KR101159932B1 - A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same - Google Patents

A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same Download PDF

Info

Publication number
KR101159932B1
KR101159932B1 KR1020090135985A KR20090135985A KR101159932B1 KR 101159932 B1 KR101159932 B1 KR 101159932B1 KR 1020090135985 A KR1020090135985 A KR 1020090135985A KR 20090135985 A KR20090135985 A KR 20090135985A KR 101159932 B1 KR101159932 B1 KR 101159932B1
Authority
KR
South Korea
Prior art keywords
fiber bundle
resin
thermoplastic
prepreg
reinforcing fiber
Prior art date
Application number
KR1020090135985A
Other languages
Korean (ko)
Other versions
KR20110079033A (en
Inventor
이상용
김진주
김호연
배만억
양철민
Original Assignee
주식회사 효성
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 주식회사 효성 filed Critical 주식회사 효성
Priority to KR1020090135985A priority Critical patent/KR101159932B1/en
Publication of KR20110079033A publication Critical patent/KR20110079033A/en
Application granted granted Critical
Publication of KR101159932B1 publication Critical patent/KR101159932B1/en

Links

Images

Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/465Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating by melting a solid material, e.g. sheets, powders of fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/02Elements
    • C08K3/04Carbon
    • C08K3/041Carbon nanotubes
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K7/00Use of ingredients characterised by shape
    • C08K7/02Fibres or whiskers
    • 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
    • C08J2300/00Characterised by the use of unspecified polymers
    • C08J2300/22Thermoplastic resins
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/011Nanostructured additives

Landscapes

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

Abstract

본 발명의 구현예들은 열가소성 프리프레그의 제조방법 및 그에 의하여 제조된 열가소성 프리프레그에 관한 것으로, 보다 구체적으로는 열가소성 수지가 결합된 CNT 컴파운드 칩을 강화섬유속에 균일하게 연속 도포하여 프리프레그 내부에 CNT 입자들이 고르게 분산된 열가소성 프리프레그의 제조방법 및 그에 의하여 제조된 열가소성 프리프레그에 관한 것이다. Embodiments of the present invention relate to a method for preparing a thermoplastic prepreg and a thermoplastic prepreg produced by the present invention, and more specifically, to a CNT compound chip having a thermoplastic resin-bonded CNT compound chip uniformly continuously applied to a reinforcing fiber bundle. A method for producing a thermoplastic prepreg in which particles are evenly dispersed and a thermoplastic prepreg produced thereby.

CNT 컴파운드 칩, 열가소성, 프리프레그, 강화섬유속 CNT Compound Chip, Thermoplastic, Prepreg, Reinforced Fiber Bundle

Description

열가소성 프리프레그의 제조방법 및 그에 의하여 제조된 열가소성 프리프레그{A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same}A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same

본 발명의 구현예들은 열가소성 프리프레그의 제조방법 및 그에 의하여 제조된 열가소성 프리프레그에 관한 것이다. Embodiments of the present invention relate to a method for producing a thermoplastic prepreg and a thermoplastic prepreg produced thereby.

최근, 프리프레그가 항공기나 자동차 부품, 스포츠(sports), 레저(leisure) 와 같은 각종 산업분야에 있어서 넓게 이용되고 있다. 예를 들면, 탄소섬유나 유리섬유로된 강화섬유의 단사를 복수개 나란히 하여 이루어진 강화섬유속을 복수개 서로 평행하게 나란하게 놓은 후, 에폭시수지나 불포화폴리에스테르 등의 열경화성 수지를 함침시켜서 시트화한 프리프레그가 항공기용 재료나 자동차용 소재 등의 일반 공업재료 외에도, 예를 들면, 의료용 소재나 스포츠레저용도의 성형재료로서 넓게 이용되고 있다. In recent years, prepregs have been widely used in various industrial fields such as aircraft, automobile parts, sports, and leisure. For example, a plurality of reinforcing fiber bundles formed by plural single yarns of reinforcing fibers made of carbon fibers or glass fibers are laid side by side in parallel with each other, and then prepreg formed by impregnating with a thermosetting resin such as epoxy resin or unsaturated polyester. In addition to general industrial materials such as aircraft materials and automobile materials, they are widely used, for example, as molding materials for medical materials and sports leisure applications.

또한, 필요에 따라 부가적인 성형단계를 거치고, 두 개 이상의 프리프레그 를 적층한 후, 경화와 압밀화 공정을 수행함으로써 프리프레그 적층체를 제조할 수도 있다. 프리프레그 또는 프리프레그 적층체는 대개 열 및 압력에 의해, 또는 진공 백 성형 및 오토클레이브 내 압축에 의해서와 같이 열과 진공을 이용하여 경화 및 압밀화된다.In addition, the prepreg laminate may be manufactured by performing an additional molding step as necessary, laminating two or more prepregs, and then performing a curing and consolidation process. Prepregs or prepreg laminates are usually cured and compacted using heat and vacuum, such as by heat and pressure, or by vacuum bag molding and compression in an autoclave.

최근, 환경보호 차원에서 기존에 기지재로 사용되던 열경화성 수지 대신 복합재료화 했을 경우 차후 분리가 가능한 열가소성수지에 대한 연구가 활발히 진행 중에 있다. 그러나, 열가소성 수지는 열경화성 수지와 달리 상대적으로 높은 점도 때문에 섬유상 기재 등 강화재 상에 함침되기 어렵다. 따라서, 이를 보완할 수 있는 새로운 프리프레그 제작공정이 기술적 과제로 인식되고 있다.Recently, studies on thermoplastic resins that can be separated later are being actively conducted in the case of composite materials instead of thermosetting resins, which are used as base materials for environmental protection. However, thermoplastic resins, unlike thermosetting resins, are difficult to be impregnated on reinforcing materials such as fibrous substrates because of their relatively high viscosity. Therefore, a new prepreg manufacturing process that can compensate for this is recognized as a technical problem.

본 발명의 구현예들은 탄소나노튜브(CNT)와 열가소성 수지가 결합된 컴파운드 칩(compound chip)을 이용하여 수지와 강화섬유의 결합력이 우수할 뿐 아니라 외력에 의한 박리현상을 현저히 저하시킬 수 있는 프리프레그의 제조방법을 제공한다.Embodiments of the present invention by using a compound chip combined with carbon nanotubes (CNT) and a thermoplastic resin (compound chip) not only has excellent bonding strength of the resin and the reinforcing fibers, but also can significantly reduce the peeling phenomenon by external force Provided is a method for producing a leg.

본 발명의 구현예들은 상기 방법에 의해 제조된 우수한 강성 및 강도를 갖는 프리프레그를 제공한다.Embodiments of the present invention provide a prepreg having good stiffness and strength produced by the method.

본 발명의 하나의 양상은, One aspect of the present invention,

강화섬유속을 제공하는 단계;Providing a reinforcing fiber bundle;

이형지를 제공하는 단계;Providing a release paper;

탄소나노튜브(CNT)와 열가소성 수지가 결합된 컴파운드칩을 상기 강화섬유속에 균일하게 공급하는 단계;Supplying a compound chip in which carbon nanotubes (CNT) and a thermoplastic resin are bonded to the reinforcing fiber bundle;

가열판을 이용하여 상기 컴파운드칩을 상기 강화섬유속에 1차 용융 및 함침시켜 강화재를 형성하는 단계; 및Forming a reinforcing material by primary melting and impregnating the compound chip into the reinforcing fiber bundle using a heating plate; And

상기 강화재를 압출기를 이용하여 2차 용융 및 함침시키는 단계를 포함하는 프리프레그 제조방법에 관한 것이다. It relates to a prepreg manufacturing method comprising the step of secondary melting and impregnating the reinforcing material using an extruder.

본 발명의 다른 양상은, 상기 방법에 의하여 제조된 우수한 강성 및 강도를 갖는 프리프레그에 관한 것이다. Another aspect of the present invention relates to a prepreg having excellent stiffness and strength produced by the method.

본 발명의 구현예들에 의하면 프리프레그 제조시 이형지에 도포하는 수지 함침 공정을 생략함으로써 공정을 단순화하여 제조비용을 절감할 수 있으며, 분산성이 좋지 못한 CNT를 칩화하여 강화섬유다발에 균일하게 연속 도포함으로써 CNT가 접목된 열가소성 프리프레그 제작이 가능하다. 또한, 본 발명의 구현예들에 의해 제조된 프리프레그는 CNT입자가 수지와 함께 강화섬유 사이에 함침되어 수지와 강화섬유의 결합력이 우수할 뿐 아니라 구조물 제작시 CNT입자들에 의해 층과 층사이의 계면결합력이 높아져 외력에 의한 박리현상을 현저히 저하시킬 수 있다.According to the embodiments of the present invention, by omitting the resin impregnation process applied to the release paper during prepreg manufacture, the manufacturing process can be simplified to reduce the manufacturing cost, and uniformly continuous to the reinforcing fiber bundles by chipping CNTs having poor dispersibility. By coating, it is possible to produce a thermoplastic prepreg grafted with CNTs. In addition, the prepreg prepared by the embodiments of the present invention is the CNT particles are impregnated between the reinforcing fibers with the resin not only excellent bonding strength of the resin and the reinforcing fibers, but also between the layers and the layers by the CNT particles during the fabrication of the structure The interfacial bonding force of can be increased, and the peeling phenomenon due to external force can be significantly reduced.

이하, 본 발명의 구현예들에 대하여 도면을 참조하여 보다 구체적으로 살펴보면 다음과 같다.Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

도 1은 본 발명의 일 구현예에 의한 열가소성 프리프레그의 제조방법을 단계적으로 설명하기 위한 도면이다. 먼저, 강화섬유속(8)이 언와인더(1)로부터 풀링되고 이형지가 이형지 공급롤(2)에 의해 공급된다.1 is a view for explaining a step of manufacturing a thermoplastic prepreg according to an embodiment of the present invention. First, the reinforcing fiber bundle 8 is pulled from the unwinder 1 and the release paper is supplied by the release paper supply roll 2.

본 발명의 일 구현예에서, 강화섬유속(8)은 복수개의 단사가 나란히 된 1 개의 섬유속이거나, 이 섬유속이 복수개 서로 평행하게 나란히 되어 시트상으로 되어 있는 섬유속일 수 있다. 또한, 강화섬유속(8)을 형성하는 강화섬유의 종류는 특별히 한정되지 않고, 탄소섬유나 유리섬유, 아라미드섬유 등이 적용될 수 있다. 또한, 이형지로는 단면 또는 양면에 열에 강한 실리콘 계열이 코팅된 종이류를 사용할 수 있다. In one embodiment of the present invention, the reinforcing fiber bundle 8 may be one fiber bundle in which a plurality of single yarns are side by side, or a fiber bundle in which a plurality of fiber bundles are parallel to each other in a sheet form. The type of reinforcing fibers forming the reinforcing fiber bundle 8 is not particularly limited, and carbon fibers, glass fibers, aramid fibers, or the like may be applied. In addition, the release paper may be a paper type coated with heat resistant silicone based on one side or both sides.

다음으로 미리 제작된 CNT 열가소성 컴파운드 칩(compound chip)(4)을 공급할 수 있는 회전형 칩공급기(3)을 통해 CNT 열가소성 컴파운드 칩(4)을 강화섬유속(8) 상단에 균일 도포한다. Next, the CNT thermoplastic compound chip 4 is uniformly coated on the reinforcing fiber bundle 8 through the rotary chip feeder 3 capable of supplying a pre-fabricated CNT thermoplastic compound chip 4.

CNT 열가소성 컴파운드 칩은 모재(Matrix)로 폴리에틸렌수지, 나일론수지, 폴리아세탈수지, 염화비닐수지, 폴리스티렌수지, ABS수지, 아크릴수지 또는 이들의 혼합물인 열가소성 수지를 사용하며 열가소성 수지에 대한 CNT의 함량비는 0.1 내지 1.5wt% 비율로 한다. CNT thermoplastic compound chip uses thermoplastic resin which is polyethylene resin, nylon resin, polyacetal resin, vinyl chloride resin, polystyrene resin, ABS resin, acrylic resin or mixtures thereof as matrix, and the content ratio of CNT to thermoplastic resin Is 0.1 to 1.5wt% ratio.

익스트루더(Extruder)와 같은 칩 형태로의 가공이 가능한 장비를 사용하여 CNT와 열가소성수지를 혼합한다. 이 때 CNT와 열가소성수지의 결합력 및 분산상태를 높이기 위해 CNT표면을 화학적으로 처리할 수 있고, 용제를 사용하거나 믹서(mixer)를 사용한 기계적 분산 등이 가능하다.CNTs and thermoplastics are mixed using equipment that can be processed into chips, such as extruders. At this time, the surface of the CNT can be chemically treated to increase the bonding strength and dispersion state of the CNT and the thermoplastic resin, and mechanical dispersion using a solvent or a mixer is possible.

이와 같이 본 발명의 구현예들은 CNT 열가소성 컴파운드 칩(4)을 사용하여 프리프레그 제조시 이형지에 도포하는 수지 함침 공정을 생략하여 공정을 단순화할 수 있다. 또한, 분산성이 좋지 못한 CNT를 칩화하여 강화섬유다발에 균일하게 연속 도포할 수 있을 뿐 아니라 CNT입자가 수지와 함께 강화섬유 사이에 함침되 어 수지와 강화섬유의 결합력을 증대시킬 수 있다. 이러한 CNT가 접목된 열가소성 프리프레그를 이용해 구조물을 제작하면 CNT입자들에 의해 층과 층사이의 계면결합력이 높아져 외력에 의한 박리현상을 현저히 저하시킬 수 있다.As described above, the embodiments of the present invention can simplify the process by omitting the resin impregnation process applied to the release paper when preparing the prepreg using the CNT thermoplastic compound chip 4. In addition, the CNTs with poor dispersibility may be chipped and uniformly applied to the reinforcing fiber bundles, and the CNT particles may be impregnated between the reinforcing fibers together with the resin to increase the bonding strength of the resin and the reinforcing fibers. When the structure is manufactured using the thermoplastic prepreg grafted with CNTs, the interfacial bonding force between the layers is increased by the CNT particles, which may significantly reduce the peeling phenomenon due to external force.

본 발명의 일 구현예에서 상기 회전형 칩공급기(3)의 내부에 톱니바퀴형상 공급기(5)가 장착될 수 있는데, 이에 의해 칩의 균일한 공급이 가능하다. 도 2는 본 발명의 일 구현예에 의한 회전형 칩공급기(3)의 내부도로서, 톱니바퀴형상 공급기(5)가 도시되었다. In one embodiment of the present invention, the gear-shaped feeder 5 may be mounted inside the rotary chip feeder 3, whereby a uniform supply of chips is possible. 2 shows an internal view of a rotary chip feeder 3 according to an embodiment of the invention, in which a gear feeder 5 is shown.

본 발명의 구현예들에서 CNT와 결합하는 열가소성 수지는 필요에 따라 열 안정제, 가소제, 화학 경화제, 무기 충진재, 점도 조절제, 광 안정제 등의 첨가제를 더 포함할 수 있다. 이러한 열가소성 합성수지 조성물은 불용성인 것이 바람직하나, 반드시 이에 한정되는 것은 아니다.In the embodiments of the present invention, the thermoplastic resin bonded to the CNT may further include additives such as a heat stabilizer, a plasticizer, a chemical curing agent, an inorganic filler, a viscosity modifier, and a light stabilizer, as necessary. The thermoplastic synthetic resin composition is preferably insoluble, but is not necessarily limited thereto.

다음, 도포된 CNT 컴파운드 칩은 가열판(6)을 통해 1차적으로 용용 함침되고, 생성된 강화재는 상하 압출기(7)를 통해 2차 용융 함침된다. 이후 냉각수에 의해 강화섬유속을 냉각시키면 열가소성 프리프레그가 형성된다.The applied CNT compound chips are then melt impregnated primarily through the heating plate 6, and the resulting reinforcing material is secondary melt impregnated through the upper and lower extruders 7. After cooling the reinforcing fiber bundle with cooling water, a thermoplastic prepreg is formed.

상하 압출기(7)는 금속 재질 또는 고무 재질의 롤이 두 개 이상 조합되어 사용된다. 또한, 형성된 열가소성 프리프레그에 요철을 부여하도록 상하 압출기(7)에는 요철이 형성될 수 있다.The upper and lower extruders 7 are used in combination of two or more rolls of metal or rubber. In addition, irregularities may be formed in the upper and lower extruders 7 to impart irregularities to the formed thermoplastic prepreg.

본 발명의 다른 구현예에 의하면 형성된 열가소성 프리프레그의 표면을 매끄럽게 하기 위하여 상기 열가소성 프리프레그를 가열하고 압연하는 단계를 더 포함할 수 있다.According to another embodiment of the present invention, the method may further include heating and rolling the thermoplastic prepreg to smooth the surface of the formed thermoplastic prepreg.

이하에서 실시예를 통하여 본 발명을 보다 상세하게 설명하고자 하나, 하기의 실시예는 단지 설명의 목적을 위한 것으로 본 발명을 제한하기 위한 것은 아니다.Hereinafter, the present invention will be described in more detail with reference to Examples, but the following Examples are for illustrative purposes only and are not intended to limit the present invention.

실시예Example 1:열가소성  1: thermoplastic 프리프레그Prepreg 제조 Produce

열가소성 프리프레그의 제조를 위한 섬유상 기재로는 단일벽 탄소섬유를, 이형지로는 양면에 실리콘이 코팅된 종이를 사용하였고, CNT함량이 0.5wt%인 CNT 열가소성 컴파운드 칩을 이용하였다. Single-walled carbon fiber was used as a fibrous base material for the preparation of the thermoplastic prepreg, and a silicon coated paper was used as a release paper, and a CNT thermoplastic compound chip having a CNT content of 0.5 wt% was used.

도 1에 도시된 바와 같이, 탄소섬유 직물을 풀링하면서, 이형지를 공급하였다. 이어서, 회전형 칩공급기을 통해 CNT 열가소성 컴파운드 칩을 강화섬유 상단에 균일하게 도포하였다. 다음, 도포된 CNT 컴파운드 칩을 가열판을 통해 1차적으로 용용 함침시키고, 생성된 강화재를 상하 압출기를 통해 2차 용융 함침시켰다. 1차 용융온도는 통상적으로 Tg-5℃이상, Tg +20℃이하의 온도에서 작업하고, 압출을 통한 2차 용융 함침은 일반적으로는 온도범위는 Tm-10℃이상 Tm+20℃이하, 압력은 0~20kg/cm2 범위이다.
이후 냉각수에 의해 탄소섬유 직물을 냉각시켜 열가소성 프리프레그를 제조하였다.
상기 제조된 프리프레그는 CNT를 먼저 열가소성 수지에 분산시키고, 이를 칩 형태로 프리프레그 제조공정에 투입함으로써, 기존 방법인 수지에 프리프레그를 분산시키거나 프리프레그 제조과정에서 CNT를 도포하는 방법에 비해 CNT 함량 조절 및 균일 분산을 확보할 수 있다.
As shown in Figure 1, while releasing the carbon fiber fabric, the release paper was fed. Subsequently, the CNT thermoplastic compound chip was evenly applied on top of the reinforcing fiber through the rotary chip feeder. Next, the applied CNT compound chip was melt impregnated primarily through a heating plate, and the resulting reinforcing material was secondary melt impregnated through an up and down extruder. The primary melting temperature is typically above Tg-5 ℃ and below Tg + 20 ℃, and the secondary melt impregnation through extrusion generally has a temperature range of Tm-10 ℃ and above Tm + 20 ℃ and pressure. Is in the range of 0 to 20 kg / cm 2 .
After cooling the carbon fiber fabric with cooling water to prepare a thermoplastic prepreg.
The prepared prepreg is first dispersed in the thermoplastic resin, and then in the form of chips into the prepreg manufacturing process, by dispersing the prepreg in the resin, which is a conventional method or applying the CNT in the prepreg manufacturing process Control of CNT content and uniform dispersion can be ensured.

도 1은 본 발명의 일 구현예에 의한 열가소성 프리프레그의 제조방법을 단계적으로 설명하기 위한 도면이다. 1 is a view for explaining a step of manufacturing a thermoplastic prepreg according to an embodiment of the present invention.

도 2는 본 발명의 일 구현예에 의한 회전형 칩공급기의 내부도이다. Figure 2 is an internal view of a rotary chip feeder according to an embodiment of the present invention.

** 도면의 주요 부호에 대한 설명 ** ** Description of the main symbols in the drawings **

1: 언와인더 2: 이형지 공급롤1: unwinder 2: release paper feed roll

3: 회전형 칩공급기 4: CNT 열가소성 컴파운드 칩3: rotary chip feeder 4: CNT thermoplastic compound chip

5: 톱니바퀴형상 공급기 6: 가열판5: gear shape feeder 6: heating plate

7: 상하 압출기 8: 강화섬유속7: top and bottom extruder 8: reinforcing fiber bundle

Claims (9)

강화섬유속을 제공하는 단계;Providing a reinforcing fiber bundle; 이형지를 제공하는 단계;Providing a release paper; 탄소나노튜브(CNT)와 열가소성 수지가 결합된 컴파운드칩을 내부에 톱니바퀴형상의 회전형 공급기가 장착된 칩공급기에 의해 상기 강화섬유속에 균일하게 공급하는 단계;Supplying a compound chip in which carbon nanotubes (CNT) and a thermoplastic resin are bonded to the reinforcing fiber bundle by a chip feeder equipped with a rotary feeder having a gear shape therein; 가열판을 이용하여 상기 컴파운드칩을 상기 강화섬유속에 1차 용융 및 함침시켜 강화재를 형성하는 단계; 및Forming a reinforcing material by primary melting and impregnating the compound chip into the reinforcing fiber bundle using a heating plate; And 상기 강화재를 압출기를 이용하여 2차 용융 및 함침시키는 단계를 포함하는 프리프레그 제조방법. The prepreg manufacturing method comprising the step of secondary melting and impregnating the reinforcing material using an extruder. 삭제delete 제 1항에 있어서, 상기 강화섬유속은 복수개의 단사가 나란히 된 1개의 섬유속인 것을 특징으로 하는 프리프레그 제조방법.The method of claim 1, wherein the reinforcing fiber bundle is a single fiber bundle having a plurality of single yarns side by side. 제 3항에 있어서, 상기 강화섬유속은 상기 1개의 섬유속이 복수개 서로 평행하게 시트상으로 되어 있는 섬유속인 것을 특징으로 하는 프리프레그 제조방법.4. The method according to claim 3, wherein the reinforcing fiber bundle is a fiber bundle in which one fiber bundle is formed in a plurality of sheets in parallel with each other. 제 1항에 있어서, 상기 강화섬유속은 탄소섬유, 유리섬유, 아라미드섬유로 이루어진 군으로부터 선택되는 1종 이상으로 형성되는 것을 특징으로 하는 프리프레그 제조방법.The method of claim 1, wherein the reinforcing fiber bundle is formed of at least one member selected from the group consisting of carbon fibers, glass fibers, and aramid fibers. 제 1항에 있어서, 상기 열가소성 수지는 폴리에틸렌수지, 나일론수지, 폴리아세탈수지, 염화비닐수지, 폴리스티렌수지, ABS수지, 아크릴수지 또는 이들의 혼합물로 이루어진 군으로부터 선택되는 1 종 이상의 열가소성 고분자인 것을 특징으로 하는 프리프레그 제조방법.The method of claim 1, wherein the thermoplastic resin is at least one thermoplastic polymer selected from the group consisting of polyethylene resin, nylon resin, polyacetal resin, vinyl chloride resin, polystyrene resin, ABS resin, acrylic resin or mixtures thereof. Prepreg manufacturing method to use. 제 1항에 있어서, 상기 열가소성 수지에 대한 탄소나노튜브(CNT)의 함량비는 0.1 내지 1.5wt% 인 것을 특징으로 하는 프리프레그 제조방법. The method of claim 1, wherein the content ratio of carbon nanotubes (CNT) to the thermoplastic resin is 0.1 to 1.5 wt%. 제1항에 있어서, 상기 제 2차 용융 및 함침 단계 이후에 상기 형성된 열가소성 프리프레그를 가열하고 압연하여 열가소성 프리프레그의 표면을 매끄럽게 하는 단계를 더 포함하는 것을 특징으로 하는 열가소성 프리프레그의 제조방법.The method of claim 1, further comprising: heating and rolling the formed thermoplastic prepreg after the second melting and impregnation step to smooth the surface of the thermoplastic prepreg. 제 1항, 3항 내지 제 8항 중 어느 한 항의 방법에 의해 제작된 프리프레그.A prepreg produced by the method of any one of claims 1 and 3 to 8.
KR1020090135985A 2009-12-31 2009-12-31 A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same KR101159932B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020090135985A KR101159932B1 (en) 2009-12-31 2009-12-31 A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020090135985A KR101159932B1 (en) 2009-12-31 2009-12-31 A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same

Publications (2)

Publication Number Publication Date
KR20110079033A KR20110079033A (en) 2011-07-07
KR101159932B1 true KR101159932B1 (en) 2012-06-26

Family

ID=44918449

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020090135985A KR101159932B1 (en) 2009-12-31 2009-12-31 A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same

Country Status (1)

Country Link
KR (1) KR101159932B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102531103B1 (en) * 2016-12-20 2023-05-10 현대자동차주식회사 Manufacturing method of carbon fiber reinforced plastics film

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03155908A (en) * 1989-11-14 1991-07-03 Toray Ind Inc Manufacture of prepreg
KR940011168B1 (en) * 1990-11-29 1994-11-24 미쓰비시레이욘 가부시키가이샤 Prepregs, process for producing the same and laminates produced with the same
JPH09183122A (en) * 1995-12-28 1997-07-15 Nippon Zeon Co Ltd Manufacture of sheet molding compound
JP2009091377A (en) * 2007-10-03 2009-04-30 Arisawa Mfg Co Ltd Apparatus for producing prepreg

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03155908A (en) * 1989-11-14 1991-07-03 Toray Ind Inc Manufacture of prepreg
KR940011168B1 (en) * 1990-11-29 1994-11-24 미쓰비시레이욘 가부시키가이샤 Prepregs, process for producing the same and laminates produced with the same
JPH09183122A (en) * 1995-12-28 1997-07-15 Nippon Zeon Co Ltd Manufacture of sheet molding compound
JP2009091377A (en) * 2007-10-03 2009-04-30 Arisawa Mfg Co Ltd Apparatus for producing prepreg

Also Published As

Publication number Publication date
KR20110079033A (en) 2011-07-07

Similar Documents

Publication Publication Date Title
US11413832B2 (en) Fluidized-bed process for manufacturing a fibrous material preimpregnated with thermoplastic polymer
EP2440390B1 (en) Method of delivering a thermoplastic and/or crosslinking resin to a composite laminate structure
KR101784534B1 (en) Thermoplastic composites and methods of making and using same
US20100218890A1 (en) Methods for preparing nanoparticle-containing thermoplastic composite laminates
JP5774788B2 (en) Heat-resistant paper and method for producing the same, fiber-reinforced heat-resistant resin molding and precursor thereof, and methods for producing the same
WO2013127368A1 (en) Composite material containing plant fibre fabrics and preparation method thereof
KR101934059B1 (en) Thermoplastic prepreg and method for producing the same
US10059080B2 (en) Method for the production of a fiber composite component, and semifinished textile product therefor
TWI697398B (en) Manufacturing method of structure
KR101417245B1 (en) Complex sheet manufacturing device with excellent saturation property and method of manufacturing high strength complex sheet
JP6700049B2 (en) Carbon fiber sheet material, prepreg, laminated body, molded body and manufacturing method thereof
JP7425731B2 (en) Carbon fiber sheet material, prepreg, molded body, method for manufacturing carbon fiber sheet material, method for manufacturing prepreg, and method for manufacturing molded body
KR20150093745A (en) Articles including untwisted fibers and methods of using them
CN105538816A (en) Flaky molded material-prepreg mixed composite material and manufacturing method thereof
CN106881931A (en) Thermoplas tic resin composite and the preparation method of thermoplas tic resin composite
WO2011116923A2 (en) Fiber reinforced putty, device and method for its manufacture, device and method to make laminates and other finished parts from the putty, and a laminate made from the putty
JP6000497B1 (en) Fiber-reinforced composite material and method for producing the same
CN109263181A (en) A kind of light fibre enhancing plastic composite board material and preparation method thereof
JP5966969B2 (en) Manufacturing method of prepreg
KR101159932B1 (en) A method of preparing thermoplastic prepreg and thermoplastic prepreg prepared by the same
KR20180079729A (en) Quasi-Isotropic Product using the fiber reinforced composite material and manufacturing method therof
JP2020063334A (en) Production method of carbon fiber prepreg, production method of carbon fiber-reinforced resin formed part, and carbon fiber-reinforced formed part
Kanhere et al. Carbon and glass fiber reinforced thermoplastic matrix composites
KR101263976B1 (en) Method For Preparing Composite Sheet Having Excellent Ecomomical Efficiency And Physical Property, Apparatus Thereof And Composite Sheet Prepared Therefrom
KR102470605B1 (en) High-glossy thermoplastic prepreg laminates which have high resin contents, and method for producing the same

Legal Events

Date Code Title Description
A201 Request for examination
E701 Decision to grant or registration of patent right
GRNT Written decision to grant
FPAY Annual fee payment

Payment date: 20150514

Year of fee payment: 4

LAPS Lapse due to unpaid annual fee