KR20080083957A - High Rigid Thermoplastic Composites - Google Patents
High Rigid Thermoplastic Composites Download PDFInfo
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- KR20080083957A KR20080083957A KR1020070024875A KR20070024875A KR20080083957A KR 20080083957 A KR20080083957 A KR 20080083957A KR 1020070024875 A KR1020070024875 A KR 1020070024875A KR 20070024875 A KR20070024875 A KR 20070024875A KR 20080083957 A KR20080083957 A KR 20080083957A
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- 229920001169 thermoplastic Polymers 0.000 title claims abstract description 81
- 239000004416 thermosoftening plastic Substances 0.000 title claims abstract description 81
- 239000002131 composite material Substances 0.000 title claims abstract description 44
- 230000002787 reinforcement Effects 0.000 claims abstract description 28
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 28
- 239000003365 glass fiber Substances 0.000 claims abstract description 25
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 20
- 239000004743 Polypropylene Substances 0.000 claims abstract description 12
- -1 polypropylene Polymers 0.000 claims abstract description 12
- 229920001155 polypropylene Polymers 0.000 claims abstract description 12
- 229920000728 polyester Polymers 0.000 claims abstract description 7
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 4
- 239000004917 carbon fiber Substances 0.000 claims abstract description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000012779 reinforcing material Substances 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 12
- 238000000465 moulding Methods 0.000 claims description 9
- 230000008569 process Effects 0.000 claims description 7
- 239000002759 woven fabric Substances 0.000 claims description 7
- 239000003733 fiber-reinforced composite Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 18
- 238000003825 pressing Methods 0.000 abstract description 2
- 238000000926 separation method Methods 0.000 abstract 1
- 239000004744 fabric Substances 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 3
- 239000000654 additive Substances 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000011152 fibreglass Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000012815 thermoplastic material Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
- B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
- B32B17/10009—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets
- B32B17/10018—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising only one glass sheet
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/045—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/02—Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0253—Polyolefin fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0276—Polyester fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
- B32B2315/08—Glass
- B32B2315/085—Glass fiber cloth or fabric
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
- B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
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- Engineering & Computer Science (AREA)
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Abstract
Description
도 1은 본 발명의 일 실시예에 따른 고강성 열가소성 보강재를 적용한 제품의 단면도이다.1 is a cross-sectional view of a product to which a high rigidity thermoplastic reinforcement is applied according to an embodiment of the present invention.
도 2는 본 발명에 따른 고강성 열가소성 보강재의 일 예를 나타내는 단면도이다.2 is a cross-sectional view showing an example of a highly rigid thermoplastic reinforcing material according to the present invention.
도 3은 본 발명의 다른 고강성 열가소성 보강재를 적용한 제품을 나타내는 실시예이다.Figure 3 is an embodiment showing a product to which another high rigidity thermoplastic reinforcement of the present invention is applied.
도 4는 본 발명에 따른 고강성 열가소성 보강재의 다른 예를 나타내는 단면도이다.4 is a cross-sectional view showing another example of a high rigid thermoplastic reinforcing material according to the present invention.
본 발명은 고강성 열가소성 복합재에 관한 것이다.The present invention relates to a high rigid thermoplastic composite.
최근 자동차 산업에서는 차량의 중량 증가에 따라 경량화 및 요구 특성이 높아지면서 사용 소재의 강도 및 강성 향상이 크게 요구되고 있다. 이러한 추세에서, 열가소성 복합재료는 높은 비강성으로 인하여 적용이 증가하고 있어 GMT(유리섬유 매트 열가소성 복합재), LFT(장섬유강화 복합재) 등의 소재의 적용이 증가하고 있다.Recently, in the automobile industry, as the weight of a vehicle increases, the weight and demand characteristics thereof increase, and thus, the strength and rigidity of the material used are greatly increased. In this trend, the application of thermoplastic composite materials is increasing due to the high specific rigidity, and the application of materials such as GMT (glass fiber mat thermoplastic composite) and LFT (long fiber reinforced composite) is increasing.
그러나, 이들 소재는 유동성을 이용한 프레스 성형법을 사용해야 하는 제약이 있기 때문에, GMT는 유동성이 가능한 부직(non-woven) 형태의 유리섬유매트를 사용하고, LFT는 촙드(chopped) 유리섬유를 사용하므로 특성을 향상시키는데 한계가 있다. However, since these materials have limitations in using a press molding method using fluidity, GMT uses a non-woven glass fiber mat capable of fluidity, and LFT uses chopped glass fiber. There is a limit to improve.
이를 해결하기 위해, 성형시 별도의 보강재를 삽입하는 방법이 적용되고 있으나, 보강재 적층 및 유동성의 어려움뿐만 아니라 박리 현상 등의 문제가 있어 적용에 한계가 있다.In order to solve this problem, a method of inserting a separate reinforcement during molding has been applied, but there are limitations in application due to problems such as peeling phenomenon as well as difficulty in laminating reinforcement and fluidity.
따라서, 본 발명의 목적은 유동성을 갖는 고강성 열가소성 복합재를 제조하여 제품 강도와 강성을 높이는 동시에 성형시 박리 현상을 없애는 것이다.Accordingly, an object of the present invention is to manufacture a highly rigid thermoplastic composite having fluidity, to improve product strength and rigidity and to eliminate peeling during molding.
본 발명의 특징 및 이점은 이하에 기술되는 실시예로부터 명확하게 이해될 것이다.The features and advantages of the present invention will be clearly understood from the embodiments described below.
상기한 목적은 직조 보강부재와, 상기 보강부재의 표면과 이면 중 적어도 한 면에 함침된 열가소성 수지 또는 열가소성 수지/유리섬유의 열가소성 복합재로 구성되는 고강성 열가소성 보강재에 의해 달성된다.The above object is achieved by a woven reinforcement member and a highly rigid thermoplastic reinforcement composed of a thermoplastic resin or a thermoplastic composite of thermoplastic resin / glass fiber impregnated on at least one of the front and back surfaces of the reinforcement member.
바람직하게, 상기 직조 보강부재는 유리섬유 직조물, 폴리에스테르 직조물, 유리섬유와 폴리프로필렌의 혼합 직조물, 또는 카본파이버로 이루어질 수 있다.Preferably, the woven reinforcing member may be made of glass fiber woven fabric, polyester woven fabric, mixed woven fabric of glass fiber and polypropylene, or carbon fiber.
또한, 상기 성형 가공은 프레스 가공일 수 있다.In addition, the molding process may be a press process.
상기의 목적은 열가소성 복합시트; 및 상기 열가소성 복합시트의 표면 또는 이면에 적층되는 고강성 열가소성 보강재를 포함하며, 상기 열가소성 보강재는 직조 보강부재와, 상기 직조 보강부재의 표면과 이면 중 적어도 한 면에 함침된 열가소성 수지 또는 열가소성 수지/유리섬유로 이루어지며, 상기 열가소성 복합시트와 상기 열가소성 보강부재가 적층된 상태에서 동시에 성형 가공되어 이루어지는 고강성 열가소성 복합재에 의해 달성된다.The above object is a thermoplastic composite sheet; And a high rigid thermoplastic reinforcing material laminated on the surface or the back of the thermoplastic composite sheet, wherein the thermoplastic reinforcing material is a woven reinforcing member, and a thermoplastic resin or thermoplastic resin impregnated on at least one of the front and back surfaces of the woven reinforcing member / It is made of a glass fiber, it is achieved by a high-stiffness thermoplastic composite which is molded at the same time in the laminated state of the thermoplastic composite sheet and the thermoplastic reinforcing member.
또한, 상기한 목적은 다수 매가 적층된 열가소성 복합시트; 및 상기 적층된 열가소성 복합시트의 최상부, 최하부 또는 이들 사이에 위치하는 고강성 열가소성 보강재를 포함하며, 상기 열가소성 보강재는 직조 보강부재와, 상기 직조 보강부재의 표면과 이면 중 적어도 한 면에 함침된 열가소성 수지 또는 열가소성 수지/유리섬유로 이루어지며, 상기 열가소성 복합시트와 상기 열가소성 보강부재가 적층된 상태에서 동시에 성형 가공되어 이루어지는 고강성 열가소성 복합재에 의해 달성된다.In addition, the above object is a thermoplastic composite sheet laminated a plurality of sheets; And a high stiffness thermoplastic reinforcing member positioned on the top, bottom, or between the laminated thermoplastic composite sheets, wherein the thermoplastic reinforcing material includes a woven reinforcing member, and a thermoplastic impregnated on at least one surface of the woven reinforcing member and a surface thereof. It is made of a resin or a thermoplastic resin / glass fiber, and is achieved by a high-stiffness thermoplastic composite material which is molded at the same time in the laminated state of the thermoplastic composite sheet and the thermoplastic reinforcing member.
바람직하게, 상기 열가소성 복합시트는 유리섬유매트 열가소성 복합재(GMT) 또는 장섬유강화 복합재(LFT)로 구성될 수 있다.Preferably, the thermoplastic composite sheet may be composed of a glass fiber mat thermoplastic composite (GMT) or a long fiber reinforced composite (LFT).
이하, 첨부된 도면을 참조하여 본 발명의 실시예를 설명한다.Hereinafter, with reference to the accompanying drawings will be described an embodiment of the present invention.
도 1은 본 발명의 일 실시예에 따른 고강성 열가소성 보강재를 적용한 제품의 단면도이다.1 is a cross-sectional view of a product to which a high rigidity thermoplastic reinforcement is applied according to an embodiment of the present invention.
도 1을 참조하면, 상하로 적층되는 두 GMT 소재(100, 300) 사이에는 본 발명 에 따른 고강성 열가소성 보강재가 삽입되고, 가령 프레스 공정으로 성형된다.Referring to FIG. 1, a high rigid thermoplastic reinforcement according to the present invention is inserted between two GMT
도 2는 본 발명에 따른 고강성 열가소성 보강재의 일 예를 나타내는 단면도이다.2 is a cross-sectional view showing an example of a highly rigid thermoplastic reinforcing material according to the present invention.
도 2를 참조하면, 유리섬유 직조물이나 폴리에스테르 직조물, 유리섬유와 폴리프로필렌의 혼합 직조물, 또는 카본파이버 등의 직조(woven) 보강부재(220)의 표면과 이면에 각각 열가소성 수지 또는 열가소성 수지와 유리섬유로 이루어진 열가소성 복합재(210, 230)가 함침된다.Referring to FIG. 2, thermoplastic resins or thermoplastic resins and glass are respectively formed on the front and back surfaces of
이와 같이 구성된 고강성 열가소성 보강재(200)를 개재하여 상하에 GMT 소재(100, 200)를 위치한 후 성형 가공하면, 고강성 열가소성 보강재(200)의 외부층을 구성하는 열가소성 복합재(210, 230)가 GMT 소재(100, 300)와의 결합력을 증가시켜 박리 현상을 방지한다. 다시 말해, 열가소성 복합재(210, 230)가 직조된 보강부재(220)의 내부로 함침되어 보강부재(200)와 결합하고, 이와 동시에 열가소성 복합재(210, 230)는 열가소성 수지나 유리섬유가 함유된 열가소성 수지로 구성되므로 열가소성인 GMT 소재(100, 300)와는 단단하게 결합이 이루어지므로 전체적으로 보강재(200)와 GMT 소재(100, 300)가 단단하게 결합한다.When the GMT
바람직하게, 열가소성 수지로는 폴리프로필렌이 적용될 수 있다.Preferably, polypropylene may be applied as the thermoplastic resin.
도 1의 실시예와 달리 고강성 열가소성 보강재(200)는 GMT 소재(100, 300)에 대해 일면만 접합할 수 있다. 도 3은 본 발명의 다른 고강성 열가소성 보강재를 적용한 제품을 나타내는 실시예이다.Unlike the embodiment of FIG. 1, the high stiffness
도 3을 참조하면, 다수의 적층된 GMT 소재(100. 110, 120) 중 최하부에 위치 한 GMT 소재(120)의 이면에 본 발명의 고강성 열가소성 보강재(200')가 접합한다.Referring to FIG. 3, the highly rigid
도 4는 본 발명에 따른 고강성 열가소성 보강재의 다른 예를 나타내는 단면도이다.4 is a cross-sectional view showing another example of a high rigid thermoplastic reinforcing material according to the present invention.
도 4를 참조하면, 직조(woven) 보강부재(220)의 표면, 즉 GMT 소재(120)와 대향하는 면에 열가소성 수지 또는 유리섬유를 함유한 열가소성 수지로 이루어진 열가소성 복합재(230)가 함침된다.Referring to FIG. 4, a thermoplastic
이와 같이, 본 발명의 보강부재는 GMT 소재와의 결합을 위해 결합면에만 열가소성 복합재를 함침해도 무방하다.As such, the reinforcing member of the present invention may be impregnated with a thermoplastic composite only on the bonding surface for bonding with the GMT material.
[표 1]은 본 발명에 따른 고강성 열가소성 보강재와 종래의 보강재의 물성을 비교한 결과를 나타낸다.Table 1 shows the results of comparing the properties of the high stiffness thermoplastic reinforcing material according to the present invention and the conventional reinforcing material.
즉, [표 1]과 같이 본 발명에 따른 보강재는 인장강도와 충격강도가 각각 50% 정도 증가함을 알 수 있다.That is, as shown in [Table 1], the reinforcing material according to the present invention can be seen that the tensile strength and the impact strength are increased by about 50%, respectively.
[표 2]는 본 발명의 고강성 열가소성 보강재를 적용한 자동차용 백 빔(back beam)에 대한 충돌 성능을 비교한 결과를 나타낸다.Table 2 shows the result of comparing the collision performance for the back beam for automobiles to which the high rigidity thermoplastic reinforcement of the present invention is applied.
빔 중량: 4.8㎏ 기준Beam weight: 4.8 kg
충돌 속도: 10kphCollision Speed: 10kph
시험방법: IIHS(미국 고속도로안정보험협회) 풀 배리어(full barrier) 기준Test Method: IIHS Full Barrier Standard
[표 2]로부터 대차 성능이 약 30% 정도 향상되었음을 알 수 있다.From Table 2, it can be seen that the balance performance is improved by about 30%.
도 5는 본 발명의 고강성 열가소성 보강재를 제조하는 한 공정을 나타내는 설명도이다. 이 예에서는 두 층의 직조 보강부재와 이들의 표면과 이면에 각각 적층 함침된 폴리프로필렌 복합재로 이루어진 보강재의 제조공정을 보여준다.5 is an explanatory view showing one step of producing the high rigid thermoplastic reinforcing material of the present invention. This example shows the manufacturing process of a reinforcement consisting of two layers of woven reinforcement members and polypropylene composites impregnated on their front and back surfaces, respectively.
압출기(extruder; 10)에 열가소성 재료인 폴리프로필렌(1)과 첨가제(2)를 투입하고 T-다이(20)를 통하여 시트 상으로 압출하는데, 롤(3a, 3b)로부터 유리섬유 직조물이나 폴리에스테르 직물과 같은 직조 보강부재가 공급되어 폴리프로필렌 복합재와 적층구조를 이룬다. Polypropylene (1) and additives (2), which are thermoplastic materials, are introduced into an extruder (10) and extruded onto a sheet through a T-die (20), which is a glass fiber woven or polyester from rolls (3a, 3b). Woven reinforcement members such as fabrics are supplied to form a laminated structure with the polypropylene composite.
이어, 캘린더(calender) 또는 DBP(Double Belt Press)(30)에서 성형 가공하고 절단장치(40)에서 적절한 형상으로 절단한 후, 스택장치(50)에 쌓는다.Subsequently, a molding process is performed in a calender or double belt press (DPP) 30, cut into an appropriate shape in the cutting device 40, and then stacked on the stacking device 50.
도 6은 본 발명의 고강성 열가소성 보강재를 제조하는 다른 공정을 나타내는 설명도이다.6 is an explanatory view showing another step of producing the high rigid thermoplastic reinforcing material of the present invention.
압출기(extruder; 10)에 열가소성 재료인 폴리프로필렌(1)과 첨가제(2) 및 유리섬유(3)를 투입하고 T-다이(20)를 통하여 시트 상으로 압출하는데, 롤(3a, 3b)로부터 유리섬유 직조물이나 폴리에스테르 직물과 같은 직조 보강부재가 공급되어 폴리프로필렌 복합재와 적층구조를 이룬다. In the extruder 10, polypropylene (1), an additive (2), and glass fiber (3), which are thermoplastic materials, are charged and extruded onto the sheet through the T-die 20, from the rolls 3a and 3b. Woven reinforcement members such as fiberglass woven fabrics or polyester fabrics are supplied to form a laminated structure with the polypropylene composite.
이어, 캘린더(calender) 또는 DBP(Double Belt Press)(30)에서 성형 가공하고 절단장치(40)에서 적절한 형상으로 절단한 후, 스택장치(50)에 쌓는다.Subsequently, a molding process is performed in a calender or double belt press (DPP) 30, cut into an appropriate shape in the cutting device 40, and then stacked on the stacking device 50.
도 7은 본 발명의 고강성 열가소성 보강재를 제조하는 또 다른 공정을 나타내는 설명도이다.7 is an explanatory view showing still another step of producing a high rigid thermoplastic reinforcing material of the present invention.
압출기(extruder; 10)에 촙드(chopped) 유리섬유와 폴리프로필렌으로 이루어진 팰릿(pallet)을 투입하고 T-다이(20)를 통하여 시트 상으로 압출하는데, 롤(3a, 3b)로부터 유리섬유 직조물이나 폴리에스테르 직물과 같은 직조 보강부재가 공급되어 폴리프로필렌 복합재와 적층구조를 이룬다. A pellet made of chopped glass fibers and polypropylene is introduced into an extruder 10 and extruded onto a sheet through a T-die 20, from which the fiberglass fabric or the rolls 3a and 3b Woven reinforcement members such as polyester fabrics are supplied to form a laminated structure with the polypropylene composite.
이어, 캘린더(calender) 또는 DBP(Double Belt Press)(30)에서 성형 가공하고 절단장치(40)에서 적절한 형상으로 절단한 후, 스택장치(50)에 쌓는다.Subsequently, a molding process is performed in a calender or double belt press (DPP) 30, cut into an appropriate shape in the cutting device 40, and then stacked on the stacking device 50.
이상에서는 본 발명의 일 실시예를 중심으로 설명하였지만, 당업자의 수준에서 다양한 변경이 가능하다. 따라서, 본 발명의 권리범위는 상기한 실시예에 한정되어서는 안 되며 이하에 기재하는 특허청구범위에 의해 해석되어야 한다.Although the above has been described with reference to one embodiment of the present invention, various modifications are possible at the level of those skilled in the art. Therefore, the scope of the present invention should not be limited to the above embodiments but should be interpreted by the claims described below.
본 발명에 따르면 유동성을 갖는 고강성 열가소성 복합재를 제공함으로써 제품 강도와 강성을 높이는 동시에 성형시 박리 현상을 없앨 수 있다.According to the present invention, by providing a highly rigid thermoplastic composite having fluidity, it is possible to increase the product strength and rigidity and at the same time eliminate the peeling phenomenon during molding.
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
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| KR101327634B1 (en) * | 2010-11-12 | 2013-11-12 | (주)엘지하우시스 | Manufacturing Method of Thermoplastic Long Fiber Composites |
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| KR101327634B1 (en) * | 2010-11-12 | 2013-11-12 | (주)엘지하우시스 | Manufacturing Method of Thermoplastic Long Fiber Composites |
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| KR101396819B1 (en) * | 2012-05-14 | 2014-05-21 | 한화엘앤씨 주식회사 | Ultra thin type woven thermoplastics complex materials with reinforced insulation surface of substrates |
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| CN113540653A (en) * | 2018-09-20 | 2021-10-22 | 乐金华奥斯株式会社 | Lower protection plate for battery module for electric vehicle |
| KR102209652B1 (en) * | 2020-07-23 | 2021-02-01 | (주)에코파워텍 | Manufacturing method for sink prevention warm insulation using purification ash and warm insulation manufactured thereof |
| WO2025036469A1 (en) * | 2023-08-16 | 2025-02-20 | 宁波信泰机械有限公司 | Automobile door outer panel |
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