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KR960004416A - Method for manufacturing glass fiber reinforced thermoplastic composite prepreg - Google Patents

Method for manufacturing glass fiber reinforced thermoplastic composite prepreg Download PDF

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Publication number
KR960004416A
KR960004416A KR1019940018168A KR19940018168A KR960004416A KR 960004416 A KR960004416 A KR 960004416A KR 1019940018168 A KR1019940018168 A KR 1019940018168A KR 19940018168 A KR19940018168 A KR 19940018168A KR 960004416 A KR960004416 A KR 960004416A
Authority
KR
South Korea
Prior art keywords
thermoplastic composite
glass fiber
composite prepreg
prepreg
glass fibers
Prior art date
Application number
KR1019940018168A
Other languages
Korean (ko)
Other versions
KR0130429B1 (en
Inventor
임대우
강창권
김태호
Original Assignee
박홍기
제일합섬 주식회사
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 박홍기, 제일합섬 주식회사 filed Critical 박홍기
Priority to KR1019940018168A priority Critical patent/KR0130429B1/en
Publication of KR960004416A publication Critical patent/KR960004416A/en
Application granted granted Critical
Publication of KR0130429B1 publication Critical patent/KR0130429B1/en

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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/244Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using glass fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/06Reinforcing macromolecular compounds with loose or coherent fibrous material using pretreated fibrous materials
    • C08J5/08Reinforcing macromolecular compounds with loose or coherent fibrous material using pretreated fibrous materials glass fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/248Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using pre-treated fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2323/00Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers
    • C08J2323/02Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers not modified by chemical after treatment
    • C08J2323/10Homopolymers or copolymers of propene
    • C08J2323/12Polypropene

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

본 발명은 특정 방향의 내 충격성, 인장강도 등이 기계적 물성을 유지하면서 그의 직각방향의 기계적물성을 향상시켜 자동차 범퍼빔, 토목, 건축용 등의 구조재에 사용될 수 있는 열가소성 복합재료 프리 프레그를 제조하는 방법에 관한 것이다.The present invention is a method of manufacturing a thermoplastic composite prepreg that can be used in structural materials such as automobile bumper beams, civil engineering, construction by improving the mechanical properties in the perpendicular direction while maintaining the mechanical properties of impact resistance, tensile strength, etc. in a specific direction It is about.

즉, 본 발명은 유리섬유 매트로 유리섬유 로빙을 무배향의 균일한 웨브(web)를 형성하고 그 위에 일방향 및 그의 직각방향으로 유리섬유를 배열한 후 니들펀칭하여 제조된 것을 사용하여 폴리프로필렌수지를 유리섬유 매트에 열용융 함침하여 판상의 열가소성 복합재료 포리프레그를 제조한 것으로서, 본 발명에 의해 제조된 경우 경량이면서 특정 방향으로의 기계적 강도가 우수할 뿐만 아니라 그의 직각방향의 물성도 향상되어 여러가지 용도로 사용 가능한 잇점이 있다.That is, the present invention forms a uniform web of glass fiber roving with a glass fiber mat, and arranges the glass fibers in one direction and at right angles thereon, and then uses a polypropylene resin prepared by needle punching. Was manufactured by hot-melt impregnating a glass fiber mat into a plate-like thermoplastic composite polypreg, and when manufactured according to the present invention, it is lightweight and has excellent mechanical strength in a specific direction, and its physical properties in a right direction are also improved. There are advantages that can be used for this purpose.

Description

유리섬유 강화 열가소성 복합재료 프리프레그의 제조방법Method for manufacturing glass fiber reinforced thermoplastic composite prepreg

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음As this is a public information case, the full text was not included.

제2도는 본 발명에 따른 열가소성 복합재료 프리프레그 단면도2 is a cross-sectional view of the thermoplastic composite prepreg according to the present invention

Claims (5)

폴리프로필렌 수지를 유지섬유 매트에 열용융 함침하여 판상의 열가소성 복합재료 프리프레그를 제조함에 있어서, 유리섬유 매트는 유리섬유 로빙을 무배향의 균일한 웨브(web)를 형성하고 그 위에 일방향 및 그의 직각 방향으로 유리섬유를 배열한 후 니들펀칭하여 제조되는 것을 특징으로 하는 열가소성 복합재료 프리프레그.In producing a plate-like thermoplastic composite prepreg by heat-melting impregnating a polypropylene resin on a fat fiber mat, the glass fiber mat forms a uniform web of non-oriented glass fiber rovings and is oriented in one direction and right angles thereon. The thermoplastic composite material prepreg is produced by needle punching after arranging the glass fibers in the direction. 제1항에 있어서, 일방향으로 배열된 유리섬유가 유리섬유 총중량에 대하여 30-70 중량%, 일방향의 직각 방향으로 배열된 유리섬유는 유리섬유 총중량의 10-30 중량% 범위 내에 있는 것을 특징으로 하는 열가소성 복합재료 프리프레그.The method of claim 1, wherein the glass fibers arranged in one direction is 30-70% by weight relative to the total weight of the glass fibers, the glass fibers arranged in a direction perpendicular to the one direction is in the range of 10-30% by weight of the total weight of the glass fibers. Thermoplastic Composite Prepreg. 제1항에 있어서, 열가소성 복합수지 프리프레그는 유리섬유가 열가소성 복합수지 프리프레그 총중량에 대하여 20-60% 범위 내에서 사용되는 것을 특징으로 하는 열가소성 복합재료 프리프레그.The thermoplastic composite prepreg according to claim 1, wherein the thermoplastic composite prepreg is used in the range of 20-60% of the glass fiber in the total weight of the thermoplastic composite prepreg. 제1항에 있어서, 유리섬유는 10-30㎛ 굵기의 유리섬유 필타멘트를 50-3000개 집속시킨 것임을 특징으로 하는 열가소성 븍합재료 프리프레그.The method of claim 1, wherein the glass fiber is a thermoplastic composite material prepreg characterized in that the concentration of 50-3000 pieces of glass fiber filament of 10-30㎛ thickness. 제1항에 있어서, 폴리프로필렌 수지는 용융지수가 2-20g/10min의 것을 사용한 것임을 특징으로 하는 열가소성 복합재료 프리프레그.The thermoplastic composite prepreg according to claim 1, wherein the polypropylene resin uses a melt index of 2-20 g / 10 min. ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019940018168A 1994-07-26 1994-07-26 Process for making glass fiber reinforced thermoplastic composite material prepreg KR0130429B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019940018168A KR0130429B1 (en) 1994-07-26 1994-07-26 Process for making glass fiber reinforced thermoplastic composite material prepreg

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019940018168A KR0130429B1 (en) 1994-07-26 1994-07-26 Process for making glass fiber reinforced thermoplastic composite material prepreg

Publications (2)

Publication Number Publication Date
KR960004416A true KR960004416A (en) 1996-02-23
KR0130429B1 KR0130429B1 (en) 1998-04-07

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100607260B1 (en) * 1999-06-03 2006-07-28 에스케이케미칼주식회사 Composite plate for a shoe
KR20200055502A (en) * 2018-11-13 2020-05-21 주식회사 포스코 Mold, apparatus and method for casting

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100716027B1 (en) * 2005-11-16 2007-05-11 삼성토탈 주식회사 Polypropylene compounds for concrete mold form panel
KR101037609B1 (en) * 2009-05-14 2011-05-30 한화엘앤씨 주식회사 Hybrid composite material with enhanced crash performances
KR101472683B1 (en) * 2013-08-14 2014-12-12 롯데케미칼 주식회사 Manufacturing method of bumper beam for vehicle
KR20150044187A (en) * 2013-10-16 2015-04-24 코오롱인더스트리 주식회사 Hybrid prepreg for car bumper and car bumper manufactured thereby
KR102552009B1 (en) * 2018-10-31 2023-07-10 주식회사 서연이화 Composite material for vehicle interior and manufacturing method for the same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100607260B1 (en) * 1999-06-03 2006-07-28 에스케이케미칼주식회사 Composite plate for a shoe
KR20200055502A (en) * 2018-11-13 2020-05-21 주식회사 포스코 Mold, apparatus and method for casting

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Publication number Publication date
KR0130429B1 (en) 1998-04-07

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