KR20110073992A - Polyethyleneterephthalate fiber for air bag and fabric using the same - Google Patents

Polyethyleneterephthalate fiber for air bag and fabric using the same Download PDF

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KR20110073992A
KR20110073992A KR1020090130817A KR20090130817A KR20110073992A KR 20110073992 A KR20110073992 A KR 20110073992A KR 1020090130817 A KR1020090130817 A KR 1020090130817A KR 20090130817 A KR20090130817 A KR 20090130817A KR 20110073992 A KR20110073992 A KR 20110073992A
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polyethylene terephthalate
fabric
less
air bag
airbag
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KR1020090130817A
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Korean (ko)
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KR101295696B1 (en
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정일원
양승철
유제안
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주식회사 효성
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Priority to KR1020090130817A priority Critical patent/KR101295696B1/en
Priority to PCT/KR2010/008942 priority patent/WO2011078513A2/en
Priority to JP2012544379A priority patent/JP2013514465A/en
Priority to CA2783546A priority patent/CA2783546C/en
Priority to US13/517,069 priority patent/US20120263401A1/en
Priority to MX2012007451A priority patent/MX2012007451A/en
Priority to CN201080058616.4A priority patent/CN102713031B/en
Priority to EP10839710.0A priority patent/EP2518195B1/en
Publication of KR20110073992A publication Critical patent/KR20110073992A/en
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Publication of KR101295696B1 publication Critical patent/KR101295696B1/en

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    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F6/00Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof
    • D01F6/58Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolycondensation products
    • D01F6/62Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolycondensation products from polyesters
    • 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
    • D01D5/08Melt spinning methods
    • 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
    • D02G3/44Yarns or threads characterised by the purpose for which they are designed
    • D02G3/446Yarns or threads for use in automotive applications
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • D03D1/02Inflatable articles
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M11/00Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
    • D06M11/77Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with silicon or compounds thereof
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/37Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/564Polyureas, polyurethanes or other polymers having ureide or urethane links; Precondensation products forming them
    • 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
    • D10B2505/00Industrial
    • D10B2505/12Vehicles
    • D10B2505/124Air bags

Abstract

PURPOSE: A polyethylene terephthalate fiber for an air bag and a fabric using the same are provided to prevent air bag burst. CONSTITUTION: A polyethylene terephthalate fiber for an air bag contains a force-deformation curve. The force-deformation curve increases under 4% in case that the initial stress is 1.0g/d at room temperature. The force-deformation curve increases under 12% in case that the intermediate stress is 4.5g/d. The force-deformation curve increases 3% or more until the fiber is cut from that the tensile strength is minimally 7.0g/d.

Description

에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물{Polyethyleneterephthalate Fiber for Air Bag and Fabric Using the Same}Polyethylene terephthalate fiber for air bag and fabric using the same

본 발명은 에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 에어백용 직물에 관한 것으로서, 상세하게는 고유점도가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트의 힘-변형 곡선을 조절하여 에어백용 직물에 적용함으로써 에어백 쿠션 전개 시험에서 터지지 않도록 변부 봉재부분의 터짐 현상이 개선된 에어백용 직물을 제공한다.The present invention relates to polyethylene terephthalate fibers for airbags and fabrics for airbags using the same, in particular by adjusting the force-strain curve of polyethylene terephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3 Application to airbag fabrics provides airbag fabrics with improved bursting of edge bars to prevent bursting in airbag cushion deployment tests.

에어백에 대한 요구 항목은, 충돌시에 원활하게 전개하기 위한 저통기성 및 에어백 자체의 손상·파열을 막기 위한 높은 에너지 흡수능력, 수납성 향상을 위한 직물 자체의 접힘성 등 여러 가지를 들 수 있다.이러한 에어백 직물의 요구 특성에 적합한 섬유로는 나일론66 소재가 주로 사용되어 왔으나 근래에는 비용절감을 위하여 나일론66 이외의 섬유 소재에 대한 관심이 높아지고 있다.The requirements for airbags include a variety of items such as low breathability for smooth deployment during a crash, high energy absorption to prevent damage and rupture of the airbag itself, and foldability of the fabric itself to improve storage. Nylon 66 material has been mainly used as a fiber suitable for the required characteristics of the airbag fabric, but in recent years, interest in fiber materials other than nylon 66 is increasing for cost reduction.

폴리에틸렌테레프탈레이트 원사를 에어백에 사용하기 위해서는 에어백 쿠션 모듈 전개시험에서 터지는 문제를 해결해야하는데, 폴리에틸렌테레프탈레이트 에어백의 에너지 흡수 성능을 개선하기 위한 노력과 에어백 가장자리 봉재 부분이 에어 백 팽창시 터지지 않도록 하기 위한 노력이 이루어지고 있다.In order to use polyethylene terephthalate yarn in the air bag, it is necessary to solve the problem of popping up in the airbag cushion module deployment test.Efforts to improve the energy absorption performance of the polyethylene terephthalate air bag and to prevent the air bag edge bar from bursting during the air bag inflation Efforts are being made.

본 발명은 폴리에틸렌테레프탈레이트 섬유를 사용한 에어백용 직물에 있어서, 폴리에틸렌테레프탈레이트의 섬유의 힘-변형곡선을 조절하여 에어백 직물이 에어백 쿠션 전개 시험에서 터지지 않도록 하는 폴리에틸렌테레프탈레이트 섬유를 제공하는 것을 목적으로 한다.It is an object of the present invention to provide a polyethylene terephthalate fiber in which an airbag fabric using polyethylene terephthalate fiber is adjusted so that the force-strain curve of the fiber of the polyethylene terephthalate is not broken in the airbag cushion development test. .

상기한 과제를 해결하기 위하여, 본 발명의 적절한 실시 형태에 따르면, 고유점도가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트에 있어서, 상온에서 1.0g/d의 초기 응력에 처해졌을 때 4% 미만 신장하고, 4.5g/d의 중기 응력에 처해졌을 때는 12% 미만 신장하며, 최소 7.0g/d의 인장강도로부터 섬유가 절단될 때까지 3% 이상 신장하는 힘-변형 곡선을 갖고, 절단 신도가 15% 이상, 최대 열응력이 0.2~0.5g/d, 말단 카르복실기(CEG) 함량이 35mmol/kg 이하, 단사 섬도가 5 데니어 이하인 것을 특징으로 하는 폴리에틸렌테레프탈레이트 멀티필라멘트를 제공한다.In order to solve the above problems, according to a preferred embodiment of the present invention, in a polyethylene terephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3, at an initial temperature of 1.0 g / d at room temperature Force-strain curves that stretch less than 4% when subjected to strain, less than 12% when subjected to medium stress of 4.5 g / d, and stretch at least 3% until the fiber is cut from a tensile strength of at least 7.0 g / d. It has a cut elongation of 15% or more, a maximum thermal stress of 0.2 ~ 0.5g / d, terminal carboxyl group (CEG) content of 35mmol / kg or less, single yarn fineness of 5 denier or less to provide a polyethylene terephthalate multifilament do.

본 발명의 다른 적절한 실시 형태에 따르면, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트의 총섬도는 150 내지 1000 데니어인 것을 특징으로 한다.According to another suitable embodiment of the present invention, the total fineness of the polyethylene terephthalate multifilament is 150 to 1000 denier.

본 발명의 또 다른 적절한 실시 형태에 따르면, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용하여 제직된 에어백용 직물을 제공한다.According to another suitable embodiment of the present invention, there is provided a fabric for an air bag woven using the polyethylene terephthalate multifilament.

본 발명의 또 다른 적절한 실시 형태에 따르면, 에어백용 직물에 실리콘계, 폴리우레탄계, 아크릴계, 네오프렌계 및 클로로프렌계로 이루어진 군에서 선택된 코팅제를 사용하여 15~60g/m2 중량으로 코팅하여 제조되고, (1) 인장 강도 190 내지 300kgf, (2) 인열 강도 25 내지 40kgf, (3) 공기투과도 0.5 CFM(Cubic Feet per Minute) 이하인 에어백용 코팅 직물을 제공한다.According to another suitable embodiment of the present invention, the airbag fabric is prepared by coating at 15 to 60 g / m 2 weight using a coating agent selected from the group consisting of silicone, polyurethane, acrylic, neoprene and chloroprene, (1 A coating fabric for an airbag having a tensile strength of 190 to 300 kgf, (2) tear strength of 25 to 40 kgf, and (3) air permeability of 0.5 CFM (Cubic Feet per Minute) is provided.

본 발명은 폴리에틸렌테레프탈레이트의 섬유의 힘-변형곡선을 조절하여 폴리에틸렌테레프탈레이트 멀티필라멘트가 상온에서 1.0g/d의 초기 응력에 처해졌을 때 4%미만 신장하고, 4.5g/d의 중기 응력에 처해졌을 때는 12%미만 신장하며, 최소 7.0g/d의 인장강도로부터 섬유가 절단될 때까지 3%이상 신장하는 힘-변형 곡선을 갖고, 절단 신도가 15% 이상, 최대 열응력은 0.2~0.6g/d, 말단 카르복실기(CEG) 함량이 35mmol/kg 이하, 단사 섬도가 5데니어 이하인 폴리에틸렌테레프탈레이트 섬유를 사용함으로써 에어백쿠션 전개시험에서 터지지 않는 에어백용 직물을 제조할 수 있다.The present invention adjusts the force-strain curve of the polyethylene terephthalate fiber, the polyethylene terephthalate multifilament is stretched to less than 4% when subjected to the initial stress of 1.0 g / d at room temperature, subjected to medium-stress of 4.5 g / d Has a force-strain curve that stretches less than 12% when stretched and stretches by at least 3% from a tensile strength of at least 7.0 g / d until the fiber is cut, elongation at break of 15% and maximum thermal stress of 0.2-0.6 g By using polyethylene terephthalate fibers having a / d, terminal carboxyl group (CEG) content of 35 mmol / kg or less and single yarn fineness of 5 denier or less, a fabric for an air bag that does not burst in an air bag cushion development test can be prepared.

본 발명은 고유점도가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 제조된 폴리에틸렌테레프탈레이트 멀티필라멘트의 힘-변형 곡선을 조절하여 에어백용 직물에 적용함으로써 에어백 쿠션 전개 시험에서 터지지 않도록 변부 봉재부분이 터짐 현상을 개선된 에어백용 직물을 제공한다.The present invention adjusts the force-strain curve of polyethylene terephthalate multifilament produced by spinning polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3, and applies it to an airbag fabric so that the edge portion of the edge is not broken in the airbag cushion development test. To provide a fabric for the air bag improved the phenomenon.

본 발명의 적절한 실시 형태에 따르면, 에어백 내부의 화약 폭발로 발생하는 배출가스의 순간적인 충격에너지를 에어백 직물이 안전하게 흡수하기 위해서 고유점도(IV)가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용한다. 수지의 고유 점도가 0.8 dl/g 미만의 IV를 갖는 폴리에스테르 원사는 충분한 인성을 갖는 원사를 제공하지 않아 적당하지 않다.According to a preferred embodiment of the present invention, in order to safely absorb the instantaneous impact energy of the exhaust gas generated by the explosive explosion inside the airbag, the airbag fabric obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity (IV) of 0.8 to 1.3. Polyethylene terephthalate multifilament is used. Polyester yarns having IVs with an inherent viscosity of less than 0.8 dl / g are not suitable because they do not provide yarns with sufficient toughness.

본 발명의 에어백용 합성섬유 멀티 필라멘트를 생성하기 위한 수지는 폴리에틸렌 테레프탈레이트, 폴리부틸렌 테레프탈레이트, 폴리에틸렌 나프탈레이트, 폴리부틸렌 나프탈레이트, 폴리에틸렌-1,2-비스(페녹시)에탄-4,4'-디카르복실레이트, 폴리(1,4-시클로헥실렌-디메틸렌 테레프탈레이트) 및 상기 중합체의 1 종 이상의 반복 단위를 포함하는 공중합체, 예를 들어 폴리에틸렌 테레프탈레이트/이소프탈레이트 코폴리에스테르, 폴리부틸렌 테레프탈레이트/나프탈레이트 코폴리에스테르, 폴리부틸렌 테레프탈레이트/데칸디카르복실레이트 코폴리에스테르, 및 상기 중합체 및 공중합체 중 둘 이상의 혼합물로 이루어지는 군으로부터 선택될 수 있다. 이들 중에서, 폴리에틸렌테레프탈레이트 수지가 기계적 성질 및 섬유 형성 측면에서 본 발명에 특히 적당하다.The resin for producing the synthetic fiber multifilament for the airbag of the present invention is polyethylene terephthalate, polybutylene terephthalate, polyethylene naphthalate, polybutylene naphthalate, polyethylene-1,2-bis (phenoxy) ethane-4, Copolymers comprising 4'-dicarboxylate, poly (1,4-cyclohexylene-dimethylene terephthalate) and at least one repeating unit of the polymer, for example polyethylene terephthalate / isophthalate copolyester , Polybutylene terephthalate / naphthalate copolyester, polybutylene terephthalate / decanedicarboxylate copolyester, and mixtures of two or more of the above polymers and copolymers. Among them, polyethylene terephthalate resin is particularly suitable for the present invention in terms of mechanical properties and fiber formation.

본 발명의 폴리에틸렌테레프탈레이트 섬유의 말단 카르복실기(CEG) 함량은 35mmol/kg 이하가 적당하다. 폴리에틸렌테레프탈레이트 원사의 말단 카르복실기(CEG) 함량이 35mmol/kg를 초과하면 원사의 내가수분해 성능이 저하되어 고온다습한 환경조건에서는 에어백 직물의 성능유지가 어렵게 된다.As for the terminal carboxyl group (CEG) content of the polyethylene terephthalate fiber of this invention, 35 mmol / kg or less is suitable. When the terminal carboxyl group (CEG) content of polyethylene terephthalate yarn exceeds 35mmol / kg, the hydrolysis performance of the yarn is lowered, making it difficult to maintain the performance of the airbag fabric under high temperature and high humidity conditions.

본 발명의 에어백용 폴리에틸렌테레프탈레이트 멀티 필라멘트로 적합한 섬유는 힘-변형곡선이 1.0g/d의 초기 응력에 처해졌을 때 4%미만 신장하는 것이 바람직한데, 만약 사가 1.0g/d의 초기 응력에 4%이상 신장하면 직물의 급격한 변형으로 초기에 직물의 손상을 초래한다. Fibers suitable for the polyethylene terephthalate multifilament for airbags of the present invention are preferred to elongate less than 4% when the force-strain curve is subjected to an initial stress of 1.0 g / d. Elongation of more than% may cause the fabric to be damaged early due to rapid deformation of the fabric.

또한, 본 발명에서, 4.5g/d의 중기 응력에 처해졌을 때는 사가 12%미만 신장하는 것이 바람직한데 이는 사가 4.5g/d의 중기 응력에 12%이상 신장하면 직물의 통기도가 급격히 증가하여 배출가스에 의한 인체에 화상을 초래한다.In addition, in the present invention, when subjected to the medium-term stress of 4.5g / d, it is preferable to extend less than 12% of yarn, which extends more than 12% to the medium-term stress of 4.5g / d, the ventilation of the fabric is rapidly increased to exhaust gas It causes burns in the human body.

또한, 본 발명에서 폴리에틸렌테레프탈레이트 원사를 사용한 직물이 에어백 용도로써 적합한 인장강력 및 인열강도를 가지려면 최소 7.0g/d의 인장강도로부터 사가 절단될 때까지 3%이상 신장하는 것이 바람직한데, 이는 최소 7.0g/d의 인장강도로부터 사가 절단될 때까지 3%미만 신장하면 사의 최대 인장하중 흡수력이 부족하여 낮은 중량의 직물로 제직할 경우 인장강도 및 인열강도가 부족한 문제가 있다. In addition, in the present invention, it is preferable that the fabric using polyethylene terephthalate yarn is stretched by 3% or more until the yarn is cut from a tensile strength of at least 7.0 g / d to have a tensile strength and tear strength suitable for use as an air bag. If the yarn is stretched less than 3% from the tensile strength of at least 7.0 g / d until the yarn is cut, there is a problem that the tensile strength and tear strength are insufficient when weaving a low weight fabric due to the lack of the maximum tensile load absorbing ability of the yarn.

본 발명의 에어백용 폴리에틸렌테레프탈레이트 멀티 필라멘트의 절단 신도는 15% 이상이 적합한데 절단 신도가 15% 미만으로 작으면 에어백 쿠션이 급팽창 할때의 에너지를 흡수능력이 떨어져서 쿠션이 터지게 되어 적합하지 않게 된다.The cutting elongation of the polyethylene terephthalate multifilament for airbags of the present invention is 15% or more, but if the cutting elongation is less than 15%, the airbag cushion is less suitable for absorbing energy when the airbag cushion is suddenly inflated. do.

본 발명의 에어백용 폴리에틸렌테레프탈레이트 멀티 필라멘트의 최대 열응력은 0.2~0.6g/d인 것이 바람직하다. 최대 열응력이 0.2g/d 미만인 원사 생산조건에서는 원사 강도가 미흡하고, 최대 열응력 0.6d/g 초과하는 생산조건에서는 원사의 신율이 낮게 되어 에어백 쿠션 전개시험에서 잘 터지는 문제가 있다.It is preferable that the maximum thermal stress of the polyethylene terephthalate multifilament for airbags of this invention is 0.2-0.6 g / d. There is a problem that the yarn strength is insufficient in the production conditions of the yarn with a maximum thermal stress of less than 0.2 g / d, and the elongation of the yarn is low at the production conditions in which the maximum thermal stress is more than 0.6d / g.

본 발명의 에어백용 폴리에틸렌테레프탈레이트 멀티 필라멘트의 총 섬도는 150∼1000데니어인 것이 적합하고, 더욱 바람직하게는 200∼700데니어이다. 총 섬도가 150데니어 미만의 원사를 사용할 경우 에어백용 직물은 수납성의 점에서는 만족하지만, 강력이 부족하여 전개시 및 전개후의 승객 충돌시에 백이 파열될 우려가 있어 바람직하지 않다. 반대로 총 섬도가 1000데니어를 넘으면, 에어백으로서 충분한 강력이 얻어져 안전성의 면에서는 만족할 수 있지만 직물이 두꺼워져서 수납성이 나빠지게 된다.It is preferable that the total fineness of the polyethylene terephthalate multifilament for airbags of this invention is 150-1000 denier, More preferably, it is 200-700 denier. If the total fineness is less than 150 denier yarns, the fabric for airbags is satisfactory in terms of storage, but it is not preferable because the bag lacks strength and may cause the bag to rupture during deployment and after a passenger collision. On the contrary, when the total fineness exceeds 1000 denier, sufficient strength is obtained as an air bag and satisfactory in terms of safety, but the fabric becomes thicker and the storage capacity becomes worse.

에어백용 직물을 구성하는 멀티 필라멘트의 단사 섬도에 관해서는 5데니어 이하인 것이 적합하고, 바람직하게는 4.5데니어 이하이다. 통상, 단사 섬도가 작은 섬유를 이용할수록, 얻어지는 직물은 유연하여 접힘성이 우수하고 수납성이 양호해진다. 또, 단사 섬도가 작아짐과 동시에 커버링성이 향상하고, 그 결과, 직물의 통기성을 억제할 수가 있다. 단사 섬도가 5데니어를 넘으면 직물의 접힘성 및 수납성의 저하, 또한 저통기성의 악화를 수반하여 에어백 직물로서 충분한 기능을 발휘하지 못하므로 바람직하지 않다.About single yarn fineness of the multifilament which comprises the fabric for airbags, it is suitable that it is 5 denier or less, Preferably it is 4.5 denier or less. Usually, the more the fiber of a single yarn fineness is used, the softer the woven fabric will be, the more excellent the foldability and the better the storage performance. Moreover, single yarn fineness becomes small, and covering property improves, As a result, the air permeability of a woven fabric can be suppressed. If the single yarn fineness exceeds 5 denier, it is not preferable because it does not exert sufficient function as an airbag fabric with deterioration of the foldability and storage property of the fabric and also deterioration of low breathability.

본 발명의 제조방법에 의해 제조된 폴리에틸렌테레프탈레이트 섬유는 에어제트 또는 워터제트룸 직기를 이용하되 직물의 잔류 유분이 0.1중량% 이하인 것이 바람직하기 때문에, 섬유에 부착되어 있는 유제의 탈락성을 고려하면 워터제트룸으로 제직하는 것이 바람직하다. 또한 제직 후, 정련처리 및 160∼190℃의 열세트처리를 하는 것이 바람직하다.In the polyethylene terephthalate fiber produced by the manufacturing method of the present invention using an air jet or water jet loom, the residual oil of the fabric is preferably 0.1% by weight or less. It is desirable to weave into water jet rooms. Furthermore, after weaving, it is preferable to perform refining treatment and hot set treatment at 160 to 190 캜.

본 발명의 제조방법에 의해 제조된 폴리에틸렌테레프탈레이트 섬유로 직물을 제직 시에는, 대칭구조를 갖는 평직을 제직하는 것이 바람직하지만, 선택적으로 매력적인 직물을 얻기 위해서 보다 가는 선밀도를 갖는 사를 대칭구조의 2/2 파나마직으로 제직할 수도 있다. When weaving a woven fabric with polyethylene terephthalate fiber produced by the production method of the present invention, it is preferable to weave a plain weave having a symmetrical structure, but in order to obtain an attractive woven fabric, a yarn having a thinner linear density may be used. You can also weave in Panama.

제직된 직물은 에어백 직물에 적합한 저통기성을 확보하기 위하여 실리콘계, 폴리우레탄계, 아크릴계, 네오프렌계, 클로로프렌계 중에서 선택되어진 코팅제를 사용하여 15~60g/m2 중량으로 코팅하여 사용할수 있다.Woven fabrics can be used by coating at 15 to 60 g / m 2 weight using a coating agent selected from silicon, polyurethane, acrylic, neoprene and chloroprene to ensure low breathability suitable for airbag fabrics.

실시예 및 비교예의 물성 평가는 아래와 같이 측정 또는 평가하였다. The physical property evaluation of an Example and a comparative example was measured or evaluated as follows.

1) 고유점도(I.V.)1) Intrinsic viscosity (I.V.)

페놀과 1,1,2,2-테트라클로로에탄올 6:4(무게비)로 혼합한 시약(90℃)에 시료 0.1g을 90분간 용해시킨 후 우베로데(Ubbelohde) 점도계에 옮겨 담아 30℃ 항온조에서 10분간 유지시키고, 점도계와 애스피레이터(Aspirator)를 이용하여 용액의 낙하초수를 구한다. 솔벤트의 낙하초수도 상기와 같은 방법으로 구한 아래의 수학식에 의해 R.V.값 및 I.V. 값을 계산하였다.After dissolving 0.1 g of the sample in a reagent (90 ° C.) mixed with phenol and 1,1,2,2-tetrachloroethanol 6: 4 (weight ratio) for 90 minutes, transfer to a Ubbelohde viscometer and place it in a 30 ° C. thermostat. The solution is held for 10 minutes at, and the drop seconds of the solution are obtained by using a viscometer and an aspirator. The number of seconds of falling of the solvent can also be obtained by the following equations obtained from the above equations. The value was calculated.

R.V. = 시료의 낙하초수/솔벤트 낙하초수R.V. = Number of drops of solvent / number of drops of solvent

I.V. = 1/4 × [(R.V.- 1)/C] + 3/4 × (In R.V./C)I.V. = 1/4 × [(R.V.-1) / C] + 3/4 × (In R.V./C)

상기 식에서 ,C는 용액중의 시료의 농도(g/100㎖)를 나타낸다.In the above formula, C represents the concentration (g / 100ml) of the sample in solution.

2) 원사의 열응력 측정2) Thermal stress measurement of yarn

카네보사(KANEBO)의 열응력 테스트기(모델명, KE-3LS)를 이용하여, 원사를 10cm의 루프상태로 만들어 상하단 후크에 걸고 시료에 0.05g/den의 초기하중을 걸어 2.2℃/초의 속도로 가열하며 시료에 발생된 응력을 도표에 기록하여 측정한다.Using KANEBO's thermal stress tester (model: KE-3LS), the yarn was looped to 10 cm, hooked on the upper and lower hooks, and subjected to an initial load of 0.05 g / den on the sample and heated at 2.2 ° C / sec. The stress generated in the sample is recorded in the chart and measured.

3) 원사의 말단 카르복실기(CEG) 함량 측정3) Measurement of terminal carboxyl group (CEG) content of yarn

GRI(Geosynthetic Research Institute)의 Test Method "GG7" 방법으로 말단 카르복실기 함량을 분석하여 mmol/kg 단위로 표시한다.The terminal carboxyl group content is analyzed by GRI (Geosynthetic Research Institute) Test Method "GG7" method and expressed in mmol / kg units.

4) 원사의 강신도 측정방법 4) How to measure the elongation of yarn

원사를 표준상태인 조건, 즉 25℃ 온도와 상대습도 65%인 상태인 항온 항습실에서 24시간 방치 후 ASTM 2256 방법으로 시료를 인장 시험기를 통해 측정한다.After leaving the yarn in a standard condition, that is, a constant temperature and humidity chamber at a temperature of 25 ° C. and a relative humidity of 65% for 24 hours, the sample is measured by a tensile tester using the ASTM 2256 method.

5) 직물의 제직과 코팅5) weaving and coating of fabrics

필라멘트 원사를 경사 방향 및 위사 방향 둘 모두에서 인치당 50×50개의 원사 밀도로 평직으로 제직한다. 생지를 지그(jig)에서 95℃의 수성욕에서 정련 및 수축시키고, 185 ℃에서 2 분 동안 열 고정한다. 그리고 실리콘계 코팅제를 사용하여 25g/m2 중량으로 코팅하였다. The filament yarns are woven into plain weave at 50 × 50 yarn densities per inch in both warp and weft directions. The dough is refined and shrunk in a jig at 95 ° C. in an aqueous bath and heat set at 185 ° C. for 2 minutes. And it was coated with a weight of 25g / m 2 using a silicone-based coating agent.

6) 직물의 인장강도6) tensile strength of fabric

인스트론(Instron) 4465(인스트론사제, 미국)를 이용하여, ASTM D 5034의 규정에 따라 표준 상태(20℃, 65상대습도)하에서 24시간 이상 방치한 후 직물의 폭 10cm, 길이 15cm로 직물의 인장강도를 측정하였다.Using Instron 4465 (manufactured by Instron, USA), the fabric is allowed to stand at 10 cm wide and 15 cm long after being left for 24 hours under standard conditions (20 ° C, 65 relative humidity) according to ASTM D 5034. Tensile strength of was measured.

7) 직물의 인열강도 7) Tear strength of fabric

인스트론(Instron) 4465(인스트론사제, 미국)를 이용하여, ASDM D 2261법에 의한 텅법 의 규정에 따라 표준 상태(20℃, 65상대습도)하에서 24시간 이상 방치한 후 직물의 인열강도를 측정하였다.Tear strength of the fabric after instron 4465 (manufactured by Instron, USA) for at least 24 hours under standard condition (20 ℃, 65 relative humidity) according to the tongue method according to ASDM D 2261 Was measured.

8) 직물의 공기투과도 8) Air Permeability of Fabric

Frazier 공기투과도 측정기를 이용하여, ASDM 737법의 규정에 따라 125 Pa압력하에서 직물의 공기투과도를 측정하였다.Using a Frazier air permeability meter, the air permeability of the fabric was measured under 125 Pa pressure according to the ASDM 737 method.

9) 에어백 쿠션의 전개 시험9) Deployment test of airbag cushion

에어백 원단으로 모듈을 제작하여 85℃에서 4시간 방치 후 3분 이내 전개 테 스트를 진행하여 터짐여부를 관찰하여 PASS와 FAIL을 평가하였다After making the module with airbag fabric and leaving it at 85 ℃ for 4 hours, the development test was conducted within 3 minutes to observe the burst and evaluated PASS and FAIL.

이하에서 실시예를 들어서 본 발명을 상세하게 설명하지만, 본 발명의 권리범위가 아래 실시예에 의하여 제한되거나 한정되는 것은 아니다.Hereinafter, the present invention will be described in detail with reference to Examples, but the scope of the present invention is not limited or limited by the following Examples.

실시예 1Example 1

방사시 GR4 온도 250℃, GR5 온도 170℃, 이완율(Relax ratio) 9.2%조건에서 생산하여 아래 표 1에 기재된 특성을 갖는 폴리에틸렌테레프탈레이트 원사로 워터제트룸 직기로 인치 당 50×50개 직물이 되도록 평직하여 에어백용 생지를 제조하였다.It is produced under the conditions of GR4 temperature 250 ℃, GR5 temperature 170 ℃, and relaxation ratio 9.2%. Plain as possible to prepare a dough for airbags.

비교예 1Comparative Example 1

방사시 GR4 온도 175℃, GR5 온도 110℃, 이완율(Relax ratio) 1.9%조건 외에는 실시예 1과 동일한 조건에서 생산하여 아래 표 1에 기재된 특성을 갖는 폴리에틸렌테레프탈레이트 원사로 실시예 1과 동일한 방법으로 에어백용 생지를 제조하였다.Polyethylene terephthalate yarn produced in the same conditions as in Example 1 except for the GR4 temperature 175 ℃, GR5 temperature 110 ℃, relaxation ratio 1.9% conditions and the characteristics shown in Table 1 below the same method as in Example 1 Dough for airbags was prepared.

실시예 2Example 2

실시예 1에서 제조된 생지를 95℃인 수성욕을 통과시켜 생지를 정련 및 열수축시킨 다음, 185℃에서 2 분 동안 열 고정한다. 그리고 실리콘계 코팅제를 사용하 여 25g/m2 중량으로 코팅한다. The dough prepared in Example 1 was refined and thermally contracted by passing through a 95 ° C. aqueous bath, and then heat-fixed at 185 ° C. for 2 minutes. And it is coated with a weight of 25g / m 2 using a silicone coating agent.

이와 같이 제조된 직물의 물성을 평가와 에어백 쿠션 전개시험 결과를 하기 표 2에 나타내었다.Evaluation of the physical properties of the fabric thus prepared and the airbag cushion development test results are shown in Table 2 below.

비교예 2Comparative Example 2

비교예 1에서 제조된 생지를 실시예 2와 동일한 방법으로 처리하여 제조한 직물의 물성을 평가와 에어백 쿠션 전개시험 결과를 하기 표 2에 나타내었다.Evaluation of the physical properties of the fabric produced by treating the dough prepared in Comparative Example 1 in the same manner as in Example 2 and airbag cushion development test results are shown in Table 2 below.

[표 1]TABLE 1

구분division 규격standard 단사
섬도
(den)
cinnabar
Island
(den)
강도
(g/den)
burglar
(g / den)
신도
(%)
Shindo
(%)
CEG
(mmol/kg)
CEG
(mmol / kg)
최대
열응력
(g/den)
maximum
Thermal stress
(g / den)
1.0g/d에서
신도(%)
At 1.0 g / d
Elongation (%)
4.5g/d에서
신도(%)
At 4.5g / d
Elongation (%)
7.0g/d에서 절단시까지의 신도(%)% Elongation from 7.0 g / d to cutting
실시예1Example 1 500d/120f500d / 120f 4.24.2 9.0 9.0 22.622.6 25.125.1 0.290.29 0.90.9 9.79.7 5.15.1 비교예1Comparative Example 1 630d/48f630d / 48f 13.213.2 8.18.1 12.312.3 25.325.3 0.53 0.53 0.80.8 5.45.4 4.0 4.0

[표 2]TABLE 2

구분division 인장강도
(경사×위사, kgf)
The tensile strength
(Slope X weft, kgf)
인열강도
(경사×위사, kgf)
Phosphorus strength
(Slope X weft, kgf)
공기투과도
(CFM)
Air permeability
(CFM)
에어백 쿠션
전개 시험
Airbag cushion
Deployment test
실시예2Example 2 223×221223 × 221 27.3×27.727.3 × 27.7 0.1이하0.1 or less PASSPASS 비교예2Comparative Example 2 241×239241 × 239 27.9×28.827.9 × 28.8 0.1이하0.1 or less FAILFAIL

Claims (4)

고유점도가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트에 있어서, In the polyethylene terephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3, 상온에서 1.0g/d의 초기 응력에 처해졌을 때 4% 미만 신장하고, 4.5g/d의 중기 응력에 처해졌을 때는 12% 미만 신장하며, 최소 7.0g/d의 인장강도로부터 섬유가 절단될 때까지 3% 이상 신장하는 힘-변형 곡선을 갖고, 절단 신도가 15% 이상, 최대 열응력이 0.2~0.5g/d, 말단 카르복실기(CEG) 함량이 35mmol/kg 이하 및 단사 섬도가 5 데니어 이하인 것을 특징으로 하는 폴리에틸렌테레프탈레이트 멀티필라멘트.Less than 4% when subjected to an initial stress of 1.0 g / d at room temperature, less than 12% when subjected to medium stress of 4.5 g / d, and when the fiber is cut from a tensile strength of at least 7.0 g / d. It has a force-strain curve that extends by 3% or more, and has an elongation at break of 15% or more, a maximum thermal stress of 0.2 to 0.5 g / d, a terminal carboxyl group (CEG) content of 35 mmol / kg or less, and a single yarn fineness of 5 denier or less. Polyethylene terephthalate multifilament characterized by the above-mentioned. 제 1항에 있어서, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트의 총섬도는 150 내지 1000 데니어인 것을 특징으로 하는 폴리에틸렌테레프탈레이트 멀티필라멘트.The polyethylene terephthalate multifilament according to claim 1, wherein the total fineness of the polyethylene terephthalate multifilament is 150 to 1000 denier. 제 1항의 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용하여 제직된 에어백용 직물.An airbag fabric woven using the polyethylene terephthalate multifilament of claim 1. 제 3항의 에어백용 직물에 실리콘계, 폴리우레탄계, 아크릴계, 네오프렌계 및 클로로프렌계로 이루어진 군에서 선택된 코팅제를 사용하여 15~60g/m2 중량으로 코팅하여 제조되고, 하기의 물성을 만족하는 에어백용 코팅 직물: (1) 인장 강도 190 내지 300kgf, (2) 인열 강도 25 내지 40kgf, (3) 공기투과도 0.5 CFM(Cubic Feet per Minute) 이하The airbag coating fabric of claim 3 is manufactured by coating at 15 to 60 g / m 2 weight using a coating agent selected from the group consisting of silicone, polyurethane, acrylic, neoprene and chloroprene, and satisfying the following properties: (1) Tensile strength 190 to 300kgf, (2) Tear strength 25 to 40kgf, (3) Air permeability less than 0.5 CFM (Cubic Feet per Minute)
KR1020090130817A 2009-12-24 2009-12-24 Polyethyleneterephthalate Fiber for Air Bag and Fabric Using the Same KR101295696B1 (en)

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KR1020090130817A KR101295696B1 (en) 2009-12-24 2009-12-24 Polyethyleneterephthalate Fiber for Air Bag and Fabric Using the Same
PCT/KR2010/008942 WO2011078513A2 (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same
JP2012544379A JP2013514465A (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for airbag and fabric using the same
CA2783546A CA2783546C (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same
US13/517,069 US20120263401A1 (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same
MX2012007451A MX2012007451A (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same.
CN201080058616.4A CN102713031B (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same
EP10839710.0A EP2518195B1 (en) 2009-12-24 2010-12-14 Polyethylene terephthalate fiber for air-bags and textiles made from same

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20170132153A (en) * 2015-03-30 2017-12-01 도레이 카부시키가이샤 A method of manufacturing a polyester bubble for an air bag, a polyester air bag and a polyester bubble for an air bag
KR20190086119A (en) * 2018-01-12 2019-07-22 효성첨단소재 주식회사 Polyethyleneterephthalate fiber
US11019548B2 (en) 2017-11-24 2021-05-25 Samsung Electronics Co., Ltd. Electronic device and communication method thereof
CN113547820A (en) * 2020-04-23 2021-10-26 现代自动车株式会社 Laminate for vehicle interior material and method for manufacturing same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0748717A (en) * 1993-08-05 1995-02-21 Teijin Ltd Polyester fiber for base fabric for air bag
JP2944220B2 (en) 1993-10-13 1999-08-30 帝人株式会社 Fabric for high-performance airbag and method for producing the same
JPH08134717A (en) * 1994-11-04 1996-05-28 Unitika Ltd Production of polyester fiber for air bag
JPH08158153A (en) * 1994-12-07 1996-06-18 Teijin Ltd Polyester filament yarn for air bag base fabric

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20170132153A (en) * 2015-03-30 2017-12-01 도레이 카부시키가이샤 A method of manufacturing a polyester bubble for an air bag, a polyester air bag and a polyester bubble for an air bag
US11019548B2 (en) 2017-11-24 2021-05-25 Samsung Electronics Co., Ltd. Electronic device and communication method thereof
US11218938B2 (en) 2017-11-24 2022-01-04 Samsung Electronics Co., Ltd. Electronic device and communication method thereof
KR20190086119A (en) * 2018-01-12 2019-07-22 효성첨단소재 주식회사 Polyethyleneterephthalate fiber
CN113547820A (en) * 2020-04-23 2021-10-26 现代自动车株式会社 Laminate for vehicle interior material and method for manufacturing same

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