 15 to 20°C.
  10. 제8항에 있어서, 상기 탄성 코어 필라멘트는 동일한 섬도의 범용 탄성 코어 필라멘트 대비 1.5% 내지 22%의 필라멘트간 합착력을 갖도록 제조하는 것을 사용하는 것을 특징으로 하는 복합 탄성사의 제조방법. [10] The method of claim 8, wherein the elastic core filament is manufactured to have an adhesion between the filaments of 1.5% to 22% compared to a general-purpose elastic core filament having the same fineness.
PCT/KR2020/006160 2019-11-14 2020-05-11 Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn WO2021096008A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US17/766,399 US20240011200A1 (en) 2019-11-14 2019-05-11 Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn
BR112022007993A BR112022007993A2 (en) 2019-11-14 2020-05-11 COMPOSITE ELASTIC YARN, EXTENSIVE FABRIC AND METHOD TO MANUFACTURE COMPOSITE ELASTIC YARN
CN202080074607.8A CN114599829B (en) 2019-11-14 2020-05-11 Composite elastic yarn, stretchable fabric, and method for producing composite elastic yarn
EP20888510.3A EP4060103A4 (en) 2019-11-14 2020-05-11 Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR10-2019-0146071 2019-11-14
KR1020190146071A KR102171832B1 (en) 2019-11-14 2019-11-14 Composite elastic yarns, fabric and preparation method of the composite elastic yarn

Publications (1)

Publication Number Publication Date
WO2021096008A1 true WO2021096008A1 (en) 2021-05-20

Family

ID=73048292

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/KR2020/006160 WO2021096008A1 (en) 2019-11-14 2020-05-11 Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn

Country Status (6)

Country Link
US (1) US20240011200A1 (en)
EP (1) EP4060103A4 (en)
KR (1) KR102171832B1 (en)
CN (1) CN114599829B (en)
BR (1) BR112022007993A2 (en)
WO (1) WO2021096008A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114150410A (en) * 2021-10-26 2022-03-08 浙江龙仕达科技股份有限公司 Full dull spandex covering yarn

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112064159B (en) * 2020-09-18 2022-08-09 山东黄河三角洲纺织科技研究院有限公司 Flax fiber blended yarn and production process thereof
KR102446940B1 (en) * 2021-08-04 2022-09-26 (주)신진텍스 Indigo fabric and manufacturing method

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4470250A (en) 1981-07-02 1984-09-11 Bayer Aktiengesellschaft Elastic covered yarn
US4998403A (en) 1990-02-01 1991-03-12 Basf Corporation Apparatus and method of covering spandex yarn
KR19990057610A (en) * 1997-12-30 1999-07-15 조정래 Manufacturing method of polyester biaxial blended yarn
JP2001279550A (en) * 2000-03-30 2001-10-10 Toray Ind Inc False twisted covered elastic yarn and method for producing the same
JP2004143630A (en) * 2002-10-25 2004-05-20 Teijin Ltd Stretchable false-twisted composite yarn and method for producing the same
US6848151B2 (en) 2003-03-31 2005-02-01 Invista Norh America S.à.r.l Air-jet method for producing composite elastic yarns
US7134265B2 (en) 2002-03-29 2006-11-14 Teijin Limited Stretchable core-sheath type composite yarn and stretchable woven-knit fabric
US8093160B2 (en) 2007-04-17 2012-01-10 Cone Denim Llc Core-spun elastic composite yarns having a filamentary core and ring-spun staple fiber sheath, and denim fabrics which include the same
JP2013544983A (en) * 2010-11-12 2013-12-19 サンコ テキスタイル イスレットメレリ サン ベ ティク エーエス Stretchable composite yarn, manufacturing method thereof, manufacturing apparatus and fabric
KR20160064378A (en) * 2014-11-27 2016-06-08 주식회사 휴비스 Improved shrinage polyester mixed yarn of different shrinkage and Manufacturing method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MX355401B (en) * 2009-12-23 2018-04-18 Invista Tech Sarl Elastic fiber containing an anti-tack additive.
KR101219986B1 (en) * 2010-12-29 2013-01-08 주식회사 효성 Polyurethaneurea Elastic Fiber having high Adhesive Power among Multi-Filament Yarn and Preparing method
CN103741303B (en) * 2013-12-27 2017-03-29 浙江庆茂纺织印染有限公司 Three-core yarn spinning device and technique
US20160160406A1 (en) * 2014-05-29 2016-06-09 Arun Agarwal Production of high cotton number or low denier core spun yarn for weaving of reactive fabric and enhanced bedding
CN104862838A (en) * 2015-05-11 2015-08-26 张涛 Core-spun elastic yarn
WO2017122879A1 (en) * 2016-01-15 2017-07-20 (주)효성 Spandex having improved unwinding properties and enhanced adhesive properties with hot melt adhesive and method for preparing same

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4470250A (en) 1981-07-02 1984-09-11 Bayer Aktiengesellschaft Elastic covered yarn
US4998403A (en) 1990-02-01 1991-03-12 Basf Corporation Apparatus and method of covering spandex yarn
KR19990057610A (en) * 1997-12-30 1999-07-15 조정래 Manufacturing method of polyester biaxial blended yarn
JP2001279550A (en) * 2000-03-30 2001-10-10 Toray Ind Inc False twisted covered elastic yarn and method for producing the same
US7134265B2 (en) 2002-03-29 2006-11-14 Teijin Limited Stretchable core-sheath type composite yarn and stretchable woven-knit fabric
JP2004143630A (en) * 2002-10-25 2004-05-20 Teijin Ltd Stretchable false-twisted composite yarn and method for producing the same
US6848151B2 (en) 2003-03-31 2005-02-01 Invista Norh America S.à.r.l Air-jet method for producing composite elastic yarns
US8093160B2 (en) 2007-04-17 2012-01-10 Cone Denim Llc Core-spun elastic composite yarns having a filamentary core and ring-spun staple fiber sheath, and denim fabrics which include the same
JP2013544983A (en) * 2010-11-12 2013-12-19 サンコ テキスタイル イスレットメレリ サン ベ ティク エーエス Stretchable composite yarn, manufacturing method thereof, manufacturing apparatus and fabric
KR20160064378A (en) * 2014-11-27 2016-06-08 주식회사 휴비스 Improved shrinage polyester mixed yarn of different shrinkage and Manufacturing method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP4060103A4

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114150410A (en) * 2021-10-26 2022-03-08 浙江龙仕达科技股份有限公司 Full dull spandex covering yarn

Also Published As

Publication number Publication date
EP4060103A1 (en) 2022-09-21
KR102171832B1 (en) 2020-10-30
CN114599829B (en) 2023-07-21
EP4060103A4 (en) 2023-11-29
US20240011200A1 (en) 2024-01-11
CN114599829A (en) 2022-06-07
BR112022007993A2 (en) 2022-07-05

Similar Documents

Publication Publication Date Title
US11441244B2 (en) Composite stretch yarn, process and fabric
WO2021096008A1 (en) Composite elastic yarn, stretchable fabric, and method for manufacturing composite elastic yarn
KR102158057B1 (en) Stretch yarns and fabrics with multiple elastic yarns
US8910461B2 (en) Size-covered composite yarns and method for making same
EP1846602A1 (en) Stretch woven fabrics
JP2013151779A (en) Method for producing elastic shirt fabric including spandex and hard yarn
TWI756474B (en) Lyocell denim, garment containing or consisting of lyocell denim, and method of producing denim fabric
CN108456967A (en) A kind of pair plays yarn, preparation method and its fabric
JP5433259B2 (en) Composite spun yarn, production method thereof, and fabric using the composite spun yarn
JP5188841B2 (en) Composite spun yarn and woven / knitted fabric
US20220298678A1 (en) A composite yarn comprising at least two bundles of coalesced elastic filaments and a plurality of inelastic elements
TW201915234A (en) Knitted continuous filament lyocell fabrics
WO2020159268A1 (en) Composite core-spun yarn having improved elastic recovery and shrinkage, and method for producing same
CN111020832A (en) Flame-retardant aramid fiber and cotton blended knitted fabric
JP2000080526A (en) Para system aramide fiber tow for stretch breaking
JPH07157935A (en) Soft conjugate yarn excellent in bulkiness and abrasion resistance
CN116438338A (en) Textile yarn and method for producing same
WO2006027967A1 (en) Elastic yarn having excellent handleability
Pillay et al. Some Applications of the Core-Spinning Technique
WO2019186574A1 (en) Single core composite elastic yarn and fabric thereof
JPH05195357A (en) Polyester spun sewing thread
JPH08127928A (en) Multilayer combined yarn and its production
KR20020053366A (en) a spun yarn and fabric which is made of nylon conjugate fiber

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 20888510

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 17766399

Country of ref document: US

REG Reference to national code

Ref country code: BR

Ref legal event code: B01A

Ref document number: 112022007993

Country of ref document: BR

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2020888510

Country of ref document: EP

Effective date: 20220614

ENP Entry into the national phase

Ref document number: 112022007993

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20220427