JP2875865B2 - Three-dimensional fabric - Google Patents
Three-dimensional fabricInfo
- Publication number
- JP2875865B2 JP2875865B2 JP22744590A JP22744590A JP2875865B2 JP 2875865 B2 JP2875865 B2 JP 2875865B2 JP 22744590 A JP22744590 A JP 22744590A JP 22744590 A JP22744590 A JP 22744590A JP 2875865 B2 JP2875865 B2 JP 2875865B2
- Authority
- JP
- Japan
- Prior art keywords
- tubular
- tubular portion
- dimensional
- fabric
- dimensional fabric
- 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 - Fee Related
Links
Landscapes
- Woven Fabrics (AREA)
Description
【発明の詳細な説明】 産業上の利用分野 本発明は、複合材からなるフランジ付きの管状物品の
強化材として使用される立体織物に関するものである。Description: TECHNICAL FIELD The present invention relates to a three-dimensional fabric used as a reinforcing material for a flanged tubular article made of a composite material.
一般に航空機などを初めとする各種の機器の構造材と
して、炭素繊維などの強化材に反応硬化型樹脂を含浸し
た複合材が使用されている。そしてこれらの複合材は使
用する機器やその部分によって適切な形状に成形するこ
とが必要であり、またその複合材に使用される強化材に
おいても、複合材の形状や荷重の方向などを考慮して、
荷重を適切に負担し得る構造を有するものであることが
要求されるのである。2. Description of the Related Art In general, composite materials obtained by impregnating a reinforcing material such as carbon fiber with a reaction-curable resin are used as structural materials for various devices such as aircraft. It is necessary to form these composites into an appropriate shape depending on the equipment used and its parts, and also consider the shape of the composite and the direction of load in the reinforcement used for the composite. hand,
It is required to have a structure that can appropriately bear the load.
而して本発明は、管状部の端末にフランジ部を一体に
形成した形状の複合材を成形するための強化材に関す
る。Accordingly, the present invention relates to a reinforcing material for molding a composite material having a shape in which a flange portion is integrally formed at an end of a tubular portion.
この種のフランジ付き管状物品は、両端にフランジを
形成してそれ自体長尺物品の巻取りボビンとして使用
し、また互いに離間した構造材を連結する部材として使
用される。また管状部の一端にフランジを形成したもの
は棒状物品の支持部材として使用され、また比較的大径
のフランジに小径の短い管状部を形成したものは、ホイ
ールとして使用することができる。その他管状部の径や
長さ、フランジ部の径などを適切に設定することによ
り、各種の機器の構造材として広範な用途に使用するこ
とができる。This type of tubular article with a flange is used as a winding bobbin for a long article by forming a flange at both ends and as a member for connecting structural members separated from each other. Further, the one having a flange formed at one end of the tubular part can be used as a support member for a rod-shaped article, and the one having a small-diameter short tubular part formed on a relatively large-diameter flange can be used as a wheel. In addition, by appropriately setting the diameter and length of the tubular portion, the diameter of the flange portion, and the like, it can be used for a wide range of applications as a structural material for various devices.
従来の技術 従来この種のフランジ付き管状物品を製作するときに
は、その強化材としては管状部とフランジ部とを別個に
製作し、それを組合わせて一体の複合材としていた。す
なわち、繊維を筒状に織成してこれを複数嵌合して管状
部の強化材とし、またドーナツ状に織成した円盤状織物
を積層してフランジ部の強化材となし、これを所定の形
状に組合わせて反応硬化型樹脂液を含浸して硬化させ、
複合材を得ていたのである。2. Description of the Related Art Conventionally, when fabricating a flanged tubular article of this type, a tubular portion and a flange portion were separately produced as reinforcing materials, and these were combined to form an integral composite material. That is, the fibers are woven into a tubular shape, and a plurality of the fibers are fitted together to form a reinforcing material for the tubular portion, and a doughnut-shaped woven disk-shaped fabric is laminated to form a reinforcing material for the flange portion, which is formed into a predetermined shape. Impregnated with a reaction-curable resin liquid in combination and cured,
I was getting a composite.
発明が解決しようとする問題点 しかしながらこの種の複合材にあっては、管状部とフ
ランジ部とで強化材が分離しており、互いに連続してい
ないため、両者の連結部の強度的が劣るものであった。Problems to be Solved by the Invention However, in this type of composite material, since the reinforcing material is separated at the tubular portion and the flange portion and is not continuous with each other, the strength of the connecting portion between the two is inferior. Was something.
また筒状織物の端末部のたて糸のみを延ばし、そのた
て糸を外方に曲げてフランジ部を形成し、管状部とフラ
ンジ部とが連続した一体の強化材とすることも行われて
いるが、この構造ではフランジ部が周方向に強化されて
いないため、放射状のひび割れを生じ易い。Also, only the warp yarn at the end of the tubular fabric is extended, and the warp yarn is bent outward to form a flange portion, and the tubular portion and the flange portion are also formed as a continuous and integral reinforcing material. In this structure, since the flange portion is not reinforced in the circumferential direction, radial cracks are easily generated.
本発明はかかる事情に鑑みなされたものであって、管
状部とフランジ部とが連続した一体の複合材を成形する
ための立体織物を提供することを目的とするものであ
る。The present invention has been made in view of such circumstances, and has as its object to provide a three-dimensional woven fabric for forming an integral composite material in which a tubular portion and a flange portion are continuous.
問題点を解決する手段 而して本発明は、環状に配置されて互いに平行に延び
るたて糸群と、当該たて糸群に交差して螺旋状に延びる
よこ糸とを織成して管状部を形成し、当該管状部の一端
において前記たて糸群が放射状に延び、前記よこ糸は当
該放射状のたて糸に交差して渦巻状に延び、当該放射状
のたて糸と渦巻状のよこ糸とにより円盤状部を形成して
なることを特徴とするものである。Means for Solving the Problems Accordingly, the present invention provides a tubular portion formed by weaving a group of warp yarns arranged in an annular shape and extending in parallel with each other, and a weft yarn extending in a spiral shape crossing the group of warp yarns. At one end of the portion, the warp group extends radially, the weft extends spirally across the radial warp yarn, and the radial warp yarn and the spiral weft form a disk-shaped portion. It is assumed that.
以下本発明を図面に従って説明する。第1図は本発明
の立体織物を示すものである。この立体織物1は管状部
2と円盤状部3とよりなっており、全体としてたて糸4
とよこ糸5とを織成した織物構造をなしている。Hereinafter, the present invention will be described with reference to the drawings. FIG. 1 shows a three-dimensional fabric of the present invention. This three-dimensional woven fabric 1 is composed of a tubular portion 2 and a disc-shaped portion 3 and has a warp yarn 4 as a whole.
It has a woven structure in which weft yarns 5 are woven.
すなわち管状部2においては、たて糸4は環状に配置
されて互いに平行に延びたたて糸群を形成しており、そ
れと交差するようによこ糸5が螺旋状に配置され、たて
糸4とよこ糸5とが筒状の織物を構成している。That is, in the tubular portion 2, the warp yarns 4 are arranged in an annular shape to form a group of warp yarns extending in parallel with each other, and the weft yarns 5 are spirally arranged so as to intersect with the warp yarns. Woven fabric.
また円盤状部3においては、たて糸4は管状部2の端
末から放射状に延びている。そしてよこ糸5はこの放射
状のたて糸4と交差して渦巻状に織込まれ、たて糸4と
よこ糸5とで円盤状の織物を構成している。In the disc-shaped portion 3, the warp yarns 4 extend radially from the end of the tubular portion 2. The weft yarn 5 is spirally woven so as to intersect with the radial warp yarn 4, and the warp yarn 4 and the weft yarn 5 constitute a disk-shaped fabric.
そして管状部2と円盤状部3とは、たて糸4が連続し
且つそれぞれの箇所においてよこ糸5と織成されて織物
構造をなしており、全体として一体の立体織物1を形成
している。The tubular portion 2 and the disc-shaped portion 3 have a woven structure in which the warp yarns 4 are continuous and are woven with the weft yarns 5 at respective positions, thereby forming an integral three-dimensional woven fabric 1 as a whole.
次にこの立体織物1を織成する方法を説明する。第2
図は立体織物1における管状部2を織成する状態を示す
ものであって、たて糸4は外方から放射状に供給され、
織り口6から下方に延びている。そして織り口6の外方
においてヘルド7により開口運動せしめられ、その開口
8内をシャットル9が回転し、該シャットル9に収容さ
れたよこ糸ボビンから繰出されたよこ糸5が織り口6に
供給されるようになっている。Next, a method of weaving the three-dimensional fabric 1 will be described. Second
The figure shows a state in which the tubular portion 2 of the three-dimensional fabric 1 is woven, and the warp yarns 4 are supplied radially from the outside,
It extends downward from the weaving opening 6. The shed 7 causes the shed 7 to open and move outside the weaving opening 6. The shuttle 9 rotates in the opening 8, and the weft yarn 5 fed from the weft bobbin accommodated in the shuttle 9 is supplied to the weaving opening 6. It has become.
そして織り口6においてたて糸4をシャットル9の回
転面に対して垂直に下方に引取りながら、シャットル9
を回転させると、織り口6においてたて糸4とよこ糸5
とが織成され、筒状の管状部2が形成される。At the weaving opening 6, the warp yarn 4 is taken vertically downward with respect to the rotation plane of the shuttle 9, and
Is rotated, the warp 4 and the weft 5
Are woven to form a tubular portion 2.
管状部2が所定の長さに亙って織成されたならば、た
て糸4の下方への引取りを停止する。そしてそのままで
ヘルド7でたて糸4を開口させながら、その開口8内で
シャットル9を回転させてよこ糸5を織込んでいくと、
織物が引取られないために織り口6が次第に外方に移動
し、そこへ次々とよこ糸5が繰込まれてゆき、第3図に
示すように管状部2の端末から外方に延びる円盤状部3
が形成されるのである。When the tubular portion 2 has been woven over a predetermined length, the lowering of the warp yarn 4 is stopped. Then, while opening the warp yarn 4 with the heald 7 as it is, rotating the shuttle 9 in the opening 8 and weaving the weft yarn 5,
Since the woven fabric is not taken, the weaving mouth 6 gradually moves outward, into which the weft thread 5 is successively fed, and as shown in FIG. 3, a disk-like shape extending outward from the end of the tubular portion 2. Part 3
Is formed.
次にこの立体織物1を使用したフランジ付き管状物品
10を説明する。第4図は一端フランジ付き管状物品10a
を示すものであって、管状部11と、該管状部11の一端か
ら外方に張出して形成されたフランジ部12とよりなって
いる。そして図面においては、三個の立体織物1を積層
して立体織物積層体13を構成し、該立体織物積層体13に
反応硬化型樹脂液を含浸させて硬化させ、成形したもの
である。Next, a flanged tubular article using this three-dimensional fabric 1
10 is explained. FIG. 4 shows a tubular article 10a having a flange at one end.
It comprises a tubular portion 11 and a flange portion 12 formed to protrude outward from one end of the tubular portion 11. In the drawing, the three-dimensional fabric 1 is laminated to form a three-dimensional fabric laminate 13, and the three-dimensional fabric laminate 13 is impregnated with a reaction-curable resin liquid, cured and molded.
そして前記立体織物積層体13においては、立体織物1
の管状部2を、他の立体織物1の円盤状部3が形成され
た側から管状部2内に順次挿入し、管状部11においては
立体織物1の管状部2を径方向に積層し、フランジ部12
において円盤状部3を厚さ方向に積層して、一体の立体
織物積層体13を形成している。In the three-dimensional fabric laminate 13, the three-dimensional fabric 1
Is sequentially inserted into the tubular portion 2 from the side on which the disk-shaped portion 3 of the other three-dimensional fabric 1 is formed, and in the tubular portion 11, the tubular portion 2 of the three-dimensional fabric 1 is laminated in the radial direction, Flange part 12
, The disc-shaped portions 3 are laminated in the thickness direction to form an integral three-dimensional woven fabric laminate 13.
また第5図は両端フランジ付き管状物品10bを示すも
のであって、管状部11とその両端に形成された一対のフ
ランジ部12とよりなっている。そしてこの両端フランジ
付き管状物品10bにおける立体織物積層体13は、第一の
立体織物1の先端側から第二の立体織物1の管状部2を
挿入し、さらにその第二の立体織物1の先端側から第三
の立体織物1の管状部2を挿入し、以下同様にして交互
に管状部2をその先端側から挿入して重ね合わせ、且つ
積層された管状部2の両端において一つ置きの立体織物
1の円盤状部3同士を重ね合わせ、管状部11においては
立体織物1の管状部2を径方向に積層すると共に、フラ
ンジ部12においては円盤状部3を厚さ方向に積層して、
一体の立体織物積層体13を形成している。FIG. 5 shows a tubular article 10b with flanges at both ends, which comprises a tubular portion 11 and a pair of flange portions 12 formed at both ends thereof. The three-dimensional woven fabric laminate 13 in the tubular article 10b with flanges at both ends inserts the tubular portion 2 of the second three-dimensional woven fabric 1 from the tip side of the first three-dimensional woven fabric 1, and further inserts the tip of the second three-dimensional woven fabric 1. The tubular portions 2 of the third three-dimensional fabric 1 are inserted from the side, and the tubular portions 2 are alternately inserted from the front end side in the same manner in the following manner, overlapped, and alternately placed at both ends of the laminated tubular portion 2 The disc-shaped portions 3 of the three-dimensional fabric 1 are overlapped with each other, and in the tubular portion 11, the tubular portions 2 of the three-dimensional fabric 1 are laminated in the radial direction, and in the flange portion 12, the disc-shaped portions 3 are laminated in the thickness direction. ,
An integrated three-dimensional woven fabric laminate 13 is formed.
実施例 第6図は、本発明の実施例を示すものである。この立
体織物1は先の実施例のものと同様に管状部2と円盤状
部3とよりなっており、全体としてたて糸4とよこ糸5
とを織成した織物構造をなしている。そして管状部2の
先端において、遊離のたて糸4が突出して放射状に延び
ており、たて糸延長部14を形成している。Embodiment FIG. 6 shows an embodiment of the present invention. This three-dimensional woven fabric 1 comprises a tubular portion 2 and a disc-shaped portion 3 as in the previous embodiment, and as a whole, a warp yarn 4 and a weft yarn 5
And a woven structure. At the tip of the tubular portion 2, the free warp yarn 4 protrudes and extends radially to form a warp yarn extension 14.
この実施例の立体織物1は、第1図の立体織物1と全
く同様に織成することができる。ただ織成した後に立体
織物1を切卸すときに、先の立体織物1においてはたて
糸4を管状部2の先端の位置で切断するのに対し、この
実施例においては、管状部2の先端からたて糸延長部14
の長さの余裕をもって切断する点で異る。The three-dimensional fabric 1 of this embodiment can be woven in exactly the same manner as the three-dimensional fabric 1 of FIG. However, when the three-dimensional fabric 1 is cut off after weaving, the warp yarn 4 is cut at the position of the tip of the tubular portion 2 in the preceding three-dimensional fabric 1, whereas in this embodiment, the warp yarn is cut from the tip of the tubular portion 2. Extension 14
In that it is cut with a margin of length.
また第7図はこの立体織物1を使用した両端フランジ
付き管状物品10bを示すものである。この両端フランジ
付き管状物品10bの立体織物積層体13においては、個々
の立体織物1は第5図の例と同様に管状部2を交互に他
の立体織物1の管状部2にその先端側から挿入して組合
わせるのであるが、管状部2を他の立体織物1の管状部
2に挿入した後、当該管状部2の先端のたて糸延長部14
を放射状に拡げ、当該地の立体織物1の円盤状部3に沿
わせるのである。FIG. 7 shows a tubular article 10b with flanges at both ends using the three-dimensional fabric 1. In the three-dimensional woven fabric laminate 13 of the tubular article 10b with flanges at both ends, the individual three-dimensional woven fabrics 1 alternately form the tubular portions 2 alternately with the tubular portions 2 of the other three-dimensional woven fabrics 1 from the front end side, as in the example of FIG. After inserting the tubular portion 2 into the tubular portion 2 of another three-dimensional fabric 1, the warp yarn extension portion 14 at the tip of the tubular portion 2 is inserted.
Is spread radially and is made to follow the disk-shaped portion 3 of the three-dimensional fabric 1 on the ground.
作用及び発明の効果 本発明によれば、複合材製のフランジ付き管状物品10
の強化材を構成する立体織物1が、その管状部2と円盤
状部3とが連続した一体の織物構造により構成されてい
るので、強化材が管状部とフランジ部とで組織がとぎれ
ることがなく、一体に連続したものとなる。According to the present invention, a flanged tubular article 10 made of a composite material is provided.
Since the three-dimensional woven fabric 1 constituting the reinforcing material is constituted by an integrated woven structure in which the tubular portion 2 and the disc-shaped portion 3 are continuous, the structure of the reinforcing material may be cut off between the tubular portion and the flange portion. Instead, they are continuously continuous.
従ってフランジ付き管状物品10においても、その管状
部11とフランジ部12とがそれぞれ強化されているだけで
なく、その連結部においても強化され、他の部分と同等
の強度を有しており、大きな力が加わったようなときに
も管状部11とフランジ部12との連結部から破損するよう
なことがない。Therefore, also in the flanged tubular article 10, the tubular portion 11 and the flange portion 12 are not only reinforced, but also reinforced at the connection portion, and have the same strength as other portions, Even when a force is applied, the connection between the tubular portion 11 and the flange portion 12 is not damaged.
しかも立体織物1の円盤状部3は管状部2と連続した
織物構造を有しているので、周方向にも充分に強化され
ており、たて糸4のみを放射状に配置した場合のように
放射状のひび割れが生じるようなこともない。In addition, since the disk-shaped portion 3 of the three-dimensional fabric 1 has a woven structure continuous with the tubular portion 2, it is sufficiently reinforced in the circumferential direction, and has a radial shape as in the case where only the warp yarns 4 are radially arranged. No cracking occurs.
第1図は本発明の立体織物を示す斜視図であり、第2図
及び第3図はその立体織物を織成する工程を示す概念図
である。また第4図及び第5図は、第1図の立体織物を
使用したフランジ付き管状物の中央縦断面図である。第
6図は本発明の立体織物の実施例を示す斜視図であり、
第7図は第6図の立体織物を使用した両端フランジ付き
管状物品の中央縦断面図である。 1……立体織物、2……管状部 3……円盤状部、4……たて糸 5……よこ糸FIG. 1 is a perspective view showing a three-dimensional fabric of the present invention, and FIGS. 2 and 3 are conceptual views showing a process of weaving the three-dimensional fabric. 4 and 5 are central longitudinal cross-sectional views of a flanged tubular article using the three-dimensional fabric of FIG. FIG. 6 is a perspective view showing an embodiment of the three-dimensional fabric of the present invention,
FIG. 7 is a central longitudinal sectional view of a tubular article having flanges at both ends using the three-dimensional fabric of FIG. DESCRIPTION OF SYMBOLS 1 ... Three-dimensional fabric, 2 ... Tubular part 3 ... Disc-shaped part, 4 ... Warp yarn 5 ... Weft yarn
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平3−59141(JP,A) 特開 昭57−133245(JP,A) 特開 昭58−220847(JP,A) 特開 昭63−309648(JP,A) 特開 昭62−170550(JP,A) (58)調査した分野(Int.Cl.6,DB名) D03D 1/00,25/00,41/00 ──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-3-59141 (JP, A) JP-A-57-133245 (JP, A) JP-A-58-220847 (JP, A) JP-A 63-133 309648 (JP, A) JP-A-62-170550 (JP, A) (58) Fields investigated (Int. Cl. 6 , DB name) D03D 1/00, 25/00, 41/00
Claims (1)
糸(4)群と、当該たて糸(4)群に交差して螺旋状に
延びるよこ糸(5)とを織成して管状部(2)を形成
し、当該管状部(2)の一端において前記たて糸(4)
群が放射状に延び、前記よこ糸(5)は当該放射状のた
て糸(4)に交差して渦巻状に延び、当該放射状のたて
糸(4)と渦巻状のよこ糸(5)とにより円盤状部
(3)を形成してなることを特徴とする、立体織物A tubular portion (2) is formed by weaving a group of warp yarns (4) arranged in an annular shape and extending parallel to each other and a weft yarn (5) extending spirally across the group of warp yarns (4). And the warp (4) at one end of the tubular portion (2).
The group extends radially, and the weft (5) spirally intersects the radial warp (4), and is formed by the radial warp (4) and the spiral weft (5). ), Characterized by forming a three-dimensional fabric
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP22744590A JP2875865B2 (en) | 1990-08-28 | 1990-08-28 | Three-dimensional fabric |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP22744590A JP2875865B2 (en) | 1990-08-28 | 1990-08-28 | Three-dimensional fabric |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH04108138A JPH04108138A (en) | 1992-04-09 |
JP2875865B2 true JP2875865B2 (en) | 1999-03-31 |
Family
ID=16860984
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP22744590A Expired - Fee Related JP2875865B2 (en) | 1990-08-28 | 1990-08-28 | Three-dimensional fabric |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2875865B2 (en) |
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US11976686B2 (en) | 2018-08-10 | 2024-05-07 | Crompton Technology Group Limited | Composite connectors and methods of manufacturing the same |
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FR2970238B1 (en) * | 2011-01-07 | 2013-01-25 | Airbus Operations Sas | PIECE AND METHOD FOR REPAIRING A DAMAGED STRUCTURE, ESPECIALLY AIRCRAFT SKIN, AND A REPAIR KIT FOR IMPLEMENTING THE SAME |
JP5598528B2 (en) * | 2012-11-29 | 2014-10-01 | 株式会社豊田自動織機 | Tubular fiber structure |
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1990
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Cited By (5)
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EP3608091A1 (en) * | 2018-08-10 | 2020-02-12 | Crompton Technology Group Limited | Composite connector and method of manufacturing the same |
US11859739B2 (en) | 2018-08-10 | 2024-01-02 | Crompton Technology Group Limited | Composite connectors and methods of manufacturing the same |
US11975498B2 (en) | 2018-08-10 | 2024-05-07 | Crompton Technology Group Limited | Composite connectors and methods of manufacturing the same |
US11976686B2 (en) | 2018-08-10 | 2024-05-07 | Crompton Technology Group Limited | Composite connectors and methods of manufacturing the same |
US11761562B2 (en) | 2019-10-07 | 2023-09-19 | Crompton Technology Group Limited | Fibre reinforced polymer composite pipes |
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JPH04108138A (en) | 1992-04-09 |
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