JPS59108656A - Carbon fiber package - Google Patents

Carbon fiber package

Info

Publication number
JPS59108656A
JPS59108656A JP21424082A JP21424082A JPS59108656A JP S59108656 A JPS59108656 A JP S59108656A JP 21424082 A JP21424082 A JP 21424082A JP 21424082 A JP21424082 A JP 21424082A JP S59108656 A JPS59108656 A JP S59108656A
Authority
JP
Japan
Prior art keywords
yarn
package
carbon fiber
winding
wound
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
Application number
JP21424082A
Other languages
Japanese (ja)
Other versions
JPS6246468B2 (en
Inventor
Ryuichi Yamamoto
隆一 山本
Hironobu Nojiri
博信 野尻
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toray Industries Inc
Original Assignee
Toray Industries Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Toray Industries Inc filed Critical Toray Industries Inc
Priority to JP21424082A priority Critical patent/JPS59108656A/en
Publication of JPS59108656A publication Critical patent/JPS59108656A/en
Publication of JPS6246468B2 publication Critical patent/JPS6246468B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H55/00Wound packages of filamentary material
    • 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

Abstract

PURPOSE:To prevent the windings of a carbon fiber package from collapsing and reduce its fluff and the cuts of its yarn, by winding the yarn so that it has a discrepancy of 50 to 150% of its mean width from the already wound yarn for every one to nine traverses. CONSTITUTION:Before a yarn is wound on a bobbin by a winder, the crossing angle and discrepancy of the yarn on the surface of the bobbin and the winding ratio of the winder are set at predetermined values. The yarn 1 is wound to have a discrepancy of 50 to 150%, preferably 75 to 125%, of the yarn width from the already wound yarn so that a crossing pattern 3 appears on the surface of a package.

Description

【発明の詳細な説明】 本発明は炭素繊維パッケージ、特に巻崩れや解舒時の毛
羽および糸切れの発生が著しく改善された炭素繊維パッ
ケージに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a carbon fiber package, and particularly to a carbon fiber package in which the occurrence of fluff and thread breakage during unrolling and unwinding is significantly improved.

今日、炭素繊維は樹脂あるいは金楓などからなるマトリ
ックスと一体化せしめ複合材料金成形する基材として注
目され、斯様な複合材料は実用化の段階に座す達したと
いえるが、この炭素繊維は、今日、その原材料としてア
クリロニトリル系繊維あるいは通常ピッチ系繊維と称さ
れる繊維を用いたものが、その主流となっており、これ
らの繊維は酸化性雰囲気下で焼成し、次いで不活性雰囲
気下で加熱炭素化せしめるのが通例である。
Today, carbon fiber is attracting attention as a base material for forming composite materials by integrating it with a matrix made of resin or gold maple, etc., and it can be said that such composite materials have reached the stage of practical application. Today, the mainstream is to use acrylonitrile fibers or pitch fibers as raw materials, and these fibers are fired in an oxidizing atmosphere and then heated in an inert atmosphere. It is customary to carbonize by heating.

さて、斯様にして得られた炭素繊維は、通常ボビンにチ
ーズ状(スフウェアエンド型)パッケージとして巻取る
場合、炭素繊維は本来一般の合成繊維に比べて物性が著
しく相違し、特にヤング率が高く、伸度が低く、かつ折
れ曲げに対して弱く、更にその表面が極めて滑らかで;
1bるため、パッケージの巻取管理、就中張力管理がむ
つかしく、たとえば炭素繊維を低張力で巻取る七、巻崩
れが生じ易く、また高張力の場合は系別や糸切れが生じ
易いという問題があった。
Now, when the carbon fiber obtained in this way is normally wound onto a bobbin as a cheese-like (software end type) package, the physical properties of carbon fiber are significantly different from those of general synthetic fibers, especially Young's modulus. is high, has low elongation, is weak against bending, and has an extremely smooth surface;
1b, it is difficult to manage the winding of the package, especially the tension management. For example, when winding carbon fiber at low tension, the winding tends to collapse, and when the tension is high, it is easy to cause line breakage and thread breakage. was there.

このため、これまで炭素繊維パッケージの巻取条件につ
いては種々の提案がなされている。
For this reason, various proposals have been made regarding the winding conditions for carbon fiber packages.

一方、前記炭素繊維はその有用性が市場において認めら
れ、需要量が増加しつつある。この炭素繊維の需要量増
大に伴ない炭素繊維もその巻量を多くした、いわゆるラ
ーヂパッケージ化(たとえば1〜10に9/パツケージ
)へと移行しつつある。
On the other hand, the usefulness of the carbon fiber has been recognized in the market, and the demand for it is increasing. With the increase in demand for carbon fiber, carbon fibers are being made into so-called large packages (for example, 9/package in 1 to 10), in which the amount of carbon fibers is increased.

ところが、炭素繊維のラーヂパッケージ化には問題が2
つある。その1つは前述したように、炭素繊維本来の特
質から巻崩れを生ぜず、かつ糸巻量の多いパッケージに
巻取ることが難しいこト、捷た他方巻上ったパッケージ
がその取扱い中、特に輸送時に巻崩れを起し易いことで
ある。このように巻崩れを起し易いパッケージ、ナイし
に一旦巻崩れを起したパッケージは解舒に際して、毛羽
や糸切れが発生し易く、また斯様な工程トラブルを起し
た炭素繊維から得られる複合材料は当然のこと乍ら品質
変動が大きくなる。
However, there are two problems with large packaging of carbon fiber.
There is one. One of these is that, as mentioned above, due to the inherent characteristics of carbon fiber, it is difficult to wind it into a package with a large amount of thread without causing collapse, and on the other hand, the rolled up package is particularly difficult to handle during handling. The problem is that the rolls tend to collapse during transportation. Packages that are prone to unrolling, and packages that have unrolled before being unrolled, tend to have fuzz and thread breakage when unrolling. Naturally, the quality of materials varies greatly.

本発明は炭素繊維のラーヂパッケージ化において、該繊
維を巻崩れの生じないパッケージとして巻取り、これに
よりパッケージの解舒時に生じる毛羽や糸切れを可及的
に減少させることを目的としたものであり、この目的を
達成するための本発明の構成は次のとおりである。
The present invention aims to reduce as much as possible the fuzz and thread breakage that occur when the package is unwound, by winding the fiber into a package that does not collapse when making large packages of carbon fibers. The configuration of the present invention to achieve this objective is as follows.

炭素繊維糸条が所定のワインド比で、ボビン上に巻取ら
れるスフウェアエンド型パッケージ(以下単にパッケー
ジという)において、該糸条が1ないし9トラバース毎
に、既に巻かれた糸条に対して、該糸条平均幅の50〜
150%のずれ(以下糸ずれ幅という)を与えるように
巻取られてなる炭素繊維パッケージ。
In a square-end package (hereinafter simply referred to as a package) in which carbon fiber yarn is wound on a bobbin at a predetermined wind ratio, the yarn is wound with respect to the already wound yarn every 1 to 9 traverses. , 50 to 50 of the yarn average width
A carbon fiber package that is wound to give a 150% deviation (hereinafter referred to as yarn deviation width).

以下、本発明を図面にもとづき具体的に説明する。Hereinafter, the present invention will be specifically explained based on the drawings.

第1図は、本発明に係る炭素繊維パッケージの見取図、
第2−1図は第1図の炭素繊維パッケージ表面に現われ
る井桁模様(但し、糸ずれ幅50%)の拡大図、第2−
2図は他の炭素繊維パッケージ表面に現われる井桁模様
(但し、糸ずれ幅150%)の拡大図である。
FIG. 1 is a sketch of a carbon fiber package according to the present invention;
Figure 2-1 is an enlarged view of the double cross pattern that appears on the surface of the carbon fiber package in Figure 1 (however, the thread deviation width is 50%).
Figure 2 is an enlarged view of the cross-shaped pattern (however, the thread deviation width is 150%) that appears on the surface of another carbon fiber package.

炭素繊維糸条(以下、単に糸条という)1は通常の巻取
機(図示せず)により、所定のワインド比のもとでトラ
バースさせながら、ボビン2上にパッケージとして連続
的に巻取られる。
Carbon fiber yarn (hereinafter simply referred to as yarn) 1 is continuously wound as a package onto a bobbin 2 while being traversed under a predetermined wind ratio by a normal winding machine (not shown). .

この際、糸条1はボビン2上、1ないし9トラバース毎
に、既に巻かれている糸条に対して50〜150%、好
ましくは75〜125%の糸ずれ幅を与えるよう巻取ら
れ、得られたパッケージ表面には井桁模様6が現われる
At this time, the yarn 1 is wound on the bobbin 2 every 1 to 9 traverses so as to give a yarn deviation width of 50 to 150%, preferably 75 to 125%, with respect to the already wound yarn, A parallel cross pattern 6 appears on the surface of the resulting package.

かかるパッケージにおいて、本発明の所期の目的を達成
するためには前記糸ずれ幅の特定化が最も肝要である。
In such a package, specifying the thread deviation width is most important in order to achieve the intended purpose of the present invention.

すなわち、糸ずれ幅が50%未満、即ち糸条と糸条との
重なり度合が糸条幅の5以上になると、糸条相互の絡み
合いが強すぎ、1vr舒に当って毛羽や糸切れが発生し
易い。また巻崩が凹凸になるため、かえってパッケージ
の巻密度が低下し、巻崩れが起り易い。
In other words, when the yarn deviation width is less than 50%, that is, when the degree of overlap between yarns is 5 or more of the yarn width, the yarns become too entangled with each other, and fluff and yarn breakage occur during 1vr sewing. easy. Moreover, since the unrolling becomes uneven, the winding density of the package is reduced, and the unrolling is more likely to occur.

一方、糸ずれ幅が150%を越える、即ち糸条と糸条と
の間隔4が糸条幅の5以上になると、前述したように炭
素繊維本来の特質から、特にラーチパッケージでは巻崩
れが起り易い。
On the other hand, if the yarn shear width exceeds 150%, that is, the distance 4 between the yarns becomes 5 or more of the yarn width, as mentioned above, due to the inherent characteristics of carbon fiber, winding collapse is likely to occur, especially in larch packages. .

この糸ずれ幅は糸条の太さく即ちトータルデニール)に
よって適宜選択するのが望ましく、たとえば6.000
デニールの糸条では糸ずれ幅の50〜100%、6.0
00デニールの糸条では糸ずれ幅の100〜150%の
範囲が好適であるように、糸条の太さが犬きぐなるに従
い、糸ずれ幅を大きくすることが望捷しい。
It is desirable to select this yarn deviation width appropriately depending on the thickness of the yarn (total denier), for example, 6.000.
For denier yarn, 50 to 100% of yarn deviation width, 6.0
Just as a range of 100 to 150% of the yarn shear width is suitable for a 00 denier yarn, it is desirable to increase the yarn shear width as the thickness of the yarn increases.

次に、糸条を前記パッケージに巻上げる場合の一態様に
ついて説明する。
Next, one aspect of winding the yarn into the package will be described.

通常の巻取機を使用して、糸条幅Y(朋)の糸条全外径
1)o(朋)、トラバース幅L(朋)のボビンに巻取る
ためには、ます糸条の巻始めにおけるボビン面での綾角
θ並びに糸ずれ幅y(朋)を設定し、これらの条件下で
の巻取機のワインド比W1に設定し、そのワインド比W
lのもとで糸条の巻取シラ行なう。
In order to wind a yarn with a yarn width Y (tomo) on a bobbin with a total outer diameter of 1)o (tomo) and a traverse width L (tomo) using a normal winding machine, start the winding of the square yarn. Set the winding angle θ and thread deviation width y (y) on the bobbin surface in , set the winding ratio W1 of the winding machine under these conditions, and set the winding ratio W
Winding of the yarn is carried out under l.

ここでワインド比Wlとは巻取機での1トラバース毎の
ボビンの回転数であり、次式(1ン〜(3)により与え
ることができる。
Here, the wind ratio Wl is the number of revolutions of the bobbin per traverse in the winder, and can be given by the following equations (1-(3)).

但し、Woは糸条幅Yi考慮しない場合のワインド比。However, Wo is the wind ratio when the yarn width Yi is not considered.

但し、dwは糸ずれ幅yのもとてのワインド比のずれ。However, dw is the deviation of the original wind ratio of the yarn deviation width y.

WO2は(1)式より求まるWoに最も近い整数値。WO2 is the integer value closest to Wo determined from equation (1).

Wl =WO−d w  ・・・・・・・・・・・・・
・・(3)この場合、綾角θは通常10〜30℃(巻終
りの綾角:4〜120 )の範囲に入るよう設計するの
が望ましい。というのは綾角が太きすぎるとトラバース
両端部に山(耳)ができ易く、糸傷みの原因となり、一
方綾角が小さすぎると巻崩れを起し易いからである。
Wl=WO-d w・・・・・・・・・・・・・・・
(3) In this case, it is desirable to design so that the winding angle θ is usually in the range of 10 to 30°C (winding angle at the end of winding: 4 to 120 degrees). This is because if the winding angle is too thick, peaks (ears) are likely to be formed at both ends of the traverse, causing damage to the thread, while if the winding angle is too small, the winding is likely to collapse.

今ここで糸条中2關の糸条を外径82mM、トラバース
幅152馴のボビンに、巻始めの綾角15°、糸ずれ量
75%(1,5m1)で巻取るだめのワインド比VV+
id次のようになる。
Now, wind the second thread in the thread onto a bobbin with an outer diameter of 82 mm and a traverse width of 152 mm, with a winding angle of 15 degrees and a thread deviation of 75% (1.5 m1).The wind ratio is VV+.
The id will be as follows.

7:4.4 = 0.0043 W、=4.4〜0.0043 =4.3957 したがって、Wlが4.5957となるよう調整された
巻取機のもとて巻取りを行なうと、糸ずれ幅75%のパ
ンケージが得られる。なお、巻取機でのワインド比の調
整手段はギヤーによって行なうのが通例である。
7:4.4 = 0.0043 W, = 4.4 to 0.0043 = 4.3957 Therefore, when winding is performed using a winding machine adjusted so that Wl is 4.5957, the yarn A pan cage with a deviation width of 75% is obtained. Note that the wind ratio in the winder is usually adjusted by means of a gear.

次に本発明を実施例により具体的に説明する。Next, the present invention will be specifically explained using examples.

実施例 アクリル繊維2種類(糸条平均幅2.OUおよび4. 
Ovn ) f通常の巻取機にて巻取るに尚り、糸ずれ
量を変更し、得られるパッケージの巻姿および解舒性t
pべた。その結果、得られたパッケージは表に示すとお
り、糸ずれ量50〜150んというパッケージNnl、
2および4においてのみ、巻姿および解舒性が共に良好
であった。
Example Two types of acrylic fibers (yarn average width: 2.OU and 4.OU)
Ovn) fWhen winding with a normal winding machine, the amount of thread deviation is changed to improve the winding shape and unwinding property of the resulting package.
P solid. As a result, as shown in the table, the obtained package is a package Nnl with a thread deviation of 50 to 150 mm.
Only in No. 2 and No. 4, both the winding form and the unwinding property were good.

以  下  余  白 上述のとおり、本発明の炭素繊維パッケージは、巻取時
既に巻かれた糸条に対して、該糸条の平均幅に利して5
0〜150%のずれを与えるよう、糸ずれ幅を規定した
ものであり、これにより、得られたパッケージは巻崩れ
が生じ難く、また解舒時に生じる毛羽や糸切れの発生が
著しく減少でき、就中2に7/パツケ一ジ以上のラーヂ
パッケージにおいてそれらの効果は顕著である。
Below Margin As mentioned above, the carbon fiber package of the present invention has an average width of 5% compared to the yarn already wound at the time of winding.
The yarn deviation width is specified to give a deviation of 0 to 150%, and as a result, the resulting package is less likely to collapse, and the occurrence of fluff and yarn breakage that occurs during unwinding can be significantly reduced. In particular, these effects are remarkable in large packages of 2 to 7 per package or more.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明に係る炭素繊維パッケージの見取図、第
2−1図は第1図の炭素繊維パッケージ表面に現われる
井桁模様(但し糸ずれ幅50%)の拡大図、第2−2図
は他の繊維繊維パッケージ表面に現われる井桁模様(但
し、糸ずれ幅150%)の拡大図である。 1:糸 条   3:井桁模様 2:ボビン    4:糸条と糸条との間隔第2・a図
Fig. 1 is a sketch of the carbon fiber package according to the present invention, Fig. 2-1 is an enlarged view of the parallel cross pattern (however, thread deviation width is 50%) appearing on the surface of the carbon fiber package in Fig. 1, and Fig. 2-2 is It is an enlarged view of a cross-shaped pattern (however, yarn deviation width is 150%) appearing on the surface of another fiber package. 1: Thread 3: Cross pattern 2: Bobbin 4: Spacing between threads 2nd figure a

Claims (2)

【特許請求の範囲】[Claims] (1) 炭素繊維糸条が所定のワインド比で、ボビン上
に巻取られるスフウェアエンド型パッケージにおいて、
該糸条が1ないし9トラバース毎に、既に巻かれた糸条
に対して、該糸条平均幅の50〜150%のずれを与え
るように巻取られてなる炭素繊維パッケージ。
(1) In a square-end package in which carbon fiber yarn is wound on a bobbin at a predetermined wind ratio,
A carbon fiber package in which the yarn is wound so as to give a deviation of 50 to 150% of the average width of the yarn from the already wound yarn every 1 to 9 traverses.
(2)  ワインド比が巻始めの糸条の綾角を10〜5
00とし、巻取りの糸条の綾角を4〜12゜となすよう
選定されてなる特許請求の範囲第(1)項記載の炭素繊
維パッケージ。
(2) The wind ratio is 10 to 5 for the winding angle of the yarn at the beginning of winding.
00, and the winding angle of the wound yarn is selected to be 4 to 12 degrees.
JP21424082A 1982-12-07 1982-12-07 Carbon fiber package Granted JPS59108656A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21424082A JPS59108656A (en) 1982-12-07 1982-12-07 Carbon fiber package

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21424082A JPS59108656A (en) 1982-12-07 1982-12-07 Carbon fiber package

Publications (2)

Publication Number Publication Date
JPS59108656A true JPS59108656A (en) 1984-06-23
JPS6246468B2 JPS6246468B2 (en) 1987-10-02

Family

ID=16652498

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21424082A Granted JPS59108656A (en) 1982-12-07 1982-12-07 Carbon fiber package

Country Status (1)

Country Link
JP (1) JPS59108656A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1234795A1 (en) * 1996-12-05 2002-08-28 Toray Industries, Inc. Carbon fiber package and carbon fiber packed member
JP2013523562A (en) * 2010-04-07 2013-06-17 ディーエスエム アイピー アセッツ ビー.ブイ. High Young's modulus yarn package and winding method of yarn package
WO2021085183A1 (en) * 2019-10-29 2021-05-06 宇部エクシモ株式会社 Wound yarn package and manufacturing method thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4941541A (en) * 1972-06-02 1974-04-18
JPS5010973A (en) * 1973-05-28 1975-02-04
JPS5328750A (en) * 1976-08-26 1978-03-17 Unitika Ltd Method of winding thread

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4941541A (en) * 1972-06-02 1974-04-18
JPS5010973A (en) * 1973-05-28 1975-02-04
JPS5328750A (en) * 1976-08-26 1978-03-17 Unitika Ltd Method of winding thread

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1234795A1 (en) * 1996-12-05 2002-08-28 Toray Industries, Inc. Carbon fiber package and carbon fiber packed member
JP2013523562A (en) * 2010-04-07 2013-06-17 ディーエスエム アイピー アセッツ ビー.ブイ. High Young's modulus yarn package and winding method of yarn package
US9751717B2 (en) 2010-04-07 2017-09-05 Dsm Ip Assets B.V. Package with high young's modulus yarn and method for winding the yarn package
US10266365B2 (en) 2010-04-07 2019-04-23 Dsm Ip Assets B.V. Package with high young's modulus yarn and method for winding the yarn package
WO2021085183A1 (en) * 2019-10-29 2021-05-06 宇部エクシモ株式会社 Wound yarn package and manufacturing method thereof
CN114555498A (en) * 2019-10-29 2022-05-27 宇部爱科喜模株式会社 Yarn package and method for manufacturing the same

Also Published As

Publication number Publication date
JPS6246468B2 (en) 1987-10-02

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