WO2015107903A1 - 被覆繊維強化樹脂成形品およびその製造方法 - Google Patents
被覆繊維強化樹脂成形品およびその製造方法 Download PDFInfo
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- WO2015107903A1 WO2015107903A1 PCT/JP2015/000175 JP2015000175W WO2015107903A1 WO 2015107903 A1 WO2015107903 A1 WO 2015107903A1 JP 2015000175 W JP2015000175 W JP 2015000175W WO 2015107903 A1 WO2015107903 A1 WO 2015107903A1
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- reinforced resin
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- fiber
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0025—Applying surface layers, e.g. coatings, decorative layers, printed layers, to articles during shaping, e.g. in-mould printing
- B29C37/0028—In-mould coating, e.g. by introducing the coating material into the mould after forming the article
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0025—Applying surface layers, e.g. coatings, decorative layers, printed layers, to articles during shaping, e.g. in-mould printing
- B29C37/0028—In-mould coating, e.g. by introducing the coating material into the mould after forming the article
- B29C2037/0035—In-mould coating, e.g. by introducing the coating material into the mould after forming the article the coating being applied as liquid, gel, paste or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2075/00—Use of PU, i.e. polyureas or polyurethanes or derivatives thereof, as moulding material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0809—Fabrics
- B29K2105/0845—Woven fabrics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/12—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
- B29L2009/005—Layered products coated
Definitions
- the present invention relates to a fiber reinforced resin molded product and a method for producing the same, and particularly, by forming a coating layer on the surface layer, the surface unevenness of the molded product due to shrinkage between the form of the reinforced fiber and the resin material is greatly reduced.
- the present invention relates to a coated fiber reinforced resin molded article having excellent surface quality and a method for producing the same.
- FRP fiber reinforced resin
- a sheet mold compound (SMC) molding method, a bulk mold compound (BMC) molding method, and the like are often used.
- the resin transfer molding (RTM) method has attracted attention and is being applied.
- the resin transfer molding (RTM) method can use reinforcing fibers in the form of continuous fibers, has very high mechanical properties, and is excellent in productivity because it can be molded in a short cycle time.
- the fiber-reinforced resin molded products obtained by these molding methods have defects due to poor filling of the resin on the surface, surface irregularities occur due to the form of the reinforcing fibers and the shrinkage of the resin, Therefore, the smoothness of the surface is often inferior to that of metal members that are often used.
- a fiber reinforced resin molded product having a large surface area or a complicated shape such as a curved surface or a vertically bent surface often takes a lot of time for repair and polishing.
- Patent Document 1 The following method has been proposed for such a problem (Patent Document 1).
- a fiber reinforcing material is placed in a heated mold, and then a matrix resin is injected into the mold cavity to impregnate the fiber reinforcing material to cover the fiber reinforced resin molded body, which will be described later.
- the matrix resin is cured until it can withstand the injection pressure of the product to obtain a fiber reinforced resin impregnated body.
- a composition (a resin different from the matrix resin) for coating the fiber reinforced resin molded body is injected between the surface of the fiber reinforced resin impregnated body and the mold surface.
- the mold is clamped again after the completion of injection, and the composition for covering the fiber-reinforced resin molded body is cured to obtain a fiber-reinforced resin molded body concealing the fibers and pinholes on the surface of the molded body.
- the coating composition on the surface.
- the surface irregularities accompanying the shrinkage of the entire surface layer resin composed of the form of the reinforcing fiber base and the matrix resin and the coating resin could not be sufficiently reduced. Because the surface irregularities accompanying the form of the reinforcing fiber substrate and the shrinkage of the entire surface resin are the thickness of the resin layer of the entire surface resin at the time of curing, and the surface layer due to the difference between the temperature when the resin is cured and the temperature normally used This is because it largely depends on the heat shrinkage of the entire resin.
- FIG. 1 shows a fiber-reinforced resin molded body immediately after demolding.
- the woven base material 1 is used at least on the surface layer as the reinforcing fiber base material
- the weft yarn 2 and the warp yarn 3 intersect with each other as seen in the AA sectional view along with the woven structure of the reinforcing fiber bundle.
- a concave portion is formed in the texture portion. In other words, irregularities are formed on the substrate surface.
- the thickness of the entire surface resin of the coated molded body of the fiber reinforced resin molded body formed between the smooth processed mold surface and the textile substrate that is, the matrix resin 4 and the coating resin 5 of the surface layer portion).
- the total thickness is not uniform. That is, the entire surface resin is thin at the convex and concave portions of the woven fabric substrate (thickness indicated by reference numeral 6 in FIG. 1), and the entire surface resin is thick at the concave portion (texture portion) (reference numeral 7 in FIG. 1). Thickness shown).
- both the matrix resin 4 and the coating resin 5 are thermally contracted. Since the absolute amount of heat shrinkage is small at the portion where the entire surface layer resin is thin, the change in the surface is small, but the portion where the entire surface layer resin is thick changes greatly. For this reason, as a result, the unevenness
- the surface position 8 indicates the surface position of the coated fiber reinforced resin molded product before heat shrinkage
- the surface position 9 indicates the surface position of the coated fiber reinforced resin molded product after heat shrinkage.
- the coating composition is formed at the same temperature as the temperature at which the fiber-reinforced resin molded product is molded. For this reason, even if the coating composition is formed at that temperature, when the coating composition is cooled to a temperature at which it is normally used, unevenness occurs due to thermal shrinkage of the resin.
- it can be a fundamental solution for reducing surface irregularities caused by a fiber reinforced resin molded product before forming a coating composition by the coating composition.
- a technique for greatly reducing the cycle time has been developed. For this reason, it is often used in combination with increasing the curing temperature of the matrix resin or the coating resin to shorten the curing time of the matrix resin or the coating resin. It was.
- an object of the present invention is to provide a method for producing a fiber reinforced resin capable of reducing surface irregularities caused by a temperature difference between a molding temperature (curing temperature) and room temperature when a fiber reinforced resin is molded.
- a method for producing a coated fiber reinforced resin molded article according to the present invention includes a first molding step of obtaining a fiber reinforced resin molded article by curing a matrix resin impregnated in a reinforced fiber at a temperature T1 (° C.), and at least The fiber reinforced resin molded product is arranged in the cavity of a molding die composed of two molds and having a cavity having substantially the same shape as the fiber reinforced resin molded product, and the temperature T2 (° C.) in the cavity is set to a temperature T1 ( The liquid coating layer forming resin material is injected into the cavity so as to cover at least a part of the surface layer of the fiber reinforced resin molded article, and the coating layer forming resin material is heated to a temperature T2.
- the first molding step and the second molding step are performed with different molding dies.
- the unevenness of the surface of the coated fiber reinforced resin molded product can be greatly reduced, and even with a complex shape fiber reinforced resin molded product having a curved surface or a vertically bent surface, the thickness is uniform. Can be coated.
- the adhesion with the coating layer is improved with respect to the portion where the coating layer of the fiber reinforced resin molded article is formed after the first molding step. It is also a preferable aspect that the surface unevenness of the coated fiber reinforced resin molded product is significantly reduced by performing the treatment to be performed and then performing the second molding step.
- the difference between the temperature T1 and the temperature T2 is set to 30 ° C. or more. Unevenness can be greatly reduced.
- the temperature T2 is set lower than 80 ° C. In this case, the surface unevenness of the coated fiber reinforced resin molded product can be greatly reduced.
- the matrix resin is a thermosetting resin, thereby greatly reducing the surface unevenness of the coated fiber reinforced resin molded article. can do.
- thermosetting resin as the resin material for forming the coating layer, and the surface irregularities of the coated fiber reinforced resin molded article are greatly increased. Can be reduced.
- the thickness of the coating layer is in the range of 50 ⁇ m to 600 ⁇ m. In this case, the surface unevenness of the coated fiber reinforced resin molded product can be greatly reduced.
- the reinforcing fibers are arranged in a cavity constituted by at least two molds and cured after injecting a liquid matrix resin.
- the surface unevenness is greatly reduced by obtaining the first fiber-reinforced resin molded product.
- the coated fiber reinforced resin molded article in which the surface unevenness according to the present invention is greatly reduced can be produced by any one of the methods described above.
- the coated fiber reinforced resin molded product according to the present invention is a coated fiber reinforced resin molded product composed of a fiber reinforced resin base material and a coating layer composed of at least a carbon fiber fabric and a resin (A), and has a certain depth.
- the concave shape formed in the fiber reinforced resin base material is a configuration in which the coating layer is laminated on the fiber reinforced resin base material in which the concave portion is formed.
- the coated fiber reinforced resin molded product according to the present invention is also a preferred embodiment in which the coating layer is formed of one layer of the thermosetting resin (B). In this case, it is possible to form a coating at once without preparing a plurality of molds.
- the coated fiber reinforced resin molded product according to the present invention is also a preferred embodiment in which a coating film by clear coating is further formed on the surface of the coating layer. In this case, the designability can be further improved.
- the coated fiber reinforced resin molded product according to the present invention has a wave scan value of short wave (SW) and long wave (LW) on the surface of the coated fiber reinforced resin molded product formed with a clear coating film.
- SW short wave
- LW long wave
- SW ⁇ 20 and LW ⁇ 8 It is also a preferable aspect to satisfy the relationship.
- class A which is an index of the surface quality of the automobile member can be achieved.
- the carbon fiber fabric is at least one fabric selected from a plain weave, a twill weave and a satin weave. In this case, the designability can be further improved.
- the coated fiber reinforced resin molded article according to the present invention is also a preferred embodiment in which the glass transition temperature (Tg (° C.)) of the resin (A) of the fiber reinforced resin base material is Tg ⁇ 100 ° C. In this case, heat resistance required for the automobile member can be satisfied.
- a method for producing a coated fiber reinforced resin molded product according to the present invention includes a first molding step of obtaining a fiber reinforced resin molded product by curing a matrix resin impregnated in a reinforced fiber at a temperature T1 (° C.); A coating layer forming resin material is injected into the cavity so as to cover at least a part of the surface layer of the fiber reinforced resin molded article, and the coating layer forming resin material is at a temperature T2 (° C.) lower than the temperature T1 (° C.). And a second molding step of obtaining a coated fiber reinforced resin molded product by curing with the above method.
- the present invention it is possible to provide a coated fiber reinforced resin molded product that can significantly reduce surface irregularities generated on the surface in accordance with the form of the reinforcing fiber, and a method for producing the same.
- the method for producing a coated fiber reinforced resin molded article in the present embodiment includes a first molding step for obtaining a fiber reinforced resin molded article by curing a matrix resin impregnated in a reinforced fiber at a temperature T1 (° C.), and at least two molds.
- the fiber reinforced resin molded product is arranged in the cavity of a mold having a cavity having substantially the same shape as the fiber reinforced resin molded product, and the temperature T2 (° C.) in the cavity is set from the temperature T1 (° C.).
- a liquid coating layer forming resin material is injected into the cavity so as to cover at least a part of the surface layer of the fiber reinforced resin molded article, and the coating layer forming resin material is heated to a temperature T2 (° C. ) To form a coated fiber reinforced resin molded product.
- the matrix resin impregnated in the reinforcing fibers can be cured at a temperature T1 (° C.) to obtain a fiber reinforced resin molded product.
- T1 temperature
- the effect is not exhibited only when limited reinforcing fibers are used, and various reinforcing fibers can be applied.
- carbon fiber or glass fiber is often used as the reinforcing fiber.
- carbon fiber is preferable because a lightweight, high-strength and high-rigidity fiber-reinforced resin molded product can be obtained. Further, when the reinforcing fibers are used in the form of continuous fibers, higher mechanical properties can be expressed.
- a UD material unidirectional material in which reinforcing fibers are arranged in one direction
- reinforcing fibers are arranged in one direction or in the same direction
- Various reinforcing fiber base materials such as NCF material (non-crimp fabric material) laminated in multiple layers in different directions and held in a sheet form with stitch yarns, and (iii) woven fabric using reinforcing fibers can be used as appropriate.
- the product value of the molded product is particularly high in the case of a product in which the fiber reinforced resin molded product can be visually recognized from the outside without being colored.
- fabrics such as plain weave, twill weave and satin weave may be preferably used.
- the basis weight of the base material also affects the design properties.
- a base material When used for a product whose woven structure is visible from the outside, it is preferable to use a base material of about 100 g / m 2 to about 300 g / m 2 .
- the thickness of the entire surface resin may not be uniform due to the stitch yarn.
- the effect of reducing surface irregularities can be obtained.
- the type of matrix resin either a thermoplastic resin or a thermosetting resin can be applied as appropriate. It is preferable to use a thermosetting resin such as an unsaturated polyester resin, an epoxy resin, a phenol resin, or a polyurethane resin as the matrix resin because a fiber-reinforced resin molded product having excellent mechanical properties can be obtained. Moreover, it is preferable that the glass transition temperature (Tg) of matrix resin is 100 degreeC or more from a heat resistant viewpoint. The glass transition temperature (Tg) of the matrix resin is more preferably 120 ° C. or higher. The glass transition temperature of the matrix resin is determined by using a differential scanning calorimeter to rapidly cool the matrix resin in liquid nitrogen at 150 ° C./min.
- a thermosetting resin such as an unsaturated polyester resin, an epoxy resin, a phenol resin, or a polyurethane resin
- Tg glass transition temperature of matrix resin is 100 degreeC or more from a heat resistant viewpoint.
- the glass transition temperature (Tg) of the matrix resin is more
- the intermediate-point glass transition temperature that appears when the temperature is raised at.
- the midpoint glass transition temperature is obtained in accordance with the method defined in JIS K7121-1987, and is a straight line equidistant from the straight line obtained by extending the low temperature side baseline and the high temperature side baseline in the vertical axis direction. It is the temperature at the point where the curve of the step-like change part of the glass transition intersects.
- the molding method in the first molding step is as follows: (i) An intermediate base material formed into a sheet shape by impregnating a reinforcing fiber bundle cut to an appropriate length in advance with a thermosetting resin is pressurized and heated with a molding die. SMC molding method that molds into a predetermined shape, and (ii) pressurizes and heats an intermediate material in a bulk shape by mixing reinforced fiber bundles cut to an appropriate length, thermosetting resin and filler (Iii) Molding a prepreg, which is an intermediate base material in which a bundle of reinforcing fibers that are drawn in parallel or made into a sheet is impregnated with a matrix resin.
- a prepreg molding method in which layers are placed in a mold and heated and pressed with a press, placed in a mold and heated in a vacuum bag, or heated and pressed in an autoclave, and (iv) a mold comprising a double-sided mold Weaving on one mold, A liquid matrix resin is supplied onto a reinforcing fiber substrate such as CF, and the like can be applied liquid compression method to heat and pressure to close the double-sided.
- the mold 11 is composed of at least two molds.
- the mold seal 12 is a part used for sealing the mold.
- the mold 11 is adjusted to a predetermined temperature by a mold temperature adjusting device 16.
- the temperature can be adjusted by flowing a heat medium through the heat medium flow path 17 and adjusting the temperature of the heat medium.
- a reinforcing fiber base material is laminated and arranged in a predetermined orientation in a cavity of a mold 11 whose temperature has been adjusted by a mold temperature controller 16 and clamped.
- the matrix resin injection path opening / closing mechanism 14 is controlled, and the matrix resin injection flow path 15 provided so as to communicate with the cavity using the matrix resin injection device 13 outside the mold 11 is used to enter the liquid matrix resin into the cavity. Is injected under pressure to impregnate the reinforcing fiber substrate. Thereafter, the matrix temperature resin is cured in the mold heated to the temperature T1 (° C.) by the mold temperature adjusting device 16 to mold the fiber reinforced resin molded product 10. Finally, the mold 11 is opened and the fiber reinforced resin molded product is taken out.
- the effect of the embodiment of the present invention is not limited by the molding method in the first molding step, and any method can be applied.
- the matrix resin on the surface portion of the fiber reinforced resin molded product is cured at a temperature T1 (° C.) by receiving heat from the heated mold 11 while being in close contact with the mold. Since the matrix resin is pressed against the mold during curing, the surface of the fiber reinforced resin molded product immediately after curing is in a state where the surface of the mold that has been processed smoothly is transferred. However, when the mold is removed from the mold of temperature T1 (° C.) and cooled to room temperature, as described above, the surface layer of the fiber reinforced resin molded product is uneven due to the textured structure of the reinforcing fiber bundle constituting the reinforcing fiber base. A thick part and a thin part are generated in the matrix resin layer. As a result, since the absolute amount of thermal shrinkage of the resin layer is different, irregularities are generated on the surface of the fiber-reinforced resin molded product.
- a coated layer can be obtained by forming a coating layer on the surface layer of the fiber reinforced resin obtained in the first molding step in the second molding step.
- the mold 18 is composed of a mold having at least two surfaces.
- the mold seal 12 is a part used for sealing the mold.
- the molding die 18 is provided with a resin material injection channel 21 for forming a coating layer.
- the resin material for forming a coating layer can be switched between a discharge state and a stopped state by an injection flow path opening / closing mechanism 20 provided in the middle of the flow path.
- a mold 18 having a cavity having substantially the same shape as the fiber-reinforced resin molded article 10 obtained in the first molding step is used.
- the mold is adjusted to a predetermined temperature by the mold temperature adjusting device 16.
- the temperature can be adjusted by flowing a heat medium through the heat medium flow path 17 and adjusting the temperature of the heat medium.
- the coating layer forming resin material injection path opening / closing mechanism 20 is controlled, and a liquid coating layer forming resin material is discharged from the coating layer forming resin material discharge device 19 outside the mold. The coating layer forming resin material is communicated with the cavity.
- the “substantially the same shape” indicates that the overall shape is substantially the same even if the difference in shape is such that a space for forming a coating layer, which will be described later, is given to the fiber-reinforced resin molded product.
- the coating layer 5 is formed on the fiber reinforced resin molded article 10 by the second forming step.
- the same molding die may be used for the first molding step and the second molding step, or different molding dies may be used.
- the mold temperature is set to T1 (° C.) in the first molding step, and then the mold temperature is lowered from T1 (° C.) to T2 (° C.) before the second molding step is performed. . For this reason, in this case, it may take time to adjust the temperature.
- a liquid coating layer forming resin material is injected so as to cover at least a part of the surface layer of the fiber reinforced resin molded product.
- the cavity of the molding die composed of two molds is expanded by about 0.1 to several mm, or the first molding step In comparison with this, it is necessary to secure a space for forming the coating layer in the cavity with the pressure of the coating layer forming resin material that is injected with the mold clamping slightly relaxed.
- the molding mold used in the first molding process is set to a temperature T1 (° C.) and the molding mold used in the second molding process. May be set to the temperature T2 (° C.), respectively, and there is no need to adjust the temperature. For this reason, cycle time can be shortened and it is preferable.
- the space for forming the coating layer in at least a part of the fiber reinforced resin molded product can be accurately formed by processing the mold used in the second forming step into a suitable shape in advance. it can.
- the mold 18 is temperature-controlled at a temperature T2 (° C.) lower than the temperature T1 (° C.).
- T2 ° C.
- T1 ° C.
- the fiber reinforced resin molded product 10 arranged in the cavity of the molding die 18 has surface irregularities caused by heat shrinkage of the resin on the surface of the molded product as described above.
- the coating layer forming resin material is pressurized and injected into the cavity from the coating layer forming resin material discharge device 19 through the coating layer forming resin material injection channel 21 provided in the mold, the fiber reinforced resin molded product side Is uneven, but the mold side (cavity side) is processed smoothly, so the coating layer is formed with a non-uniform thickness, and the coating layer forming resin material is at a temperature T2 (° C.). Harden.
- the coating layer forming material is filled in the mold and continued to be injected for a certain period of time after curing shrinkage has started, thereby reducing surface quality degradation due to curing shrinkage of the coating layer forming material. .
- the coated fiber reinforced resin molded article shown in FIG. 3 is a coated fiber reinforced resin molded article composed of at least a fiber reinforced resin base material and a coating layer made of a carbon fiber fabric and a resin (A), and has a certain depth.
- Db depth of the concave shape formed in the fiber reinforced resin base material
- Db depth of the concave shape formed in the coating layer
- the difference between the temperature T1 (° C.) for curing the matrix resin in the first molding step and the temperature T2 (° C.) for curing the coating layer in the second molding step is 30 ° C. or more. It is preferable to do. That is, it is preferable to make the temperature T2 (° C.) 30 ° C. or more lower than the temperature T1 (° C.) because the effect of reducing the surface unevenness of the coated fiber reinforced resin molded product can be sufficiently exhibited.
- the difference between the temperature T1 (° C.) for curing the matrix resin in the first molding step and the temperature T2 (° C.) for curing the coating layer in the second molding step is more preferably 40 ° C. or more, and further preferably 50 ° C. or more. .
- the temperature T2 (° C.) is lower than 80 ° C.
- the thermal shrinkage of the resin when cooled to room temperature after forming the coating layer is smaller than when it is 80 ° C. or higher.
- the surface unevenness of the coated fiber reinforced resin molded article is preferably at a level that is hardly worrisome.
- the temperature T2 is more preferably 60 ° C. or less, and further preferably 50 ° C. or less.
- the resin material for forming the coating layer has a low viscosity so that it can be cured quickly at a low temperature, has excellent adhesion to a fiber-reinforced resin molded product as a base, and can be efficiently injected into a narrow space.
- a thermosetting resin can be suitably used as the coating layer forming resin material.
- unsaturated polyester resin, an epoxy resin, a phenol resin, a polyurethane resin etc. can be used conveniently, for example.
- the coating layer itself may be colored and may form a coating film that improves the appearance design, or may be a base layer for coating in a later step.
- the resin material for forming the coating layer can be specialized in characteristics suitable for improving the surface irregularities of the coated fiber reinforced resin molded product, unlike the matrix resin which is largely related to the mechanical properties of the fiber reinforced resin molded product. For this reason, it is easy to devise various methods.
- inorganic particles can be blended in the resin material for forming the coating layer in order to disperse the stress accompanying shrinkage and to reduce the linear expansion coefficient / curing shrinkage.
- the thickness of the coating layer of the coated fiber reinforced resin molded product according to the embodiment of the present invention is preferably 50 ⁇ m or more, and more preferably 100 ⁇ m or more. Moreover, it is preferable to form the coating layer of the coated fiber reinforced resin molded article of the embodiment of the present invention so as to have a thickness of 600 ⁇ m or less, and more preferably a thickness of 500 ⁇ m or less. By setting the thickness to 50 ⁇ m or more, it becomes difficult to form a portion where the coating layer is missing, and it is easy to obtain the effect of relaxing the surface irregularities of the coated fiber reinforced resin molded product. On the other hand, when the thickness is 600 ⁇ m or less, an increase in the weight of the coating layer can be suppressed, and the characteristics of the fiber-reinforced resin molded product that is lightweight and excellent in mechanical properties are easily exhibited.
- the coated fiber reinforced resin molded product of the embodiment of the present invention improves the adhesion of the resin material for forming the coating layer to the surface on which the surface layer is coated at least in the second molding step after the first molding step. It is also a preferred embodiment to perform a surface treatment for the purpose.
- the fiber reinforced resin molded product after the first molding step is added to the matrix resin when the release material applied to the mold is transferred to the surface so that the mold can be easily released from the mold. Depending on the internal mold release material, there may be a case where sufficient adhesion with the coating layer cannot be exhibited.
- the fiber reinforced resin molded product is taken out from the mold, and at least the surface on which the coating layer is to be formed is polished with an abrasive or the like so that the matrix resin or mold release on the surface layer of the fiber reinforced resin molded product
- the surface of the fiber reinforced resin layer that has been subjected to the pretreatment for improving the adhesion with the coating layer the surface is polished with sandpaper or the like to remove the outermost layer or to form a polishing mark.
- a second molding step may be performed. By performing these treatments, the unevenness that can occur in the molded product can be made smaller than the unevenness caused by the fibers.
- this coating layer is preferably a single layer. In this case, it is because a coating layer can be formed at once without preparing a plurality of coating molds.
- the representative means can be determined from the cross-section of the coated fiber reinforced resin using a method using a surface roughness meter, a microscope, or the like. For example, it may be obtained from the maximum peak height (Pt) using a contact type surface roughness meter, or may be obtained from a cross section using a microscope.
- Pt maximum peak height
- SEM X-ray fluorescence analysis
- the coated fiber reinforced resin molding in this embodiment is used.
- the product has a Da / Db of 0.7 or less.
- Da / Db is preferably 0.5 or less.
- the surface unevenness Da ( ⁇ m) of the coated fiber reinforced resin molded product is a distance 22
- the unevenness Db ( ⁇ m) of the surface of the fiber reinforced resin molded product is a distance 23.
- the surface unevenness Da ( ⁇ m) of the coated fiber reinforced resin molded product is a distance 22a
- the unevenness Db ( ⁇ m) of the fiber reinforced resin molded product is a distance 23a.
- the evaluation of the present invention uses wave scan (WaveScan), which can quantify the image sharpness and the phenomenon in which waviness is seen on the paint surface (also called orange peel) when a certain level of glossiness is obtained. Can also be measured.
- WaveScan wave scan
- the best surface condition is called “Class A”.
- SW short wave
- LW long wave
- SW is 20 or less
- LW is 4 or less.
- the product using the molded product according to the embodiment of the present invention is preferably a component having a large surface area. That is, preferably at the product surface area 900 cm 2 or more, still more preferably 8000 cm 2 or more.
- the larger the surface area the shorter the polishing work time for footing and surface smoothing can be prevented, and the generation of polishing powder during work can be prevented, and high design can be achieved with simple work. it can.
- coated fiber reinforced resin molded product of the present invention can be produced by the method as described above.
- FIG. Uses a mold made of S55C, which has a plurality of mold temperature control pipes consisting of heating pipes inside, and has a resin inlet on the upper mold and has a plane size of 700 mm x 600 mm, a height of 300 mm, and a clearance of 1.6 mm did.
- FIG. A mold having the same shape and mechanism as a molding mold having a cavity of 1.9 mm was used.
- Bidirectional fabric CO6343B manufactured by Toray Industries, Inc. (weave yarn: carbon fiber T300-3K, weave structure: plain weave, fabric basis weight: 198 g / m 2 , thickness: 0.25 mm, warp yarn weave density: 12.5 / 25mm, weft density: 12.5 / 25mm).
- Matrix resin TR-C38 manufactured by Toray Industries, Inc. (glass transition temperature: 135 ° C. (evaluated with cured matrix resin after curing at 120 ° C. for 10 minutes))
- the temperature of the coating mold was adjusted to a predetermined temperature, a fiber reinforced resin molded product was placed on the lower mold, the upper mold was closed, and the mold was evacuated. Then, according to the combinations shown in Table 1, after adding 5 parts of the main agent to 100 parts of the main agent on the hardener side, the main agent and the hardener were mixed to have an epoxy equivalent of 1: 1. The resin was poured into the mold, the upper mold was opened, and the coated fiber reinforced resin molded product was taken out. Then, the surrounding resin was dropped with a disc grinder to complete.
- Example 1 The fiber reinforced resin molded product was coated and evaluated under the resins and coating conditions shown in Table 1. The difference between the curing temperature of the matrix resin and the curing temperature of the coating resin was sufficient, and the curing temperature of the coating resin was also low, so the fluorescent lamp that had moved to the surface was very clean without undulation. Further, the WS value also satisfied the class A.
- coated fiber reinforced resin molded article and the manufacturing method thereof according to the present invention can be applied to any fiber reinforced resin for which excellent surface quality is desired.
Abstract
Description
Db/Da≦0.7
の関係を満たすものである。この関係を満たすことで、被覆繊維強化樹脂成形品の表面凹凸を大幅に低減することができる。
SW≦20、かつLW≦8
の関係を満たすことも好ましい態様である。この場合、自動車部材の表面品位の指標であるクラスAを達成することができる。
・100tプレス機(株式会社山本鉄工所製)
・金型温調機(株式会社サーモテック製)
・図4に断面形状を示す。内部に加熱配管からなる型温調配管が複数配置されており、上型に樹脂注入口を有する、平面寸法700mm×600mm、高さ300mm、クリアランス1.6mmを有するS55Cでできた金型を使用した。
[被覆用金型]
・図5に断面形状を示す。キャビティを1.9mmとった成形用金型と同様の形状、機構をもつ金型を使用した。
・二方向性織物:東レ(株)製CO6343B(織糸:炭素繊維T300-3K、織組織:平織り,織物目付:198g/m2、厚さ:0.25mm、縦糸織密度:12.5本/25mm,横糸織密度:12.5本/25mm)。
[マトリクス樹脂]
・マトリクス樹脂:東レ(株)製TR-C38(ガラス転移温度:135℃(120℃で10分硬化させた後のマトリクス樹脂硬化物で評価))
・主剤:新日本理化(株)製BEO-60E
・硬化剤:三井化学(株)製NBDA、三菱化学(株)製QX-11、昭和電工(株)製MT-PE1、新日本理化(株)製MH-700
・触媒;日本化学工業(株)製ヒシコーリンPX-4ET、北興化学工業(株)製ホクコーTPP
・プライマー:大橋化学工業(株)製Po.800(NH)001
・クリアー:日本ビー・ケミカル(株)製KX28106
・ウェーブスキャン機器:BYK製ウェーブスキャンデュアル
・デジタルマイクロスコープ:(株)キーエンス製VHX-1000
・強化繊維基材から、縦糸、横糸の方向をそれぞれ0°、90°としたときに、0°の方向が長軸方向となるよう、型紙を使って切り出した。
・成形用金型の温度を120℃にあわせた後、切り出した基材を金型の上に6枚乗せ、上型を閉じ、金型内を真空状態にした後、マトリクス樹脂を流し込み、10分間硬化させて、上型を開け、繊維強化樹脂成形品を取り出した。その後、繊維強化樹脂成形品の周りの樹脂をディスクグラインダで落とし、完成させた。
・被覆用金型の温度を所定の温度に調整し、下型に繊維強化樹脂成形品を置き、上型を閉じた後、金型内を真空引きした。その後、表1の組み合わせに従い、触媒が必要なものは、硬化剤側に、主剤100部に対して5部加えた後、主剤・硬化剤をエポキシ等量で1:1になるよう混ぜた後、金型内に樹脂を流し込み、上型を明け、被覆繊維強化樹脂成形品を取り出した。その後、周りの樹脂をディスクグラインダで落とし、完成させた。
・塗装膜厚が、プライマーとクリアーあわせて30μmになるよう、所定の条件で塗装した。
・評価は被覆繊維強化樹脂成形品への蛍光灯の移りこみ具合、断面からのDb(μm)とDa(μm)の算出、および塗装後のウェーブスキャン(WS)値の確認を行った。
・塗装が完了した被覆繊維強化樹脂成形品を、ディスクグラインダで2cm角に切り出しサンプルを作製した。サンプルの断面を、ポリッシャーで磨いた後、デジタルマイクロスコープ(VHX-1000)で観察し、断面からDb(μm)とDa(μm)を求めた。測定場所を5回変え、最もDa(μm)が大きくなった際の値を、表1に記載した。
・塗装が完了した被覆繊維強化樹脂成形品表面を、ウェーブスキャン機器(ウェーブスキャンデュアル)を用いて、Db(μm)を5回測定し、その平均値を、表1に記載した。
・表1に示す樹脂と被覆条件で繊維強化樹脂成形品への被覆を行い、評価を行った。マトリクス樹脂の硬化温度と、被覆用樹脂の硬化温度の差が十分にあり、被覆用樹脂の硬化温度も低かったため、表面に移りこんだ蛍光灯は、うねりなく非常にきれいだった。また、WS値もクラスAを満たす結果であった。
・表1に示す樹脂と被覆条件で繊維強化樹脂成形品への被覆を行ったが、被覆用樹脂に求められる硬化温度に対して、温度が低かったため、被覆用の樹脂が十分に固まっておらず、脱型ができなかった。
・表1に示す樹脂と被覆条件で繊維強化樹脂成形品への被覆を行い、評価を行った。マトリクス樹脂の硬化温度と、被覆用樹脂の硬化温度の差がそれほどなく、被覆用樹脂の硬化温度も高かったため、成形品のクロス凹凸を拾ってしまい、蛍光灯の移りこみは、うねりが見えた。また、WS値はクラスAを達成することができなかった。
2 織物基材を構成する強化繊維束(横糸)
3 織物基材を構成する強化繊維束(縦糸)
4 マトリクス樹脂
5 被覆層
6 織物基材の凸部分に対応する表層樹脂全体の厚さ
7 織物基材の凹部分に対応する表層樹脂全体の厚さ
8 熱収縮前の被覆繊維強化樹脂成形品の表面位置
9 熱収縮後の被覆繊維強化樹脂成形品の表面位置
10 繊維強化樹脂成形品
11 成形型
12 金型シール
13 マトリクス樹脂注入装置
14 マトリクス樹脂注入経路開閉機構
15 マトリクス樹脂注入流路
16 金型温度調節装置
17 熱媒流路
18 成形型
19 被覆層形成用樹脂材料吐出装置
20 被覆層形成用樹脂材料注入経路開閉機構
21 被覆層形成用樹脂材料注入流路
22 被覆繊維強化樹脂成形品の表面凹凸量(Da)
23 繊維強化樹脂成形品表面の凹凸量(Db)
24 空隙部分
Claims (16)
- 強化繊維に含浸されたマトリクス樹脂を温度T1(℃)で硬化させ繊維強化樹脂成形品を得る第1の成形工程と、少なくとも2つの型から構成され、前記繊維強化樹脂成形品と略同一形状のキャビティを有する成形型の該キャビティ内に該繊維強化樹脂成形品を配置し、前記キャビティ内温度T2(℃)を温度T1(℃)よりも低い温度として、前記繊維強化樹脂成形品の少なくとも一部の表層を覆うように液状の被覆層形成用樹脂材料を前記キャビティ内に注入し、前記被覆層形成用樹脂材料を温度T2(℃)で硬化させて被覆繊維強化樹脂成形品を得る第2の成形工程を含む、被覆繊維強化樹脂成形品の製造方法。
- 前記第1の成形工程と、第2の成形工程が、別の成形型で実施される、請求項1に記載の被覆繊維強化樹脂成形品の製造方法。
- 前記温度T1(℃)と前記温度T2(℃)の差が30℃以上である、請求項1~2のいずれか1項に記載の被覆繊維強化樹脂成形品の製造方法。
- 前記温度T2(℃)が80℃よりも低い、請求項1~3のいずれか1項に記載の、被覆繊維強化樹脂成形品の製造方法。
- 前記マトリクス樹脂が熱硬化性樹脂である、請求項1~4のいずれか1項に記載の被覆繊維強化樹脂成形品の製造方法。
- 前記被覆層形成用樹脂材料が熱硬化性樹脂である、請求項1~5のいずれか1項に記載の被覆繊維強化樹脂成形品の製造方法。
- 前記被覆層の厚さが50μmから600μmの範囲である、請求項1~6のいずれか1項に記載の被覆繊維強化樹脂成形品の製造方法。
- 請求項1~7のいずれか1項に記載された方法により製造された、被覆繊維強化樹脂成形品。
- 少なくとも炭素繊維織物と樹脂(A)からなる繊維強化樹脂基材及び被覆層から構成される被覆繊維強化樹脂成形品であって、一定深さの凹部が形成された前記繊維強化樹脂基材上に前記被覆層が積層された構成であり、前記繊維強化樹脂基材の断面形状において、前記繊維強化樹脂基材に形成された凹部形状の深さをDa(μm)、前記被覆層に形成された凹部形状の深さをDb(μm)とすると、
Db/Da≦0.7
の関係を満たすことを特徴とする被覆繊維強化樹脂成形品。 - 請求項1~8のいずれか1項に記載の方法で製造された被覆繊維強化樹脂成形品であって、前記被覆繊維強化樹脂成形品は、前記強化繊維が炭素繊維織物であり、前記マトリクス樹脂が樹脂(A)である繊維強化樹脂基材および前記被覆層から構成され、かつ、一定深さの凹部が形成された前記繊維強化樹脂基材上に前記被覆層が積層された構成であり、前記繊維強化樹脂基材の断面形状において、前記繊維強化樹脂基材に形成された凹部形状の深さをDa(μm)、前記被覆層に形成された凹部形状の深さをDb(μm)とすると、
Db/Da≦0.7
の関係を満たすことを特徴とする被覆繊維強化樹脂成形品。 - 前記被覆層は熱硬化性樹脂(B)の1層で形成された構成である請求項9または10に記載の被覆繊維強化樹脂成形品。
- 前記被覆層表面にさらにクリアー塗装による塗膜を形成した構成である請求項9~11のいずれか1項に記載の被覆繊維強化樹脂成形品。
- 前記被覆繊維強化樹脂成形品にクリアー塗装による塗膜を形成した表面のWave Scan値のショートウェーブ(SW)とロングウェーブ(LW)とが、
SW≦20、かつLW≦8
の関係を満たす請求項9~12のいずれか1項に記載の被覆繊維強化樹脂成形品。 - 前記炭素繊維織物は、平織り、綾織及び繻子織から選択される少なくとも1つの織物である請求項9~13のいずれか1項に記載の被覆繊維強化樹脂成形品。
- 前記繊維強化樹脂基材の樹脂(A)のガラス転移温度(Tg(℃))がTg≧100℃である、請求項9~14のいずれか1項に記載の被覆繊維強化樹脂成形品。
- 強化繊維に含浸されたマトリクス樹脂を温度T1(℃)で硬化させ繊維強化樹脂成形品を得る第1の成形工程と、前記繊維強化樹脂成形品の少なくとも一部の表層を覆うように被覆層形成用樹脂材料をキャビティ内に注入し、前記被覆層形成用樹脂材料を前記温度T1(℃)よりも低い温度T2(℃)で硬化させて被覆繊維強化樹脂成形品を得る第2の成形工程とを含む、被覆繊維強化樹脂成形品の製造方法。
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JP6889134B2 (ja) * | 2018-09-07 | 2021-06-18 | 矢崎総業株式会社 | 樹脂装飾部品及び文字板 |
JP6887975B2 (ja) * | 2018-09-07 | 2021-06-16 | 矢崎総業株式会社 | 樹脂装飾部品及び文字板 |
JP2020041851A (ja) * | 2018-09-07 | 2020-03-19 | 矢崎総業株式会社 | 樹脂装飾部品及び文字板 |
CN111098523B (zh) * | 2019-11-13 | 2021-02-26 | 北京玻钢院复合材料有限公司 | 一种复合材料轻质舱体及其制备方法 |
US11453182B2 (en) * | 2019-12-05 | 2022-09-27 | GM Global Technology Operations LLC | Methods for forming class-A components with moldable carbon fiber |
CN114845848A (zh) * | 2019-12-20 | 2022-08-02 | 株式会社棚泽八光社 | 树脂成型用模具、树脂成型用模具的制造方法、树脂成型品的制造方法及树脂成型品制造系统 |
JP7322771B2 (ja) * | 2020-03-24 | 2023-08-08 | トヨタ自動車株式会社 | 繊維強化樹脂成形品の製造方法 |
CN113085229B (zh) * | 2021-04-22 | 2022-02-15 | 同济大学 | 碳纤维增强热固性树脂基复合材料分层损伤修复装置及方法 |
CN114905818A (zh) * | 2021-11-25 | 2022-08-16 | 江苏奇一科技有限公司 | 一种连续纤维增强热塑性复合板、制备方法及其生产线 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07223231A (ja) * | 1994-02-15 | 1995-08-22 | Sekisui Chem Co Ltd | 型内被覆成形品の製造方法 |
JP2008143077A (ja) * | 2006-12-12 | 2008-06-26 | Toyota Auto Body Co Ltd | 型内被覆成形方法及び型内被覆成形品 |
JP2013209510A (ja) | 2012-03-30 | 2013-10-10 | Dainippon Toryo Co Ltd | 繊維強化樹脂成形体被覆組成物、該被覆組成物を塗装して得られる繊維強化樹脂成形体及び該繊維強化樹脂成形体の製造方法 |
Family Cites Families (77)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4081578A (en) * | 1974-06-27 | 1978-03-28 | The General Tire & Rubber Company | In-mold coating composition and method of applying same |
NL7903428A (nl) * | 1979-05-02 | 1980-11-04 | Stamicarbon | Werkwijze voor het vervaardigen van uit thermohardende hars gevormde voorwerpen. |
US4245006A (en) * | 1979-05-18 | 1981-01-13 | The General Tire & Rubber Company | Low-pressure low-temperature in-mold coating method |
US4320160A (en) * | 1979-08-21 | 1982-03-16 | Toray Industries, Inc. | Fabric structure for fiber reinforced plastics |
US4356230A (en) * | 1980-07-10 | 1982-10-26 | International Telephone And Telegraph Corporation | Molded plastic product having a plastic substrate containing a filler and an in-mold plastic coating firmly bonded thereon and a process for its manufacture |
JPS5841950A (ja) * | 1981-08-31 | 1983-03-11 | 東レ株式会社 | 繊維強化樹脂用補強基材 |
US4534888A (en) * | 1982-10-25 | 1985-08-13 | The General Tire & Rubber Company | In-mold coating |
US4414173A (en) * | 1981-11-02 | 1983-11-08 | The General Tire & Rubber Company | In-mold coating |
US4515710A (en) * | 1983-07-18 | 1985-05-07 | Gencorp Inc. | In-mold coating composition |
US4668460A (en) * | 1985-04-02 | 1987-05-26 | The Sherwin-Williams Company | Method of molding and coating a substrate in a mold. |
JPS63152637A (ja) * | 1986-12-16 | 1988-06-25 | Toray Ind Inc | 樹脂の補強用プリフオ−ム材 |
DE3706227A1 (de) * | 1987-02-26 | 1988-09-08 | Bayer Ag | Formbares halbzeug fuer die fertigung biegesteifer formteile |
US4762740A (en) * | 1987-06-15 | 1988-08-09 | Ford Motor Company | Resin transfer molding core, preform and process |
FR2619399B1 (fr) * | 1987-08-11 | 1991-10-25 | Brochier Sa | Structure textile pour la realisation de stratifies a hautes proprietes mecaniques |
US4900608A (en) * | 1988-04-04 | 1990-02-13 | Gencorp Inc. | Flexible epoxy-coated fabric |
US5087405A (en) * | 1988-11-08 | 1992-02-11 | Coplas, Inc. | In mold overlay process for gel coated glass fiber reinforced laminates |
US5009821A (en) * | 1989-02-23 | 1991-04-23 | Libbey-Owens-Ford Co. | Molding method for eliminating fiber readout |
US5084353A (en) * | 1989-05-12 | 1992-01-28 | Gencorp Inc. | Thermosetting in-mold coating compositions |
US5580621A (en) * | 1990-04-30 | 1996-12-03 | American Standard Inc. | Polyester backed acrylic composite molded structure and method of manufacturing thereof |
US5100935A (en) * | 1990-07-19 | 1992-03-31 | The Budd Company | Flexible sheet molding compound and method of making the same |
US5362819A (en) * | 1992-01-30 | 1994-11-08 | Gencorp Inc. | Polyester-flexible polymer block copolymers and mixtures thereof |
WO1993023236A1 (en) * | 1992-05-12 | 1993-11-25 | American Standard Inc. | Polyester backed acrylic composite molded structure and method of manufacturing thereof |
US5358779A (en) * | 1992-06-26 | 1994-10-25 | Gencorp Inc. | Enhanced surface appearance of glass fiber reinforced plastics (FRP) |
US5427725A (en) * | 1993-05-07 | 1995-06-27 | The Dow Chemical Company | Process for resin transfer molding and preform used in the process |
TW297046B (ja) * | 1993-06-15 | 1997-02-01 | Dow Chemical Co | |
US5993906A (en) * | 1993-06-23 | 1999-11-30 | Cambridge Industries, Inc. | Edge seal process and product |
DE69403757T2 (de) * | 1993-11-22 | 1997-12-11 | Michelin & Cie | Verfahren zur Herstellung von formgepressten Verbundstoffteilen |
EP0737124B1 (en) * | 1994-10-28 | 2000-08-23 | The Dow Chemical Company | Improved process for resin transfer molding |
US6048488A (en) * | 1997-04-04 | 2000-04-11 | The United States Of America As Represented By The Secretary Of The Army | One-step resin transfer molding of multifunctional composites consisting of multiple resins |
US7727436B2 (en) * | 1998-03-05 | 2010-06-01 | Omnova Solutions Inc. | Coating derived from polyesters crosslinked with melamine formaldehyde |
BR9802274C1 (pt) * | 1998-06-19 | 2002-03-26 | Luciano Alfredo Fusco | Processo contìnuo de fabricação de laminados decorativos plásticos para finalidades diversas e produto resultante |
JP4342620B2 (ja) * | 1998-12-02 | 2009-10-14 | 富士重工業株式会社 | ハニカムサンドイッチ構造複合材パネルの成形方法 |
JP4586278B2 (ja) * | 2000-03-06 | 2010-11-24 | 東レ株式会社 | Frp製板材 |
US6740185B2 (en) * | 2001-02-06 | 2004-05-25 | General Electric Company | Method of preparing preforms for RTM molding processes |
CA2446416A1 (en) * | 2001-05-08 | 2002-11-14 | Michael Jewett | System and method of making an in-mold clear-coated composite |
JP3894035B2 (ja) * | 2001-07-04 | 2007-03-14 | 東レ株式会社 | 炭素繊維強化基材、それからなるプリフォームおよび複合材料 |
ES2596505T3 (es) * | 2001-08-07 | 2017-01-10 | Toray Industries, Inc. | Procedimiento para la fabricación de un elemento de PRF grande |
US7059665B2 (en) * | 2001-08-28 | 2006-06-13 | Toray Industries, Inc. | CFRP plate material and method for preparation thereof |
US7105231B2 (en) * | 2001-10-22 | 2006-09-12 | Omnova Solutions Inc. | In-mold coating barrier for a substrate injection orifice |
DE10228649A1 (de) * | 2002-06-26 | 2004-01-22 | Bakelite Ag | Verfahren zur Herstellung eines faserverstärkten Produktes auf Epoxidharzbasis |
AU2003262050B2 (en) * | 2002-11-14 | 2009-07-02 | Toray Industries, Inc. | Reinforcing fiber substrate, composite material and method for producing the same |
JP2004249585A (ja) * | 2003-02-20 | 2004-09-09 | Toray Ind Inc | 繊維強化プラスチック成形体およびその製造方法 |
US7431789B2 (en) * | 2003-07-15 | 2008-10-07 | Vrac, Llc | Covalently compatible in-mold coating compositions for use with epoxy |
EP1656429B1 (en) * | 2003-07-22 | 2008-02-20 | Omnova Solutions Inc. | Base-coat in-mold coating |
US20050051920A1 (en) * | 2003-09-04 | 2005-03-10 | Joel Thomson | Methods and devices for in-mold printing on molded parts |
US20050194713A1 (en) * | 2003-12-29 | 2005-09-08 | John Erickson | Method of making a molded article |
WO2005077632A1 (ja) * | 2004-02-17 | 2005-08-25 | Toray Industries, Inc. | Rtm成形方法および装置 |
WO2005095079A1 (ja) * | 2004-03-30 | 2005-10-13 | Toray Industries, Inc. | プリフォーム、frpおよびそれらの製造方法 |
JP4774839B2 (ja) * | 2004-07-08 | 2011-09-14 | 東レ株式会社 | 繊維強化複合材料の製造方法 |
US9884976B1 (en) * | 2004-08-19 | 2018-02-06 | Red Spot Paint & Varnish Co., Inc. | Coating compositions and methods, and articles coated with same |
US8257823B2 (en) * | 2004-12-06 | 2012-09-04 | Toray Industries, Inc. | Molding precursor, process for producing molded fiber-reinforced resin, and molded fiber-reinforced resin |
CA2606808C (en) * | 2005-05-03 | 2013-09-17 | Stork Sp Aerospace B.V. | Device for injecting a resin into at least one fibre layer of a fibre- reinforced product to be manufactured |
WO2007013204A1 (ja) * | 2005-07-29 | 2007-02-01 | Toray Industries, Inc. | 強化繊維織物とその製造方法 |
WO2007102395A1 (ja) * | 2006-03-08 | 2007-09-13 | Toray Industries, Inc. | 繊維強化樹脂の製造方法 |
US8993462B2 (en) * | 2006-04-12 | 2015-03-31 | James Hardie Technology Limited | Surface sealed reinforced building element |
US7846366B2 (en) * | 2006-05-18 | 2010-12-07 | Gm Global Technology Operations, Inc. | Method for molding cosmetic composite panels with visible carbon fiber weaves |
US20100178482A1 (en) * | 2006-09-28 | 2010-07-15 | Nitto Denko Corporation | Reinforcing material for vehicle ceiling material |
CN101516589B (zh) * | 2006-09-28 | 2012-06-27 | 东丽株式会社 | 复合预浸料坯基材的制造方法、层合基材及纤维增强塑料 |
US20100086737A1 (en) * | 2007-02-26 | 2010-04-08 | Hexcel Composites Limited | Surface finish for composite materials |
JP5018210B2 (ja) * | 2007-04-26 | 2012-09-05 | 東レ株式会社 | 繊維強化樹脂の製造方法 |
CN102292201B (zh) * | 2009-01-29 | 2014-04-09 | 东丽株式会社 | Rtm成型方法、及纤维增强树脂成型体的制造方法 |
JP5395459B2 (ja) * | 2009-02-25 | 2014-01-22 | 大成プラス株式会社 | 炭素繊維織物シートの樹脂成形体 |
JP4825899B2 (ja) * | 2009-06-22 | 2011-11-30 | トヨタ自動車株式会社 | 繊維強化樹脂の製造方法、繊維強化樹脂の製造装置 |
EP2514587A4 (en) * | 2009-12-17 | 2017-01-11 | Toray Industries, Inc. | Layered carbon-fiber product, preform, and processes for producing these |
JP6253979B2 (ja) * | 2010-04-13 | 2017-12-27 | ヘンケル アイピー アンド ホールディング ゲゼルシャフト ミット ベシュレンクテル ハフツング | 硬化性組成物、複合材製造のための前記組成物の使用プロセス、ならびに優れた表面仕上げおよび高い繊維固着を有する複合材の製造プロセス |
JP5545182B2 (ja) * | 2010-11-15 | 2014-07-09 | 日産自動車株式会社 | メタリック塗装方法及び積層塗膜 |
KR101914803B1 (ko) * | 2011-02-25 | 2018-11-02 | 도레이 카부시키가이샤 | Frp의 제조 방법 |
FR2975038B1 (fr) * | 2011-05-10 | 2014-03-07 | Airbus Operations Sas | Procede de fabrication d'une piece en materiau composite et piece ainsi obtenue. |
JP5791365B2 (ja) * | 2011-05-16 | 2015-10-07 | 三菱重工業株式会社 | Rtm成形方法及びrtm成形装置 |
GB201115724D0 (en) * | 2011-09-12 | 2011-10-26 | Origin Ltd | Methods of manufacturing plastic articles |
CN103842172A (zh) * | 2011-09-28 | 2014-06-04 | 住友电木株式会社 | 透明复合基板和显示元件基板 |
JP5682838B2 (ja) * | 2011-11-29 | 2015-03-11 | 三菱レイヨン株式会社 | エポキシ樹脂組成物、プリプレグ、繊維強化複合材料とその製造方法 |
CN104781303B (zh) * | 2012-11-13 | 2017-11-10 | 陶氏环球技术有限责任公司 | 用于树脂传递模塑方法的含多亚乙基四胺的环氧树脂体系 |
WO2014160506A2 (en) * | 2013-03-13 | 2014-10-02 | Cubic Tech Corporation | Systems and method for producing three-dimensional articles from flexible composite materials |
JP6354758B2 (ja) * | 2013-07-26 | 2018-07-11 | 旭硝子株式会社 | 繊維強化樹脂シートおよびその製造方法 |
PT2875937T (pt) * | 2013-11-22 | 2021-04-30 | Vitrulan Composites Oy | Um reforço unidirecional, método de produzir um reforço unidirecional e a sua utilização |
TW201527065A (zh) * | 2013-12-19 | 2015-07-16 | Proto Co Ltd | 熱硬化性樹脂成形品及其製造方法 |
-
2015
- 2015-01-16 WO PCT/JP2015/000175 patent/WO2015107903A1/ja active Application Filing
- 2015-01-16 CN CN201580002777.4A patent/CN105829046B/zh not_active Expired - Fee Related
- 2015-01-16 EP EP15737301.0A patent/EP3095577B1/en active Active
- 2015-01-16 US US15/039,345 patent/US20170157804A1/en not_active Abandoned
- 2015-01-16 KR KR1020167013980A patent/KR102231918B1/ko active IP Right Grant
- 2015-01-16 JP JP2015514260A patent/JP6094668B2/ja not_active Expired - Fee Related
-
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- 2017-02-16 JP JP2017026505A patent/JP2017109502A/ja active Pending
-
2020
- 2020-04-27 US US16/859,283 patent/US20200254654A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07223231A (ja) * | 1994-02-15 | 1995-08-22 | Sekisui Chem Co Ltd | 型内被覆成形品の製造方法 |
JP2008143077A (ja) * | 2006-12-12 | 2008-06-26 | Toyota Auto Body Co Ltd | 型内被覆成形方法及び型内被覆成形品 |
JP2013209510A (ja) | 2012-03-30 | 2013-10-10 | Dainippon Toryo Co Ltd | 繊維強化樹脂成形体被覆組成物、該被覆組成物を塗装して得られる繊維強化樹脂成形体及び該繊維強化樹脂成形体の製造方法 |
Non-Patent Citations (1)
Title |
---|
See also references of EP3095577A4 |
Cited By (11)
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JP2017075225A (ja) * | 2015-10-14 | 2017-04-20 | 住友ゴム工業株式会社 | タイヤ |
WO2019013025A1 (ja) * | 2017-07-13 | 2019-01-17 | 東レ株式会社 | 成形品およびその製造方法 |
JPWO2019013025A1 (ja) * | 2017-07-13 | 2020-05-07 | 東レ株式会社 | 成形品およびその製造方法 |
JP7215170B2 (ja) | 2017-07-13 | 2023-01-31 | 東レ株式会社 | 自動車の外装部材用成形品およびその製造方法 |
WO2019054074A1 (ja) * | 2017-09-15 | 2019-03-21 | ウシオ電機株式会社 | 炭素繊維強化プラスチック構造体および加工装置 |
JP2019051653A (ja) * | 2017-09-15 | 2019-04-04 | ウシオ電機株式会社 | 炭素繊維強化プラスチック構造体および加工装置 |
US11701868B2 (en) | 2017-09-15 | 2023-07-18 | Ushio Denki Kabushiki Kaisha | Carbon fiber reinforced plastic structure and processing apparatus |
JP2019098631A (ja) * | 2017-12-04 | 2019-06-24 | 株式会社Subaru | 繊維強化樹脂体及びその製造方法 |
US10828850B2 (en) | 2017-12-04 | 2020-11-10 | Subaru Corporation | Fiber-reinforced plastic and method of producing the fiber-reinforced plastic |
JP2019171241A (ja) * | 2018-03-27 | 2019-10-10 | マツダ株式会社 | 繊維強化樹脂成形品の塗装方法及びその塗装製品 |
JP7159585B2 (ja) | 2018-03-27 | 2022-10-25 | マツダ株式会社 | 繊維強化樹脂成形品の塗装方法 |
Also Published As
Publication number | Publication date |
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CN105829046A (zh) | 2016-08-03 |
JP6094668B2 (ja) | 2017-03-15 |
EP3095577A1 (en) | 2016-11-23 |
JPWO2015107903A1 (ja) | 2017-03-23 |
US20170157804A1 (en) | 2017-06-08 |
KR102231918B1 (ko) | 2021-03-25 |
EP3095577A4 (en) | 2018-01-10 |
US20200254654A1 (en) | 2020-08-13 |
KR20160108304A (ko) | 2016-09-19 |
EP3095577B1 (en) | 2023-07-26 |
JP2017109502A (ja) | 2017-06-22 |
CN105829046B (zh) | 2018-05-04 |
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