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JP4067855B2 - Fiber-reinforced resin plate with improved bending strength in the longitudinal direction - Google Patents

Fiber-reinforced resin plate with improved bending strength in the longitudinal direction Download PDF

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Publication number
JP4067855B2
JP4067855B2 JP2002102044A JP2002102044A JP4067855B2 JP 4067855 B2 JP4067855 B2 JP 4067855B2 JP 2002102044 A JP2002102044 A JP 2002102044A JP 2002102044 A JP2002102044 A JP 2002102044A JP 4067855 B2 JP4067855 B2 JP 4067855B2
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Prior art keywords
fiber
reinforced resin
longitudinal direction
layer
reinforcing
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JP2003291233A (en
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勝 座古
巌 小宮
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FUKUI FIBERTECH CO Ltd
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FUKUI FIBERTECH CO Ltd
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  • Moulding By Coating Moulds (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、いわゆるFRPと呼ばれる繊維強化樹脂製板状物に関し、特に、風力発電用の風車翼として好適に用いられる長手方向に曲げ強度が改善された繊維強化樹脂製板状物に関するものである。
【0002】
【従来の技術】
従来より、風力発電の風車翼やヘリコプターの回転翼、あるいは飛行機の主翼や尾翼などの固定翼には、繊維強化樹脂製板状物が用いられている。中でも、風車翼などの回転翼においては、遠心力と空気抵抗によって、翼の長手方向に大きな曲げ応力が発生する。
【0003】
このため、翼の長手方向における曲げ強度を向上させたものが要求されている。例えば、特開昭64−63132号公報や特開平6−74142号公報においては、翼の長手方向に多くの補強繊維を配列させ、補強繊維によって、長手方向の曲げ強度を向上させる方法が提案されている。しかしながら、補強繊維は、太くても数十デニール程度であり、長手方向の曲げ強度を飛躍的に向上させることは困難であった。
【0004】
【発明が解決しようとする課題】
そこで、本発明者は、長手方向に飛躍的に曲げ強度を向上させた繊維強化樹脂製板状物を得るべく、鋭意検討していたところ、繊維強化樹脂製板状物中に、さらにその長手方向に繊維強化樹脂棒を挿入するという方法に想到した。一般的に、繊維強化樹脂(FRP)は非常に各種強度の高いものであり、FRPを更に何らかの素材で強化しようという発想は生じないものである。しかし、本発明者は、このような常識に反して、FRP中に更にFRPを挿入するという、従来無かった発想を得たのである。そして、この発想を実現すべく研究を重ねたところ、繊維強化樹脂棒をある特定の補強繊維構造体で挟着すれば、容易に、繊維強化樹脂棒を挿入させることができ、長手方向に曲げ強度が改善された繊維強化樹脂製板状物が得られることを見出し、本発明に至ったのである。
【0005】
【課題を解決するための手段】
すなわち、本発明は、所定の間隔を置いて、平行に且つ長手方向に配置された複数本の繊維強化樹脂棒を、その上面及び下面に配置した少なくとも二枚の補強繊維構造体で挟着した後、全体に樹脂を含浸させてなる繊維強化樹脂製板状物であり、該補強繊維構造体の少なくとも一枚は、全補強繊維が一定の方向に引き揃えられた層Aと、全補強繊維が他の一定の方向に引き揃えられた層Bとの少なくとも二層が積層されてなるものであることを特徴とする長手方向に曲げ強度が改善された繊維強化樹脂製板状物に関するものである。
【0006】
本発明で使用する繊維強化樹脂棒1は、従来公知のものが用いられる。繊維強化樹脂棒1の断面形状は任意でよく、例えば、円形、楕円形、四辺形、三角形などでよい。曲げ強度を向上させるのに、最も好ましいのは円形である。
【0007】
繊維強化樹脂棒1は、従来公知の方法で製造される。例えば、ガラス繊維ローヴィングなどの補強繊維束に樹脂を含浸させ、それを樹脂が含浸されたガラス繊維マットに被覆し、その後、加熱成形金型内で成形及び樹脂を硬化させることによって、得ることができる(連続引抜成形法)。補強繊維としては、ガラス繊維の他、炭素繊維なども用いることができる。また、樹脂としては、不飽和ポリエステル樹脂やエポキシ樹脂などを用いることができる。補強繊維と樹脂の重量割合は、一般的には、補強繊維の重量割合の方が多く、補強繊維:樹脂=60〜95:40〜5、程度である。
【0008】
補強繊維構造体2は、繊維強化樹脂棒1の上面及び下面に配置されて、繊維強化樹脂棒1を挟着するから、少なくとも二枚必要である。この二枚のうち少なくとも一枚は、全補強繊維が一定の方向に引き揃えられた層Aと、全補強繊維が他の一定の方向に引き揃えられた層Bとの少なくとも二層が積層されてなるものである。このような補強繊維構造体2は、特に、LIBA社製の「COPCENTRA MAX 3 CNC」なる装置(図3)や、マイヤー社製の「マルチアクシャルモデル14024」なる装置で製造することができる。これらの装置を用いれば、一定の方向に配列した補強繊維層Aと、他の一定の方向に配列した補強繊維層Bとが積層された補強繊維構造体2を容易に得ることができる。図3に記載した例では、四箇所から補強繊維が供給されており、長手方向に配列した補強繊維層と、幅方向の配列した補強繊維層と、長手方向に対して左45°(+45°)の方向に配列した補強繊維層と、長手方向に対して右45°(−45°)の方向に配列した補強繊維層とが積層されてなる四層の補強繊維構造体2が得られている。なお、図3の装置で、補強繊維の供給箇所を増加させれば、さらに多層の補強繊維構造体も得られるし、補強繊維の供給箇所を減少させれば、二層又は三層の補強繊維構造体も得られる。このような補強繊維構造体2と併用しうる他の補強繊維構造体としては、従来公知のものが用いられる。例えば、補強繊維マットやチョップドストランドマット(所定長に切断された補強繊維を集積したもの)が用いられる。
【0009】
本発明では、特に長手方向に曲げ強度を向上させようというものであるから、長手方向に配列した補強繊維層Aと幅方向の配列した補強繊維層Bとを具備する補強繊維構造体2を用いるのが好ましい。補強繊維層Aによって、長手方向の曲げ強度が若干なりとも向上するからである。また、補強繊維層Aだけでは取り扱いにくいため、補強繊維層Bを積層し、両層A,Bを縫い糸で縫製し、一体化する。縫製の態様は、どのようなものでもよいが、ラッセル編の鎖編糸を編成しながら、一体化してもよい。その他、ミシンによる縫製であってもよい。
【0010】
また、長手方向の曲げ強度の向上は、繊維強化樹脂棒によって十分に達成しうるので、バイヤス方向の曲げ強度を若干なりとも向上させるため、長手方向に対して左45°の方向に配列した補強繊維層Aと長手方向に対して右45°の方向に配列した補強繊維層Bとを具備する補強繊維構造体2を用いるのが好ましい。この両層A,Bによって、両バイヤス方向の曲げ強度を若干なりとも向上させることができるのである。また、両層A,Bを縫い糸によって縫製すれば、一体化され、取り扱いやすくなる。なお、図3に記載した例の如く、四層の補強繊維構造体とすれば、幅方向及び両バイヤス方向のいずれもがほぼ均等に、その曲げ強度が若干向上し、特に幅方向と両バイヤス方向とで、バランスのとれた曲げ強度となるので好ましい。
【0011】
補強繊維構造体2を構成する補強繊維は、ガラス繊維や炭素繊維などが採用される。図3に示した装置で補強繊維構造体を得る場合は、一般的に、ガラス長繊維(ガラス繊維ストランド)や炭素長繊維(炭素繊維ストランド)を集束したローヴィングが用いられる。ガラス繊維などのデニールは任意であり、また、ローヴィングの重量も任意である。なお、併用される他の補強繊維構造体が補強繊維マットやチョップドストランドマットである場合、ガラス繊維や炭素繊維は、一般的に、適宜の長さに切断したものが用いられる。
【0012】
準備された繊維強化樹脂棒1は、その複数本を用いて、図2(i)に示したように、所定の間隔を置いて、補強繊維構造体2上に、平行に且つ長手方向に配置される。次に、図2(ii)に示したように、配置された複数本の繊維強化樹脂棒1,1・・・の上面に、補強繊維構造体2が配置される。この結果、配置された繊維強化樹脂棒1,1・・・の上面及び下面に、補強繊維構造体2,2が配置されることになる。上面及び下面に配置する補強繊維構造体2,2は、同種のものであっても、異種のものであっても良い。また、一般的に、上面及び下面には一枚づつ、すなわち、二枚の補強繊維構造体2,2が配置されるが、例えば、下面に二枚、上面に一枚というように、三枚以上の補強繊維構造体が配置されていても良い。ここで、一枚の補強繊維構造体とは、一枚物として取り扱えるという意味であり、図3で示した装置で製造される多層構造の補強繊維構造体で、層間が縫い糸によって一体化しているものは、全体として一枚という意味である。
【0013】
次に、図2(iii)に示したように、平行に配置された繊維強化樹脂棒1,1間において、補強繊維構造体2,2を縫い糸3で縫製する。図2では、繊維強化樹脂棒1,1・・・間において、縫製箇所が一箇所であるが、例えば二箇所以上を縫い糸3で縫製してもよい。また、図2では、繊維強化樹脂棒1,1・・・間の中間位置で縫製した例を示したが、むしろ、繊維強化樹脂棒1の近傍の両側で縫製するほうが、補強繊維構造体2,2同士が密着しやすくなるため、好ましい。縫い糸3として、従来公知のものが採用されるが、耐熱性や強度の点から、ポリエステル糸を用いるのが好ましい。また、炭素繊維糸やガラス繊維糸を用いることも、好ましいことである。この場合の縫製の態様も任意であるが、例えば、ラッセル編の鎖編糸を編成しながら、あるいはミシンによる縫製で一体化すればよい。以上によって、繊維強化樹脂棒1,1・・・は補強繊維構造体2,2で挟着され、全体が一体化する。
【0014】
繊維強化樹脂棒1,1・・・が補強繊維構造体2,2によって挟着された一体化物には、全体に樹脂を含浸させる。含浸方法は、従来公知の方法で行えばよく、例えば、樹脂浴に浸漬する方法や、樹脂を何度も塗布する方法などが採用される。この樹脂としても、繊維強化樹脂棒1に用いられている樹脂の場合と同様に、不飽和ポリエステル樹脂やエポキシ樹脂などを用いることができる。樹脂の含浸量も任意であるが、一体化物の重量を100重量部とすると、50〜150重量部程度が好ましい。特に、樹脂の含浸量は、一体化物の重量と同程度が最も好ましい。
【0015】
樹脂を含浸させた後、所定の方法で樹脂を硬化させれば、本発明に係る繊維強化樹脂製板状物を得ることができる。ここで、板状物とは、概ね平板状になっているという意味であり、曲面が存在することを否定しているものではない。例えば、風力発電の風車翼やヘリコプターの回転翼が持つ、多数の曲面や捩れが存在していても、概ね平板状であるため、本発明に係る板状物に含まれる。また、飛行機の主翼や尾翼などにも、多数の曲面や捩れが設けられているが、この場合も、同様に本発明に係る板状物に含まれる。
【0016】
【実施例】
以下、本発明を実施例に基づいて説明するが、本発明は実施例に限定されるものではない。
【0017】
実施例
まず、図3に記載した装置を用いて、長手方向に配列した補強繊維層Aと幅方向の配列した補強繊維層Bとを積層し、両層A,Bをポリエステル糸で鎖編糸で編成しながら縫って一体化し、幅1.27mの補強繊維構造体を得た。この際、両層A,Bを作成するのに使用した補強繊維は、ガラス長繊維(ストランド)からなるローヴィング(2.2g/m)である。そして、各層A,Bは、各々433g/m2となるように調整した。
【0018】
一方、連続引抜成形法で得られた繊維強化樹脂丸棒を、10mmの間隔を置いて平行に、かつ、繊維強化樹脂丸棒の長手方向が上記の補強繊維構造体の長手方向と一致するようにして、補強繊維構造体上に配置した。この丸棒は、径が2.95mmであり、その重量は14.64g/mである。そして、補強繊維は、ガラス繊維であり、その含有量は79重量%である。また、樹脂は、熱硬化性不飽和ポリエステル樹脂であって、140℃で加熱硬化させたものである。
【0019】
次に、平行に配置された繊維強化樹脂丸棒の上面に、市販品である目付450g/m2 のチョップドストランドマットを配置した。このチョップドストランドマットは、ガラスストランドを1インチ程度に切断したチョップを堆積し、不飽和ポリエステル樹脂で固めたものである。なお、このチョップドストランドマットも、補強繊維構造体である。
【0020】
以上のようにして、図2(ii)に示した状態とし、その後、繊維強化樹脂丸棒間の一箇所を、ポリエステル糸で鎖編糸を編成しながら縫い、図3記載の装置で得られた補強繊維構造体と、チョップドストランドマットからなる補強繊維構造体とで、平行に配置された繊維強化樹脂丸棒を挟着して、一体化物を得た。この一体化物の重量は、2800g/m2であった。なお、ポリエステル糸は、図3記載の装置で得られた補強繊維構造体の積層を一体化するのにも使用されており、また一体化物を得るのにも使用されているが、全使用量は、20g/m2である。
【0021】
この一体化物に、不飽和ポリエステル樹脂(日本ユピカ社製「5836P−2」)100重量部と、硬化剤であるアセチルアセトンパーオキサイド1重量部とよりなる樹脂組成物を含浸した。樹脂組成物の含浸量は、一体化物100重量部に対して、樹脂組成物が117重量部となるようにした。そして、12〜15℃の雰囲気下で、20分以上放置し、不飽和ポリエステル樹脂を硬化させた。
【0022】
以上のようにして得られた繊維強化樹脂製板状物に関して、その長手方向について、JIS K 7055に規定された3点曲げ試験を行った。その結果、最大応力が238MPaで、弾性係数が6.16GPaであった。
【0023】
比較例
繊維強化樹脂丸棒を使用しない他は、実施例と同様にして一体化物を得た。この一体化物の重量は、1336g/m2であった。そして、この一体化物に、実施例で用いた樹脂組成物を含浸した。含浸量は、一体化物100重量部に対して、樹脂組成物が108重量部となるようにした。その後は、実施例と同様にして不飽和ポリエステル樹脂を硬化させ、繊維強化樹脂製板状物を得た。この繊維強化樹脂製板状物について、実施例と同様の3点曲げ試験を行ったところ、最大応力が181MPaで、弾性係数が3.62GPaであった。
【0024】
実施例で得られた繊維強化樹脂製板状物と、比較例で得られた繊維強化樹脂製板状物とを対比すれば明らかなように、最大応力及び弾性係数共に、実施例の方が高く、長手方向における曲げ強度が向上していることが分かる。
【0025】
【発明の効果】
以上説明したように、本発明に係る繊維強化樹脂製板状物は、その長手方向に、繊維強化樹脂棒が挿入され、一体化されているので、長手方向における曲げ強度を向上させうるという効果を奏する。そして、使用する補強繊維構造体の少なくとも一枚は、全補強繊維が一定の方向に引き揃えれた層Aと、全補強繊維が他の一定の方向に引き揃えられた層Bとの少なくとも二層が積層されてなるものを用いるので、補強繊維構造体の厚みや物性を適宜変更でき、所望の繊維強化樹脂製板状物を得ることができるという効果を奏する。
【0026】
また、本発明に係る繊維強化樹脂製板状物は、少なくとも二枚の補強繊維構造体で繊維強化樹脂棒が挟着され、しかも繊維強化樹脂棒間が縫い糸によって縫製されてなる一体化物に、樹脂含浸すれば、容易に得ることができるものである。すなわち、繊維強化樹脂棒と補強繊維構造体とが一体となっているため、取り扱いやすく、どのような樹脂含浸の方法でも採用することができるという効果を奏する。
【0027】
また、本発明において使用する補強繊維構造体として、全補強繊維が一定の方向に引き揃えれた層Aと、全補強繊維が他の一定の方向に引き揃えられた層Bとの少なくとも二層が積層されてなり、しかも、層Aと層Bとが縫い糸によって縫製されているものを用いれば、補強繊維構造体の厚みや物性をどのように変更しようと、一枚物として取り扱うことができ、所望の繊維強化樹脂製板状物を得ることができるという効果を奏する。
【0028】
また、繊維強化樹脂棒を構成する繊維及び樹脂と、補強繊維構造体を構成する補強繊維、更には最終的に含浸する樹脂として、同種のものを採用すれば、それぞれがより強固に一体化した繊維強化樹脂製板状物が得られるという効果を奏する。例えば、全ての繊維をガラス繊維とし、全ての樹脂をポリエステル不飽和樹脂とすれば、全体がより均質に、より強固に一体化した繊維強化樹脂製板状物が得られるという効果を奏する。
【図面の簡単な説明】
【図1】本発明の一例に係る繊維強化樹脂製板状物の斜視図である。
【図2】本発明の一例に係る繊維強化樹脂製板状物を得る際の手順の一部を示した側面図である。
【図3】本発明に用いる補強繊維構造体を得るのに、最適な装置を示した斜視図である。
【符号の説明】
1 繊維強化樹脂棒
2 補強繊維構造体
3 縫い糸
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a fiber-reinforced resin plate-like material called a so-called FRP, and particularly to a fiber-reinforced resin plate-like material with improved bending strength in the longitudinal direction, which is preferably used as a wind turbine blade for wind power generation. .
[0002]
[Prior art]
Conventionally, fiber-reinforced resin plates are used for wind turbine blades of wind power generation, rotor blades of helicopters, or fixed wings such as main wings and tail wings of airplanes. In particular, in a rotary blade such as a wind turbine blade, a large bending stress is generated in the longitudinal direction of the blade due to centrifugal force and air resistance.
[0003]
For this reason, what improved the bending strength in the longitudinal direction of a wing | blade is requested | required. For example, Japanese Patent Application Laid-Open No. 64-63132 and Japanese Patent Application Laid-Open No. 6-74142 propose a method in which a large number of reinforcing fibers are arranged in the longitudinal direction of the blade and the bending strength in the longitudinal direction is improved by the reinforcing fibers. ing. However, even if the reinforcing fiber is thick, it is about several tens of deniers, and it has been difficult to dramatically improve the bending strength in the longitudinal direction.
[0004]
[Problems to be solved by the invention]
Therefore, the present inventor has intensively studied to obtain a fiber-reinforced resin plate-like material having dramatically improved bending strength in the longitudinal direction. I came up with a method of inserting a fiber-reinforced resin rod in the direction. In general, fiber reinforced resin (FRP) has very high strength, and the idea of further strengthening FRP with some material does not occur. However, the present inventor obtained an idea that did not exist before, such as inserting FRP further into FRP against such common sense. Then, was repeated research to realize this idea, if pinched in particular reinforcing fibrous structure with a fiber-reinforced resin rod readily can Rukoto injects the fiber-reinforced resin rod, in the longitudinal direction The present inventors have found that a fiber-reinforced resin plate having improved bending strength can be obtained, and have reached the present invention.
[0005]
[Means for Solving the Problems]
That is, in the present invention, a plurality of fiber reinforced resin rods arranged in parallel and in the longitudinal direction at predetermined intervals are sandwiched between at least two reinforcing fiber structures arranged on the upper surface and the lower surface thereof. After that, it is a fiber reinforced resin plate made by impregnating the entire resin , and at least one of the reinforcing fiber structures includes a layer A in which all reinforcing fibers are aligned in a certain direction, and all reinforcing fibers. In particular, the present invention relates to a fiber-reinforced resin plate-like material with improved bending strength in the longitudinal direction, wherein at least two layers are laminated with a layer B aligned in another predetermined direction. is there.
[0006]
A conventionally known fiber reinforced resin rod 1 used in the present invention is used. The cross-sectional shape of the fiber reinforced resin rod 1 may be arbitrary, and may be, for example, a circle, an ellipse, a quadrangle, or a triangle. A circular shape is most preferable for improving the bending strength.
[0007]
The fiber reinforced resin rod 1 is manufactured by a conventionally known method. For example, it can be obtained by impregnating a reinforcing fiber bundle such as glass fiber roving with resin, coating it on a glass fiber mat impregnated with resin, and then molding and curing the resin in a thermoforming mold. Yes (continuous pultrusion method). As the reinforcing fiber, carbon fiber or the like can be used in addition to glass fiber. As the resin, an unsaturated polyester resin, an epoxy resin, or the like can be used. The weight ratio of the reinforcing fiber and the resin is generally larger than the weight ratio of the reinforcing fiber, and is about reinforcing fiber: resin = 60 to 95:40 to 5.
[0008]
Since the reinforcing fiber structure 2 is disposed on the upper and lower surfaces of the fiber reinforced resin rod 1 and sandwiches the fiber reinforced resin rod 1, at least two sheets are necessary. At least one of the two sheets is formed by laminating at least two layers of a layer A in which all the reinforcing fibers are aligned in a certain direction and a layer B in which all the reinforcing fibers are aligned in another certain direction. It will be. Such a reinforced fiber structure 2 can be manufactured by a device called “COPCENTRA MAX 3 CNC” manufactured by LIBA (FIG. 3) or a device called “multi-axial model 14024” manufactured by Meyer. By using these apparatuses, it is possible to easily obtain the reinforcing fiber structure 2 in which the reinforcing fiber layer A arranged in a certain direction and the reinforcing fiber layer B arranged in another certain direction are laminated. In the example shown in FIG. 3, the reinforcing fibers are supplied from four locations, the reinforcing fiber layers arranged in the longitudinal direction, the reinforcing fiber layers arranged in the width direction, and 45 ° to the left (+ 45 °) with respect to the longitudinal direction. ), And a four-layer reinforcing fiber structure 2 is obtained by laminating a reinforcing fiber layer arranged in the direction of 45 ° to the right (−45 °) with respect to the longitudinal direction. Yes. If the number of reinforcing fiber supply points is increased in the apparatus of FIG. 3, a multilayer reinforcing fiber structure can be obtained, and if the number of reinforcing fiber supply points is decreased, two or three layers of reinforcing fiber structures can be obtained. A structure is also obtained. A conventionally well-known thing is used as another reinforcing fiber structure which can be used together with such a reinforcing fiber structure 2 . For example, a reinforcing fiber mat or a chopped strand mat (a collection of reinforcing fibers cut into a predetermined length) is used.
[0009]
In the present invention, since the bending strength is particularly improved in the longitudinal direction, the reinforcing fiber structure 2 including the reinforcing fiber layer A arranged in the longitudinal direction and the reinforcing fiber layer B arranged in the width direction is used. Is preferred. This is because the reinforcing fiber layer A improves the bending strength in the longitudinal direction even slightly. Further, since the reinforcing fiber layer A alone is difficult to handle, the reinforcing fiber layer B is laminated, and both layers A and B are sewn with sewing threads and integrated. Any manner of sewing may be used, but they may be integrated while knitting a chain yarn of Russell knitting. In addition, it may be sewn with a sewing machine.
[0010]
Further, since the improvement in the bending strength in the longitudinal direction can be sufficiently achieved by the fiber reinforced resin rod, in order to improve the bending strength in the bias direction to some extent, the reinforcement arranged in the direction of 45 ° to the left with respect to the longitudinal direction. It is preferable to use the reinforcing fiber structure 2 including the fiber layer A and the reinforcing fiber layer B arranged in the direction of 45 ° to the right with respect to the longitudinal direction. The two layers A and B can improve the bending strength in both bias directions to some extent. Moreover, if both layers A and B are sewn with a sewing thread, they are integrated and easy to handle. As in the example shown in FIG. 3, when the four-layer reinforcing fiber structure is used, the bending strength is slightly improved in both the width direction and the both bias directions, and the width direction and the both biases are particularly improved. The bending strength is balanced depending on the direction, which is preferable.
[0011]
Glass fiber, carbon fiber, etc. are employ | adopted for the reinforcing fiber which comprises the reinforcing fiber structure 2. FIG. When the reinforcing fiber structure is obtained with the apparatus shown in FIG. 3, generally, a rowing in which long glass fibers (glass fiber strands) or long carbon fibers (carbon fiber strands) are bundled is used. Deniers such as glass fiber are optional, and the weight of the rowing is also optional. In addition, when the other reinforcing fiber structure used together is a reinforcing fiber mat or a chopped strand mat, the glass fiber or carbon fiber is generally cut to an appropriate length.
[0012]
The prepared fiber reinforced resin rods 1 are arranged in parallel and in the longitudinal direction on the reinforcing fiber structure 2 at a predetermined interval as shown in FIG. Is done. Next, as shown in FIG. 2 (ii), the reinforcing fiber structure 2 is disposed on the upper surfaces of the plurality of disposed fiber reinforced resin rods 1, 1. As a result, the reinforcing fiber structures 2, 2 are arranged on the upper and lower surfaces of the arranged fiber reinforced resin rods 1, 1,. The reinforcing fiber structures 2 and 2 arranged on the upper surface and the lower surface may be the same type or different types. In general, two reinforcing fiber structures 2 and 2 are arranged on the upper surface and the lower surface, that is, two reinforcing fiber structures 2 and 2, for example, three on the lower surface and one on the upper surface. The above reinforcing fiber structure may be arranged. Here, a single reinforcing fiber structure means that it can be handled as a single piece, and is a multilayered reinforcing fiber structure manufactured by the apparatus shown in FIG. 3, and the layers are integrated by sewing threads. A thing means one piece as a whole.
[0013]
Next, as shown in FIG. 2 (iii), the reinforcing fiber structures 2 and 2 are sewn with the sewing thread 3 between the fiber reinforced resin rods 1 and 1 arranged in parallel. In FIG. 2, there is one sewing location between the fiber reinforced resin rods 1, 1..., For example, two or more locations may be sewn with the sewing thread 3. 2 shows an example in which sewing is performed at an intermediate position between the fiber reinforced resin rods 1, 1..., Rather, the reinforcing fiber structure 2 is sewn on both sides in the vicinity of the fiber reinforced resin rod 1. , 2 are easy to adhere to each other, which is preferable. A conventionally known sewing thread 3 is used as the sewing thread 3, but a polyester thread is preferably used from the viewpoint of heat resistance and strength. It is also preferable to use carbon fiber yarn or glass fiber yarn. The manner of sewing in this case is also arbitrary. For example, it may be integrated while knitting a chain stitch yarn of Russell knitting or by sewing with a sewing machine. As described above, the fiber reinforced resin rods 1, 1... Are sandwiched between the reinforcing fiber structures 2 and 2, and the whole is integrated.
[0014]
The integrated product in which the fiber reinforced resin rods 1, 1... Are sandwiched between the reinforcing fiber structures 2 and 2 is impregnated with resin. The impregnation method may be performed by a conventionally known method. For example, a method of immersing in a resin bath or a method of applying a resin many times is adopted. As this resin, similarly to the case of the resin used for the fiber reinforced resin rod 1, an unsaturated polyester resin, an epoxy resin, or the like can be used. The amount of resin impregnation is also arbitrary, but if the weight of the integrated product is 100 parts by weight, it is preferably about 50 to 150 parts by weight. In particular, the resin impregnation amount is most preferably about the same as the weight of the integrated product.
[0015]
If the resin is cured by a predetermined method after impregnating the resin, the fiber-reinforced resin plate-like material according to the present invention can be obtained. Here, the plate-like object means that the plate-like object is substantially flat, and does not deny that a curved surface exists. For example, even if there are a large number of curved surfaces and twists of wind turbine blades of wind power generation and helicopter rotor blades, they are almost flat and are included in the plate-like object according to the present invention. In addition, a large number of curved surfaces and twists are provided on the main wing and tail wing of an airplane, and this case is also included in the plate-like object according to the present invention.
[0016]
【Example】
EXAMPLES Hereinafter, although this invention is demonstrated based on an Example, this invention is not limited to an Example.
[0017]
Example First, by using the apparatus shown in FIG. 3, the reinforcing fiber layer A arranged in the longitudinal direction and the reinforcing fiber layer B arranged in the width direction were laminated, and both layers A and B were chain-knitted with polyester yarn. And sewed and integrated to obtain a reinforcing fiber structure having a width of 1.27 m. At this time, the reinforcing fibers used to prepare both layers A and B are rowing (2.2 g / m) made of long glass fibers (strands). And each layer A and B was adjusted so that it might become 433 g / m < 2 >, respectively.
[0018]
On the other hand, the fiber reinforced resin round bars obtained by the continuous pultrusion method are parallel to each other with an interval of 10 mm, and the longitudinal direction of the fiber reinforced resin round bars coincides with the longitudinal direction of the reinforcing fiber structure. Then, it was arranged on the reinforcing fiber structure. This round bar has a diameter of 2.95 mm and a weight of 14.64 g / m. The reinforcing fiber is a glass fiber, and its content is 79% by weight. The resin is a thermosetting unsaturated polyester resin that is heat-cured at 140 ° C.
[0019]
Next, a commercially available chopped strand mat having a basis weight of 450 g / m @ 2 was placed on the upper surface of the fiber reinforced resin round bars arranged in parallel. This chopped strand mat is obtained by depositing chops obtained by cutting glass strands into about 1 inch and hardening them with unsaturated polyester resin. This chopped strand mat is also a reinforcing fiber structure.
[0020]
As described above, the state shown in FIG. 2 (ii) is obtained, and then one point between the fiber reinforced resin round bars is sewn while knitting a chain knitting yarn with a polyester yarn, and is obtained by the apparatus shown in FIG. The fiber reinforced resin round bars arranged in parallel were sandwiched between the reinforced fiber structure and the reinforced fiber structure made of the chopped strand mat to obtain an integrated product. The weight of this integrated product was 2800 g / m 2 . The polyester yarn is also used to integrate the laminated reinforcing fiber structure obtained by the apparatus shown in FIG. 3, and is also used to obtain an integrated product. Is 20 g / m 2 .
[0021]
This integrated product was impregnated with a resin composition composed of 100 parts by weight of an unsaturated polyester resin (“5836P-2” manufactured by Nippon Iupika Co., Ltd.) and 1 part by weight of acetylacetone peroxide as a curing agent. The impregnation amount of the resin composition was such that the resin composition was 117 parts by weight with respect to 100 parts by weight of the integrated product. And it was left to stand for 20 minutes or more in 12-15 degreeC atmosphere, and the unsaturated polyester resin was hardened.
[0022]
A three-point bending test defined in JIS K 7055 was performed on the longitudinal direction of the fiber-reinforced resin plate-like material obtained as described above. As a result, the maximum stress was 238 MPa and the elastic modulus was 6.16 GPa.
[0023]
Comparative Example An integrated product was obtained in the same manner as in Example except that the fiber reinforced resin round bar was not used. The weight of this integrated product was 1336 g / m 2 . Then, this integrated product was impregnated with the resin composition used in the examples. The amount of impregnation was such that the resin composition was 108 parts by weight with respect to 100 parts by weight of the integrated product. Thereafter, the unsaturated polyester resin was cured in the same manner as in the Example to obtain a fiber-reinforced resin plate. When this fiber reinforced resin plate was subjected to the same three-point bending test as in the example, the maximum stress was 181 MPa and the elastic modulus was 3.62 GPa.
[0024]
As is clear from the comparison between the fiber reinforced resin plate obtained in the example and the fiber reinforced resin plate obtained in the comparative example, both the maximum stress and the elastic modulus of the example are better. It can be seen that the bending strength in the longitudinal direction is high.
[0025]
【The invention's effect】
As described above, since the fiber reinforced resin plate-like product according to the present invention has a fiber reinforced resin rod inserted and integrated in the longitudinal direction, the bending strength in the longitudinal direction can be improved. Play. At least one of the reinforcing fiber structures to be used is at least two layers of a layer A in which all the reinforcing fibers are aligned in a certain direction and a layer B in which all the reinforcing fibers are aligned in another certain direction. Therefore, the thickness and physical properties of the reinforcing fiber structure can be changed as appropriate, and the desired fiber-reinforced resin plate-like product can be obtained.
[0026]
Further, the fiber-reinforced resin plate according to the present invention is an integrated product in which a fiber-reinforced resin rod is sandwiched between at least two reinforcing fiber structures, and the fiber-reinforced resin rod is sewn with a sewing thread. If it is impregnated with a resin, it can be easily obtained. That is, since the fiber-reinforced resin rod and the reinforcing fiber structure are integrated, it is easy to handle, and any resin impregnation method can be employed.
[0027]
Further, as the reinforcing fiber structure used in the present invention, there are at least two layers of a layer A in which all reinforcing fibers are aligned in a certain direction and a layer B in which all reinforcing fibers are aligned in another certain direction. If the layer A and the layer B are sewn with sewing threads, they can be handled as a single piece regardless of how the thickness and physical properties of the reinforcing fiber structure are changed. The desired fiber-reinforced resin plate can be obtained.
[0028]
In addition, if the same type is used as the fiber and resin constituting the fiber reinforced resin rod, the reinforcing fiber constituting the reinforcing fiber structure, and finally the resin to be impregnated, each is more firmly integrated. There is an effect that a fiber-reinforced resin plate-like material is obtained. For example, if all the fibers are glass fibers and all the resins are polyester unsaturated resins, it is possible to obtain a fiber-reinforced resin plate-like product that is more uniformly integrated as a whole.
[Brief description of the drawings]
FIG. 1 is a perspective view of a fiber-reinforced resin plate according to an example of the present invention.
FIG. 2 is a side view showing a part of a procedure for obtaining a fiber-reinforced resin plate according to an example of the present invention.
FIG. 3 is a perspective view showing an optimum apparatus for obtaining a reinforcing fiber structure used in the present invention.
[Explanation of symbols]
1 Fiber reinforced resin rod 2 Reinforced fiber structure 3 Sewing thread

Claims (7)

所定の間隔を置いて、平行に且つ長手方向に配置された複数本の繊維強化樹脂棒を、その上面及び下面に配置した少なくとも二枚の補強繊維構造体で挟着した後、全体に樹脂を含浸させてなる繊維強化樹脂製板状物であり、該補強繊維構造体の少なくとも一枚は、全補強繊維が一定の方向に引き揃えられた層Aと、全補強繊維が他の一定の方向に引き揃えられた層Bとの少なくとも二層が積層されてなるものであることを特徴とする長手方向に曲げ強度が改善された繊維強化樹脂製板状物。After sandwiching a plurality of fiber reinforced resin rods arranged in parallel and in the longitudinal direction at a predetermined interval with at least two reinforcing fiber structures arranged on the upper surface and the lower surface thereof, the resin is entirely added. It is a fiber reinforced resin plate impregnated , and at least one of the reinforcing fiber structures includes a layer A in which all reinforcing fibers are aligned in a certain direction, and all reinforcing fibers are in another certain direction. A fiber-reinforced resin plate having improved bending strength in the longitudinal direction, wherein at least two layers of the layer B and the layer B aligned in the above are laminated . 隣り合う繊維強化樹脂棒間で、少なくとも二枚の補強繊維構造体が縫い糸によって縫製されて、該繊維強化樹脂棒を挟着している請求項1記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。  2. A fiber with improved bending strength in the longitudinal direction according to claim 1, wherein at least two reinforcing fiber structures are sewn with sewing threads between adjacent fiber reinforced resin rods, and the fiber reinforced resin rods are sandwiched between the fibers. Reinforced resin plate. 層Aを構成する補強繊維は、長手方向に引き揃えられており、層Bを構成する補強繊維は、幅方向に引き揃えられている請求項記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。Fiber reinforced fibers constituting the layer A is being aligned in the longitudinal direction, the reinforcing fibers constituting the layer B, which is improved longitudinal bending strength according to claim 1, wherein are aligned in the width direction Reinforced resin plate. 層Aを構成する補強繊維は、長手方向に対して+45°の方向に引き揃えられており、層Bを構成する補強繊維は、長手方向に対して−45°の方向に引き揃えられている請求項記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。The reinforcing fibers constituting the layer A are aligned in the + 45 ° direction with respect to the longitudinal direction, and the reinforcing fibers constituting the layer B are aligned in the −45 ° direction with respect to the longitudinal direction. A fiber-reinforced resin plate-like product having improved bending strength in the longitudinal direction according to claim 1 . 層Aと層Bとが縫い糸によって縫製されている請求項記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。Fiber-reinforced resin plate-like workpiece in the longitudinal direction of the bending strength is improved according to claim 1 wherein in which a layer A and layer B is sewn by sewing thread. 繊維強化樹脂棒に含有されている繊維がガラス繊維であり、補強繊維構造体を構成する繊維もガラス繊維である請求項1記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。  2. The fiber-reinforced resin plate-like product with improved bending strength in the longitudinal direction according to claim 1, wherein the fibers contained in the fiber-reinforced resin rod are glass fibers, and the fibers constituting the reinforcing fiber structure are also glass fibers. . 繊維強化樹脂棒中の樹脂は不飽和ポリエステル樹脂が硬化したものであり、全体に含浸させた樹脂も不飽和ポリエステル樹脂である請求項1記載の長手方向に曲げ強度が改善された繊維強化樹脂製板状物。  The resin in the fiber reinforced resin rod is obtained by curing an unsaturated polyester resin, and the resin impregnated throughout is also an unsaturated polyester resin. The fiber reinforced resin with improved bending strength in the longitudinal direction according to claim 1 Plate.
JP2002102044A 2002-04-04 2002-04-04 Fiber-reinforced resin plate with improved bending strength in the longitudinal direction Expired - Fee Related JP4067855B2 (en)

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