Patent Application
20130280479
This disclosure relates to a carbon-fiber-reinforced plastic molded article and, specifically, to a carbon-fiber-reinforced plastic molded article in which carbon fibers are uniformly arranged at the design surface and which has an excellent appearance design property.
In a conventional carbon-fiber-reinforced plastic molded article, for example, when being molded after stacking unidirectional carbon fiber prepregs, even if the used prepreg is prepared by arranging carbon fiber bundles in one direction, a fluctuation of partial positions of carbon fiber bundles or a torsion of a part which is formed by partial joining of single fibers of carbon fibers in carbon fiber bundles, exists on the surface and, when formed into the molded article, the design property of the molded article is poor from the viewpoint of uniformity of appearance quality. Disturbances in fiber arrangement such as the fluctuation and the torsion vary in how they are seen depending upon the incident angle of light illuminated to the surface of the molded article. They give a discomfort to the appearance quality and they are called “visual irritation,” “glistening,” “fluctuation” and the like and they have been shunned.
To avoid such so-called “appearance irregularities,” painting and the like has been performed. But, because the weight increases and, in addition, the design property of carbon fibers cannot be exhibited, further improvement of design property is desired for the fields required to perform transparent or semitransparent painting to be able to recognize the interior state.
To prevent the properties and appearance of a molded article from being damaged, although a technology to optimize the property of curing or viscosity of epoxy resin composition used for a prepreg is known (for example, JP-A-2004-099814), a technology attempting to solve the problem of reduction of appearance quality ascribed to the above-described fluctuation in positions of carbon fiber bundles or disturbance in arrangement of carbon fibers on the design surface is not known. Further, although a manner of making the irregularities hard to be seen by concealing the surface by a glass scrim cloth is known (for example, US-A-2009-110872), its advantage is small and, to exhibit the design property of carbon fibers, improvement of the disturbance in arrangement and the like of carbon fibers themselves is necessary.
Accordingly, in particular, paying attention to the problem of reduction of appearance quality ascribed to fluctuation in positions of carbon fiber bundles or disturbance in arrangement of carbon fibers on a design surface of a molded article, it could be helpful to provide a carbon-fiber-reinforced plastic molded article in which carbon fibers are uniformly arranged at the design surface and which has an excellent appearance design property.
We provide a carbon-fiber-reinforced plastic molded article which includes a laminate with at least two layers including a unidirectionally continuous-carbon-fiber-reinforced sheet in which continuous carbon fiber bundles are arranged in a predetermined one direction, wherein, when carbon fibers of an outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming a design surface of the molded article are observed at the design surface, an area fraction of regions where a proportion of carbon fibers which are inclined at angles of 3° or more to the predetermined one direction is 0.5% or more is 20% or less relative to the whole area of the design surface.
We provide a carbon-fiber-reinforced plastic molded article which comprises a laminate with at least two layers including a unidirectionally continuous-carbon-fiber-reinforced sheet in which continuous carbon fiber bundles are arranged in a predetermined one direction characterized in that, when carbon fibers of an outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming a design surface of the molded article are observed at the design surface, an area fraction of regions where a proportion of carbon fibers which are inclined at angles of 3° or more to the predetermined one direction is 0.5% or more is 20% or less relative to the whole area of the design surface.
In the molded article comprising the laminate with two or more layers, in particular, paying attention to an outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article, the area fraction of regions where the proportion of carbon fibers on the design surface of the unidirectionally continuous-carbon-fiber-reinforced sheet, which are inclined at angles of 3° or more, is 0.5% or more is 20% or less. Namely, the regions, where the proportion of carbon fibers on the design surface which are inclined at angles of 3° or more is 0.5% or more, cause at a high possibility reduction of the appearance quality called “visual irritation” and the like ascribed to the disturbance in arrangement of carbon fibers as aforementioned, but the area fraction of such regions relative to the whole area of the design surface is suppressed to 20% or less. It is more preferred that the area fraction of such regions relative to the whole area of the design surface is 10% or less. Thus, by suppressing the area fraction of the regions causing the reduction of the appearance quality at a high possibility to be low, a good design surface can be ensured and a good appearance design property can be achieved as the whole of the molded article.
Further, in the carbon-fiber-reinforced plastic molded article, to achieve the above-described excellent design surface more securely, it is preferred that the fiber areal weight of the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article is 30 g/m2 or more and 100 g/m2 or less, and more preferably it is 40 g/m2 or more and 80 g/m2 or less. Thus, by controlling it at a low areal weight of 100 g/m2 or less, the carbon fibers are likely to be spread more uniformly, and an excellent design property of the molded article to be aimed can be achieved more easily. Further, by controlling the fiber areal weight at 30 g/m2 or more, when the carbon fibers are spread uniformly, the single fiber can easily maintain its straightness.
Further, in the carbon-fiber-reinforced plastic molded article, to achieve the above-described excellent design surface more securely, it is preferred that the resin content of the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article is 15 mass % or more and 50 mass % or less, and more preferably it is 20 mass % or more and 40 mass % or less. By controlling the resin content at 15 mass % or more, when the molded article is produced, the resin is liable to uniformly exist on the surface. From such a viewpoint, more preferably it is 20 mass % or more. Further, by controlling the resin content at 50 mass % or less, the arrangement of the fibers can be prevented from being disturbed by the flowability of the resin at the time of molding. From such a viewpoint, more preferably it is 40 mass % or less.
Further, in the carbon-fiber-reinforced plastic molded article, it is preferred that the fineness of one carbon fiber bundle in the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article is 300 tex or less. To achieve the above-described excellent design surface of the molded article, it is effective to apply a tension to the continuous carbon fiber bundles at a stage for producing a prepreg which forms the above-described outermost unidirectionally continuous-carbon-fiber-reinforced sheet part and, by this, it becomes possible to suppress the fluctuation in positions of the carbon fiber bundles and to suppress the disturbance in arrangement of the carbon fibers even at the stage of the prepreg. However, if the carbon fiber bundles are too thick, because there is a fear that such suppression effects become little, the fineness per one carbon fiber bundle is preferably controlled at 300 tex or less. Although the lower limit of the fineness per one carbon fiber bundle is not particularly restricted, about 90 tex or more is sufficient for production of a prepreg.
Further, in the carbon-fiber-reinforced plastic molded article, it is preferred that the tensile elastic modulus of a carbon fiber used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article is 270 GPa or more. Namely, as carbon fibers to be used, carbon fibers which can be easily arranged in the predetermined one direction when applied with a tension to make continuous carbon fiber bundles and each of which has a tensile elastic modulus of 270 GPa or more are used. By such a condition, in the process for producing a prepreg which forms the above-described outermost unidirectionally continuous-carbon-fiber-reinforced sheet part after molding, when a tension is applied to the continuous carbon fiber bundles as described above, the fluctuation in positions of carbon fiber bundles hardly occurs as well as the disturbance in arrangement of carbon fibers in the carbon fiber bundles hardly occurs. Maintaining such a condition a prepreg to form the outermost unidirectionally continuous-carbon-fiber-reinforced sheet part is made, and after laminating it as an outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of a molded article, the molded article is molded. Therefore, also in the design surface of the molded article which has been molded, a more excellent design surface, which is less in fluctuation in positions of carbon fiber bundles and which is suppressed to be small in disturbance in arrangement of carbon fibers, can be realized.
As the carbon fibers, although pitch group and polyacrylonitrile group carbon fibers can be used, polyacrylonitrile group carbon fibers are preferred because of the relatively high tensile strength. The tensile strength of the carbon fiber bundle is preferably 3,500 MPa or more, and more preferably 4,500 MPa or more. By selecting such a range, it becomes possible to lighten a composite to be obtained.
Hereinafter, the prepreg forming the unidirectionally continuous-carbon-fiber-reinforced sheet part will be explained in more detail.
In the carbon-fiber-reinforced plastic molded article, in the stage where a prepreg used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article, it is necessary to spread carbon fibers uniformly and, to spread them uniformly, it is preferred that the number of single fibers in a carbon fiber bundle is 15,000 or less. From such a viewpoint, although the number of single fibers is desired to be less, if the number of single fibers becomes smaller, to obtain a prepreg to be aimed, it becomes necessary to use a greater number of carbon fiber bundles and produce the prepreg by arranging the carbon fiber bundles with a uniform tension, and it is believed that such a condition increases industrial difficulty and, therefore, the number is preferably 500 or more in practice. Further preferably, the number is 1,000 or more and 7,000 or less.
As the resin component used for the prepreg employed for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface, both a thermosetting resin and a thermoplastic resin can be used. In the case of a thermosetting resin, it is excellent in stiffness and strength of molded article and, in the case of a thermoplastic resin, it is excellent in impact strength and recycling property of molded article. As such thermosetting resins, for example, unsaturated polyester, vinyl ester, epoxy, phenol, resol, urea-melamine, polyimide and the like, and copolymer or modified material thereof, and/or a resin blended with two or more thereof and the like can be used. Furthermore, to improve the impact resistance, an elastomer or a rubber component may be added to the above-described thermosetting resin.
Further, from the viewpoint that the carbon fibers in the prepreg used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface are spread uniformly, it is preferred to use a package wound with a carbon fiber bundle used as a raw material of the prepreg having a small yarn width relative to a target width per one carbon fiber bundle in the prepreg. Further, by a condition where a yarn having a too small yarn width is not used, the prepreg can be made without causing an irregularity at the time of spreading. The yarn width is more preferably 95% or less relative to the target width, and further preferably 90% or less, and preferably 25% or more, and more preferably 30% or more. The target width is referred to as a value dividing the whole width of the prepreg by the number of used carbon fiber bundles. By controlling this value at 90% or less, interference of yarns adjacent to each other can be suppressed even if the yarns are spread at the time of making the prepreg, the straightness of single fibers can be maintained and, therefore, a prepreg having uniform thickness and spreading property can be produced. The yarn width of the carbon fiber bundle can be achieved by adequately setting the fineness of carbon fibers, the number of the filaments, the process conditions on and after the surface treatment during production of carbon fibers, in particular, the winding condition, and selecting yarns within these conditions.
The process of producing the prepreg is not particularly restricted as long as it can give a tension to arrange yarns in one direction and it has a function for spreading the carbon fiber bundles before impregnation of resin. However, because there is a possibility to cause entanglement of single fibers in the carbon fiber bundles in an equipment such as one to spread the carbon fiber bundles by blowing compressed air, use of a spreading means due to rolls and the like is preferred.
Further, it is preferred that, with respect to the width of the carbon fiber sheet produced as described above, the total width of fiber bundles becomes 80-98% relative to the sheet width of the prepreg, preferably 85-95%, by applying a tension of 0.5-6 cN/tex, preferably 1.5-3 cN/tex, to each carbon fiber bundle. By controlling it 85% or more, a phenomenon, where the carbon fiber sheet greatly moves during resin impregnation by the resin forcibly pressed, can be prevented, and the straightness of carbon fibers can be maintained. Further, by controlling it 95% or less, reduction of the straightness by being damaged with the movement of carbon fibers in the thickness direction during resin impregnation can be suppressed and, in addition, reduction of the straightness due to overlapping of single fibers can also be suppressed.
The carbon-fiber-reinforced plastic molded article is obtained by laminating a prepreg used for a unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface as the outermost layer, laminating the other layers which are not particularly restricted and which are the same prepregs as that for the outermost layer or layers composed of other materials, and molding. If the same prepregs are laminated, the materials may be one kind, and an error at the time of lamination can be avoided, and such a condition is preferred. In the case where the areal weight of the same prepregs is low, because many number of layers are to be laminated to obtain a carbon-fiber-reinforced plastic molded article having a required thickness, use of prepregs different in kind of carbon fibers or areal weight is also preferred from the viewpoint of shortening of operation time for lamination or cost. Further, it is also preferred to form a sandwich structure by using a resin sheet, a foamed resin sheet or a light metal sheet for the other layers and using a carbon-fiber-reinforced sheet for an outermost layer opposite to the above-described outermost layer, from the viewpoint of lightening in weight or cost.
In the carbon-fiber-reinforced plastic molded article, it is preferred that the prepregs used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheets forming the design surfaces and the other layers, which form the laminate, are disposed to become symmetric from the center of the laminate toward both surface layers. “Being disposed to become symmetric” means, for example, at the time of laminating the carbon-fiber-reinforced sheets, in the case where the number of lamination is an even number, to be disposed to become symmetric relatively to a plane brought into contact with carbon-fiber-reinforced sheets corresponding to half of the number of lamination and, in the case where the number of lamination is an odd number, to be disposed so that the carbon-fiber-reinforced sheets disposed on both sides relative to a carbon-fiber-reinforced sheet disposed at the center become symmetric relatively to the carbon-fiber-reinforced sheet disposed at the center. Furthermore, it is further preferred to be disposed so that the fiber orientations of the respective carbon-fiber-reinforced sheets become also symmetric. For example, in the case where prepregs used for unidirectionally continuous-carbon-fiber-reinforced sheets with an identical weave structure are laminated by 6 layers (an even number), they can be laminated so that the fiber arrangement directions become 0°/90°/0°/0°/90°/0° from the upper side. Further, in the case where unidirectionally continuous-carbon-fiber-reinforced prepregs are laminated by 7 layers (an odd number), they can be laminated so that the fiber arrangement directions become 0°/90°/0°/90°/0°/90°/0° from the upper side. If disposed in such a symmetric manner, a carbon-fiber-reinforced plastic molded article without a warp or a deflection can be obtained. On the contrary, if not disposed at a symmetric condition, depending upon the arrangement of the reinforcing fiber bundles, the disposition becomes a cause generating a warp or a deflection. Therefore, it is preferred that the prepreg used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming a design surface is laminated as the outermost layer and laminated also as the opposite-side outermost layer. Further, in the case where the carbon fiber areal weight of the outermost unidirectionally continuous-carbon-fiber-reinforced sheet is low, by laminating prepregs used for the outermost unidirectionally continuous-carbon-fiber-reinforced sheets forming the design surfaces at the outermost layer and the opposite-side outermost layer so that the sheets are laminated at a lamination condition of 0°/0°/90°/0°/90°/0°/90°/0°/0° from the upper side, the outermost layer forming the design surface and the second layer present thereunder become an identical direction, the influence that the concavo-convex of the second-layer prepreg gives to the design property of the outermost layer can be suppressed small, and such a condition is preferred.
Further, in the carbon-fiber-reinforced plastic molded article, for the purpose of improving the adhesive property in case of making it adhere to another member, an interposition sheet for adhesion can be laminated at an outermost layer at a side opposite to the outermost layer forming the design surface. As this interposition sheet for adhesion, a sheet comprising polyamide-group resin, polyester-group resin, polycarbonate-group resin, EVA resin (ethylenevinyl acetate copolymer resin), styrene-group resin or PPS (polyphenylene sulfide) group resin can be exemplified. Further, a modified material thereof may be employed. Such a thermoplastic resin may be used solely, or two or more may be used together as a copolymer or blend polymer thereof.
The process of producing the carbon-fiber-reinforced plastic molded article is not particularly restricted, processes using thermosetting resins such as hand lay-up molding, spray-up molding, vacuum bag molding, pressurization molding, autoclave molding, press molding and transfer molding, and processes using thermoplastic resins such as press molding and stamping molding, can be exemplified. In particular, from the viewpoint of process ability and mechanical properties, vacuum bag molding, press molding and transfer molding can be suitably employed.
By molding using a laminate laminated with the prepreg at the outermost layer, even if molded without particularly applying a tension in the carbon fiber direction of the prepreg at the time of the molding, a carbon-fiber-reinforced plastic molded article excellent in design property can be obtained without causing small fluctuation of disturbance of arrangement of the carbon fiber bundles.
At the time of producing the carbon-fiber-reinforced plastic molded article, it is necessary to mold while applying a pressure to obtain a predetermined shape and, for example, in the process such as press molding, it is preferred to mold at a pressing pressure of 0.5-5 MPa. If the pressure is too low, a molded article made by a pressing mold, having a predetermined thickness, cannot be obtained, and if the pressure is too high, the resin flows, and a resin deficit such as a pinhole may occur in the outermost layer forming the design surface, and such a condition is not preferred.
Further, in the carbon-fiber-reinforced plastic molded article, a structure can also be employed wherein a resin sheet having an areal weight of 15 g/m2 or less is further provided on the outermost layer forming the design surface of the molded article. As this resin sheet, for example, a non-woven fabric resin sheet can be used. The kind of the resin of the resin sheet is not particularly restricted and, for example, polyethylene terephthalate (PET) can be used. Since such a resin sheet essentially does not bear the strength or stiffness of the molded article, it may be thin and, therefore, a resin sheet with a low areal weight of 15 g/m2 or less may be employed. By adding such a resin sheet, even if very fine light and dark part is generated on the design surface formed by the above-described outermost unidirectionally continuous-carbon-fiber-reinforced sheet, it becomes possible to cover the light and dark part by the resin sheet with respect to the appearance, an excellent appearance design surface on which a light and dark part does not appear can be realized more securely. Although this resin sheet forms a final outermost layer, if the resin sheet becomes too thick over the areal weight of 15 g/m2, there is a fear that carbon fibers in the inside layer cannot be observed and, further, in case of using a non-woven fabric, there is a fear that the resin does not extend up to the design surface and the surface appearance deteriorates.
Although the carbon-fiber-reinforced plastic molded article can be used as a housing of equipment excellent in design property, for example, even as it is, it can be made into a housing of equipment integrated by bonding with a second member. Although the second member is not particularly restricted, a thermoplastic resin member and the like can be suitably used. As the method of integrating, bonding using an adhesive and the like can be employed. Further, in the above-described case where an interposition sheet for adhesion is laminated at an outermost layer at a side opposite to the design surface of the carbon-fiber-reinforced plastic molded article, as the method of integrating, exemplified is a method of making another member adhere thereto at a process temperature of the melting point of the thermoplastic resin forming the interposition sheet for adhesion or higher and, then, cooling to bond them. Further, as the method of bonding the thermoplastic resin as the second member by melting it, for example, thermal welding, vibration welding, ultrasonic welding, laser welding, insert injection molding and outsert injection molding can be exemplified.
Such a carbon-fiber-reinforced plastic molded article can be applied to any molded article required with an excellent design surface on which a defect in appearance design property such as the aforementioned one does not appear and, for example, it is suitable as a housing of equipment in various fields. In particular, if it is applied to a housing of equipment of an electric/electronic product, an extremely excellent design surface can be obtained.
In the carbon-fiber-reinforced plastic molded article, a design surface exhibiting an excellent appearance, in which reduction of the appearance quality ascribed to fluctuation in positions of carbon fiber bundles and disturbance in arrangement of carbon fibers on the design surface is extremely small, can be obtained, and a carbon-fiber-reinforced plastic molded article having an excellent appearance design property can be provided. In particular, by applying our articles to a housing of equipment, it becomes possible to greatly enhance the merchandise value of a product having the housing of equipment.
Hereinafter, our articles will be explained in detail together with examples.
In the carbon-fiber-reinforced plastic molded article, although the molded article comprises a laminate with at least two layers including a unidirectionally continuous-carbon-fiber-reinforced sheet in which continuous carbon fiber bundles are arranged in a predetermined one direction, among these, in particular, when carbon fibers of an outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming a design surface of the molded article are observed at the design surface, an area fraction of regions where a proportion of carbon fibers which are inclined at angles of 3° or more to the predetermined one direction is 0.5% or more is 20% or less relative to the whole area of the design surface. Then, as aforementioned, as this outermost unidirectionally continuous-carbon-fiber-reinforced sheet, preferably one having a carbon fiber areal weight of 30 g/m2 or more and 100 g/m2 or less is used. Further, preferably, as aforementioned, the resin content of the outermost unidirectionally continuous-carbon-fiber-reinforced sheet is controlled to be 15 mass % or more and 50 mass % or less, and the fineness of one carbon fiber bundle in the outermost unidirectionally continuous-carbon-fiber-reinforced sheet is controlled at 300 tex or less. Further, preferably, as aforementioned, in the process of producing a prepreg, a unidirectionally continuous-carbon-fiber-reinforced sheet, prepared through a process in which each carbon fiber bundle is enlarged in width up to 80-98% of a target width by being given with a tension of 0.5-6 cN/tex to the carbon fiber bundles in advance before a resin is impregnated into the carbon fiber bundles, is used for the outermost layer forming the design surface of the molded article. Further, it is preferred to use carbon fibers each having a tensile elastic modulus of 270 GPa or more as the carbon fibers used for this outermost unidirectionally continuous-carbon-fiber-reinforced sheet. Furthermore, in the case where a resin sheet is further provided on the outermost layer forming the design surface of the molded article, it is preferred to use a resin sheet having an areal weight of 15 g/m2 or less.
The method of determining “the area fraction of regions, where the proportion of carbon fibers which are inclined at angles of 3° or more is 0.5% or more, relative to the design surface” as the appearance property by image processing will be explained.
For example, as shown in
The measurement conditions at this determination are, for example, as follows:
Images taken out by photographing are processed as follows. The environment for carrying out the image processing is, for example, as follows:
First, image processing (1) is carried out in the following order:
Examples of image before processing (0) and extracted image (1) are shown in
Next, image processing (2) as shown in
Next, the areas of the fibers extracted in the above-described extracted images (1) and (2) are calculated respectively, the proportion of the above-described fibers 10 having inclined at ±3° or more is calculated using the following equation:
Proportion of fibers having inclined at ±3° or more (%)=[Area of fibers extracted in extracted image (2) (number of picture elements)]/[Area of fibers extracted in extracted image (1) (number of picture elements)]×100.
With respect to all the images observed as described above (25 points or more), the proportion of the inclined fibers is calculated, for example, as shown in Table 1 (in Table 1, Examples 1, 2 and Comparative Example 1 described later are exemplified.). Then, the rate of occurrence as to what % is the area fraction of regions where the proportion of carbon fibers on the design surface which are inclined at angles of 3° or more is 0.5% or more is calculated (the rate of occurrence is also exemplified in Table 1).
In Examples and Comparative Examples described later, with respect to the above-described estimation of appearance of design due to the rate of occurrence of the regions where the proportion of carbon fibers on the design surface which are inclined at angles of 3° or more is 0.5% or more, the case where the rate of occurrence was 10% or less was ranked as “⊚” (particularly excellent), the case where the rate was more than 10% and 20% or less was ranked as “∘” (excellent), and the case where the rate was more than 20% was ranked as “x” (the appearance of design is not good).
Further, in the respective Examples and Comparative Examples, in addition, the tensile strength (MPa) and the tensile elastic modulus (GPa) of the used carbon fibers, and the fineness of the carbon fiber bundle (tex) were determined, and with respect to the prepreg for the outermost unidirectionally continuous-carbon-fiber-reinforced sheet forming the design surface of the molded article, the fiber areal weight (g/m2), the fiber content (wt %), the tension applied to the carbon fiber bundles at the time of producing the prepreg (cN/tex), the yarn width after spreading of carbon fibers (mm), the yarn after processing into prepreg (mm) and the rate of enlarging the width (%) were determined, and further, in case where a resin sheet was provided on the outermost layer, its areal weight (g/m2) was also determined.
Hereinafter, our articles will be explained based on Examples and Comparative Examples.
Dimethyl sulfoxide solution containing 20 mass % of acrylonitrile-based polymer with an intrinsic viscosity [η] of 1.80 comprising 99.5 mol % of acrylonitrile and 0.5 mol % of itaconic acid was used as a spinning raw liquid, it was discharged once into air using a die with 6,000 holes each having a hole diameter of 0.15 mm, and then, it was introduced into a coagulation bath of 35% dimethyl sulfoxide aqueous solution controlled at a temperature of 10° C. to prepare coagulated yarns. After the coagulated yarns washed by water and stretched, they were provided with a surfactant whose main component was amino-modified silicone dispersion, and then, they were dried and compacted, and stretched using a steam stretching apparatus, and the obtained precursor fibers each having a circular section and a smooth surface were wound.
The precursor fibers were served to a carbonization process, they were oxidized without causing twist while being unrolled not to cause twist, and then, carbonized at conditions of a maximum temperature of 1900° C. and a tension of 5 g/tex of carbonized yarn. Thereafter, after they were provided with compatibility with matrix by successively anodizing them with the same tension, a sizing agent was provided and dried to obtain carbon fibers having a fineness of 250 tex, number of filaments of 6,000, a strand strength determined based on JIS R7608:2007 of 5,490 MPa, an elastic modulus of 295 GPa and a yarn width on a bobbin of 3.5 mm.
jER1005F supplied by Mitsubishi Chemical Corporation of 20 parts by mass and jER828 of 80 parts by mass were melt blended, and DICY-7 supplied by Mitsubishi Chemical Corporation of 7.5 parts by mass and “Omicure” supplied by CVC Specialty Chemicals, Inc. of 4.2 parts by mass were added and mixed to obtain a resin composition. This resin composition was coated onto a carrier sheet to obtain a resin sheet for a prepreg.
The above-described carbon fiber bundles were arranged at a tension of 1.9 cN/tex, a carbon fiber sheet was obtained using a multi-stage width enlargement apparatus having a plurality of rollers, and a carbon-fiber-reinforced prepreg was obtained at the conditions shown in Table 2. This unidirectional carbon-fiber-reinforced prepreg was cut at a predetermined size, it was used for the first layer and the eighth layer as the outermost layers, and using prepregs “P3052S” supplied by Toray Industries, Inc. (carbon fiber areal weight: 150 g/m2) for the inner layers (the second to the seventh layers), a laminate having totally eight layers was formed. As to the lamination structure, when the longitudinal direction of a carbon fiber molded article is referred to as 0° direction, the layers were laminated to become 0°/0°/90°/0°/0°/90°/0°/0°. After a material prepared by nipping this laminate with releasing films was evacuated by vacuum for 5 minutes for the purpose of removing air present in the laminate, it was press molded (temperature of mold: 150° C., pressure: 1.5 MPa, curing time: 20 minutes, target thickness after pressing: 0.8 mm) to obtain a carbon-fiber-reinforced plastic molded article. A tension for the purpose of arranging the carbon fibers of the prepreg was not particularly applied during the time after cutting the prepreg to the molding. The above-described conditions, the property of the obtained molded article (rate of occurrence of the regions where the proportion of carbon fibers on the design surface which are inclined at angles of 3° or more is 0.5% or more), and the result of the estimation of the appearance based thereon are shown in Table 2.
The examination results of cases (Examples 2-8, Comparative Examples 1-8) where at least one of the conditions of tensile elastic modulus of carbon fibers, fineness of carbon fiber bundle, carbon fiber areal weight and content of resin in prepreg, tension at the time of production, rate of enlarging width, and other conditions such as a case where a resin sheet (PET non-woven fabric with an areal weight of 15 g/m2 or less) was provided on the design surface, was changed from the above-described Example 1 are shown in Table 2 and Table 3.
As shown in Table 2 and Table 3, by controlling the tensile elastic modulus of carbon fibers, the fineness of carbon fiber bundle, the carbon fiber areal weight and content of resin in the prepreg, the tension at the time of production, and the like, in the preferable conditions, it was understood that an excellent appearance of design of the molded article could be obtained without causing disturbance of carbon fiber bundles even in the molding (Examples 1, 3, 5-8). Moreover, in case where a resin sheet was provided, if the areal weight was within our preferred conditions, the rate of occurrence of the regions where the proportion of carbon fibers on the design surface which were inclined at angles of 3° or more is 0.5% or more was lowered, the property of the molded article was improved (Examples 2, 4). On the other hand, in the case where the carbon fiber areal weight and content of resin in the prepreg, the tension at the time of production and the like, were not in our preferred conditions, the appearance of design was not improved (Comparative Examples 1, 3-8). Even if a resin sheet was further provided to such a molded article, the appearance of design could not be improved (Comparative Example 2).
The carbon-fiber-reinforced plastic molded article can be applied to any molded article requiring an excellent design surface and, in particular, it is suitable as a housing of equipment.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2010-276880 | Dec 2010 | JP | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/JP2011/077749 | 12/1/2011 | WO | 00 | 6/13/2013 |
