JPH03216307A - Manufacture of prepreg - Google Patents
Manufacture of prepregInfo
- Publication number
- JPH03216307A JPH03216307A JP1170790A JP1170790A JPH03216307A JP H03216307 A JPH03216307 A JP H03216307A JP 1170790 A JP1170790 A JP 1170790A JP 1170790 A JP1170790 A JP 1170790A JP H03216307 A JPH03216307 A JP H03216307A
- Authority
- JP
- Japan
- Prior art keywords
- sheet
- prepreg
- release
- fiber
- release sheet
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 22
- 229920005989 resin Polymers 0.000 claims abstract description 29
- 239000011347 resin Substances 0.000 claims abstract description 29
- 239000012783 reinforcing fiber Substances 0.000 claims abstract description 28
- 238000005520 cutting process Methods 0.000 claims abstract description 14
- 238000000034 method Methods 0.000 claims description 13
- 238000004804 winding Methods 0.000 claims description 7
- 238000005470 impregnation Methods 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 18
- 239000000835 fiber Substances 0.000 abstract description 10
- 238000010438 heat treatment Methods 0.000 abstract description 10
- 238000010030 laminating Methods 0.000 abstract description 2
- 239000010410 layer Substances 0.000 description 22
- 210000005069 ears Anatomy 0.000 description 10
- -1 polyethylene Polymers 0.000 description 6
- 239000003733 fiber-reinforced composite Substances 0.000 description 5
- 239000010408 film Substances 0.000 description 5
- 229920005992 thermoplastic resin Polymers 0.000 description 5
- 229920001187 thermosetting polymer Polymers 0.000 description 5
- 238000000465 moulding Methods 0.000 description 4
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 3
- 239000004698 Polyethylene Substances 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- RTZKZFJDLAIYFH-UHFFFAOYSA-N ether Substances CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229920000573 polyethylene Polymers 0.000 description 3
- 229920001721 polyimide Polymers 0.000 description 3
- 229920001296 polysiloxane Polymers 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000004695 Polyether sulfone Substances 0.000 description 2
- 239000004642 Polyimide Substances 0.000 description 2
- 239000013039 cover film Substances 0.000 description 2
- RAXXELZNTBOGNW-UHFFFAOYSA-N imidazole Natural products C1=CNC=N1 RAXXELZNTBOGNW-UHFFFAOYSA-N 0.000 description 2
- 239000006082 mold release agent Substances 0.000 description 2
- 229920002492 poly(sulfone) Polymers 0.000 description 2
- 229920006393 polyether sulfone Polymers 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 125000003903 2-propenyl group Chemical group [H]C([*])([H])C([H])=C([H])[H] 0.000 description 1
- YKFRAOGHWKADFJ-UHFFFAOYSA-N Aramite Chemical compound ClCCOS(=O)OC(C)COC1=CC=C(C(C)(C)C)C=C1 YKFRAOGHWKADFJ-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- PEEHTFAAVSWFBL-UHFFFAOYSA-N Maleimide Chemical compound O=C1NC(=O)C=C1 PEEHTFAAVSWFBL-UHFFFAOYSA-N 0.000 description 1
- 239000004696 Poly ether ether ketone Substances 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004693 Polybenzimidazole Substances 0.000 description 1
- 239000004697 Polyetherimide Substances 0.000 description 1
- 239000004721 Polyphenylene oxide Substances 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 229920002472 Starch Polymers 0.000 description 1
- 239000003082 abrasive agent Substances 0.000 description 1
- 238000007259 addition reaction Methods 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- NIDNOXCRFUCAKQ-UHFFFAOYSA-N bicyclo[2.2.1]hept-5-ene-2,3-dicarboxylic acid Chemical compound C1C2C=CC1C(C(=O)O)C2C(O)=O NIDNOXCRFUCAKQ-UHFFFAOYSA-N 0.000 description 1
- 239000004202 carbamide Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000011203 carbon fibre reinforced carbon Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000006482 condensation reaction Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000003851 corona treatment Methods 0.000 description 1
- 239000004643 cyanate ester Substances 0.000 description 1
- 239000004205 dimethyl polysiloxane Substances 0.000 description 1
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 description 1
- 229920006351 engineering plastic Polymers 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 229920000435 poly(dimethylsiloxane) Polymers 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920002480 polybenzimidazole Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000570 polyether Polymers 0.000 description 1
- 229920002530 polyetherether ketone Polymers 0.000 description 1
- 229920001601 polyetherimide Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野1
本発明は、繊維強化プラスチック(FRP)等の繊維強
化複合祠料の成形に用いられるプリプレグの製造方法に
関し、とくに、FRP製ゴルフシャフトを成形する際に
バイアス層に用いられるプリプレグの製造方法に関する
。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field 1] The present invention relates to a method for manufacturing a prepreg used for molding a fiber-reinforced composite abrasive material such as fiber-reinforced plastic (FRP), and particularly relates to a method for manufacturing a prepreg used for molding a golf shaft made of FRP. The present invention relates to a method for manufacturing a prepreg used for a bias layer.
[従来の技術]
繊維強化複合材料の成形に用いられるプリプレグとして
、強化繊維をシート状に一方向に引き揃えてシートの形
態としたものが知られている。このようなプリプレグの
製造は、たとえば第4図に示すように行われている。[Prior Art] As a prepreg used for molding fiber-reinforced composite materials, a sheet made by aligning reinforcing fibers in one direction is known. Such prepreg is manufactured, for example, as shown in FIG. 4.
送られてきた強化繊維シー1〜1の上下両面にそれぞれ
、一面に樹脂を担持した離型シート2、3を重ね合せ、
この重合せ体4を、加熱手段5により予熱し、加熱ロー
ル6とプレスロール7により、加熱するとともに両側か
ら加圧し、樹脂を強化繊維シート1に転移、含浸させて
プリプレグ8を作製し、一方の離型シート2を剥離した
後、プリブレグ8を他方の離型シート3とともにブリプ
レグロール9として巻き取る方法である。このブリプレ
グロール9が、繊維強化複合trA利の成形のためのプ
リプレグ材を作成する際に、第5図に示すように、シー
ト状に巻き戻されて使用ざれる。強化繊維シート1に樹
脂を含浸させるために加圧するときには、強化繊維シー
ト1および樹脂がシート幅方向に押し拡げられるので、
離型シート2、3には作製すべきプリプレグ8の幅より
も広幅のものが使用ざれる。したがって、プリプレグ8
と離型シート3との積層体においては、プリプレグ8の
幅方向両外側部分に、離型シート3の耳部10が存在し
ている。Release sheets 2 and 3 carrying resin on one side are superimposed on the upper and lower surfaces of the reinforcing fiber sheets 1 to 1 that have been sent, respectively.
This polymerized body 4 is preheated by a heating means 5, heated and pressed from both sides by a heating roll 6 and a press roll 7, and the resin is transferred and impregnated into the reinforcing fiber sheet 1 to produce a prepreg 8. In this method, after peeling off the release sheet 2, the prepreg 8 is wound up together with the other release sheet 3 as a bripreg roll 9. This prepreg roll 9 is used by being rewound into a sheet shape, as shown in FIG. 5, when preparing a prepreg material for molding a fiber-reinforced composite trA resin. When applying pressure to impregnate the reinforcing fiber sheet 1 with resin, the reinforcing fiber sheet 1 and the resin are expanded in the width direction of the sheet.
The release sheets 2 and 3 used have a wider width than the prepreg 8 to be produced. Therefore, prepreg 8
In the laminate of the release sheet 3 and the release sheet 3, the ears 10 of the release sheet 3 are present on both outer sides in the width direction of the prepreg 8.
このようなプリプレグ8と離型シート3との積層体を用
いて、繊維強化複合材料のバイアス層用プリプレグは、
通常、次のように作られる。Using such a laminate of the prepreg 8 and the release sheet 3, the prepreg for the bias layer of the fiber reinforced composite material is
It is usually made as follows.
バイアス1は、繊維強化複合材料において、主に補強し
ようとする方向に強化繊維が配列ざれるメインのプリプ
レグ層に対し、強化繊維の配列方向を必る角度傾斜させ
て積層される層である。したがって、よす第6図に示す
ように、ブリプレグロール9から巻き戻されたプリブレ
グ8と離型シ−. +・3との積層シートを、強化繊維
の配列方向11に対し所定の角度αだけ傾(プた切断線
12に沿って切断する。次に、切断した平行四辺形のシ
ート13から、第7図に示すように両端の耳部10を切
断して除去する。耳部10の除去されたシート14を、
第8図に示すように、複数、耳部除去辺15が互に突合
せ接続されるように、離型シート16上に配置する。こ
のとき、離型シート3は上側に位置し、プリプレグ8は
離型シート3と離型シート16との間に位置する。そし
て、上から、アイロン等により加熱して、プリプレグ8
と離型シート3との積層シートを離型シート16に仮接
着する。次に第9図に示すように、上記仮接着ざれたシ
ートを、バイアス層として使用されるプリプレグ材の規
定長「、たとえば、ゴルフクラブのシャフトのバイアス
層として巻かれる部分の長さに切断線17に沿って切断
していく。規定長Lに切断されたシート18を、たとえ
ば第10図に示すように、加熱ロール19と加圧ロール
20からなるカレンダー装置に通し、プリブレグ8と離
型シート16とを接看する。作製されたシート18から
、離型シー1− 3を剥離し、離型シ−i−3の剥離さ
れたシート21を、第11図に示すような切断線22に
沿って切断することにより、バイアス層の成形に用いら
れる、所定寸法の、プリプレグ8と離型シート16との
各積層シート23か得られる。この積層シート23が、
テーパシャフト状のマンドレル(図示略〉上に、あるい
は該マンドレル上に既に巻かれたメインのプリプレグ層
上に巻かれ、外面側の離型シート16が剥離、除去され
て、バイアス層の成形に供される。なお、所定寸法に切
断ざれた各積層シート23は、プリプレグ8面同士を接
着することにより二層構造とすることもでき、必要に応
じて順次積層することにより、さらに多層構造のバイア
ス層用プリプレグ材とすることもできる。Bias 1 is a layer in a fiber-reinforced composite material that is laminated with the reinforcing fibers arranged at a certain angle with respect to the main prepreg layer in which reinforcing fibers are arranged mainly in the direction to be reinforced. Therefore, as shown in FIG. 6, the pre-reg 8 unwound from the pre-preg roll 9 and the release sheet. The laminated sheet of + and 3 is cut along the cut line 12 at a predetermined angle α with respect to the reinforcing fiber arrangement direction 11.Next, from the cut parallelogram sheet 13, the 7th As shown in the figure, the ears 10 at both ends are cut and removed.The sheet 14 from which the ears 10 have been removed is
As shown in FIG. 8, a plurality of edge removal sides 15 are arranged on a release sheet 16 so as to butt and connect with each other. At this time, the release sheet 3 is located on the upper side, and the prepreg 8 is located between the release sheet 3 and the release sheet 16. Then, heat the prepreg 8 with an iron or the like from above.
A laminated sheet of the mold release sheet 3 and the mold release sheet 3 is temporarily adhered to the mold release sheet 16. Next, as shown in FIG. 9, cut the temporarily adhered sheet to the specified length of the prepreg material to be used as the bias layer, for example, to the length of the part to be wound as the bias layer of the shaft of a golf club. The sheet 18 cut to a specified length L is passed through a calender device consisting of a heating roll 19 and a pressure roll 20, for example, as shown in FIG. The mold release sheet 1-3 is peeled off from the prepared sheet 18, and the sheet 21 from which the mold release sheet i-3 has been peeled is cut along the cutting line 22 as shown in FIG. By cutting along the lines, each laminated sheet 23 of the prepreg 8 and the release sheet 16 of a predetermined size, which is used for forming the bias layer, is obtained.This laminated sheet 23 is
It is wound on a tapered shaft-shaped mandrel (not shown) or on the main prepreg layer already wound on the mandrel, and the release sheet 16 on the outer side is peeled off and removed, and used for forming a bias layer. In addition, each laminated sheet 23 cut to a predetermined size can be made into a two-layer structure by gluing the eight prepreg faces together, and if necessary, by sequentially laminating them, a bias of a multi-layer structure can be formed. It can also be used as a prepreg material for layers.
[発明か解決しようとする課題]
上記のようなバイアス層用プリプレグ材の作製方法にお
いては、第8図に示したようにバイアス層用プリプレグ
を連続的に突合せ接続するためには、必ず第7図に示1
ように離型シート3の耳部10を切断、除去でる工程が
必要になる。[Problems to be Solved by the Invention] In the method for manufacturing the bias layer prepreg material as described above, in order to continuously butt connect the bias layer prepreg material as shown in FIG. As shown in the figure 1
A process of cutting and removing the ears 10 of the release sheet 3 is required.
本発明は、プリプレグ製造段階での工夫により、プリプ
レグ製造後バイアス層用プリプレグ材作製時の、第7図
に示したような離型シート耳部の切断、除去工程を不要
化し、バイアス層用プリプレグ材の作製を容易にするこ
とを目的とする。The present invention eliminates the need for cutting and removing the release sheet edges as shown in FIG. 7 during the production of bias layer prepreg material after prepreg production, by making improvements in the prepreg production stage, and makes it possible to create a bias layer prepreg material by eliminating the need for cutting and removing the release sheet edges as shown in Figure 7. The purpose is to facilitate the production of materials.
[課題を解決するための手段]
この目的に沿う本発明のプリプレグの製造方法は、強化
繊維を一方向に互いに並行に引き揃えてなるシートの上
下両面に、少なくとも一方が一面に樹脂を担持した離型
シートをその樹脂担持面においてそれぞれ重ね合せ、担
持樹脂を強化繊維シートに転移、含浸させてプリプレグ
を作製し、該プリプレグから一方の離型シートを剥離し
、プリプレグを他方の離型シートとともに巻き取る方法
から成る。[Means for Solving the Problems] A method for producing a prepreg of the present invention in accordance with this objective is to carry a resin on at least one of the upper and lower surfaces of a sheet formed by aligning reinforcing fibers in one direction and parallel to each other. The release sheets are stacked on each other on their resin-supporting surfaces, and the supported resin is transferred to and impregnated into the reinforcing fiber sheet to produce a prepreg.One release sheet is peeled from the prepreg, and the prepreg is removed together with the other release sheet. It consists of the method of winding.
[作 用]
このような方法においては、プリプレグ¥A造段階で既
に、離型シートの耳部が切断、除去され、巻き取られた
ブリプレグロールにおけるプリプレグと離型シートの幅
は実質的に同一の幅とされる。[Function] In such a method, the edges of the release sheet are already cut and removed at the prepreg A manufacturing stage, and the widths of the prepreg and release sheet in the rolled up prepreg roll are substantially equal to each other. They are assumed to have the same width.
したがって、ブリプレグロールを巻き戻したプリプレグ
と離型シートとの積層シートには、もはや離型シートの
耳部は存在せず、従来の、バイアス層用プリプレグ材を
作製する際の離型シート耳部切断工程は不要になり、作
製工程全体が簡素化される。Therefore, in the laminated sheet of prepreg and release sheet obtained by unwinding the Bripreglo roll, there is no longer an edge of the release sheet, and the edge of the release sheet is no longer present when producing the prepreg material for the bias layer. The cutting process becomes unnecessary, and the entire manufacturing process is simplified.
[実施例]
以下に、本発明の実施例を、゛図面を参照して説明覆る
。[Examples] Examples of the present invention will be described below with reference to the drawings.
第1図は本発明の一実施例に係る方法を実施するための
プリプレグ製造装置を、第2図は、第1図の装置により
製造されたプリプレグと離型シートとの積層シーi〜を
、第3図はその断面をそれぞれ小している。FIG. 1 shows a prepreg manufacturing apparatus for carrying out a method according to an embodiment of the present invention, and FIG. 2 shows a laminated sheet i~ of prepreg and a release sheet manufactured by the apparatus of FIG. 1. In FIG. 3, the cross sections are respectively reduced.
第1図において、31は、強化繊維束をシート状に一方
向に引き揃えてなる強化繊維シー1−を示している。In FIG. 1, numeral 31 indicates a reinforcing fiber sheet 1- formed by aligning reinforcing fiber bundles in a sheet shape in one direction.
強化繊維は、炭素繊維、黒鉛繊維、有機高弾性率繊維(
アラミト繊維等)、炭化ケイ素繊維、アルミナ繊維、ホ
ロン繊維、タングステンカーバイド繊維、ガラス繊維等
の高強度、高弾性率繊維である。このような強化繊維は
、同じプリプレグについてただ1種類のものを使用して
もよいし、異なる種類の強化繊維を規則的に、または不
規則に並べるなどして併用してもよい。Reinforcing fibers include carbon fiber, graphite fiber, organic high modulus fiber (
These are high-strength, high-modulus fibers such as aramit fibers, silicon carbide fibers, alumina fibers, holon fibers, tungsten carbide fibers, and glass fibers. Only one type of such reinforcing fibers may be used for the same prepreg, or different types of reinforcing fibers may be used in combination by arranging them regularly or irregularly.
少なくとも一方(本実施例では両方)が、一面(強化繊
維シート31側の面)に樹脂を担持してぃる離型シート
32、33が、離型シートロール34、35からそれぞ
れ巻き戻され、ガイドロール36、37で方向転換され
た後、連続的に送り出されてきた強化繊維シート31の
両面(上下面)に重ね合せられる。Release sheets 32 and 33, on which at least one side (both sides in this example) support resin on one side (the surface on the reinforcing fiber sheet 31 side), are rewound from release sheet rolls 34 and 35, respectively; After being changed in direction by guide rolls 36 and 37, it is superimposed on both sides (upper and lower surfaces) of the reinforcing fiber sheet 31 that has been continuously fed out.
上記離型シート32、33としては、たとえば、厚み0
.05〜0.2#程度のクラフト紙、ロール紙、グラシ
ン紙などの紙の両面に、クレー、澱粉、ポリエチレン、
ポリビニルアルコールなどの口止剤の塗布層を設け、さ
らにその各塗布層の上にシリコーン系または非シリコー
ン系の離型剤、好ましくはポリシメチルシロキサンとポ
リジメチルハイド口シェンシロキサンとの縮合反応型ま
たは付加反応型シリコーンからなる離型剤を塗布したよ
うなものである。コロナ放電処理などによって離型性を
付与した合成樹脂フィルムや、離型剤を塗布した合成樹
脂フィルムを使用することもできる(たとえばポリエチ
レンフィルム、ポリプロピレンフィルム〉。この離型シ
ート32、33の幅は、作製されるべきプリプレグの幅
よりも大きい幅に設定されている。The release sheets 32 and 33 have a thickness of 0, for example.
.. Clay, starch, polyethylene,
A coating layer of a sealing agent such as polyvinyl alcohol is provided, and a silicone or non-silicone mold release agent, preferably a condensation reaction type of polydimethylsiloxane and polydimethylhydride sealant siloxane or It is like applying a mold release agent made of addition reaction type silicone. It is also possible to use a synthetic resin film that has been given release properties by corona discharge treatment or a synthetic resin film that has been coated with a release agent (for example, polyethylene film, polypropylene film).The width of the release sheets 32 and 33 is as follows: , the width is set to be larger than the width of the prepreg to be produced.
上下の離型シート32、33の少なくとも一方に、強化
繊維シート31に転移、含浸される樹脂が担持されてい
る。この担持樹脂には、熱硬化性樹脂や、熱硬化性樹脂
と熱可塑性樹脂を混合した樹脂を使用できる。熱硬化性
樹脂としては、エボキシ樹脂、マレイミド樹脂、ポリイ
ミド樹脂、アセチレン末端を有する樹脂、ビニル末端を
有する樹脂、アリル末端を有する樹脂、ナジック酸末端
を有する樹脂、シアン酸エステル末端を有する樹脂があ
げられる。これらは、一般に硬化剤や硬化触媒と組合せ
て用いることかできる。また、適宜、これらの熱硬化性
樹脂を混合して用いることも可能である。At least one of the upper and lower release sheets 32 and 33 carries a resin that is transferred to and impregnated into the reinforcing fiber sheet 31. This supporting resin may be a thermosetting resin or a mixture of a thermosetting resin and a thermoplastic resin. Examples of thermosetting resins include epoxy resins, maleimide resins, polyimide resins, resins with acetylene ends, resins with vinyl ends, resins with allyl ends, resins with nadic acid ends, and resins with cyanate ester ends. It will be done. These can generally be used in combination with curing agents and curing catalysts. Moreover, it is also possible to use a mixture of these thermosetting resins as appropriate.
また、樹脂として、上記の熱硬化性樹脂に熱可塑性樹脂
を混合して用いることも好適である。好適な熱可塑性樹
脂は、主鎖に、炭素炭素結合、アミド結合、イミド結合
、エステル結合、エーテル結合、カーボネート結合、ウ
レタン結合、尿素結合、チオエーテル結合、スルホン結
合、イミダゾール結合、カルボニル結合から選ばれる結
合を有する熱可塑性樹脂であり、より好ましくは、ポリ
アクリレート、ボリアミド、ポリアラミド、ポリエステ
ル、ポリカーホナート、ポリフエニレンスルフイド、ポ
リベンズイミダゾール、ポリイミド、ポリエーテルイミ
ト、ポリスルホン、ポリエーテルスルホン、ポリエーテ
ルエーテルケトンのようなエンジニアニングプラスチッ
クに属する熱可塑性樹脂の一群である。特に、ポリイミ
ド、ポリエーテルイミド、ポリスルホン、ポリエーテル
スルホン、ポリエーテルエーテルケトンは耐熱性に関し
優れた特性をもつ。Further, as the resin, it is also suitable to use a mixture of the above-mentioned thermosetting resin and a thermoplastic resin. Suitable thermoplastic resins have a main chain selected from carbon-carbon bonds, amide bonds, imide bonds, ester bonds, ether bonds, carbonate bonds, urethane bonds, urea bonds, thioether bonds, sulfone bonds, imidazole bonds, and carbonyl bonds. A thermoplastic resin having a bond, more preferably polyacrylate, polyamide, polyaramid, polyester, polycarbonate, polyphenylene sulfide, polybenzimidazole, polyimide, polyether imite, polysulfone, polyether sulfone, poly It is a group of thermoplastic resins that belong to engineering plastics such as ether ether ketone. In particular, polyimide, polyetherimide, polysulfone, polyether sulfone, and polyether ether ketone have excellent heat resistance properties.
強化繊維シート31と上下の樹脂担持離型シート32、
33との重合せ体38は、加熱板39で予熱された後、
本実施例では、3段の加熱ロール40a , 40b
,40cで加熱ざれるとともに、3段のプレスロール4
1a 、4tb 、41cで加圧され、該加熱、加圧に
より離型シート32、33に担持されていた樹脂が強化
繊維シート31に転移、含浸されて、プリプレグ42か
形成ざれる。reinforcing fiber sheet 31 and upper and lower resin-supported release sheets 32;
After the polymer 38 with 33 is preheated with a heating plate 39,
In this embodiment, three stages of heating rolls 40a and 40b are used.
, 40c, and three-stage press roll 4.
1a, 4tb, and 41c, and due to the heating and pressurization, the resin supported on the release sheets 32 and 33 is transferred and impregnated into the reinforcing fiber sheet 31, and a prepreg 42 is formed.
プリプレグ42と上下の離型シート32、33との積層
体から、ガイドロール43の位置で、一方の(上側の)
離型シー1−32が剥離され、離型シート32はシート
単体で離型シートロール44として巻き取られる。離型
シート32を剥離した後には、プリプレグ42と下側の
離型シート33との積層シート45となるが、この積層
シート45から、プリプレグ42の幅よりもプリプレグ
42両側にはみ出している離型シ]〜33の耳部46が
、カツタ47により、連続的に切断され、積層シーl〜
45から分離されて除去される。From the laminate of the prepreg 42 and the upper and lower release sheets 32 and 33, one (upper)
The release sheet 1-32 is peeled off, and the release sheet 32 is wound up as a release sheet roll 44 as a single sheet. After the mold release sheet 32 is peeled off, a laminated sheet 45 consisting of the prepreg 42 and the lower mold release sheet 33 is obtained. The ears 46 of ~33 are continuously cut by the cutter 47, and the laminated seal l~33 is cut continuously by the cutter 47.
45 and removed.
切断された耳部46は、適当な巻取装置く図示略》によ
って巻き取られるか、適当な粉砕機(図示略)によって
引き取られ粉砕処理される。The cut ears 46 are wound up by a suitable winding device (not shown) or taken up and crushed by a suitable crusher (not shown).
離型シート33の耳部46が切断、除去ざれた後、プリ
プレグ42と離型シート33とか同一幅に揃えられたプ
リプレグ42と離型シート33との積層シート48が、
巻芯49上にブリプレグロール50として巻き取られる
。After the ears 46 of the release sheet 33 are cut and removed, a laminated sheet 48 of the prepreg 42 and the release sheet 33, which are arranged to have the same width, is formed.
It is wound up on a winding core 49 as a burry preg roll 50.
このブリプレグロール50が、バイアス層用プリプレグ
材作製時に、第2図に示すようにシート状に巻き戻され
る。巻き戻された積層シート48は、第6図に示した方
法と同様に、強化繊維の配列方向51に対し所定の角度
αだけ傾けた切断線52に沿って平行四辺形のシート5
3に切断される。この積層シート48には、第3図に断
面を示すように、離型シート33の耳部46は存在しな
いから、従来方法では必要であった、第7図に示した耳
部切断工程が不要になる。なお、上記の角度αは、用途
等に応じて決める。たとえば、ゴルフシャ71〜の場合
、ねじれ防止の作用をもつバイアス層においては、長手
h向に対して強化繊維か±45゜の方向に配列されてい
るのが理想的なのであるが、成形時における、マントレ
ルへの巻き付けやすさ(プリプレグの厚み、強化繊維の
剛性等に左右される)、マンドレルのテーパー(6,’
1000前後)による巻き付け方向のずれや巻き付け力
のずれ等を考慮すると、30゜<α<47゜の範囲にす
るのが好ましい。This pre-preg roll 50 is rewound into a sheet shape as shown in FIG. 2 when producing the prepreg material for the bias layer. Similarly to the method shown in FIG. 6, the rewound laminated sheet 48 is cut into a parallelogram sheet 5 along a cutting line 52 inclined by a predetermined angle α with respect to the reinforcing fiber arrangement direction 51.
It is cut into 3. As shown in the cross section in FIG. 3, this laminated sheet 48 does not have the ears 46 of the release sheet 33, so the edge cutting process shown in FIG. 7, which was necessary in the conventional method, is unnecessary. become. Note that the above-mentioned angle α is determined depending on the application and the like. For example, in the case of golf shoes 71~, it is ideal for the reinforcing fibers to be arranged in a direction of ±45° with respect to the longitudinal direction H in the bias layer that has the effect of preventing twisting. , ease of wrapping around the mantrell (depends on prepreg thickness, stiffness of reinforcing fibers, etc.), mandrel taper (6,'
Considering the deviation in the winding direction and the deviation in the winding force due to the angle of 30°<α<47°, it is preferable to set the angle in the range of 30°<α<47°.
切断ざれた複数の平行四辺形の積層シート53を用いて
、バイアス層用プリプレグ材を作製する方法は、第8図
ないし第11図に示した方法と同じである。The method for producing the bias layer prepreg material using a plurality of cut parallelogram-shaped laminated sheets 53 is the same as the method shown in FIGS. 8 to 11.
なお、図示は省略するが、積層シート48をブリプレグ
ロール50として巻き取る前、および第11図に示した
積層シート作製後一方の離型シー1〜を剥離した後に、
べとつきやすい状態にあるプリプレグ面側表面をカバー
フイルム(たとえばポリエチレンフイルム)でカバーし
ておいてもよい。このカバーフイルムは、後の工程で、
必要に応じて剥ぎとればよい。Although not shown, before winding up the laminated sheet 48 as a buripregrol 50 and after peeling off one of the release sheets 1 to 1 after producing the laminated sheet shown in FIG. 11,
The prepreg side surface, which tends to become sticky, may be covered with a cover film (for example, polyethylene film). This cover film is made in a later process.
You can peel it off if necessary.
[発明の効果]
以上説明したように、本発明のプリプレグの製造方法に
よるときは、プリプレグ製造段階でブリプレグと離型シ
ーi一との積層体から離型シート耳部を切断、除去して
おくようにしたので、パイアス層用プリプレグ材を作製
する段階ではこの耳部の切断、除去工程が不要になり、
バイアス層用プリプレグ材の作製を大幅に容易化できる
という効果が得られる。[Effects of the Invention] As explained above, when using the prepreg manufacturing method of the present invention, the release sheet ears are cut and removed from the laminate of the prepreg and the release sheet i in the prepreg manufacturing stage. This eliminates the need for cutting and removing the ears at the stage of producing the prepreg material for the piecing layer.
The effect is that the preparation of the prepreg material for the bias layer can be greatly facilitated.
第1図は本発明の一実施例に係るプリプレグの製造方法
を実施するためのプリプレグ製造装置の概略側面図、
第2図は第1図の装置により製造されたプリプレグと離
型シートとの積層シートの斜視図、第3図は第2図の■
一■線に沿う断面図、第4図は従来のプリプレグ製造装
置の概略側面図、
第5図は第4図の装置により製造されたプリプレグと離
型シートとの積層シートの斜視図、第6図は第5図のシ
ー1〜の平面図、
第7図は第6図のシートから切断ざれたシートの、離型
シート耳部除去の様子を示す拡大平面図、第8図は第7
図の耳部切断で得られたシー1−を離型シート上に配置
していく様子を示した平面図、第9図は第8図で得られ
たシートを規定表に切断する様子を示した拡大平面図、
第10図は第9図で得られたシートを加熱、加圧するカ
レンダー装置の概略側面図、
第11図は第10図で得られたシートから一方の離型シ
ートを剥離したシートの平面図、
ておる。
31・−・・・・強化I!維シート
32、33・・・・・・離型シート
38・・・・・・重合せ体
39・・・・・・加熱板
40a , 40b , 40c・・・・・・加熱ロー
ル41a , 41b , 41c・・・・・・プレス
ロール42・・・・・・プリプレグ
45、48・・・・・・積層シート
46・・・・・・耳部
47・・・・・・カツタ
49・・・・・・巻芯
50・・・・・・ブリプレグロール
51・・・・・・強化繊維の配列方向
52・・・・・・切断線
53・・・・・・切断されたシート
第1
図
34
第2i!I
第3図
42
第4
図
)
3
○
3FIG. 1 is a schematic side view of a prepreg manufacturing apparatus for carrying out a prepreg manufacturing method according to an embodiment of the present invention, and FIG. 2 is a lamination of the prepreg manufactured by the apparatus of FIG. 1 and a release sheet. Perspective view of the seat, Figure 3 is shown in Figure 2.
4 is a schematic side view of a conventional prepreg manufacturing device; FIG. 5 is a perspective view of a laminated sheet of prepreg and a release sheet manufactured by the device shown in FIG. 4; The figure is a plan view of the sheets 1 to 1 in FIG. 5, FIG.
A plan view showing how the sheet 1- obtained by cutting the edges shown in the figure is placed on a release sheet, and Fig. 9 shows how the sheet obtained in Fig. 8 is cut into a specified shape. Fig. 10 is a schematic side view of a calender device that heats and presses the sheet obtained in Fig. 9; Fig. 11 shows one of the release sheets peeled from the sheet obtained in Fig. 10. Top view of the seat. 31・・・・・Reinforcement I! fiber sheets 32, 33...release sheet 38...polymerized body 39...heating plates 40a, 40b, 40c...heating rolls 41a, 41b, 41c...Press roll 42...Prepreg 45, 48...Laminated sheet 46...Ear portion 47...Cut 49... ... Core 50 ... Bripreglo roll 51 ... Arrangement direction of reinforcing fibers 52 ... Cutting line 53 ... Cut sheet 1 Fig. 34 2nd i! I Figure 3 42 Figure 4) 3 ○ 3
Claims (1)
ートの上下両面に、少なくとも一方が一面に樹脂を担持
した離型シートをその樹脂担持面においてそれぞれ重ね
合せ、担持樹脂を強化繊維シートに転移、含浸させてプ
リプレグを作製し、該プリプレグから一方の離型シート
を剥離し、プリプレグを他方の離型シートとともに巻き
取るプリプレグの製造方法において、前記一方の離型シ
ートを剥離した後、プリプレグの幅よりもはみ出してい
る前記他方の離型シートの耳部を切断、除去し、しかる
後に該他方の離型シートとともにプリプレグを巻き取る
ことを特徴とするプリプレグの製造方法。1. On both upper and lower surfaces of a sheet made of reinforcing fibers aligned parallel to each other in one direction, a release sheet with at least one side carrying resin is superimposed on the resin-carrying surface, and the supported resin is formed into a reinforcing fiber sheet. In a method for manufacturing a prepreg, in which a prepreg is produced by transfer and impregnation, one release sheet is peeled from the prepreg, and the prepreg is wound together with the other release sheet, after peeling off the one release sheet, the prepreg is A method for producing a prepreg, which comprises cutting and removing an edge of the other release sheet that protrudes beyond the width of the sheet, and then winding up the prepreg together with the other release sheet.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011707A JPH07115352B2 (en) | 1990-01-23 | 1990-01-23 | Prepreg manufacturing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011707A JPH07115352B2 (en) | 1990-01-23 | 1990-01-23 | Prepreg manufacturing method |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH03216307A true JPH03216307A (en) | 1991-09-24 |
JPH07115352B2 JPH07115352B2 (en) | 1995-12-13 |
Family
ID=11785518
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011707A Expired - Fee Related JPH07115352B2 (en) | 1990-01-23 | 1990-01-23 | Prepreg manufacturing method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07115352B2 (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0429013U (en) * | 1990-06-29 | 1992-03-09 | ||
WO2001018312A1 (en) * | 1999-09-09 | 2001-03-15 | Heinrich August Schoeller Söhne Gmbh & Co. Kg. | Transparent paper and method for the production thereof |
EP1134314A1 (en) * | 2000-03-16 | 2001-09-19 | Hexcel Composites | Intermediate composite product, manufacturing of such a product and usage as a molding material |
WO2007040125A1 (en) * | 2005-09-30 | 2007-04-12 | Sumitomo Bakelite Co., Ltd. | Process for producing prepreg with carrier, prepreg with carrier, process for producing thin-type double sided board, thin-type double sided board, and process for producing multilayered printed wiring board |
GB2445937A (en) * | 2006-11-23 | 2008-07-30 | Curon Ltd | Polymer composite |
JP2014079815A (en) * | 2012-10-12 | 2014-05-08 | Shima Seiki Mfg Ltd | Cutting method and cutting device |
WO2014084119A1 (en) * | 2012-11-30 | 2014-06-05 | 三菱重工業株式会社 | Device for manufacturing roll for angled layer, and operating method for device for manufacturing roll for angled layer |
JP2014121796A (en) * | 2012-12-20 | 2014-07-03 | Sanyu Rec Co Ltd | Roll of prepreg, production method of the same, and production device of the same |
CN109070389A (en) * | 2016-04-11 | 2018-12-21 | 三菱化学株式会社 | The manufacturing method of fibre reinforced resin material and the manufacturing device of fibre reinforced resin material |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58212936A (en) * | 1983-04-18 | 1983-12-10 | 東レ株式会社 | Fiber reinforced resin tubular body |
JPS59120420A (en) * | 1982-12-27 | 1984-07-12 | Toray Ind Inc | Manufacture of prepreg in form of tape |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE754321A (en) | 1969-08-04 | 1971-01-18 | Rolls Royce | METHOD FOR MANUFACTURING LONGITUDINALLY ALIGNED CARBON FIBER TAPES |
-
1990
- 1990-01-23 JP JP2011707A patent/JPH07115352B2/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59120420A (en) * | 1982-12-27 | 1984-07-12 | Toray Ind Inc | Manufacture of prepreg in form of tape |
JPS58212936A (en) * | 1983-04-18 | 1983-12-10 | 東レ株式会社 | Fiber reinforced resin tubular body |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0429013U (en) * | 1990-06-29 | 1992-03-09 | ||
WO2001018312A1 (en) * | 1999-09-09 | 2001-03-15 | Heinrich August Schoeller Söhne Gmbh & Co. Kg. | Transparent paper and method for the production thereof |
EP1134314A1 (en) * | 2000-03-16 | 2001-09-19 | Hexcel Composites | Intermediate composite product, manufacturing of such a product and usage as a molding material |
FR2806425A1 (en) * | 2000-03-16 | 2001-09-21 | Hexcel Composites | COMPOSITE INTERMEDIATE PRODUCT, PROCESS FOR PRODUCING SUCH A PRODUCT, AND USE AS A MOLDING MATERIAL |
JPWO2007040125A1 (en) * | 2005-09-30 | 2009-04-16 | 住友ベークライト株式会社 | Manufacturing method of prepreg with carrier, prepreg with carrier, manufacturing method of thin double-sided board, thin double-sided board, and manufacturing method of multilayer printed wiring board |
WO2007040125A1 (en) * | 2005-09-30 | 2007-04-12 | Sumitomo Bakelite Co., Ltd. | Process for producing prepreg with carrier, prepreg with carrier, process for producing thin-type double sided board, thin-type double sided board, and process for producing multilayered printed wiring board |
JP2011132535A (en) * | 2005-09-30 | 2011-07-07 | Sumitomo Bakelite Co Ltd | Manufacturing process for prepreg with carrier, prepreg with carrier, manufacturing process for thin double-sided plate, thin double-sided plate and manufacturing process for multilayer-printed circuit board |
JP4957552B2 (en) * | 2005-09-30 | 2012-06-20 | 住友ベークライト株式会社 | Manufacturing method of prepreg with carrier for printed wiring board, prepreg with carrier for printed wiring board, manufacturing method of thin double-sided board for printed wiring board, thin double-sided board for printed wiring board, and manufacturing method of multilayer printed wiring board |
GB2445937A (en) * | 2006-11-23 | 2008-07-30 | Curon Ltd | Polymer composite |
JP2014079815A (en) * | 2012-10-12 | 2014-05-08 | Shima Seiki Mfg Ltd | Cutting method and cutting device |
WO2014084119A1 (en) * | 2012-11-30 | 2014-06-05 | 三菱重工業株式会社 | Device for manufacturing roll for angled layer, and operating method for device for manufacturing roll for angled layer |
JP2014121796A (en) * | 2012-12-20 | 2014-07-03 | Sanyu Rec Co Ltd | Roll of prepreg, production method of the same, and production device of the same |
CN109070389A (en) * | 2016-04-11 | 2018-12-21 | 三菱化学株式会社 | The manufacturing method of fibre reinforced resin material and the manufacturing device of fibre reinforced resin material |
CN109070389B (en) * | 2016-04-11 | 2021-06-15 | 三菱化学株式会社 | Method for producing fiber-reinforced resin material and apparatus for producing fiber-reinforced resin material |
Also Published As
Publication number | Publication date |
---|---|
JPH07115352B2 (en) | 1995-12-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR920002379B1 (en) | Prepreg and manufacture thereof | |
KR101411169B1 (en) | Reinforced thermoplastic-resin sheet material, reinforced thermoplastic-resin multilayer sheet material, process for producing the same, and reinforced thermoplastic-resin multilayer molded article | |
EP2106900B1 (en) | Mould and method for vacuum assisted resin transfer moulding | |
WO2007119371A1 (en) | Process for manufacturing preform and apparatus therefor | |
US5496602A (en) | Low resin content unidirectional fiber tape | |
JP2020059145A (en) | Laminate device and laminate method of prepreg tape | |
JPH03216307A (en) | Manufacture of prepreg | |
CN112313055A (en) | Prepreg sheet and method for producing same, fiber-reinforced composite material molded article and method for producing same, and method for producing preform | |
EP2403705B1 (en) | Method and kit for manufacturing composite parts | |
JP2004292604A (en) | Continuous production process for strand prepreg | |
JPH03207610A (en) | Manufacture of prepreg | |
JP4086942B2 (en) | Prepreg manufacturing equipment | |
JPH0489209A (en) | Manufacture of prepreg | |
JPS59120420A (en) | Manufacture of prepreg in form of tape | |
JPH03155908A (en) | Manufacture of prepreg | |
JP4000253B2 (en) | Prepreg with carrier sheet and carrier sheet for prepreg | |
JPH03243309A (en) | Manufacture of prepreg | |
JPS60157812A (en) | Manufacture of prepreg bonded with scrim cloth | |
CN112243449A (en) | Ultrathin prepreg sheet and composite material thereof | |
JPH03149230A (en) | Production of prepreg | |
JP3308965B2 (en) | Prepreg | |
JPH0230518A (en) | Continuous manufacturing device of fiber-reinforced composite material | |
JPH03222734A (en) | Unidirectionally arranged reinforcing fiber sheet and manufacture thereof | |
JPH0531839A (en) | Unidirectionally arranged reinforced fiber sheet | |
JPH11114954A (en) | Prepreg taking-up apparatus |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
LAPS | Cancellation because of no payment of annual fees |