TWM479216U - Multi-layer composite material - Google Patents

Multi-layer composite material Download PDF

Info

Publication number
TWM479216U
TWM479216U TW102214385U TW102214385U TWM479216U TW M479216 U TWM479216 U TW M479216U TW 102214385 U TW102214385 U TW 102214385U TW 102214385 U TW102214385 U TW 102214385U TW M479216 U TWM479216 U TW M479216U
Authority
TW
Taiwan
Prior art keywords
thermosetting resin
resin matrix
layer
cured
multilayer composite
Prior art date
Application number
TW102214385U
Other languages
Chinese (zh)
Inventor
Cheng-Sheng Chen
Original Assignee
Cheng-Sheng Chen
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 Cheng-Sheng Chen filed Critical Cheng-Sheng Chen
Priority to TW102214385U priority Critical patent/TWM479216U/en
Publication of TWM479216U publication Critical patent/TWM479216U/en
Priority to CN201420425129.2U priority patent/CN204109491U/en

Links

Landscapes

  • Laminated Bodies (AREA)

Description

多層複合材料Multi-layer composite

本新型是有關於一種多層複合材料,特別是指一種基礎層包括熱固性樹脂基質、透明可撓性基材及編織纖維的多層複合材料。The present invention relates to a multilayer composite material, and more particularly to a multilayer composite material comprising a base layer comprising a thermosetting resin matrix, a transparent flexible substrate, and a woven fiber.

現今電子產品的設計趨勢強調輕薄化,且朝攜帶型產品發展;以往採用射出成型的電子產品塑膠外殼,考量塑膠外殼之厚度小於2mm時可能因為強度不足等問題而容易破裂損壞因此不宜再薄型化,因此,近年來積極尋求其他更適當的材料,例如使用力學性質優良且外觀良好的鋁鎂合金或編織纖維複合材料等材料來製備電子產品的外殼。Today's electronic product design trend emphasizes lightness and thinness, and it is moving toward portable products. In the past, the plastic case of injection molded electronic products, when considering the thickness of the plastic case less than 2mm, may be easily broken and damaged due to insufficient strength, so it is not suitable for thinning. Therefore, in recent years, other more suitable materials have been actively sought, for example, an aluminum-magnesium alloy or a woven fiber composite material having excellent mechanical properties and good appearance to prepare an outer casing of an electronic product.

用於製備外殼的碳纖維複合材料的製程主要是將編織纖維含浸熱固性樹脂形成一預浸漬物後,再將該預浸漬物進行熱壓成型,形成一具有編織紋路的編織纖維複合材料,其中該編織纖維可例如碳纖維等。但預浸漬物在熱壓的過程中,可能因為存在未固化的熱固性樹脂滑動,導致原本整齊交織的編織紋路偏移,雖然不影響成品的結構強韌程度,但其外觀不佳,對電子品的外形及美觀程度影響甚鉅。The carbon fiber composite material used for preparing the outer casing is mainly prepared by impregnating the woven fiber with a thermosetting resin to form a prepreg, and then hot pressing the prepreg to form a woven fiber composite material having a woven texture, wherein the weaving The fibers may be, for example, carbon fibers or the like. However, during the hot pressing process, the uncured thermosetting resin may slide due to the presence of the uncured thermosetting resin, which may cause the texture of the finished product to be offset. Although it does not affect the structural toughness of the finished product, its appearance is not good, and the electronic product is not good. The shape and aesthetics of the impact are enormous.

因此,為解決前述問題並提升編織纖維複合材料的品質,必須提出表面品質優良且良率更高的多層複合材料。Therefore, in order to solve the aforementioned problems and improve the quality of the woven fiber composite material, it is necessary to propose a multilayer composite material having excellent surface quality and higher yield.

因此,本新型之目的,即在提供一種外觀良好的多層複合材料。Therefore, the object of the present invention is to provide a multilayer composite material having a good appearance.

於是本新型多層複合材料,包含:一基礎層,包括:一固化的第一熱固性樹脂基質,一透明可撓性片材,及一夾置於該固化的第一熱固性樹脂基質及該透明可撓性片材中間的第一編織纖維,是先使該透明可撓性片材與該第一編織纖維熔融接合,再使該固化的第一熱固性樹脂基質與該第一編織纖維結合且穿透該第一編織纖維進而與該透明可撓性片材接觸。The novel multilayer composite material comprises: a base layer comprising: a cured first thermosetting resin matrix, a transparent flexible sheet, and a first thermosetting resin matrix sandwiched between the curing and the transparent flexible The first woven fabric in the middle of the sheet is obtained by first fusion-bonding the transparent flexible sheet with the first woven fabric, and then bonding the cured first thermosetting resin matrix to the first woven fabric and penetrating the same The first woven fabric is in turn in contact with the transparent flexible sheet.

本新型之功效在於該多層複合材料除保有多層複合材料的良好機械性質外,沒有編織紋路偏移的問題,外觀良好,適用於作為各類電子產品之外殼。The utility model has the advantages that the multi-layer composite material has no problem of woven grain deviation except for maintaining good mechanical properties of the multilayer composite material, and has good appearance, and is suitable for being used as an outer casing of various electronic products.

1‧‧‧基礎層1‧‧‧Basic layer

11‧‧‧第一熱固性樹脂基質11‧‧‧First thermosetting resin matrix

12‧‧‧透明可撓性片材12‧‧‧Transparent flexible sheet

13‧‧‧第一編織纖維13‧‧‧First woven fiber

131‧‧‧第一表面131‧‧‧ first surface

132‧‧‧第二表面132‧‧‧ second surface

2‧‧‧中間層2‧‧‧Intermediate

21‧‧‧第二彈性膜21‧‧‧Second elastic film

211‧‧‧接觸面211‧‧‧Contact surface

22‧‧‧充填膜22‧‧‧ Filling film

23‧‧‧第二熱固性樹脂基質23‧‧‧Second thermosetting resin matrix

24‧‧‧第二編織纖維24‧‧‧Second woven fiber

3‧‧‧熱塑性材料層3‧‧‧ thermoplastic layer

本新型之其他的特徵及功效,將於參照圖式的實施方式中清楚地呈現,其中:圖1是一流程示意圖,說明本新型多層複合材料的第一較佳實施例及其製備方法; 圖2是剖面圖,說明本新型多層複合材料的第二較佳實施例;圖3是一剖面圖,說明本新型多層複合材料的第三較佳實施例;圖4是一流程示意圖,說明本新型多層複合材料的第四較佳實施例及其製備方法。Other features and effects of the present invention will be apparent from the following description of the drawings, wherein: FIG. 1 is a flow diagram illustrating a first preferred embodiment of the novel multilayer composite and a method of making the same; Figure 2 is a cross-sectional view showing a second preferred embodiment of the novel multilayer composite material; Figure 3 is a cross-sectional view showing a third preferred embodiment of the novel multilayer composite material; Figure 4 is a schematic flow chart showing the present invention A fourth preferred embodiment of a novel multilayer composite and a method of making same.

在本新型被詳細描述之前,應當注意在以下的說明內容中,類似的元件是以相同的編號來表示。Before the present invention is described in detail, it should be noted that in the following description, similar elements are denoted by the same reference numerals.

參閱圖1,本新型多層複合材料的第一較佳實施例包含一基礎層1,包括:一固化的第一熱固性樹脂基質11,一透明可撓性片材12,及一夾置於該固化的第一熱固性樹脂基質11及該透明可撓性片材12中間的第一編織纖維13。該多層複合材料的製備方法是先使該透明可撓性片材12與該第一編織纖維13熔融接合,再使該固化的第一熱固性樹脂基質11與該第一編織纖維13結合且穿透該第一編織纖維13進而與該透明可撓性片材12接觸。其中熔融接合採用一般方法即可,可例如但不限於各式熱壓接合方法。較佳地,該透明可撓性片材12的厚度是0.15mm至0.20mm,該第一編織纖維13的厚度為0.25mm。Referring to Figure 1, a first preferred embodiment of the novel multilayer composite comprises a base layer 1 comprising: a cured first thermosetting resin matrix 11, a transparent flexible sheet 12, and a sandwiched in the curing The first thermosetting resin matrix 11 and the first woven fabric 13 in the middle of the transparent flexible sheet 12. The multilayer composite material is prepared by first fusion-bonding the transparent flexible sheet 12 with the first woven fabric 13, and then bonding and curing the cured first thermosetting resin matrix 11 to the first woven fabric 13. The first woven fabric 13 is in turn in contact with the transparent flexible sheet 12. The fusion bonding may be carried out by a general method, and may be, for example but not limited to, various types of thermocompression bonding methods. Preferably, the transparent flexible sheet 12 has a thickness of 0.15 mm to 0.20 mm, and the first woven fabric 13 has a thickness of 0.25 mm.

當第一較佳實施例之多層複合材料應用於製作電子產品之外殼時,建議以該透明可撓性片材12為外面,第一熱固性樹脂基質11為內面,即可以使該第一編織纖維13的織紋通過該透明可撓性片材12被看見,並有助於提升 該電子產品的美觀程度。較佳地,該第一編織纖維為一具有編織紋路的織物(經Weave或Fabric),而使本新型該多層複合材料能夠同時具良好的機械性質與美觀的功效。When the multilayer composite material of the first preferred embodiment is applied to the outer casing of the electronic product, it is recommended that the transparent flexible sheet 12 be the outer surface, and the first thermosetting resin substrate 11 be the inner surface, that is, the first weaving can be made. The texture of the fibers 13 is seen through the transparent flexible sheet 12 and contributes to the lifting The aesthetics of the electronic product. Preferably, the first woven fabric is a woven fabric (via Weave or Fabric), so that the multilayer composite of the present invention can have both good mechanical properties and aesthetic effects.

較佳地,該透明可撓性片材12的熔點是低於該第一編織纖維13的熔點,使該透明可撓性片材12與該第一編織纖維13於熔融接合時不致損傷或導致該第一編織纖維13形變。Preferably, the transparent flexible sheet 12 has a melting point lower than the melting point of the first woven fiber 13, so that the transparent flexible sheet 12 and the first woven fiber 13 are not damaged or caused by fusion bonding. The first woven fabric 13 is deformed.

該透明可撓性片材12並沒有特別的限制,只要能與該第一編織纖維13熔融接合即可。較佳地,該透明可撓性片材12是由一第一彈性材料所形成;更佳地,該第一彈性材料是選自於肖氏硬度(Shore hardness)為90A以上的熱塑性彈性體(Thermoplastic Elastomer,簡稱TPE)、人造橡膠與尼龍(Nylon)之一組合,或是聚醚醯胺嵌段(polyether block amide)。其中,熱塑性彈性體包括苯乙烯系熱塑性彈性體、聚烯系熱塑性彈性體、聚氨酯系熱塑性彈性體、聚酯系熱塑性彈性體、聚醯胺系熱塑性彈性體。The transparent flexible sheet 12 is not particularly limited as long as it can be fusion-bonded to the first woven fibers 13. Preferably, the transparent flexible sheet 12 is formed of a first elastic material; more preferably, the first elastic material is selected from a thermoplastic elastomer having a Shore hardness of 90 A or more ( Thermoplastic Elastomer (TPE), a combination of elastomer and nylon (Nylon), or a polyether block amide. Among them, the thermoplastic elastomer includes a styrene-based thermoplastic elastomer, a polyolefin-based thermoplastic elastomer, a polyurethane-based thermoplastic elastomer, a polyester-based thermoplastic elastomer, and a polyamide-based thermoplastic elastomer.

該第一編織纖維13的種類並沒有特別限制,較佳地為強化纖維。強化纖維例如:鋁、黃銅、不鏽鋼等金屬纖維;聚丙烯腈、嫘縈系等碳纖維;石墨纖維、玻璃等絕緣性纖維;芳香族聚醯胺、聚酯、丙烯酸、耐綸、聚乙烯等有機纖維;以及碳化矽、氮化矽(silicon nitride)等無機纖維。更佳地,該第一編織纖維13為碳纖維。The kind of the first woven fiber 13 is not particularly limited, and is preferably a reinforcing fiber. Reinforcing fibers such as: metal fibers such as aluminum, brass, and stainless steel; carbon fibers such as polyacrylonitrile and lanthanum; insulating fibers such as graphite fibers and glass; aromatic polyamides, polyesters, acrylics, nylons, polyethylenes, etc. Organic fibers; and inorganic fibers such as tantalum carbide and silicon nitride. More preferably, the first woven fabric 13 is a carbon fiber.

該第一熱固性樹脂基質11的種類可例如但不限於環氧樹脂及酚醛樹脂,其中當該第一熱固性樹脂基質11 為酚醛樹脂時,由於酚醛樹脂的耐火等級較高,所製得的多層複合材料特別適用於作為建材或家具。較佳地,該第一熱固性樹脂基質11的種類是環氧樹脂。The kind of the first thermosetting resin matrix 11 may be, for example but not limited to, an epoxy resin and a phenol resin, wherein when the first thermosetting resin matrix 11 In the case of a phenolic resin, since the phenolic resin has a high fire resistance rating, the obtained multilayer composite material is particularly suitable for use as a building material or furniture. Preferably, the type of the first thermosetting resin matrix 11 is an epoxy resin.

參閱圖2。本新型多層複合材料的第二較佳實施例包含一基礎層1及一中間層2。將該中間層2疊置於該基礎層1的可固化的第一熱固性樹脂基質11上,該中間層2包括一由第二彈性材料形成的第二彈性膜21,使該中間層2與該可固化的第一熱固性樹脂基質11接觸;對疊置的該中間層2及該基礎層1施予熱和壓力至固化,使該中間層2與該第一熱固性樹脂基質11黏合。See Figure 2. A second preferred embodiment of the novel multilayer composite material comprises a base layer 1 and an intermediate layer 2. Laminating the intermediate layer 2 on the curable first thermosetting resin substrate 11 of the base layer 1, the intermediate layer 2 comprising a second elastic film 21 formed of a second elastic material, the intermediate layer 2 being The curable first thermosetting resin matrix 11 is contacted; the intermediate layer 2 and the base layer 1 which are stacked are subjected to heat and pressure to cure, and the intermediate layer 2 is bonded to the first thermosetting resin matrix 11.

該第二彈性材料的說明及變化態樣是與前述形成該該透明可撓性片材12的第一彈性材料相同,在此不再贅述。The description and variations of the second elastic material are the same as those of the first elastic material forming the transparent flexible sheet 12, and will not be described herein.

該中間層2的厚度是依據後續用途及需求進行調整,以增加強度或吸震效果。較佳地,該中間層2的厚度是0.8mm至2.5mm;更佳地是0.8mm至1.3mm。The thickness of the intermediate layer 2 is adjusted according to the subsequent use and needs to increase the strength or shock absorption effect. Preferably, the intermediate layer 2 has a thickness of from 0.8 mm to 2.5 mm; more preferably from 0.8 mm to 1.3 mm.

參閱圖3。本新型多層複合材料的第三較佳實施例包含一基礎層1、一中間層2,及一射出成型於該中間層2之第二彈性膜21上的熱塑性材料3。See Figure 3. A third preferred embodiment of the novel multilayer composite material comprises a base layer 1, an intermediate layer 2, and a thermoplastic material 3 which is formed on the second elastic film 21 of the intermediate layer 2.

熱塑性材料層3的製作說明如下:射出成型製程中,當該熱塑性材料射出時,該熱塑性材料是具有一升高溫度,且該升高溫度是足以熔化該第二彈性膜21的接觸面211,因此,在射出成型的過程中,當該熱塑性材料與該接觸面211接觸時,該熱塑性材料與該接觸面211會產生 融熔接合。要特別說明的是,只有該接觸面211會在射出成形製程中被該熱塑性材料熔融,該第二彈性膜21的形狀仍維持完整且厚度均勻。此外,亦可以是先進行射出成型形成該熱塑性材料層3,再採用習知方法如透過黏膠或雷射光加熱等方法使該熱塑性材料層3與該接觸面211結合,使該熱塑性材料層3結合於該第二彈性膜21上。The fabrication of the thermoplastic material layer 3 is as follows: in the injection molding process, when the thermoplastic material is ejected, the thermoplastic material has an elevated temperature, and the elevated temperature is sufficient to melt the contact surface 211 of the second elastic film 21, Therefore, in the process of injection molding, when the thermoplastic material is in contact with the contact surface 211, the thermoplastic material and the contact surface 211 are generated. Fusion bonding. It is to be noted that only the contact surface 211 is melted by the thermoplastic material in the injection molding process, and the shape of the second elastic film 21 remains intact and uniform in thickness. In addition, the thermoplastic material layer 3 may be formed by injection molding, and the thermoplastic material layer 3 may be bonded to the contact surface 211 by a conventional method such as adhesion through a viscose or laser light to make the thermoplastic material layer 3 Bonded to the second elastic film 21.

較佳地,該第二彈性膜21的厚度是大於等於0.15mm,使該熱塑性材料層3熱塑成型於該第二彈性膜21的接觸面211時,該第二彈性膜21不至於因受熱收縮(shrink),或僅會發生極微小的收縮;更佳地,該第二彈性膜21的厚度是0.15至0.3mm。Preferably, the thickness of the second elastic film 21 is 0.15 mm or more. When the thermoplastic material layer 3 is thermoplastically molded on the contact surface 211 of the second elastic film 21, the second elastic film 21 is not heated. Shrink, or only a slight shrinkage occurs; more preferably, the thickness of the second elastic film 21 is 0.15 to 0.3 mm.

較佳地,該熱塑性材料層3是至少一種選自於由下列熱塑性材料所構成之群組:尼龍6、尼龍66、熱塑性聚氨酯、聚碳酸酯(Polycarbonate,簡稱PC)、丙烯睛-丁二烯-苯乙烯(Acrylonitrile Butadiene Styrene,簡稱ABS)、聚碳酸酯與丙烯睛-丁二烯-苯乙烯的混合物,及聚醚醯胺嵌段。Preferably, the thermoplastic material layer 3 is at least one selected from the group consisting of nylon 6, nylon 66, thermoplastic polyurethane, polycarbonate (PC), acrylonitrile butadiene. Acrylonitrile Butadiene Styrene (ABS), a mixture of polycarbonate and acrylonitrile butadiene styrene, and a polyether guanamine block.

較佳地,該熱塑性材料層3是一經圖案化的熱塑性材料層。該熱塑性材料層3經圖案化後可例如但不限於形成一個或一個以上的功能性組件;當該多層複合材料應用各式電子產品外殼時,透過該功能性組件可利於組裝及完整密合。Preferably, the layer of thermoplastic material 3 is a patterned layer of thermoplastic material. The thermoplastic material layer 3 can be patterned, for example but not limited to, to form one or more functional components; when the multilayer composite material is applied to various electronic product housings, the functional components can facilitate assembly and complete adhesion.

參閱圖4。本新型多層複合材料的第四較佳實施例包含一基礎層1及一中間層2。與第二較佳實施例不同的 地方在於:該中間層2還包含一充填膜22、一固化的第二熱固性樹脂基質23,及一第二編織纖維24。See Figure 4. A fourth preferred embodiment of the novel multilayer composite material comprises a base layer 1 and an intermediate layer 2. Different from the second preferred embodiment The intermediate layer 2 further comprises a filling film 22, a cured second thermosetting resin matrix 23, and a second woven fiber 24.

第四較佳實施例的具體作法是:首先將該第一編織纖維13與該透明可撓性片材12重疊後施予熱和壓力,使該透明可撓性片材12熔融接合至該第一編織纖維13的第一表面131,再使該第一編織纖維13、該固化的第一熱固性樹脂基質11、該充填膜22、該固化的第二熱固性樹脂基質23、該第二編織纖維24與該第二彈性膜21是依序疊合且透過施予熱和壓力黏合成疊。該第四較佳實施例可以視後續用途及需求,選擇性地設置一熱塑性材料層3,具體作法與前述相同,將一熱塑性材料射出成形於該中間層2的第二彈性膜21上,即形成該熱塑性材料層3,在此不再贅述。A specific embodiment of the fourth preferred embodiment is that first, the first woven fiber 13 is overlapped with the transparent flexible sheet 12, and heat and pressure are applied to fuse the transparent flexible sheet 12 to the first The first surface 131 of the woven fiber 13 and the first woven fiber 13, the cured first thermosetting resin substrate 11, the filling film 22, the cured second thermosetting resin matrix 23, and the second woven fiber 24 are The second elastic film 21 is sequentially laminated and bonded to the heat and pressure. The fourth preferred embodiment can selectively provide a layer of thermoplastic material 3 according to the subsequent use and needs. In the same manner as described above, a thermoplastic material is injection molded on the second elastic film 21 of the intermediate layer 2, that is, The layer of thermoplastic material 3 is formed and will not be described again.

該充填膜22的功能在於提供緩衝或吸震,其材料可例如但不限於熱塑性彈性體,或是聚醚醯胺嵌段,於製備時亦可以預先夾置並固定於該固化的第一熱固性樹脂基質11及該固化的第二熱固性樹脂基質23中間。The function of the filling film 22 is to provide buffering or shock absorption, and the material thereof may be, for example, but not limited to, a thermoplastic elastomer or a polyether amide block, which may be preliminarily sandwiched and fixed to the cured first thermosetting resin during preparation. The matrix 11 and the cured second thermosetting resin matrix 23 are intermediate.

該第二熱固性樹脂基質23的說明及變化態樣是與前述第一熱固性樹脂基質11相同,在此不再贅述。該第二編織纖維24的說明及變化態樣是與前述第一編織纖維13相同,在此不再贅述。The description and variations of the second thermosetting resin matrix 23 are the same as those of the first thermosetting resin matrix 11, and will not be described herein. The description and variations of the second woven fabric 24 are the same as those of the first woven fabric 13, and will not be described herein.

綜上所述,本新型製備多層複合材料的方法透過施予熱和壓力使一第一編織纖維13夾置於一固化的第一熱固性樹脂基質11及一透明可撓性片材12中間,所製得 的多層複合材料表面外觀良好,編織纖維的織紋不易偏移,且該多層複合材料保有優良的力學性質,適用於作為電子產品的外殼、家具、建材,及汽車的引擎蓋、葉子板或保險桿等,故確實能達成本新型之目的。In summary, the novel method for preparing a multilayer composite material is formed by sandwiching a first woven fiber 13 between a cured first thermosetting resin substrate 11 and a transparent flexible sheet 12 by applying heat and pressure. Got The multi-layer composite material has a good surface appearance, the texture of the woven fiber is not easily offset, and the multi-layer composite material retains excellent mechanical properties, and is suitable for use as an outer casing of an electronic product, furniture, building materials, and an automobile hood, fender or insurance. Rods, etc., can indeed achieve the purpose of this new type.

惟以上所述者,僅為本新型之較佳實施例而已,當不能以此限定本新型實施之範圍,即大凡依本新型申請專利範圍及專利說明書內容所作之簡單的等效變化與修飾,皆仍屬本新型專利涵蓋之範圍內。However, the above is only a preferred embodiment of the present invention, and is not intended to limit the scope of the present invention, that is, the simple equivalent changes and modifications made in accordance with the scope of the present patent application and the contents of the patent specification, All remain within the scope of this new patent.

1‧‧‧基礎層1‧‧‧Basic layer

11‧‧‧第一熱固性樹脂基質11‧‧‧First thermosetting resin matrix

12‧‧‧透明可撓性片材12‧‧‧Transparent flexible sheet

13‧‧‧第一編織纖維13‧‧‧First woven fiber

Claims (5)

一種多層複合材料,包含:一基礎層,包括:一固化的第一熱固性樹脂基質,一透明可撓性片材,及一夾置於該固化的第一熱固性樹脂基質及該透明可撓性片材中間的第一編織纖維,是先使該透明可撓性片材與該第一編織纖維熔融接合,再使該固化的第一熱固性樹脂基質與該第一編織纖維結合且穿透該第一編織纖維進而與該透明可撓性片材接觸。A multilayer composite comprising: a base layer comprising: a cured first thermosetting resin matrix, a transparent flexible sheet, and a first thermosetting resin matrix sandwiched between the curing and the transparent flexible sheet The first woven fiber in the middle of the material is obtained by first fusion-bonding the transparent flexible sheet with the first woven fiber, and then bonding the cured first thermosetting resin matrix to the first woven fiber and penetrating the first The woven fibers are in turn in contact with the transparent flexible sheet. 如請求項1所述的多層複合材料,還包含:一中間層,與該固化的第一熱固性樹脂基質黏合且包括一由第二彈性材料形成之第二彈性膜;及一結合於該中間層之第二彈性膜上的熱塑性材料層。The multilayer composite material of claim 1, further comprising: an intermediate layer bonded to the cured first thermosetting resin matrix and comprising a second elastic film formed of a second elastic material; and a bonding to the intermediate layer a layer of thermoplastic material on the second elastic film. 如請求項2所述的多層複合材料,其中,該熱塑性材料層是一經圖案化的熱塑性材料層。The multilayer composite of claim 2 wherein the thermoplastic layer is a patterned layer of thermoplastic material. 如請求項2所述的多層複合材料,其中,該中間層還包含一充填膜、一固化的第二熱固性樹脂基質及一第二編織纖維,該第一編織纖維、該固化的第一熱固性樹脂基質、該充填膜、該固化的第二熱固性樹脂基質、該第二編織纖維與該第二彈性膜是依序疊合且透過施予熱和壓力黏合成疊。The multilayer composite material of claim 2, wherein the intermediate layer further comprises a filling film, a cured second thermosetting resin matrix, and a second woven fiber, the first woven fiber, the cured first thermosetting resin The substrate, the filling film, the cured second thermosetting resin matrix, the second woven fiber and the second elastic film are sequentially laminated and bonded to each other by applying heat and pressure. 如請求項2所述的多層複合材料,其中,該第二彈性材料是選自於肖氏硬度為90A以上的熱塑性彈性體、人造橡膠與尼龍之一組合,或是聚醚醯胺嵌段。The multilayer composite material according to claim 2, wherein the second elastic material is selected from the group consisting of a thermoplastic elastomer having a Shore hardness of 90 A or more, a combination of an elastomer and a nylon, or a polyether amide block.
TW102214385U 2013-07-31 2013-07-31 Multi-layer composite material TWM479216U (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
TW102214385U TWM479216U (en) 2013-07-31 2013-07-31 Multi-layer composite material
CN201420425129.2U CN204109491U (en) 2013-07-31 2014-07-30 Multilayer composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW102214385U TWM479216U (en) 2013-07-31 2013-07-31 Multi-layer composite material

Publications (1)

Publication Number Publication Date
TWM479216U true TWM479216U (en) 2014-06-01

Family

ID=51394550

Family Applications (1)

Application Number Title Priority Date Filing Date
TW102214385U TWM479216U (en) 2013-07-31 2013-07-31 Multi-layer composite material

Country Status (2)

Country Link
CN (1) CN204109491U (en)
TW (1) TWM479216U (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3473129A4 (en) * 2016-06-16 2020-02-19 Carimax Corporation Multilayer sheet comprising fabric and resin, travel bag case made thereferom, and apparatus for manufacturing same
CN107839140B (en) * 2016-09-19 2019-12-17 简单绿能股份有限公司 manufacturing process of foaming pad with multiple lines

Also Published As

Publication number Publication date
CN204109491U (en) 2015-01-21

Similar Documents

Publication Publication Date Title
US8562886B2 (en) Composite laminate having an improved cosmetic surface and method of making same
CN101662899A (en) Electronic product outer shell and manufacturing method thereof
JP2008514458A5 (en)
PL1727669T3 (en) Composite part
WO2016174989A1 (en) Decorative sheet, method for manufacturing molded article, and molded article
JP2007331369A (en) Fiber-reinforced plastic molded object and its manufacturing method
JP7153253B2 (en) fiber reinforced plastic molding
TWI527693B (en) Multi - layer composite material and its manufacturing method
CN107696628B (en) Composite material of different material lamination and products thereof
WO2018015757A1 (en) A composite sheet material and a method of manufacture thereof
TWM479216U (en) Multi-layer composite material
US20170043613A1 (en) Composite body made of fibre-composite material and a decorative element
JP3751023B2 (en) Laminated members with different elasticity in the edge area
KR102067091B1 (en) Manufacturing method of back cover for mobile communication device
US20160193820A1 (en) Coloured carbon-fibre composite materials
US20130052417A1 (en) Rigid reinforced composite material and manufacturing method thereof
JP2021084422A (en) Wooden decorative board, molded article having wooden decorative board, and method of manufacturing molded article
US20130330991A1 (en) Composite material and method for preparing the same
US20160096317A1 (en) Method of making a molded article and molded article
TWI580576B (en) Heterogeneous composites and products thereof
US11110691B2 (en) Composite product
WO2006083740A3 (en) Novel thick laminate fabrication method
WO2019155013A8 (en) Method for manufacturing a prepreg made of a composite material
WO2013099993A1 (en) Injection molded article using prepreg, and production method for injection molded article
TWM367806U (en) Combined structure on surface of composite material