JP6368228B2 - Fabric-reinforced resin molded body manufacturing method and fabric-reinforced resin molded body - Google Patents

Description

  The present invention relates to a method for producing a fabric-reinforced resin molded body and a fabric-reinforced resin molded body. More specifically, the present invention relates to a method of manufacturing a resin molded body using a fabric such as a woven fabric, a knitted fabric, and a nonwoven fabric as a reinforcing material, and a resin molded body manufactured by this method.

  In recent years, resin molded products are frequently used in various fields and applications. For example, resin suits are frequently used for travel suitcases and the like for reasons such as light weight. On the other hand, resin suitcases are handled as cargo when checked in as baggage when boarding an airplane, and may be damaged, cracked, broken, or perforated during transportation. Conventionally, fiber reinforced plastics (FRP) are used for such resin molded bodies that require high strength.

  In addition, a fabric reinforced resin molded body using a fabric as a reinforcing material has been proposed (see Patent Documents 1 and 2). For example, Patent Documents 1 and 2 disclose resin molded bodies obtained by compression molding by impregnating a woven sheet obtained by plain weaving of carbon fiber or aramid fiber with a thermosetting epoxy resin.

Japanese Patent Laid-Open No. 5-208471 JP 2009-184239 A

  However, a resin molded body using fiber reinforced plastic is liable to be warped after heat molding and has a problem in shape retention. The problem of “warping” after molding is particularly remarkable when deep drawing is performed. In addition to the above-described shape retention, the fabric reinforced resin molded article using the woven fabric sheet described in Patent Documents 1 and 2 has a problem that the manufacturing cost increases because the reinforcing material is expensive. is there.

  Accordingly, the main object of the present invention is to provide a method for producing a fabric-reinforced resin molded body and a fabric-reinforced resin molded body in which warpage hardly occurs after molding.

  In fiber reinforced plastics, the fiber that is the reinforcing material is partially stretched during thermoforming, but the partial stretching strain applied to the reinforcing fiber is relaxed after molding, and the molded body warps. Conceivable. Therefore, the present inventor has conducted earnest experimental studies on the reinforcing material and the forming method, and by using a fabric formed by using the reinforcing fiber and the predetermined binder fiber, by using a specific method, The present inventors have found that a fabric-reinforced resin molded body that does not occur can be obtained, and have reached the present invention.

That is, in the present invention, first, heating is performed by heating a fabric formed using a reinforcing fiber and a binder fiber having a melting point lower than that of the reinforcing fiber and capable of adhering the reinforcing fiber, or a sheet material using the fabric. Process,
A molding step in which the fabric or the sheet material heated in the heating step is compression-molded or vacuum-molded in a cold state using a mold;
The manufacturing method of the fabric reinforced resin molding which has this.
In the heating step, heating can be performed at a temperature equal to or higher than the melting point of the binder fiber and lower than the melting point of the reinforcing fiber.
The binder fiber that can be used in the production method according to the present invention is not particularly limited as long as the effects of the present invention are not impaired, but a polyolefin resin having a melting point of 130 ° C. or lower can be used.
The reinforcing fiber that can be used in the production method according to the present invention is not particularly limited as long as the effects of the present invention are not impaired, but a crystalline thermoplastic resin having a melting point higher than that of the binder fiber by 20 ° C. or more can be used. . Further, as the reinforcing fiber, a reinforcing fiber having a tensile Young's modulus at 120 ° C. of 7 cN / dtex or more can be used.
In the manufacturing method according to the present invention, as the sheet material, a plurality of the fabrics are laminated and thermocompression bonded at a temperature at which the binder fibers are melted, or one or more of the fabrics and the same kind as the binder fibers It is possible to use a laminate obtained by laminating a resin sheet made of the above resin and thermocompression bonding at a temperature at which the binder fiber melts.
In the manufacturing method according to the present invention, a plain woven fabric can be used as the fabric.

  In the present invention, next, a reinforcing fiber having a crystallinity of the reinforcing fiber of 70% or more measured by a calorimetric method using a differential scanning calorimeter at a heating rate of 30 ° C./min, and the reinforcing fiber After heating the fabric formed by mixing the binder fiber having a lower melting point and capable of adhering the reinforcing fiber, or a sheet material using the fabric, using a mold, cold, A fabric-reinforced resin molded body obtained by compression molding or vacuum molding is provided.

Here, technical terms used in the present invention are defined.
“Fabric” is a concept that includes all fabrics formed using fibers such as woven fabrics, knitted fabrics, and non-woven fabrics.
The “fabric reinforced resin molded product” refers to a resin molded product reinforced by all the fabrics included in the fabric.

  ADVANTAGE OF THE INVENTION According to this invention, the fabric reinforcement | strengthening resin molding which does not generate | occur | produce a curvature after shaping | molding can be manufactured by using the fabric formed by mixing a reinforcing fiber and the binder fiber which adhere | attaches this reinforcing fiber.

It is a flowchart figure which shows the manufacturing method of the fabric reinforcement | strengthening resin molding of embodiment of this invention. AC is a schematic diagram which shows the manufacturing method of the fabric reinforced resin molding shown in FIG. 1 in order of the process. It is a perspective view which shows typically an example of the fabric 11 (plain woven fabric) using the reinforcement fiber and the binder fiber. It is a cross-sectional schematic diagram which shows typically an example of the fabric 11 using the reinforcing fiber 1 and the binder fiber 2. FIG. It is a cross-sectional schematic diagram which shows typically an example of fabric reinforcement resin. It is a perspective view which shows the structural example of the fabric reinforcement | strengthening resin molding 20 of embodiment of this invention. A and B are schematic views showing a method for evaluating warpage.

  DESCRIPTION OF EMBODIMENTS Hereinafter, preferred embodiments for carrying out the present invention will be described in detail with reference to the drawings. In addition, embodiment described below shows an example of typical embodiment of this invention, and, thereby, the range of this invention is not interpreted narrowly.

<Method for producing fabric-reinforced resin molded article>
FIG. 1 is a flowchart showing a method for manufacturing a fabric reinforced resin molded body according to an embodiment of the present invention, and FIGS. 2A to 2C are schematic views showing the method for manufacturing the fabric reinforced resin molded body shown in FIG. is there. As shown in FIG.1 and FIG.2, in the manufacturing method of the fabric reinforcement | strengthening resin molding of this embodiment (henceforth only a resin molding), the fiber for binder and the binder fiber which adhere | attaches this reinforcement fiber are mixed and mixed. The process of heating the fabric 11 or the sheet material 12 formed in this way (heating process S1) and the process of molding the heated fabric 11 or the sheet material 12 (molding process S2) are performed.

(1) Material The reinforcing fiber used in the method for producing a resin molded body according to the present invention and the binder yarn to which the reinforcing fiber is bonded can be formed by melt spinning or the like.

[Reinforcing fiber]
In the present invention, the reinforcing fiber functions as a reinforcing material in the molded body. The type of the reinforcing fiber that can be used in the present invention is not particularly limited, but it is preferable to use a crystalline resin. By using a crystalline resin, the reinforcing effect in the molded body can be improved.

  Moreover, it is necessary not to melt even in the state of the molded body from the time of fiber production. Specifically, it is preferable to use a crystalline thermoplastic resin having a melting point higher than that of the binder fiber by 20 ° C. or more for the reinforcing fiber. Examples of the reinforcing fiber that satisfies such conditions include isotactic polypropylene (i-PP) and polyethylene terephthalate (PET).

  Here, the drawing conditions of the reinforcing fiber are not particularly limited, but the drawing temperature is preferably set to 145 ° C. or more from the viewpoint of improving the fiber properties. On the other hand, the draw ratio is preferably higher from the viewpoint of increasing the crystallinity of the reinforcing fiber, but if the draw ratio is too high, the crystal orientation is disturbed and the crystallinity is lowered. Therefore, in order to increase the crystallinity of the reinforcing fiber, it is desirable to draw in multiple stages rather than one stage. When stretching in one stage, since a large stretch ratio is applied at a stretch, stretching is started before the material to be stretched enters the heating tank, and particularly neck (necking) stretching is started extremely, and as a result, oriented crystals are hardly formed. It is to become.

  For example, when the reinforcing fiber is formed by two-stage stretching, it is preferable to perform the first stage with warm water and the second stage in highly saturated steam. In that case, from the viewpoint of improving the crystallinity of the reinforcing fiber, it is preferable to set the draw ratio of the second stage to 1.5 to 2.5 times. When the draw ratio of the second stage is less than 1.5 times, the oriented crystal formed in the first stage may be disturbed and the crystallinity may be lowered. On the other hand, when the draw ratio at the second stage exceeds 2.5, thread breakage may occur or the oriented crystal may be broken and the crystallinity may be lowered.

  In addition, the stretch ratio in the first stage in the case where the reinforcing fiber is formed by two-stage stretching is not particularly limited, but may be, for example, 4.0 to 10.0 times. Further, the stretching of the reinforcing fiber is not limited to two steps, and may be performed in three or more steps.

  The reinforcing fiber used in the production method according to the present invention uses a differential scanning calorimeter, has a rate of temperature increase of 30 ° C./min, and has a crystallinity of 60% or more measured by the calorific value method. When the crystallinity of the reinforcing fiber is less than 60%, distortion occurs during molding, and the molded body warps. On the other hand, by setting the crystallinity of the reinforcing fiber to 70% or more, it is possible to reduce distortion generated during molding and to produce a resin molded body without warping.

  The crystallinity of the reinforcing fiber defined here is a value calculated from the heat of fusion of the reinforcing fiber measured using a differential scanning calorimeter (DSC). In calculating the degree of crystallinity, the literature value of heat of fusion (209 J / g, temperature rising rate 10 ° C./min) in the complete crystal of the resin constituting the reinforcing fiber was set to 100% crystallinity. The measurement amount of the reinforcing fiber was about 10 mg, and the temperature was scanned from room temperature to a temperature 30 to 40 ° C. higher than the melting point of the reinforcing fiber at a temperature rising rate of 30 ° C./min.

  When the melting point of a resin is measured using DSC, the rate of temperature increase is generally set to 10 ° C./min. However, the amount of heat of fusion of oriented crystallization such as a stretched product is measured, and the fiber is measured. When obtaining the difference in the degree of crystallinity, if the rate of temperature rise is slow, crystallization proceeds during temperature rise, and the amount of heat of fusion in a state different from that before measurement is measured. Therefore, in this embodiment, the crystallinity of the reinforcing fiber is defined by a value measured at a rate of temperature increase of 30 ° C./min.

  Furthermore, the reinforcing fiber used in the method for producing a resin molded body according to the present invention preferably has a tensile Young's modulus at 120 ° C. of 7 cN / dtex or more. Thereby, the distortion which generate | occur | produces at the time of shaping | molding can be made small.

  The surface of the reinforcing fiber can be subjected to a surface treatment so as to have a functional group. The surface treatment method is not particularly limited, and a known surface treatment method such as electrolytic treatment or sizing agent treatment can be freely selected and used. In the present invention, in particular, when surface treatment is performed, it is preferable to select a surface treatment using a sizing agent, and it is more preferable to use a sizing agent containing a coupling agent.

  When the sizing agent containing a coupling agent is used, the type of coupling agent to be used is not limited, and a known coupling agent can be freely selected and used as long as the effects of the present invention are not impaired. For example, silane coupling agents such as aminosilane and epoxysilane; titanium coupling agents and the like can be mentioned. Moreover, if the thing containing a resin emulsion other than a coupling agent is used as a sizing agent, handling can be facilitated.

  Thus, when the surface-treated reinforcing fiber is used, an adhesive property with the binder fiber is imparted, and a molded article having good strength and appearance can be obtained.

[Binder fiber]
In the present invention, the binder fiber is a fiber having a melting point lower than that of the reinforcing fiber and capable of bonding the reinforcing fiber. The type of the reinforcing fiber that can be used in the present invention is not particularly limited, but it is preferable to use a polyolefin-based resin having a melting point of 130 ° C. or lower from the viewpoint of being economical in terms of thermal efficiency and capable of being molded at a relatively low temperature.

  More specifically, the binder fibers include low density polyethylene, linear low density polyethylene, high density polyethylene and ethylene resins such as ethylene vinyl acetate, binary systems of α-olefins such as ethylene and butene and propylene, or Random or block copolymerized polypropylene, which is a ternary copolymer, can be used. Among these polyolefin-based resins, low-density polyethylene, linear low-density polyethylene, and high-density polyethylene are preferable because they have a clear melting point and show a sharp melting behavior with respect to temperature.

[Mixed fiber]
In the method for producing a resin molded body according to the present invention, a mixed fiber using the reinforcing fiber and the bondable binder fiber can be used. The mixed fiber can be obtained by mixing the reinforcing fiber and the binder fiber with known air.

[Fabric 11 and sheet material 12]
The fabric used in the method for producing a resin molded body according to the present invention can be produced using the above-described combingle fibers of reinforcing fibers and binder fibers, and is, for example, a woven fabric, a knitted fabric, or a nonwoven fabric. Moreover, it is also possible to use what combined the above-mentioned reinforcing fiber and binder fiber instead of using the Comingle fiber. Furthermore, the fabric used in the present invention only needs to use the above-described reinforcing fiber and binder fiber, and may be mixed with other different fiber types.

  FIG. 3 is a perspective view schematically showing a plain woven fabric which is an example of the fabric. The structure of the fabric 11 is not particularly limited, and can be appropriately selected according to applications such as a plain weave, a satin weave, and a deformed structure of these original structures other than the plain weave shown in FIG. Moreover, the manufacturing method of a fabric is not specifically limited, either, A well-known method can be applied.

  Furthermore, in the method for producing a resin molded body of the present embodiment, the above-described fabric can be used alone, but a sheet material obtained by laminating a plurality of fabrics and thermocompression bonding at a temperature at which the binder fiber melts, Alternatively, it is preferable to use a sheet material obtained by laminating two or more fabrics and a resin sheet made of the same kind of resin as the binder fiber and thermocompression bonding at a temperature at which the binder fiber melts.

  Thus, by thermocompression-bonding the fabric into a sheet, the crystallinity of the reinforcing fibers can be increased, and the operability in the heating step S1 and the molding step S2 can be improved. In addition, the sheet material in which the resin sheet is laminated on the fabric can reduce the moisture permeability and air permeability that are the characteristics of the fabric, so that it can be applied to applications that dislike water permeability such as home appliances, and vacuum forming methods. Can also be applied.

  In addition, in the manufacturing method of the resin molding which concerns on this invention, even if the film which consists of polyolefin, polyester, or ABS (acrylonitrile butadiene styrene copolymer) resin is bonded together to the single side | surface or both surfaces of the fabric or sheet material mentioned above. Good. Thereby, it becomes possible to color the surface of a resin molding or to give design properties, such as a pattern.

  The weight ratio between the reinforcing fiber and the binder fiber used for the fabric can be freely set according to the use of the molded article to be produced. In the present invention, it is preferable to use reinforcing fibers at a weight ratio of 1 to 4 with respect to the binder fiber 1. By using a reinforcing fiber in a weight ratio of 1 or more with respect to the binder fiber 1, the strength of the molded body can be improved, and by reducing the reinforcing fiber to a weight ratio of 4 or less, the strength is reduced due to insufficient adhesion between the reinforcing fibers. Can be prevented.

[Heating step S1]
As shown in FIGS. 2A and 2B, in the heating step S <b> 1, the fabric 11 or the sheet material 12 using the fabric is heated after being cut or laminated as necessary. At that time, the heating method is not particularly limited, and a known heating device such as an oven or a hot plate can be used. Moreover, you may heat the fabric 11 or the sheet | seat material 12 in the state clamped with the metal plate etc. as needed. Thereby, thermal contraction can be prevented.

  The heating temperature of the fabric 11 or the sheet material 12 is preferably set to a temperature not lower than the melting point of the binder fiber and lower than the melting point of the reinforcing fiber. Thereby, a fabric reinforced resin molded article having good shape retention (shape retention) can be obtained.

  FIG. 4 is a schematic cross-sectional view schematically showing an example of the fabric 11 using the reinforcing fiber 1 and the binder fiber 2. When the fabric 11 is heated at a temperature higher than the melting point of the binder fiber 2 and lower than the melting point of the reinforcing fiber 1, only the binder fiber 2 is melted and fused and integrated into the binder fiber 2 as shown in FIG. A fabric-reinforced resin having a sea-island structure in which the reinforcing fibers 1 exist in an island shape is obtained. Here, “sea-island structure” refers to a phase separation structure in a polymer blend, for example, an interconnected type in which island components are interconnected or a layered structure in which sea components and island components are distributed in the thickness direction. Including.

[Molding step S2]
FIG. 6 is a perspective view showing a configuration example of a fabric reinforced resin molded body manufactured by the method of the present embodiment. As shown in FIG. 2C, the fabric 11 or the sheet material 12 heated in the heating step S1 described above is compression-molded or vacuum-molded using the molds 13a and 13b while being cold. Thereby, for example, substantially box-shaped bodies such as the deep-drawn molded body 20 shown in FIG. 6 can be manufactured, and fabric-reinforced resin molded bodies having various shapes can be manufactured.

  The conditions at the time of compression molding and vacuum molding are not particularly limited. For example, the pressure is 1 to 5 MPa, the temperature of the fabric 11 or the sheet material 12 is 120 to 150 ° C., and the cooling time is 30 to 60 seconds. To do. In addition, in the manufacturing method of the resin molding of this embodiment, although it shape | molds in cold, this is in order to manufacture efficiently the fabric reinforcement | strengthening resin molding with favorable shape retainability (shape retention). It is.

  As described above in detail, in the method for producing a resin molded body of this embodiment, since a fabric using multifilaments having two or more different melting points is used, a resin is applied to a woven fabric using carbon fibers or aramid fibers. Compared to the impregnated composite sheet, a resin molded body in which the reinforcing fibers and the binder fibers are integrated with no gap is obtained. Thereby, the intensity | strength of a molded object can be raised.

  Further, in the method for producing a resin molded body of the present embodiment, after pre-heating at a temperature lower than the melting point of the reinforcing fiber, cold forming is performed, so that each fiber constituting the fabric is distorted. Can be prevented. As a result, the shape retention of the molded body can be improved. The method for producing a resin molded body according to the present embodiment is suitable for producing a resin molded body using a woven fabric, a knitted fabric, and a nonwoven fabric, but is particularly effective when a woven fabric having poor stretchability is used as a reinforcing material.

  Hereinafter, the present invention will be described in more detail based on examples. In addition, the Example demonstrated below shows an example of the typical Example of this invention, and, thereby, the range of this invention is not interpreted narrowly.

  In this example, a resin molded body was produced using a plain woven fabric formed by reinforcing fibers and binder fibers produced by the following method and conditions, and the performance was evaluated.

<Reinforcing fiber A>
Isotactic polypropylene (i-PP) [melt flow rate (MFR) = 18 g / 10 min (230 ° C., 21.18 N), melting point = 165 ° C.] was used. Spinning these materials using a spinning nozzle with holes with 240 holes at a spinning temperature of 240 ° C. while measuring the amount of discharged resin with a molten resin gear pump attached to the spinning nozzle head. Spinning was performed at a speed of 60 m / min to produce a single spun fiber having a fineness of 16147 dtex.

Subsequently, in the resulting single spun fibers (240) a spin-draw method (spinning stretching direct method), the first draw roller (G1) = 60 m / min, the first elongated Shinso temperature = 95 ° C. (hot water) Second stretching roller (G2) speed = 405 m / min, second stretching tank temperature = 153 ° C. (high-pressure saturated steam), third stretching roller (G3) speed = 805 m / min, first stretching ratio (G2 / G1) The speed ratio was 6.75 times, the second stretch ratio (G3 / G2 speed ratio) was 1.99 times, and the total stretch ratio (G3 / G1 speed ratio) was 13.42 times. By this stretching step, PP single reinforcing fiber A was obtained.

  The physical properties of the stretched reinforcing fiber A were fineness = 1196 dtex, tensile Young's modulus = 93 cN / dtex (room temperature tensile test), and 13.2 cN / dtex (120 ° C. hot tensile test). Further, with respect to the obtained stretched composite fiber A, the heat of fusion was measured with a differential scanning calorimeter (DSC) under the condition of a heating rate of 30 ° C./min, and the heat of fusion of the complete crystal of the i-PP resin The crystallinity was calculated from the comparison of. As a result, the crystallinity was 72%. The orientation crystallinity after heat treatment at 120 ° C. was 65%.

<Reinforcing fiber B>
An ethylene-propylene random copolymer (co-PP) [melt flow rate (MFR) = 5 g / 10 min (230 ° C., 21.18 N), melting point = 145 ° C.] was used. Spinning these materials using a spinning nozzle with holes with 240 holes at a spinning temperature of 240 ° C. while measuring the amount of discharged resin with a molten resin gear pump attached to the spinning nozzle head. Spinning was performed at a speed of 60 m / min to produce a spun fiber having a fineness of 15795 dtex. Subsequently, in the resulting single spun fibers (240) a spin-draw method (spinning stretching direct method), the first draw roller (G1) = 60 m / min, the first elongated Shinso temperature = 95 ° C. (hot water) Second stretching roller (G2) speed = 405 m / min, second stretching tank temperature = 153 ° C. (high-pressure saturated steam), third stretching roller (G3) speed = 805 m / min, first stretching ratio (G2 / G1) The speed ratio was 6.75 times, the second stretch ratio (G3 / G2 speed ratio) was 1.99 times, and the total stretch ratio (G3 / G1 speed ratio) was 13.42 times. By this stretching step, co-PP single reinforcing fiber B was obtained.

  The physical properties of the stretched reinforcing fiber B were fineness = 1225 dtex, tensile Young's modulus = 95 cN / dtex (room temperature tensile test), and 13.2 cN / dtex (120 ° C. hot tensile test). Further, with respect to the obtained stretched composite fiber B, the heat of fusion was measured with a differential scanning calorimeter (DSC) under the condition of a heating rate of 30 ° C./min, and the heat of fusion of the complete crystal of the co-PP resin The crystallinity was calculated from the comparison of. As a result, the crystallinity was 71%. The orientation crystallinity after heat treatment at 120 ° C. was 63%.

<Reinforcing fiber C>
PET fiber [IV = 0.65] was used. Spinning these materials using a spinning nozzle with a hole number of 240 holes at a spinning temperature of 280 ° C. while measuring the amount of discharged resin with a molten resin gear pump attached to the spinning nozzle head. Spinning was performed at a speed of 60 m / min to produce a spun fiber having a fineness of 23400 dtex. Subsequently, in the resulting single spun fibers (240) a spin-draw method (spinning stretching direct method), the first draw roller (G1) = 60 m / min, the first elongated Shinso temperature = 95 ° C. (hot water) Second stretching roller (G2) speed = 405 m / min, second stretching tank temperature = 193 ° C. (hot air tank temperature), third stretching roller (G3) speed = 805 m / min, and the first stretching ratio (G2 / G1) The speed ratio was 6.75 times, the second stretch ratio (G3 / G2 speed ratio) was 1.99 times, and the total stretch ratio (G3 / G1 speed ratio) was 13.42 times. Through this stretching process, a single PET reinforcing fiber C was obtained.

  The properties of the stretched reinforcing fiber C were fineness = 1755 dtex, tensile Young's modulus = 114 cN / dtex (room temperature tensile test), and 7.8 cN / dtex (120 ° C. hot tensile test). Further, with respect to the obtained stretched composite fiber C, the degree of crystallinity is calculated from the contrast with the heat of fusion of the complete crystal of the PET resin by a differential scanning calorimeter (DSC) under the condition of a heating rate of 30 ° C./min. did. As a result, the crystallinity was 75%. The degree of oriented crystallinity after treatment at 120 ° C. was 75%.

<Reinforcing fiber D>
Four commercially available Dyneema (registered trademark, 275T192, type SK71) manufactured by Toyobo Co., Ltd. were combined to obtain a reinforcing fiber D.

  The physical properties of the stretched reinforcing fiber D were fineness = 1100 dtex, tensile Young's modulus = 1250 cN / dtex (room temperature tensile test), and 36.0 cN / dtex (120 ° C. hot tensile test). In addition, with respect to the obtained stretched composite fiber D, the degree of crystallinity is calculated from the contrast with the heat of fusion of the complete crystal of HDPE resin using a differential scanning calorimeter (DSC) at a temperature rising rate of 30 ° C./min. did. As a result, the crystallinity was 95%. The orientation crystallinity after heat treatment at 120 ° C. was 92%.

<Binder fiber α>
LLDPE (Linear Low Density Polyethylene) [melt flow rate (MFR) = 8 g / 10 min (230 ° C., 21.18 N), melting point = 125 ° C.] was used. Using a spinning nozzle having a hole with 240 holes, the spinning speed of this material is measured at a spinning temperature of 210 ° C. while measuring a predetermined amount of discharged resin with a molten resin gear pump attached to the spinning nozzle head. Spinning was performed at 60 m / min to produce a spun fiber having a fineness of 8395 dtex. Subsequently, in the resulting single spun fibers (240) a spin-draw method (spinning stretching direct method), the first draw roller (G1) = 60 m / min, the first elongated Shinso temperature = 95 ° C. (hot water) Second stretching roller (G2) speed = 405 m / min, second stretching tank temperature = normal temperature, third stretching roller (G3) speed = 407, first stretching ratio (G2 / G1 speed ratio) = 6.75 times The film was stretched under the conditions of the second stretch ratio (G3 / G2 speed ratio) = 1.0 times stretch ratio and the total stretch ratio (G3 / G1 speed ratio) = 6.78 times. Through this stretching process, LLDPE single fiber α was obtained.

<Binder fiber β>
HDPE (High Density Polyethylene) [Melt Flow Rate (MFR) = 8 g / 10 min (230 ° C., 21.18 N), melting point = 134 ° C.] was used except that HDPE was used in the same manner as the binder fiber α. Fiber β was obtained.

  Regarding these reinforcing fibers A to D and binder fibers α and β, the production conditions and fiber properties other than the above are summarized in Table 1 below.

The “tensile strength” shown in Table 1 is a value measured by the following method.
(1) Room temperature According to the method specified in JIS L1013, using an autograph AG-100kN IS manufactured by Shimadzu Corporation under the conditions of a sample length of 100 mm and a tensile speed of 100 mm / min, 5 times per sample Measurements were made. And the intensity | strength (cN / dtex), elongation (%), and Young's modulus (cN / dtex) were calculated | required from the average value.

(2) 120 ° C
After adjusting for 1 hour in a 120 ° C atmosphere using a heating furnace, set the sample, and after 3 minutes (the temperature of the sample reaches 120 ° C after about 2 minutes), follow the method specified in JIS L1013. Accordingly, measurement was performed 5 times per sample using Autograph AG-100kN IS manufactured by Shimadzu Corporation under the conditions of a sample length of 100 mm and a pulling speed of 100 mm / min. And the intensity | strength (cN / dtex), elongation (%), and Young's modulus (cN / dtex) were calculated | required from the average value.

[Example 1]
(1) Fabric production Fabricated plain woven fabric by combining 2 composite reinforcing fibers A and 2 binder fibers α into 1824 dtex and using a loom to set the original yarn density in the vertical and horizontal directions to 8.33 yarns / 25 mm respectively. did. The surface density of the obtained woven fabric was 122 g / m ² .

(2) Production of sheet material The obtained plain woven fabric was cut into a size of 1.5 m in length and width, and three of these were laminated and heated using a hot plate (2 m in length x 2 m in width) with a hot press machine. A thermocompression fabric sheet was prepared. As a preparation for preparing a sheet, an aluminum plate having a length and width of 1.8 m and a thickness of 1.5 mm was preheated to a predetermined temperature with a hot press machine in advance. Then, the above-described plain woven fabric was placed on the aluminum plate and thermocompression bonded under predetermined conditions. After releasing the press pressure, the entire aluminum plate was taken out, and a separately prepared aluminum plate for cooling was placed on the plate to quench the sheet, and then only the sheet was removed to prepare a thermocompression fabric sheet. At that time, the hot press conditions were a flat plate temperature of 120 ° C., a pressure of 1.6 MPa, and a pressure holding time of 45 seconds. The obtained thermocompression bonded fabric sheet had a thickness of 1.1 mm and an area density of 341 g / m ² .

(3) Compression molding test In the compression molding test, a male mold having a convex shape having a vertical length of 500 mm, a horizontal length of 700 mm, a height of 120 mm, a top end curvature R80 mm, and a bottom end curvature R10 mm was used. On the other hand, as the female mold, a mold having a concave shape corresponding to the male mold was used, and the male and female molds were mounted on a press machine and used for the compression molding test. Each mold was used in such a state that the mold temperature could be maintained in the range of 30 ° C. to 70 ° C. by passing cold water or hot water through the in-mold water cooling tube.

  The upper and lower surfaces of the fabric sheet obtained above were preheated with a far-infrared (IR) heater until the surface temperature became 120 ° C to 130 ° C. After reaching the predetermined temperature, the fabric sheet was quickly inserted into the compression test mold, compression molding was performed for 4 seconds with the clearance between the male and female molds being 1 mm, and then cold molding was maintained for 60 seconds. After the cold forming was completed, the mold was removed to obtain a box-shaped formed body.

  Next, the box-shaped molded body was allowed to stand at room temperature for 24 hours and then visually observed for shapes such as warpage and deformation, and the degree of warpage of the side wall surface with respect to the bottom surface was measured as a warpage angle α (°). 7A and 7B are schematic views showing a method for evaluating warpage. As shown in FIG. 7A, the warp angle α (°) is α = 0 ° when the angle θ formed by the bottom portion and the side wall portion of the box-shaped molded body is 90 °, and the side wall portion is inward as shown in FIG. 7B. The case of warping was determined as + θ °, and the case of warping to the bottom side was determined as −θ °. As a result, warpage and deformation were not recognized in the obtained box-shaped molded article, and the warp angle α was 0 °, which was good moldability.

[Example 2]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the reinforcing fiber B was used as the reinforcing fiber. The obtained thermocompression bonding fabric sheet had a thickness of 1.1 mm and an area density of 335 g / m ² .

  Next, the thermocompression-bonded fabric sheet obtained above was placed so that the surface on the woven fabric side was in contact with the male side of the mold, and a compression molding test was performed under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 3]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the reinforcing fiber C was used as the reinforcing fiber and the weight ratio of the reinforcing fiber to the binder fiber was 75:25. The obtained thermocompression bonded fabric sheet had a thickness of 1.1 mm and a surface density of 441 g / m ² .

  Next, the thermocompression-bonded fabric sheet obtained above was placed so that the surface on the woven fabric side was in contact with the male side of the mold, and a compression molding test was performed under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 4]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the reinforcing fiber D was used as the reinforcing fiber. The obtained thermocompression bonded fabric sheet had a thickness of 1.3 mm and an areal density of 334 g / m ² .

  Next, the thermocompression-bonded fabric sheet obtained above was placed so that the surface on the woven fabric side was in contact with the male side of the mold, and a compression molding test was performed under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 5]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the weight ratio of the reinforcing fibers to the binder fibers was 80:20. The obtained thermocompression bonded fabric sheet had a thickness of 1.4 mm and an areal density of 582 g / m ² .

  Next, a compression molding test was performed using the thermocompression bonded fabric sheet obtained above under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 6]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 5 except that the weight ratio of the reinforcing fibers and the binder fibers was 50:50. The obtained thermocompression bonded fabric sheet had a thickness of 1.3 mm and an areal density of 485 g / m ² .

  Next, a compression molding test was performed using the thermocompression bonded fabric sheet obtained above under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 7]
Made of LLDPE resin with a surface density of 200 g / m ² [melt flow rate (MF
R) = 8 g / 10 min (190 ° C., 21.18 N), melting point = 117 ° C.] A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the sheet was laminated on one side. . The obtained thermocompression bonded fabric sheet had a thickness of 1.3 mm and an areal density of 525 g / m ² .

  Next, the thermocompression-bonded fabric sheet obtained above was placed so that the surface on the woven fabric side was in contact with the male side of the mold, and a compression molding test was performed under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, no warpage or deformation was observed in the box-shaped molded body, and the warp angle α was 0 °, indicating good moldability.

[Example 8]
A thermocompression bonded fabric sheet was produced by the same method and conditions as in Example 1 except that the reinforcing fiber B was used as the reinforcing fiber, β was used as the binder fiber, and the pressing temperature was 138 ° C. The obtained thermocompression bonded fabric sheet had a thickness of 1.1 mm and an area density of 340 g / m ² .

  Next, the thermocompression-bonded fabric sheet obtained above was placed so that the surface on the woven fabric side was in contact with the male side of the mold, and a compression molding test was performed under the same method and conditions as in Example 1. As a result, in the visual observation after standing at room temperature for 24 hours, the box-shaped molded body was not warped or deformed much, but there were portions where the reinforcing fibers could not withstand the heat partially, and the angle α Warped by 2 °. Moreover, although the moldability was not good, it could be molded.

[Comparative Example 1]
A plain woven fabric was prepared in the same manner and under the same conditions as in Example 1 except that two reinforcing fibers A were combined to obtain 2392 dtex. The surface density of the obtained woven fabric was 157 g / m ² . Next, using this woven fabric, a thermocompression bonded fabric sheet was produced under the same method and conditions as in Example 1, but no thermocompression bonded sheet was obtained.

  The above results are summarized in Table 2 below.

  The box-shaped molded articles using the thermocompression bonded fabric sheets of Examples 1 to 7 shown in Table 2 were free from warpage and excellent in moldability. From this result, according to the present invention, it was confirmed that a fabric-reinforced resin molded body that hardly warps after molding can be produced.

  In addition, from the results of Example 8, it was found that even when the melting points of the reinforcing fiber and the binder fiber are close to each other, a fabric-reinforced resin molded body with less warpage can be produced by devising the pressing temperature and the like. However, it has been found that it is preferable to use a reinforcing fiber having a melting point 20 ° C. higher than the melting point of the binder fiber in order to reduce the occurrence of warpage and improve the moldability.

11 Fabric 12 Sheet material 13a, 13b Mold 1 Reinforcing fiber 2 Binder fiber 20 Resin molding

Claims (7)

Fabric formed using a reinforcing fiber having a tensile Young's modulus at 120 ° C. of 7 cN / dtex or more and a binder fiber having a melting point lower than that of the reinforcing fiber and capable of adhering the reinforcing fiber, or a sheet using the fabric A heating process for heating the material;
A molding step in which the fabric or the sheet material heated in the heating step is compression-molded or vacuum-molded in a cold state using a mold;
The manufacturing method of the fabric reinforcement | strengthening resin molding which has this.   The method for producing a fabric-reinforced resin molded article according to claim 1, wherein in the heating step, heating is performed at a temperature equal to or higher than the melting point of the binder fiber and lower than the melting point of the reinforcing fiber. The binder fiber is a polyolefin resin having a melting point of 130 ° C. or less,
The method for producing a fabric-reinforced resin molded article according to claim 1 or 2, wherein the reinforcing fiber is a crystalline thermoplastic resin having a melting point higher by 20 ° C or more than the binder fiber. The said sheet | seat material is a manufacturing method of the fabric reinforcement | strengthening resin molding as described in any one of Claim 1 to 3 which laminates | stacks the said multiple sheets of fabric and thermocompression-bonded at the temperature which the said binder fiber fuse | melts. The sheet material 1 or the two or more of said fabric, said binder consists of fibers of the same type as the resin and resin sheet are laminated, claims 1-3 wherein the binder fiber is obtained by thermocompression bonding at a temperature of melting The manufacturing method of the fabric reinforced resin molding as described in any one of these. The method for producing a fabric-reinforced resin molded body according to any one of claims 1 to 5 , wherein the fabric is a plain woven fabric. A fabric formed by mixing a reinforcing fiber and a binder fiber having a melting point lower than that of the reinforcing fiber and capable of adhering the reinforcing fiber, or using the fabric ,
The reinforcing fiber is
A differential scanning calorimeter was used and the heating rate was 30 ° C / min.
The crystallinity of the strong fiber is 70% or more, and
The tensile Young's modulus at 120 ° C. is 7 cN / dtex or more.
Fabric reinforced resin molding.