WO2019139406A1 - Polyethylene terephthalate yarn for airbag - Google Patents

Polyethylene terephthalate yarn for airbag Download PDF

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Publication number
WO2019139406A1
WO2019139406A1 PCT/KR2019/000457 KR2019000457W WO2019139406A1 WO 2019139406 A1 WO2019139406 A1 WO 2019139406A1 KR 2019000457 W KR2019000457 W KR 2019000457W WO 2019139406 A1 WO2019139406 A1 WO 2019139406A1
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WO
WIPO (PCT)
Prior art keywords
fabric
airbag
yarn
polyethylene terephthalate
multifilament
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PCT/KR2019/000457
Other languages
French (fr)
Korean (ko)
Inventor
정일원
김성주
Original Assignee
효성첨단소재 주식회사
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Publication of WO2019139406A1 publication Critical patent/WO2019139406A1/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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/23Inflatable members
    • B60R21/235Inflatable members characterised by their material
    • 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
    • D01D5/088Cooling filaments, threads or the like, leaving the spinnerettes
    • 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
    • D01D5/096Humidity control, or oiling, of filaments, threads or the like, leaving the spinnerettes
    • 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
    • D01D5/098Melt spinning methods with simultaneous stretching
    • 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
    • D02J1/22Stretching or tensioning, shrinking or relaxing, e.g. by use of overfeed and underfeed apparatus, or preventing stretch
    • 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
    • D02J1/22Stretching or tensioning, shrinking or relaxing, e.g. by use of overfeed and underfeed apparatus, or preventing stretch
    • D02J1/228Stretching in two or more steps, with or without intermediate steps
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • D03D1/02Inflatable articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/23Inflatable members
    • B60R21/235Inflatable members characterised by their material
    • B60R2021/23504Inflatable members characterised by their material characterised by material
    • B60R2021/23509Fabric
    • 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

Definitions

  • the tear strength of the fabric exposed to a high temperature environment must be sufficiently high to reduce the damage of the airbag due to the tearing of the fabric during the airbag deployment .
  • the airbag fabric requires various characteristics such as low air permeability for smooth deployment at the time of collision, high energy absorbing ability for preventing damage breakage of the airbag itself, and foldability of the fabric itself for improving the storage capacity.
  • Nylon 66 materials have been mainly used as the fibers suitable for the airbag fabrics, but in recent years, there has been a growing interest in fiber materials other than nylon 66 due to economical reasons such as cost reduction.
  • Japanese Patent Application Laid-Open Publication No. 1-41438 discloses that the above-mentioned object is achieved by manufacturing a fabric for airbags made of fibers having a strength of 8.5 g / d or more and a monofilament fineness of 3 denier or less .
  • the airbag fabric disclosed in the above publication is substantially a so-called coated fabric coated with an elastomer such as chloroprene rubber on the surface of the fabric, , The strength and retention properties are surely satisfied, but the point that maintenance of low air permeability can not be sufficiently satisfied.
  • Japanese Laid-Open Patent Publication No. 4-201650 discloses a polyamide multifilament comprising a plurality of single filaments each having a single-filament fineness of 1.0 to 12 denier and a single filament deformation of 1.5 to 7.0, A technique for obtaining a fabric for weaving is disclosed.
  • the technology of manufacturing the airbag fabric of the above publication also satisfies the requirement as an airbag fabric when applied to a covering fabric.
  • the problem of air permeability when applied to a non-bloomed fabric, when applied to a non-bloomed fabric, .
  • U.S. Patent No. 5,073,418 discloses a method of making a cloth with a yarn of 500 denier or less and then performing a color rendering in order to reduce the air permeability by knife rendering to improve airtightness.
  • a color rendering in order to reduce the air permeability by knife rendering to improve airtightness.
  • European Patent Publication No. 416483 discloses a heat shrinkable or heat shrinkable non-coated fabric for airbag production using a synthetic filament yarn having a substantially symmetrical structure with a denier of 300 to 400 dtex, So that the tear strength of the fabric is lowered.
  • European Patent Publication No. 436950 discloses a process for making a fabric made of a polyamide filament yarn having a heat shrinkage rate of 6 to 15% at 160 DEG C and a fabric structure of at least nearly symmetric at a temperature of 60 to 140 DEG C in an aqueous bath, A synthetic filament yarn is rapidly heated in an aqueous bath of a high temperature so that a product fabric of the fabric can be applied to various kinds of fabrics for airbags Since the fabric must exhibit stable performance even when exposed to the climatic environment, the tear strength of the fabric exposed to the high temperature environment must be sufficiently high to reduce the damage of the bag due to tearing of the fabric during the airbag deployment.
  • the airbag fabric to be mounted on a vehicle must exhibit stable performance even when exposed to various climatic environments. Therefore, the tear strength of the fabric exposed to the high temperature environment must be sufficiently high, It is possible to reduce the damage of the airbag caused by the airbag, and the strength of the yarn in the high temperature tensile test of 85 ° C is 6.5gf / den. Or more and a breaking elongation of 19% or more, the tear strength of the fabric is higher even after aging at 80 DEG C, and the object is to provide a polyethylene terephthalate fiber for airbags suitable for high temperature environments.
  • 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 dl / g, wherein the yarn has a strength of 6.5 gf / dec.
  • a polyethylene terephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3 dl / g, wherein the yarn has a strength of 6.5 gf / dec.
  • the toughness of the polyethylene terephthalate yarn measured by the high temperature tensile test at 85 ⁇ is 32 ⁇ 10 -1 g / d or more.
  • the polyethylene terephthalate multifilament is characterized in that the total fineness of the polyethylene terephthalate multifilament is 100 to 1000 denier and the fineness of the multifilament is 2 to 10.
  • the airbag fabric is characterized in that the airbag fabric aged at 80 DEG C for 48 hours has an intrinsic tear strength of 19 kgf or more.
  • the tear strength of the fabric exposed to the high temperature environment must be sufficiently high to reduce the breakage of the airbag due to tearing of the fabric during the airbag deployment process .
  • the airbag fabric has a yarn strength of 6.5 gf / den in 85 ° C high temperature tensile test. And the elongation at break of 19% or more, the tear strength of the fabric is higher even after aging at 80 < 0 > C.
  • FIG. 1 is a schematic view showing a process for producing a fiber for a polyethylene terephthalate airbag.
  • the present invention relates to a polyethylene terephthalate multifilament prepared by spinning a polyethyleneterephthalate chip having an intrinsic viscosity of 0.8 to 1.3 dl / g by adjusting the force-deformation curve of the polyethylene terephthalate multifilament to a fabric for an airbag,
  • the present invention provides a fabric for an airbag that is improved in the portion of the airbag.
  • the present invention relates to a polyethylene terephthalate (PET) obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity (IV) of 0.8 to 1.3 dl / g for safely absorbing instantaneous impact energy of an exhaust gas generated by explosive explosion of an airbag in an airbag fabric. Multifilaments are used.
  • a polyester yarn having an intrinsic viscosity of less than 0.8 dl / g is not suitable because it does not provide a yarn having sufficient toughness.
  • the intrinsic viscosity (IV) exceeds 1.3 dl / g, the radioactivity is deteriorated.
  • polyester chips having intrinsic viscosity in the range of 0.80 to 1.30 dl / g are melted by setting the temperature condition of extruder 1 to be low.
  • the temperature of the molten polymer is set to 290 to 300 DEG C and the temperature is applied for keeping the gear pump 2 warm.
  • the set temperature of the keeping temperature of the gear pump 2 is lowered,
  • the temperature of the polymer is adjusted to be 290 to 300 ° C so that the pyrolysis due to heat generation or high temperature is not caused to the maximum, so that the properties of the polymer itself are not lost as much as possible.
  • the diameter of the nozzle hole of the spinneret 3 is set to 0.3 to 0.6 phi and the ratio of the hole length to the hole diameter (L / D) of the spinneret 3 is set to 2 to 3, Thereby imparting a high degree of extensibility.
  • the length of the hood heater 4 is increased to 250 to 400 mm and the temperature of the hood heater 4 is raised to 300 to 380 ° C so that the spun fibers are subjected to the conditions in the hood .
  • the amorphous and non-oriented yarns thus formed are supplied to the air supply pipe inlet 5 in a large amount of air having a temperature of 10 to 17 ⁇ ⁇ and discharged to the air exhaust pipe outlet 6 so as to be rapidly quenched .
  • the supply amount was made 50 to 90 mmAq (aqua) and the exhaust amount was made 70 to 100 mmAq.
  • a certain type of guide is applied before the godet roller (GR) 2, GR 3 is applied to GR 3 and GR 3 in order to ensure that the width of the contact area is in the range of 1,000 ⁇ 3,000 (mm 2 ) ( 2 mm to 10,000 mm) of the surface of the multifilament yarn on the surface of the upper surface of the first and second rollers GR 1 and GR 4, and after the second drawing is performed on the GR 3 and GR 4, the rollers GR 4 and GR 5 are relaxed, 13).
  • the strength of the yarn is 6.5 gf / And the elongation at break of 19% or more, the tear strength of the fabric is higher even after aging at 80 < 0 > C.
  • the polyethylene terephthalate raw material of the present invention has a toughness of 32 x 10 < -1 > g / d or more as measured in a high temperature tensile test at 85 deg.
  • the strength of the yarn is 6.5 gf / And the cutting elongation is 19% or more
  • the process used for forming the yarn in the hood is such that the polyethylene terephthalate multifilament has a structure that is as amorphous and non-oriented as possible when passing through a hood heater (4) And the thus formed amorphous and non-oriented yarns are rapidly cooled in the cooling zones 5 and 6 to maintain the amorphous and no-orientation states as much as possible to enable the operation at a high stretching ratio.
  • the factor that greatly affects the multifilament of the present invention is the contact width of the filament yarn in the GR in which the initial primary drawing and the secondary drawing are performed. By adjusting the contact width, a desired force-strain curve of the multifilament of the present invention is obtained.
  • the polyethylene terephthalate filaments passing through the cooling zones (5, 6) have contact areas of a certain width with the surfaces of GR 2 and GR 3, which have a great influence on the initial primary and secondary stretching.
  • the width of contact of the multifilament yarn with the surface of the godet roller where the initial primary stretching takes place is 2,000 to 4,000 mm 2 and the width of the multifilament yarn contacting the surface of the godet roller where the secondary stretching takes place is 7,000 to 9,000 mm 2 desirable.
  • the width of contact with the multifilament yarn on the surface of the godet roller where the initial primary elongation occurs is less than 2,000 mm 2 and / or the width of contact with the multifilament yarn on the godet roller surface where the second elongation occurs is less than 7,000 mm 2 . It is difficult to obtain a preferable multifilament of the present invention because heat transfer is difficult and the unevenness of the emulsion results in lowering in stretchability.
  • the contact area increases in proportion to the number of turns (turn number) of the filaments wound on the drawn GR. That is, the contact width can be adjusted by adjusting the number of windings.
  • Another important factor is to adjust the warp wound on the GR by applying a constant shape guide to keep the yarn spread constant between the GRs.
  • a prism-shaped guide it is preferable to use a prism-shaped guide. If the shape of the V-shaped guide is narrow, the width decreases and eventually the contact width decreases. If the guide is in the form of a pratt, the width increases and the contact width increases.
  • the guide groove width is preferably 2.5 to 6.5 mm. More preferably 3 to 5 mm, and most preferably 4 mm.
  • the width of the prat-shaped guide groove is 6.5 mm, there is a problem that pin yarn is generated due to the contact between the pillars.
  • the width of the V-shaped guide groove is 2.5 mm, the godet roller is not uniformly heat- there is a problem.
  • Another factor controlling the contact width is the stretching tension of the roller, the stretching temperature, and the amount of emulsion.
  • the width of contact of the multifilament yarn to the surface of GR 2 which has a large influence on the primary drawing by organically binding the various factors, is 2,000 to 4,000 mm 2 , and GR 3
  • the width of the surface of the multifilament yarn contacting the surface is adjusted to 7,000 to 9,000 mm 2 , thereby obtaining the desired multifilament of the present invention.
  • the polyethylene terephthalate produced through such a process had a yarn strength of 6.5 gf / And the elongation at break is 19% or more.
  • the polyethylene terephthalate raw material has a toughness of 32 x 10 < -1 > g / d or more as measured in a high temperature tensile test at 85 deg.
  • the total fineness of the polyethylene terephthalate multifilament for an airbag of the present invention is preferably 100 to 1000 denier, more preferably 200 to 700 denier.
  • the fabric for airbags is satisfactory in terms of retractability but is not preferable because of the lack of strength and the bag may rupture at the time of deployment and collision after deployment.
  • the total fineness exceeds 1000 denier, sufficient strength is obtained as an airbag, which can be satisfied from the viewpoint of safety, but the fabric becomes thick and the retention becomes poor.
  • the monofilament fineness of the multifilament constituting the fabric for an airbag is preferably 5 denier or less, and more preferably 4.5 denier or less.
  • the resultant fabric is flexible and excellent in folding property and storage stability. Further, the single yarn fineness is reduced and the covering property is improved, and as a result, the air permeability of the fabric can be suppressed. If the single yarn fineness exceeds 5 denier, it is not preferable because the folding property and the storage ability of the fabric are deteriorated, and the low air permeability is deteriorated and the sufficient function as the airbag fabric can not be exhibited.
  • a polyester chip having an intrinsic viscosity of 1.00 dl / g was extruded through a nozzle having a diameter of 0.4 mm, a ratio of length to diameter (L / D) of 3 and a number of holes of 120, cooled with air at 15 ° C, And the temperature of the godet roller 2 was 100 ⁇ and the godet roller 3 temperature was 125 ⁇ .
  • the spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were the conditions specified in Table 1, and the godet roller 2
  • the number of windings of the filaments in the godet roller 3 (second elongation point) is 7, the shape of the guide before the godet rollers 2 and 3 is prat, and the width of the guide groove is 4 mm, and the speed of the godet roller GR 4 was set at 2700 m / min, and 500 denier / 120f was radiated and stretched.
  • the main conditions are the same as those of Examples 1, 2 and 3, and the spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were set as shown in Table 1.
  • the guides of the godet rollers 2 and 3 were wide, The width of the groove is 6.5 mm, the number of filaments wound on the godet roller 2 is 5, and that on the godet roller 3 is 7.
  • the main conditions were the same as in Comparative Example 1, and the spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were set as shown in Table 1.
  • the width of the guide grooves was 2.5 mm), the number of times of winding is 6 in the godet roller 2 of the filament, and 8 in the godet roller 3.
  • Phenol and 1,1,2,3-tetrachloroethanol in a weight ratio of 6: 4 was dissolved in a reagent (90 DEG C) for 90 minutes so as to have a concentration of 0.4 g / 100 mL, and the solution was dissolved in Ubbelohde
  • the solution was transferred to a viscometer and maintained at 30 ° C in a thermostatic chamber for 10 minutes.
  • the drop number of the solution was obtained by using a viscometer and an aspirator.
  • the number of drops of the solvent was also determined by the same method, and then the RV value and the IV value were calculated by the following equation.
  • C represents the concentration (g / 100 mL) of the sample in the solution.
  • the yarn is allowed to stand in a standard temperature condition, that is, in a constant temperature and humidity room at a temperature of 25 ° C and a relative humidity of 65% RH for 24 hours, and then the sample is measured by a tensile tester using the ASTM 2256 method.
  • the sample length is 250 mm
  • the tensile speed is 300 mm / min
  • the initial load is 0.05 gf /
  • the test was carried out using a universal material testing machine (Instron, model 5565) equipped with an environmental chamber of 3119-600 Series for testing at a high temperature, not at room temperature. The sample was mounted, and the strength test was carried out when the chamber temperature reached 85 ⁇ . Tensile tests were carried out five times per sample and average values were used.
  • the shrinkage of the yarn is measured in a test light shrinkage tester at 180 ° C for 2 minutes under a condition of 0.05 gf / denier load.
  • the yarn thus produced is woven in a water jet loom in plain weave with an oblique density of 50 and an oblique density of 49, and then dried through a can dryer having a surface temperature of 180 ° C.
  • the air bag fabric thus manufactured was subjected to hot tear strength test in the following manner.
  • the fabric for airbags was aged at 80 DEG C for 48 hours and left for 24 hours under the conditions of 25 DEG C and 65% RH.
  • the tear strength of the fabrics was measured using a universal material testing machine (Instron, Model 4465) , The tear strength was calculated as an average value of the maximum peaks of peaks issued when the test pieces were torn while constantly pulling at a test speed of 50 mm / min.
  • Example 1 Example 2 Example 3 Comparative Example 1 Comparative Example 2 Radiation temperature 295 DEG C 295 DEG C 290 ° C 305 °C 305 °C Stretching cost 5.8 5.9 6.0 5.4 5.4 Relax ratio 9.0% 9.0% 8.5% 10.0% 11.0% Heat treatment temperature (godet roller temperature 4) 245 ° C 240 °C 235 ° C 245 ° C 250 °C The winding number of the filament at the godet roller 2 (first elongation point) 5 times 5 times 5 times 5 times 6 times The number of take-up times of the filament at the godet roller 3 (second elongation point) 7 times 7 times 7 times 7 times 8 times The shape of the guide before the godet rollers 2 and 3 and the width of the guide groove Pratt shape, width 4mm Pratt shape, width 4mm Pratt shape, width 4mm Pratt shape, width 6.5mm V groove shape, width 2.5mm 85 °C Measured yarn strength (gf / den.) 7.2 7.3 7.5

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Artificial Filaments (AREA)

Abstract

A fabric for an airbag equipped for an automobile needs to exert stable performance even when exposed to various climatic environments, and thus the tearing strength of a fabric exposed to a high-temperature environment must be sufficiently high to reduce the breakage of an airbag due to tearing of the fabric during the development of the airbag, so that the present invention provides a polyethylene terephthalate fiber for an airbag, allowing a fabric for an airbag to express high tearing strength even after the exposure to a high-temperature environment of 80°C for 48 hours.

Description

에어백용 폴리에틸렌테레프탈레이트 원사Polyethylene terephthalate yarn for airbags
본 출원은 2018.1.11자 한국 특허 출원 제10-2018-0003734호에 기초한 우선권의 이익을 주장하며, 해당 한국 특허 출원의 문헌에 개시된 모든 내용은 본 명세서의 일부로서 포함된다.This application claims the benefit of priority based on Korean Patent Application No. 10-2018-0003734 filed on August 11, 2018, and the entire contents of the Korean patent application are incorporated herein by reference.
본 발명은 자동차에 장착되는 에어백용 직물은 다양한 기후 환경에 노출되어도 안정적인 성능을 발휘해야 하므로, 고온 환경에 노출된 직물의 인열강력이 충분히 높아야 에어백 전개 과정에서 직물이 찢어짐으로 인한 에어백의 파손을 줄일 수 있다.Since the fabric for an airbag mounted on an automobile must exhibit a stable performance even when exposed to various climatic environments, the tear strength of the fabric exposed to a high temperature environment must be sufficiently high to reduce the damage of the airbag due to the tearing of the fabric during the airbag deployment .
에어백 직물은 충돌 시에 원활하게 전개하기 위한 저통기성, 에어백 자체의 손상파열을 막기 위한 높은 에너지 흡수 능력 및 수납성 향상을 위한 직물 자체의 접힘성 등 여러가지 특성이 요구된다. 이러한 에어백 직물의 요구 특성에 적합한 섬유로는 나일론66 소재가 주로 사용되어 왔으나, 근래에는 비용 절감 등 경제성을 이유로 나일론66 이외의 섬유 소재에 대한 관심이 높아지고 있다. The airbag fabric requires various characteristics such as low air permeability for smooth deployment at the time of collision, high energy absorbing ability for preventing damage breakage of the airbag itself, and foldability of the fabric itself for improving the storage capacity. Nylon 66 materials have been mainly used as the fibers suitable for the airbag fabrics, but in recent years, there has been a growing interest in fiber materials other than nylon 66 due to economical reasons such as cost reduction.
에어백으로서 적합한 강력 및 저통기성을 손상시키지 않고, 접힘성이 우수하며, 수납 용적이 작은 에어백을 실현시키는 기술이 많이 개시되어 있다. 예를 들면, 일본 특개평 1-41438 공보에는, 강도 8.5 g/d이상, 단사 섬도가 3데니어 이하의 섬유로 이루어지는 사조(絲條)로 에어백용 직물을 제조함으로써, 상기의 목적이 달성된다고 개시하고 있다. 상기 공보에는 피복 직물 및 비피복 직물의 차이에 관하여 전혀 언급되어 있지 않지만, 상기 공보에 개시된 에어백용 직물은 실질적으로는 직물의 표면에 클로로프렌고무 등의 엘라스토머를 도포한 이른바 피복 직물로서, 비피복 직물에 당해 기술을 적용한 경우에는 강력 및 수납성은 확실히 만족시키나, 저통기성의 유지라는 점은 충분히 만족시킬 수 없었다.A large number of techniques for realizing an airbag that is excellent in collapsibility and small in storage capacity without damaging the strength and low air permeability suitable for the airbag have been disclosed. For example, Japanese Patent Application Laid-Open Publication No. 1-41438 discloses that the above-mentioned object is achieved by manufacturing a fabric for airbags made of fibers having a strength of 8.5 g / d or more and a monofilament fineness of 3 denier or less . Although no mention has been made on the difference between the coated fabric and the non-coated fabric in the above publication, the airbag fabric disclosed in the above publication is substantially a so-called coated fabric coated with an elastomer such as chloroprene rubber on the surface of the fabric, , The strength and retention properties are surely satisfied, but the point that maintenance of low air permeability can not be sufficiently satisfied.
또, 일본 특개평 4-201650 호 공보에는, 단사 섬도 1.0~12데니어, 단사 변형도 1.5~7.0인 이형 단면을 가지는 복수개의 단사로 이루어지는 폴리아미드 멀티필라멘트를 이용함으로써, 강력 및 접힘성이 우수한 에어백용 직물을 얻는 기술이 개시되어 있다. 그러나, 상기 공보의 에어백용 직물의 제조 기술도 피복 직물에 적용한 경우에는 에어백용 직물로서의 요구 특성을 만족시키지만, 비피폭 직물에 적용 시에는 통기성, 특히 봉제부에서의 통기성에 해결해야 할 과제가 남는 것이었다.Japanese Laid-Open Patent Publication No. 4-201650 discloses a polyamide multifilament comprising a plurality of single filaments each having a single-filament fineness of 1.0 to 12 denier and a single filament deformation of 1.5 to 7.0, A technique for obtaining a fabric for weaving is disclosed. However, the technology of manufacturing the airbag fabric of the above publication also satisfies the requirement as an airbag fabric when applied to a covering fabric. However, when applied to a non-bloomed fabric, the problem of air permeability, .
비피복 직물에 관한 기술로서는 일본 특개평 7-252740호 공보 기재의 방법이 있다. 상기 공보에는 편평율 1.5이상의 편평 단면사를 이용함으로써, 저통기성, 접힘성 및 수납성이 우수한 비피복 에어백용 직물이 얻어진다고 개시되어있다. 그러나, 상기 공보의 비피복 에어백용 직물은 저압(124Pa)하에서의 통기도가 0.3cc/㎠/sec 이상으로, 근래 요구되는 저통기성을 충분히 만족할 수 있는 것은 아니었다.As a technique relating to a non-coated fabric, there is a method described in Japanese Patent Application Laid-Open No. 7-252740. It is disclosed in this publication that a fabric for a non-covered airbag having a low air permeability, a folding property, and a high retractability is obtained by using a flat cross-section yarn having a flatness of 1.5 or more. However, the uncoated airbag fabric of the above publication has an air permeability of 0.3 cc / cm < 2 > / sec or more at a low pressure (124 Pa), and has not satisfactorily satisfied the low air permeability required recently.
미국특허 제 5,073,418호에는 칼렌더링에 의하여 공기투과도를 낮추어 기밀성 향상의 효과를 나타내기 위해 500데니어 이하의 원사로 원단을 제조한 후 칼렌더링하는 방법을 개시하고 있으나, 이와 같은 방법은 원단의 인열강도가 하락되는 문제가 있다.U.S. Patent No. 5,073,418 discloses a method of making a cloth with a yarn of 500 denier or less and then performing a color rendering in order to reduce the air permeability by knife rendering to improve airtightness. However, There is a problem that the price falls.
유럽특허 공보 제 416483호에는 실질적으로 대칭적 구조를 갖고, 데니어가 300~400dtex인 합성 필라멘트사를 이용한 에어백 제조용 열수축성 또는 열수축된 비피복 직물을 개시하고 있으나, 이와 같은 방법은 합성 필라멘트사가 열수축 공정에서 급격히 강력이 저하되어, 원단의 인열 강도가 하락되는 문제가 있다.European Patent Publication No. 416483 discloses a heat shrinkable or heat shrinkable non-coated fabric for airbag production using a synthetic filament yarn having a substantially symmetrical structure with a denier of 300 to 400 dtex, So that the tear strength of the fabric is lowered.
유럽특허 공보 제 436950호에는 160℃에서의 열풍 수축률이 6~15%이고 직물 구조가 적어도 거의 대칭인 폴리아미드 필라멘트사로 이루어진 직물을 수성욕 중에서 60~140℃의 온도에서 처리하는 것을 포함하는, 조밀한 조직을 갖는 피복 처리를 요하지 않는 공업용 직물의 제조 방법을 개시하고 있으나, 이와 같은 방법은 합성 필라멘트사가 고온의 수성욕에서 열수축이 급격히 진행되어 직물의 품본 발명은 자동차에 장착되는 에어백용 직물은 다양한 기후 환경에 노출되어도 안정적인 성능을 발휘해야 하므로, 고온 환경에 노출된 직물의 인열강력이 충분히 높아야 에어백 전개과정에서 직물이 찢어짐으로 인한 bag의 파손을 줄일 수 있다.European Patent Publication No. 436950 discloses a process for making a fabric made of a polyamide filament yarn having a heat shrinkage rate of 6 to 15% at 160 DEG C and a fabric structure of at least nearly symmetric at a temperature of 60 to 140 DEG C in an aqueous bath, A synthetic filament yarn is rapidly heated in an aqueous bath of a high temperature so that a product fabric of the fabric can be applied to various kinds of fabrics for airbags Since the fabric must exhibit stable performance even when exposed to the climatic environment, the tear strength of the fabric exposed to the high temperature environment must be sufficiently high to reduce the damage of the bag due to tearing of the fabric during the airbag deployment.
상기의 과제를 해결하고자 본 발명은 자동차에 장착되는 에어백용 직물은 다양한 기후 환경에 노출되어도 안정적인 성능을 발휘해야 하므로, 고온 환경에 노출된 직물의 인열강력이 충분히 높아야 에어백 전개과정에서 직물이 찢어짐으로 인한 에어백의 파손을 줄일 수 있어, 에어백용 직물이 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 원사로 제조된 직물은 80℃에서 에이징 후에도 직물의 인열강력이 더 높게 발현되어 고온 환경에 적합한 에어백용 폴리에틸렌테레프탈레이트 섬유를 제공하는 것을 목적으로 한다.In order to solve the above problems, the airbag fabric to be mounted on a vehicle must exhibit stable performance even when exposed to various climatic environments. Therefore, the tear strength of the fabric exposed to the high temperature environment must be sufficiently high, It is possible to reduce the damage of the airbag caused by the airbag, and the strength of the yarn in the high temperature tensile test of 85 ° C is 6.5gf / den. Or more and a breaking elongation of 19% or more, the tear strength of the fabric is higher even after aging at 80 DEG C, and the object is to provide a polyethylene terephthalate fiber for airbags suitable for high temperature environments.
상기한 바와 같은 목적을 달성하기 위하여 본 발명은, 고유점도가 0.8~1.3dl/g인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트에 있어서, 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트를 제공한다.In order to achieve the above object, 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 dl / g, wherein the yarn has a strength of 6.5 gf / dec. By weight and a elongation at break of 19% or more, based on the total weight of the poly (ethylene terephthalate) multifilament.
본 발명의 다른 적절한 실시 형태에 따르면, 상기 85℃ 고온 인장시험에서 측정한 폴리에틸렌테레프탈레이트 원사의 터프니스가 32×10 -1g/d 이상인 것이 특징이다.According to another preferred embodiment of the present invention, the toughness of the polyethylene terephthalate yarn measured by the high temperature tensile test at 85 캜 is 32 × 10 -1 g / d or more.
본 발명의 또 다른 적절한 실시 형태에 따르면, 상기 폴리에틸렌테레프탈레이트 멀티필라멘트는 폴리에틸렌테레프탈레이트 멀티필라멘트의 총섬도가 100 내지 1000 데니어이고, 멀티필라멘트의 섬도가 2 내지 10 인 것이 특징이다. According to another preferred embodiment of the present invention, the polyethylene terephthalate multifilament is characterized in that the total fineness of the polyethylene terephthalate multifilament is 100 to 1000 denier and the fineness of the multifilament is 2 to 10.
본 발명의 또 다른 적절한 실시 형태에 따르면, 상기 에어백용 직물은 80℃에서 48시간 에이징 한 에어백직물의 경사방향 인열강력이 19kgf이상인 것을 특징으로하는 에어백용 직물을 제공한다.According to another preferred embodiment of the present invention, the airbag fabric is characterized in that the airbag fabric aged at 80 DEG C for 48 hours has an intrinsic tear strength of 19 kgf or more.
본 발명의 자동차에 장착되는 에어백용 직물은 다양한 기후 환경에 노출되어도 안정적인 성능을 발휘해야 하므로, 고온 환경에 노출된 직물의 인열강력이 충분히 높아야 에어백 전개 과정에서 직물이 찢어짐으로 인한 에어백의 파손을 줄일 수 있다. 에어백용 직물이 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 원사로 제조된 직물은 80℃에서 에이징 후에도 직물의 인열강력이 더 높게 발현된다.Since the airbag fabric to be mounted on the automobile of the present invention must exhibit stable performance even when exposed to various climatic environments, the tear strength of the fabric exposed to the high temperature environment must be sufficiently high to reduce the breakage of the airbag due to tearing of the fabric during the airbag deployment process . The airbag fabric has a yarn strength of 6.5 gf / den in 85 ° C high temperature tensile test. And the elongation at break of 19% or more, the tear strength of the fabric is higher even after aging at 80 < 0 > C.
도 1은 폴리에틸렌테레프탈레이트 에어백용 섬유의 제조공정 개략도이다.BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic view showing a process for producing a fiber for a polyethylene terephthalate airbag.
이하 도면과 실시예를 바탕으로 본 발명을 더욱 상세히 설명한다.Best Mode for Carrying Out the Invention The present invention will be described in more detail based on the drawings and examples.
본 발명은 다양한 변경을 가할 수 있고 여러 가지 실시예를 가질 수 있는바, 특정 실시예들을 도면에 예시하고 상세한 설명에 상세하게 설명하고자 한다.While the invention is susceptible to various modifications and alternative forms, specific embodiments thereof are shown by way of example in the drawings and will herein be described in detail.
그러나, 이는 본 발명을 특정한 실시 형태에 대해 한정하려는 것이 아니며, 본 발명의 사상 및 기술 범위에 포함되는 모든 변경, 균등물 내지 대체물을 포함하는 것으로 이해되어야 한다. 본 발명을 설명함에 있어서 관련된 공지 기술에 대한 구체적인 설명이 본 발명의 요지를 흐릴 수 있다고 판단되는 경우 그 상세한 설명을 생략한다.It should be understood, however, that the invention is not intended to be limited to the particular embodiments, but includes all modifications, equivalents, and alternatives falling within the spirit and scope of the invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.
본 발명은 고유점도가 0.8~1.3dl/g 인 폴리에틸렌테레프탈레이트 칩을 방사하여 제조된 폴리에틸렌테레프탈레이트 멀티필라멘트의 힘-변형 곡선을 조절하여 에어백용 직물에 적용함으로써 에어백 쿠션 전개 시험에서 터지지 않도록 변부 봉재 부분이 터짐 현상을 개선된 에어백용 직물을 제공한다.The present invention relates to a polyethylene terephthalate multifilament prepared by spinning a polyethyleneterephthalate chip having an intrinsic viscosity of 0.8 to 1.3 dl / g by adjusting the force-deformation curve of the polyethylene terephthalate multifilament to a fabric for an airbag, The present invention provides a fabric for an airbag that is improved in the portion of the airbag.
본 발명은 에어백 내부의 화약 폭발로 발생하는 배출 가스의 순간적인 충격에너지를 에어백 직물이 안전하게 흡수하기 위해서 고유점도(IV)가 0.8~1.3dl/g인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용한다. 수지의 고유 점도가 0.8dl/g 미만인 폴리에스테르 원사는 충분한 인성을 갖는 원사를 제공하지 않아 적당하지 않다. 또한 고유점도(IV)가 1.3dl/g을 초과하면 방사성이 떨어진다.The present invention relates to a polyethylene terephthalate (PET) obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity (IV) of 0.8 to 1.3 dl / g for safely absorbing instantaneous impact energy of an exhaust gas generated by explosive explosion of an airbag in an airbag fabric. Multifilaments are used. A polyester yarn having an intrinsic viscosity of less than 0.8 dl / g is not suitable because it does not provide a yarn having sufficient toughness. When the intrinsic viscosity (IV) exceeds 1.3 dl / g, the radioactivity is deteriorated.
본 발명을 첨부된 도면에 따라 구체적으로 설명한다. The present invention will be described in detail with reference to the accompanying drawings.
도 1에서 고유점도가 0.80 ~ 1.30dl/g범위의 폴리에스테르 칩을 익스트루더(1)의 온도 조건을 낮게 설정하여 용융한다. 이 때 용융된 폴리머의 온도를 290 ~ 300℃로 하고 기어펌프(2)의 보온을 위해 온도를 부여하는 데 이때도 기어펌프(2)의 보온의 설정 온도를 낮게 하여 기어펌프(2)를 통과하는 폴리머의 온도를 290 ~ 300℃가 될 수 있도록 조정하여 발열이나 고온에 의한 열분해가 최대한 일어나지 않도록 하여서 폴리머 자체가 가지고 있는 물성 특성을 최대한 잃지 않도록 한다. 방사 구금(3)의 노즐 홀의 직경을 0.3 ~ 0.6φ, 방사 구금(3)의 홀 길이와 홀 직경의 비율(L/D)을 2~3으로 하여 방사 드래프트를 일정 수준으로 유지하고 고뎃 롤러 상에서 높은 연신성을 부여 할 수 있도록 한다. 후드 히터(Hood Heater)(4)의 길이를 250 ~ 400mm로 늘리고 후드 히터(4)의 온도를 300 ~ 380℃로 높여 방사된 섬유로 하여금 최대한 무정 및 무배향의 구조를 가질 수 있도록 후드 내의 조건을 만들어 준다. 이렇게 형성된 무정, 무배향의 사를 10 ~ 17℃ 온도를 가지는 공기의 많은 양을 공기 공급관 입구(5)로 공급하고, 공기 배기관 출구(6)로 배출 하여 빠른 냉각(Quenching)이 될 수 있도록 한다. 이 때, 급기량은 50 ~ 90mmAq(아쿠아)이 되게 하고 배기량은 70 ~ 100mmAq가 되도록 하였다. 상기 무정, 무배향 상태의 고화된 사를 방사 유제 공급장치(7)를 통해 적당량의 오일링을 거친 후, 고뎃 롤러(GR) 2 전에 일정한 형태의 가이드를 적용하여 GR 2 상의 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이를 1,000 ~ 3,000(mm 2) 정도 되게 만들어 GR 2과 GR 3에서 1차 연신을 잘 되게 한 다음 GR 3 상에서도 사의 퍼짐을 일정하게 유지할 수 있도록 하는 GR 3 전에 가이드를 적용하여 GR 3 상의 표면에 멀티필라멘트 사가 접촉하는 넓이를 2,000 ~ 10,000(mm 2) 정도 되게 만들어 GR 3과 GR 4 상에서 2차 연신을 수행이 잘되게 하고 고뎃 롤러 GR 4와 GR 5 사이에서 릴랙스를 시킨 후 권취롤러(13)에 권취한다.In Fig. 1, polyester chips having intrinsic viscosity in the range of 0.80 to 1.30 dl / g are melted by setting the temperature condition of extruder 1 to be low. At this time, the temperature of the molten polymer is set to 290 to 300 DEG C and the temperature is applied for keeping the gear pump 2 warm. At this time, too, the set temperature of the keeping temperature of the gear pump 2 is lowered, The temperature of the polymer is adjusted to be 290 to 300 ° C so that the pyrolysis due to heat generation or high temperature is not caused to the maximum, so that the properties of the polymer itself are not lost as much as possible. The diameter of the nozzle hole of the spinneret 3 is set to 0.3 to 0.6 phi and the ratio of the hole length to the hole diameter (L / D) of the spinneret 3 is set to 2 to 3, Thereby imparting a high degree of extensibility. The length of the hood heater 4 is increased to 250 to 400 mm and the temperature of the hood heater 4 is raised to 300 to 380 ° C so that the spun fibers are subjected to the conditions in the hood . The amorphous and non-oriented yarns thus formed are supplied to the air supply pipe inlet 5 in a large amount of air having a temperature of 10 to 17 占 폚 and discharged to the air exhaust pipe outlet 6 so as to be rapidly quenched . At this time, the supply amount was made 50 to 90 mmAq (aqua) and the exhaust amount was made 70 to 100 mmAq. After the solidified yarn in the amorphous and non-oriented state is passed through an appropriate amount of oil ring through the emulsifying agent supply device 7, a certain type of guide is applied before the godet roller (GR) 2, GR 3 is applied to GR 3 and GR 3 in order to ensure that the width of the contact area is in the range of 1,000 ~ 3,000 (mm 2 ) ( 2 mm to 10,000 mm) of the surface of the multifilament yarn on the surface of the upper surface of the first and second rollers GR 1 and GR 4, and after the second drawing is performed on the GR 3 and GR 4, the rollers GR 4 and GR 5 are relaxed, 13).
본 발명에 따르면, 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 원사로 제조된 직물은 80℃에서 에이징 후에도 직물의 인열강력이 더 높게 발현된다. According to the present invention, in the high temperature tensile test at 85 캜, the strength of the yarn is 6.5 gf / And the elongation at break of 19% or more, the tear strength of the fabric is higher even after aging at 80 < 0 > C.
본 발명의 폴리에틸렌테레프탈레이트 원사는 85℃ 고온 인장시험에서 측정한 터프니스가 32×10 -1g/d 이상인 것이 특징이다.The polyethylene terephthalate raw material of the present invention has a toughness of 32 x 10 < -1 > g / d or more as measured in a high temperature tensile test at 85 deg.
본 발명의 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 원사로 형성하기위해 사용된 공정은 폴리에틸렌테레프탈레이트 멀티필라멘트가 후드 히터(Hood Heater)(4) 통과 시 최대한 무정 및 무배향의 구조를 가질 수 있도록 후드 내의 조건을 만들어 주며, 이렇게 형성된 무정, 무배향의 사를 냉각구역(5, 6)에서 급속 냉각시켜 무정, 무배향 상태를 최대한 유지시켜 높은 연신비로 작업을 가능하도록 하는 단계를 포함한다.In the 85 DEG C high temperature tensile test of the present invention, the strength of the yarn is 6.5 gf / And the cutting elongation is 19% or more, the process used for forming the yarn in the hood is such that the polyethylene terephthalate multifilament has a structure that is as amorphous and non-oriented as possible when passing through a hood heater (4) And the thus formed amorphous and non-oriented yarns are rapidly cooled in the cooling zones 5 and 6 to maintain the amorphous and no-orientation states as much as possible to enable the operation at a high stretching ratio.
본 발명의 멀티필라멘트에 영향을 많이 주는 인자는 초기 1차 연신과 2차 연신이 일어나는 GR에서 필라멘트 사의 접촉 넓이이다. 상기 접촉 넓이를 조절함으로써 바람직한 본 발명의 멀티필라멘트의 힘-변형곡선이 얻어진다. 냉각구역(5,6)을 통과한 폴리에틸렌테레프탈레이트 필라멘트는 초기 1차 연신과 2차 연신에 많은 영향을 주는 GR 2과 GR 3 표면과 일정한 넓이의 접촉면적을 갖는다. 초기 1차 연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이는 2,000 ~ 4,000mm 2인 것이 바람직하며, 2차 연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이는 7,000 ~ 9,000mm 2인 것이 바람직하다. The factor that greatly affects the multifilament of the present invention is the contact width of the filament yarn in the GR in which the initial primary drawing and the secondary drawing are performed. By adjusting the contact width, a desired force-strain curve of the multifilament of the present invention is obtained. The polyethylene terephthalate filaments passing through the cooling zones (5, 6) have contact areas of a certain width with the surfaces of GR 2 and GR 3, which have a great influence on the initial primary and secondary stretching. It is preferable that the width of contact of the multifilament yarn with the surface of the godet roller where the initial primary stretching takes place is 2,000 to 4,000 mm 2 and the width of the multifilament yarn contacting the surface of the godet roller where the secondary stretching takes place is 7,000 to 9,000 mm 2 desirable.
초기 1차 연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이가 2,000mm 2 미만 및/또는 2차 연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이가 7,000mm 2 미만일 경우, 멀티필라멘트 간에 균일한 열전달이 어렵고, 유제 불균일으로 연신성의 저하 초래로 본 발명의 바람직한 멀티필라멘트를 얻기가 어렵다. In the case where the width of contact with the multifilament yarn on the surface of the godet roller where the initial primary elongation occurs is less than 2,000 mm 2 and / or the width of contact with the multifilament yarn on the godet roller surface where the second elongation occurs is less than 7,000 mm 2 , It is difficult to obtain a preferable multifilament of the present invention because heat transfer is difficult and the unevenness of the emulsion results in lowering in stretchability.
반대로, 초기 1차 연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이가 4,000mm 2 초과 및/또는 2차 고연신이 일어나는 고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이가 9,000mm 2 초과일 경우, 멀티필라멘트간 접촉에 의한 핀사 유발 및 Tar 발생과 같은 문제가 일어난다. 그러므로 적절한 접촉 면적을 가지게 하여 무정 무배향의 멀티필라멘트가 최대 연신성을 획득할 수 있도록 알맞게 조정되어야 한다.On the other hand, if the initial primary stretching takes place to the extent godet Saga multifilament contact with the roller surface than 4,000mm 2, and / or the second stretching and the extent to which this occurs godet Saga multifilament contact with the roller surface than 9,000mm 2, Problems such as pin yarn induction and tar occurrence due to contact between multifilament occur. Therefore, multifilaments with an amorphous orientation should be appropriately adjusted to achieve maximum extensibility with an appropriate contact area.
고뎃 롤러 표면에 멀티필라멘트 사가 접촉하는 넓이에 주는 인자는 여러 가지이다. 인자로는 접촉하는 넓이는 연신 GR에 권취된 팔라멘트의 권취 횟수(turn 수)에 비례하여 증가한다. 즉 권취 횟수를 조절하여 접촉 넓이를 조절할 수 있다.There are various factors that affect the extent to which the multifilament yarn contacts the surface of the godet roller. As a factor, the contact area increases in proportion to the number of turns (turn number) of the filaments wound on the drawn GR. That is, the contact width can be adjusted by adjusting the number of windings.
또 다른 중요한 인자로는, GR사이에 사의 퍼짐을 일정하게 유지할 수 있도록 일정한 형태가이드를 적용하여 GR에 권취된 사폭을 조절 하는 것이다. Another important factor is to adjust the warp wound on the GR by applying a constant shape guide to keep the yarn spread constant between the GRs.
본 발명에서는 가이드 형태가 프랫 형태인 것을 사용하는 것이 바람직하다. 가이드 형태가 좁은 브이홈의 형태이면 사폭이 줄어들어 결국 접촉 넓이가 줄어들고, 가이드가 프랫한 형태이면 사폭이 커져 접촉 넓이가 증가한다. In the present invention, it is preferable to use a prism-shaped guide. If the shape of the V-shaped guide is narrow, the width decreases and eventually the contact width decreases. If the guide is in the form of a pratt, the width increases and the contact width increases.
본 발명의 고뎃 롤러 2와 3 전의 가이드가 프랫 형태일 때는 가이드 홈 폭은 2.5 내지 6.5mm인 것이 바람직하다. 더욱 바람직하게는 3 내지 5mm이고, 가장 바람직하게는 4mm이다. 프랫 형태 가이드 홈 폭이 6.5mm인 경우에는 필라간 접촉에 의한 핀사가 생기는 문제가 있고, 브이 홈 형태 가이드 홈 폭이 2.5mm인 경우에는 고뎃 롤러에서 균일한 열전달이 이루어지지 않아 연신성이 저하되는 문제가 있다.When the godet rollers 2 and 3 of the present invention are in the form of a prat, the guide groove width is preferably 2.5 to 6.5 mm. More preferably 3 to 5 mm, and most preferably 4 mm. In the case where the width of the prat-shaped guide groove is 6.5 mm, there is a problem that pin yarn is generated due to the contact between the pillars. When the width of the V-shaped guide groove is 2.5 mm, the godet roller is not uniformly heat- there is a problem.
접촉넓이를 조절하는 또 다른 인자는 롤러의 연신장력, 연신온도 및 유제량 등이 있다.Another factor controlling the contact width is the stretching tension of the roller, the stretching temperature, and the amount of emulsion.
본 발명은 상기 여러 가지 인자를 유기적으로 결합시킴으로써 1차 연신에 많은 영향을 주는 GR 2의 표면에 멀티필라멘트 사가 접촉하는 넓이는 2,000 ~ 4,000mm 2로, 2차 연신이 일어나는 고뎃 롤러인 GR 3의 표면에 멀티필라멘트 사가 접촉하는 넓이는 7,000 ~ 9,000mm 2로 조절함으로써 바람직한 본 발명의 멀티필라멘트를 얻을 수 있다.In the present invention, the width of contact of the multifilament yarn to the surface of GR 2, which has a large influence on the primary drawing by organically binding the various factors, is 2,000 to 4,000 mm 2 , and GR 3 The width of the surface of the multifilament yarn contacting the surface is adjusted to 7,000 to 9,000 mm 2 , thereby obtaining the desired multifilament of the present invention.
이와 같은 공정을 거쳐서 제조된 폴리에틸렌테레프탈레이트는 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상이다. 상기 폴리에틸렌테레프탈레이트 원사는 85℃ 고온 인장시험에서 측정한 터프니스가 32×10 -1g/d 이상인 것을 특징으로 한다. The polyethylene terephthalate produced through such a process had a yarn strength of 6.5 gf / And the elongation at break is 19% or more. The polyethylene terephthalate raw material has a toughness of 32 x 10 < -1 > g / d or more as measured in a high temperature tensile test at 85 deg.
본 발명의 에어백용 폴리에틸렌테레프탈레이트 멀티 필라멘트의 총 섬도는 100~1000데니어인 것이 적합하고, 더욱 바람직하게는 200~700데니어이다. 총 섬도가 100데니어 미만의 원사를 사용할 경우 에어백용 직물은 수납성의 점에서는 만족하지만, 강력이 부족하여 전개 시 및 전개후의 승객 충돌 시에 백이 파열될 우려가 있어 바람직하지 않다. 반대로 총 섬도가 1000데니어를 초과하면, 에어백으로서 충분한 강력이 얻어져 안전성의 면에서는 만족할 수 있지만 직물이 두꺼워져서 수납성이 나빠지게 된다.The total fineness of the polyethylene terephthalate multifilament for an airbag of the present invention is preferably 100 to 1000 denier, more preferably 200 to 700 denier. When a yarn having a total fineness of less than 100 deniers is used, the fabric for airbags is satisfactory in terms of retractability but is not preferable because of the lack of strength and the bag may rupture at the time of deployment and collision after deployment. On the contrary, if the total fineness exceeds 1000 denier, sufficient strength is obtained as an airbag, which can be satisfied from the viewpoint of safety, but the fabric becomes thick and the retention becomes poor.
에어백용 직물을 구성하는 멀티 필라멘트의 단사 섬도에 관해서는 5데니어 이하인 것이 바람직하고, 보다 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 초과하면, 직물의 접힘성 및 수납성의 저하, 또한 저통기성의 악화를 수반하여 에어백 직물로서 충분한 기능을 발휘하지 못하므로 바람직하지 않다.The monofilament fineness of the multifilament constituting the fabric for an airbag is preferably 5 denier or less, and more preferably 4.5 denier or less. Generally, as the fiber having a small single filament fineness is used, the resultant fabric is flexible and excellent in folding property and storage stability. Further, the single yarn fineness is reduced and the covering property is improved, and as a result, the air permeability of the fabric can be suppressed. If the single yarn fineness exceeds 5 denier, it is not preferable because the folding property and the storage ability of the fabric are deteriorated, and the low air permeability is deteriorated and the sufficient function as the airbag fabric can not be exhibited.
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. However, the scope of the present invention is not limited or limited by the following examples.
실시예 1, 2, 3Examples 1, 2, and 3
고유점도 1.00dl/g의 폴리에스테르 칩을 직경이 0.4mm, 길이와 직경의 비(L/D)가 3이고 구멍수 120개인 노즐을 통해 용융 폴리머를 압출하고 15℃의 공기로 냉각시킨 다음 집속시켜 오일링하고, 고뎃 롤러 2의 온도 100℃, 고뎃 롤러 3 온도 125℃이고, 방사온도, 연신비, 이완률 및 고뎃 롤러 4 온도는 표 1에 명기한 조건으로 하였고, 고뎃 롤러 2(1차 연신점)에서 필라멘트의 권취 횟수는 5회, 고뎃 롤러 3(2차 연신점)에서 필라멘트의 권취 횟수는 7회이고, 고뎃 롤러 2와 3의 전에 가이드의 형태가 프랫한 형태로 가이드 홈의 폭이 4mm 이고 고뎃 롤러 GR 4의 속도를 2700m/min으로 하여 500데니어/120f를 방사하고 연신하였다.A polyester chip having an intrinsic viscosity of 1.00 dl / g was extruded through a nozzle having a diameter of 0.4 mm, a ratio of length to diameter (L / D) of 3 and a number of holes of 120, cooled with air at 15 ° C, And the temperature of the godet roller 2 was 100 캜 and the godet roller 3 temperature was 125 캜. The spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were the conditions specified in Table 1, and the godet roller 2 The number of windings of the filaments in the godet roller 3 (second elongation point) is 7, the shape of the guide before the godet rollers 2 and 3 is prat, and the width of the guide groove is 4 mm, and the speed of the godet roller GR 4 was set at 2700 m / min, and 500 denier / 120f was radiated and stretched.
비교예 1Comparative Example 1
상기 실시예 1, 2, 3과 주요한 조건은 같으며 방사온도, 연신비, 이완률 및 고뎃 롤러 4 온도는 표 1에 명기한 조건으로 하였고, 고뎃 롤러 2, 3 전의 가이드 형태가 넓은 프랫 형태이며 가이드 홈의 폭은 6.5mm 이고 고뎃 롤러 2에서 필라멘트의 권취 횟수는 5회이며 고뎃 롤러 3에서는 7회이다.The main conditions are the same as those of Examples 1, 2 and 3, and the spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were set as shown in Table 1. The guides of the godet rollers 2 and 3 were wide, The width of the groove is 6.5 mm, the number of filaments wound on the godet roller 2 is 5, and that on the godet roller 3 is 7.
비교예 2Comparative Example 2
비교예 1과 주요한 조건은 같으며 방사온도, 연신비, 이완률 및 고뎃 롤러 4 온도는 표 1에 명기한 조건으로 하였고, 고뎃 롤러 2, 3 전의 가이드 형태가 좁은 브이홈(가이드 홈의 폭은 2.5mm)이며 필라멘트의 고뎃 롤러 2에서 권취 횟수는 6회이며 고뎃 롤러 3에서는 8회이다.The main conditions were the same as in Comparative Example 1, and the spinning temperature, the stretching ratio, the relaxation rate and the godet roller 4 temperature were set as shown in Table 1. The width of the guide grooves was 2.5 mm), the number of times of winding is 6 in the godet roller 2 of the filament, and 8 in the godet roller 3.
측정방법How to measure
상기 실시예 1 내지 3, 비교예 1 내지 2를 통해 제조된 원사 및 에어백용 직물의 물성은 아래의 시험 방법을 통해 측정하였다.The physical properties of the yarn and airbag fabric prepared through Examples 1 to 3 and Comparative Examples 1 and 2 were measured by the following test methods.
1) 폴리에스테르 칩의 고유점도(I.V.) 측정1) Intrinsic viscosity (I.V.) measurement of polyester chips
페놀과 1,1,2,3-테트라클로로에탄올을 6:4의 무게비로 혼합한 시약(90℃)에 시료 0.1g을 농도가 0.4g/100mL 되도록 90분간 용해시킨 후 우베로데(Ubbelohde)점도계에 옮겨 담아 30℃ 항온조에서 10분간 유지시키고, 점도계와 흡인장치(aspirator)를 이용하여 용액의 낙하 초수를 구했다. 용매의 낙하 초수도 동일한 방법으로 구한 다음, 하기 수학식에 의해 R.V.값 및 I.V.값을 계산하였다.Phenol and 1,1,2,3-tetrachloroethanol in a weight ratio of 6: 4 was dissolved in a reagent (90 DEG C) for 90 minutes so as to have a concentration of 0.4 g / 100 mL, and the solution was dissolved in Ubbelohde The solution was transferred to a viscometer and maintained at 30 ° C in a thermostatic chamber for 10 minutes. The drop number of the solution was obtained by using a viscometer and an aspirator. The number of drops of the solvent was also determined by the same method, and then the RV value and the IV value were calculated by the following equation.
R.V. = 시료의 낙하 초수/용매의 낙하 초수R.V. = Samples falling in water / solvent drops in seconds
I.V. = 1/4 × [(R.V.- 1)/C] + 3/4 × (ln R.V./C)I.V. = 1/4 x [(R.V.- 1) / C] + 3/4 (ln R.V./C)
상기 식에서, C는 용액 중의 시료의 농도(g/100mL)를 나타낸다.In the above equation, C represents the concentration (g / 100 mL) of the sample in the solution.
2) 원사의 강신도 측정2) Measuring the strength of yarn
원사를 표준상태인 조건, 즉 25℃ 온도와 상대습도 65% RH 인 상태인 항온 항습실에서 24시간 방치 후 ASTM 2256 방법으로 시료를 인장 시험기를 통해 측정한다.The yarn is allowed to stand in a standard temperature condition, that is, in a constant temperature and humidity room at a temperature of 25 ° C and a relative humidity of 65% RH for 24 hours, and then the sample is measured by a tensile tester using the ASTM 2256 method.
3) 원사의 고온 인장 강신도 측정 3) High tensile strength of yarn
원사의 최대 강도(gf/den.)과 최대 신도(%)를 측정함에 있어서 시료장은 250mm이고, 인장속도는 300mm/min이며, 초기 하중은 0.05gf/den.로 설정하여 ASTM 2256 방법으로 원사의 인장시험을 진행하되, 측정 온도는 상온이 아닌 고온 조건에서 시험하기 위하여 3119-600 Series environmental chamber가 장착된 만능재료 시험기(Instron사, 모델 5565) 장비를 사용하여서 environmental chamber 온도가 85℃인 상태에서 시료를 장착하고, 챔버 온도가 85℃에 도달한 시점에 강신도 시험을 진행하였다. 시료당 5회씩 인장시험을 하여 평균값을 사용하였다.In measuring the maximum strength (gf / d.) And maximum elongation (%) of the yarn, the sample length is 250 mm, the tensile speed is 300 mm / min, the initial load is 0.05 gf / The test was carried out using a universal material testing machine (Instron, model 5565) equipped with an environmental chamber of 3119-600 Series for testing at a high temperature, not at room temperature. The sample was mounted, and the strength test was carried out when the chamber temperature reached 85 캜. Tensile tests were carried out five times per sample and average values were used.
이때 표준조건(25℃, 65%RH)에서 측정한 섬도(데니어) 값으로 고온 인장시험 했을 때 원사의 강력(kgf)값을 나누어서 고인 인장시험 후 강도(gf/den.)값은 계산 하였다.The strength (gf / den.) After the tensile test was calculated by dividing the strength (kgf) of the yarn when subjected to high temperature tensile test at a fineness (denier) value measured under standard conditions (25 ° C., 65% RH).
4) 원사의 건열 수축률 측정4) Dry heat shrinkage measurement of yarn
원사를 테스트라이트 수축률 시험기(Testrite shrinkage tester)에서 180℃에서 2분 동안 0.05gf/데니어 하중을 가한 조건으로 수축률을 측정한다.The shrinkage of the yarn is measured in a test light shrinkage tester at 180 ° C for 2 minutes under a condition of 0.05 gf / denier load.
5) 직물의 80℃ 고온 에이징후 인열강력 측정5) Tensile strength measurement after 80 ℃ high temperature aging of fabric
이렇게 생산된 원사로 워터제트룸 직기에서 인치 당 경사 밀도 50개, 위사 밀도 49로 평직으로 제직한 뒤, 표면 온도가 180℃인 Can dryer를 거쳐서 건조한다. 이렇게 제조된 에어백용 직물을 아래와 같은 방법으로 고온 인열강력을 측정하였다. 에어백용 직물을 80℃에서 48시간 에이징 한 뒤 25℃, 65%RH 조건에서 24시간 방치 후 직물의 인열강력을 만능재료 시험기(Instron사, 모델 4465)를 이용하여, ASDM D 2261법에 의한 텅법의 측정방법에 따라 시험 속도 50mm/min로 일정하게 당기면서 시험편을 인열 시킬 때 발행되는 피크 중 최대 피크 5개의 평균값으로 인열강력을 계산하였다.The yarn thus produced is woven in a water jet loom in plain weave with an oblique density of 50 and an oblique density of 49, and then dried through a can dryer having a surface temperature of 180 ° C. The air bag fabric thus manufactured was subjected to hot tear strength test in the following manner. The fabric for airbags was aged at 80 DEG C for 48 hours and left for 24 hours under the conditions of 25 DEG C and 65% RH. The tear strength of the fabrics was measured using a universal material testing machine (Instron, Model 4465) , The tear strength was calculated as an average value of the maximum peaks of peaks issued when the test pieces were torn while constantly pulling at a test speed of 50 mm / min.
실시예 1Example 1 실시예2Example 2 실시예3Example 3 비교예 1Comparative Example 1 비교예2Comparative Example 2
방사 온도Radiation temperature 295℃295 DEG C 295℃295 DEG C 290℃290 ° C 305℃305 ℃ 305℃305 ℃
연신비Stretching cost 5.85.8 5.95.9 6.06.0 5.45.4 5.45.4
이완률(Relax ratio)Relax ratio 9.0%9.0% 9.0%9.0% 8.5%8.5% 10.0%10.0% 11.0%11.0%
열처리 온도(4번 고뎃롤러 온도)Heat treatment temperature (godet roller temperature 4) 245℃245 ° C 240℃240 ℃ 235℃235 ° C 245℃245 ° C 250℃250 ℃
고뎃 롤러 2(1차 연신점)에서 필라멘트의 권취회수The winding number of the filament at the godet roller 2 (first elongation point) 5회5 times 5회5 times 5회5 times 5회5 times 6회6 times
고뎃 롤러 3(2차 연신점)에서 필라멘트의 권취회수The number of take-up times of the filament at the godet roller 3 (second elongation point) 7회7 times 7회7 times 7회7 times 7회7 times 8회8 times
고뎃 롤러 2와 3의 전에 가이드의 형태와 가이드 홈의 폭The shape of the guide before the godet rollers 2 and 3 and the width of the guide groove 프랫 형태,폭 4mmPratt shape, width 4mm 프랫 형태,폭 4mmPratt shape, width 4mm 프랫 형태,폭 4mmPratt shape, width 4mm 프랫 형태,폭 6.5mmPratt shape, width 6.5mm 브이홈 형태, 폭 2.5mmV groove shape, width 2.5mm
85℃ 측정 원사 강도(gf/den.)85 ℃ Measured yarn strength (gf / den.) 7.27.2 7.37.3 7.57.5 6.46.4 6.26.2
85℃ 측정 원사 절단신율(%)85 ℃ Measuring elongation of yarn (%) 21.121.1 22.222.2 22.322.3 24.024.0 23.023.0
85℃ 측정 원사의 터프니스(×10 -1g/d)Toughness of yarn measured at 85 ° C (× 10 -1 g / d) 33.133.1 34.434.4 35.435.4 31.431.4 29.229.2
80℃에서 48시간 에이징 한 직물의 경사방향 인열강력(kgf)Tear strength (kgf) of the fabric aged at 80 ° C for 48 hours. 19.719.7 20.120.1 20.420.4 18.518.5 18.118.1
실시예 1~3과 같이 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 원사로 제조된 직물은 80℃에서 에이징 후에도 직물의 인열강력이 더 높게 발현되어 고온 환경에 에어백이 노출되었을 때 에어백 전개과정에서 직물이 찢어짐으로 인한 bag의 파손을 줄일 수 있는 장점이 있다.As in Examples 1 to 3, in the high temperature tensile test at 85 캜, the strength of the yarn was 6.5 gf / Or more and a breaking elongation of 19% or more, the tear strength of the fabric is higher than that of the fabric after aging at 80 ° C, so that when the airbag is exposed to a high temperature environment, the bag is prevented from being broken due to tearing There are advantages to be able to.
본 출원에서 특별히 다르게 정의되지 않는 한, 기술적이거나 과학적인 용어를 포함해서 여기서 사용되는 모든 용어들은 본 발명이 속하는 기술 분야에서 통상의 지식을 가진 자에 의해 일반적으로 이해되는 것과 동일한 의미를 가지고 있다.Unless specifically defined otherwise herein, all terms used herein, including technical or scientific terms, have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.
일반적으로 사용되는 사전에 정의되어 있는 것과 같은 용어들은 관련 기술의 문맥상 가지는 의미와 일치하는 의미를 가지는 것으로 해석되어야 하며, 본 출원에서 명백하게 정의하지 않는 한, 이상적이거나 과도하게 형식적인 의미로 해석되지 않는다.Terms such as those defined in commonly used dictionaries are to be interpreted as having a meaning consistent with the contextual meaning of the related art and are to be interpreted as either ideal or overly formal in the sense of the present application Do not.
[부호의 설명][Description of Symbols]
1: 익스트루더1: Extruder
2: 기어펌프2: Gear pump
3: 방사구금3: spinning detention
4: 후드 히터4: Hood heater
5: 공기 공급관 입구5: Air inlet inlet
6: 공기 배기관 출구6: Exhaust air outlet
7: 방사유제 공급장치7: Radial emulsion feeder
8: 연신 고뎃 롤러 GR18: Drawing godet roller GR1
9: 연신 고뎃 롤러 GR29: Drawing godet roller GR2
10: 연신 고뎃 롤러 GR310: Drawing godet roller GR3
11: 연신 고뎃 롤러 GR411: Drawing godet roller GR4
12: 연신 고뎃 롤러 GR512: Drawing godet roller GR5
13: 권취롤러(와인더)13: Winding roller (winder)

Claims (5)

  1. 고유점도가 0.8~1.3dl/g인 폴리에틸렌테레프탈레이트 칩을 방사하여 얻은 폴리에틸렌테레프탈레이트 멀티필라멘트에 있어서, 85℃ 고온 인장시험에서 원사의 강도가 6.5gf/den. 이상이고 절단 신율은 19% 이상인 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.In a polyethyleneterephthalate multifilament obtained by spinning a polyethylene terephthalate chip having an intrinsic viscosity of 0.8 to 1.3 dl / g, the yarn has a strength of 6.5 gf / den in 85 < 0 > C high temperature tensile test. By weight and a elongation at break of 19% or more for polyethylene terephthalate multifilament for airbags.
  2. 제 1 항에 있어서,The method according to claim 1,
    상기 85℃ 고온 인장시험에서 측정한 폴리에틸렌테레프탈레이트 원사의 터프니스가 32×10 -1g/d이상인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.Wherein the polyethylene terephthalate yarn has a toughness of 32 x 10 < -1 > g / d or more as measured in the 85 DEG C high temperature tensile test.
  3. 제 1 항에 있어서,The method according to claim 1,
    상기 폴리에틸렌테레프탈레이트 멀티필라멘트의 총섬도가 100 내지 1000 데니어이고, 멀티필라멘트의 섬도가 2 내지 10 인 것을 특징으로 하는 에어백용 폴리에틸렌테레프탈레이트 멀티필라멘트.Wherein the polyethylene terephthalate multifilament has a total fineness of 100 to 1000 denier and a multifilament has a fineness of 2 to 10. 2. The polyethylene terephthalate multifilament for airbags according to claim 1,
  4. 제 1항의 폴리에틸렌테레프탈레이트 멀티필라멘트를 사용하여 제직된 에어백용 직물.A fabric for an air bag woven using the polyethylene terephthalate multifilament of claim 1.
  5. 제 4 항에 있어서,5. The method of claim 4,
    상기 에어백용 직물은 80℃에서 48시간 에이징 한 에어백직물의 경사방향 인열강력이 19kgf이상인 것을 특징으로하는 에어백용 직물.Wherein the airbag fabric has an airbag fabric aged for 48 hours at < RTI ID = 0.0 > 80 C < / RTI >
PCT/KR2019/000457 2018-01-11 2019-01-11 Polyethylene terephthalate yarn for airbag WO2019139406A1 (en)

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