JPH0489208A - Manufacture of prepreg - Google Patents
Manufacture of prepregInfo
- Publication number
- JPH0489208A JPH0489208A JP20342790A JP20342790A JPH0489208A JP H0489208 A JPH0489208 A JP H0489208A JP 20342790 A JP20342790 A JP 20342790A JP 20342790 A JP20342790 A JP 20342790A JP H0489208 A JPH0489208 A JP H0489208A
- Authority
- JP
- Japan
- Prior art keywords
- prepreg
- grooves
- laminate
- matrix resin
- reinforcing fibers
- 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.)
- Pending
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 13
- 229920005989 resin Polymers 0.000 claims abstract description 26
- 239000011347 resin Substances 0.000 claims abstract description 26
- 239000011159 matrix material Substances 0.000 claims abstract description 24
- 239000012783 reinforcing fiber Substances 0.000 claims description 30
- 238000010438 heat treatment Methods 0.000 claims description 12
- 238000003825 pressing Methods 0.000 claims description 3
- 239000002131 composite material Substances 0.000 abstract description 9
- 239000000835 fiber Substances 0.000 abstract description 9
- 230000006835 compression Effects 0.000 abstract 3
- 238000007906 compression Methods 0.000 abstract 3
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 238000000465 moulding Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 5
- 229920000049 Carbon (fiber) Polymers 0.000 description 4
- 239000004917 carbon fiber Substances 0.000 description 4
- 238000001723 curing Methods 0.000 description 3
- 239000003822 epoxy resin Substances 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- 229920000647 polyepoxide Polymers 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000013007 heat curing Methods 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- XQUPVDVFXZDTLT-UHFFFAOYSA-N 1-[4-[[4-(2,5-dioxopyrrol-1-yl)phenyl]methyl]phenyl]pyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C(C=C1)=CC=C1CC1=CC=C(N2C(C=CC2=O)=O)C=C1 XQUPVDVFXZDTLT-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 239000013039 cover film Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 239000012784 inorganic fiber Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229920003192 poly(bis maleimide) Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- -1 poron Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229920006337 unsaturated polyester resin Polymers 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Landscapes
- Reinforced Plastic Materials (AREA)
Abstract
Description
【発明の詳細な説明】
上の1
本発明は、マトリクス樹脂と強化繊維とからなるプリプ
レグの製造方法に関し、詳しくはプリプレグを積層して
加熱硬化することにより複合材料成型品を製造するに際
し、積層物界面にボイドの残存のない複合材料成型品を
得ることを可能としたストライプ入りのプリプレグを製
造する方法に関する。DETAILED DESCRIPTION OF THE INVENTION 1. The present invention relates to a method for manufacturing a prepreg made of a matrix resin and reinforcing fibers, and more specifically, when manufacturing a composite material molded product by laminating prepregs and curing them by heating, The present invention relates to a method for producing a striped prepreg that makes it possible to obtain a composite material molded product with no residual voids at the object interface.
支匙立旦l
マトリクス樹脂と強化繊維とからなるプリプレグを積層
し、そのプリプレグ積層物を加熱硬化して、複合材料成
型品を製造することが行なわれている。Composite material molded products are manufactured by laminating prepregs made of matrix resin and reinforcing fibers and heating and curing the prepreg laminate.
このようなプリプレグによる複合材料成型品の製造法で
は、積層したプリプレグ同士の界面、即ちプリプレグ積
層物界面に挟まれた空気がボイドとして残存するので、
これを防止するためにプリプレグ積層物を例えばオート
クレーブ中で真空弓きすることにより、プリプレグ積層
物界面から空気を除去し、次いでオートクレーブ中で外
圧を作用させてプリプレグ同士の界面の空気が除去され
た空洞を潰して密着させながら、積層物を加熱硬化する
ことが行なわれる。In this method of manufacturing composite material molded products using prepregs, air sandwiched between the interfaces between the laminated prepregs, that is, the interfaces of the prepreg laminates, remains as voids.
To prevent this, air is removed from the prepreg laminate interface by, for example, vacuuming the prepreg laminate in an autoclave, and then external pressure is applied in the autoclave to remove air at the interface between the prepregs. The laminate is heated and cured while the cavities are crushed and brought into close contact.
が しようとする
しかしながら、プリプレグという平たく且つ表面が平滑
なシート状物の積層物であるプリプレグ積層物を真空引
きしても、その積層物界面がら空気を除去することは難
しく、積層物界面に空気がボイドとして少なからず残存
する。このため外圧を作用させながらプリプレグ積層物
を加熱硬化しても、得られる複合材料成形品は残存した
ボイドの影響で、強度等の所期の特性を必ずしも十分に
得ることができなかった。However, even if a prepreg laminate, which is a laminate of flat, smooth-surfaced sheets called prepregs, is vacuumed, it is difficult to remove air from the interface of the laminate; remains as a void. For this reason, even if the prepreg laminate is heat-cured while applying external pressure, the resulting composite material molded product cannot always obtain sufficient desired properties such as strength due to the influence of the remaining voids.
そこで本発明者等は、積層物界面にボイドの残存のない
複合材料成形品を得るべく鋭意研究を重ねたところ、プ
リプレグの強化繊維の配列方向に沿った溝をプリプレグ
の少なくとも一方の表面全面にストライプ状に形成して
やれば、これを積層したプリプレグ積層物を真空引きし
たときに、積層物界面の空気を上記溝を通って積層物外
にほぼ完全に除去できると共に、その後の加熱硬化時に
作用させる外圧によって、プリプレグ積層物界面の溝及
び空気が除去された空洞を潰して密着させることができ
、その結果、積層物界面のボイドの残存がない密着が良
好な複合材料成形品を得ることができることが判った。Therefore, the present inventors conducted extensive research in order to obtain a composite material molded product with no residual voids at the interface of the laminate, and found that grooves along the alignment direction of the reinforcing fibers of the prepreg were formed on the entire surface of at least one side of the prepreg. If it is formed into a stripe shape, when the prepreg laminate in which these are laminated is vacuumed, the air at the interface of the laminate can be almost completely removed through the grooves and out of the laminate, and at the same time it can be used during subsequent heat curing. External pressure can be used to crush the grooves and cavities from which air has been removed at the interface of the prepreg laminate, resulting in a composite material molded product with good adhesion and no residual voids at the interface of the laminate. It turns out.
従って本発明の目的は、プリプレグの強化繊維方向の溝
をプリプレグ少なくとも一方の表面全面にストライプ状
に形成したストライプ入りのプリプレグを容易に得るこ
とができる製造方法を提供することである。Therefore, an object of the present invention is to provide a manufacturing method that can easily produce a striped prepreg in which grooves in the direction of the reinforcing fibers of the prepreg are formed in stripes on the entire surface of at least one side of the prepreg.
を するための
上記目的は本発明に係るプリプレグの製造方法にて達成
される。要約すれば本発明は、相対する面の少なくとも
一方にマトリクス樹脂を塗布した1対の離型紙の間に強
化繊維を介挿して、前記1対の離型紙の外側から加熱手
段で加熱すると同時に加圧ローラで加圧することにより
、前記マトリクス樹脂と強化繊維とからなるプリプレグ
を形成するに際し、前記加圧ローラのうちの前記1対の
離型紙の少な(とも一方の外側に配設された加圧ローラ
を、その軸線方向に沿って複数個の段を設けて加圧に使
用することにより、前記プリプレグとして、表面に前記
強化繊維の配列方向にストライプ状に溝を形成したプリ
プレグを得ることを特徴とするプリプレグの製造方法で
ある。The above objects are achieved by the prepreg manufacturing method according to the present invention. In summary, the present invention involves inserting reinforcing fibers between a pair of release papers coated with a matrix resin on at least one of their opposing surfaces, and simultaneously heating the pair of release papers from the outside with a heating means. When forming a prepreg made of the matrix resin and reinforcing fibers by applying pressure with a pressure roller, a small amount of the release paper of the pair of the pressure rollers (both of which are placed on the outside of one A plurality of steps are provided along the axial direction of the roller and used for pressure, thereby obtaining the prepreg having grooves formed in stripes on its surface in the direction in which the reinforcing fibers are arranged. This is a method for manufacturing prepreg.
見通上 以下、本発明の実施例について詳細に説明する。Forecast Examples of the present invention will be described in detail below.
第1図は、本発明の製造方法によって製造されるストラ
イプ入りプリプレグの一例を示す斜視図、第2図は、同
じく横断面図、第3図は、本発明の製造方法の一実施例
を示す説明図である。FIG. 1 is a perspective view showing an example of a striped prepreg manufactured by the manufacturing method of the present invention, FIG. 2 is a cross-sectional view, and FIG. 3 is a diagram showing an example of the manufacturing method of the present invention. It is an explanatory diagram.
第1図及び第2図に示すように、本発明の方法によるス
トライプ入りブリブレグエは、マトリクス樹脂2と強化
繊維3とからなるプリプレグ4の表面の少なくも一方に
、強化繊維3の配列方向に沿ったa5をその全面にスト
ライプ状に形成してなっている。As shown in FIGS. 1 and 2, the striped blob regue according to the method of the present invention is produced by forming a striped blob regue on at least one surface of a prepreg 4 made of a matrix resin 2 and reinforcing fibers 3 along the direction in which the reinforcing fibers 3 are arranged. A5 is formed in stripes on the entire surface.
本発明の方法では、プリプレグ4を製造の際の熱圧部6
で上下の加圧ローラ7a、7bの少なくとも一方に、第
4図に示すように、段8を設けて加圧に使用することに
より、少な(とも一方の表面に溝5を有するプリプレグ
4を形成し、ストライプ入りプリプレグlを得るもので
ある。以下、説明する。In the method of the present invention, the prepreg 4 is produced in a hot pressing section 6.
As shown in FIG. 4, at least one of the upper and lower pressure rollers 7a and 7b is provided with a step 8 and used for pressure, thereby forming a prepreg 4 having grooves 5 on one surface. Then, a striped prepreg L is obtained.This will be explained below.
第3図に示すように、供給ローラ9a、9bからマトリ
クス樹脂2を塗布した上下の離型紙12a、12bが、
マトリクス樹脂2を塗布した面を相対した態様で熱圧部
6に供給され、その上下の離型紙12a、12bのマト
リクス樹脂2の間に強化繊維供給ローラ13から強化繊
維3を供給して、強化繊維3が介挿される。As shown in FIG. 3, upper and lower release papers 12a and 12b coated with matrix resin 2 from supply rollers 9a and 9b are
The reinforcing fibers 3 are supplied from the reinforcing fiber supply roller 13 between the matrix resin 2 of the upper and lower release papers 12a and 12b, and reinforced. Fiber 3 is inserted.
本実施例では、マトリクス樹脂2には硬化剤を配合した
エポキシ樹脂を用い、強化繊維3には炭素繊維を用いた
。尚、上記の離型紙12a、12bのうちの一方は、マ
トリクス樹脂2の塗布を省略することができる。In this example, the matrix resin 2 was an epoxy resin mixed with a curing agent, and the reinforcing fibers 3 were carbon fibers. Incidentally, the application of the matrix resin 2 to one of the release papers 12a and 12b can be omitted.
圧熱部6は、一対の離型紙12a、12bの外側の両方
に配置された上下の加圧ローラ7a、7bと、同じ(外
側の一方又は両方に配置された加熱プレート等の図示し
ない加熱手段とからなっている。The pressure heating section 6 is the same as the upper and lower pressure rollers 7a and 7b arranged on both the outer sides of the pair of release papers 12a and 12b (heating means (not shown) such as a heating plate arranged on one or both of the outer sides). It consists of
上下の離型紙12a、12bのマトリクス樹脂2及びそ
の間に介挿された強化繊維3は、離型紙12a、12b
の外側から上下の加圧ローラ7a、7bにより加圧され
て、強化繊維3にマトリクス樹脂2が含浸され、又図示
しない加熱手段により加熱されてマトリクス樹脂2が半
硬化され、これによりマトリクス樹脂2と強化繊維3と
からなるプリプレグ4が得られる。The matrix resin 2 of the upper and lower release papers 12a, 12b and the reinforcing fibers 3 inserted therebetween are the release papers 12a, 12b.
Pressure is applied from the outside by upper and lower pressure rollers 7a and 7b to impregnate the reinforcing fibers 3 with the matrix resin 2, and the matrix resin 2 is semi-cured by being heated by a heating means (not shown). A prepreg 4 consisting of the reinforcing fibers 3 and the reinforcing fibers 3 is obtained.
このとき、本発明では、プリプレグ4の少なくとも一方
の表面の全面に強化繊維3の配列方向に溝5をストライ
プ状に形成すべく、上記の加圧ローラ7a、7bのうち
の少なくとも一方の加圧ローラに、その軸線方向に沿っ
て複数個の段を設けている。At this time, in the present invention, in order to form grooves 5 in stripes in the direction in which the reinforcing fibers 3 are arranged on the entire surface of at least one of the prepregs 4, at least one of the pressure rollers 7a and 7b is applied. The roller is provided with a plurality of stages along its axial direction.
本実施例では、第4図に示すように、上の加圧ローラ7
aに軸線方向に複数個の段8を設けている。上の加圧ロ
ーラ7aの段8の凸部8aは、上の離型紙12a上から
マトリクス樹脂2及び強化繊維3を加圧して、その凸部
8aでプリプレグ4の上の表面に強化繊維3の配列方向
に相補的に溝5を形成するためのものである。In this embodiment, as shown in FIG.
A is provided with a plurality of steps 8 in the axial direction. The convex portion 8a of the stage 8 of the upper pressure roller 7a presses the matrix resin 2 and the reinforcing fibers 3 from above the upper release paper 12a, and the convex portion 8a applies the reinforcing fibers 3 to the upper surface of the prepreg 4. This is for forming grooves 5 complementary to each other in the arrangement direction.
本実施例では、凸部8aの幅を2〜3mmとし、凹部8
bの幅を0.3〜1mmとしたが、凸部8aの幅、凸部
8a同士の間の凹部8bの幅等は、プリプレグ4に形成
する溝5の幅、溝5の配列ピッチ等及びマトリクス樹脂
2の種類、強化繊維3の配列密度等により適宜決定すれ
ばよい。In this embodiment, the width of the convex portion 8a is 2 to 3 mm, and the concave portion 8a has a width of 2 to 3 mm.
Although the width of b is set to 0.3 to 1 mm, the width of the convex portions 8a, the width of the concave portions 8b between the convex portions 8a, etc. are determined by the width of the grooves 5 formed in the prepreg 4, the arrangement pitch of the grooves 5, etc. It may be determined as appropriate depending on the type of matrix resin 2, the arrangement density of reinforcing fibers 3, etc.
本実施によれば、プリプレグ4の表面に上の加圧ローラ
7aの段8の凸部8aで相補的に溝5が形成され、これ
によりプリプレグ4の上の表面全面に強化繊維3の配列
方向に溝5をストライプ状に形成した、マトリクス樹脂
2をエポキシ樹脂とし、強化繊維3を炭素繊維としたス
トライプ入りプリプレグ1が容易に得られる。According to this embodiment, the grooves 5 are formed on the surface of the prepreg 4 in a complementary manner by the convex portions 8a of the steps 8 of the upper pressure roller 7a, so that the grooves 5 are formed on the entire surface of the prepreg 4 in the direction in which the reinforcing fibers 3 are arranged. A striped prepreg 1 in which grooves 5 are formed in striped shapes, matrix resin 2 is made of epoxy resin, and reinforcing fibers 3 are made of carbon fiber can be easily obtained.
以上のようにしてストライプ入りプリプレグ1が得られ
たならば、その後は、ストライプ入りプリプレグ1上か
ら上の離型紙12aを巻き取りローラ13で巻き取って
除去し、代りに供給ローラ14からカバーフィルム15
をストライプ入りプリプレグ1上に供給して被せ、巻き
取りローラ16で巻き取ればよい。Once the striped prepreg 1 has been obtained in the above manner, the release paper 12a above the striped prepreg 1 is taken up and removed by the winding roller 13, and the cover film 12a is removed from the supply roller 14 instead. 15
It is sufficient to supply the striped prepreg 1 and cover it with the striped prepreg 1, and then wind it up with the winding roller 16.
このようにして得られたストライプ入りブリブレグエに
よれば、これを第5図に示すように溝5を上側にして積
層することにより、そのプリプレグ積層物17を真空引
きする際に、積層したストライプ入りプリプレグ1同士
の界面に挟まれた空気を、溝5を通って積層物17外に
ほぼ完全に除去することができ、又その後の加熱硬化時
に作用させる外圧によって、プリプレグ積層物17の界
面の溝5及び空気が除去された空洞を潰して密着させる
ことができる。従って、積層物界面のボイドの残存がな
い密着が良好な、炭素繊維複合材料成形品を得ることが
できる。According to the striped brimbregue thus obtained, by stacking them with the grooves 5 facing upward as shown in FIG. 5, when the prepreg laminate 17 is evacuated, the striped The air caught between the interfaces between the prepregs 1 can be almost completely removed from the laminate 17 through the grooves 5, and the grooves at the interfaces of the prepreg laminate 17 can be removed by the external pressure applied during subsequent heat curing. 5 and the cavity from which air has been removed can be crushed and brought into close contact. Therefore, it is possible to obtain a carbon fiber composite material molded product with good adhesion and no residual voids at the interface of the laminate.
以上の実施例では、上の加圧ローラ7aに段8を設けた
が、段8を設けるのは下の加圧ローラ7aでも、上下の
加圧ローラ7a、7bの両方でもよく、またその設は方
もこれら加圧ローラ7a、7bの全てでな(、少な(と
も最下流のものに設ければよい。下の加圧ローラ7aに
段8を設けたときには、同様にして、プリプレグ4の下
面に溝5が形成されたストライプ入りプリプレグが得ら
れ、上下の加圧ローラ7a、7bの両方に段8を設けた
ときには、プリプレグ4の上下面に溝5が形成されたス
トライプ入りプリプレグが得られる。In the above embodiment, the step 8 is provided on the upper pressure roller 7a, but the step 8 may be provided on the lower pressure roller 7a or both of the upper and lower pressure rollers 7a and 7b. In addition, it is sufficient to install not only all of these pressure rollers 7a and 7b, but also a small number of them on the most downstream one.When a stage 8 is provided on the lower pressure roller 7a, the prepreg 4 is A striped prepreg with grooves 5 formed on the lower surface is obtained, and when steps 8 are provided on both the upper and lower pressure rollers 7a and 7b, a striped prepreg with grooves 5 formed on the upper and lower surfaces of the prepreg 4 is obtained. It will be done.
又以上では、上下の離型紙12a、12bは両者ともマ
トリクス樹脂2を塗布した場合を示したが、マトリクス
樹脂2は少なくとも一方に塗布されていればよい。Further, in the above description, the case where the matrix resin 2 is applied to both the upper and lower release papers 12a and 12b is shown, but the matrix resin 2 may be applied to at least one of them.
又マトリクス樹脂2としてエポキシ樹脂を使用し、強化
繊維3として炭素繊維を使用した場合を例にとって説明
したが、マトリクス樹脂2として不飽和ポリエステル樹
脂、ポリイミド樹脂、ビスマレイミド樹脂等の熱硬化性
樹脂を使用することができ、強化繊維3としてガラス繊
維、アラミド繊維、ポリエステル繊維等の有機繊維、ポ
ロン等の無機繊維、チタン等の金属繊維或いはそれらの
繊維を同時に使用したハイブリッド繊維を使用すること
ができる。In addition, although the explanation has been given using an example in which epoxy resin is used as the matrix resin 2 and carbon fiber is used as the reinforcing fiber 3, it is also possible to use a thermosetting resin such as an unsaturated polyester resin, polyimide resin, or bismaleimide resin as the matrix resin 2. As the reinforcing fiber 3, organic fibers such as glass fibers, aramid fibers, and polyester fibers, inorganic fibers such as poron, metal fibers such as titanium, or hybrid fibers using these fibers simultaneously can be used. .
光」Lの」L里
以上説明したように、本発明の方法では、相対する面の
少なくとも一方にマトリクス樹脂を塗布した1対の離型
紙の間に強化繊維を介挿して、その1対の離型紙の外側
から加熱手段で加熱すると同時に加圧ローラで加圧する
ことにより、マトリクス樹脂と強化繊維とからなるプリ
プレグを形成するに際し、上記加圧ローラのうちの1対
の離型紙の少なくとも一方の外側に配設された加圧ロー
ラを、その軸線方向に沿って複数個の段を設けて加圧に
使用するので、表面に強化繊維の配列方向に沿った溝を
ストライプ状に形成したストライプ入りプリプレグを容
易に得ることができる。As explained above, in the method of the present invention, reinforcing fibers are inserted between a pair of release papers coated with matrix resin on at least one of their opposing surfaces, and When forming a prepreg made of matrix resin and reinforcing fibers by heating the release paper from the outside with a heating means and at the same time applying pressure with a pressure roller, at least one of the release papers of a pair of the pressure rollers is heated. Since the pressure roller placed on the outside is used for pressure by providing multiple steps along its axial direction, the striped surface has grooves formed in stripes along the direction in which the reinforcing fibers are arranged. Prepreg can be easily obtained.
第1図は、本発明の製造方法によって製造されるストラ
イプ入りプリプレグの一例を示す斜視図である。
第2図は、同じ(横断面図である。
第3図は、本発明の製造方法の一実施例を示す説明図で
ある。
第4図は、第3図の方法で使用する上の加圧ローラを示
す平面図である。
第5図は、本発明に係るストライプ入りプリプレグの積
層物を示す正面図である。
a
:ストライプ入りプリプレグ
:マトリクス樹脂
二強化繊維
ニブリブレグ
:溝
・熱圧部
:上の加圧ローラ
:段
:凸部
ニブリブレグ積層物
復代理人FIG. 1 is a perspective view showing an example of a striped prepreg manufactured by the manufacturing method of the present invention. FIG. 2 is the same cross-sectional view. FIG. 3 is an explanatory view showing one embodiment of the manufacturing method of the present invention. FIG. FIG. 5 is a plan view showing a pressure roller. FIG. 5 is a front view showing a laminate of striped prepreg according to the present invention. Upper pressure roller: Step: Convex part nibble leg laminate agent
Claims (1)
布した1対の離型紙の間に強化繊維を介挿して、前記1
対の離型紙の外側から加熱手段で加熱すると同時に加圧
ローラで加圧することにより、前記マトリクス樹脂と強
化繊維とからなるプリプレグを形成するに際し、前記加
圧ローラのうちの前記1対の離型紙の少なくとも一方の
外側に配設された加圧ローラを、その軸線方向に沿って
複数個の段を設けて加圧に使用することにより、前記プ
リプレグとして、表面に前記強化繊維の配列方向にスト
ライプ状に溝を形成したプリプレグを得ることを特徴と
するプリプレグの製造方法。1) A reinforcing fiber is inserted between a pair of release papers coated with matrix resin on at least one of the opposing surfaces, and
When forming a prepreg made of the matrix resin and reinforcing fibers by heating the pair of release paper from the outside with a heating means and simultaneously applying pressure with a pressure roller, the release paper of the pair of the pressure rollers is heated. By using a pressure roller disposed on the outside of at least one of the surfaces in a plurality of stages along the axial direction of the pressure roller, stripes are formed on the surface of the prepreg in the direction in which the reinforcing fibers are arranged. A prepreg manufacturing method characterized by obtaining a prepreg having grooves formed therein.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20342790A JPH0489208A (en) | 1990-07-31 | 1990-07-31 | Manufacture of prepreg |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20342790A JPH0489208A (en) | 1990-07-31 | 1990-07-31 | Manufacture of prepreg |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0489208A true JPH0489208A (en) | 1992-03-23 |
Family
ID=16473905
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20342790A Pending JPH0489208A (en) | 1990-07-31 | 1990-07-31 | Manufacture of prepreg |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0489208A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002249605A (en) * | 2001-02-26 | 2002-09-06 | Toray Ind Inc | Partially impregnated prepreg |
WO2009133143A1 (en) * | 2008-04-30 | 2009-11-05 | Vestas Wind Systems A/S | A consolidated composite pre-from |
US20100239848A1 (en) * | 2009-03-20 | 2010-09-23 | Jerome Le Corvec | Film and Prepreg with Nanoparticles, Processes of Making Thereof, and Reinforced Component Made Therewith |
GB2483730A (en) * | 2010-10-18 | 2012-03-21 | Gurit Uk Ltd | Prepregs comprising a plurality of dry fibre channels |
US10329696B2 (en) * | 2012-12-21 | 2019-06-25 | Cytec Industries Inc. | Curable prepregs with surface openings |
-
1990
- 1990-07-31 JP JP20342790A patent/JPH0489208A/en active Pending
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002249605A (en) * | 2001-02-26 | 2002-09-06 | Toray Ind Inc | Partially impregnated prepreg |
WO2009133143A1 (en) * | 2008-04-30 | 2009-11-05 | Vestas Wind Systems A/S | A consolidated composite pre-from |
CN102123852A (en) * | 2008-04-30 | 2011-07-13 | 维斯塔斯风力系统有限公司 | A consolidated composite pre-from |
US8986487B2 (en) | 2008-04-30 | 2015-03-24 | Vestas Wind Systems A/S | Consolidated composite pre-form |
US20100239848A1 (en) * | 2009-03-20 | 2010-09-23 | Jerome Le Corvec | Film and Prepreg with Nanoparticles, Processes of Making Thereof, and Reinforced Component Made Therewith |
GB2483730A (en) * | 2010-10-18 | 2012-03-21 | Gurit Uk Ltd | Prepregs comprising a plurality of dry fibre channels |
GB2483730B (en) * | 2010-10-18 | 2012-10-17 | Gurit Uk Ltd | Composite materials |
US10329696B2 (en) * | 2012-12-21 | 2019-06-25 | Cytec Industries Inc. | Curable prepregs with surface openings |
US10821680B2 (en) * | 2012-12-21 | 2020-11-03 | Cytec Industries Inc. | Curable prepregs with surface openings |
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