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JPH0151586B2 - - Google Patents

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Publication number
JPH0151586B2
JPH0151586B2 JP60044289A JP4428985A JPH0151586B2 JP H0151586 B2 JPH0151586 B2 JP H0151586B2 JP 60044289 A JP60044289 A JP 60044289A JP 4428985 A JP4428985 A JP 4428985A JP H0151586 B2 JPH0151586 B2 JP H0151586B2
Authority
JP
Japan
Prior art keywords
endless
yarn
fiber
fiber structure
threads
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.)
Expired
Application number
JP60044289A
Other languages
Japanese (ja)
Other versions
JPS61207657A (en
Inventor
Tetsuro Hirokawa
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.)
Shikishima Canvas KK
Original Assignee
Shikishima Canvas KK
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 Shikishima Canvas KK filed Critical Shikishima Canvas KK
Priority to JP60044289A priority Critical patent/JPS61207657A/en
Publication of JPS61207657A publication Critical patent/JPS61207657A/en
Publication of JPH0151586B2 publication Critical patent/JPH0151586B2/ja
Granted legal-status Critical Current

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  • Nonwoven Fabrics (AREA)
  • Woven Fabrics (AREA)

Description

【発明の詳細な説明】 産業上の利用分野 本発明は複合材強化用繊維構造体に関するもの
であり、更に詳しくは、繊維構造体の端面に実質
上糸条の切断端が存在しない形態保持性の良好
な、且つ、糸条積層密度の高い複合材強化用繊維
構造体に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to a fibrous structure for reinforcing composite materials, and more specifically, a fibrous structure with shape retention in which substantially no cut ends of threads are present on the end face of the fibrous structure. The present invention relates to a fiber structure for reinforcing composite materials that has good properties and a high yarn lamination density.

従来の技術 宇宙飛翔体、航空機、自動車、鉄道車輌あるい
は船舶等の強度を要求される機械装置の構成部材
として、あるいは建築物の構築部材として、ガラ
ス繊維織物や炭素繊維織物等の三次元的な繊維構
造体によつて補強された合成樹脂の複合材が使用
されている。更に1000℃以上の耐熱性が要求され
る構造部材の成形素材として炭素繊維/炭素マト
リツクス、黒鉛繊維/炭素マトリツクスあるい
は、黒鉛繊維/黒鉛マトリツクス等の組合せによ
る複合材が使用されている。
Prior Art Three-dimensional fabrics such as glass fiber fabrics and carbon fiber fabrics are used as structural members of mechanical devices that require strength such as spacecraft, aircraft, automobiles, railway vehicles, and ships, or as structural members of buildings. A composite material of synthetic resin reinforced with a fibrous structure is used. Furthermore, composite materials made of combinations of carbon fiber/carbon matrix, graphite fiber/carbon matrix, graphite fiber/graphite matrix, etc. are used as molding materials for structural members that are required to have heat resistance of 1000° C. or higher.

このような繊維構造体によつて補強された複合
材成形品は、軽量であるのと同時に強度や可撓性
等が極めて大であり、上記用途分野に限らず種々
の産業分野に於いてその有用性が評価されてい
る。而して斯かる複合材成形品(例えばFRPや
C―Cコンポジツト)等の強度的な特性は、強化
用基材として使用される繊維構造体中の繊維の含
有率、繊維配列、組織、あるいは構造等によつて
大きな影響を受ける。これらの繊維構造体の製造
手段として、例えば米国特許第4183232号明細書、
フランス国特許第2440494号公報、あるいは特開
昭59−71457号公報等が開示されている。
Composite molded products reinforced with such fiber structures are lightweight and at the same time have extremely high strength and flexibility, and are used not only in the above application fields but also in various industrial fields. Its usefulness has been evaluated. Therefore, the strength properties of such composite molded products (for example, FRP and C-C composites) are determined by the fiber content, fiber arrangement, texture, or It is greatly affected by the structure etc. As means for manufacturing these fiber structures, for example, US Pat. No. 4,183,232,
French Patent No. 2440494, Japanese Patent Application Laid-Open No. 59-71457, etc. are disclosed.

発明が解決しようとする問題点 しかしながら、上記米国特許に記載された繊維
構造体には寸法が制約されると共に繊維積層面に
対して垂直方向に糸条の切断端が露出するという
欠点が認められ、また、フランス国特許に記載さ
れた繊維構造体には寸法の制約ならびに繊維積層
面に対して半径方向に糸条の切断端が露出すると
いう欠点が認められている。更に特開昭59−
71457号公報に記載された繊維構造体にも寸法が
制約されるという前記同様の問題点が見受けられ
ている。これに加うるに、これらの公知の複合材
強化用の繊維構造体は、何れも補強用繊維の含有
比率が低いので必要な強度を保持するのに難点が
あり、且つ、その端面に無数の糸端を切断状態で
露出せしめており、このため熱硬化性樹脂、熱可
塑性樹脂、あるいはピツチ等の含浸に際し糸条が
抜け落ちて繊維構造体に形崩れが発生したり、あ
るいは該形崩れ発生部位を取除くために樹脂やピ
ツチ等が硬化した後、該部に切削加工を施したり
する必要がある。また、複雑な形状を有する複合
材成形品の製造に際しては機械加工が必須とな
り、それに起因する強度低下という問題も派生す
る。
Problems to be Solved by the Invention However, the fiber structure described in the above-mentioned U.S. patent has drawbacks in that its dimensions are restricted and the cut ends of the yarns are exposed in the direction perpendicular to the fiber lamination surface. Furthermore, the fiber structure described in the French patent has the drawbacks of dimensional limitations and exposure of the cut ends of the threads in the radial direction relative to the fiber lamination surface. Moreover, JP-A-59-
The fibrous structure described in Japanese Patent No. 71457 also suffers from the same problem of size restrictions. In addition, all of these known fiber structures for reinforcing composite materials have a low content ratio of reinforcing fibers, so it is difficult to maintain the necessary strength. The ends of the yarn are cut and exposed, so when impregnated with thermosetting resin, thermoplastic resin, pitch, etc., the yarn may fall off and cause the fiber structure to lose its shape, or the portion where the shape loss occurs. In order to remove this part, it is necessary to cut the part after the resin, pitch, etc. have hardened. Additionally, machining is essential when manufacturing a composite molded product having a complex shape, which also causes the problem of reduced strength.

本発明の主要な目的は、在来の複合材成形品の
補強材として使用される繊維構造体に認められる
上記の如き問題点を解消し得る複合材強化用の繊
維構造体を提供することにある。
The main object of the present invention is to provide a fiber structure for reinforcing composite materials that can solve the above-mentioned problems observed in fiber structures used as reinforcing materials for conventional composite molded products. be.

本発明の他の主要な目的は、繊維材料で補強さ
れた複合材成形品の外表面および内表面に基材を
構成している繊維糸条の糸端が露出しない特異な
構造的特徴を備えた繊維構造体と提供することに
ある。
Another main object of the present invention is to provide a composite molded product reinforced with fiber material with a unique structural feature in which the ends of the fiber threads constituting the base material are not exposed on the outer and inner surfaces. The object of the present invention is to provide a fibrous structure that has a unique structure.

問題点を解決するための手段 斯かる目的に鑑みて本発明は、糸条を1層また
は2層以上に亘つて所定の配列方向(例えば円筒
状繊維構造体の軸線方向、X)を維持して蛇行配
列した後、前記第1の配列方向(X軸方向)と異
なる第2の配列方向(例えば円筒状繊維構造体の
円周方向、Y)に張力付与下に捲回配列され、前
記積層に対して、締付け力を与える第1の無端糸
条1と、該第1の無端糸条1の積層を貫通し第3
の配列方向(例えば円筒状繊維構造体の半径方
向、Z)に蛇行配列される第2の無端糸条2と、
前記第1の無端糸条1の積層の表面に形成された
第2の無端糸条2のループ2′にカンヌキ糸とし
て挿通される第3の無端糸条3とからなり、第1
の無端糸条1の積層を前記第2の無端糸条2およ
び第3の無端糸条3によつて締付けて無端糸条の
積層密度を向上せしめた複合材強化用繊維構造体
を要旨とするものである。
Means for Solving the Problems In view of the above object, the present invention maintains a predetermined arrangement direction (for example, the axial direction of a cylindrical fiber structure, X) of yarns over one or more layers. After being arranged in a meandering manner, the laminated layers are arranged in a winding manner under tension in a second arrangement direction (for example, the circumferential direction of the cylindrical fiber structure, Y) different from the first arrangement direction (X-axis direction). , a first endless yarn 1 that applies a tightening force, and a third endless yarn that penetrates the stack of the first endless yarn 1.
a second endless yarn 2 arranged meanderingly in the arrangement direction (for example, the radial direction of the cylindrical fiber structure, Z);
A third endless yarn 3 is inserted as a cannula thread into the loop 2' of the second endless yarn 2 formed on the surface of the stack of the first endless yarn 1, and
The gist of the present invention is a fiber structure for reinforcing a composite material, in which a stack of endless threads 1 is tightened by the second endless thread 2 and the third endless thread 3 to improve the stacking density of the endless threads. It is something.

実施例 第1図は複合材強化用の繊維構造体が中空円筒
形をなしている場合を例示する一部破断斜視図で
あり、第2図はその横断面図である。
Embodiment FIG. 1 is a partially cutaway perspective view illustrating a case where a fiber structure for reinforcing a composite material has a hollow cylindrical shape, and FIG. 2 is a cross-sectional view thereof.

本実施例に於いては、繊維構造体を形成する第
1の無端糸条1は、先ず中空円筒状をなす繊維構
造体の軸線方向(X軸方向)に1層蛇行配列し、
次に円周方向Yに位相をずらせて更に1層蛇行配
列し糸条の配列層を形成した後、配列方向を変換
して前記繊維構造体の軸線方向(X軸方向)に対
して略直交するように、該繊維構造体の円周方向
Yに張力付与下に捲回配列され、X軸方向に蛇行
配列された糸条の配列層に対して、所定の締付け
力を与える。上記X軸方向およびY方向に沿う第
1の無端糸条1の蛇行配列と捲回配列の組合わせ
は、最終的に得られる繊維構造体の設計寸法に合
致するように繰返し回数が決定される。第2の無
端糸条2は、蛇行配列と捲回配列の繰返しによつ
て形成された第1の無端糸条1の積層を貫通して
第3の方向に延びている。例えば本実施例に於い
ては、第2の無端糸条2が繊維構造体の半径方向
(Z軸方向)に蛇行配列されている。更に第1図
に示すように該Z軸方向への蛇行配列によつて第
1の無端糸条1の積層の表面に形成された第2の
無端糸条2のループ2′にカンヌキ糸として第3
の無端糸条3が挿通されている。このように、第
1の無端糸条1の積層は、第2の無端糸条2およ
び第3の無端糸条3によつて強固に締付けられ、
積層密度を向上せしめた複合材強化用繊維構造体
を形成している。
In this embodiment, the first endless yarn 1 forming the fiber structure is arranged in a meandering manner in one layer in the axial direction (X-axis direction) of the fiber structure having a hollow cylindrical shape.
Next, the phase is shifted in the circumferential direction Y and the yarns are further arranged in a meandering manner to form an arrangement layer of yarns, and then the arrangement direction is changed so that the arrangement direction is approximately perpendicular to the axial direction (X-axis direction) of the fiber structure. A predetermined tightening force is applied to the arrayed layer of threads arranged in a winding manner under tension in the circumferential direction Y of the fiber structure and meanderingly arranged in the X-axis direction. The number of repetitions of the combination of the meandering arrangement and the winding arrangement of the first endless yarn 1 along the X-axis direction and the Y direction is determined so as to match the design dimensions of the finally obtained fiber structure. . The second endless yarn 2 extends in the third direction through the stack of first endless yarns 1 formed by repeating the meandering arrangement and the winding arrangement. For example, in this embodiment, the second endless yarn 2 is arranged in a meandering manner in the radial direction (Z-axis direction) of the fiber structure. Furthermore, as shown in FIG. 1, the loops 2' of the second endless yarns 2 formed on the surface of the stack of the first endless yarns 1 by the meandering arrangement in the Z-axis direction are coated with cannula threads. 3
An endless thread 3 is inserted through the thread. In this way, the stack of the first endless yarn 1 is firmly tightened by the second endless yarn 2 and the third endless yarn 3,
A fiber structure for reinforcing composite materials with improved lamination density is formed.

これらの繊維構造体は、このままで、または常
法に従つて熱硬化性樹脂、熱可塑性樹脂またはピ
ツチ等の含浸工程を経て最終製品に仕上げられ
る。
These fibrous structures can be finished into final products as they are, or after being impregnated with a thermosetting resin, thermoplastic resin, pitch, or the like according to a conventional method.

上記実施例は本発明の具体的実施態様を繊維構
造体が中空円筒体である場合について例示するも
のであるが、本発明は斯かる例示説明によつてそ
の要旨を限定解釈されるべきものではなく、例え
ば第3図に示すように円錐台形、コーンケーブ形
あるいは紡錘形等の繊維構造体も含まれる。ま
た、上記実施例に於いては実質的に1本の無端糸
条1が蛇行配列と捲回配列を繰返して積層体を形
成しているが、繊維構造体の表面に切断端が形成
されない限り、繊維構造体の形状と寸法に応じて
2本以上の第1の無端糸条を積層体の形成途上で
接合して繊維構造体を形成することも可能であ
る。また、繊維構造体に要求される強度特性に応
じて無端糸条1,2,3の太さや糸条構成繊維の
種類を変更することもできる。
Although the above examples illustrate specific embodiments of the present invention in the case where the fiber structure is a hollow cylindrical body, the gist of the present invention should not be construed as limited by such illustrative explanations. For example, as shown in FIG. 3, fiber structures such as a truncated cone shape, a cone cave shape, or a spindle shape are also included. Further, in the above embodiment, substantially one endless yarn 1 repeats the meandering arrangement and the winding arrangement to form a laminate, but as long as no cut ends are formed on the surface of the fiber structure. It is also possible to form a fiber structure by joining two or more first endless threads during the formation of the laminate depending on the shape and dimensions of the fiber structure. Furthermore, the thickness of the endless yarns 1, 2, and 3 and the type of yarn-constituting fibers can be changed depending on the strength characteristics required of the fiber structure.

本発明に於ける無端糸条としては、例えば炭素
繊維、炭化珪素繊維、黒鉛繊維、ガラス繊維、金
属繊維、ポリアミド繊維、あるいはポリエステル
繊維等の引揃え糸や撚り糸が使用される。
As the endless yarn in the present invention, for example, drawn yarn or twisted yarn such as carbon fiber, silicon carbide fiber, graphite fiber, glass fiber, metal fiber, polyamide fiber, or polyester fiber is used.

発明の効果 本発明に係る繊維構造体は、その糸条積層密度
が大きく、且つ、強固な締付け構造を備えている
ので、最終製品の形態安定性が在来の繊維構造体
に比較して顕著に向上する。更に本発明に於いて
は、繊維構造体の形状や寸法、あるいは要求強度
に応じて糸条の配列方向、使用本数、積層密度を
適宜変更することができるから、最終製品の要求
特性に対して容易に適合することができる。また
本発明に係る繊維構造体は、その表面に糸条の切
断端が実質上露出していないから、運搬途上や樹
脂の含浸工程等に於いて糸条が抜け落ちて繊維構
造体に形崩れが発生するおそれがなく、また形状
補正のため樹脂またはピツチ等が硬化した後、該
部に切削加工を施す必要もない。従つて本発明に
係る繊維構造体は、複雑な形状を有する複合材の
成形に容易に適合し得るのみならず、機械加工に
起因する強度低下の防止に対しても大きく寄与し
得るものであ。
Effects of the Invention The fiber structure according to the present invention has a high yarn lamination density and a strong tightening structure, so the morphological stability of the final product is remarkable compared to conventional fiber structures. improve. Furthermore, in the present invention, the arrangement direction of the yarns, the number of yarns used, and the lamination density can be changed as appropriate depending on the shape and dimensions of the fiber structure, or the required strength. Can be easily adapted. In addition, since the fiber structure according to the present invention has substantially no cut ends of the threads exposed on its surface, the threads may fall off during transportation or during the resin impregnation process, causing the fiber structure to lose its shape. There is no risk of this occurring, and there is no need to cut the part after the resin or pitch has hardened to correct the shape. Therefore, the fibrous structure according to the present invention can not only be easily adapted to molding composite materials having complicated shapes, but also can greatly contribute to preventing strength reduction due to machining. .

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

第1図は複合材強化用の繊維構造体が中空円筒
形をなしている場合を例示する一部破断斜視図で
あり、第2図は第1図の線A―Aに沿う繊維構造
体の横断面図である。また第3図は本発明に係る
繊維構造体を例示する斜視図である。 1……第1の無端糸条、2……第2の無端糸
条、3……第3の無端糸条、2′……第2の無端
糸条のループ。
FIG. 1 is a partially cutaway perspective view illustrating a case where the fiber structure for reinforcing a composite material has a hollow cylindrical shape, and FIG. 2 is a partially cutaway perspective view of the fiber structure along line A-A in FIG. FIG. Moreover, FIG. 3 is a perspective view illustrating a fiber structure according to the present invention. 1...First endless yarn, 2...Second endless yarn, 3...Third endless yarn, 2'...Loop of second endless yarn.

Claims (1)

【特許請求の範囲】[Claims] 1 糸条を1層または2層以上に亘つて所定の配
列方向を維持して蛇行配列した後、前記第1の配
列方向と異なる第2の配列方向に張力付与下に捲
回配列され、前記積層に対して締付け力を与える
第1の無端糸条と、該第1の無端糸条の積層を貫
通し第3の配列方向に蛇行配列される第2の無端
糸条と、前記第1の無端糸条の積層の表面に形成
された第2の無端糸条のループにカンヌキ糸とし
て挿通される第3の無端糸条とからなり、第1の
無端糸条の積層を前記第2の無端糸条および第3
の無端糸条によつて締付けて無端糸条の積層密度
を向上せしめた複合材強化用繊維構造体。
1. After one or more layers of yarn are arranged in a meandering manner while maintaining a predetermined arrangement direction, the threads are wound and arranged under tension in a second arrangement direction different from the first arrangement direction, and the a first endless yarn that applies a tightening force to the lamination; a second endless yarn that passes through the lamination of the first endless yarn and is arranged in a meandering manner in a third arrangement direction; A third endless yarn is inserted as a cannula yarn into a loop of the second endless yarn formed on the surface of the stack of endless yarns, and the first endless yarn stack is connected to the second endless yarn loop. Thread and third
A fiber structure for reinforcing composite materials, which is tightened with endless threads to improve the lamination density of the endless threads.
JP60044289A 1985-03-06 1985-03-06 Composite reinforced fiber structure Granted JPS61207657A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60044289A JPS61207657A (en) 1985-03-06 1985-03-06 Composite reinforced fiber structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60044289A JPS61207657A (en) 1985-03-06 1985-03-06 Composite reinforced fiber structure

Publications (2)

Publication Number Publication Date
JPS61207657A JPS61207657A (en) 1986-09-16
JPH0151586B2 true JPH0151586B2 (en) 1989-11-06

Family

ID=12687345

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60044289A Granted JPS61207657A (en) 1985-03-06 1985-03-06 Composite reinforced fiber structure

Country Status (1)

Country Link
JP (1) JPS61207657A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2648711B2 (en) * 1986-11-07 1997-09-03 株式会社 ペトカ Manufacturing method of pitch-based carbon fiber three-dimensional fabric
JPH07111017B2 (en) * 1989-02-20 1995-11-29 株式会社豊田自動織機製作所 Three-dimensional fabric and manufacturing method thereof
JPH07111016B2 (en) * 1989-02-27 1995-11-29 株式会社豊田自動織機製作所 Three-dimensional fabric and manufacturing method thereof
JP2834473B2 (en) * 1989-05-09 1998-12-09 敷島紡績株式会社 Deformed reinforced substrates for composites
JP2702571B2 (en) * 1989-11-28 1998-01-21 三菱重工業株式会社 Reinforcement base material for composite fasteners
JP2714735B2 (en) * 1992-05-20 1998-02-16 財団法人鉄道総合技術研究所 Large diameter rod made of organic synthetic fiber

Also Published As

Publication number Publication date
JPS61207657A (en) 1986-09-16

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