JP4277971B2 - How to unpack carbon fiber bundles - Google Patents

How to unpack carbon fiber bundles Download PDF

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Publication number
JP4277971B2
JP4277971B2 JP2001039587A JP2001039587A JP4277971B2 JP 4277971 B2 JP4277971 B2 JP 4277971B2 JP 2001039587 A JP2001039587 A JP 2001039587A JP 2001039587 A JP2001039587 A JP 2001039587A JP 4277971 B2 JP4277971 B2 JP 4277971B2
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Japan
Prior art keywords
carbon fiber
fiber bundle
bobbin
unwinding
winding
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JP2001039587A
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JP2002241051A (en
Inventor
和江 大内
正孝 杉山
知明 田中
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Sakai Composites Corp
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Sakai Composites Corp
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2301/00Handling processes for sheets or webs
    • B65H2301/50Auxiliary process performed during handling process
    • B65H2301/51Modifying a characteristic of handled material
    • B65H2301/514Modifying physical properties
    • B65H2301/5143Warming
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00Handled material; Storage means
    • B65H2701/30Handled filamentary material
    • B65H2701/31Textiles threads or artificial strands of filaments
    • B65H2701/314Carbon fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00Handled material; Storage means
    • B65H2701/50Storage means for webs, tapes, or filamentary material
    • B65H2701/52Integration of elements inside the core or reel
    • B65H2701/528Heating or cooling devices

Description

【0001】
【発明の属する技術分野】
本発明は炭素繊維束の解舒方法に関し、さらに詳しくはサイジング剤で処理された炭素繊維束を巻いた巻糸ボビンから、その炭素繊維束を解舒する際に糸切れや毛羽立ちを低減可能にする解舒方法に関する。
【0002】
【従来の技術】
炭素繊維は、繊維強化樹脂(CFRP)などの複合材を形成又は製造するときの補強材として広く使用されている。一般に炭素繊維束は、製造工程で巻糸ボビンに巻き上げられるとき、繊維強化樹脂のマトリックス樹脂との界面接着性を向上させるためや、収束性を向上させるため、サイジング剤によって予め表面処理されてから巻き取られている。
【0003】
そのサイジング剤は、エポキシ樹脂などの比較的低分子量の未硬化熱硬化性樹脂を主剤として構成されているが、常温で粘着性を有しているため、炭素繊維束が巻糸ボビンに巻かれた状態になると巻糸層間に接着現象が生じ、炭素繊維束を解舒するときに高い剥離抵抗を生ずる。他方、炭素繊維束は、複合化される前の裸糸の状態では破断伸度がほとんどゼロに近いため、脆く折れやすいという特性を有している。
【0004】
そのため炭素繊維束は、巻糸ボビンから解舒する際に大きな剥離抵抗を受けると、強い曲げおよび引張り荷重が掛かることにより、糸切れや毛羽立ちを生じやすいという問題がある。生産中に糸切れが発生すると、生産工程の中断を余儀なくされるため稼働率は低下し、また糸切れを継ぐことにより品質低下を招く。また、毛羽立ちは、同様に品質低下の原因になっていた。
【0005】
【発明が解決しようとする課題】
本発明の目的は、巻糸ボビンから解舒する際の糸切れや毛羽立ちを低減可能にする炭素繊維束の解舒方法を提供することにある。
【0006】
【課題を解決するための手段】
本発明の炭素繊維束の解舒方法は、未硬化の熱硬化性樹脂を主剤とするサイジング剤で処理された炭素繊維束を巻いた巻糸ボビンから、該炭素繊維束を解舒して高次工程へ供給する際に、前記巻糸ボビンを加熱しながら解舒するか、又は予熱により保温状態を維持しながら解舒することを特徴とするものである。
【0007】
このように巻糸ボビンから炭素繊維束を解舒する際に巻糸ボビンを加熱するか、或いは予め加熱して保温状態に維持することにより、未硬化熱硬化性樹脂のサイジング剤を軟化状態にする。したがって、炭素繊維束を解舒する時の炭素繊維束相互間の剥離抵抗が低下し、糸切れや毛羽立ちの発生を低減し、操業性の向上と共に、品質向上を可能にすることができる。
【0008】
【発明の実施の形態】
本発明において、炭素繊維束の表面処理に使用されるサイジング剤は、未硬化の熱硬化性樹脂を主剤とする限り、特に種類は限定されない。例えば、エポキシ樹脂、不飽和ポリエステル樹脂、ビニルエステル樹脂などを例示することができる。
【0009】
本発明において、炭素繊維束を解舒する際に行う巻糸ボビンの加熱は、巻糸ボビンを1個ずつを個別に加熱するようにしてもよく、或いは複数本ずつの単位でまとめて加熱するようにしてもよい。この巻糸ボビンの加熱処理により、炭素繊維束に表面処理されていたサイジング剤が軟化状態になり、巻糸層間の剥離抵抗を低減するため、炭素繊維束を解舒する時の糸切れや毛羽立ちを少なくすることができる。このような加熱処理は、予め解舒工程に供する前に巻糸ボビンを加熱し、その予熱によって得られた保温状態を維持しながら解舒するようにしてもよい。
【0010】
上記加熱処理における加熱温度或いは予熱後の保温温度は、40〜90℃の範囲にすることが好ましい。温度が40℃よりも低いと、サイジング剤の軟化が不十分になり、糸切れ防止効果が低減する。また、90℃よりも高温にした場合は、糸切れ防止効果は十分であるが、その効果は飽和状態になるため、加熱エネルギーを余分に消費するというデメリットを生ずる。さらにサイジング剤の硬化反応を惹起されるため、マトリックス樹脂との融和が阻害されるようになり、界面接着性を低下させるデメリットも生ずるようになる。
【0011】
本発明は、炭素繊維束を解舒する工程であれば、特に用途上の適用工程は限定されない。例えば、整経工程などの製織準備工程、製織工程、プリプレグ製造工程、フィラメントワインディング工程、ディッピング(含浸)工程、プルトルージョン(引抜き)工程、ローピング法エクストルージョン(押出し)工程、チョップドファイバーカッティング工程などを例示することができる。
【0012】
図1は、本発明を炭素繊維束の整経工程に適用した場合を例示する。
【0013】
図1において、1はサイジング剤で表面処理された炭素繊維束Yが巻き上げられた巻糸ボビンであり、多数個の巻糸ボビン1が多列多段にクリールスタンド2に懸架されている。サイジング剤には、エポキシ樹脂等の未硬化熱硬化性樹脂を主剤とするものが使用されている。3は整経ドラムであり、この整経ドラム3が回転駆動されることにより、多数個の巻糸ボビン1から炭素繊維束Yがそれぞれ解舒され、それら多数本の炭素繊維束Yが一定間隔に平行に並べられて、整経ドラム3に巻き上げられる。
【0014】
クリールスタンド2に多列多段に懸架された多数個の巻糸ボビン1は、透明な樹脂シート4aに囲まれた閉空間4の中に収納されている。閉空間4には上部と下部とに排気口5と供給口6とが設けられ、これらの間に送風機8とヒータ9を連結したダクト7が接続されている。送風機8とヒータ9は、運転状態において、送風機8が閉空間4内の空気を排出口5からダクト7へ吸引し、それをヒータ9が加熱して供給口6から再び閉空間4へ供給するようになっている。このように加熱空気の循環を繰り返すことにより、閉空間4内の多数個の巻糸ボビン1を加熱する。
【0015】
上述のように多数個の巻糸ボビン1から炭素繊維束Yを解舒しながら整経ドラム2に巻き上げるとき、巻糸ボビン1を加熱しながら行っているため、炭素繊維束Yに含浸した表面のサイジング剤が軟化し、その軟化によって巻糸ボビン1上の炭素繊維束Yが相互間の接着力が低下し、小さな解舒張力であっても容易に剥離することができる。したがって、炭素繊維束Yは過度の曲げ荷重を加えられることなく解舒される。したがって、糸切れを発生したり、毛羽立ちを生じたりすることなく、操業性の向上と共に品質を向上することができる。
【0016】
図2は、本発明を炭素繊維の製織工程における緯糸用巻糸ボビンに適用した場合を例示する。
【0017】
緯糸用の巻糸ボビン1は1個だけが閉空間4に収納され、緯入れする毎に一定長さの炭素繊維束Yが巻糸ボビン1から解舒されるようになっている。閉空間4には供給口6から加熱空気が供給され、排気口6から排気されるようになっていて、内部の巻糸ボビン1が常時加熱されるようになっている。
【0018】
この図2の態様の場合にも、炭素繊維束Yは表面のサイジング剤が加熱によって軟化状態になるため、巻糸ボビン1から解舒されるときの剥離抵抗が小さくなり、過度の曲げや引張り荷重を受けることなく小さな解舒張力で解舒される。したがって、糸切れや毛羽を生ずることなく操業性を向上すると共に、品質を向上する。
【0019】
【実施例】
エポキシ樹脂を主剤とするサイジング剤で表面処理した炭素繊維束(弾性率230GPa、引張強度3,530MPa)が巻き上げられた巻糸ボビンを複数本使用し、解舒速度120m/分で解舒しながら整経ドラムに巻き上げる整経を行うに当たり、図1の装置を使用して、閉空間に70℃の加熱空気を供給して巻糸ボビンを加熱する場合(実施例)と、加熱空気は供給せずに温度20℃の常温状態にした場合(比較例)とで、工程中の糸切れ発生回数を調べた。
【0020】
その結果、本発明の実施例では、糸切れが全く発生しなかったが、比較例の方法では、40回/105 mの糸切れを発生した。
【0021】
【発明の効果】
上述したように本発明によれば、炭素繊維束を解舒するとき巻糸ボビンを加熱するか、或いは予め加熱して保温状態にするため、サイジング剤が軟化状態になることによって炭素繊維束相互間の剥離抵抗を低減させ、炭素繊維束に無理な曲げ荷重を掛けることなく容易に解舒することが可能になる。したがって、解舒時の糸切れを発生せず、かつ毛羽立ちの発生も低減することができる。
【図面の簡単な説明】
【図1】本発明を実施する整経工程の一例を示す概略図である。
【図2】本発明を実施する製織工程の緯糸用巻糸ボビンの部分を示す概略図である。
【符号の説明】
1 巻糸ボビン
2 クリールスタンド
3 整経ドラム
4 閉空間
5 排気口
6 供給口
7 ダクト
8 送風機
9 ヒータ
F 炭素繊維束
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a method for unwinding a carbon fiber bundle, and more particularly, from a wound bobbin wound with a carbon fiber bundle treated with a sizing agent, when the carbon fiber bundle is unwound, thread breakage and fluffing can be reduced. It relates to the method of unraveling.
[0002]
[Prior art]
Carbon fiber is widely used as a reinforcing material when forming or manufacturing a composite material such as fiber reinforced resin (CFRP). In general, when a carbon fiber bundle is wound around a bobbin in a manufacturing process, it is subjected to a surface treatment in advance with a sizing agent in order to improve the interfacial adhesion with the matrix resin of the fiber reinforced resin or to improve the convergence. It is wound up.
[0003]
The sizing agent is mainly composed of an uncured thermosetting resin having a relatively low molecular weight such as an epoxy resin. However, since the sizing agent has adhesiveness at room temperature, a carbon fiber bundle is wound around a winding bobbin. In this state, an adhesion phenomenon occurs between the winding layers, and a high peeling resistance is generated when the carbon fiber bundle is unwound. On the other hand, the carbon fiber bundle has a characteristic that it is brittle and easily broken because the elongation at break is almost zero in the state of the bare yarn before being combined.
[0004]
For this reason, when the carbon fiber bundle is subjected to a large peeling resistance when unwound from the bobbin, there is a problem that yarn breakage and fluff are likely to occur due to strong bending and tensile loads. When yarn breakage occurs during production, the production process is forced to be interrupted, so the operating rate is lowered, and the quality is lowered by continuing the yarn breakage. In addition, fluffing was a cause of quality degradation.
[0005]
[Problems to be solved by the invention]
An object of the present invention is to provide a carbon fiber bundle unwinding method that can reduce yarn breakage and fluffing when unwinding from a wound bobbin.
[0006]
[Means for Solving the Problems]
The method for unwinding the carbon fiber bundle of the present invention comprises unwinding the carbon fiber bundle from a wound bobbin wound with a carbon fiber bundle treated with a sizing agent mainly composed of an uncured thermosetting resin. When supplying to the next step, the winding bobbin is unwound while being heated, or unwound while maintaining a heat-retaining state by preheating.
[0007]
Thus, when unwinding the carbon fiber bundle from the bobbin bobbin, the bobbin bobbin is heated, or preheated and maintained in a heat retaining state, so that the uncured thermosetting resin sizing agent is softened. To do. Accordingly, the peeling resistance between the carbon fiber bundles when the carbon fiber bundle is unwound is reduced, the occurrence of yarn breakage and fluffing is reduced, and the operability is improved and the quality can be improved.
[0008]
DETAILED DESCRIPTION OF THE INVENTION
In the present invention, the type of the sizing agent used for the surface treatment of the carbon fiber bundle is not particularly limited as long as an uncured thermosetting resin is a main component. For example, an epoxy resin, an unsaturated polyester resin, a vinyl ester resin, etc. can be illustrated.
[0009]
In the present invention, the heating of the bobbin that is performed when the carbon fiber bundle is unwound may be performed by heating the bobbins one by one or by heating in units of a plurality of units. You may do it. This heat treatment of the bobbin bobbin softens the sizing agent that has been surface-treated on the carbon fiber bundle, and reduces the peeling resistance between the winding layers. Can be reduced. In such a heat treatment, the bobbin bobbin may be heated in advance before being subjected to the unwinding step, and unwinding while maintaining the heat retaining state obtained by the preheating.
[0010]
It is preferable that the heating temperature in the heat treatment or the warming temperature after preheating is in the range of 40 to 90 ° C. When temperature is lower than 40 degreeC, the softening of a sizing agent will become inadequate and the thread breakage prevention effect will reduce. Further, when the temperature is higher than 90 ° C., the yarn breakage preventing effect is sufficient, but since the effect is saturated, there is a demerit that extra heating energy is consumed. Furthermore, since the curing reaction of the sizing agent is induced, the compatibility with the matrix resin is hindered, and there is a disadvantage that the interfacial adhesion is lowered.
[0011]
As long as the present invention is a process of unwinding a carbon fiber bundle, the application process in particular is not limited. For example, weaving preparation process such as warping process, weaving process, prepreg manufacturing process, filament winding process, dipping (impregnation) process, pultrusion (drawing) process, roping method extrusion (extrusion) process, chopped fiber cutting process, etc. It can be illustrated.
[0012]
FIG. 1 illustrates the case where the present invention is applied to a warping process of a carbon fiber bundle.
[0013]
In FIG. 1, reference numeral 1 denotes a winding bobbin on which a carbon fiber bundle Y surface-treated with a sizing agent is wound, and a large number of winding bobbins 1 are suspended on a creel stand 2 in multiple rows and stages. As the sizing agent, one having an uncured thermosetting resin such as an epoxy resin as a main component is used. Reference numeral 3 denotes a warping drum. When the warping drum 3 is rotationally driven, the carbon fiber bundles Y are unwound from a large number of winding bobbins 1, and the carbon fiber bundles Y are spaced at regular intervals. And are wound up on the warping drum 3.
[0014]
A large number of wound bobbins 1 suspended in multiple rows and stages on a creel stand 2 are accommodated in a closed space 4 surrounded by a transparent resin sheet 4a. The closed space 4 is provided with an exhaust port 5 and a supply port 6 at an upper part and a lower part, and a duct 7 connecting a blower 8 and a heater 9 is connected therebetween. In the operating state, the blower 8 and the heater 9 suck the air in the closed space 4 from the discharge port 5 to the duct 7, and the heater 9 heats and supplies the air to the closed space 4 again from the supply port 6. It is like that. By repeating the circulation of the heated air in this way, the multiple bobbins 1 in the closed space 4 are heated.
[0015]
As described above, when the carbon fiber bundle Y is unwound from a large number of the wound bobbins 1 and wound onto the warping drum 2, the surface of the carbon fiber bundle Y impregnated is obtained because the wound bobbin 1 is heated. The sizing agent is softened, and the softening of the carbon fiber bundle Y on the winding bobbin 1 reduces the mutual adhesive force, and can be easily peeled even with a small unwinding tension. Therefore, the carbon fiber bundle Y is unwound without being applied with an excessive bending load. Therefore, it is possible to improve the operability and the quality without causing yarn breakage or fluffing.
[0016]
FIG. 2 illustrates a case where the present invention is applied to a weft bobbin for wefts in a carbon fiber weaving process.
[0017]
Only one winding bobbin 1 for weft is stored in the closed space 4, and a carbon fiber bundle Y having a certain length is unwound from the winding bobbin 1 every time weft insertion. Heated air is supplied to the closed space 4 from the supply port 6 and is exhausted from the exhaust port 6 so that the inner bobbin 1 is constantly heated.
[0018]
In the case of the embodiment of FIG. 2 as well, the carbon fiber bundle Y is softened by heating the surface sizing agent, so that the peel resistance when unwound from the bobbin 1 is reduced, and excessive bending or tension is applied. It is unwound with a small unwinding tension without receiving a load. Accordingly, the operability is improved and the quality is improved without causing yarn breakage or fluff.
[0019]
【Example】
Using a plurality of wound bobbins wound with carbon fiber bundles (elastic modulus 230 GPa, tensile strength 3,530 MPa) surface-treated with a sizing agent mainly composed of an epoxy resin, while unwinding at a unwinding speed of 120 m / min When performing the warping to be wound up on the warping drum, the apparatus shown in FIG. 1 is used to supply heated air at 70 ° C. to the closed space to heat the bobbin bobbin (Example). The number of occurrences of yarn breakage during the process was examined in the case of normal temperature of 20 ° C. (comparative example).
[0020]
As a result, in the examples of the present invention, no yarn breakage occurred, but in the method of the comparative example, yarn breakage of 40 times / 10 5 m occurred.
[0021]
【The invention's effect】
As described above, according to the present invention, when the carbon fiber bundle is unwound, the winding bobbin is heated or preheated so as to be kept warm. It is possible to reduce the peeling resistance between them and easily unwind them without applying an excessive bending load to the carbon fiber bundle. Therefore, yarn breakage during unwinding does not occur and occurrence of fluffing can be reduced.
[Brief description of the drawings]
FIG. 1 is a schematic view showing an example of a warping process for carrying out the present invention.
FIG. 2 is a schematic diagram showing a portion of a weft bobbin for wefts in a weaving process for carrying out the present invention.
[Explanation of symbols]
1 Winding Bobbin 2 Creel Stand 3 Warping Drum 4 Closed Space 5 Exhaust Port 6 Supply Port 7 Duct 8 Blower 9 Heater F Carbon Fiber Bundle

Claims (3)

未硬化の熱硬化性樹脂を主剤とするサイジング剤で処理された炭素繊維束を巻いた巻糸ボビンから、該炭素繊維束を解舒して高次工程へ供給する際に、前記巻糸ボビンを加熱しながら解舒するか、又は予熱により保温状態を維持しながら解舒する炭素繊維束の解舒方法。When winding a carbon fiber bundle treated with a sizing agent mainly composed of an uncured thermosetting resin, the carbon fiber bundle is unwound and supplied to a higher-order process. A method for unwinding a carbon fiber bundle that unwinds while heating or unwinds while maintaining a heat-retaining state by preheating. 前記巻糸ボビンを閉空間内に収納し、該閉空間に加熱気体を供給することにより前記巻糸ボビン条を加熱する請求項1に記載の炭素繊維束の解舒方法。The method for unwinding a carbon fiber bundle according to claim 1, wherein the winding bobbin is housed in a closed space, and the winding bobbin strip is heated by supplying a heating gas to the closed space. 前記巻糸ボビンの加熱温度又は予熱後の保温温度を40〜90℃にする請求項1又は2に記載の炭素繊維束の解舒方法。The method for unwinding a carbon fiber bundle according to claim 1 or 2, wherein a heating temperature of the bobbin bobbin or a heat retaining temperature after preheating is set to 40 to 90 ° C.
JP2001039587A 2001-02-16 2001-02-16 How to unpack carbon fiber bundles Expired - Lifetime JP4277971B2 (en)

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