WO2011078513A2 - 에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물 - Google Patents
에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물 Download PDFInfo
- Publication number
- WO2011078513A2 WO2011078513A2 PCT/KR2010/008942 KR2010008942W WO2011078513A2 WO 2011078513 A2 WO2011078513 A2 WO 2011078513A2 KR 2010008942 W KR2010008942 W KR 2010008942W WO 2011078513 A2 WO2011078513 A2 WO 2011078513A2
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- WO
- WIPO (PCT)
- Prior art keywords
- polyethylene terephthalate
- less
- terephthalate multifilament
- fabric
- multifilament
- Prior art date
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Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F6/00—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof
- D01F6/58—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolycondensation products
- D01F6/62—Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolycondensation products from polyesters
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D5/00—Formation of filaments, threads, or the like
- D01D5/12—Stretch-spinning methods
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D1/00—Woven fabrics designed to make specified articles
- D03D1/02—Inflatable articles
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
- D03D15/20—Woven 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
- D03D15/283—Woven 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
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
- D03D15/50—Woven 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
- D03D15/573—Tensile strength
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
- D06M15/19—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
- D06M15/21—Macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
- D06M15/263—Macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds of unsaturated carboxylic acids; Salts or esters thereof
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
- D06M15/19—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
- D06M15/37—Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
- D06M15/564—Polyureas, polyurethanes or other polymers having ureide or urethane links; Precondensation products forming them
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
- D06M15/19—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
- D06M15/37—Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
- D06M15/643—Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds containing silicon in the main chain
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
- D06M15/693—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with natural or synthetic rubber, or derivatives thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R21/00—Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
- B60R21/02—Occupant safety arrangements or fittings, e.g. crash pads
- B60R21/16—Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
- B60R21/23—Inflatable members
- B60R21/235—Inflatable members characterised by their material
- B60R2021/23504—Inflatable members characterised by their material characterised by material
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2331/00—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
- D10B2331/04—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyesters, e.g. polyethylene terephthalate [PET]
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/12—Vehicles
- D10B2505/124—Air bags
Definitions
- the present invention relates to polyethylene terephthalate fibers for airbags and fabrics for airbags using the same, in particular, to control the force-strain curve of polyethylene terephthalate multifilament produced by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3
- the present invention provides an airbag fabric having improved edge rupture phenomenon by applying to an airbag fabric so as not to burst in an airbag cushion deployment test.
- Airbag fabrics require various characteristics such as low breathability for smooth deployment in 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 recently, interest in fiber materials other than nylon 66 is increasing for economic reasons such as cost reduction.
- An object of the present invention is to improve the bursting phenomenon of the edge portion of the fabric for airbags using polyethylene terephthalate fiber, by adjusting the force-strain curve of the polyethylene terephthalate multifilament so as not to burst in the airbag cushion development test.
- the polyethylene terephthalate multifilament for airbags produced by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3, less than 4% when subjected to an initial stress of 1.0 g / d at room temperature Elongation, less than 12% when subjected to medium stress of 4.5 g / d, a force-strain curve extending at least 3% until the fiber is cut from a tensile strength of at least 7.0 g / d, and elongation at break
- a polyethylene terephthalate multifilament for airbags characterized in that 15% or more and single yarn fineness is 5 denier or less.
- the polyethylene terephthalate multifilament has a F / F static friction coefficient of yarn divided by F / M static friction coefficient of 1.5 or more.
- the polyethylene terephthalate multifilament has a terminal carboxyl group (CEG) content of 35 mmol / kg or less.
- the polyethylene terephthalate multifilament has a maximum thermal stress of 0.2 to 0.5 g / d.
- the polyethylene terephthalate multifilament has a total fineness of 150 to 1000 denier.
- a fabric for an air bag woven using the polyethylene terephthalate multifilament wherein the air bag fabric selected from the group consisting of silicone, polyurethane, acrylic, neoprene and chloroprene-based A coating for 15 to 60 g / m 2 is used to prepare a fabric for an air bag using a coating agent of a species.
- the present invention stretches less than 4% when subjected to an initial stress of 1.0 g / d at room temperature, and less than 12% when subjected to medium stresses of 4.5 g / d, and at least 7.0 g / d of tensile strength of the fiber.
- 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 sewing portion bursts so as not to burst in the airbag cushion development test. To provide a fabric for the air bag improved the phenomenon.
- the present invention provides a polyethylene terephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3 in order to safely absorb the instantaneous impact energy of the exhaust gas generated by the explosives inside the air bag. use.
- Polyester yarns having an intrinsic viscosity of less than 0.8 dl / g are not suitable because they do not provide yarns with sufficient toughness.
- Resin for producing the multi-filament for the air bag of the present invention in addition to polyethylene terephthalate, polybutylene terephthalate, polyethylene naphthalate, polybutylene naphthalate, polyethylene-1,2-bis (phenoxy) ethane-4,4 Preferred are copolymers comprising '-dicarboxylate, poly (1,4-cyclohexylene-dimethylene terephthalate) and at least one repeating unit of the polymer.
- polyethylene terephthalate / isophthalate copolyester polybutylene terephthalate / naphthalate copolyester, polybutylene terephthalate / decanedicarboxylate copolyester, and two or more of the above polymers and copolymers It may be selected from the group consisting of a mixture. Among them, in the present invention, polyethylene terephthalate resin is particularly preferable in terms of mechanical properties and fiber formation.
- the terminal carboxyl group (CEG) content of the polyethylene terephthalate fiber of this invention is 35 mmol / kg or less.
- the terminal carboxyl group (CEG) content of the polyethylene terephthalate yarn exceeds 35mmol / kg, the hydrolysis performance of the yarn is lowered, it is difficult to maintain the performance of the airbag fabric under high temperature and high humidity conditions.
- Fibers suitable for the polyethylene terephthalate multifilament for airbags of the present invention preferably elongate less than 4% when the force-strain curve is subjected to an initial stress of 1.0 g / d. If the polyethylene terephthalate multifilament is stretched by more than 4% at an initial stress of 1.0 g / d, the fabric may be suddenly deformed and the fabric may be initially damaged.
- fabrics using polyethylene terephthalate multifilament are preferably stretched at least 3% from the tensile strength of at least 7.0 g / d until the yarn is cut in order to have suitable tensile and tear strengths for airbag applications. This is because when the yarn is stretched less than 3% from the tensile strength of at least 7.0g / d until the yarn is cut, there is a problem that the tensile strength and tear strength is insufficient when weaving into a low-weight fabric due to the lack of the maximum tensile load absorption capacity of the yarn.
- the breaking elongation of the polyethylene terephthalate multifilament for an air bag is preferably 15% or more.
- the energy absorbing capacity of the airbag cushion when it is inflated is poor, causing the cushion to burst, which is not suitable.
- the maximum thermal stress of the polyethylene terephthalate multifilament for air bags is preferably 0.2 to 0.6 g / d.
- the yarn strength is insufficient in the production conditions of yarn with a maximum thermal stress of less than 0.2g / d, and the elongation of yarn is low at production conditions with a maximum thermal stress of more than 0.6d / g.
- the total fineness of the polyethylene terephthalate multifilament for an air bag is suitably 150 to 1000 denier, more preferably 200 to 700 denier. If the total fineness of the yarn is less than 150 denier, the fabric for the airbag is satisfactory in terms of storage, but it is not preferable because the bag lacks strength and may cause the bag to rupture at the time of 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.
- single yarn fineness of the multifilament which comprises the fabric for airbags it is preferable that it is 5 denier or less, More preferably, it is 4.5 denier or less.
- 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.
- single yarn fineness becomes small covering property improves and, as a result, the air permeability of a 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.
- the F / F friction coefficient relative ratio value means a value obtained by dividing the interfiber static friction coefficient F / F ⁇ s of polyethylene terephthalate yarn by the fibre-metal intermetallic friction coefficient F / M ⁇ s. It is preferable that the F / F friction coefficient relative ratio value is 1.5 or more, and more preferably, a yarn having a characteristic of 2.0 or more is suitable as a fabric for an air bag. If the F / F friction coefficient relative ratio value is less than 1.5, it is not preferable because the interfiber friction coefficient is insufficient and the bar part of the edge part is increased in the airbag cushion development test.
- the type of spinning oil may be either an emulsion type or a solvent type, but it is preferable to use an oil having a relatively high F / F friction coefficient as compared to the F / M friction coefficient.
- a polyethylene terephthalate yarn for an air bag was manufactured by spinning the selected spinning oil in an emulsion type spinning oil with an adhesion amount of 0.6% OPU.
- the polyethylene terephthalate fiber produced by the manufacturing method of the present invention can use an air jet or a water jet loom, but since the residual oil content of the fabric is preferably 0.1% by weight or less, the dropping property of the oil adhered to the fiber In consideration of this, it is preferable to weave water jet rooms. Furthermore, after weaving, it is preferable to perform refining treatment and hot set treatment at 160 to 190 ⁇ .
- the woven fabric may be coated with a weight of 15 to 60 g / m 2 using a coating agent selected from silicone, polyurethane, acrylic, neoprene and chloroprene to ensure low breathability suitable for airbag fabric.
- a coating agent selected from silicone, polyurethane, acrylic, neoprene and chloroprene to ensure low breathability suitable for airbag fabric.
- I.V. 1/4 ⁇ [(R.V.-1) / C] + 3/4 ⁇ (In R.V./C)
- C represents the concentration of the sample in solution (g / 100ml).
- 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.
- the terminal carboxyl group content is analyzed by GRI (Geosynthetic Research Institute) Test Method “GG7” method and expressed in mmol / kg units.
- the sample 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.
- the fabric was allowed to stand for 10 hours or more in a standard condition (20 ° C., 65% relative humidity) according to ASTM D 5034. The tensile strength of the fabric was measured.
- the fabric was fabricated after standing for 24 hours or more under standard conditions (20 ° C, 65% relative humidity) according to the tongue method according to ASDM D 2261. Thermal strength was measured.
- the air permeability of the fabric was measured under 125 Pa pressure according to the ASDM 737 method.
- Dough for airbags was prepared by using a polyethylene terephthalate yarn of the properties shown in Table 1 to be 50 ⁇ 50 fabrics per inch with a waterjet loom.
- the spinning oil used was selected from the emulsion type spinning oil of Takemoto Co., Ltd., which had a relatively high F / F friction coefficient (product name: TNX-021) and spun with an OPU 0.6% adhesion amount.
- Dough for airbags was prepared in the same manner as in Example 1 using polyethylene terephthalate yarns having the properties shown in Table 1.
- the spinning oil used was selected to have a relatively low F / F coefficient of friction (Product Name: TN-0071T) among the Croda-wool's solvent type spinning oil, and was spun with 0.6% OPU adhesion.
- Example 2 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 coating with a weight of 25g / m 2 using a silicone coating agent to prepare a coating fabric for air bags. Evaluation of the physical properties of the fabric thus prepared and the airbag cushion development test results are shown in Table 2 below.
- Polyethylene terephthalate yarns produced under GR4 temperature of 250 ° C, GR5 temperature of 170 ° C, and relaxation ratio of 9.2% have the characteristics shown in Table 3 below. Plain as possible to prepare a dough for airbags.
- Example 3 The dough prepared in Example 3 was passed through an aqueous bath at 95 ° C. to refine and heat shrink the dough, 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.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Woven Fabrics (AREA)
- Air Bags (AREA)
- Artificial Filaments (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
Abstract
Description
구분 | 규격 | 단사섬도(den) | 강도(g/den) | 신도(%) | F/F마찰계수 상대비 | 1.0g/d에서 신도(%) | 4.5g/d에서 신도(%) | 7.0g/d에서 절단시까지의 신도(%) | CEG 함량(mmol/kg) |
실시예1 | 500d/120f | 4.2 | 9.0 | 22.6 | 3.16 | 0.9 | 9.7 | 5.1 | 25.4 |
비교예1 | 500d/120f | 4.1 | 9.1 | 20.3 | 1.43 | 0.9 | 9.8 | 5.3 | 25.2 |
구분 | 인장강도(경사×위사, kgf) | 인열강도(경사×위사, kgf) | 공기투과도(CFM) | 에어백 쿠션전개 시험 |
실시예2 | 223×221 | 27.3×27.7 | 0.1이하 | PASS |
비교예2 | 219×215 | 27.0×28.6 | 0.1이하 | FAIL |
구분 | 규격 | 단사섬도(den) | 강도(g/den) | 신도(%) | CEG(mmol/kg) | 최대열응력(g/den) | 1.0g/d에서 신도(%) | 4.5g/d에서 신도(%) | 7.0g/d에서 절단시까지의 신도(%) |
실시예3 | 500d/120f | 4.2 | 9.0 | 22.6 | 25.1 | 0.29 | 0.9 | 9.7 | 5.1 |
비교예3 | 630d/48f | 13.2 | 8.1 | 12.3 | 25.3 | 0.53 | 0.8 | 5.4 | 4.0 |
구분 | 인장강도(경사×위사, kgf) | 인열강도(경사×위사, kgf) | 공기투과도(CFM) | 에어백 쿠션전개 시험 |
실시예4 | 223×221 | 27.3×27.7 | 0.1이하 | PASS |
비교예4 | 241×239 | 27.9×28.8 | 0.1이하 | FAIL |
Claims (7)
- 고유점도가 0.8∼1.3인 폴리에틸렌테레프탈레이트 칩을 방사하여 제조된 에어백용 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% 이상이고, 단사 섬도가 5데니어 이하인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.
- 청구항 1에 있어서, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트는 원사의 F/F 정마찰계수를 F/M 정마찰 계수로 나눈 값이 1.5이상인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.
- 청구항 1에 있어서, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트는 말단 카르복실기(CEG) 함량이 35mmol/kg 이하인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.
- 청구항 1에 있어서, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트는 최대 열응력이 0.2~0.5g/d인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.
- 청구항 1에 있어서, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트는 총섬도가 150 내지 1000 데니어인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.
- 청구항 1의 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용하여 제직된 에어백용 직물.
- 청구항 6의 에어백용 직물에 실리콘계, 폴리우레탄계, 아크릴계, 네오프렌 및 클로로프렌계로 이루어진 군에서 선택된 1종의 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) 이하
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2783546A CA2783546C (en) | 2009-12-24 | 2010-12-14 | Polyethylene terephthalate fiber for air-bags and textiles made from same |
JP2012544379A JP2013514465A (ja) | 2009-12-24 | 2010-12-14 | エアバッグ用ポリエチレンテレフタレート繊維及びこれを利用した織物 |
US13/517,069 US20120263401A1 (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 |
CN201080058616.4A CN102713031B (zh) | 2009-12-24 | 2010-12-14 | 气囊用聚对苯二甲酸乙二醇酯纤维及由其制造的织物 |
MX2012007451A MX2012007451A (es) | 2009-12-24 | 2010-12-14 | Fibra de tereftalato de polietileno para bolsas de aire y textiles hechos de la misma. |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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KR1020090130817A KR101295696B1 (ko) | 2009-12-24 | 2009-12-24 | 에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물 |
KR10-2009-0130817 | 2009-12-24 | ||
KR10-2009-0132770 | 2009-12-29 | ||
KR1020090132770A KR101295697B1 (ko) | 2009-12-29 | 2009-12-29 | 에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물 |
Publications (3)
Publication Number | Publication Date |
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WO2011078513A2 true WO2011078513A2 (ko) | 2011-06-30 |
WO2011078513A3 WO2011078513A3 (ko) | 2011-11-10 |
WO2011078513A8 WO2011078513A8 (ko) | 2012-06-21 |
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PCT/KR2010/008942 WO2011078513A2 (ko) | 2009-12-24 | 2010-12-14 | 에어백용 폴리에틸렌테레프탈레이트 섬유 및 이를 이용한 직물 |
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US (1) | US20120263401A1 (ko) |
EP (1) | EP2518195B1 (ko) |
JP (1) | JP2013514465A (ko) |
CN (1) | CN102713031B (ko) |
CA (1) | CA2783546C (ko) |
MX (1) | MX2012007451A (ko) |
WO (1) | WO2011078513A2 (ko) |
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US20130224468A1 (en) * | 2010-09-17 | 2013-08-29 | Kolon Industries, Inc. | Polyester fiber and method for preparing the same |
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GB2495645A (en) * | 2010-06-24 | 2013-04-17 | Hyosung Corp | Fabric for airbag, using polyethylene terephthalate fiber with excellent heat resistance |
CN105452558B (zh) * | 2013-08-13 | 2018-02-13 | 旭化成株式会社 | 涂层织物 |
KR20160000443A (ko) | 2014-06-24 | 2016-01-04 | 코오롱인더스트리 주식회사 | 에어백용 폴리에스테르 원단의 제조방법 |
EP3686326A4 (en) * | 2017-09-22 | 2021-10-06 | Kolon Industries, Inc. | HIGH STRENGTH POLYETHYLENE TEREPHTHALATE FIBER AND ITS MANUFACTURING PROCESS |
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JPH06306728A (ja) * | 1993-04-21 | 1994-11-01 | Toray Ind Inc | エアバッグ用基布 |
JPH06313265A (ja) * | 1993-04-28 | 1994-11-08 | Unitika Ltd | エアーバツグ用シートの製造方法 |
JPH0748717A (ja) * | 1993-08-05 | 1995-02-21 | Teijin Ltd | エアバッグ基布用ポリエステル繊維 |
JP3180524B2 (ja) * | 1993-09-20 | 2001-06-25 | 東レ株式会社 | エアバッグ用基布 |
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CA2141768A1 (en) * | 1994-02-07 | 1995-08-08 | Tatsuro Mizuki | High-strength ultra-fine fiber construction, method for producing the same and high-strength conjugate fiber |
JP2944891B2 (ja) * | 1994-07-19 | 1999-09-06 | 帝人株式会社 | エアバッグ基布用ポリエステル繊維 |
JPH08134717A (ja) * | 1994-11-04 | 1996-05-28 | Unitika Ltd | エアバッグ用ポリエステル繊維の製造方法 |
JPH08158153A (ja) * | 1994-12-07 | 1996-06-18 | Teijin Ltd | エアバッグ基布用ポリエステル糸条 |
JP2001254243A (ja) * | 2000-03-09 | 2001-09-21 | Toray Ind Inc | エアバッグ用基布およびエアバッグ |
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JP2007284826A (ja) * | 2006-04-18 | 2007-11-01 | Toray Ind Inc | エアバッグ用基布の製造方法 |
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GB2495645A (en) * | 2010-06-24 | 2013-04-17 | Hyosung Corp | Fabric for airbag, using polyethylene terephthalate fiber with excellent heat resistance |
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- 2010-12-14 JP JP2012544379A patent/JP2013514465A/ja active Pending
- 2010-12-14 WO PCT/KR2010/008942 patent/WO2011078513A2/ko active Application Filing
- 2010-12-14 CA CA2783546A patent/CA2783546C/en active Active
- 2010-12-14 CN CN201080058616.4A patent/CN102713031B/zh active Active
- 2010-12-14 EP EP10839710.0A patent/EP2518195B1/en active Active
- 2010-12-14 MX MX2012007451A patent/MX2012007451A/es active IP Right Grant
- 2010-12-14 US US13/517,069 patent/US20120263401A1/en not_active Abandoned
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US20130224468A1 (en) * | 2010-09-17 | 2013-08-29 | Kolon Industries, Inc. | Polyester fiber and method for preparing the same |
US9951176B2 (en) * | 2010-09-17 | 2018-04-24 | Kolon Industries, Inc. | Polyester fiber and method for preparing the same |
Also Published As
Publication number | Publication date |
---|---|
WO2011078513A8 (ko) | 2012-06-21 |
EP2518195B1 (en) | 2018-10-31 |
CN102713031B (zh) | 2014-09-17 |
US20120263401A1 (en) | 2012-10-18 |
CA2783546A1 (en) | 2011-06-30 |
EP2518195A4 (en) | 2013-08-07 |
JP2013514465A (ja) | 2013-04-25 |
EP2518195A2 (en) | 2012-10-31 |
CN102713031A (zh) | 2012-10-03 |
CA2783546C (en) | 2015-12-22 |
WO2011078513A3 (ko) | 2011-11-10 |
MX2012007451A (es) | 2012-10-15 |
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