JP2015063019A - Thermoplastic laminate sheet and production method of the same - Google Patents
Thermoplastic laminate sheet and production method of the same Download PDFInfo
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- JP2015063019A JP2015063019A JP2013196847A JP2013196847A JP2015063019A JP 2015063019 A JP2015063019 A JP 2015063019A JP 2013196847 A JP2013196847 A JP 2013196847A JP 2013196847 A JP2013196847 A JP 2013196847A JP 2015063019 A JP2015063019 A JP 2015063019A
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- 229920001169 thermoplastic Polymers 0.000 title claims abstract description 22
- 239000004416 thermosoftening plastic Substances 0.000 title claims abstract description 22
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000010410 layer Substances 0.000 claims abstract description 70
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 31
- 239000004917 carbon fiber Substances 0.000 claims abstract description 30
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 29
- 239000004744 fabric Substances 0.000 claims abstract description 25
- -1 polypropylene Polymers 0.000 claims abstract description 17
- 239000012790 adhesive layer Substances 0.000 claims abstract description 16
- 239000004743 Polypropylene Substances 0.000 claims abstract description 15
- 238000001816 cooling Methods 0.000 claims abstract description 14
- 229920001155 polypropylene Polymers 0.000 claims abstract description 14
- 239000002313 adhesive film Substances 0.000 claims abstract description 11
- 229920000098 polyolefin Polymers 0.000 claims abstract description 7
- 238000010438 heat treatment Methods 0.000 claims abstract description 6
- 150000001336 alkenes Chemical class 0.000 claims abstract description 5
- JRZJOMJEPLMPRA-UHFFFAOYSA-N olefin Natural products CCCCCCCC=C JRZJOMJEPLMPRA-UHFFFAOYSA-N 0.000 claims abstract description 5
- 125000004805 propylene group Chemical group [H]C([H])([H])C([H])([*:1])C([H])([H])[*:2] 0.000 claims abstract description 5
- QQONPFPTGQHPMA-UHFFFAOYSA-N propylene Natural products CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000002759 woven fabric Substances 0.000 claims description 10
- 229920001684 low density polyethylene Polymers 0.000 claims description 3
- 239000004702 low-density polyethylene Substances 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 3
- 229920005604 random copolymer Polymers 0.000 claims description 3
- 239000002344 surface layer Substances 0.000 claims description 2
- 229920005673 polypropylene based resin Polymers 0.000 claims 1
- 238000005452 bending Methods 0.000 abstract description 17
- 238000000465 moulding Methods 0.000 abstract description 8
- 239000011229 interlayer Substances 0.000 abstract 1
- 239000012792 core layer Substances 0.000 description 16
- 229920005989 resin Polymers 0.000 description 7
- 239000011347 resin Substances 0.000 description 7
- 238000007666 vacuum forming Methods 0.000 description 6
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 239000000835 fiber Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000000704 physical effect Effects 0.000 description 4
- 229920001187 thermosetting polymer Polymers 0.000 description 4
- 230000032798 delamination Effects 0.000 description 3
- 229920000092 linear low density polyethylene Polymers 0.000 description 3
- 239000004707 linear low-density polyethylene Substances 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 238000011437 continuous method Methods 0.000 description 2
- 239000011162 core material Substances 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical group C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- 239000005977 Ethylene Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 229920001519 homopolymer Polymers 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920000139 polyethylene terephthalate Polymers 0.000 description 1
- 239000005020 polyethylene terephthalate Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
Description
本発明は、内層(コア層)の両表面に炭素織物層を一体化した熱可塑性積層シート及びその製造方法に関する。 The present invention relates to a thermoplastic laminated sheet in which carbon fabric layers are integrated on both surfaces of an inner layer (core layer) and a method for producing the same.
従来から、炭素繊維やアラミド繊維などの強化繊維織物を複数枚積層したり、発泡体シートなどと一体化した積層体は知られている。特許文献1には、発泡体からなる内層(コア層)シートの表面に炭素繊維織物層を一体化した積層シートは提案されている。また、特許文献2には炭素繊維表面にエポキシ樹脂をサイジング剤として塗布し、熱硬化性樹脂との接着強度を高めることが提案されている。さらに、特許文献3には炭素繊維と熱硬化性樹脂の片面に熱可塑性樹脂層を積層し、真空成形することが提案されている。
Conventionally, a laminate in which a plurality of reinforcing fiber fabrics such as carbon fibers and aramid fibers are laminated or integrated with a foam sheet is known.
しかし、従来の積層体は炭素繊維に熱硬化性樹脂を積層しており、成形時に熱硬化させるための硬化時間が必要で、成形時間が長くかかり、成形コストが高いという問題があった。 However, the conventional laminate has a problem that a thermosetting resin is laminated on carbon fibers, and a curing time is required for thermosetting at the time of molding, which requires a long molding time and a high molding cost.
本発明は、前記従来の問題を解決するため、層間剥離がなく、軽量であり、曲げに対する物理的強度も高く、成形コストも安価な熱可塑性積層シート及びその製造方法を提供する。 In order to solve the above-described conventional problems, the present invention provides a thermoplastic laminated sheet that does not have delamination, is lightweight, has high physical strength against bending, and has a low molding cost, and a method for producing the same.
本発明の熱可塑性積層シートは、内層の両表面に接着層を介して織物層が貼り合わされた積層シートであって、前記内層はポリプロピレンシート又はプロピレンを含むオレフィン系シートであり、前記織物層は炭素繊維織物であり、前記接着層は熱融着ポリオレフィン系フィルムであり、前記積層シートは熱可塑性であることを特徴とする。 The thermoplastic laminated sheet of the present invention is a laminated sheet in which a fabric layer is bonded to both surfaces of the inner layer via an adhesive layer, the inner layer being a polypropylene sheet or an olefin-based sheet containing propylene, and the fabric layer is It is a carbon fiber woven fabric, the adhesive layer is a heat-sealable polyolefin film, and the laminated sheet is thermoplastic.
本発明の熱可塑性積層シートの製造方法は、前記の積層シートの製造方法であって、内層と、その両表面に接着用フィルムと、その両表面に炭素繊維織物層を配置して加熱加圧し、次いで冷却することを特徴とする。 The method for producing a thermoplastic laminated sheet of the present invention is a method for producing the above laminated sheet, wherein an inner layer, an adhesive film on both surfaces thereof, and a carbon fiber fabric layer on both surfaces are heated and pressurized. And then cooling.
本発明は、積層シートを構成する内層及び接着層がオレフィン系樹脂であるため、成形コストを安価にすると同時に、層間剥離がなく、軽量であり、曲げに対する物理的強度も高い熱可塑性積層シートを提供できる。また、この積層シートは熱可塑性であり、真空成形、プレス成形、熱変形を利用した曲げ加工成形等に好適で、安価な成形体とすることもできる。本発明の製造方法は、効率よく合理的に本発明の積層シートを製造できる。 In the present invention, since the inner layer and the adhesive layer constituting the laminated sheet are olefin-based resins, a thermoplastic laminated sheet that reduces the molding cost, has no delamination, is lightweight, and has high physical strength against bending. Can be provided. Moreover, this laminated sheet is thermoplastic, and is suitable for vacuum forming, press forming, bending forming using thermal deformation, and the like, and can be an inexpensive formed body. The production method of the present invention can produce the laminated sheet of the present invention efficiently and rationally.
本発明の積層シートは、内層(コア層)の両表面に接着層を介して炭素繊維織物層が貼り合わされた積層シートである。内層(コア層)はポリプロピレンシート又はプロピレンを含むオレフィン系シートである。この内層(コア層)シートはフィルムであっても良い。ポリプロピレンシート又はポリプロピレンを含むシートは、実用的に物理的特性を満足する分野があり、コストも安い利点がある。さらに、接着層として熱融着ポリオレフィン系フィルムを使用することにより、内層(コア層)と炭素繊維織物層との加熱加圧接着が可能となり、積層一体化しやすい。 The laminated sheet of the present invention is a laminated sheet in which a carbon fiber fabric layer is bonded to both surfaces of an inner layer (core layer) via an adhesive layer. The inner layer (core layer) is a polypropylene sheet or an olefin-based sheet containing propylene. The inner layer (core layer) sheet may be a film. A polypropylene sheet or a sheet containing polypropylene has an advantage of practically satisfying physical properties and has an advantage of low cost. Furthermore, by using a heat-sealable polyolefin film as the adhesive layer, the inner layer (core layer) and the carbon fiber woven layer can be heated and pressurized and easily laminated and integrated.
内層(コア層)は非発泡ポリプロピレン系シートを使用するのが好ましい。非発泡ポリプロピレン系シートはプレス成形によっても内層(コア層)が潰れることはなく、真空成形、熱変形を利用した曲げ加工成形等も容易にできる。 The inner layer (core layer) is preferably a non-foamed polypropylene sheet. The non-expanded polypropylene sheet does not crush the inner layer (core layer) even by press molding, and can be easily formed by vacuum forming, bending processing using thermal deformation, or the like.
内層(コア層)はプロピレン-エチレンランダムコポリマー(RPP)であるのが好ましい。RPPはプロピレンユニットが50モル%を超え、エチレンユニットが50モル%未満のランダムコポリマーで、融点は135〜150℃であり、一般的に市販されている。RPPは熱融着性に優れる利点がある。内層(コア層)の好ましい厚さは0.1〜2mmであり、より好ましくは0.2〜1.5mmである。 The inner layer (core layer) is preferably a propylene-ethylene random copolymer (RPP). RPP is a random copolymer containing more than 50 mol% propylene units and less than 50 mol% ethylene units, and has a melting point of 135 to 150 ° C. and is generally commercially available. RPP has an advantage of excellent heat-fusibility. The preferred thickness of the inner layer (core layer) is 0.1 to 2 mm, more preferably 0.2 to 1.5 mm.
熱融着ポリオレフィン系フィルムは低密度ポリエチレン(LLDPE)であるのが好ましい。LLDPEは熱加工性、接着性、透明性に優れる。 The heat-sealable polyolefin film is preferably low density polyethylene (LLDPE). LLDPE is excellent in heat processability, adhesiveness and transparency.
炭素繊維織物は平織、綾織(斜文織)、朱子織、その他の変化織など、どのような組織の織物であっても良い。炭素繊維織物の単位面積当たりの重量(目付)は50〜500g/m2の範囲が好ましい。 The carbon fiber woven fabric may be a woven fabric having any structure such as plain weave, twill weave (oblique fabric), satin weave, and other changed weaves. The weight (unit weight) per unit area of the carbon fiber fabric is preferably in the range of 50 to 500 g / m 2 .
本発明の積層シートは、炭素繊維織物層のいずれか一方の表層に接着層を介してポリプロピレン系樹脂層をさらに備えても良い。このようにするとポリプロピレン系樹脂層で覆われた板状体のシートとすることができ、成形体としての応用範囲も広くなる。 The laminated sheet of the present invention may further include a polypropylene resin layer on any one surface layer of the carbon fiber woven fabric layer via an adhesive layer. If it does in this way, it can be set as the sheet | seat of the plate-shaped body covered with the polypropylene-type resin layer, and the application range as a molded object becomes wide.
さらに本発明の積層シートは、内層(コア層)と炭素繊維織物層の間に多軸繊維シートを加えることもできる。多軸繊維シートは倉敷紡績株式会社製、商品名“クラマス”を挙げることができる。一例として多軸繊維の方向は0°/+60°/−60°、1平方メートル当たりの重量(目付け)は350g/m2であり、トータル繊度1850deci texのPPフィラメントを多数本使用し、ステッチ糸としてポリエチレンテレフタレート糸を使用した多軸繊維シートがある。 Furthermore, the laminated sheet of this invention can also add a polyaxial fiber sheet between an inner layer (core layer) and a carbon fiber fabric layer. An example of the multiaxial fiber sheet is “Kuramas” manufactured by Kurashiki Boseki Co., Ltd. As an example, the direction of the multiaxial fiber is 0 ° / + 60 ° / −60 °, the weight per square meter (weight per unit area) is 350 g / m 2 , and many PP filaments with a total fineness of 1850 deci tex are used as stitch yarn. There is a multiaxial fiber sheet using polyethylene terephthalate yarn.
本発明の積層シートの製造方法は、内層と、その両表面に接着用フィルムと、その両表面に炭素繊維織物層を配置して加熱加圧し、次いで冷却する。一例として、内層と、その両表面に接着用フィルムと、その両表面に炭素繊維織物層を配置して連続的に熱プレスし、引き続き連続的に冷却し、積層シートを連続的に製造する。熱プレス工程の雰囲気温度は 150〜190℃が好ましく、さらに好ましくは160〜180℃である。加圧力は1 MPa程度が好ましい。加熱時間は0.5〜5分間が好ましく、さらに好ましくは1〜 4分間である。冷却工程の時間は0.5〜5分間が好ましく、さらに好ましくは1〜4分間である。冷却温度は30℃程度以下になるまでが好ましい。成形後の積層シート全体の厚みは0.5〜5mmが好ましい。連続的方法は大量生産に好ましい。 In the method for producing a laminated sheet of the present invention, an inner layer, an adhesive film on both surfaces thereof, and a carbon fiber fabric layer on both surfaces are heated and pressurized, and then cooled. As an example, an inner layer, an adhesive film on both surfaces thereof, and a carbon fiber woven fabric layer on both surfaces thereof are continuously hot pressed, continuously cooled, and a laminated sheet is continuously manufactured. The atmospheric temperature in the hot pressing step is preferably 150 to 190 ° C, more preferably 160 to 180 ° C. The applied pressure is preferably about 1 MPa. The heating time is preferably 0.5 to 5 minutes, more preferably 1 to 4 minutes. The time for the cooling step is preferably 0.5 to 5 minutes, and more preferably 1 to 4 minutes. The cooling temperature is preferably up to about 30 ° C. or less. The thickness of the entire laminated sheet after molding is preferably 0.5 to 5 mm. A continuous process is preferred for mass production.
本発明の製造方法は前記連続法に限らず、1回ごとの加熱加圧プレスと冷却法によっても製造できる。サンプルを作製したり、小規模に製造する際にはこの方法で十分である。この方法の製造条件も前記連続法と同様である。 The production method of the present invention is not limited to the continuous method, and can be produced by a heating and pressing press and a cooling method for each time. This method is sufficient when producing samples or manufacturing on a small scale. The manufacturing conditions of this method are the same as in the continuous method.
次に図面を用いて説明する。以下の図面において、同一符号は同一部を示す。図1は本発明の一実施態様の積層シートの模式的断面図である。この積層シート6は、内層1の両表面に接着層2a,2Bを介して炭素繊維織物層3a,3bが貼り合わされ一体化されている。
Next, it demonstrates using drawing. In the following drawings, the same reference numerals indicate the same parts. FIG. 1 is a schematic cross-sectional view of a laminated sheet according to an embodiment of the present invention. In this laminated
図2は本発明の別の実施態様の積層シートの模式的断面図である。この積層シート7は、内層1の両表面に接着層2a,2Bを介して炭素繊維織物層3a,3bと、さらに接着層4a,4bを介してポリプロピレン系樹脂層(表皮層)5a,5bが積層一体化されている。表皮層は透明とし、内部の炭素繊維織物の織模様の外観とすることもできる。また、表皮層には様々な模様を印刷したり着色することもできる。
FIG. 2 is a schematic cross-sectional view of a laminated sheet according to another embodiment of the present invention. This laminated sheet 7 has carbon
図3は本発明の一実施態様における積層シートの製造装置10を示す模式的断面図である。この積層シートの製造装置10は、原料シートの供給ロール14,15a,15b,16a,16bと、加熱加圧領域20と、冷却領域21から構成され、全体は連続的に動く。まず内層(コア)は供給ロール14a,14bから、接着用フィルムは供給ロール15a,15bから、炭素繊維織物は供給ロール16a,16bからそれぞれ加圧ロール17a,17bに供給される。加圧ロール17a,17b及び22a,22bには金属製板18,19がエンドレス状に組み込まれており、まず加熱加圧領域20で加圧加熱される。次に、冷却領域21では冷却用エアーが矢印aから供給され矢印bから排出されることにより冷却される。効率の良い冷却をする場合は、冷却用エアーに加えて冷却領域21に水冷パイプを配置して冷却する。加圧ロール22a,22bから取り出された積層シート23は所定の長さにカットされる。
FIG. 3 is a schematic cross-sectional view showing a laminated
図4は本発明の一実施態様の積層シートを真空成形した成形体の模式的斜視図である。横の最大長さ260mm,奥行きの最大長さ170mm,高さ500mmの成形体の例である。この積層シートは深絞り成形できる利点がある。さらに、この積層シートは熱可塑性であり、真空成形、プレス成形、熱変形を利用した曲げ加工成形等において、成形サイクルが短く、加工コストも安価である。 FIG. 4 is a schematic perspective view of a molded body obtained by vacuum forming the laminated sheet of one embodiment of the present invention. This is an example of a molded body having a maximum horizontal length of 260 mm, a maximum depth of 170 mm, and a height of 500 mm. This laminated sheet has the advantage that it can be deep drawn. Furthermore, this laminated sheet is thermoplastic, and in vacuum forming, press forming, bending forming utilizing thermal deformation, etc., the forming cycle is short and the processing cost is low.
以下実施例により、本発明をさらに具体的に説明する。なお本発明は下記の実施例に限定されるものではない。 Hereinafter, the present invention will be described more specifically with reference to examples. The present invention is not limited to the following examples.
<曲げ弾性率と曲げ応力の測定方法>
JISK7171に準拠した3点曲げ試験で測定した。試験片サイズは幅20mm、長さ50mm、試験速度は1mm/minとした。押さえジグの形状はR5、支点の形状はR2、支点間隔24mmとした。
<Measurement method of bending elastic modulus and bending stress>
It measured by the 3 point | piece bending test based on JISK7171. The test piece size was 20 mm wide, 50 mm long, and the test speed was 1 mm / min. The shape of the holding jig was R5, the shape of the fulcrum was R2, and the fulcrum interval was 24 mm.
(実施例1)
<内層(コア層)>
内層(コア層)として市販のランダムタイプポリプロピレン(RPP)シート、融点145℃、厚み500μm、単位面積当たりの重量450g/m2を使用した。
<炭素繊維織物>
炭素繊維織物層として平織物、単位面積当たりの重量(目付)は65g/m2を用いた。
<接着フィルム>
市販の低密度ポリエチレン(LLDPE)、融点110℃、厚み30μm、単位面積当たりの重量27g/m2を使用した。
<積層シートの作成>
内層(コア層)の両面に接着フィルムと炭素繊維織物をこの順番に積層し、温度170℃、圧力1Mpa、1分間プレス成形し、その後室温(27℃)まで冷却した。これにより接着フィルムを溶着させて全体を一体化し、積層シートを得た。この積層シートの模式的断面図は図1に示すとおりである。
Example 1
<Inner layer (core layer)>
As the inner layer (core layer), a commercially available random type polypropylene (RPP) sheet, a melting point of 145 ° C., a thickness of 500 μm, and a weight per unit area of 450 g / m 2 was used.
<Carbon fiber fabric>
A plain woven fabric was used as the carbon fiber woven layer, and a weight (unit weight) per unit area of 65 g / m 2 was used.
<Adhesive film>
Commercially available low density polyethylene (LLDPE), melting point 110 ° C., thickness 30 μm, weight per unit area 27 g / m 2 was used.
<Creation of laminated sheet>
An adhesive film and a carbon fiber woven fabric were laminated in this order on both surfaces of the inner layer (core layer), press-molded at a temperature of 170 ° C., a pressure of 1 Mpa for 1 minute, and then cooled to room temperature (27 ° C.). As a result, the adhesive film was welded to integrate the whole to obtain a laminated sheet. A schematic cross-sectional view of this laminated sheet is as shown in FIG.
得られた積層シートの曲げ弾性率と曲げ応力を表1にまとめて示す。 Table 1 shows the bending elastic modulus and bending stress of the obtained laminated sheet.
(実施例2)
炭素繊維織物層として平織物、単位面積当たりの重量(目付)は130g/m2を用いた以外は実施例1と同様に実施した。得られた積層シートの物性は表1にまとめて示す。
(Example 2)
The same procedure as in Example 1 was performed except that a plain woven fabric was used as the carbon fiber woven layer, and the weight per unit area (weight per unit area) was 130 g / m 2 . The physical properties of the obtained laminated sheet are summarized in Table 1.
(実施例3)
実施例1における炭素繊維織物層の外側に実施例1に記載した接着フィルムを載せ、その上に表皮層としてホモポリマータイプポリプロピレン(HPP,融点160℃):25wt%とランダムタイプポリプロピレン(RPP,融点145℃):75wt%をブレンドした厚み200μm、単位面積当たりの重量180g/m2を積層した以外は実施例1と同様に実施した。この積層シートの模式的断面図は図2に示すとおりである。得られた積層シートの物性は表1にまとめて示す。
(Example 3)
The adhesive film described in Example 1 is placed on the outer side of the carbon fiber fabric layer in Example 1, and a homopolymer type polypropylene (HPP, melting point 160 ° C.): 25 wt% and a random type polypropylene (RPP, melting point) as a skin layer thereon. 145 ° C.): The same procedure as in Example 1 was conducted except that a thickness of 200 μm blended with 75 wt% and a weight of 180 g / m 2 per unit area were laminated. A schematic cross-sectional view of this laminated sheet is as shown in FIG. The physical properties of the obtained laminated sheet are summarized in Table 1.
(比較例1)
比較例1として実施例1の内層(コア層)の物性を表1にまとめて示す。なお、各例の曲げ弾性率及び曲げ応力のデータはMD(長さ方向)のデータである。
(Comparative Example 1)
Table 1 summarizes the physical properties of the inner layer (core layer) of Example 1 as Comparative Example 1. In addition, the data of the bending elastic modulus and bending stress of each example are data of MD (length direction).
表1から明らかなとおり、本発明の実施例品は曲げ弾性率と曲げ応力が高く、層間剥離はなく、軽量であり、曲げに対する物理的強度も高い積層シートであった。また、この積層シートは熱可塑性であり、真空成形、プレス成形、熱変形を利用した曲げ加工成形等に好適で、安価な成形体であった。さらに、炭素繊維織物層は熱融着ポリオレフィン系フィルムを介して内層に接着しているため、織物の美しい織柄がそのまま積層シートの表面に現れる成形体とすることができた。 As apparent from Table 1, the product of the example of the present invention was a laminated sheet having high bending elastic modulus and bending stress, no delamination, light weight, and high physical strength against bending. Further, this laminated sheet was thermoplastic, suitable for vacuum forming, press forming, bending forming utilizing thermal deformation, and the like, and was an inexpensive formed body. Furthermore, since the carbon fiber woven layer is bonded to the inner layer through a heat-sealable polyolefin film, a beautiful woven pattern of the woven fabric can be formed as it is on the surface of the laminated sheet.
本発明の積層シートを用いた成形品は、自動車部品、自動車内装品、家電製品、医療用保護具、スーツケース、容器、棚、パレット、パネル、バッグ、自動倉庫用スリーブボックス、ドア、ロール回収用長尺ボックス、畳の芯材、展示ブース様壁材、Tボード(トラック用当て板)、簡易テーブルセット等の民生用積層品に適用できる。 Molded articles using the laminated sheet of the present invention are automobile parts, automobile interior parts, home appliances, medical protective equipment, suitcases, containers, shelves, pallets, panels, bags, sleeve boxes for automatic warehouses, doors, rolls. It can be applied to consumer laminated products such as long boxes, tatami core materials, exhibition booth-like wall materials, T-boards (truck backing plates), and simple table sets.
1 内層(コア層)
2a,2b 接着層
3a,3b 炭素繊維織物層
4a,4b 接着層
5a,5b 表皮層
6,7,23 積層シート
10 積層シート製造装置
14a,14b,15a,15b,16a,16b 供給ロール
17a,17b,22a,22b 加圧ロール
18,19 金属製板
20 加熱加圧領域
21 冷却領域
1 Inner layer (core layer)
2a, 2b
Claims (6)
前記内層はポリプロピレンシート又はプロピレンを含むオレフィン系シートであり、
前記織物層は炭素繊維織物であり、
前記接着層は熱融着ポリオレフィン系フィルムであり、
前記積層シートは熱可塑性であることを特徴とする熱可塑性積層シート。 A laminated sheet in which a fabric layer is bonded to both surfaces of the inner layer via an adhesive layer,
The inner layer is a polypropylene sheet or an olefin-based sheet containing propylene,
The fabric layer is a carbon fiber fabric;
The adhesive layer is a heat-sealable polyolefin film,
The thermoplastic laminated sheet, wherein the laminated sheet is thermoplastic.
内層と、その両表面に接着用フィルムと、その両表面に炭素繊維織物層を配置して加熱加圧し、次いで冷却することを特徴とする熱可塑性積層シートの製造方法。 A method for producing a thermoplastic laminated sheet according to any one of claims 1 to 5,
A method for producing a thermoplastic laminated sheet, comprising: an inner layer; an adhesive film on both surfaces thereof; and a carbon fiber woven fabric layer on both surfaces, heating and pressing, and then cooling.
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