JP3954611B2 - Method for producing three-dimensional inorganic fiber fabric - Google Patents

Method for producing three-dimensional inorganic fiber fabric Download PDF

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JP3954611B2
JP3954611B2 JP2004350521A JP2004350521A JP3954611B2 JP 3954611 B2 JP3954611 B2 JP 3954611B2 JP 2004350521 A JP2004350521 A JP 2004350521A JP 2004350521 A JP2004350521 A JP 2004350521A JP 3954611 B2 JP3954611 B2 JP 3954611B2
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yarn
fiber
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woven
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JP2006161184A (en
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陽一 菅野
文明 三浦
浩 長沢
哲司 伊藤
正尚 吉田
慎 東瀬
ふさ子 佐々木
彰 古舘
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福島県
株式会社ニーズプロダクト
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  • Treatment Of Fiber Materials (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
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Description

本発明は、繊維強化樹脂材料の骨格材として使用される炭素繊維、ガラス繊維または炭化ケイ素系繊維などの無機繊維織物複数枚積層した三次元無機繊維織物の製造方法に関するものである。 The present invention relates to a manufacturing method of a three dimensional inorganic fiber woven fabric has carbon fibers used as a skeletal material for the fiber reinforced resin material, an inorganic fiber fabric, such as glass fibers or silicon carbide fiber laminating a plurality.

近年、炭素繊維を用いた織物を重ねて骨格材とし、これに樹脂を含浸させて所定の形状に成型した繊維強化樹脂材料が、ロケットや航空機、電車、自動車のボディー材料として使用されるようになってきた。従来の炭素繊維織物を製造する方法は、図10に示すように、複数本の炭素繊維1を束ねてこれに樹脂を含浸させて帯状の糸2を形成し、これを経糸Xと緯糸Yとして製織し、炭素繊維織物3を形成している。これは樹脂を含浸させて帯状に形成した糸2を使用しているので、可撓性が少なく、炭素繊維1を曲げると折損する問題があり、製織する工程での取扱が面倒であった。 In recent years, fiber reinforced resin materials, which are made of carbon fiber woven fabrics and used as skeleton materials, impregnated with resin and molded into a predetermined shape, are used as body materials for rockets, aircraft, trains, and automobiles. It has become. As shown in FIG. 10 , a conventional method for producing a carbon fiber fabric is a method of bundling a plurality of carbon fibers 1 and impregnating them with a resin to form a band-like yarn 2, which is used as warp yarn X and weft yarn Y. The carbon fiber fabric 3 is formed by weaving. Since this uses the yarn 2 formed by impregnating the resin and formed into a belt shape, the flexibility is low, and there is a problem of breaking when the carbon fiber 1 is bent, and handling in the weaving process is troublesome.

また図11に示すように炭素繊維織物3を積層して縫合する場合、従来はZピン方式や、ステッチ方式(例えば特許文献1)などの方法により行なっていたが、ミシン針4を挿入する時に炭素繊維1と衝突して繊維の糸切れや摩耗などの損傷を生じて強度が低下する問題があった。特にロケットや航空機の翼やボディーなど、薄くて高強度が要求される繊維強化樹脂材料の骨格材として用いる場合には、縫合時の炭素繊維1の糸切れが強度を低下させる大きな問題となっていた。
特開2003−342856
In addition, as shown in FIG. 11 , when the carbon fiber fabrics 3 are laminated and stitched, the conventional methods such as the Z-pin method and the stitch method (for example, Patent Document 1) have been used, but when the sewing needle 4 is inserted. There was a problem that the carbon fiber 1 collides with the fiber, causing damage such as fiber breakage or wear, resulting in a decrease in strength. In particular, when used as a skeleton material for fiber-reinforced resin materials that are thin and require high strength, such as rockets and aircraft wings and bodies, thread breakage of the carbon fiber 1 at the time of stitching has become a major problem in reducing strength. It was.
JP2003-342856

本発明は上記問題を改善し、炭素繊維、ガラス繊維または炭化ケイ素系繊維などの無機繊維の糸に可撓性を持たせて、製織時の折損を防止すると共に、この無機繊維織物を積層して縫合する場合、ミシン針と無機繊維との衝突を回避して繊維の糸切れや摩耗などの損傷を防止し、繊維強化樹脂材料の骨格材として有効な強度の高い三次元無機繊維織物の製造方法を提供するものである。 The present invention improves the above-mentioned problems, and imparts flexibility to the yarns of inorganic fibers such as carbon fibers, glass fibers, or silicon carbide fibers to prevent breakage during weaving and to laminate this inorganic fiber fabric. When sewing, the collision between the sewing needle and the inorganic fiber is avoided to prevent damage such as thread breakage or abrasion of the fiber, and the production of a high-strength three-dimensional inorganic fiber fabric that is effective as a skeleton material for fiber-reinforced resin materials A method is provided.

本発明の請求項1記載の三次元無機繊維織物の製造方法は、複数本の無機繊維を束ねて、水溶性または可燃性の鞘糸でカバーリングして収束し、このカバーリングした収束糸を、認識糸を織り込んでミシン針が貫通する空隙を形成するように製織してメッシュ状の織物を形成した後、この織物を複数枚積層してテーブルにセットし、CCDカメラを取付けたミシンまたは/および前記テーブルをX―Y方向に移動可能な送り装置に取付けて、CCDカメラにより認識糸の位置を画像認識し、前記認識糸をガイドとして送り装置を制御し、空隙の位置にミシン針を挿入して縫合糸により積層織物間の縫合を行なった後、カバーリングした鞘糸を精練または焼却して開繊することを特徴とするものである。
In the method for producing a three-dimensional inorganic fiber fabric according to claim 1 of the present invention, a plurality of inorganic fibers are bundled and covered with a water-soluble or combustible sheath yarn to converge. After forming a mesh fabric by weaving the recognition yarn so as to form a gap through which the sewing needle penetrates, a plurality of these fabrics are stacked and set on a table, and / or a sewing machine attached with a CCD camera The table is attached to a feeding device that can move in the XY directions, the position of the recognition thread is recognized by a CCD camera, the feeding device is controlled using the recognition thread as a guide, and a sewing needle is inserted into the gap position. Then, after the laminated fabrics are sutured with sutures, the covered sheath yarns are scoured or incinerated to be opened.

本発明の請求項2記載の三次元無機繊維織物の製造方法は、無機繊維が炭素繊維、ガラス繊維または炭化ケイ素系繊維であることを特徴とものである。 The method for producing a three-dimensional inorganic fiber fabric according to claim 2 of the present invention is characterized in that the inorganic fiber is carbon fiber, glass fiber, or silicon carbide fiber.

本発明の請求項記載の三次元無機繊維織物の製造方法は、認識糸として、無機繊維と色差のある繊維、または蛍光処理した繊維を用いることを特徴とするものである。 The method for producing a three-dimensional inorganic fiber fabric according to claim 3 of the present invention is characterized in that a fiber having a color difference from the inorganic fiber or a fiber subjected to fluorescence treatment is used as the recognition yarn.

本発明に係る請求項1記載の三次元無機繊維織物の製造方法によれば、複数本の無機繊維を束ねて、水溶性または可燃性の鞘糸でカバーリングして収束糸の状態にしてから織物にするので、取扱が容易で曲げによる折損を防止できる。また無機繊維織物をミシン針が貫通する空隙が形成されているメッシュ状の織物の状態で積層して、積層織物間を縫合するので、ミシン針とメッシュ状の織物の面内糸である無機繊維との衝突が回避されて無機繊維の糸切れや摩耗などの損傷を防止することができる。この時、無機繊維織物に認識糸を織り込んで、CCDカメラにより認識糸の位置を画像認識し、この位置に基づいてミシン針の挿入部分をコンピュータで演算して、その位置座標を決定するので、メッシュ状の織物をテーブル上に斜めにセットしても認識糸に沿って縫合していき無機繊維の切断を防止することができるAccording to the method for producing a three-dimensional inorganic fiber fabric according to claim 1 of the present invention, a plurality of inorganic fibers are bundled and covered with a water-soluble or combustible sheath yarn to form a convergent yarn state. since the fabric, Ru prevent breakage due to bending is easy to handle. In addition, since inorganic fiber fabrics are laminated in the state of a mesh-like fabric in which a gap through which a sewing needle penetrates is formed, and stitched between the laminated fabrics, the inorganic fibers that are the in-plane threads of the sewing needle and the mesh-like fabric Can be avoided, and damage such as thread breakage and wear of the inorganic fiber can be prevented. At this time, the recognition yarn is woven into the inorganic fiber fabric, the position of the recognition yarn is image-recognized by the CCD camera, and the position of the sewing needle is calculated by the computer based on this position, and the position coordinate is determined. Even if a mesh-like woven fabric is set obliquely on a table, it can be sewn along the recognition yarn to prevent the inorganic fibers from being cut .

また請求項2記載の三次元無機繊維織物の製造方法によれば、無機繊維が炭素繊維、ガラス繊維または炭化ケイ素系繊維など、可撓性が低い繊維でも収束糸の状態にしてから織物にするので、取扱が容易で曲げによる折損を防止することができる。 According to the method for producing a three-dimensional inorganic fiber woven fabric according to claim 2, even if the inorganic fiber is a low-flexibility fiber such as carbon fiber, glass fiber or silicon carbide fiber, it is made into a convergent yarn state and then made into a woven fabric. Therefore, handling is easy and breakage due to bending can be prevented.

また請求項記載の三次元無機繊維織物の製造方法によれば、認識糸として、無機繊維と色差のある繊維、または蛍光処理した繊維を用いることにより、CCDカメラによる認識糸の位置の認識が容易である。 According to the method for manufacturing a three-dimensional inorganic fiber fabric according to claim 3 , the recognition yarn position can be recognized by the CCD camera by using a fiber having a color difference from the inorganic fiber or a fiber subjected to fluorescence treatment as the recognition yarn. Easy.

以下本発明の実施の一形態を図1ないし図を参照して詳細に説明する。先ず図1(A)に示すように、複数本の炭素繊維1に樹脂を少し含浸させて帯状に形成した糸2を芯糸として、水溶性または可燃性の鞘糸5でカバーリングした収束糸6を形成する。水溶性の鞘糸5としては、例えば湯で溶解するポリビニールアルコール糸を用い、また可燃性の鞘糸5としては、例えばナイロン糸やポリエステル糸など焼却できる繊維を用いる。 Hereinafter an embodiment of the present invention with reference to FIGS be described in detail. First, as shown in FIG. 1 (A), a convergent yarn covered with a water-soluble or combustible sheath yarn 5 using a yarn 2 formed by impregnating a plurality of carbon fibers 1 with a little resin and formed into a belt shape as a core yarn. 6 is formed. As the water-soluble sheath yarn 5, for example, a polyvinyl alcohol yarn that dissolves in hot water is used, and as the combustible sheath yarn 5, for example, a nylon fiber or a polyester yarn that can be incinerated is used.

またこのカバーリング方法としてはシングル巻きでも、あるいは図1(B)に示すように、ダブル巻きでも良い。次に、カバーリングした収束糸6を経糸Xと緯糸Yとして製織機で平織すると、図2に示すように空隙7が格子状に形成されたメッシュ状の織物8が製織される。このように複数本の炭素繊維1を芯糸として鞘糸5でカバーリングすることにより、収束糸6は丸糸となってその外周が鞘糸5で補強されるので、炭素繊維1は曲げに対して強くなり、糸の取扱が容易で、準備や製織工程がスムーズに行なえる。 Further, the covering method may be single winding or double winding as shown in FIG. Next, when the covered converging yarn 6 is plain-woven with a weaving machine as warp yarn X and weft Y, a mesh-like woven fabric 8 in which voids 7 are formed in a lattice shape as shown in FIG. 2 is woven. By covering the plurality of carbon fibers 1 with the sheath yarn 5 as a core yarn in this way, the converging yarn 6 becomes a round yarn and the outer periphery thereof is reinforced with the sheath yarn 5, so that the carbon fiber 1 is bent. It is strong against thread handling, and the preparation and weaving process can be performed smoothly.

次に画像認識により縫合する場合、先ずに示すように、カバーリングした収束糸6を筬15に通す。この筬15は、単位幅の羽16を3個並設し、この横に単位幅の半分の幅の空き羽17を形成し、羽16にそれぞれカバーリングした収束糸6を通すと共に、空き羽17の片側に隣接する羽16に認識糸18を通して織成すると図に示すように、認識糸18を織り込んだミシン針4が貫通する空隙7を形成したメッシュ状の織物8Aが形成される。 If you then sutured by the image recognition, first, as shown in FIG. 3, through a convergence yarn 6 which is covering the reed 15. This ridge 15 has three unit width wings 16 arranged side by side, forming vacant wings 17 having a width half of the unit width on the side, and passing the converging yarns 6 respectively covering the wings 16, and vacant wings the wing 16 adjacent to one side of 17 and weaving through recognition yarns 18 as shown in FIG. 4, mesh-like fabric. 8A sewing needle 4 woven recognition yarn 18 to form a gap 7 which penetrates.

またこれとは別に、認識糸18を入れずに図に示す筬15にカバーリングした収束糸6だけを通して製織し、図2に示すようにミシン針4が貫通する空隙7を形成したメッシュ状の織物8Bを2枚形成する。この認識糸18のない2枚のメッシュ状の織物8Bを重ね、更に一番上に認識糸18を入れたメッシュ状の織物8Aを図に示すように重ねて、縫合糸11で縫合する。この認識糸18としてはカバーリングした炭素繊維1の収束糸6が灰色なので、これと色調の異なる例えば白色のものを用いる。またこの認識糸18は、鞘糸5と同様に精練または焼却して開繊できる材質が好ましい。 Separately from this, weaving is performed only through the converging yarn 6 covered on the ridge 15 shown in FIG. 3 without inserting the recognition yarn 18, and a mesh 7 in which a gap 7 through which the sewing needle 4 passes is formed as shown in FIG. 2. Two woven fabrics 8B are formed . Overlapping two mesh fabrics 8B without this recognition yarn 18, further a mesh-like fabric 8A containing the recognized yarn 18 superimposed as shown in FIG. 4 at the top, sutured with sutures 11. As the recognition yarn 18, the converged yarn 6 of the covered carbon fiber 1 is gray. The recognition yarn 18 is preferably made of a material that can be opened by scouring or incineration in the same manner as the sheath yarn 5.

このミシン装置は、図および図に示すように基台20の上に縦方向に沿って2本のレール21が取付けられ、ここにローラ22を設けたテーブル23が縦方向に可動自在に取付けられている。このテーブル23のフレーム24は、図に示すように基台20に取付けたモータ25に接続したボールネジ26によりX方向に可動自在に支持されている。 In this sewing machine, as shown in FIGS. 6 and 7 , two rails 21 are mounted on a base 20 along a vertical direction, and a table 23 provided with a roller 22 is movable in the vertical direction. Installed. Frame 24 of the table 23 is movably supported in the X direction by a ball screw 26 connected to a motor 25 mounted to the base 20 as shown in FIG.

またミシン27は図に示すように、両側にモータ支持台28、28が立設されこの間にY方向に可動自在に支持されている。モータ支持台28、28の間には2本のボールネジ26、26と2本のミシン駆動シャフト30、30およびガイドレール41が平行に取付けられている。上部のボールネジ26はモータ31に接続され、ベルト32を介して下部のボールネジ26に連結され、同期して回転するようになっている。また上部のミシン駆動シャフト30はモータ33に接続され、ベルト32を介して下部のミシン駆動シャフト30に連結され、同期して回転するようになっている。 In addition, as shown in FIG. 6 , motor support bases 28 and 28 are provided upright on both sides of the sewing machine 27, and are supported movably in the Y direction therebetween. Two ball screws 26, 26, two sewing machine drive shafts 30, 30 and a guide rail 41 are attached between the motor support bases 28, 28 in parallel. The upper ball screw 26 is connected to a motor 31 and connected to the lower ball screw 26 via a belt 32 so as to rotate synchronously. The upper sewing machine drive shaft 30 is connected to a motor 33 and is connected to the lower sewing machine drive shaft 30 via a belt 32 so as to rotate synchronously.

上部のボールネジ26とガイドレール41にはミシン支持部34が取付けられ、Y方向に可動自在に支持されている。また針板35に取付けた釜36は下部のボールネジ26と下部のミシン駆動シャフト30に取付けられ、Y方向に可動自在に支持されている。前記ミシン支持部34にはシリンダ37とガイドシャフト38によりミシン本体39が上下動自在に支持されている。 A sewing machine support portion 34 is attached to the upper ball screw 26 and the guide rail 41, and is supported so as to be movable in the Y direction. The shuttle 36 attached to the needle plate 35 is attached to the lower ball screw 26 and the lower sewing machine drive shaft 30 and is supported movably in the Y direction. A sewing machine main body 39 is supported on the sewing machine support portion 34 by a cylinder 37 and a guide shaft 38 so as to be movable up and down.

このミシン本体39に取付けたミシン針4は、図示しない駆動機構を介して上部のミシン駆動シャフト30に連結され、このミシン針4と下方の釜36とは同期してY方向に移動するようになっている。更にミシン本体39の横にはCCDカメラ40が斜め下方に向かって取付けられている。 The sewing machine needle 4 attached to the sewing machine body 39 is connected to the upper sewing machine drive shaft 30 via a drive mechanism (not shown), and the sewing machine needle 4 and the lower shuttle 36 move in the Y direction in synchronization. It has become. Further, a CCD camera 40 is attached to the side of the sewing machine main body 39 obliquely downward.

次に上記構成のミシン27により縫合する作用について説明すると、先ずテーブル23の上に、図に示すように認識糸18のない2枚のメッシュ状の織物8Bを重ね、更に一番上に認識糸18を入れたメッシュ状の織物8Aを重ねてセットする。次にCCDカメラ40で一番上に重ねたメッシュ状の織物8Aの画像を認識して、認識糸18、18が交差する部分Cを検知する。この検知した交差部分Cから所定のXーY方向に離れた距離に設定したミシン針4の挿入部分をコンピュータで演算して、その位置座標を決定する。 Next, to explain the action of sutured sewing machine 27 having the above structure, first, on the table 23, stacked two meshed fabric 8B without recognition yarns 18 as shown in FIG. 4, further recognition at the top The mesh-shaped woven fabric 8A containing the yarn 18 is set in an overlapping manner. Next, the CCD camera 40 recognizes the image of the mesh fabric 8A superimposed on the top, and detects the portion C where the recognition yarns 18 and 18 intersect. The insertion portion of the sewing needle 4 set at a distance away from the detected crossing portion C in a predetermined XY direction is calculated by a computer, and its position coordinates are determined.

次にこの位置情報に基づいてモータ25を駆動させると、テーブル23がX方向に移動し、モータ31を駆動させると、ミシン針4と釜36が動機してY方向に移動して、前記位置座標までメッシュ状の織物8を移動させる。ここでモータ33を駆動させることによりミシン針4が上下動し、釜36が回転して縫合糸11により縫合される。この過程で、CCDカメラ40で画像を認識して、隣接する認識糸18、18の交差部分Cを検知し、ミシン針4の次の挿入部分の位置座標を演算している。このように認識糸18の交差部分Cを画像認識しながら順次縫合することにより、図に示す状態とする。 Next, when the motor 25 is driven based on this position information, the table 23 moves in the X direction, and when the motor 31 is driven, the sewing needle 4 and the shuttle 36 move to move in the Y direction, and the position is The mesh fabric 8 is moved to the coordinates. Here, by driving the motor 33, the sewing needle 4 moves up and down, and the shuttle 36 rotates and is sutured by the suture thread 11. In this process, the image is recognized by the CCD camera 40, the crossing portion C of the adjacent recognition threads 18 and 18 is detected, and the position coordinates of the next insertion portion of the sewing needle 4 are calculated. By sequentially suturing while thus the intersection C of the recognition thread 18 and image recognition, and the state shown in FIG.

この場合、図8に示すようにミシンで縫合すると、ミシン針4は空隙7を貫通して、図に示すようにPBO繊維、アラミド繊維、炭素繊維などの縫合糸11で縫合される。この時、ミシン針4としては先端が球形のボール状になったものや、あるいは図に示すようにボールペン状にボール12が回転自在に支持されたものを使用する。従って先端が、球状に形成されたミシン針4がメッシュ状の織物8の面内糸であるカバーリングされた収束糸6と衝突しても、互いに断面が円形であるのでその表面で滑って、収束糸6を損傷することなく縫合することができる。 In this case, when sutured with perforations, as shown in FIG. 8, the needle 4 extends through the gaps 7, PBO fibers as shown in FIG. 4, aramid fibers, is sutured with sutures 11 such as carbon fiber. At this time, as the sewing needle 4, a needle having a spherical ball tip, or a ball pen-shaped ball 12 rotatably supported as shown in FIG. 9 is used. Therefore, even if the tip 4 of the sewing needle 4 formed into a spherical shape collides with the covered converging yarn 6 that is an in-plane yarn of the mesh-like woven fabric 8, the cross-sections of the sewing needles 4 are circular so that they slide on the surface. The converging thread 6 can be sutured without being damaged.

このように、水溶性の鞘糸5でカバーリングされた収束糸6により製織したメッシュ状の織物8Aと8Bとを重ねて縫合した後、これを湯に浸漬して鞘糸5を溶解させて精練すると、収束していた炭素繊維1が開繊し、図に示すように経糸Xと緯糸Yが密に織られた三次元炭素繊維織物13が形成される。また可燃性の鞘糸5でカバーリングされた収束糸6により製織したメッシュ状の織物8は、バーナーで燃焼すると鞘糸5が焼却されて、収束していた炭素繊維1だけが残って開繊し、密に織られた三次元炭素繊維織物13が形成される。 In this way, mesh fabrics 8A and 8B woven with converging yarns 6 covered with water-soluble sheath yarns 5 are overlapped and stitched, and then immersed in hot water to dissolve sheath yarns 5. When scouring, the converged carbon fibers 1 are opened, and a three-dimensional carbon fiber woven fabric 13 in which warp yarns X and weft yarns Y are densely woven as shown in FIG. 5 is formed. The mesh fabric 8 woven with the converging yarn 6 covered with the combustible sheath yarn 5 is burned by the burner, so that the sheath yarn 5 is incinerated, and only the converged carbon fiber 1 remains to open the fiber. As a result, a densely woven three-dimensional carbon fiber fabric 13 is formed.

従って本発明方法によれば、ミシン針4が貫通する空隙7が形成されているメッシュ状の織物8の状態で積層して縫合するので、ミシン針4とメッシュ状の織物8の面内糸である炭素繊維1との衝突が回避されて炭素繊維1の糸切れや摩耗などの損傷が防止される。更にこれを縫合・開繊することにより三次元炭素繊維織物13を製造するので、これを骨格材として使用した繊維強化樹脂材料の強度を向上させることができる。 Therefore, according to the method of the present invention, since the layers are stitched in the state of the mesh fabric 8 in which the gap 7 through which the sewing needle 4 passes is formed, the in-plane thread of the sewing needle 4 and the mesh fabric 8 is used. Collision with a certain carbon fiber 1 is avoided, and damage such as thread breakage or wear of the carbon fiber 1 is prevented. Furthermore, since the three-dimensional carbon fiber fabric 13 is manufactured by stitching and opening it, the strength of the fiber reinforced resin material using this as a skeleton material can be improved.

このように、CCDカメラ40により、認識糸18の交差部分Cの位置を画像処理して認識し、この位置に基づいてミシン針4の挿入部分をコンピュータで演算して、その位置座標を決定するので、メッシュ状の織物8をフレーム24上に斜めにセットしても炭素繊維1の切断を防止することができる。更に、筬15は図に示すように、認識糸18を通した部分の横に空き羽17を形成し、この広い部分にミシン針4の挿入部の位置座標を設定しているので、炭素繊維1の切断を防止することができる。 In this way, the CCD camera 40 recognizes the position of the crossing portion C of the recognition yarn 18 by image processing, and based on this position, the computer inserts the insertion portion of the sewing needle 4 and determines its position coordinates. Therefore, even if the mesh-like woven fabric 8 is set on the frame 24 at an angle, the carbon fiber 1 can be prevented from being cut. Further, as shown in FIG. 3 , the heel 15 has an empty wing 17 formed next to the portion through which the recognition thread 18 is passed, and the position coordinates of the insertion portion of the sewing needle 4 are set in this wide portion. Cutting of the fiber 1 can be prevented.

なお上記説明ではテーブル23をX方向に、ミシン27をY方向に移動させる場合について示したが、テーブル23を固定し、ミシン27をXーY方向に移動させても良く、またミシン27を固定し、テーブル23をXーY方向に移動させる構造でも良い。この場合、CCDカメラ40はテーブル23に取付けても良い。また認識糸18としてカバーリングした収束糸6と色差のある繊維を用いた場合について示したが、蛍光処理した繊維を用いることもでき、この場合には紫外線を照射しながら、発光した認識糸18をCCDカメラ40で認識しながら縫合する。 In the above description, the table 23 is moved in the X direction and the sewing machine 27 is moved in the Y direction. However, the table 23 may be fixed and the sewing machine 27 may be moved in the XY direction, and the sewing machine 27 is fixed. However, a structure in which the table 23 is moved in the XY direction may be used. In this case, the CCD camera 40 may be attached to the table 23. Further, although the case where the converging yarn 6 covered and the fiber having a color difference are used as the recognition yarn 18 is shown, a fluorescent-treated fiber can also be used. In this case, the recognition yarn 18 emitted while emitting ultraviolet rays. Is sewn while being recognized by the CCD camera 40.

なお上記説明では無機繊維として炭素繊維を用いた場合について説明したが、ガラス繊維または炭化ケイ素系繊維を用いても同様の効果を得ることができる。 In addition, although the case where carbon fiber was used as an inorganic fiber was demonstrated in the said description, the same effect can be acquired even if it uses glass fiber or a silicon carbide type fiber.

以下本発明の実施例を説明する。炭素繊維1を6000本、帯状に形成した糸2を、ポリビニールアルコール糸を鞘糸5としてダブルカバーリングして灰色の収束糸6を形成する。これを経糸Xおよび緯糸Yとし、また認識糸18として白色のポリビニールアルコール糸を用い、これを図に示す筬15に通して製織し、幅40cm、長さ1mのメッシュ状の織物8Aを形成した。この場合、筬密度は地部が6.5(羽/cm)、空き羽13.0(羽/cm)とし、経糸総数を365本(地部の炭素繊維収束糸156本、耳部の炭素繊維収束糸156本、認識糸53本)、緯糸打込数16.5(本/吋)とし、糸配列を炭素繊維収束糸3本、認識糸1本の繰り返しとした。 Examples of the present invention will be described below. A gray converging yarn 6 is formed by double covering the yarn 2 formed of 6000 carbon fibers 1 in a belt shape with a polyvinyl alcohol yarn as a sheath yarn 5. These are used as warp yarn X and weft yarn Y, and white polyvinyl alcohol yarn is used as recognition yarn 18, and this is woven through a ridge 15 shown in FIG. 3 to form a mesh-like fabric 8A having a width of 40 cm and a length of 1 m. Formed. In this case, the density of the cocoon is 6.5 (wings / cm) for the ground portion, 13.0 (wings / cm) for the free wings, and the total number of warps is 365 (156 carbon fiber converging yarns for the ground portion, carbon for the ear portion) 156 fiber converging yarns, 53 recognition yarns), weft threading number of 16.5 (lines / 吋), and the yarn arrangement was a repetition of 3 carbon fiber converging yarns and 1 recognition yarn.

また同様に認識糸18を入れずに平織したメッシュ状の織物8Bを2枚形成した。次に図および図に示すテーブル23の上に、認識糸18のない2枚のメッシュ状の織物8Bを重ね、更に一番上に認識糸18を入れたメッシュ状の織物8Aを重ねてセットする。次にCCDカメラ40で一番上に重ねたメッシュ状の織物8Aの画像を認識して、認識糸18、18が交差する部分Cを検知し、この検知した交差部分から所定のXーY方向に離れた距離に設定したミシン針4の挿入部分をコンピュータで演算して、その位置座標を決定する。 Similarly, two plain-woven mesh fabrics 8B without forming the recognition yarn 18 were formed. Next, on the table 23 shown in FIGS. 6 and 7 , two mesh fabrics 8B without the recognition yarn 18 are stacked, and further, the mesh fabric 8A with the recognition yarn 18 placed on top is stacked. set. Next, the image of the mesh fabric 8A superimposed on the top is recognized by the CCD camera 40, and a portion C where the recognition yarns 18 and 18 intersect is detected, and a predetermined XY direction is detected from the detected intersection. The computer inserts the insertion portion of the sewing machine needle 4 set at a distance away from the center, and determines its position coordinates.

次にこの位置座標に基づいてテーブル23をX方向に、ミシン針4と釜36をY方向に移動して、前記位置座標までメッシュ状の織物8A、8Bを移動させて、ミシン針4を上下動させてアラミド繊維糸を縫合糸11として順次縫合して図4の状態にする。次に3枚縫合されたメッシュ状の織物8A、8Bを湯に浸漬して、ポリビニールアルコール糸で形成された鞘糸5と認識糸18を溶解させて精練すると、図5に示すように収束していた炭素繊維1が開繊し、密に織られた三次元炭素繊維織物13が形成された。この三次元炭素繊維織物13はミシン針4による炭素繊維1の損傷がなく、繊維強化樹脂材料の骨格材として強度の高い織物を得ることができた。 Next, based on the position coordinates, the table 23 is moved in the X direction, the sewing needle 4 and the shuttle 36 are moved in the Y direction, the mesh fabrics 8A and 8B are moved to the position coordinates, and the sewing needle 4 is moved up and down. The aramid fiber thread is sequentially sutured as the suture thread 11 to the state shown in FIG . Next, the mesh fabrics 8A and 8B stitched in three pieces are dipped in hot water, and the sheath yarn 5 and the recognition yarn 18 formed of polyvinyl alcohol yarn are dissolved and refined to converge as shown in FIG. The carbon fiber 1 was opened, and a densely woven three-dimensional carbon fiber fabric 13 was formed. This three-dimensional carbon fiber fabric 13 did not damage the carbon fiber 1 by the sewing needle 4, and a high strength fabric could be obtained as a skeleton material of the fiber reinforced resin material.

本発明方法により製造された三次元無機繊維織物は、ロケットや航空機、電車、自動車のボディー材料として使用される繊維強化樹脂材料の骨格材として広く利用することができる。 The three- dimensional inorganic fiber fabric produced by the method of the present invention can be widely used as a skeleton material for fiber-reinforced resin materials used as body materials for rockets, aircraft, trains, and automobiles.

(A)、(B)は炭素繊維をカバーリングして収束糸を形成している状態を示す正面図である。(A), (B) is a front view which shows the state which covers carbon fiber and forms the convergence yarn. 図1のカバーリングした収束糸を用いて平織したメッシュ状の織物を示す平面図である。It is a top view which shows the mesh-shaped textile fabric plain-woven using the converged yarn which covered FIG. 収束糸と認識糸を通した筬を示す正面図である。It is a front view which shows the wrinkles which passed the convergence yarn and the recognition yarn. 認識糸を織り込んだメッシュ状の織物を重ねて縫合糸で縫合した状態を示す平面図である。It is a top view which shows the state which piled up the mesh-shaped textile fabric which woven the recognition thread | yarn, and was sewn with the suture thread. に示す縫合したメッシュ状の織物を開繊した三次元炭素繊維織物を示す平面図である。FIG. 5 is a plan view showing a three-dimensional carbon fiber fabric obtained by opening the stitched mesh fabric shown in FIG. 4 . ミシンを示す正面図である。It is a front view which shows a sewing machine. ミシンを示す側面図である。It is a side view which shows a sewing machine. 平織したメッシュ状の織物を複数枚重ねてミシンで縫合している状態を示す断面図である。It is sectional drawing which shows the state which piles up the multiple mesh fabrics which carried out plain weaving, and was sewn with the sewing machine. ボールが回転自在に支持されたミシン針を示す断面図である。It is sectional drawing which shows the sewing needle with which the ball was rotatably supported. 従来の帯状の炭素繊維糸を平織した炭素繊維織物を示す平面図である。It is a top view which shows the carbon fiber fabric which plain-woven the conventional strip-shaped carbon fiber yarn. 10の炭素繊維織物を複数枚重ねてミシンで縫合している状態を示す断面図である。It is sectional drawing which shows the state which piles up several carbon fiber fabrics of FIG. 10 , and is sewn with the sewing machine.

符号の説明Explanation of symbols

1 炭素繊維
2 帯状の糸
3 炭素繊維織物
4 ミシン針
5 鞘糸

6 カバーリングした収束糸
7 空隙
8 メッシュ状の織物
9 炭素繊維織物
11 縫合糸
12 ボール
13 三次元炭素繊維織物
15 筬
16 羽

17 空き羽
18 認識糸
20 基台
21 レール
22 ローラ
23 テーブル
24 フレーム
25 モータ
26 ボールネジ

27 ミシン
28 モータ支持台
30 ミシン駆動シャフト
31 モータ
32 ベルト
33 モータ
34 ミシン支持部
35 針板
36 釜

37 シリンダ
38 ガイドシャフト
39 ミシン本体
40 CCDカメラ
1 Carbon fiber
2 Banded thread
3 Carbon fiber fabric
4 Sewing needle
5 sheath thread

6 Covered converging yarn
7 gap
8 Mesh fabric
9 Carbon fiber fabric
11 Suture
12 balls
13 Three-dimensional carbon fiber fabric
15 筬
16 wings

17 Empty feathers
18 Recognition thread
20 base
21 rails
22 Laura
23 tables
24 frames
25 motor
26 Ball screw

27 Sewing machine
28 Motor support
30 Sewing machine drive shaft
31 motor
32 belts
33 Motor
34 Sewing machine support
35 needle plate
36 Kettle

37 cylinders
38 Guide shaft
39 Sewing machine
40 CCD camera

Claims (3)

複数本の無機繊維を束ねて、水溶性または可燃性の鞘糸でカバーリングして収束し、このカバーリングした収束糸を、認識糸を織り込んでミシン針が貫通する空隙を形成するように製織してメッシュ状の織物を形成した後、この織物を複数枚積層してテーブルにセットし、CCDカメラを取付けたミシンまたは/および前記テーブルをX―Y方向に移動可能な送り装置に取付けて、CCDカメラにより認識糸の位置を画像認識し、前記認識糸をガイドとして送り装置を制御し、空隙の位置にミシン針を挿入して縫合糸により積層織物間の縫合を行なった後、カバーリングした鞘糸を精練または焼却して開繊することを特徴とする三次元無機繊維織物の製造方法。 Bundling a plurality of inorganic fibers and covering them with water-soluble or combustible sheath yarns to converge, and weaving the covered converged yarns so that a recognition thread is woven and a gap is formed through the sewing needle. After forming a mesh-like woven fabric, a plurality of the woven fabrics are stacked and set on a table, a sewing machine with a CCD camera attached and / or the table is attached to a feeding device that can move in the XY direction, The position of the recognition thread is recognized by a CCD camera, the feeding device is controlled using the recognition thread as a guide, a sewing needle is inserted at the position of the gap, and stitching between the laminated fabrics is performed with the suture, and then the covering is performed. A method for producing a three-dimensional inorganic fiber fabric, characterized in that the sheath yarn is scoured or incinerated for opening. 無機繊維が炭素繊維、ガラス繊維または炭化ケイ素系繊維であることを特徴とする請求項1記載の三次元無機繊維織物の製造方法。 The method for producing a three-dimensional inorganic fiber fabric according to claim 1, wherein the inorganic fibers are carbon fibers, glass fibers, or silicon carbide fibers. 認識糸として、無機繊維と色差のある繊維、または蛍光処理した繊維を用いることを特徴とする請求項1記載の三次元無機繊維織物の製造方法。 The method for producing a three-dimensional inorganic fiber fabric according to claim 1, wherein a fiber having a color difference from the inorganic fiber or a fiber subjected to fluorescence treatment is used as the recognition yarn.
JP2004350521A 2004-12-03 2004-12-03 Method for producing three-dimensional inorganic fiber fabric Expired - Fee Related JP3954611B2 (en)

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JP5092288B2 (en) 2005-09-02 2012-12-05 三菱化学株式会社 Adhesive resin composition and laminate
CN103288461A (en) * 2013-04-25 2013-09-11 利津县慧通纤维材料有限公司 Degraded high-performance ceramic-fiber-based composite cloth and preparation method thereof
CN103361828A (en) * 2013-07-31 2013-10-23 吴江市欧冠纺织有限公司 Bamboo carbon fabric
JP6338146B2 (en) * 2014-05-12 2018-06-06 兵庫県 Fiber material for use at the ear during weaving
CN117512877B (en) * 2023-11-03 2024-04-16 绍兴红葡萄纺织装饰品有限公司 Layer-fused sun-shading fabric, hook machine for manufacturing and manufacturing method

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