WO2014034606A1 - Three-dimensional fiber structure, prepreg using same and process for manufacturing three-dimensional fiber structure - Google Patents

Three-dimensional fiber structure, prepreg using same and process for manufacturing three-dimensional fiber structure Download PDF

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Publication number
WO2014034606A1
WO2014034606A1 PCT/JP2013/072736 JP2013072736W WO2014034606A1 WO 2014034606 A1 WO2014034606 A1 WO 2014034606A1 JP 2013072736 W JP2013072736 W JP 2013072736W WO 2014034606 A1 WO2014034606 A1 WO 2014034606A1
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yarn
fiber
dimensional
fiber structure
laminated
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PCT/JP2013/072736
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French (fr)
Japanese (ja)
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原田 亮
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株式会社 豊田自動織機
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Publication of WO2014034606A1 publication Critical patent/WO2014034606A1/en

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    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/22Yarns or threads characterised by constructional features, e.g. blending, filament/fibre
    • D02G3/36Cored or coated yarns or threads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/514Oriented
    • B32B2307/518Oriented bi-axially
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness

Definitions

  • the present invention relates to a three-dimensional fiber structure, a prepreg using the same, and a method for manufacturing the three-dimensional fiber structure.
  • Fiber reinforced composite materials are widely used as lightweight structural materials.
  • a three-dimensional fiber structure such as a three-dimensional fabric as a reinforcing base material for a composite material.
  • a bent portion instead of a simple flat plate shape.
  • a frame corresponding to the shape of the three-dimensional fiber structure is provided, and a plurality of frames are provided on the frame.
  • a method of using a device in which the regulating members are arranged at a predetermined pitch see Patent Document 1.
  • a plurality of yarn layers are laminated by arranging yarns (continuous fibers) in a folded manner between the regulating members on the frame body, and after forming the laminated yarn group, the laminated yarn group is held on the frame body. In the state, the thickness direction thread is inserted.
  • the elongation of constraining yarns such as thickness direction yarns and stitch yarns constituting the conventional three-dimensional fiber structure is very small. Therefore, when a bent part is formed on a flat plate-like three-dimensional fiber structure, wrinkles and distortion occur in the bent part during bending. As a result, the dimensional accuracy of the manufactured three-dimensional fiber structure having a bent portion is deteriorated, and the strength of the composite material using the three-dimensional fiber structure as a reinforcing substrate is reduced.
  • the present invention has been made in view of the above-mentioned conventional problems, and its purpose is to use a flat plate-like three-dimensional fiber structure as a reinforcing substrate of a three-dimensional fiber-reinforced resin having a bent portion.
  • it is providing the three-dimensional fiber structure which can manufacture a fiber reinforced resin in the state in which generation
  • a fiber layer composed of continuous fibers is laminated, and a laminated fiber layer having at least biaxial orientation and a direction intersecting the fiber layer
  • a three-dimensional fiber structure in which the laminated fiber layers are bonded by the bonding yarn, and a helical thread is used as the bonding yarn.
  • a three-dimensional fiber structure is provided.
  • the continuous fiber is not limited to a single fiber (monofilament) but includes a fiber bundle in which a plurality of single fibers are bundled.
  • the spiral yarn used as the binding yarn is a core-sheath yarn in which a spiral yarn is wound so as to form a sheath covering the periphery of the core yarn, as in a so-called covering yarn.
  • the binding yarn may be configured so that the core yarn does not perform the binding function as a yarn in a state in which a fiber reinforced resin using a three-dimensional fiber structure as a reinforcing material is manufactured. For example, an example in which the core yarn is dissolved in the matrix resin constituting the fiber reinforced resin can be given.
  • a flat three-dimensional fiber structure is used.
  • a three-dimensional fiber structure is formed in which the generation of wrinkles and distortion in the bent portion is prevented or suppressed. This is because the laminated fiber layer tends to shift in the direction along the interface of the fiber layer when bending the flat three-dimensional fiber structure.
  • the binding yarn is not linear but spiral, the binding yarn is stretched to allow the misalignment of the laminated fiber layer, and the three-dimensional structure having the bending portion in a state where generation of wrinkles and distortion in the bending portion is suppressed.
  • a fiber structure is formed.
  • a configuration in which only a spiral thread is present as a binding thread is obtained by, for example, combining a laminated fiber layer with a composite thread having a core-sheath structure in which a spiral thread is wound so as to form a sheath around the core thread. Thereafter, it is formed by pulling out only the core yarn.
  • the core yarn of the core-sheath composite yarn is made of a material that can be dissolved in the matrix resin of the fiber reinforced resin, and in the fiber reinforced resin manufacturing process, the spiral yarn remains in the core-sheath composite yarn.
  • the core yarn may be dissolved in the matrix resin.
  • the spiral thread has a spiral pitch of 100 to 1000 revolutions / m. If the pitch of the spiral is too large, even if it can be bent into a three-dimensional fiber structure having a bent portion in a state where generation of wrinkles and distortion in the bent portion is suppressed, the three-dimensional fiber structure is In a state where it is used as a reinforced base material for fiber reinforced resin, the function of the helical thread as a reinforced fiber is lowered. When the helical pitch is 100 to 1000 revolutions / m, the helical thread can reliably retain the function of the reinforcing fiber in a state where the three-dimensional fiber structure is used as a reinforcing substrate of the fiber reinforced resin. Can do.
  • the binding yarn is preferably a yarn constituting a sheath portion of a composite yarn having a core-sheath structure including a core yarn and a sheath covering the periphery of the core yarn.
  • thermosetting resin or a thermoplastic resin
  • a bonded yarn having a laminated fiber layer in which fiber layers made of continuous fibers are laminated and having at least a biaxial orientation, and a portion arranged in a direction intersecting the fiber layer.
  • the binding yarn includes a core sheath and a sheath that covers the periphery of the core yarn.
  • thermosetting while being formed by a mold in a state in which the three-dimensional fiber structure is used as a reinforcing substrate and the three-dimensional fiber structure is impregnated with the uncured thermosetting resin.
  • a method for manufacturing fiber-reinforced composites that cures functional resins is proposed. It is.
  • a flat three-dimensional fiber structure is used as a reinforcing substrate of a three-dimensional fiber reinforced resin having a bent portion, generation of wrinkles and distortion in the bent portion is suppressed.
  • a three-dimensional fiber structure capable of producing a fiber reinforced resin can be provided.
  • (A) is a schematic perspective view of a flat plate-like three-dimensional fiber structure
  • (b) is a schematic cross-sectional view showing the relationship between the laminated fiber layer and the binding yarn
  • (c) is a spiral binding yarn and a retaining yarn
  • the schematic diagram of the three-dimensional fiber structure formed in the three-dimensional shape and having a curved surface portion.
  • (A), (b) is a schematic diagram of the three-dimensional fiber structure of another embodiment.
  • a flat plate-like three-dimensional fiber structure 11 includes a laminated fiber layer 12 and a laminated fiber layer 12 arranged so that continuous fibers have at least biaxial orientation.
  • the first and second fiber layers 12a and 12b constituting the binding yarn 13 have a portion arranged in a direction intersecting with the first and second fiber layers 12a and 12b.
  • the laminated fiber layers 12 are bonded by a binding yarn 13.
  • As the continuous fiber for example, carbon fiber is used.
  • the number of filaments of carbon fibers is about several hundred to several tens of thousands, and the number of fiber bundles suitable for the required performance is selected.
  • the laminated fiber layer 12 includes a first fiber layer 12a composed of first continuous fibers 14a having an arrangement angle of 0 ° and a second fiber comprising second continuous fibers 14b having an arrangement angle of 90 °. And the layer 12b.
  • the first continuous fibers 14a having an arrangement angle of 0 ° extend so as to be orthogonal to the paper surface shown in FIG. 1B, and the second continuous fibers 14b having an orientation angle of 90 ° are orthogonal to the first continuous fibers 14b.
  • the plurality of first fiber layers 12a and the plurality of second fiber layers 12b are alternately laminated to form a biaxially oriented laminated fiber layer 12.
  • the binding yarn 13 is inserted in a loop shape from the other outer surface (upper surface in FIG. 1) so as to be folded back at one outer surface (lower surface in FIG. 1) of the laminated fiber layer 12.
  • Retaining yarns (ear yarns) 15 arranged in a direction orthogonal to the arrangement direction of the binding yarns 13 are inserted into the loop portion protruding from the lower surface of the laminated fiber layer 12, and the connecting yarns 13 are formed by the retaining yarns 15.
  • the first and second fiber layers 12 a and 12 b of the laminated fiber layer 12 are bonded together by the joint yarn 13 and the retaining yarn 15.
  • a spiral thread is used as the binding thread 13.
  • a covering yarn composite yarn having a core-sheath structure is used.
  • the sheath portion is made of glass fiber
  • the core yarn is a general synthetic yarn
  • the sheath portion is a high-strength and high-modulus fiber (for example, And aramid fibers).
  • the spiral pitch of the spiral yarns constituting the binding yarn 13 has an appropriate value range depending on the thickness of the three-dimensional fiber structure 11, the fiber volume content (Vf), the radius of curvature of the bent portion, the bending angle, and the like. Since they are different, a preliminary test is performed in advance to set an appropriate value.
  • the helical pitch of the binding yarn 13 is moved along the adjacent fiber layers when the bending portion is formed in the flat three-dimensional fiber structure 11 along with the bending process. It is set to a value that is allowed to do.
  • the helical pitch of the helical yarn constituting the binding yarn 13 is preferably 100 to 1000 revolutions / m, and more preferably 100 to 600 revolutions / m. Except for FIG. 1C, the illustration of the binding yarn 13 in a spiral shape is omitted.
  • the flat plate-like three-dimensional fiber structure 11 configured as described above is processed into a three-dimensional three-dimensional fiber structure 11 having a curved surface portion by bending, and then used as a reinforced base material for fiber reinforced resin. Is done.
  • the bending of the flat three-dimensional fiber structure 11 is performed, for example, by gripping the three-dimensional fiber structure 11 in at least two places by a clamping device having a mold surface of a predetermined shape, and then holding the three-dimensional fiber structure 11. Is pressed with a presser having a pressing surface of a predetermined shape between the gripped portions. At this time, at least one clamping device is moved so as to reduce the interval between the gripping portions of the three-dimensional fiber structure 11 so that unnecessary force is not applied to the three-dimensional fiber structure 11.
  • the three-dimensional fiber structure is deformed so as to follow the pressing surface of the presser, and is pressed by the pressing surface of the presser and the mold surface of the clamping device, and shaping is performed.
  • This bending method is basically the same as the method disclosed in, for example, Japanese Patent Application Laid-Open No. 2007-1046.
  • the first and second fiber layers 12a and 12b constituting the three-dimensional fiber structure 11 are arranged on the boundary surfaces of the first and second fiber layers 12a and 12b. A force is applied to move them along each other.
  • the binding yarn 13 that joins the laminated fiber layers 12 is formed in a spiral shape, the binding yarn 13 follows the mutual movement of the first and second fiber layers 12a and 12b, unlike the case where the binding yarn 13 is linear. As the binding yarn 13 extends, the first and second fiber layers 12a and 12b move smoothly, and the generation of wrinkles and distortion at the bent portion is prevented or suppressed.
  • FIG. 2 shows a three-dimensional fiber structure 11 having a substantially inverted U-shaped cross section.
  • the three-dimensional fiber structure 11 has four bent portions 16, but these bent portions 16 are free from wrinkles and distortion.
  • the obtained three-dimensional fiber structure 11 having a three-dimensional shape is impregnated with a matrix resin to form a prepreg. Thereafter, the matrix resin is cured to form FRP (fiber reinforced resin) as a composite material.
  • FRP fiber reinforced resin
  • a resin transfer molding (RTM) method or a vacuum RTM method (VaRTM method) is employed for the treatment of impregnating the three-dimensional fiber structure 11 with resin.
  • RTM method resin transfer molding
  • VaRTM method vacuum RTM method
  • a three-dimensional fiber structure 11 is placed in a mold, and a thermosetting resin before curing constituting the matrix resin is injected into the mold, and the thermosetting resin is used as a three-dimensional fiber. After the structure 11 is impregnated, it is cured by heating.
  • the laminated fiber layer 12 having at least biaxial orientation in which the first and second fiber layers 12a and 12b made of continuous fibers are laminated is the first and second fiber layers 12a, They are bound by a binding thread 13 having portions arranged in a direction crossing 12b.
  • a spiral thread is used as the binding thread 13. Therefore, when the flat three-dimensional fiber structure 11 is shaped into a three-dimensional shape having the bent portion 16, the three-dimensional fiber structure 11 in which generation of wrinkles and distortion in the bent portion 16 is prevented or suppressed is obtained. It is done.
  • the spiral pitch of the spiral thread constituting the binding thread 13 is 100 to 1000 revolutions / m. If the pitch of the spiral is too large, even if the three-dimensional fiber structure can be bent, in the state where the three-dimensional fiber structure is used as a reinforcing substrate for the fiber reinforced resin, The function as a reinforcing fiber is lowered. In this invention, since the helical pitch is 100 to 1000 revolutions / m, the helical thread ensures the function of the reinforcing fiber in a state where the three-dimensional fiber structure is used as the reinforcing substrate of the fiber reinforced resin. Can be held in.
  • the embodiment is not limited to the above-described embodiment, and may be embodied as follows, for example.
  • the core yarn is a bent portion of at least a flat plate-like three-dimensional fiber structure 11.
  • the core yarn loses its binding function as a yarn when it is shaped into a three-dimensional shape having 16 or before it is shaped into a three-dimensional shape.
  • the sheath portion of the composite yarn functions as a spiral yarn, that is, the binding yarn 13.
  • the core yarn of the composite yarn having the core-sheath structure may be made of a material that can be dissolved in the matrix resin of the fiber reinforced resin.
  • the matrix resin is a thermoplastic resin
  • the core yarn is constituted by a yarn made of a thermoplastic resin, and the plate-like three-dimensional fiber structure 11 is impregnated with the matrix resin in the production process of the fiber reinforced resin.
  • the fiber reinforced resin intermediate is processed into a three-dimensional fiber reinforced resin having a bent portion 16 by press molding.
  • the core yarn is dissolved in the matrix resin, and when the fiber reinforced resin intermediate is press-molded, it does not function as a yarn, and the sheath of the composite yarn Since the portion functions as the binding yarn 13, generation of wrinkles and distortion in the bent portion 16 is prevented or suppressed during press molding of the fiber reinforced resin intermediate.
  • the core yarn of the core-sheath structure yarn may be formed of a material that can be dissolved in the thermosetting resin.
  • Phenoxy resin may be used as the material for the core yarn.
  • a phase in which the phenoxy resin is mixed with the matrix resin exists around the binding yarn 13.
  • a resin rich portion tends to exist in the vicinity of the binding yarn 13, and microcracks are easily generated in the resin rich portion.
  • phenoxy resin when phenoxy resin is mixed, phenoxy resin is flexible because it has a long molecular chain, and has excellent flexibility, and also has good adhesion because it has a hydroxyl group as a hydrophilic group and a hydrocarbon group as a hydrophobic group.
  • the toughness of the resin-rich portion is improved and the generation of microcracks is suppressed.
  • the binding yarn 13 that bonds the laminated fiber layer 12 is not limited to the configuration in which the laminated fiber layer 12 is inserted into the laminated fiber layer 12 in a folded state from one surface and is prevented from being detached by the retaining yarn 15. Instead, a stitch thread is used, and a single binding thread 13 is inserted into the laminated fiber layer 12 from one side using a needle, and the needle is inserted in the other side so that the needle insertion position is changed.
  • the laminated fiber layer 12 may be bonded by repetition.
  • the insertion interval or density of the binding yarn 13 may be set according to the strength required for the target composite material.
  • the laminated fiber layer 12 in which the first and second fiber layers 12a and 12b composed of the first and second continuous fibers 14a and 14b are laminated may be at least biaxially oriented, and the arrangement angle of the continuous fibers is 0 degree. And the combination of 90 degrees.
  • a fiber layer composed of continuous fibers with an arrangement angle of +45 degrees and ⁇ 45 degrees is provided, and a configuration with a four-axis orientation is adopted, or the arrangement angle is 0
  • a triaxially oriented configuration may be adopted, which is a combination of a continuous fiber having a degree or 90 degrees and a bias fiber bundle arranged obliquely with respect to the continuous fiber.
  • the laminated fiber layer 12 is not limited to a configuration in which a plurality of fiber layers configured such that continuous fibers having the same arrangement angle are positioned on a single plane, but a configuration in which a woven fabric is laminated as a fiber layer. It may be.
  • a woven fabric for example, a plain woven fabric is used, but a multilayer woven fabric such as a double woven fabric, a triple woven fabric, or an air woven fabric may be laminated.
  • the laminated fiber layer 12 can be formed in a shorter time than the laminated fiber layer 12 is formed by laminating fiber layers in which continuous fibers are arranged.
  • the shape of the three-dimensional fiber structure 11 having the bent portion 16 constituted by the flat plate-like three-dimensional fiber structure 11 is not limited to the configuration having the four bent portions 16 as shown in FIG.
  • a cross-sectional L-shaped configuration having one bent portion 16 or a cross-sectional crank-shaped configuration having two bent portions 16 as shown in FIG. May be.
  • SYMBOLS 11 Three-dimensional fiber structure, 12 ... Laminated fiber layer, 12a, 12b ... 1st and 2nd fiber layer, 13 ... Binding yarn, 14a, 14b ... 1st and 2nd continuous fiber.

Abstract

This three-dimensional fiber structure (11) comprises: a laminated fiber layer (12) in which first and second fiber layers (12a, 12b) that are each composed of filaments are stacked and which exhibits at least biaxial orientation; and a binding yarn (13) which has portions that are arranged in a direction crossing the first and second fiber layers (12a, 12b) and by which the laminated fiber layer (12) is bound. A spiral yarn is used as the binding yarn (13).

Description

三次元繊維構造体、それを使用したプリプレグ、及び、三次元繊維構造体の製造方法Three-dimensional fiber structure, prepreg using the same, and method for producing three-dimensional fiber structure
 本発明は、三次元繊維構造体、それを使用したプリプレグ、及び、三次元繊維構造体の製造方法に関する。 The present invention relates to a three-dimensional fiber structure, a prepreg using the same, and a method for manufacturing the three-dimensional fiber structure.
 繊維強化複合材(以下、単に複合材と言う。)は軽量の構造材として広く使用されている。複合材用の強化基材として三次元織物等の三次元繊維構造体がある。三次元繊維構造体を複合材の強化基材として広い用途に使用可能とするためには、単純な平板状ではなく曲げ部を備えることが必要となる。 Fiber reinforced composite materials (hereinafter simply referred to as composite materials) are widely used as lightweight structural materials. There is a three-dimensional fiber structure such as a three-dimensional fabric as a reinforcing base material for a composite material. In order to be able to use the three-dimensional fiber structure as a reinforced base material for a composite material in a wide range of applications, it is necessary to provide a bent portion instead of a simple flat plate shape.
 曲げ部を有する三次元繊維構造体の製造方法としては、平板状の三次元繊維構造体を作製して、その三次元繊維構造体に曲げ部を賦形する方法がある。 As a method for producing a three-dimensional fiber structure having a bent portion, there is a method of producing a flat three-dimensional fiber structure and shaping the bent portion in the three-dimensional fiber structure.
 また、複数の板状部が接続部において屈曲した状態で連続する形状の三次元繊維構造体を形成するため、その三次元繊維構造体の形状に対応する枠体を設け、その枠体に複数の規制部材を所定ピッチで配置した装置を使用する方法が知られている(特許文献1参照)。この方法では、枠体上の規制部材の間に糸(連続繊維)を折り返し状に配列して複数の糸層を積層することにより、積層糸群を形成した後、積層糸群を枠体に保持した状態で、厚さ方向糸が挿入される。 Further, in order to form a three-dimensional fiber structure having a shape in which a plurality of plate-like portions are bent in the connection portion, a frame corresponding to the shape of the three-dimensional fiber structure is provided, and a plurality of frames are provided on the frame. There is known a method of using a device in which the regulating members are arranged at a predetermined pitch (see Patent Document 1). In this method, a plurality of yarn layers are laminated by arranging yarns (continuous fibers) in a folded manner between the regulating members on the frame body, and after forming the laminated yarn group, the laminated yarn group is held on the frame body. In the state, the thickness direction thread is inserted.
特開平9-137336号公報Japanese Patent Laid-Open No. 9-137336
 従来の三次元繊維構造体を構成する厚さ方向糸やスティッチ糸等の拘束糸の伸びは非常に小さい。そのため、平板状の三次元繊維構造体に曲げ部を賦形する場合には、曲げ加工時に、曲げ部において皺や歪みが発生する。その結果、製造された曲げ部を有する三次元繊維構造体の寸法精度の悪化や、三次元繊維構造体を強化基材として使用する複合材の強度低下が生じる。 The elongation of constraining yarns such as thickness direction yarns and stitch yarns constituting the conventional three-dimensional fiber structure is very small. Therefore, when a bent part is formed on a flat plate-like three-dimensional fiber structure, wrinkles and distortion occur in the bent part during bending. As a result, the dimensional accuracy of the manufactured three-dimensional fiber structure having a bent portion is deteriorated, and the strength of the composite material using the three-dimensional fiber structure as a reinforcing substrate is reduced.
 一方、特許文献1の方法では、特殊な枠体を使用して、積層糸群を形成した後、その積層糸群に厚さ方向糸が挿入されるため、積層工程及び厚さ方向糸の挿入工程が非常に煩雑で工数がかかる。 On the other hand, in the method of Patent Document 1, after forming a laminated yarn group using a special frame, the thickness direction yarn is inserted into the laminated yarn group, so that the lamination step and the thickness direction yarn insertion step are performed. Very cumbersome and time consuming.
 本発明は、前記従来の問題に鑑みてなされたものであって、その目的は、平板状の三次元繊維構造体を、曲げ部を有する三次元形状の繊維強化樹脂の強化基材に使用しても、曲げ部における皺や歪みの発生が抑制された状態で繊維強化樹脂の製造が可能な三次元繊維構造体及びその製造方法を提供することにある。 The present invention has been made in view of the above-mentioned conventional problems, and its purpose is to use a flat plate-like three-dimensional fiber structure as a reinforcing substrate of a three-dimensional fiber-reinforced resin having a bent portion. However, it is providing the three-dimensional fiber structure which can manufacture a fiber reinforced resin in the state in which generation | occurrence | production of the wrinkles and distortion in a bending part was suppressed, and its manufacturing method.
 前記の目的を達成するため、本発明の第1の態様によれば、連続繊維からなる繊維層が積層され、かつ、少なくとも2軸配向を有する積層繊維層と、前記繊維層と交差する方向に配列される部分を有する結合糸とを有し、前記積層繊維層が前記結合糸によって結合された三次元繊維構造体であって、前記結合糸として螺旋状の糸が使用されていることを特徴とする三次元繊維構造体が提供される。 In order to achieve the above object, according to the first aspect of the present invention, a fiber layer composed of continuous fibers is laminated, and a laminated fiber layer having at least biaxial orientation and a direction intersecting the fiber layer A three-dimensional fiber structure in which the laminated fiber layers are bonded by the bonding yarn, and a helical thread is used as the bonding yarn. A three-dimensional fiber structure is provided.
 ここで、連続繊維とは、単繊維(モノフィラメント)に限らず、単繊維が複数本束ねられた繊維束を含む。また、結合糸として使用される螺旋状の糸とは、所謂カバーリングヤーンのように、芯糸の周囲を覆う鞘を形成するように、螺旋状の糸が巻き付けられた芯鞘構造の糸も含む。結合糸は、三次元繊維構造体を強化材として使用した繊維強化樹脂を製造した状態で、芯糸が糸としての結合機能を果たさない構成であればよい。例えば、芯糸が繊維強化樹脂を構成するマトリックス樹脂に溶ける例が挙げられる。 Here, the continuous fiber is not limited to a single fiber (monofilament) but includes a fiber bundle in which a plurality of single fibers are bundled. The spiral yarn used as the binding yarn is a core-sheath yarn in which a spiral yarn is wound so as to form a sheath covering the periphery of the core yarn, as in a so-called covering yarn. Including. The binding yarn may be configured so that the core yarn does not perform the binding function as a yarn in a state in which a fiber reinforced resin using a three-dimensional fiber structure as a reinforcing material is manufactured. For example, an example in which the core yarn is dissolved in the matrix resin constituting the fiber reinforced resin can be given.
 本発明の第1の態様の三次元繊維構造体では、2軸配向を有する積層繊維層を結合する結合糸として、螺旋状の糸が使用されているため、平板状の三次元繊維構造体を曲げ部を有する三次元形状に賦形した場合、曲げ部における皺や歪みの発生が防止または抑制された三次元繊維構造体が形成される。なぜならば、平板状の三次元繊維構造体に曲げ加工を施す際に、積層繊維層が繊維層の界面に沿った方向にずれようとする。そのとき、結合糸が直線状ではなく螺旋状のため、積層繊維層のずれを許容するように結合糸が伸び、曲げ部における皺や歪みの発生が抑制された状態で曲げ部を有する三次元繊維構造体が形成される。 In the three-dimensional fiber structure according to the first aspect of the present invention, since a helical thread is used as a binding thread for joining the laminated fiber layers having biaxial orientation, a flat three-dimensional fiber structure is used. When it is shaped into a three-dimensional shape having a bent portion, a three-dimensional fiber structure is formed in which the generation of wrinkles and distortion in the bent portion is prevented or suppressed. This is because the laminated fiber layer tends to shift in the direction along the interface of the fiber layer when bending the flat three-dimensional fiber structure. At that time, since the binding yarn is not linear but spiral, the binding yarn is stretched to allow the misalignment of the laminated fiber layer, and the three-dimensional structure having the bending portion in a state where generation of wrinkles and distortion in the bending portion is suppressed. A fiber structure is formed.
 結合糸として螺旋状の糸のみが存在する構成は、例えば、芯糸とその周囲に鞘を形成するように螺旋状の糸が巻き付けられた芯鞘構造を有する複合糸で積層繊維層を結合した後、芯糸のみを引き抜くことによって、形成される。また、芯鞘構造の複合糸の芯糸を繊維強化樹脂のマトリックス樹脂に溶解可能な材質で構成し、繊維強化樹脂の製造工程において、芯鞘構造の複合糸のうち、螺旋状の糸を残して芯糸をマトリックス樹脂に溶解させるようにしてもよい。 A configuration in which only a spiral thread is present as a binding thread is obtained by, for example, combining a laminated fiber layer with a composite thread having a core-sheath structure in which a spiral thread is wound so as to form a sheath around the core thread. Thereafter, it is formed by pulling out only the core yarn. Further, the core yarn of the core-sheath composite yarn is made of a material that can be dissolved in the matrix resin of the fiber reinforced resin, and in the fiber reinforced resin manufacturing process, the spiral yarn remains in the core-sheath composite yarn. The core yarn may be dissolved in the matrix resin.
 本発明の第1の態様において、前記螺旋状の糸は、100~1000回転/mの螺旋のピッチを有することが望ましい。螺旋のピッチが大きすぎると、曲げ部における皺や歪みの発生が抑制された状態で、曲げ部を有する三次元繊維構造体に曲げ加工することができたとしても、その三次元繊維構造体が繊維強化樹脂の強化基材として使用された状態において、螺旋状の糸の強化繊維としての機能が低くなる。螺旋のピッチが100~1000回転/mであれば、螺旋状の糸は、三次元繊維構造体が繊維強化樹脂の強化基材として使用された状態において、強化繊維の機能を確実に保持することができる。 In the first aspect of the present invention, it is desirable that the spiral thread has a spiral pitch of 100 to 1000 revolutions / m. If the pitch of the spiral is too large, even if it can be bent into a three-dimensional fiber structure having a bent portion in a state where generation of wrinkles and distortion in the bent portion is suppressed, the three-dimensional fiber structure is In a state where it is used as a reinforced base material for fiber reinforced resin, the function of the helical thread as a reinforced fiber is lowered. When the helical pitch is 100 to 1000 revolutions / m, the helical thread can reliably retain the function of the reinforcing fiber in a state where the three-dimensional fiber structure is used as a reinforcing substrate of the fiber reinforced resin. Can do.
 前記結合糸の積層繊維層からの抜け止めを行う抜け止め糸を更に有することが望ましい。 It is desirable to further have a retaining thread for retaining the binding thread from the laminated fiber layer.
 前記結合糸は、芯糸とその芯糸の周囲を覆う鞘とを備えた芯鞘構造を有する複合糸の鞘の部分を構成する糸であることが望ましい。 The binding yarn is preferably a yarn constituting a sheath portion of a composite yarn having a core-sheath structure including a core yarn and a sheath covering the periphery of the core yarn.
 前記三次元繊維構造体に熱硬化製樹脂又は熱可塑性樹脂を含浸したプリプレグを形成することが望ましい。 It is desirable to form a prepreg in which the three-dimensional fiber structure is impregnated with a thermosetting resin or a thermoplastic resin.
 本発明の第2の態様によれば、連続繊維からなる繊維層が積層され、かつ、少なくとも2軸配向を有する積層繊維層と、前記繊維層と交差する方向に配列される部分を有する結合糸とを有し、前記積層繊維層が前記結合糸によって結合された三次元繊維構造体の製造方法において、前記結合糸は、芯糸とその芯糸の周囲を覆う鞘とを備えた芯鞘構造の複合糸における前記鞘を構成する螺旋状の糸であり、前記芯糸が熱硬化性樹脂に溶解可能な繊維で構成され、前記鞘の部分を構成する糸が熱硬化性樹脂に溶解不能な繊維で構成され、前記三次元繊維構造体を強化基材として使用し、前記三次元繊維構造体に未硬化の前記熱硬化性樹脂を含浸させた状態で成形型により賦形しつつ前記熱硬化性樹脂を硬化させる繊維強化複合材の製造方法が提供される。 According to the second aspect of the present invention, a bonded yarn having a laminated fiber layer in which fiber layers made of continuous fibers are laminated and having at least a biaxial orientation, and a portion arranged in a direction intersecting the fiber layer. In the method of manufacturing a three-dimensional fiber structure in which the laminated fiber layer is bonded by the binding yarn, the binding yarn includes a core sheath and a sheath that covers the periphery of the core yarn. A spiral thread constituting the sheath of the composite yarn, wherein the core thread is composed of fibers that can be dissolved in a thermosetting resin, and the thread that constitutes the sheath is insoluble in the thermosetting resin. The thermosetting while being formed by a mold in a state in which the three-dimensional fiber structure is used as a reinforcing substrate and the three-dimensional fiber structure is impregnated with the uncured thermosetting resin. A method for manufacturing fiber-reinforced composites that cures functional resins is proposed. It is.
 この場合、曲げ部における皺や歪みの発生が抑制された状態で繊維強化樹脂の製造が可能である。 In this case, it is possible to manufacture the fiber reinforced resin in a state where generation of wrinkles and distortion in the bent portion is suppressed.
 本発明によれば、平板状の三次元繊維構造体を、曲げ部を有する三次元形状の繊維強化樹脂の強化基材に使用しても、曲げ部における皺や歪みの発生が抑制された状態で繊維強化樹脂の製造が可能な三次元繊維構造体を提供することができる。 According to the present invention, even when a flat three-dimensional fiber structure is used as a reinforcing substrate of a three-dimensional fiber reinforced resin having a bent portion, generation of wrinkles and distortion in the bent portion is suppressed. Thus, a three-dimensional fiber structure capable of producing a fiber reinforced resin can be provided.
(a)は平板状の三次元繊維構造体の模式斜視図、(b)は積層繊維層と結合糸との関係を示す模式断面図、(c)は螺旋状の結合糸が抜け止め糸と係合している状態の部分模式図。(A) is a schematic perspective view of a flat plate-like three-dimensional fiber structure, (b) is a schematic cross-sectional view showing the relationship between the laminated fiber layer and the binding yarn, (c) is a spiral binding yarn and a retaining yarn The partial schematic diagram of the state which has engaged. 三次元形状に賦形され、曲面部を有する三次元繊維構造体の模式図。The schematic diagram of the three-dimensional fiber structure formed in the three-dimensional shape and having a curved surface portion. (a),(b)は別の実施形態の三次元繊維構造体の模式図。(A), (b) is a schematic diagram of the three-dimensional fiber structure of another embodiment.
 以下、本発明を具体化した一実施形態を図1及び図2にしたがって説明する。 Hereinafter, an embodiment embodying the present invention will be described with reference to FIGS. 1 and 2.
 図1(a),(b)に示すように、平板状の三次元繊維構造体11は、連続繊維が少なくとも2軸配向を有するように配列された積層繊維層12と、積層繊維層12を構成する第1及び第2繊維層12a,12bと交差する方向に配列される部分を有する結合糸13とを有する。積層繊維層12は結合糸13によって結合されている。連続繊維としては、例えば、炭素繊維が使用される。炭素繊維のフィラメント数は数百~数万本程度であり、要求性能に適した本数の繊維束が選択される。 As shown in FIGS. 1A and 1B, a flat plate-like three-dimensional fiber structure 11 includes a laminated fiber layer 12 and a laminated fiber layer 12 arranged so that continuous fibers have at least biaxial orientation. The first and second fiber layers 12a and 12b constituting the binding yarn 13 have a portion arranged in a direction intersecting with the first and second fiber layers 12a and 12b. The laminated fiber layers 12 are bonded by a binding yarn 13. As the continuous fiber, for example, carbon fiber is used. The number of filaments of carbon fibers is about several hundred to several tens of thousands, and the number of fiber bundles suitable for the required performance is selected.
 図1(b)に示すように、積層繊維層12は、配列角度0°の第1連続繊維14aから成る第1繊維層12aと、配列角度90°の第2連続繊維14bから成る第2繊維層12bとによって構成されている。配列角度0°の第1連続繊維14aは図1(b)を記載した紙面に直交するように延び、配向角度90゜の第2連続繊維14bは第1連続繊維14bと直交している。複数の第1繊維層12aと複数の第2繊維層12bとは交互に積層されて、2軸配向の積層繊維層12が形成されている。 As shown in FIG. 1B, the laminated fiber layer 12 includes a first fiber layer 12a composed of first continuous fibers 14a having an arrangement angle of 0 ° and a second fiber comprising second continuous fibers 14b having an arrangement angle of 90 °. And the layer 12b. The first continuous fibers 14a having an arrangement angle of 0 ° extend so as to be orthogonal to the paper surface shown in FIG. 1B, and the second continuous fibers 14b having an orientation angle of 90 ° are orthogonal to the first continuous fibers 14b. The plurality of first fiber layers 12a and the plurality of second fiber layers 12b are alternately laminated to form a biaxially oriented laminated fiber layer 12.
 結合糸13は、積層繊維層12の一方の外面(図1の下面)で折り返すように他方の外面(図1の上面)からループ状に挿入されている。積層繊維層12の下面から突出したループ部には、結合糸13の配列方向と直交する方向に配列された抜け止め糸(耳糸)15が挿入され、その抜け止め糸15によって、結合糸13が抜け止めされている。従って、結合糸13と抜け止め糸15との共同により、積層繊維層12の第1及び第2繊維層12a,12bが結合されている。 The binding yarn 13 is inserted in a loop shape from the other outer surface (upper surface in FIG. 1) so as to be folded back at one outer surface (lower surface in FIG. 1) of the laminated fiber layer 12. Retaining yarns (ear yarns) 15 arranged in a direction orthogonal to the arrangement direction of the binding yarns 13 are inserted into the loop portion protruding from the lower surface of the laminated fiber layer 12, and the connecting yarns 13 are formed by the retaining yarns 15. Has been secured. Therefore, the first and second fiber layers 12 a and 12 b of the laminated fiber layer 12 are bonded together by the joint yarn 13 and the retaining yarn 15.
 図1(c)に示すように、結合糸13として螺旋状の糸が使用されている。螺旋状の結合糸13によって積層繊維層12を結合する場合、例えば、芯鞘構造のカバーリングヤーン(複合糸)が用いられる。その場合、積層繊維層12をカバーリングヤーン及び抜け止め糸15で結合した後、カバーリングヤーンの芯糸のみを引き抜き、鞘部分の糸が結合糸13として残される。カバーリングヤーンとして、例えば、芯糸が一般的な化繊糸、鞘部がガラス繊維で構成されたものや、芯糸が一般的な化繊糸、鞘部が高強度・高弾性率繊維(例えば、アラミド繊維)で構成されたものが挙げられる。 As shown in FIG. 1 (c), a spiral thread is used as the binding thread 13. When the laminated fiber layers 12 are bonded by the spiral bonding yarn 13, for example, a covering yarn (composite yarn) having a core-sheath structure is used. In that case, after the laminated fiber layer 12 is bonded with the covering yarn and the retaining yarn 15, only the core yarn of the covering yarn is pulled out, and the sheath yarn remains as the bonded yarn 13. As the covering yarn, for example, the core yarn is a general synthetic yarn, the sheath portion is made of glass fiber, the core yarn is a general synthetic yarn, the sheath portion is a high-strength and high-modulus fiber (for example, And aramid fibers).
 結合糸13を構成する螺旋状の糸の螺旋ピッチは、三次元繊維構造体11の厚さ、繊維体積含有率(Vf)、曲げ部の曲率半径、曲げ角度等により、適正な値の範囲が異なるため、予め予備試験を行って適正な値に設定される。結合糸13の螺旋ピッチは、平板状の三次元繊維構造体11に曲げ部を賦形する際に、曲げ加工に伴い、結合糸13によって結合された繊維層が隣り合う繊維層に沿って移動することを許容される値に設定される。結合糸13を構成する螺旋状の糸の螺旋のピッチは100~1000回転/mであることが好ましく、螺旋のピッチが100~600回転/mであることがより好ましい。なお、図1(c)以外では、結合糸13を螺旋状に図示することを省略している。 The spiral pitch of the spiral yarns constituting the binding yarn 13 has an appropriate value range depending on the thickness of the three-dimensional fiber structure 11, the fiber volume content (Vf), the radius of curvature of the bent portion, the bending angle, and the like. Since they are different, a preliminary test is performed in advance to set an appropriate value. The helical pitch of the binding yarn 13 is moved along the adjacent fiber layers when the bending portion is formed in the flat three-dimensional fiber structure 11 along with the bending process. It is set to a value that is allowed to do. The helical pitch of the helical yarn constituting the binding yarn 13 is preferably 100 to 1000 revolutions / m, and more preferably 100 to 600 revolutions / m. Except for FIG. 1C, the illustration of the binding yarn 13 in a spiral shape is omitted.
 前記のように構成された平板状の三次元繊維構造体11は、曲げ加工により曲面部を有する三次元形状の三次元繊維構造体11に加工された後、繊維強化樹脂の強化基材として使用される。平板状の三次元繊維構造体11の曲げ加工は、例えば、三次元繊維構造体11を所定形状の型面を有するクランプ装置によって少なくとも2箇所において把持し、次に把持した三次元繊維構造体11を、把持した箇所の間において所定形状の押圧面を有するプレッサで押圧する。このとき、三次元繊維構造体11に不要な力が加わらないように、少なくとも一つのクランプ装置が三次元繊維構造体11の把持部の間隔を狭めるように移動される。そして、三次元繊維構造体がプレッサの押圧面に沿うように変形され、プレッサの押圧面とクランプ装置の型面とで押圧されて、賦形が行われる。この曲げ加工方法は、例えば、特開2007-1046号公報に開示されている方法と基本的に同様である。 The flat plate-like three-dimensional fiber structure 11 configured as described above is processed into a three-dimensional three-dimensional fiber structure 11 having a curved surface portion by bending, and then used as a reinforced base material for fiber reinforced resin. Is done. The bending of the flat three-dimensional fiber structure 11 is performed, for example, by gripping the three-dimensional fiber structure 11 in at least two places by a clamping device having a mold surface of a predetermined shape, and then holding the three-dimensional fiber structure 11. Is pressed with a presser having a pressing surface of a predetermined shape between the gripped portions. At this time, at least one clamping device is moved so as to reduce the interval between the gripping portions of the three-dimensional fiber structure 11 so that unnecessary force is not applied to the three-dimensional fiber structure 11. Then, the three-dimensional fiber structure is deformed so as to follow the pressing surface of the presser, and is pressed by the pressing surface of the presser and the mold surface of the clamping device, and shaping is performed. This bending method is basically the same as the method disclosed in, for example, Japanese Patent Application Laid-Open No. 2007-1046.
 三次元繊維構造体11がプレッサで押圧される際、三次元繊維構造体11を構成する第1及び第2繊維層12a,12bに対し、第1及び第2繊維層12a,12bの境界面に沿って相互に移動させようとする力が加わる。しかし、積層繊維層12を結合する結合糸13は螺旋状に形成されているため、結合糸13が直線状の場合とは異なり、第1及び第2繊維層12a,12bの相互移動に追随して結合糸13が伸びることにより、第1及び第2繊維層12a,12bの相互移動が円滑に行われ、曲げ部における皺や歪みの発生が防止または抑制される。その結果、曲げ部における皺や歪みが抑制された三次元形状の三次元繊維構造体11が得られる。図2には、ほぼ逆U字状の断面を有する三次元繊維構造体11が示されている。この三次元繊維構造体11は4つの曲げ部16を有しているが、これらの曲げ部16に皺や歪みはない。 When the three-dimensional fiber structure 11 is pressed by the presser, the first and second fiber layers 12a and 12b constituting the three-dimensional fiber structure 11 are arranged on the boundary surfaces of the first and second fiber layers 12a and 12b. A force is applied to move them along each other. However, since the binding yarn 13 that joins the laminated fiber layers 12 is formed in a spiral shape, the binding yarn 13 follows the mutual movement of the first and second fiber layers 12a and 12b, unlike the case where the binding yarn 13 is linear. As the binding yarn 13 extends, the first and second fiber layers 12a and 12b move smoothly, and the generation of wrinkles and distortion at the bent portion is prevented or suppressed. As a result, a three-dimensional three-dimensional fiber structure 11 in which wrinkles and distortions in the bent portion are suppressed is obtained. FIG. 2 shows a three-dimensional fiber structure 11 having a substantially inverted U-shaped cross section. The three-dimensional fiber structure 11 has four bent portions 16, but these bent portions 16 are free from wrinkles and distortion.
 得られた三次元形状の三次元繊維構造体11には、マトリックス樹脂が含浸されてプリプレグが形成される。その後、マトリックス樹脂が硬化されて、複合材としてのFRP(繊維強化樹脂)が形成される。三次元繊維構造体11に樹脂を含浸させる処理には、例えば、レジントランスファーモールディング(RTM)法や、真空RTM法(VaRTM法)が採用される。RTM法では、成形型内に三次元繊維構造体11を載置し、この成形型内に、マトリック樹脂を構成する硬化前の熱硬化性樹脂が注入され、その熱硬化性樹脂を三次元繊維構造体11に含浸させた後、加熱硬化させる。 The obtained three-dimensional fiber structure 11 having a three-dimensional shape is impregnated with a matrix resin to form a prepreg. Thereafter, the matrix resin is cured to form FRP (fiber reinforced resin) as a composite material. For the treatment of impregnating the three-dimensional fiber structure 11 with resin, for example, a resin transfer molding (RTM) method or a vacuum RTM method (VaRTM method) is employed. In the RTM method, a three-dimensional fiber structure 11 is placed in a mold, and a thermosetting resin before curing constituting the matrix resin is injected into the mold, and the thermosetting resin is used as a three-dimensional fiber. After the structure 11 is impregnated, it is cured by heating.
 この実施形態によれば、以下に示す効果を得ることができる。 According to this embodiment, the following effects can be obtained.
 (1)三次元繊維構造体11では、連続繊維からなる第1及び第2繊維層12a,12bが積層された少なくとも2軸配向を有する積層繊維層12が、第1及び第2繊維層12a,12bと交差する方向に配列される部分を有する結合糸13によって結合されている。結合糸13としては螺旋状の糸が使用されている。したがって、平板状の三次元繊維構造体11を、曲げ部16を有する三次元形状に賦形した場合、曲げ部16における皺や歪みの発生が防止または抑制された三次元繊維構造体11が得られる。 (1) In the three-dimensional fiber structure 11, the laminated fiber layer 12 having at least biaxial orientation in which the first and second fiber layers 12a and 12b made of continuous fibers are laminated is the first and second fiber layers 12a, They are bound by a binding thread 13 having portions arranged in a direction crossing 12b. A spiral thread is used as the binding thread 13. Therefore, when the flat three-dimensional fiber structure 11 is shaped into a three-dimensional shape having the bent portion 16, the three-dimensional fiber structure 11 in which generation of wrinkles and distortion in the bent portion 16 is prevented or suppressed is obtained. It is done.
 (2)結合糸13を構成する螺旋状の糸の螺旋のピッチは100~1000回転/mである。螺旋のピッチが大きすぎると、三次元繊維構造体に曲げ加工を行うことができても、その三次元繊維構造体が繊維強化樹脂の強化基材として使用された状態において、螺旋状の糸の強化繊維としての機能が低くなる。この発明では、螺旋のピッチが100~1000回転/mであるため、螺旋状の糸は、三次元繊維構造体が繊維強化樹脂の強化基材として使用された状態において、強化繊維の機能を確実に保持することができる。 (2) The spiral pitch of the spiral thread constituting the binding thread 13 is 100 to 1000 revolutions / m. If the pitch of the spiral is too large, even if the three-dimensional fiber structure can be bent, in the state where the three-dimensional fiber structure is used as a reinforcing substrate for the fiber reinforced resin, The function as a reinforcing fiber is lowered. In this invention, since the helical pitch is 100 to 1000 revolutions / m, the helical thread ensures the function of the reinforcing fiber in a state where the three-dimensional fiber structure is used as the reinforcing substrate of the fiber reinforced resin. Can be held in.
 実施形態は前記の実施形態に限定されるものではなく、例えば、次のように具体化してもよい。 The embodiment is not limited to the above-described embodiment, and may be embodied as follows, for example.
 三次元繊維構造体11では、連続繊維からなる第1及び第2繊維層12a,12bが積層された少なくとも2軸配向の積層繊維層12が、第1及び第2繊維層12a,12bと交差する方向に配列される部分を有する結合糸13によって結合され、結合糸13として螺旋状の糸が使用されていればよい。例えば、カバーリングヤーンのように、芯糸の周囲に鞘状に螺旋状の糸が巻き付けられた芯鞘構造の複合糸において、芯糸は、少なくとも平板状の三次元繊維構造体11を曲げ部16を有する三次元形状に賦形する際、又は、三次元形状に賦形するまでに、芯糸が糸としての結合機能を失う状態になるものであればよい。この場合には、複合糸の鞘の部分が螺旋状の糸、すなわち、結合糸13として機能する。 In the three-dimensional fiber structure 11, at least a biaxially oriented laminated fiber layer 12 in which the first and second fiber layers 12a and 12b made of continuous fibers are laminated intersects the first and second fiber layers 12a and 12b. It is only necessary that the yarns are coupled by the coupling yarns 13 having the portions arranged in the direction, and the spiral yarns are used as the coupling yarns 13. For example, in a composite yarn having a core-sheath structure in which a spiral thread is wound around a core yarn like a covering yarn, the core yarn is a bent portion of at least a flat plate-like three-dimensional fiber structure 11. What is necessary is just to be in a state where the core yarn loses its binding function as a yarn when it is shaped into a three-dimensional shape having 16 or before it is shaped into a three-dimensional shape. In this case, the sheath portion of the composite yarn functions as a spiral yarn, that is, the binding yarn 13.
 芯鞘構造の複合糸の芯糸を、繊維強化樹脂のマトリックス樹脂に溶解可能な材質で構成してもよい。例えば、マトリックス樹脂が熱可塑性樹脂の場合、芯糸を熱可塑性樹脂製の糸によって構成し、繊維強化樹脂の製造工程において、平板状の三次元繊維構造体11にマトリックス樹脂を含浸させて平板状の繊維強化樹脂中間体を構成した後、その繊維強化樹脂中間体をプレス成形で曲げ部16を有する三次元形状の繊維強化樹脂に加工する。この場合、平板状の繊維強化樹脂中間体の段階で、芯糸はマトリックス樹脂に溶解した状態になり、繊維強化樹脂中間体をプレス成形する際に、糸として機能しなくなり、複合糸の鞘の部分が結合糸13として機能するため、繊維強化樹脂中間体のプレス成形の際に、曲げ部16における皺や歪みの発生が防止または抑制される。 The core yarn of the composite yarn having the core-sheath structure may be made of a material that can be dissolved in the matrix resin of the fiber reinforced resin. For example, when the matrix resin is a thermoplastic resin, the core yarn is constituted by a yarn made of a thermoplastic resin, and the plate-like three-dimensional fiber structure 11 is impregnated with the matrix resin in the production process of the fiber reinforced resin. After the fiber reinforced resin intermediate is configured, the fiber reinforced resin intermediate is processed into a three-dimensional fiber reinforced resin having a bent portion 16 by press molding. In this case, at the stage of the flat fiber reinforced resin intermediate, the core yarn is dissolved in the matrix resin, and when the fiber reinforced resin intermediate is press-molded, it does not function as a yarn, and the sheath of the composite yarn Since the portion functions as the binding yarn 13, generation of wrinkles and distortion in the bent portion 16 is prevented or suppressed during press molding of the fiber reinforced resin intermediate.
 芯鞘構造の糸の芯糸を、熱硬化性樹脂に溶解可能な材質で形成してもよい。この場合、平板状の三次元繊維構造体11に未硬化の状態の熱硬化性樹脂を含浸させる必要があるため、熱可塑性樹脂の場合と異なり、含浸時に加熱を自由に行うことはできない。芯糸の材質としてフェノキシ樹脂を使用してもよい。フェノキシ樹脂を使用した場合、得られた繊維強化樹脂では、結合糸13の周囲にフェノキシ樹脂がマトリックス樹脂と混合された相が存在する。繊維強化樹脂では、結合糸13の付近に樹脂リッチ部が存在し易くなり、樹脂リッチ部ではマイクロクラックが発生し易い。しかし、フェノキシ樹脂が混在すると、フェノキシ樹脂は、分子鎖が長いので屈曲性があり、柔軟性に優れ、また、親水基としての水酸基、疎水基としての炭化水素基を有するため、接着性が良く、樹脂リッチ部の靱性が向上し、マイクロクラックの発生が抑制される。 The core yarn of the core-sheath structure yarn may be formed of a material that can be dissolved in the thermosetting resin. In this case, since it is necessary to impregnate the flat three-dimensional fiber structure 11 with an uncured thermosetting resin, unlike the case of a thermoplastic resin, heating cannot be freely performed during the impregnation. Phenoxy resin may be used as the material for the core yarn. When the phenoxy resin is used, in the obtained fiber reinforced resin, a phase in which the phenoxy resin is mixed with the matrix resin exists around the binding yarn 13. In the fiber reinforced resin, a resin rich portion tends to exist in the vicinity of the binding yarn 13, and microcracks are easily generated in the resin rich portion. However, when phenoxy resin is mixed, phenoxy resin is flexible because it has a long molecular chain, and has excellent flexibility, and also has good adhesion because it has a hydroxyl group as a hydrophilic group and a hydrocarbon group as a hydrophobic group. In addition, the toughness of the resin-rich portion is improved and the generation of microcracks is suppressed.
 積層繊維層12を結合する結合糸13は、積層繊維層12に一方の面から折り返した状態で挿入されるとともに、抜け止め糸15で抜け止めされる構成に限らない。それに代えてステッチ糸を使用し、針を用いて1本の結合糸13を積層繊維層12に一方の面から挿通し、他方の面で針の挿通位置を変えて折り返すように挿通し、その繰り返しによって積層繊維層12を結合するようにしてもよい。 The binding yarn 13 that bonds the laminated fiber layer 12 is not limited to the configuration in which the laminated fiber layer 12 is inserted into the laminated fiber layer 12 in a folded state from one surface and is prevented from being detached by the retaining yarn 15. Instead, a stitch thread is used, and a single binding thread 13 is inserted into the laminated fiber layer 12 from one side using a needle, and the needle is inserted in the other side so that the needle insertion position is changed. The laminated fiber layer 12 may be bonded by repetition.
 結合糸13の挿入間隔または密度は、目的とする複合材に要求される強度に対応して設定してもよい。 The insertion interval or density of the binding yarn 13 may be set according to the strength required for the target composite material.
 第1及び第2連続繊維14a,14bからなる第1及び第2繊維層12a,12bが積層された積層繊維層12は、少なくとも2軸配向であればよく、連続繊維の配列角度は、0度と90度との組み合わせに限らない。例えば、配列角度が0度と90度との繊維層に加え、配列角度が+45度及び-45度の連続繊維からなる繊維層を設けて4軸配向の構成を採用したり、配列角度が0度又は90度の連続繊維と、その連続繊維に対して斜めに配列されるバイアス繊維束との組み合わせによる3軸配向の構成を採用したりしてもよい。 The laminated fiber layer 12 in which the first and second fiber layers 12a and 12b composed of the first and second continuous fibers 14a and 14b are laminated may be at least biaxially oriented, and the arrangement angle of the continuous fibers is 0 degree. And the combination of 90 degrees. For example, in addition to a fiber layer with an arrangement angle of 0 degrees and 90 degrees, a fiber layer composed of continuous fibers with an arrangement angle of +45 degrees and −45 degrees is provided, and a configuration with a four-axis orientation is adopted, or the arrangement angle is 0 Alternatively, a triaxially oriented configuration may be adopted, which is a combination of a continuous fiber having a degree or 90 degrees and a bias fiber bundle arranged obliquely with respect to the continuous fiber.
 積層繊維層12は、配列角度が同じ連続繊維がそれぞれ一平面上に位置するように配列されて構成された複数の繊維層が積層された構成に限らず、繊維層として織物が積層された構成であってもよい。織物としては、例えば、平織りの織物が使用されるが、二重織物、三重織物、風通織物等の多層織物を積層してもよい。この場合、連続繊維を配列した繊維層を積層して積層繊維層12を構成するより、積層繊維層12の形成を短時間で行うことができる。 The laminated fiber layer 12 is not limited to a configuration in which a plurality of fiber layers configured such that continuous fibers having the same arrangement angle are positioned on a single plane, but a configuration in which a woven fabric is laminated as a fiber layer. It may be. As the woven fabric, for example, a plain woven fabric is used, but a multilayer woven fabric such as a double woven fabric, a triple woven fabric, or an air woven fabric may be laminated. In this case, the laminated fiber layer 12 can be formed in a shorter time than the laminated fiber layer 12 is formed by laminating fiber layers in which continuous fibers are arranged.
 平板状の三次元繊維構造体11から構成される曲げ部16を有する三次元繊維構造体11の形状は、図2に示すように、4つの曲げ部16を有する構成に限らない。例えば、図3(a)に示すように、1つの曲げ部16を有する断面L字状の構成や、図3(b)に示すように、2つの曲げ部16を有する断面クランク状の構成にしてもよい。 The shape of the three-dimensional fiber structure 11 having the bent portion 16 constituted by the flat plate-like three-dimensional fiber structure 11 is not limited to the configuration having the four bent portions 16 as shown in FIG. For example, as shown in FIG. 3A, a cross-sectional L-shaped configuration having one bent portion 16 or a cross-sectional crank-shaped configuration having two bent portions 16 as shown in FIG. May be.
 11…三次元繊維構造体、12…積層繊維層、12a,12b…第1及び第2繊維層、13…結合糸、14a,14b…第1及び第2連続繊維。 DESCRIPTION OF SYMBOLS 11 ... Three-dimensional fiber structure, 12 ... Laminated fiber layer, 12a, 12b ... 1st and 2nd fiber layer, 13 ... Binding yarn, 14a, 14b ... 1st and 2nd continuous fiber.

Claims (7)

  1.  連続繊維からなる繊維層が積層され、かつ、少なくとも2軸配向を有する積層繊維層と、前記繊維層と交差する方向に配列される部分を有する結合糸とを有し、前記積層繊維層が前記結合糸によって結合された三次元繊維構造体であって、前記結合糸として螺旋状の糸が使用されていることを特徴とする三次元繊維構造体。 A fiber layer composed of continuous fibers is laminated, and has a laminated fiber layer having at least biaxial orientation, and a binding yarn having a portion arranged in a direction intersecting the fiber layer, and the laminated fiber layer is A three-dimensional fiber structure bonded by a binding yarn, wherein a helical thread is used as the binding yarn.
  2.  前記螺旋状の糸は、100~1000回転/mの螺旋のピッチを有する請求項1に記載の三次元繊維構造体。 The three-dimensional fiber structure according to claim 1, wherein the helical thread has a helical pitch of 100 to 1000 revolutions / m.
  3.   前記結合糸の積層繊維層からの抜け止めを行う抜け止め糸を更に有する請求項1に記載の三次元繊維構造体。 The three-dimensional fiber structure according to claim 1, further comprising a retaining thread for retaining the binding thread from the laminated fiber layer.
  4.  前記結合糸は、芯糸とその芯糸の周囲を覆う鞘とを備えた芯鞘構造を有する糸の鞘の部分を構成する糸である請求項1又は請求項2に記載の三次元繊維構造体。 The three-dimensional fiber structure according to claim 1 or 2, wherein the binding yarn is a yarn constituting a sheath portion of a yarn having a core-sheath structure including a core yarn and a sheath covering the periphery of the core yarn. body.
  5.  請求項1~4のいずれか一項に記載の前記三次元繊維構造体に熱硬化製樹脂又は熱可塑性樹脂が含浸されたプリプレグ。 A prepreg obtained by impregnating the three-dimensional fiber structure according to any one of claims 1 to 4 with a thermosetting resin or a thermoplastic resin.
  6.  連続繊維からなる繊維層が積層され、かつ、少なくとも2軸配向を有する積層繊維層と、前記繊維層と交差する方向に配列される部分を有する結合糸とを有し、前記積層繊維層が前記結合糸によって結合された三次元繊維構造体の製造方法において、
     前記結合糸は、芯糸とその芯糸の周囲を覆う鞘とを備えた芯鞘構造の糸における前記鞘を構成する螺旋状の糸であり、
     前記芯糸が熱硬化性樹脂に溶解可能な繊維で構成され、前記鞘の部分を構成する糸が熱硬化性樹脂に溶解不能な繊維で構成され、
     前記三次元繊維構造体を強化基材として使用し、前記三次元繊維構造体に未硬化の前記熱硬化性樹脂を含浸させた状態で成形型により賦形しつつ前記熱硬化性樹脂を硬化させる繊維強化複合材の製造方法。
    A fiber layer composed of continuous fibers is laminated, and has a laminated fiber layer having at least biaxial orientation, and a binding yarn having a portion arranged in a direction intersecting the fiber layer, and the laminated fiber layer is In the method for producing a three-dimensional fiber structure bonded by a binding yarn,
    The binding yarn is a helical thread that constitutes the sheath in a core-sheath yarn comprising a core yarn and a sheath covering the periphery of the core yarn,
    The core yarn is composed of a fiber that can be dissolved in a thermosetting resin, and the yarn constituting the sheath portion is composed of a fiber that is insoluble in the thermosetting resin,
    The three-dimensional fiber structure is used as a reinforcing substrate, and the thermosetting resin is cured while being shaped by a mold in a state where the three-dimensional fiber structure is impregnated with the uncured thermosetting resin. Manufacturing method of fiber reinforced composite material.
  7. 前記芯糸としてフェノキシ樹脂繊維が使用される請求項6に記載の繊維強化複合材の製造方法。 The method for producing a fiber-reinforced composite material according to claim 6, wherein a phenoxy resin fiber is used as the core yarn.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4000843A4 (en) * 2019-07-19 2022-08-24 Kabushiki Kaisha Toyota Jidoshokki Fiber structure and fiber-reinforced composite

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02133632A (en) * 1988-11-10 1990-05-22 Toray Ind Inc Sewing yarn for forming preform material for reinforcing resin
JP2003129351A (en) * 2001-10-18 2003-05-08 Toyobo Co Ltd Woven interlining cloth excellent in stretch recovery
JP2007152672A (en) * 2005-12-02 2007-06-21 Fuji Heavy Ind Ltd Three-dimensional fiber-reinforced resin composite material and three-dimensional fabric
JP2007283586A (en) * 2006-04-14 2007-11-01 Toyota Industries Corp Manufacturing process of fiber-reinforced composite
JP2008112720A (en) * 2006-10-04 2008-05-15 Shinano Kenshi Co Ltd Conductive material and its manufacturing method

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02133632A (en) * 1988-11-10 1990-05-22 Toray Ind Inc Sewing yarn for forming preform material for reinforcing resin
JP2003129351A (en) * 2001-10-18 2003-05-08 Toyobo Co Ltd Woven interlining cloth excellent in stretch recovery
JP2007152672A (en) * 2005-12-02 2007-06-21 Fuji Heavy Ind Ltd Three-dimensional fiber-reinforced resin composite material and three-dimensional fabric
JP2007283586A (en) * 2006-04-14 2007-11-01 Toyota Industries Corp Manufacturing process of fiber-reinforced composite
JP2008112720A (en) * 2006-10-04 2008-05-15 Shinano Kenshi Co Ltd Conductive material and its manufacturing method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4000843A4 (en) * 2019-07-19 2022-08-24 Kabushiki Kaisha Toyota Jidoshokki Fiber structure and fiber-reinforced composite

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