JP2006015663A - Method for manufacturing fiber-reinforced resin structure, fiber-reinforced resin structure and composite base material - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for manufacturing a fiber-reinforced resin structure with high strength and at a low cost, a fiber-reinforced resin structure and a composite base material used for the former. <P>SOLUTION: The method for manufacturing the fiber-reinforced resin structure comprises a process to arrange the composite base material 100 inside a molding die, a process to supply an uncured resin inside the molding die and a process to cure the uncured resin. The composite base material 100 is complete with a fiber base material 20, a plurality of fiber bundles 50A arranged in parallel with each other on the fiber base material 20 and a sewing thread 70. The sewing thread 70 sews the fiber base material 20 and a plurality of the fiber bundles 50A together. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

  The present invention relates to a method for producing a fiber-reinforced resin structure, a fiber-reinforced resin structure, and a composite base material used for these.

  BACKGROUND ART Fiber reinforced resin structures reinforced with a fiber base material such as glass cloth are used in a wide range of fields such as bathtubs and ship casings. Such a fiber reinforced resin structure is manufactured by filling an uncured resin in a space having a predetermined shape in which a fiber base material is disposed and curing the resin.

  Specifically, for example, an RTM (Resin Transfer Molding) method in which a fiber base material is placed in a space defined by a pair of molds and uncured resin is supplied into this space, VaRTM (Vacuum Assisted Resin Transfer Molding) method for supplying a cured resin, a fiber base material is placed in a space defined between a mold and a flexible film, and this space is uncured while decompressing the space. A vacuum infusion method for supplying resin is known.

  In recent years, in order to further improve the performance of the fiber reinforced resin structure, it is required to reduce the voids in the fiber reinforced resin structure, and the uncured resin is quickly and sufficiently impregnated in the fiber base material. There is a need.

As a method for sufficiently impregnating the uncured resin in the fiber substrate, for example, a flow net which is a thermoplastic resin such as polypropylene or polyethylene or a mesh-like sheet made of metal is used as a mold or a flexible On the surface of a core material such as a foaming substance or the like, which is disposed between a porous film and a fiber base material to supply uncured resin (see, for example, Patent Documents 1 and 2) A method for forming grooves (for example, refer to Patent Document 3), a method for forming irregularities on the inner surface of a mold (for example, refer to Patent Documents 1 and 3), and a conduit for dispersing resin and supplying it into the space. A method of forming a mold or a flexible film (for example, Patent Document 4) is known. It is also known to use a continuous strand mat as a fiber base (for example, Patent Document 5).
JP 2001-62932 A US Pat. No. 4,902,215 JP 2000-501659 A Japanese National Patent Publication No. 10-504501 JP 2002-120315 A

  However, even if a flow net as described above, a mold having a groove, unevenness, conduit, etc., a flexible film, or a core material having a groove are used, the fiber base material is not yet used. The cured resin may not be sufficiently impregnated, and the strength of the fiber reinforced resin structure may be reduced. Moreover, since the above-mentioned fluid net needs to be finally removed, the cost is increased and the environment is deteriorated due to an increase in waste. Furthermore, it is not easy to produce a mold having grooves, irregularities, conduits, etc., or a core material having grooves, which often leads to an increase in cost.

  In addition, when a continuous strand mat is used as a fiber base material, this continuous strand mat is formed by stacking continuous glass fibers in a spiral shape and molding it into a mat shape with a binder, and because it has a strong repulsive force, it is shaped. It is difficult to increase the amount of the glass component, and the impregnation of the resin is easily inhibited by the binder component. Therefore, also in this case, the strength of the fiber reinforced resin structure tends to be weak.

  The present invention has been made in view of the above problems, and an object of the present invention is to provide a fiber reinforced resin structure manufacturing method, a fiber reinforced resin structure, and a composite base material used for these, which are high in strength and low in cost. And

The method for producing a fiber-reinforced resin structure according to the present invention includes a step of placing a composite substrate in a mold,
A step of supplying an uncured resin into the mold and a step of curing the uncured resin. The composite base material includes a fiber base material, a plurality of fiber bundles A arranged in parallel with each other on the fiber base material, and a sewing thread. The sewing thread stitches the fiber base material and the plurality of fiber bundles A together. .

  According to the present invention, uncured resin can suitably flow along the gap between the fiber bundles A in the mold. Further, in the composite base material, the fiber bundle A is sewn to the fiber base material with a sewing thread. Therefore, compared to the case where the fiber bundle A and the fiber base material are combined with a binder or the like, the inside of the fiber base material and the fiber The uncured resin can be suitably impregnated in the bundle A, and the uncured resin can easily penetrate through the composite substrate and flow. Therefore, it becomes easy to spread uncured resin evenly in the mold, and the number of unimpregnated portions of the resin in the fiber-reinforced resin structure can be reduced.

  Further, in the composite base material, the fiber bundle A is sewn to the fiber base material with a sewing thread, so that the resin impregnation is superior to the case where the fiber bundle A and the fiber base material are combined with a binder or the like. Furthermore, the glass content in the fiber reinforced resin structure can be increased.

  As a result, a fiber-reinforced resin structure having a sufficiently high strength can be obtained.

  Furthermore, since this composite base material functions as a fiber reinforcing material, it is not necessary to remove the composite base material after forming the fiber reinforced resin structure, and the composite base material itself can be easily manufactured. A reinforced resin structure can be manufactured.

  Here, the fineness of the fiber bundle A is 500 to 5000 tex, and the arrangement density of the fiber bundle A on the fiber substrate is preferably 4 to 10 fibers / 25 mm.

According to this, since gaps are formed between the fiber bundles A with an appropriate width, an appropriate height, and an appropriate repetition interval, the uncured resin can flow well through the gaps. Here, if the fineness is less than 500 tex, it is difficult to ensure a sufficient height of the fiber bundle A on the fiber base material, and the fluidity tends to be lowered. On the other hand, if the fineness exceeds 5000 tex, the number of gaps that can be secured on the fiber base tends to be too small. Furthermore, when the density of the fiber bundle A on the fiber substrate exceeds the range of 4 to 10 fibers / 25 mm, the gap interval tends to be too wide or too narrow.
In particular, in order to sufficiently ensure the fluidity of the resin, the ratio of the fiber bundle width of the fiber bundle A to the gap between the fiber bundles A in the composite base material is 3: 1 to 1: 2. Preferably, it is 2: 1 to 1: 1.5.

  When the fineness of the fiber bundle A is relatively large, the fiber bundle A is preferably a bundle of a plurality of fiber bundles AA.

  According to this, since the fiber bundle A in which a plurality of fiber bundles AA are bundled is stitched to the fiber base material, the fiber bundle A is not easily crushed even if it receives pressure in the mold, and the fiber bundle A The width and height of the gap are easily maintained. A suitable fineness of each fiber bundle AA is 500 to 2000 tex.

  Further, between the fiber bundles A, a fiber bundle B which is arranged in parallel with the fiber bundle A and has a fineness smaller than the fineness of the fiber bundle A is further arranged, and the fiber bundle B and the fiber base material are stitched together with a sewing thread. May be.

  According to this, the glass content of the fiber reinforced resin structure can be easily improved without significantly reducing the fluidity of the resin.

  In the composite base material, it is preferable that the fiber bundle A and the fiber base material are sewn together by tricot knitting using a sewing thread.

  When the fiber bundle A is sewn to the fiber base material by tricot knitting in this way, the fiber bundle A is more difficult to be crushed and a sufficient gap is secured between the fiber bundles A.

  The fiber base material is preferably formed from a plurality of fiber bundles C arranged in a direction intersecting with the fiber bundle A and arranged in parallel to each other.

  According to this, since the uncured resin can further flow along the gap of the fiber bundle C, the resin can easily flow in the direction orthogonal to the fiber bundle A, and the fiber reinforcement with less unimpregnated portion of the resin. A resin structure can be formed. Further, the strength of the fiber reinforced resin structure including the composite base material is sufficiently strengthened in the direction intersecting the fiber bundle A. Furthermore, it becomes easier for uncured resin to flow across the composite substrate.

  Further, in the step of arranging the composite base material in the mold, it is preferable to arrange a plurality of the composite base materials in a stacked manner.

  According to this, since a plurality of composite base materials are laminated, a fiber-reinforced resin structure having a large thickness can be suitably manufactured while reducing the number of unimpregnated portions of the resin. As an arrangement interval of the composite base material, an interval of 1 to 10 mm is preferable in a state after curing.

  Moreover, as for a shaping | molding die, it is preferable that one side is a metal mold | die and the other is a metal mold | die or a film.

  According to this, a fiber reinforced resin structure can be suitably manufactured in the RTM method, VaRTM method, infusion method or the like.

  A composite base material according to the present invention includes a fiber base material, a plurality of fiber bundles A arranged in parallel to each other on the fiber base material, and a sewing thread, and the sewing thread stitches the fiber base material and the plurality of fiber bundles A together. ing. Moreover, in this composite base material, the fineness of the fiber bundle A is 500 to 5000 tex, and the arrangement density of the fiber bundle A on the fiber base material is 4 to 10 fibers / 25 mm. Furthermore, in this composite base material, the fiber base material is formed of a plurality of fiber bundles C arranged in a direction intersecting with the fiber bundle A and arranged in parallel to each other.

  Such a composite base material is suitable as a fiber reinforcing material for the above-mentioned fiber reinforced resin structure.

  Here, it is preferable that the fiber bundle A and the fiber base material are sewn together by tricot knitting using a sewing thread.

  The fiber reinforced resin structure according to the present invention includes the above-described composite base material and a resin impregnated in the composite base material.

  ADVANTAGE OF THE INVENTION According to this invention, the manufacturing method of a fiber reinforced resin structure with high intensity | strength and low cost, a fiber reinforced resin structure, and the composite base material used for these are provided.

  Hereinafter, preferred embodiments of a method for producing a fiber-reinforced resin structure, a fiber-reinforced resin structure, and a composite substrate of the present invention will be described in detail with reference to the drawings. In the following description, the same or corresponding parts are denoted by the same reference numerals, and redundant description is omitted.

(First embodiment)
First, the manufacturing method of the fiber reinforced resin structure which concerns on 1st embodiment of this invention, and the composite base material used for this are demonstrated.

(Composite substrate)
In manufacturing a fiber reinforced resin structure, first, a composite substrate 100 as shown in FIGS. 1 to 2 is prepared.

  The composite substrate 100 includes a fiber substrate 20 having a plurality of fiber bundles 10 (fiber bundles C), a plurality of fiber bundles 50 (fiber bundles A) arranged in parallel with each other at a predetermined interval on the fiber substrate 20, and Each fiber bundle 50 has a sewing thread 70 for sewing and fixing the fiber base material 20 and has a sheet shape.

  The fiber base material 20 is simply a fiber bundle 10 (fiber bundle C) formed by bundling a large number of fibers and arranged substantially parallel at a predetermined interval. Such a fiber base material 20 sufficiently strengthens the strength of a fiber reinforced resin structure (described later) including the composite base material 100 in a direction parallel to the fiber bundle 10, that is, a direction orthogonal to the fiber bundle 50. preferable. In addition, a gap 53 is formed between the fiber bundles 10, and the resin easily flows in a direction along the gap 53, that is, in a direction orthogonal to the fiber bundle 50. The flow of the uncured resin to the substrate can also be improved, and a fiber-reinforced resin structure with fewer unimpregnated portions of resin can be formed.

  The fineness and pitch of the fiber bundle 10 are not particularly limited, but from the viewpoint of improving the flow of uncured resin in the direction parallel to the fiber bundle 10 and the flow of uncured resin in the direction penetrating the fiber base material 20. It is determined on the basis of the characteristics of the fiber bundle 50 to be described later. Specifically, the weight ratio R = (weight of the fiber bundle 50 / weight of the fiber bundle 10) is a numerical value that is 0.4 to 2.5. It is preferable that

  Each of the fiber bundles 50 is a fiber bundle having a large number of glass fibers, and is directed in a direction intersecting with the axial direction of the fiber bundle 10 of the fiber substrate 20, preferably in a direction orthogonal to the axial direction of the fiber bundle 10. It is arranged so as to overlap on the fiber base material 20.

  The fineness of each fiber bundle 50 and the arrangement density of the fiber bundle 50 on the fiber substrate 20 are not particularly limited, but the fineness of the fiber bundle 50 is 500 to 5000 tex and the arrangement density of the fiber bundle 50 is 4 to 10 per 25 mm. Preferably there is. As a result, a gap 52 disposed between the fiber bundles 50 with a sufficient height, a sufficient width, and a suitable interval can be secured, and a good flow of uncured resin along the gap 52 is realized. The Here, if the fineness of the fiber bundle 50 is less than 500 tex, it is difficult to ensure a sufficient height of the fiber bundle 50 on the fiber base material 20, and the fluidity of the uncured resin tends to be lowered. On the other hand, when the fineness exceeds 5000 tex, the number of the gaps 52 that can be secured on the fiber base material 20 tends to be too small. Furthermore, when the density of the fiber bundle 50 on the fiber base 20 exceeds the range of 4 to 10 pieces / 25 mm, the gap 52 tends to be too wide or too narrow. In particular, the ratio between the fiber bundle width W50 (see FIG. 1) of the fiber bundle 50 (fiber bundle A) in the composite base material 100 and the gap G50 between the fiber bundles 50 in order to sufficiently secure the fluidity of the resin. Is preferably 3: 1 to 1: 2, more preferably 2: 1 to 1: 1.5.

  Further, the fiber bundle 50 is formed by bundling a plurality of fiber bundles 55 (fiber bundles AA) including a large number of fibers as shown in FIG. 2 when the fineness is relatively large, such as when the fineness exceeds 2000 tex. It is preferable. As described above, when each fiber bundle 50 includes a plurality of fiber bundles 55, the fiber bundle 50 is not easily crushed even under pressure, and a gap 52 having a sufficient height and width is easily held between the fiber bundles 50. The fineness of each fiber bundle 55 is preferably 500 to 2000 tex, more preferably 500 to 1500 tex, and each fiber bundle 50 preferably includes about 2 to 3 such fiber bundles 55.

  Here, although the material of the fiber of the fiber base material 20 and the fiber bundle 50 is not specifically limited, Glass fiber, an aramid fiber, carbon fiber, etc. can be used conveniently, Especially glass fiber can be used conveniently.

  The sewing thread 70 is used to sew and fix the fiber bundle 50 and the fiber base material 20 together. The fineness of the sewing thread 70 is preferably 50 to 200 denier. The stitch pitch of the sewing thread 70 is preferably 4 to 20/25 mm.

  Although the material of the sewing thread 70 is not particularly limited, for example, a thread made from a fiber such as glass or resin such as polyester can be suitably used.

  The method of sewing with the sewing thread 70 is not particularly limited, but it is preferable that the sewing thread 70 sews each fiber bundle 50 and each fiber bundle 10 of the fiber base material 20 by tricot knitting. As a result, the fiber bundle 50 becomes more difficult to be crushed even under pressure during molding, and a gap is easily maintained between the fiber bundles 50.

(Manufacturing method of fiber reinforced resin structure)
Then, the manufacturing method of the fiber reinforced resin structure using such a composite base material as a fiber reinforced material is demonstrated.

  First, as shown in FIGS. 3 and 4, a reinforced base material layer is provided between a lower mold (metal mold) 150 made of metal or the like having a predetermined surface shape and a flexible vacuum bag (film) 160. 300 is arranged.

  Specifically, for example, the composite base material 100 and the fiber base material 200 are laminated in a predetermined manner on the lower mold 150 and placed as the reinforced base material layer 300.

  As a lamination method, for example, as shown in FIG. 3, one or a plurality of fiber base materials 200 and a single composite base material 100 are alternately laminated to form a reinforced base material layer 300. it can.

  Here, in the reinforced base material layer 300, in order to improve the fluidity of the uncured resin by reducing the thickness of one or more fiber base materials 200 sandwiched between the composite base materials 100 as much as possible. The arrangement interval of 100, that is, the thickness of one or a plurality of fiber substrates 200 sandwiched between the composite substrates 100 is preferably set to an interval of 1 to 10 mm in a state after curing.

  Further, the thickness of one or a plurality of fiber substrates 200 disposed between the composite substrate 100 and the vacuum bag 160 and between the composite substrate 100 and the lower mold 150 is also determined between the composite substrates 100. Preferably, the thickness is the same as when sandwiched between the two. Note that the composite base material 100 may be disposed so as to contact the lower mold 150 and the vacuum bag 160.

  The fiber base material 200 is not particularly limited as long as it is a base material that can reinforce the resin, but a cloth formed from glass fiber, carbon fiber, aramid fiber, etc., chopped strand mat, continuous strand mat, multiaxial assembly fabric, etc. Can be used, and these can include a single sheet or a plurality of sheets.

  Thereafter, plate-like jigs 154 a and 154 b are respectively spanned between the edge regions 300 a and 300 b on the upper surface of the reinforcing base layer 300 facing each other and the surface of the lower mold 150. The jigs 154 a and 154 b are configured to define predetermined gaps 153 a and 153 b between the vacuum bag 160 and the lower molding die 150 on the outer sides of both end faces of the reinforced base material layer 300. Here, as shown in FIG. 4, the direction of the axis of the fiber bundle 50 of the composite substrate 100 is parallel to the direction in which the pair of jigs 154a and 154b are connected, that is, the direction in which the resin flows as described later. Has been.

  Here, as shown in FIGS. 3 and 4, an opening 156a of a line 156 for supplying uncured liquid resin is formed on the surface of the lower mold 150 facing the jig 154a (left side in the figure). In addition, an opening 158a of a line 158 that exhausts gas from above the lower mold 150 by pressure reduction is formed on the surface of the lower mold 150 that faces the jig 154b (right side in the drawing). . Line 156 is connected to a pump (not shown) that supplies uncured resin, while line 158 is connected to a vacuum pump (not shown).

  Subsequently, after the sealing material 162 is disposed on the lower mold 150 so as to surround the reinforcing base material layer 300 and the jigs 154a and 154b, the vacuum bag 160 formed of a flexible film is reinforced. The lower mold 150 is placed over the base material layer 300 and the jigs 154a and 154b.

  Here, the film of the vacuum bag 160 is not particularly limited as long as it is an airtight and flexible material. For example, a film of nylon, polyester, polyethylene, PVC polypropylene, polyimide, or the like can be used.

(Resin supply and curing)
Subsequently, the air formed in the space between the vacuum bag 160 and the lower mold 150 is decompressed by exhausting air from the line 158. As a result, the vacuum bag 160 is pressed downward by atmospheric pressure. Then, while continuing the exhaust, an uncured liquid resin 90 is supplied from a line 156 into a space formed between the vacuum bag 160 and the lower mold 150. Here, the vacuum bag 160 and the lower mold 150 constitute the mold 170.

  Here, the uncured liquid resin 90 to be supplied is not particularly limited as long as it is a curable resin. For example, heat such as epoxy resin, phenol resin, unsaturated polyester resin, vinyl ester resin, and modified epoxy resin can be used. A curable resin is mentioned.

  Then, after the uncured resin is supplied, the uncured resin is cured by predetermined heating or cooling to room temperature by being left standing. Thereafter, the vacuum bag 160 is removed, and the fiber reinforced resin structure 400 in which the cured resin 95 and the reinforced base layer 300 are integrated is taken out as shown in FIG. The manufacturing method of the fiber reinforced resin structure is thus completed. The manufactured fiber reinforced resin structure 400 includes the fiber substrate 200, the composite substrate 100, and the cured resin 95 impregnated therein.

  According to such a method of manufacturing a fiber reinforced resin structure, the fiber base material 200 is pressed against the composite base material 100 by pressure reduction by a vacuum pump. However, a gap 52 (see FIGS. 1 and 2) formed between the fiber bundles 50 of the composite substrate 100 is formed between the composite substrate 100 and the fiber substrate 200. For this reason, the uncured resin 90 supplied from the line 156 easily flows in the horizontal direction shown in FIGS. 1 and 3 using the gap 52 as a flow path. The uncured resin 90 that has preferably moved along the gap 52 of the composite substrate 100 in this manner is then preferably impregnated into the fiber substrate 200 on the side facing the fiber bundle 50 of the composite substrate 100. Can do.

  In addition, since the composite base material 100 itself is obtained by stitching the fiber base material 20 and the fiber bundle 50 with the sewing thread 70 without using a binder or the like, the uncured resin is used for the fiber base material 20 of the composite base material 100. It can flow through easily. Therefore, the uncured resin can be sufficiently impregnated into the fiber substrate 200 facing the fiber substrate 20 of the composite substrate 100. Furthermore, since the fiber base material 20 and the fiber bundle 50 of the composite base material 100 do not contain a binder, the uncured resin is preferably impregnated.

  Thereby, uncured resin can be impregnated over every corner of each fiber base material 200 and composite base material 100 between the vacuum bag 160 and the lower mold 150, and the resin in the fiber reinforced resin structure can be impregnated. The number of unimpregnated parts can be reduced.

  Moreover, since this composite base material 100 does not contain a binder or the like, the resin is easily impregnated into each of the fiber bundles 10 and 50, and further, the glass content of the fiber reinforced resin structure can be easily improved. Can do.

  As a result, according to the present production method, a fiber-reinforced resin structure having a sufficiently high strength can be obtained.

  Further, since the composite base material 100 functions as a fiber reinforcement, it is not necessary to remove the composite base material from the fiber reinforced resin structure after the formation of the fiber reinforced resin structure, and the composite base material 100 itself is easy. Therefore, a fiber reinforced resin structure can be manufactured at low cost.

  In addition, since a plurality of composite base materials 100 are disposed between the vacuum bag 160 and the lower mold 150, a thick fiber reinforced resin structure can be formed while reducing unimpregnated portions of the resin. It can manufacture suitably. In this embodiment, the fiber base material 200 is sandwiched between the composite base materials 100, but the present invention can be implemented without the fiber base material 200 being sandwiched.

  Further, the uncured resin 90 is supplied along the axis direction of the fiber bundle 50 of the composite substrate 100. Therefore, the flow of the uncured resin is made smoother from the gap 153a toward the gap 153b.

  Furthermore, since the pressure in the space formed between the vacuum bag 160 and the lower mold 150 is reduced, the uncured resin can be more easily impregnated into the reinforced base material layer 300, and the line The supply pressure of the uncured resin from 156 can be lowered.

  Furthermore, since the fiber base 20 is formed of a plurality of fiber bundles 10 arranged in a direction intersecting with the fiber bundle 50, the uncured resin is further formed along the gap 53 (see FIG. 1) of the fiber bundle 10. 90 can flow, the uncured resin 90 can easily flow in the direction orthogonal to the fiber bundle 50, and the fiber reinforced resin structure 400 with fewer unimpregnated portions of the resin can be formed. Further, the strength of the fiber reinforced resin structure 400 including the composite substrate 100 is sufficiently strengthened in the direction intersecting the fiber bundle 50.

(Second embodiment)
Subsequently, a second embodiment of the present invention will be described with reference to FIGS. Since this embodiment is different from the first embodiment only in the composite base material, only this will be described. The composite substrate 110 in this embodiment is different from the composite substrate 100 in that fiber bundles 60 (fiber bundles B) are arranged between the fiber bundles 50 on the fiber substrate 20. The fiber bundles 60 are arranged in parallel with the fiber bundle 50, that is, so as to intersect with the fiber bundle 10 of the fiber base 20. Correspondingly, the sewing thread 70 fixes the fiber bundle 50 and the fiber bundle 60 to the fiber base material 20 by tricot knitting.

  The fiber bundle 60 is formed by bundling a large number of glass fibers similar to the fiber bundle 50, and the fineness thereof is preferably smaller than the fiber bundle 50 and 40% or less of the fiber bundle 50. More preferably, it is 30% or less of the bundle 50.

  According to such a composite substrate 110, the glass content of the fiber-reinforced resin structure can be increased without significantly impairing the fluidity of the uncured resin as compared with the composite substrate 100.

(Third embodiment)
Next, a third embodiment of the present invention will be described with reference to FIG. This embodiment is different from the first and second embodiments in that a VaRTM (Vacuum Assisted Resin Transfer Molding) method is employed instead of the vacuum infusion method. Specifically, instead of the vacuum bag 160, an upper mold (mold) 155 made of metal or the like having a predetermined surface shape is used. Also in this embodiment, there exists an effect similar to 1st and 2nd embodiment. Here, the upper mold 155 and the lower mold 150 constitute a mold 175.

  In addition, this invention is not limited to the said embodiment, It can take various deformation | transformation aspects.

  For example, in the above embodiment, the reinforced base material layer 300 is formed from the composite base material 100 and the fiber base material 200, but may be formed only from the composite base material 100.

  Moreover, in the said embodiment, although the direction of the axis | shaft of the fiber bundle 50 of the composite base material 100 is made the same as the direction through which uncured resin flows, implementation is also possible as a crossing direction.

  Moreover, in the said embodiment, although the fiber base material 20 which arranged the fiber bundle 10 is employ | adopted, as the fiber base material 20, fiber bundles, such as a chopped strand mat and a continuous strand mat, are not located in parallel. The present invention can also be carried out using a knitted fabric or a knitted fiber bundle such as a roving cloth.

  Moreover, in the said embodiment, although the surface of the lower side shaping | molding die 150 is planar, the surface shape of the lower side shaping | molding die 150 or the upper side shaping | molding die 155 is changed according to the shape of the fiber reinforced resin structure to manufacture. It goes without saying that it is good. The material of the mold such as the lower mold or the upper mold is not particularly limited as long as it does not cause a problem due to deformation or the like due to temperature and pressure during molding. For example, the material of the mold includes metals such as iron and stainless steel, fiber reinforced thermosetting resin (FRP), wood, and the like.

  Furthermore, in the said embodiment, although the inside of the space where uncured resin should be supplied is pressure-reduced, even if it press-fits uncured resin with a normal pressure, implementation is possible.

  Subsequently, an example according to the present embodiment will be described.

First, the composite base materials C _{1 to} C ₆ , roving cloth R ₁ , roving cloth R ₂ and chopped strand mat M used in this example will be described.

The composite base material C ₁ has a plurality of fiber bundles C arranged in parallel with each other at a pitch of 7/25 mm on a fiber base material in which a plurality of fiber bundles C are arranged in parallel with a pitch of 12.2 / 25 mm. The fiber bundle C and the fiber bundle A are sewn together by tricot knitting using a sewing thread so that the fiber bundle C and the fiber bundle A are arranged vertically. The fiber bundle A is made of one glass fiber bundle AA having a fineness of 1100 tex, the fiber bundle C is made of one glass fiber bundle having a fineness of 280 tex, the sewing thread is a polyester yarn having a fineness of 70 denier, and the pitch of the tricot knitting is 12 Book / 25 mm. The fiber bundle width of the fiber bundle A in the composite substrate C ₁ is 1.5 mm, and the gap between the fiber bundles A is 2 mm.

The composite substrate C ₂ is different from the composite substrate C _{1 in} that the fiber bundle A is a bundle of two glass fiber bundles AA having a fineness of 1100 tex, and the fiber bundle A has a fiber bundle width of 2 mm. The gap between the bundles A is 1.5 mm.

The difference between the composite base material C _{3 and the} composite base material C ₂ is that the fiber bundle B is arranged in parallel with the fiber bundle A between the fiber bundle A and the fiber bundle A, and the fiber bundle A and the fiber bundle B are arranged. This is a point where the fiber bundle C is sewn together with a sewing thread. The fiber bundle B is composed of one glass fiber bundle having a fineness of 280 tex.

The composite substrate C ₄ is different from the composite substrate C _{3 in} that the fiber bundle B is composed of one glass fiber bundle having a fineness of 600 tex and the pitch of the fiber bundle C is 12.4 fibers / 25 mm. .

The difference between the composite base material C _{5 and the} composite base material C ₂ is that the fiber bundle C is composed of one glass fiber bundle having a fineness of 600 tex and the pitch of the fiber bundle C is 12.4 pieces / 25 mm. .

The composite base material C ₆ is different from the composite base material C _{1 in} that the fiber bundle A is composed of one glass fiber bundle AA having a fineness of 2300 tex, and the fiber bundle A is arranged at a pitch of 4.5 pieces / 25 mm. The bundle C is composed of one glass fiber bundle having a fineness of 2300 tex, the fiber bundle C is arranged at a pitch of 8.5 pieces / 25 mm, and the fiber width of the fiber bundle A is 4 mm.

FIG. 9 shows the configuration and unit weight of these composite base materials C _{1 to} C ₆ , the basis weight K1 of (fiber bundle A + fiber bundle B), the basis weight K2 of fiber bundle C, and the basis weight ratio R = K1 / K2.

The roving cloth R ₁ is a glass fiber roving cloth (WR570) manufactured by Nitto Boseki Co., Ltd., with a pitch of 6.5 pieces / 25 mm, a width of 5.8 pieces / 25 mm, and a mass (single weight) of 580 g. / M ² .

Roving cloth _{R 2} is a Nitto Boseki Co., Ltd. fiberglass roving cloth (WR800), pitch vertical 4.6 present / 25 mm, lateral 3.8 present / 25 mm, the mass (unit weight) of 800 g / m ² .

The chopped strand mat M is a chopped strand mat (MC900) made using glass fibers manufactured by Nitto Boseki Co., Ltd., and has a mass (single weight) of 900 g / m ² .

(Examples 1-6, Comparative Example 1)
First, in Examples 1 to 6, each composite base material C _{1 to} C ₆ was used to evaluate the ease of flow of an uncured resin during infusion molding. First, it was cut such each composite matrix _C 1 -C ₆ to 300mm square. Then, each composite base material C ₁ -C ₆ three sheets so that the direction of the fiber bundle A are the same as the reinforced base material layer and disposed between the lower mold and Valentin accumulation bag.

  And while supplying an unsaturated polyester resin (Dainippon Ink Chemical Co., Ltd., polylite PC184, resin temperature 15-17 degreeC) from the one end side of the direction parallel to the axis | shaft of the fiber bundle A in a reinforcement base material layer, the other end The gas was discharged from the side by a vacuum pump and the pressure was reduced (depressurized value −0.05 MPa), and the time change of the flow front position of the resin in the direction parallel to the axis of the fiber bundle A was measured. Here, specifically, resin supply and gas exhaust were performed via spiral hoses provided at both ends in the axial direction of the fiber bundle A of the reinforced base material layer. A resin supply line and a gas exhaust line were connected to the center of each of the spiral hoses. Similarly, the same resin is supplied from one end side to the other end side in the direction (width direction of the fiber bundle A) perpendicular to the axis of the fiber bundle A to each reinforcing base layer, and the fibers The change in the flow front position in the direction perpendicular to the axis of the bundle A was also measured.

In Comparative Example 1, in place of the composite base material C _1, the position of the flow front, but using 3 sheets of roving cloth R ₁ cut to the same size as the composite matrix C ₁ in the same manner as in Example 1 The time change was measured. In Examples 1 to 6 and Comparative Example 1, no fluid resin net is used.

  In Examples 1 to 6 and Comparative Example 1, the time taken to advance the flow front position by 200 mm is shown in FIG. 10, the change of the flow front position in the direction parallel to the axis of the fiber bundle A is shown in FIG. The change of the flow front position in the direction orthogonal to the axis of the bundle A is shown as a graph in FIG.

  Compared to Comparative Example 1, it is confirmed that the uncured resin flows well in Examples 1 to 6. In particular, in Examples 1, 2, 3, 4, and 5, the flow in the direction parallel to the fiber bundle A is particularly good, and among them, the flow in the direction perpendicular to the fiber bundle A is particularly good and more preferable. .

(Example 7, Comparative Example 2)
In Example 7, the configuration of the reinforcing base material is (MR ₂ MC ₅ ) * 9 + MR ₂ M, and the time change of the flow front position in the direction parallel to the axis of the fiber bundle A in the same manner as described above And measured separately on the mold side. In Example 7, the resin net for flow is not used as in Examples 1-6. In the above configuration, M represents a chopped strand mat M, R ₂ represents a roving cloth R ₂ , and C ₂ represents a composite substrate C ₂ (the same applies hereinafter). “(MR ₂ MC ₅ ) * 9” means that (MR ₂ MC ₅ ) is repeated 9 times (the same applies hereinafter).

In Comparative Example 2, the configuration of the reinforced base material is (MR ₂ ) * 19 + M, and a conventional fluid resin net is interposed between the reinforced base material and the mold, and the same as described above. Then, the time change of the flow front position in the direction parallel to the axis of the fiber bundle A was individually measured on the film side and the mold side. The results are shown in FIG. In Example 7 using the composite substrate according to the present invention, as compared with the conventional Comparative Example 2, it is uncured satisfactorily without unevenness on both the vacuum bag side and the mold side without using a resin net for flow. Resin flowed. In addition, the thickness of the fiber reinforced resin structure after curing was about 27 mm.

(Examples 8 to 10, Comparative Example 3)
In Example 8, the configuration of the reinforced base material is MR ₂ MC ₅ from the vacuum bag side to the mold side, and the time change of the flow front position in the direction parallel to the axis of the fiber bundle A is performed in the same manner as described above. Measured separately on the vacuum bag side and the mold side. In Example 9, the configuration of the reinforced base material is MR ₂ MR ₂ MR ₂ MC ₅ , in Example 10, the configuration of the reinforced base material is MR ₂ MR ₂ MR ₂ MR ₂ MC _5, and in Comparative Example 3, The material configuration was MR ₂ MR ₂ MR ₂ MR ₂ MR ₅ M, and the time change of the flow front position in the direction parallel to the axis of the fiber bundle A was measured in the same manner as in Example 8. In Examples 8 to 10 and Comparative Example 3, the resin net for flow is not used. The results and the spacing between the composite substrates are shown in FIG.

  Although the fluidity slightly decreased as the distance between the composite substrates increased, Examples 8 to 10 exhibited sufficient fluidity compared to the comparative example.

(Example 11, Comparative Example 4)
In Example 11, the configuration of the reinforced base material is MC ₅ MC ₅ M from the vacuum bag side to the mold side, while in Comparative Example 4, the configuration of the reinforced base material is MR ₂ MR ₂ M and the fiber reinforced resin structure Body samples were obtained and examined for their glass content, 3-point bending strength, and flexural modulus. In particular, in Example 11, the three-point bending strength and the bending elastic modulus were measured in two directions, ie, the direction parallel to the axis of the fiber bundle A of the composite substrate in the sample and the direction orthogonal to the direction. As the resin, 100 parts by weight of an epoxy acrylate resin (Neopol 8250L manufactured by Nippon Iupika Co., Ltd.), 1.5 parts by weight of cumene hydroperoxide (Nippon Yushi Co., Ltd. Park Mill H-80) as a curing agent, A mixture of 0.3 part by weight of 6% cobalt naphthenate was used as a promoter. The reduced pressure value was −0.05 MPa, and after-curing was performed at 60 ° C. for 2 hours. In Example 11, no fluid resin net was used, but in Comparative Example 4, a fluid resin net was used. The three-point bending strength test was performed based on JISK7055. Specifically, since the thickness of the sample of the fiber reinforced resin structure in Example 11 was 3.8 mm, the test was performed at a distance between fulcrums of 60 mm and a test speed of 1.88 mm / min. Since the thickness of the sample was 4.4 mm, the test was performed at a distance between fulcrums of 70 mm and a test speed of 2.18 mm / min. In addition, five samples were prepared for each test. The results are shown in FIG.

  The fiber reinforced resin structure of Example 11 had higher three-point bending strength and bending elastic modulus than the fiber reinforced resin structure of Comparative Example 4.

FIG. 1 is a plan view of a composite substrate according to the first embodiment. FIG. 2 is a II-II cross-sectional view of the composite substrate of FIG. FIG. 3 is a schematic configuration diagram illustrating a method for manufacturing a fiber-reinforced resin structure according to the first embodiment. FIG. 4 is a partially broken top view of FIG. FIG. 5 is a schematic cross section showing a fiber reinforced resin structure obtained by the manufacturing method of FIG. FIG. 6 is a plan view of the composite substrate according to the second embodiment. 7 is a VII-VII cross-sectional view of the composite substrate of FIG. FIG. 8 is a schematic configuration diagram illustrating a method for manufacturing a fiber-reinforced resin structure according to the third embodiment. FIG. 9 is a table showing the configuration and the like of the composite substrate used in the examples. FIG. 10 is a table showing the results of Examples 1 to 6 and Comparative Example 1. FIG. 11 is a graph showing changes in the flow front position in the direction parallel to the fiber bundle 50 (fiber bundle A) in Examples 1 to 6 and Comparative Example 1. FIG. 12 is a graph showing changes in the flow front position in the direction orthogonal to the fiber bundle 50 (fiber bundle A) in Examples 1 to 6 and Comparative Example 1 (width direction of the fiber bundle A). FIG. 13 is a table showing the results of Example 7 and Comparative Example 2. FIG. 14 is a table showing the results of Examples 8 to 10 and Comparative Example 3. FIG. 15 is a table showing the results of Example 11 and Comparative Example 4.

Explanation of symbols

  DESCRIPTION OF SYMBOLS 10 ... Fiber bundle (fiber bundle C), 50 ... Fiber bundle (fiber bundle A), 55 ... Fiber bundle (fiber bundle AA), 60 ... Fiber bundle (fiber bundle B), 70 ... Sewing thread, 90 ... Uncured resin 95 ... Cured resin, 100 ... Composite base material, 150 ... Lower mold (mold), 155 ... Upper mold (mold), 160 ... Vacuum bag (film), 170, 175 ... Mold, 200 ... fiber reinforced resin structure.

Claims (11)

Placing the composite substrate in a mold;
Supplying an uncured resin into the mold,
Curing the uncured resin,
The composite substrate includes a fiber substrate, a plurality of fiber bundles A arranged in parallel to each other on the fiber substrate, and a sewing thread, and the sewing thread stitches the fiber substrate and the plurality of fiber bundles A together. A method for producing a fiber-reinforced resin structure. The fineness of the fiber bundle A is 500 to 5000 tex,
The method for producing a fiber-reinforced resin structure according to claim 1, wherein the arrangement density of the fiber bundles A on the fiber substrate is 4 to 10 pieces / 25 mm.   The method for producing a fiber-reinforced resin structure according to claim 1 or 2, wherein each of the fiber bundles A is a bundle of a plurality of fiber bundles AA.   Between the fiber bundles A, a fiber bundle B which is arranged in parallel with the fiber bundle A and has a fineness smaller than the fineness of the fiber bundle A is further arranged, and the fiber bundle B and the fiber base material The manufacturing method of the fiber reinforced resin structure in any one of Claims 1-3 stitched together by the sewing thread.   The manufacturing method of the fiber reinforced resin structure in any one of Claims 1-4 in which the said fiber bundle A and the said fiber base material are stitched together by the tricot knitting by the said sewing thread in the said composite base material.   The fiber reinforced resin structure according to any one of claims 1 to 5, wherein the fiber base is formed from a plurality of fiber bundles C arranged in a direction intersecting with the fiber bundle A and parallel to each other. Manufacturing method.   The manufacturing method of the fiber reinforced resin structure in any one of Claims 1-6 which arrange | positions the said composite base material in multiple steps in the process of arrange | positioning a composite base material in a shaping | molding die.   The method for producing a fiber-reinforced resin structure according to any one of claims 1 to 7, wherein one of the molds is a mold and the other is a mold or a film. A fiber base material, a plurality of fiber bundles A arranged in parallel to each other on the fiber base material, and a sewing thread, wherein the sewing thread stitches the fiber base material and the plurality of fiber bundles A;
The fineness of the fiber bundle A is 500 to 5000 tex, the arrangement density of the fiber bundle A on the fiber base material is 4 to 10 pieces / 25 mm,
The fiber base material is a composite base material formed from a plurality of fiber bundles C arranged in a direction intersecting with the fiber bundle A and parallel to each other.   The composite base material according to claim 9, wherein the fiber bundle A and the fiber base material are stitched together by tricot knitting using the sewing thread. The fiber reinforced resin structure containing the composite base material of Claim 9 or 10, and the resin which the said composite base material was impregnated.

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