KR20170085877A - High-strength Nylon 66 filament having excellent strength ratio - Google Patents

High-strength Nylon 66 filament having excellent strength ratio Download PDF

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KR20170085877A
KR20170085877A KR1020160005561A KR20160005561A KR20170085877A KR 20170085877 A KR20170085877 A KR 20170085877A KR 1020160005561 A KR1020160005561 A KR 1020160005561A KR 20160005561 A KR20160005561 A KR 20160005561A KR 20170085877 A KR20170085877 A KR 20170085877A
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nylon
strength
yarn
present
ratio
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KR102301292B1 (en
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최재신
박진경
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주식회사 효성
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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
    • D01F6/60Monocomponent artificial filaments or the like of synthetic polymers; Manufacture thereof from homopolycondensation products from polyamides
    • 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
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G69/00Macromolecular compounds obtained by reactions forming a carboxylic amide link in the main chain of the macromolecule
    • C08G69/02Polyamides derived from amino-carboxylic acids or from polyamines and polycarboxylic acids
    • C08G69/08Polyamides derived from amino-carboxylic acids or from polyamines and polycarboxylic acids derived from amino-carboxylic acids
    • C08G69/14Lactams
    • 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
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/02Yarns or threads characterised by the material or by the materials from which they are made
    • D02G3/04Blended or other yarns or threads containing components made from different materials
    • D02G3/047Blended or other yarns or threads containing components made from different materials including aramid fibres
    • 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
    • D02G3/46Sewing-cottons or the like
    • 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
    • D02G3/48Tyre cords
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • D03D1/02Inflatable articles
    • DTEXTILES; PAPER
    • D07ROPES; CABLES OTHER THAN ELECTRIC
    • D07BROPES OR CABLES IN GENERAL
    • D07B5/00Making ropes or cables from special materials or of particular form
    • D07B5/06Making ropes or cables from special materials or of particular form from natural or artificial staple fibres
    • DTEXTILES; PAPER
    • D07ROPES; CABLES OTHER THAN ELECTRIC
    • D07BROPES OR CABLES IN GENERAL
    • D07B1/00Constructional features of ropes or cables
    • D07B1/02Ropes built-up from fibrous or filamentary material, e.g. of vegetable origin, of animal origin, regenerated cellulose, plastics
    • D07B1/025Ropes built-up from fibrous or filamentary material, e.g. of vegetable origin, of animal origin, regenerated cellulose, plastics comprising high modulus, or high tenacity, polymer filaments or fibres, e.g. liquid-crystal polymers
    • DTEXTILES; PAPER
    • D07ROPES; CABLES OTHER THAN ELECTRIC
    • D07BROPES OR CABLES IN GENERAL
    • D07B2205/00Rope or cable materials
    • D07B2205/20Organic high polymers
    • D07B2205/2046Polyamides, e.g. nylons
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2401/00Physical properties
    • D10B2401/06Load-responsive characteristics
    • D10B2401/063Load-responsive characteristics high strength
    • 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

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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)
  • Health & Medical Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Artificial Filaments (AREA)

Abstract

본 발명은 나일론 66의 초고강도(Super-High Tenacity, SHT) 섬유의 특성과 관련된 것으로 파단 부위 탄성율이 40d/g 이하로 제조하여 높은 강력 이용률을 발현할 수 있는 나일론 66 고강도 섬유에 관한 것이다. 본 발명에 의하여 제조된 강력 이용률이 높은 나일론 66 고강도 섬유는 원사 제조 공정 조건을 조절함으로서 파단 부위의 탄성율이 낮고, 원사 강도는 높으며, 절단 신도가 높은 섬유를 제조할 수 있어 자동차용 에어백용 직물이나 재봉사, 로프, 호스 보강재 등 산업용 섬유로서 광범위하게 사용될 수 있다.The present invention relates to a nylon 66 high-strength fiber, which is related to the properties of super-high tenacity (SHT) fibers of nylon 66 and which can exhibit a high tensile strength by producing a tensile elastic modulus of 40 d / g or less. The nylon 66 high strength fiber having high strength utilization produced by the present invention can produce fibers having low elastic modulus at the fracture site, high yarn strength and high cutting elongation by controlling yarn manufacturing process conditions, Sewing thread, rope, hose reinforcement, and the like.

Description

강력 이용률이 높은 나일론 66 고강도 섬유{High-strength Nylon 66 filament having excellent strength ratio}High-strength nylon 66 filament having excellent strength ratio [

본 발명은 나일론 66의 초고강도(Super-High Tenacity, SHT) 섬유의 특성과 관련된 것으로 파단 부위 탄성율이 40d/g 이하로 제조하여 높은 강력 이용률을 발현할 수 있는 나일론 66 고강도 섬유에 관한 것이다.The present invention relates to a nylon 66 high-strength fiber, which is related to the properties of super-high tenacity (SHT) fibers of nylon 66 and which can exhibit a high tensile strength by producing a tensile elastic modulus of 40 d / g or less.

나일론 66은 헥사메틸렌 디아민과 아디프산을 축중합시킴으로서 제조되는 폴리아미드로, 의료용 및 산업용 섬유, 플라스틱 성형품 등에 널리 이용되고 있으며, 우수한 특성을 바탕으로 자동차 에어백용 직물, 재봉사, 산업용 로프 등 산업자재 용도로 그 수요가 광범위하게 요구되고 있는 소재이다. 순수 나일론 66 칩을 사용하여 원사를 제조하는 경우에는 헥사메틸렌 디아민과 아디프산 사이의 반응 및 여러 부반응에 의해 프리폴리머 내부에 겔상 물질(gel-like material)이 생성되어, 이후의 후속 공정에서 여러 가지 문제를 일으키게 된다. 이렇게 중합물 내부에 존재하는 겔이 고상 중합단계에서 환상 또는 3차원화 방식으로 계속 성장하게 되고 용융 및 방사단계에서 더욱 성장, 발전하는 동시에 새로운 겔이 생성되어 용융상 필라멘트 내부에 구정(spherulite)를 발생기킨다. 이러한 겔 발생이 많으면 방사 팩 및 노즐 필터에 포집되어 필터 교체 주기 단축 등의 방사 작업성을 저하시키고 일부 크기가 작은 겔은 미연신사에 포함되어 연신공정에서 연신성을 저하시켜 핀사 발생이 많아지게 되어 이후 자동차 에어백용 직물등의 제직 공정에서 작업성을 저하시키는 요인으로 작용하여 문제가 되기도 한다. Nylon 66 is a polyamide produced by polycondensation of hexamethylenediamine and adipic acid. It is widely used in medical and industrial textile, plastic molding, etc., and has excellent properties such as automobile airbag fabric, sewing thread, It is a material for which demand is widely demanded. In the case of producing a yarn using pure nylon 66 chips, a gel-like material is generated inside the prepolymer due to the reaction between hexamethylenediamine and adipic acid and various side reactions, and various subsequent processes Causing problems. In this way, the gel present in the polymerized phase continues to grow in a cyclic or three-dimensional manner in the solid-phase polymerization step, and further grows and develops in the melting and spinning stages, and at the same time, a new gel is formed and spherulite is generated in the melt- It is. If such a gel is generated, it is caught in a spinning pack and a nozzle filter, and the spinning workability such as shortening of the filter replacement cycle is lowered. A gel having a small size is included in the undrawn yarn to reduce the drawability in the drawing process, There is a problem that it acts as a factor to lower the workability in the weaving process of the automobile airbag fabric and the like.

한국공개특허 제 2010-0021790호Korea Patent Publication No. 2010-0021790

본 발명은 강력 이용률이 높은 나일론 66 고강도 섬유를 제조함에 있어서, 파단 부위의 기울기 즉 파단부위의 탄성율을 40g/d 이하로 한정한 원사를 개발하는 데 목적이 있다.An object of the present invention is to develop a yarn in which the slope of the fracture site, that is, the modulus of elasticity of the fracture site is limited to 40 g / d or less in the production of nylon 66 high strength fiber having high strength utilization.

본 발명에 바람직한 실시 형태에 따르면 산업용 고강도 나일론 66 섬유에 있어서, 파단 부위의 탄성율이 40g/d 이하이고, 이완율은 4 내지 5%이고, 이완영역의 온도는 240 내지 280℃인 것을 특징으로 하는 강력 이용률이 높은 나일론 66 고강도 섬유를 제공한다. 이때 원사 강도는 11g/d 이상이고 절단신도가 15 내지 28%, D/C의 강력 이용율은 85% 이상인 것을 특징으로 한다.According to a preferred embodiment of the present invention, in the high-strength industrial nylon 66 fiber for industrial use, the elastic modulus at the fracture site is 40 g / d or less, the relaxation rate is 4 to 5%, and the relaxation zone temperature is 240 to 280 ° C Provides high strength nylon 66 high strength fibers. At this time, the yarn strength is 11 g / d or more, the cut elongation is 15 to 28%, and the strength utilization ratio of D / C is 85% or more.

본 발명에 의하여 제조된 강력 이용률이 높은 나일론 66 고강도 섬유는 원사 제조 공정 조건을 조절함으로서 파단 부위의 탄성율이 낮고, 원사 강도는 높으며, 절단 신도가 높은 섬유를 제조할 수 있어 자동차용 에어백용 직물이나 재봉사, 로프, 호스 보강재 등 산업용 섬유로서 광범위하게 사용될 수 있다.The nylon 66 high strength fiber having high strength utilization produced by the present invention can produce fibers having low elastic modulus at the fracture site, high yarn strength and high cutting elongation by controlling yarn manufacturing process conditions, Sewing thread, rope, hose reinforcement, and the like.

본 발명에 의해 제조된 나일론 66 원사는 최종 원사의 강도가 11g/d 이상, 절단신도가 15%이상을 가지면서 D/C의 강력 이용률은 85%이상을 가지는 특성을 가지며, 파단 부위의 탄성율은 40g/d 이하이다.The nylon 66 yarn produced by the present invention has the characteristics that the strength of the final yarn is 11 g / d or more, the elongation at break is 15% or more and the strength utilization ratio of D / C is 85% or more. 40 g / d or less.

본 발명에 사용되는 나일론 66의 2.8~3.6 수준이며, 중합물의 상대점도가 높을수록 고강도 발현에 유리하다.The nylon 66 used in the present invention has a level of 2.8 to 3.6, and as the relative viscosity of the polymer is higher, it is advantageous in high-intensity expression.

아래에서 본 발명에 따른 나일론 66 고강도 섬유의 제조방법을 설명한다.A method for producing nylon 66 high strength fiber according to the present invention will be described below.

본 발명의 나일론 66 고강도 섬유는 압출기에서 용융시킨 용융물을 방사구금을 통과시켜 방사한 후 다단 롤러를 통과시키면서 연신-열고정-이완을 동시에 행하는 스핀-드로우 공법으로 제조할 수 있다.The nylon 66 high-strength fiber of the present invention can be manufactured by a spin-draw process in which a melt melted in an extruder is radiated through a spinneret and is then passed through a multi-stage roller while simultaneously performing stretching-heat fixing-relaxation.

구체적으로 본 발명은 (A) 헥사메틸렌아디프아미드 반복 단위를 85몰% 이상 함유하는 폴리헥사메틸렌아디프아미드를 방사구금을 통하여 용융 압출하는 단계, (B) 방사구금 아래에서 냉각기체를 사용하여 냉각 고화시키고 미연신사를 인취하는 단계, (C) 상기 미연사를 다단 연신, 열처리 및 이완을 거쳐 연신사를 권취하는 단계에 의해 제조되는 나일론 66 고강도 섬유를 제공하는 것이다. Specifically, the present invention relates to a process for producing a poly (hexamethylene adipamide) comprising (A) melt extruding polyhexamethylene adipamide containing 85 mol% or more of hexamethylene adipamide repeating unit through spinneret, (B) (C) winding the softening yarn through the multi-stage stretching, heat treatment and relaxation of the non-twisted yarn to obtain a nylon 66 high-strength fiber.

본 발명에 사용되는 폴리헥사메틸렌아디프아미드 중합물은 최소한 85몰%의 헥사메틸렌아디프아미드 반복 단위를 함유하며, 바람직하게는 헥사메틸렌아디프아미드 단위만으로 구성된다. The polyhexamethylene adipamide polymer used in the present invention contains at least 85 mol% of repeating units of hexamethylene adipamide and preferably consists only of hexamethylene adipamide units.

선택적으로, 상기 폴리헥사메틸렌아디프아미드 대신에 임의의 폴리아미드 단독중합체 및 공중합체가 사용될 수 있다. 이러한 폴리아미드는 주로 지방족이다. 폴리(헥사메틸렌 아디프아미드) (나일론 66); 폴리(e-카프로아미드) (나일론 6); 및 그들의 공중합체 등의 널리 사용되는 나일론 중합체가 사용될 수 있다. 나일론 66이 가장 바람직하다. 유리하게 사용될 수 있는 기타 나일론 중합체는 나일론 12, 나일론 46, 나일론 6·10 및 나일론 6·12이다.Alternatively, any polyamide homopolymer and copolymer may be used in place of the polyhexamethylene adipamide. Such polyamides are predominantly aliphatic. Poly (hexamethylene adipamide) (nylon 66); Poly (e-caproamide) (nylon 6); And widely used nylon polymers such as copolymers thereof can be used. Nylon 66 is the most preferred. Other nylon polymers that may be advantageously used are nylon 12, nylon 46, nylon 6. 10, and nylon 6. 12.

폴리헥사메틸렌아디프아미드 칩은, 열안정성 향상을 위하여 최종 중합체 중의 구리 금속으로서의 잔존량이 50 내지 80 ppm이 되도록 하는 양으로 첨가할 수 있는데, 이 양이 50 ppm보다 적으면 방사시 열안정성이 떨어져서 열분해가 일어나고, 80 ppm보다 많으면 필요 이상의 구리 금속이 이물질로 작용하여 방사시 문제가 된다.The polyhexamethylene adipamide chip may be added in an amount such that the residual amount of the copper metal in the final polymer is 50 to 80 ppm in order to improve the thermal stability. If the amount is less than 50 ppm, the thermal stability upon spinning falls If it exceeds 80 ppm, more copper than necessary will act as a foreign substance, which is a problem in spinning.

상기 폴리헥사메틸렌아디프아미드 칩을 본 발명의 방법에 따라 섬유화한다.The polyhexamethylene adipamide chips are fiberized according to the method of the present invention.

단계 (A)에서, 폴리헥사메틸렌아디프아미드 칩을 팩 및 노즐을 통해 바람직하게는 270 내지 310℃의 방사온도에서, 바람직하게는 20 내지 200의 방사 드래프트비(최초 권취롤러 위에서의 선속도/노즐에서의 선속도)로 저온 용융방사함으로써 열분해에 의한 중합체의 점도의 저하를 방지할 수 있다. 방사 드래프트비가 20보다 작으면 필라멘트 단면 균일성이 나빠져 연신작업성이 현저히 떨어지고, 200을 초과하면 방사 중 필라멘트 파손이 발생하여 정상적인 원사를 생산하기 어렵게 된다. In step (A), the polyhexamethylene adipamide chips are passed through the pack and nozzle, preferably at a spinning temperature of from 270 to 310 DEG C, preferably from 20 to 200, of a radiation draft ratio (linear velocity / The linear velocity at the nozzle), it is possible to prevent the viscosity of the polymer from lowering due to thermal decomposition. If the radiation draft ratio is less than 20, the uniformity of the filament cross section is deteriorated to deteriorate the drawing workability remarkably. If it exceeds 200, filament breakage occurs during spinning, and normal yarn production becomes difficult.

또한 본 발명에서는 팩내의 여과 체류시간을 3 내지 30초로 조정하는 것이 중요한 인자이다. 만일 팩내의 여과 체류시간이 3초 미만이면 이물질의 여과 효과가 불충분하며, 30초이상이면 과도한 팩압 증가로 인하여 열분해가 심하다. Further, in the present invention, adjusting the filtration retention time in the pack to 3 to 30 seconds is an important factor. If the filtration retention time in the pack is less than 3 seconds, the filtering effect of the foreign substance is insufficient, and if it is more than 30 seconds, the pyrolysis is severe due to excessive packing pressure increase.

또한 본 발명에서는 압출기 스크루의 L/D(길이/직경)을 10 내지 40으로 하는 것이 바람직한데 이는 스쿠루의 L/D가 10미만이면 균일한 용융이 어렵고, 40을 초과하면 과도한 전단응력에 의한 분자량 저하가 심하여 물성이 떨어진다.Further, in the present invention, it is preferable to set the L / D (length / diameter) of the extruder screw to 10 to 40. If the L / D of the screw is less than 10, uniform melting is difficult. If it exceeds 40, The lowering of the molecular weight is severe and the physical properties are deteriorated.

단계 (B)에서, 상기 단계 (A)의 용융방출사를 냉각구역을 통과시켜 급냉고화시킨다. In step (B), the molten discharge of step (A) is quenched and solidified by passing through a cooling zone.

냉각구역에서는 냉각공기를 불어주는 방법에 따라 오픈 냉각(open quenching)법, 원형 밀폐 냉각(circular closed quenching)법 및 방사형 아웃플로우 냉각(radial outflow quenching)법 등을 적용할 수 있으며, 오픈 냉각(open quenching)법이 바람직하다. 이어, 냉각구역(3)을 통과하면서 고화된 방출사(4)를 유제 부여장치(5)에 의해 0.5 내지 1.0%로 오일링할 수 있다.In the cooling zone, an open quenching method, a circular closed quenching method, and a radial outflow quenching method can be applied according to a method of blowing cooling air, quenching method is preferable. The solidified discharged yarn 4 can then be oiled to 0.5 to 1.0% by the emulsion applying device 5 while passing through the cooling zone 3.

단계(C)에서, 미연신사의 바람직한 방사속도는 200 내지 1,000m/분이다. In step (C), the preferred spinning speed of the unstretched yarn is 200 to 1,000 m / min.

단계 (D)에서, 첫 번째 연신 롤러(6)를 통과한 사를 스핀드로(spin draw) 공법으로 일련의 연신 롤러(7, 8, 9 및 10)를 통과시키면서 총연신비 4.0배 이상, 바람직하기로는 4.5 내지 6.5 으로 연신시킴으로써 최종 연신사를 얻는다.In the step (D), the yarn passed through the first stretching roller 6 is passed through a series of stretching rollers 7, 8, 9 and 10 by a spin draw method, Is drawn to 4.5 to 6.5 to obtain a final drawn yarn.

한편 스핀-드로우 공법에 의해 나일론 66 고강력사를 제조하는 경우에는, 황산 상대점도가 2.7 내지 3.4인 나일론 66 공중합 칩을 압출기에서 용융시키고, 기어 펌프를 통하여 방사구금까지 이송한 다음, 압출시켜 냉각 고화시킨 후, 유제 부여장치를 이용하여 유제를 부여하고 방사속도 400 내지 1,000m/분으로 방사한 후 여러 쌍의 고데트 롤러를 통과시키면서 연신-열고정-이완시킨다. 이때, 제1 고데트 롤러와 제2 고데트 롤러 사이의 프리드로우 연신비는 1.01 내지 1.08로 하고, 제2 고데트 롤러와 제3 고데트 롤러 사이의 1단 연신비는 2.5 내지 3.5, 제3 고데트 롤러와 제4 고데트 롤러 사이의 2단 연신비는 1.5 내지 2.5로 하여 전체 연신비가 4.0 내지 6.0의 수준으로 되게 연신한 후 0 내지 6%의 수준으로 이완 공정을 적용한 2,100 내지 4,000m/분의 속도로 권취한다. 제1 고데트 롤러의 온도는 상온이고, 제2 고데트 롤러의 온도는 상온 내지 90℃, 제3 고데트 롤러의 온도는 120 내지 200℃, 제4 고데트 롤러의 온도는 180 내지 230℃, 제5 고데트 롤러의 온도는 상온 내지 150℃로 하는 것이 바람직하다.On the other hand, in the case of producing nylon 66 high-strength yarn by the spin-draw method, nylon 66 copolymer chips having a relative sulfuric acid viscosity of 2.7 to 3.4 are melted in an extruder and transferred to a spinneret through a gear pump, Then, an emulsion is applied by using an emulsion applying device, and the emulsion is radiated at a spinning speed of 400 to 1,000 m / min, and then stretched, heat fixed and relaxed while passing through a plurality of pairs of high-defect rollers. At this time, the free draw ratio between the first and second high-deflection rollers and the second high-deflection roller is 1.01 to 1.08, the first-stage stretching ratio between the second and third high-deflection rollers is 2.5 to 3.5, The stretching ratio between the rollers and the fourth felt rollers is 1.5 to 2.5, the total stretching ratio is adjusted to a level of 4.0 to 6.0, and a stretching speed of 2,100 to 4,000 m / min . The temperature of the first high detent roller is at room temperature, the temperature of the second high detent roller is in a range of from room temperature to 90 DEG C, the temperature of the third high detent roller is in a range of 120 to 200 DEG C, the temperature of the fourth high detent roller is in a range of 180 to 230 DEG C, It is preferable that the temperature of the fifth high deterioration roller is from room temperature to 150 deg.

여기서 원사 제조 공정 중 이완율을 4 내지 12%로 하고, 이완온도를 150 내지 280℃로 설정하고 Spin Draft 및 연신비에 따라 파단 부위의 탄성율을 40g/d 이하로 제조되도록 하는데 본 발명의 특징이 있다. 강력 이용률은 특히 원사의 파단 부위의 기울기와 밀접한 관련이 있으므로 제조되는 나일론 66 고강도 섬유의 파단 부위 탄성율은 40d/g 이하가 되도록 제조하는 것이 바람직하다. Here, the relaxation rate is set to 4 to 12% in the yarn manufacturing process, the relaxation temperature is set to 150 to 280 ° C, and the elasticity of the broken portion is made to be 40 g / d or less according to the spin draft and the stretching ratio . Since the tenacity of the yarn is closely related to the slope of the yarn breakage region, it is preferable to fabricate the nylon 66 high strength fiber so that the modulus of elasticity at the breaking site is 40 d / g or less.

이와 같은 본 발명의 방법에 의하여 제조되는 나일론 66 고강력사는 항공기 타이어 또는 특수 산업용 자재로서 사용 가능하다.The nylon 66 high strength yarn manufactured by the method of the present invention can be used as an aircraft tire or a special industrial material.

하기의 실시예 및 비교예를 통하여 본 발명을 보다 더 상세하게 설명한다. 단 하기 실시예 및 비교예는 예시하기 위한 것일 뿐 본 발명을 한정하지 않으며 본 발명의 범위를 국한시키는 것으로 간주해서는 아니된다.The present invention will be described in more detail with reference to the following examples and comparative examples. EXAMPLES The following examples and comparative examples are for illustrative purposes only and are not to be construed as limiting the scope of the present invention.

하기의 실시예 및 비교예의 결과에서 분석 항목별 측정조건은 다음과 같다.The measurement conditions for the analysis items in the results of the following Examples and Comparative Examples are as follows.

(1) 상대점도(I.V.)(1) Relative viscosity (I.V.)

황산(90%)에 시료 0.1g을 농도가 0.4g/100ml 되도록 90분간 용해시킨 후 우베로데(Ubbelohde) 점도계에 옮겨담아 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.값을 계산하였다.0.1 g of the sample was dissolved in sulfuric acid (90%) for 90 minutes so as to have a concentration of 0.4 g / 100 ml, transferred to a Ubbelohde viscometer, maintained in a thermostatic chamber at 30 ° C for 10 minutes, and the resultant was subjected to a viscometer and an aspirator To obtain the falling seconds of the solution. The number of drops of the solvent was also determined by the same method, and then the RV value was calculated by the following equation.

R.V. = 시료의 낙하 초수/용매의 낙하 초수R.V. = Samples falling in water / solvent drops in seconds

(2) 강신도(2) The power of God

인스트론(Instron) 5565(인스트론사제, 미국)를 이용하여, ASTM D 885의 규정에 따라 표준 상태(20℃, 65% 상대습도)하에서 24시간 이상 방치한 후 250mm의 시료 길이, 300mm/분의 인장속도 및 80turns/m의 조건으로 강신도를 측정하였다.After standing for 24 hours or more in a standard state (20 ° C, 65% relative humidity) according to ASTM D 885 using an Instron 5565 (Instron, USA), a sample length of 250 mm, a length of 300 mm / And a tensile strength of 80 turns / m.

(3) 파단 부위 탄성율(3) Elasticity at break

파단 부위 탄성율은 (절신-2)~절신 구간에서의 segment 기울기로 측정을 실시하였다.The elastic modulus at the fracture site was measured by the slope of the segment at the (cutting-2) to the cutting segment.

(4) D/C 강력 이용율(4) D / C Strong Utilization Rate

D/C 강력 이용율(%) = D/C 강력/(원사 강력 × Ply 수) × 100D / C Strength Utilization (%) = D / C Strength / (Yarn Strength x Ply Number) x 100

실시예 1Example 1

구리 금속을 각각 80ppm 포함하는 상대점도(RV) 3.4인 폴리헥사메틸렌아디프아미드 칩을 압출기를 사용하여 296℃의 온도에서 20의 방사 드래프트비로 용융방사하였다. 이때 팩내 여과 체류시간은 17초이고, 사용된 압출기의 스쿠루는 L/D가 35로 조정하였고, 2개의 유니트를 갖는 스태틱 믹서를 팩의 중합체 도관 내에 설치하여 용융방사되는 중합체를 고르게 혼합시켰다. 이어, 방출사를 길이 600mm의 냉각구역을 통과시켜 고화시킨 다음 방사 유제로 오일링하였다. 이 미연신사를 470m/분의 방사속도로 권취하고, 2단 연신시켰다. 총 연신비 6.0으로 열고정(이완 온도)하고 8% 이완시킨 다음 권취하여 1890d 데니어의 최종 연신사를 제조하였다.A polyhexamethylene adipamide chip having a relative viscosity (RV) of 3.4, each containing 80 ppm of copper metal, was melt-spun using an extruder at a temperature of 296 占 폚 at a radiation draft ratio of 20. At this time, the retention time of the filtration in the pack was 17 seconds. In the used extruder, the screw was adjusted to L / D of 35 and a static mixer having two units was installed in the polymer conduit of the pack to mix the melt-spun polymer uniformly. Then, the discharged yarn was solidified by passing through a cooling zone having a length of 600 mm, followed by oiling with a spinning oil. This unstretched yarn was wound at a spinning speed of 470 m / min and stretched in two stages. The final stretching ratio of 1890d denier was prepared by heat setting (relaxation temperature) at a total stretching ratio of 6.0 and relaxation of 8% followed by winding.

비교예 1Comparative Example 1

Spin Draft를 변경한 것 이외에는 실시예 1과 동일하게 연신사를 제조하였다.A spinning lug was produced in the same manner as in Example 1, except that Spin Draft was changed.

비교예1Comparative Example 1 실시예1Example 1 상대점도(R.V.)Relative viscosity (R.V.) 3.03.0 3.03.0 섬도(denier)Denier 18901890 18901890 Spin DraftSpin Draft 3030 2020 연신비Stretching cost 6.156.15 6.06.0 강도(d/g)Strength (d / g) 9.69.6 1111 절단신도(%)Cutting Elongation (%) 13.513.5 18.218.2 D/C 강력 이용률(%)D / C Strong Utilization Rate (%) 8080 8989 파단부위 탄성율(g/d)Elastic modulus at break (g / d) 4141 3535

상기 실시예1은 비교예1에 비하여 강도 11g/d의 나일론 66 고강도 섬유를 얻었으며, 절단 신도 및 강력 이용률도 비교예1과 비교하여 우수한 수준인 것을 알 수 있다. 또한 파단부위 탄성율의 경우에도 실시예 1은 비교예 1에 비해 낮은 값을 보여 종합적으로 실시예 1은 비교예 1에 비하여 높은 강력 이용률을 발현하는 것으로 나타났다.In Example 1, nylon 66 high strength fiber having a strength of 11 g / d was obtained as compared with Comparative Example 1, and the breaking elongation and the strength utilization ratio were also superior to those of Comparative Example 1. Also, in the case of the elastic modulus at the fracture site, Example 1 was lower than Comparative Example 1, and overall Example 1 exhibited a higher strength utilization ratio than Comparative Example 1.

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. 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.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. 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.

Claims (2)

산업용 고강도 나일론 66 섬유에 있어서,
파단 부위의 탄성율이 40g/d 이하인 것을 특징으로 하는 강력 이용률이 높은 나일론 66 고강도 섬유.
For industrial high strength nylon 66 fibers,
And a modulus of elasticity at the fracture site is 40 g / d or less.
제 1항에 있어서,
상기 나일론 66 고강도 섬유의 원사 강도는 11g/d 이상이고 절단신도가 15 내지 28%, 딥코드(D/C)의 강력 이용율은 85% 이상인 것을 특징으로 하는 강력 이용률이 높은 나일론 66 고강도 섬유.
The method according to claim 1,
Wherein the nylon 66 high strength fiber has a yarn strength of 11 g / d or more, a cutting elongation of 15 to 28%, and a dope cord (D / C) of 85% or more.
KR1020160005561A 2016-01-15 2016-01-15 High-strength Nylon 66 filament having excellent strength ratio KR102301292B1 (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6350519A (en) * 1987-07-31 1988-03-03 Toray Ind Inc Polyhexamethylene adipamide fiber
JPH09268471A (en) * 1996-03-28 1997-10-14 Tong Yang Nylon Co Ltd Polyamide yarn for reinforcing material for rubber product and its production
KR100462924B1 (en) * 2003-10-22 2004-12-23 주식회사 효성 Low shrinkage polyamide fibers for uncoated airbag and process for preparing the same
KR20100021790A (en) 2008-08-18 2010-02-26 주식회사 효성 High-strenth nylon 66 yarn and the preparation thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6350519A (en) * 1987-07-31 1988-03-03 Toray Ind Inc Polyhexamethylene adipamide fiber
JPH09268471A (en) * 1996-03-28 1997-10-14 Tong Yang Nylon Co Ltd Polyamide yarn for reinforcing material for rubber product and its production
KR100462924B1 (en) * 2003-10-22 2004-12-23 주식회사 효성 Low shrinkage polyamide fibers for uncoated airbag and process for preparing the same
KR20100021790A (en) 2008-08-18 2010-02-26 주식회사 효성 High-strenth nylon 66 yarn and the preparation thereof

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