JP2018079630A - Carbon fiber composite decorative plate - Google Patents

Carbon fiber composite decorative plate Download PDF

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JP2018079630A
JP2018079630A JP2016223909A JP2016223909A JP2018079630A JP 2018079630 A JP2018079630 A JP 2018079630A JP 2016223909 A JP2016223909 A JP 2016223909A JP 2016223909 A JP2016223909 A JP 2016223909A JP 2018079630 A JP2018079630 A JP 2018079630A
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carbon fiber
composite decorative
fiber composite
decorative board
phenol resin
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JP6847510B2 (en
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中村 優
Yu Nakamura
優 中村
尚幸 田辺
Naoyuki Tanabe
尚幸 田辺
杉浦 好典
Yoshinori Sugiura
好典 杉浦
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Inoac Corp
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Inoue MTP KK
Inoac Corp
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Abstract

PROBLEM TO BE SOLVED: To provide a carbon fiber composite decorative plate which is excellent in incombustibility, has good shaping of three-dimensional bending shape, and is lightweight.SOLUTION: There are provided carbon fiber composite decorative plates 10A and 10B in which a core material 11 where a melamine resin foam having open cells is impregnated with a phenol resin and the phenol resin is cured in a compressive state of the melamine resin foam, a fiber reinforcement material 21 where a carbon fiber fabric is impregnated with the phenol resin and the phenol resin is cured, and a face material 31 formed of a woven cloth formed of a heat-resistant log fiber yarn coated with a fluororesin are laminated and integrated, where a resin ratio specified by resin ratio={(weight of melamine resin foam+weight of phenol resin in carbon fiber composite decorative plate)÷(weight of carbon fiber composite decorative plate excluding weight of face material)}×100 is 40-70%.SELECTED DRAWING: Figure 3

Description

本発明は、三次元的な曲げ形状の賦形が良好な炭素繊維複合化粧板に関する。   The present invention relates to a carbon fiber composite decorative board having a good three-dimensional bent shape.

従来、鉄道車両などの車両用部材には、軽量化の要求から、内装材などにはガラス繊維や炭素繊維などを用いた繊維強化複合材料(FRP)の成形体が部分的に採用されている。さらに、車両用部材は、使用部位によっては三次元的な曲げ形状に賦形されたものが必要な場合があり、その場合には三次元的な曲げ形状部の表面に美観低下を生じないものが求められる。また、車両用部材には、不燃性及び軽量性も求められる。   Conventionally, molded articles of fiber reinforced composite materials (FRP) using glass fibers, carbon fibers, etc. have been partially used for interior parts, etc., for vehicle members such as railway vehicles, because of the demand for weight reduction. . Furthermore, depending on the use part, the vehicle member may need to be shaped into a three-dimensional bent shape, in which case the appearance of the surface of the three-dimensional bent shape portion does not deteriorate. Is required. In addition, the vehicle member is also required to be nonflammable and lightweight.

特許文献1には、表面化粧層及び芯材層を有するメラミン樹脂層と、接着剤層と、金属層がこの順に積層されたメラミン樹脂金属化粧板について、JIS K 6902の曲げ成形性試験(A法)を行った実施例が記載されている。   In Patent Document 1, a melamine resin metal decorative plate in which a melamine resin layer having a surface decorative layer and a core material layer, an adhesive layer, and a metal layer are laminated in this order is subjected to a bending formability test of JIS K 6902 (A Example of performing the method) is described.

特許文献2には、金属板の両表面に熱硬化性樹脂を含浸した繊維基材を重ね、更にそれぞれの表面にメラミン樹脂を含浸した繊維基材を重ね、加熱加圧成形した金属コア両面化粧板において、両表面のメラミン樹脂含浸繊維基材の一方又は両方に、ポリエステル繊維等の有機又は無機繊維不織布を使用したものについて、JIS K 6902による耐屈曲性を測定した実施例が記載されている。   Patent Document 2 discloses a metal core double-sided cosmetic that is formed by superimposing a fiber base material impregnated with a thermosetting resin on both surfaces of a metal plate, and further superimposing a fiber base material impregnated with a melamine resin on each surface, followed by heat and pressure molding. The example which measured the bending resistance by JISK6902 about what used organic or inorganic fiber nonwoven fabrics, such as polyester fiber, for one or both of the melamine resin impregnation fiber base materials of both surfaces in a board is indicated. .

しかしながら、特許文献1及び特許文献2に記載されているJIS K 6902の曲げ成形性試験(A法)では、V字形の溝が形成された治具上に配置した試験体を、溝の上方から押して折り曲げているため、試験体の屈曲する部分が一箇所となり、二次元的な曲げが判断できるだけであって、実用的に求められる三次元的な曲げに対して判断することができなかった。   However, in the bending formability test (Method A) of JIS K 6902 described in Patent Document 1 and Patent Document 2, a specimen placed on a jig in which a V-shaped groove is formed is viewed from above the groove. Since it was pushed and bent, the bending portion of the test specimen became one place, and it was only possible to determine two-dimensional bending, and it was not possible to determine the practically required three-dimensional bending.

特開2014−208453号公報JP 2014-208453 A 特開平07−266497号公報Japanese Patent Application Laid-Open No. 07-266497

本発明は前記の点に鑑みなされたものであって、不燃性に優れ、かつ三次元的な曲げ形状の賦形が良好で、かつ軽量な炭素繊維複合化粧板の提供を目的とする。   This invention is made | formed in view of the said point, Comprising: It aims at provision of the carbon fiber composite decorative board which is excellent in nonflammability, is good in the shaping of a three-dimensional bending shape, and is lightweight.

請求項1の発明は、芯材と、前記芯材の両面に積層された繊維補強材と、前記両面の繊維補強材の少なくとも一方の繊維補強材の表面に積層された面材とからなる炭素繊維複合化粧板において、前記芯材は、連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸して前記メラミン樹脂発泡体の圧縮状態で前記フェノール樹脂が硬化したものであり、前記繊維補強材は、炭素繊維織物にフェノール樹脂が含浸硬化したものからなり、前記面材は、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布であり、前記芯材は一つの層を形成しており、前記芯材と前記繊維補強材と前記面材は、前記芯材のメラミン樹脂発泡体に含浸したフェノール樹脂と、前記繊維補強材の炭素繊維織物に含浸したフェノール樹脂の硬化によって接着しており、樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100で規定される樹脂比率が40〜70%であることを特徴とする。なお、請求項1の発明は、上記式で示される樹脂比率を40〜70%とするフェノール樹脂を接着剤として、圧縮成形時に積層部材が一体に賦形加工される炭素繊維複合化粧板である。この一体に賦形加工される際に、上記メラミン樹脂発泡体からなる芯材が圧縮されるとともに前記フェノール樹脂である接着剤が前記芯材との接着層を形成する工程を含み、かつ、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布である面材も前記接着剤が積層硬化して接着層を形成する工程を含むものである。すなわち、上記複数の工程を経た一体成形品では、メラミン樹脂発泡体が圧縮された芯材となって一層を形成する。成形後においては、フェノール樹脂を含浸した上記メラミン樹脂発泡体からなる接着剤を供給する層としての芯材は、もはやその機能を果たしており、請求項1の発明である一体成形品をその成形後の構造で表現したとしても、かかる機能を表現することができない。したがって、請求項1の発明は、その構造又は特性により直接特定することが不可能であり、重合組成物を得るためのプロセス(製法)によって初めて特定することが可能なものである。   The invention of claim 1 is a carbon comprising a core material, a fiber reinforcing material laminated on both surfaces of the core material, and a face material laminated on the surface of at least one of the fiber reinforcing materials on both surfaces. In the fiber composite decorative board, the core material is obtained by impregnating a melamine resin foam having open cells with a phenol resin and curing the phenol resin in a compressed state of the melamine resin foam. The carbon fiber woven fabric is made by impregnating and curing a phenol resin, the face material is a woven fabric made of heat-resistant long fiber yarn coated with a fluororesin, and the core material forms a single layer. The core material, the fiber reinforcing material, and the face material are bonded by curing the phenol resin impregnated in the melamine resin foam of the core material and the phenol resin impregnated in the carbon fiber fabric of the fiber reinforcing material. , Resin ratio = {(weight of melamine resin foam + weight of phenolic resin in carbon fiber composite decorative board) / (weight of carbon fiber composite decorative board excluding weight of face material)} × 100 Is 40 to 70%. The invention according to claim 1 is a carbon fiber composite decorative board in which a laminated member is integrally shaped during compression molding using a phenol resin having a resin ratio represented by the above formula of 40 to 70% as an adhesive. . When the molding process is integrally performed, the core material made of the melamine resin foam is compressed, and the adhesive that is the phenol resin forms a bonding layer with the core material, and fluorine The face material, which is a woven fabric made of heat-resistant long fiber yarns coated with a resin, also includes a step in which the adhesive is laminated and cured to form an adhesive layer. That is, in the integrally molded product that has undergone the plurality of steps, the melamine resin foam becomes a compressed core material to form one layer. After the molding, the core material as the layer for supplying the adhesive made of the melamine resin foam impregnated with the phenol resin no longer performs the function, and the integrally molded product according to the invention of claim 1 is formed after the molding. Even if expressed in the structure of, such a function cannot be expressed. Therefore, the invention of claim 1 cannot be specified directly by its structure or characteristics, and can be specified for the first time by a process (production method) for obtaining a polymerized composition.

請求項2の発明は、請求項1において、前記芯材の両面に積層された前記繊維補強材のすべての積層枚数は、2枚〜10枚であることを特徴とする。   The invention according to claim 2 is characterized in that, in claim 1, the total number of the fiber reinforcing members laminated on both surfaces of the core material is 2 to 10.

請求項3の発明は、請求項1または2において、前記炭素繊維複合化粧板の破壊荷重(JIS K7074準拠)は100N以上850N以下であり、比重(JIS K7112準拠)は0.50〜1.10であることを特徴とする。   The invention of claim 3 is the invention according to claim 1 or 2, wherein the carbon fiber composite decorative board has a breaking load (in accordance with JIS K7074) of 100 N or more and 850 N or less, and a specific gravity (in accordance with JIS K7112) of 0.50 to 1.10. It is characterized by being.

請求項4の発明は、請求項1から3の何れか一項において、前記炭素繊維複合化粧板には三次元的に賦形された賦形部を有し、前記賦形部の凸部又は凹部の頂部における曲率半径が3mm以上であることを特徴とする。   Invention of Claim 4 has the shaping part shape | molded three-dimensionally in the said carbon fiber composite decorative board in any one of Claim 1 to 3, The convex part of the said shaping part, or The curvature radius at the top of the recess is 3 mm or more.

請求項5の発明は、請求項1から4の何れか一項において、鉄道車両用材料燃焼性試験(国土交通省令第151号に準拠した試験)に不燃合格することを特徴とする。   The invention of claim 5 is characterized in that in any one of claims 1 to 4, the material combustibility test for railway vehicles (a test based on Ordinance No. 151 of the Ministry of Land, Infrastructure, Transport and Tourism) passes nonflammability.

請求項6の発明は、連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸し、前記メラミン樹脂発泡体が圧縮された状態で前記フェノール樹脂が硬化した芯材と、炭素繊維織物にフェノール樹脂が含浸硬化した繊維補強材と、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布で構成された面材とよりなって、前記芯材の両面には前記繊維補強材が一枚以上積層され、前記両面の繊維補強材の少なくとも一方の繊維補強材の表面には前記面材が積層され、前記芯材と前記繊維補強材と前記面材が積層一体化している炭素繊維複合化粧板の製造方法であって、連続気泡を有するメラミン樹脂発泡体と炭素繊維織物の何れか一方または両方にフェノール樹脂を、樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100で規定される樹脂比率が40〜70%の範囲となるように含浸させる含浸工程と、前記含浸工程後に前記メラミン樹脂発泡体の両面に、それぞれ前記炭素繊維織物を複数積層配置し、前記メラミン樹脂発泡体の両面に積層配置された炭素繊維織物の少なくとも一方の炭素繊維織物に面材を積層する積層工程と、前記積層工程で得られた積層体を金型で深絞り成形して三次元的に賦形すると共に、前記積層体を圧縮状態で加熱して前記フェノール樹脂を硬化させ、前記フェノール樹脂の硬化によって前記メラミン樹脂発泡体と前記炭素繊維織物と前記面材を一体化させる深絞り成形工程と、を行うことを特徴とする。   According to the sixth aspect of the present invention, a phenol resin is impregnated with a melamine resin foam having open cells and the phenol resin is cured in a state in which the melamine resin foam is compressed, and the carbon fiber fabric has a phenol resin. It consists of an impregnated and hardened fiber reinforcing material and a face material composed of a woven fabric made of heat-resistant long fiber yarns coated with a fluororesin, and one or more of the fiber reinforcing materials are laminated on both sides of the core material. A carbon fiber composite decorative board in which the face material is laminated on a surface of at least one of the fiber reinforcement materials on both sides, and the core material, the fiber reinforcement material, and the face material are laminated and integrated. In the production method, a phenol resin is added to one or both of a melamine resin foam having an open cell and a carbon fiber fabric, and a resin ratio = {(weight of melamine resin foam + feature in a carbon fiber composite decorative board. Impregnation step of impregnating so that the resin ratio specified by the weight of the carbon resin) ÷ (weight of the carbon fiber composite decorative board excluding the weight of the face material)} × 100 is in the range of 40 to 70%; After the step, a plurality of the carbon fiber fabrics are stacked on both sides of the melamine resin foam, and a face material is stacked on at least one of the carbon fiber fabrics stacked on both sides of the melamine resin foam. A lamination process, and the laminate obtained in the lamination process is deep-drawn with a mold and shaped three-dimensionally, the laminate is heated in a compressed state to cure the phenol resin, and the phenol A deep drawing forming step of integrating the melamine resin foam, the carbon fiber fabric, and the face material by curing the resin is performed.

炭素繊維複合化粧板に関する本発明は、芯材が、連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸してメラミン樹脂発泡体の圧縮状態でフェノール樹脂が硬化したもので芯材を構成し、芯材に積層された繊維補強材を炭素繊維織物にフェノール樹脂が含浸硬化したもので構成し、繊維補強材に積層された面材をフッ素樹脂で被覆された耐熱性長繊維糸からなる織布で構成し、樹脂比率が40〜70%としたことにより、鉄道車両用材料燃焼性試験に不燃合格でき、かつ三次元的な曲げ形状の賦形が良好で、軽量なものにできる。したがって、難燃剤を添加したり、金属部材を使用するといった手段を用いることがなく、不燃合格している。   The present invention relating to a carbon fiber composite decorative board, the core material comprises a core material in which a phenol resin is impregnated with a melamine resin foam having open cells and the phenol resin is cured in a compressed state of the melamine resin foam, A woven fabric composed of heat-resistant long fiber yarns, which are composed of carbon fiber fabrics impregnated and hardened with a phenolic resin, and the face material laminated on the fiber reinforcement material is covered with fluororesin. The resin ratio is 40 to 70%, so that it can pass the nonflammability of the rail vehicle material flammability test, and the three-dimensional bending shape is good and lightweight. Therefore, the flame retardant is passed without using a means such as adding a flame retardant or using a metal member.

炭素繊維複合化粧板の製造方法に関する本発明は、鉄道車両用材料燃焼性試験に不燃合格でき、かつ三次元的な曲げ形状の賦形が良好で、軽量な炭素繊維複合化粧板を製造することができる。   The present invention relating to a method for producing a carbon fiber composite decorative board is to produce a lightweight carbon fiber composite decorative board that can pass the non-combustibility of the material flammability test for railway vehicles and has good three-dimensional bending shape shaping. Can do.

本発明における炭素繊維複合化粧板の第1実施形態の部分斜視図である。It is a fragmentary perspective view of 1st Embodiment of the carbon fiber composite decorative board in this invention. 本発明における炭素繊維複合化粧板の第2実施形態の部分斜視図である。It is a fragmentary perspective view of 2nd Embodiment of the carbon fiber composite decorative board in this invention. 本発明における第1実施形態及び第2実施形態の一部の断面図である。It is partial sectional drawing of 1st Embodiment and 2nd Embodiment in this invention. 本発明における製造方法の一実施形態の工程を示す図である。It is a figure which shows the process of one Embodiment of the manufacturing method in this invention. 実施例及び比較例の構成と外観、弾性率、破壊荷重、燃焼性試験及び比重の結果を示す表である。It is a table | surface which shows the result of the structure and external appearance of an Example and a comparative example, an elasticity modulus, a fracture load, a flammability test, and specific gravity.

以下、本発明の炭素繊維複合化粧板及びその製造方法について図面を用いて説明する。
図1に示す本発明の第1実施形態に係る炭素繊維複合化粧板10Aは、図3に示すように芯材11と、前記芯材11の両面に積層一体化された2層の繊維補強材21、21と、最外層の繊維補強材21の表面に積層一体化された面材31とよりなり、三次元的に賦形された賦形部11Aを有する。前記賦形部11Aは、凸形状側が意匠面側(図1参照)とされ、反対の凹形状側が裏面側となっている。
Hereinafter, the carbon fiber composite decorative board and the manufacturing method thereof of the present invention will be described with reference to the drawings.
A carbon fiber composite decorative board 10A according to the first embodiment of the present invention shown in FIG. 1 includes a core material 11 and two layers of fiber reinforcement laminated and integrated on both surfaces of the core material 11 as shown in FIG. 21 and 21 and a face material 31 laminated and integrated on the surface of the outermost fiber reinforcing material 21, and has a shaped portion 11A shaped three-dimensionally. In the shaping portion 11A, the convex shape side is the design surface side (see FIG. 1), and the opposite concave shape side is the back surface side.

図2に示す本発明の第2実施形態に係る炭素繊維複合化粧板10Bは、図3に示すように芯材11と、前記芯材11の両面に積層一体化された2層の繊維補強材21、21と、最外層の繊維補強材21の表面に積層一体化された面材31とよりなり、三次元的に賦形された賦形部11Bを有する。前記賦形部11Bは、凹形状側が意匠面(図2参照)とされ、反対の凸形状側が裏面となっている。   A carbon fiber composite decorative board 10B according to the second embodiment of the present invention shown in FIG. 2 includes a core material 11 and two layers of fiber reinforcement laminated and integrated on both surfaces of the core material 11 as shown in FIG. 21 and 21 and a face material 31 laminated and integrated on the surface of the outermost fiber reinforcing material 21, and has a shaped part 11B shaped three-dimensionally. In the shaping portion 11B, the concave shape side is a design surface (see FIG. 2), and the opposite convex shape side is a back surface.

前記第1実施形態の炭素繊維複合化粧板10A及び第2実施形態の炭素繊維複合化粧板10Bは、鉄道車両用の部材として好適なものである。鉄道車両用の部材としては、天井材、内張り材(壁材等)、窓枠材等が挙げられる。   The carbon fiber composite decorative board 10A of the first embodiment and the carbon fiber composite decorative board 10B of the second embodiment are suitable as members for railway vehicles. As a member for rail vehicles, ceiling materials, lining materials (wall materials, etc.), window frame materials, and the like can be given.

前記芯材11は、一層で構成されており、連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸して前記メラミン樹脂発泡体の圧縮状態でフェノール樹脂が硬化したものである。前記芯材11は、一枚でもよく、複数枚の連続気泡を有するメラミン樹脂発泡体を積層して一層を構成しても良い。前記メラミン樹脂発泡体は樹脂単体が良好な難燃性を有するため、前記芯材11の構成材として好適なものである。前記メラミン樹脂発泡体の圧縮前の元厚みは、前記炭素繊維複合化粧板10A、10Bの厚みにより異なるが、例えば3〜50mmを挙げる。また、前記メラミン樹脂発泡体は、圧縮容易性、含浸性、軽量性、剛性の点から、圧縮前の密度が5〜15kg/mのものが好ましい。 The core material 11 is composed of a single layer, and is obtained by impregnating a melamine resin foam having open cells with a phenol resin and curing the phenol resin in a compressed state of the melamine resin foam. The core material 11 may be a single sheet or a single layer formed by laminating a plurality of melamine resin foams having open cells. The melamine resin foam is suitable as a constituent material of the core material 11 because the resin alone has good flame retardancy. Although the original thickness before compression of the said melamine resin foam changes with thickness of the said carbon fiber composite decorative board 10A, 10B, 3-50 mm is mentioned, for example. The melamine resin foam preferably has a density before compression of 5 to 15 kg / m 3 from the viewpoints of easy compression, impregnation, light weight, and rigidity.

前記繊維補強材21は、炭素繊維織物にフェノール樹脂が含浸して硬化したものからなる。
前記炭素繊維織物は、軽量及び強度、高剛性に優れるものであり、特に、繊維が一方向のみではない織り方のものが好ましく、例えば、縦糸と横糸で構成される平織、綾織、朱子織及び3方向の糸で構成される三軸織および開繊糸を織って得られる上記織物などが好適である。また、前記炭素繊維織物は、フェノール樹脂の含浸及び剛性、強度の点から、繊維重さが90〜400g/mのものが好ましい。前記繊維補強材21を構成する炭素繊維織物は、前記芯材11の両面にそれぞれ1層以上積層されていればよい。積層数を多くし過ぎると炭素繊維複合化粧板が重くなったり、三次元形状の良好な成形が難しくなったりするため、より好ましい積層数は2層から10層である。また、積層数は前記芯材11の両面で等しくするのが、前記炭素繊維複合化粧板10の剛性、強度向上、難燃性、成形後の経時的な変形を防止する点で好ましい。
The fiber reinforcing material 21 is made of a carbon fiber woven fabric impregnated with a phenol resin and cured.
The carbon fiber woven fabric is excellent in light weight, strength, and high rigidity, and in particular, a weaving method in which the fibers are not only in one direction is preferable, for example, a plain weave, a twill weave, a satin weave composed of warp and weft The above-described woven fabric obtained by weaving a triaxial weave composed of three-direction yarns and a spread yarn is preferable. The carbon fiber fabric preferably has a fiber weight of 90 to 400 g / m 2 in view of impregnation with phenol resin, rigidity, and strength. The carbon fiber fabric constituting the fiber reinforcing material 21 may be laminated on one or more layers on both surfaces of the core material 11. If the number of laminated layers is increased too much, the carbon fiber composite decorative board becomes heavy and it is difficult to form a good three-dimensional shape. Therefore, the more preferable number of laminated layers is 2 to 10. Further, it is preferable that the number of laminated layers is equal on both surfaces of the core material 11 in terms of preventing rigidity and strength of the carbon fiber composite decorative board 10, improving flame retardancy, and deformation over time after molding.

前記メラミン樹脂発泡体及び前記炭素繊維織物に含浸するフェノール樹脂は、含浸後の硬化によって前記炭素繊維複合化粧板10の剛性及び強度、難燃性を高める。   The phenol resin impregnated in the melamine resin foam and the carbon fiber fabric enhances the rigidity and strength of the carbon fiber composite decorative board 10 and flame retardancy by curing after impregnation.

前記面材31は、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布で構成される。
耐熱性長繊維糸は、耐熱性長繊維が糸状とされたものである。また耐熱性長繊維としては、ポリイミド繊維、芳香族系ポリアミド繊維、炭素繊維、グラファイト化繊維、耐炎化繊維などを挙げることができる。なお、耐熱性長繊維は一種類に限られず、複数種類が組み合わされてもよい。
フッ素樹脂は、ポリテトラフロロエチレン樹脂、テトラフロロエチレン−ヘキサフロロプロピレン共重合体、テトラフロロエチレン−パーフロロビニルエーテル共重合体、ポリフッ化ビニリデン、エチレン−テトラフロロエチレン共重合体、エチレン−クロロトリフロロエチレン共重合体などを挙げることができる。
The face material 31 is composed of a woven fabric made of heat-resistant long fiber yarns coated with a fluororesin.
The heat-resistant long fiber yarn is obtained by forming a heat-resistant long fiber into a yarn shape. Examples of the heat-resistant long fibers include polyimide fibers, aromatic polyamide fibers, carbon fibers, graphitized fibers, and flame-resistant fibers. The heat-resistant long fiber is not limited to one type, and a plurality of types may be combined.
Fluororesin is composed of polytetrafluoroethylene resin, tetrafluoroethylene-hexafluoropropylene copolymer, tetrafluoroethylene-perfluorovinyl ether copolymer, polyvinylidene fluoride, ethylene-tetrafluoroethylene copolymer, ethylene-chlorotrifluoro. An ethylene copolymer etc. can be mentioned.

実施例として、炭素繊維複合化粧板の両側に、前記面材31が設けられる実施形態を示したが、筐体もしくは車両等の内装材等に用いられる場合、炭素繊維複合化粧板の片側のみに設けられる実施形態(図示せず)も多くある。また、前記面材31が炭素繊維複合化粧板の片側のみに設ける場合は、意匠面側に設けられる。   As an example, an embodiment in which the face material 31 is provided on both sides of a carbon fiber composite decorative board is shown, but when used as an interior material of a housing or a vehicle, etc., only on one side of the carbon fiber composite decorative board. There are many embodiments (not shown) provided. Moreover, when the said face material 31 is provided only in the one side of a carbon fiber composite decorative board, it is provided in the design surface side.

前記芯材11と前記繊維補強材21と前記面材31は、前記芯材11のメラミン樹脂発泡体に含浸したフェノール樹脂と、前記繊維補強材21の炭素繊維織物に含浸したフェノール樹脂の硬化によって接着している。   The core material 11, the fiber reinforcing material 21, and the face material 31 are formed by curing the phenol resin impregnated in the melamine resin foam of the core material 11 and the phenol resin impregnated in the carbon fiber fabric of the fiber reinforcing material 21. Glued.

前記炭素繊維複合化粧板10A、10Bに含まれるフェノール樹脂は、前記炭素繊維複合化粧板10A、10Bの剛性増加、前記芯材11と前記繊維補強材21と前記面材31の接着一体化、及び不燃性付与の作用がある。前記フェノール樹脂の量は、少なすぎると、剛性、接着一体性が低下するようになり、一方、多すぎると、不燃性試験に合格できないこともあり、前記面材31の織目からフェノール樹脂が浸み出し外観不良ともなる。
フェノール樹脂は、面材を除いた前記芯材11及び積層される前記繊維補強材21からなる積層部分における樹脂比率が、40〜70%となる量が好ましい。
この樹脂比率は、以下の式で示される。樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100。
The phenolic resin contained in the carbon fiber composite decorative boards 10A and 10B increases the rigidity of the carbon fiber composite decorative boards 10A and 10B, and the adhesive integration of the core material 11, the fiber reinforcing material 21, and the face material 31, and Has the effect of imparting incombustibility. If the amount of the phenolic resin is too small, the rigidity and adhesion integrity will decrease. On the other hand, if the amount is too large, the nonflammability test may not pass. It also oozes out and looks bad.
The amount of the phenol resin is preferably such that the resin ratio in the laminated portion including the core material 11 excluding the face material and the laminated fiber reinforcing material 21 is 40 to 70%.
This resin ratio is shown by the following formula. Resin ratio = {(weight of melamine resin foam + weight of phenol resin in carbon fiber composite decorative board) / (weight of carbon fiber composite decorative board excluding weight of face material)} × 100.

前記三次元的に賦形された賦形部11A、11Bは、深絞り成形により三次元的に凸形状(炭素繊維複合化粧板10Aの場合)あるいは凹形状(炭素繊維複合化粧板10Bの場合)に賦形されたものであり、凸部の頂部11Aaあるいは凹部の頂部11Bbにおける曲率半径が3mm以上で構成されている。曲率半径を3mm以上とすることにより、前記面材31の前記賦形部11A、11Bの部分に、皺や亀裂などの美観を損なう不具合を生じないようにできる。   The three-dimensionally shaped shaping portions 11A and 11B are three-dimensionally convex (in the case of the carbon fiber composite decorative board 10A) or concave shape (in the case of the carbon fiber composite decorative board 10B) by deep drawing. The curvature radius at the top 11Aa of the convex part or the top part 11Bb of the concave part is 3 mm or more. By setting the radius of curvature to 3 mm or more, it is possible to prevent a problem that impairs the appearance such as wrinkles and cracks in the shaped portions 11A and 11B of the face material 31.

実施形態の前記炭素繊維複合化粧板10A、10Bは、一面が開口した箱状からなり、そのコーナー部(角部)が前記三次元的に賦形された賦形部11A、11Bで構成されている。前記三次元的に賦形された賦形部11A、11Bは、コーナー部の形状に限られず、前記炭素繊維複合化粧板で構成する部材に応じた形状とされる。例えば、平面の一部に形成した半球状の凸部や凹部などでもよい。   The carbon fiber composite decorative boards 10A and 10B according to the embodiment have a box shape with one side opened, and the corner portions (corner portions) are formed by the three-dimensional shaped portions 11A and 11B. Yes. The three-dimensionally shaped shaping portions 11A and 11B are not limited to the shape of the corner portion, but are shaped according to the members formed of the carbon fiber composite decorative board. For example, a hemispherical convex portion or concave portion formed on a part of the plane may be used.

前記炭素繊維複合化粧板10A、10Bは、鉄道車両用材料燃焼性試験(鉄道車両用非金属材料)に不燃合格するものである。本発明は、鉄道車両用材料燃焼性試験のうち、省令83条、2.旅客車、客室内張に該当し、一般旅客車、地下鉄等旅客車及び新幹線旅客車、特殊鉄道に使用できる。
また、前記炭素繊維複合化粧板10A、10Bは、鉄道車両用部材としての強度を保持させるため、弾性率(JIS K7074−1988 A法)が10GPa以上、破壊荷重(JIS K7074準拠)が100N以上850N以下であるのが好ましい。かつ軽量性のために比重(JIS K7112準拠)は0.50〜1.10程度が好ましい。すなわち、比重に対する破壊荷重である比強度を、[比強度=破壊荷重÷比重]で計算した。比強度は、100〜1015が好ましい。
The carbon fiber composite decorative boards 10A and 10B pass the nonflammability of the railway vehicle material flammability test (non-metallic material for railway vehicles). The present invention relates to a ministerial ordinance Article 83, 2. Applicable to passenger cars and passenger linings, and can be used for passenger cars such as ordinary passenger cars, subways, Shinkansen passenger cars, and special railways.
Further, the carbon fiber composite decorative boards 10A and 10B have a modulus of elasticity (JIS K7074-1988 A method) of 10 GPa or more and a breaking load (JIS K7074 conformity) of 100 N or more and 850 N in order to maintain the strength as a railcar member. It is preferable that: In addition, the specific gravity (conforming to JIS K7112) is preferably about 0.50 to 1.10. That is, the specific strength which is the breaking load with respect to the specific gravity was calculated by [specific strength = breaking load / specific gravity]. The specific strength is preferably 100 to 1015.

本発明の炭素繊維複合化粧板の製造方法について説明する。炭素繊維複合化粧板の製造方法は、含浸工程、積層工程、深絞り成形工程とからなる。
含浸工程では、連続気泡を有するメラミン樹脂発泡体と炭素繊維織物の何れか一方または両方にフェノール樹脂を含浸させる。フェノール樹脂を、芯材及び繊維補強材の全体に効率的に含浸させるには、メラミン樹脂発泡体と炭素繊維織物の両方にフェノール樹脂を含浸させるのが好ましい。以下の例では、メラミン樹脂発泡体と炭素繊維織物の両方にフェノール樹脂を含浸させる場合について示す。また、使用するメラミン樹脂発泡体は、圧縮容易性、含浸性、軽量性、剛性の点から、厚み(圧縮する前の厚み)が3〜50mm、密度(圧縮前の密度)が5〜15kg/mのものが好ましい。
The manufacturing method of the carbon fiber composite decorative board of the present invention will be described. The method for producing a carbon fiber composite decorative board includes an impregnation process, a lamination process, and a deep drawing process.
In the impregnation step, one or both of the melamine resin foam and carbon fiber fabric having open cells are impregnated with the phenol resin. In order to efficiently impregnate the entire core material and fiber reinforcing material with the phenol resin, it is preferable to impregnate both the melamine resin foam and the carbon fiber fabric with the phenol resin. In the following example, a case where both a melamine resin foam and a carbon fiber fabric are impregnated with a phenol resin is shown. Moreover, the melamine resin foam to be used has a thickness (thickness before compression) of 3 to 50 mm and a density (density before compression) of 5 to 15 kg / in terms of ease of compression, impregnation, lightness, and rigidity. Those of m 3 are preferred.

図4に示す(4−1)のように、含浸工程は含浸工程Aと含浸工程Bの2種類からなる。
含浸工程Aでは、連続気泡を有するメラミン樹脂発泡体110Aにフェノール樹脂110Bを含浸させ、含浸済みメラミン樹脂発泡体110Cを得る。
一方、含浸工程Bでは、炭素繊維織物210Aにフェノール樹脂210Bを含浸させ、含浸済み炭素繊維織物210Cを形成する。
As shown in (4-1) shown in FIG. 4, the impregnation step includes two types of impregnation step A and impregnation step B.
In the impregnation step A, the melamine resin foam 110A having open cells is impregnated with the phenol resin 110B to obtain an impregnated melamine resin foam 110C.
On the other hand, in the impregnation step B, the carbon fiber fabric 210A is impregnated with the phenol resin 210B to form the impregnated carbon fiber fabric 210C.

前記炭繊維織物210Aへのフェノール樹脂210Bの含浸作業は、前記芯材110Aの両面に積層する炭素繊維織物の数に応じた枚数の炭素繊維織物に対して行う。前記含浸時のフェノール樹脂110B、210Bは、未硬化の液状からなる。また、含浸を容易にするため、前記フェノール樹脂110B、210Bは溶剤に溶かしたものが好ましく、含浸後に、含浸済みメラミン樹脂発泡体110C及び含浸済み炭素繊維織物210Cを、前記フェノール樹脂の硬化反応を生じない温度で乾燥させることにより、前記含浸済みメラミン樹脂発泡体110C及び前記含浸済み炭素繊維織物210Cから溶剤を除去する。含浸手段は、液状のフェノール樹脂を収容した槽に前記メラミン樹脂発泡体あるいは炭素繊維織物を浸ける方法、スプレーにより行う方法、ロールコータにより行う方法等、適宜の方法により行う。また、フェノール樹脂の含浸量の調節は隙間を適宜調整した二本の絞りローラーに通すことにより行う。隙間を適宜調整した二本の絞りローラーに、フェノール樹脂を含浸した連続気泡を有するメラミン樹脂発泡体及びフェノール樹脂を含浸した炭素繊維織物を通すことにより、余分なフェノール樹脂を絞り取ることができ、更に、フェノール樹脂を、連続気泡を有するメラミン樹脂発泡体及び炭素繊維織物に均一に分散させることができる。
なお、本実施例では、フェノール樹脂を溶剤に溶かした溶剤系で行ったが、フェノール樹脂を水に溶かした水溶系で行ってもよい。
The carbon fiber woven fabric 210A is impregnated with the phenol resin 210B on the number of carbon fiber woven fabrics corresponding to the number of carbon fiber woven fabrics laminated on both surfaces of the core material 110A. The phenol resins 110B and 210B at the time of impregnation are made of an uncured liquid. In order to facilitate impregnation, the phenol resins 110B and 210B are preferably dissolved in a solvent. After impregnation, the impregnated melamine resin foam 110C and the impregnated carbon fiber fabric 210C are subjected to a curing reaction of the phenol resin. By drying at a temperature that does not occur, the solvent is removed from the impregnated melamine resin foam 110C and the impregnated carbon fiber fabric 210C. The impregnation means is performed by an appropriate method such as a method of immersing the melamine resin foam or carbon fiber fabric in a tank containing a liquid phenolic resin, a method of spraying, or a method of using a roll coater. The amount of phenol resin impregnated is adjusted by passing it through two squeezing rollers with gaps appropriately adjusted. Excess phenolic resin can be squeezed by passing a melamine resin foam having open cells impregnated with phenolic resin and a carbon fiber fabric impregnated with phenolic resin through two squeezing rollers with appropriate adjustment of the gap, Furthermore, the phenol resin can be uniformly dispersed in the melamine resin foam having an open cell and the carbon fiber fabric.
In this embodiment, the solvent system is obtained by dissolving a phenol resin in a solvent, but it may be performed in a water system in which a phenol resin is dissolved in water.

前記メラミン樹脂発泡体110Aへのフェノール樹脂110Bの含浸と、前記炭素繊維織物210Aへのフェノール樹脂210Bの含浸は、樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100で規定される樹脂比率が、40〜70%となるように行われる。具体的には、含浸前のメラミン樹脂発泡体の重量、含浸前の炭素繊維織物全体(全積層数)の重量、含浸後(乾燥後)のメラミン樹脂発泡体の重量、含浸後(乾燥後)の炭素繊維織物全体(全積層数)の重量、及び面材の重量を測定し、測定値を用いて前記の樹脂比率を算出し、前記樹脂比率が40〜70%となるように調整して炭素繊維複合化粧板の製造を行う。なお、樹脂比率の式における炭素繊維複合化粧板中のフェノール樹脂の重量は、[面材の目付量から換算できる面材の重量を除いた含浸後(乾燥後)の炭素繊維織物全体(全積層数)重量−含浸前の炭素繊維織物全体(全積層数)の重量]によって算出することができ、また、炭素繊維複合化粧板の重量は、炭素繊維複合化粧板を計測後、面材の目付量から換算できる面材の重量を除いた重量である。   The impregnation of the melamine resin foam 110A with the phenol resin 110B and the impregnation of the carbon fiber fabric 210A with the phenol resin 210B are as follows: Resin ratio = {(Melamine resin foam weight + phenol resin in the carbon fiber composite decorative board ) (Weight of carbon fiber composite decorative board excluding weight of face material)} × 100, the resin ratio specified is 40 to 70%. Specifically, the weight of the melamine resin foam before impregnation, the weight of the entire carbon fiber fabric (total number of laminated layers) before impregnation, the weight of the melamine resin foam after impregnation (after drying), and after the impregnation (after drying) Measure the weight of the entire carbon fiber fabric (total number of layers) and the weight of the face material, calculate the resin ratio using the measured values, and adjust the resin ratio to be 40 to 70%. Manufacture of carbon fiber composite decorative board. In addition, the weight of the phenol resin in the carbon fiber composite decorative board in the formula of the resin ratio is [the entire carbon fiber fabric after impregnation (after drying) excluding the weight of the face material that can be converted from the basis weight of the face material (total lamination) Number) weight-weight of the entire carbon fiber fabric before impregnation (total number of laminated layers)], and the weight of the carbon fiber composite decorative board is measured after measuring the carbon fiber composite decorative board. It is the weight excluding the weight of the face material that can be converted from the amount.

図4に示す(4−2)の積層工程では、前記含浸済みメラミン樹脂発泡体110Cの両面に、前記含浸済み炭素繊維織物210Cを複数枚積層配置し、さらに最外層の前記含浸済み炭素繊維織物210Cの表面に面材310Cを積層して積層体100Cとする。前記含浸済み炭素繊維織物210Cの積層枚数は、前記含浸済みメラミン樹脂発泡体110Cの両面で等しくされる。また、前記面材310Cは、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布で構成されている。前記面材310Cを、片面のみに設ける場合には、前記含浸済みメラミン樹脂発泡体110Cの片面側の含浸済み炭素繊維織物210Cの最外層の表面のみに面材310Cを積層する。前記含浸済みメラミン樹脂発泡体110Cと前記含浸済み炭素繊維織物210C及び前記面材310Cは、平面サイズが同サイズのものが好ましいが、異なっていている場合には、後述の深絞り成形工程後、最終的にトリミングする。   In the laminating step (4-2) shown in FIG. 4, a plurality of impregnated carbon fiber fabrics 210C are laminated on both surfaces of the impregnated melamine resin foam 110C, and the impregnated carbon fiber fabric of the outermost layer is further disposed. A face material 310C is laminated on the surface of 210C to form a laminate 100C. The number of layers of the impregnated carbon fiber fabric 210C is equalized on both surfaces of the impregnated melamine resin foam 110C. The face material 310C is made of a woven fabric made of heat-resistant long fiber yarns coated with a fluororesin. When the face material 310C is provided only on one side, the face material 310C is laminated only on the surface of the outermost layer of the impregnated carbon fiber fabric 210C on one side of the impregnated melamine resin foam 110C. The impregnated melamine resin foam 110C, the impregnated carbon fiber woven fabric 210C and the face material 310C preferably have the same plane size, but if they are different, after the deep drawing process described later, Final trimming.

図4に示す(4−3)の深絞り成形工程では、前記積層体100Cをプレス成形用金型の下型41と上型43により、深絞り成形して三次元的に賦形すると共に、圧縮して加熱する。前記下型41には、深絞り成形用凹部42が形成されている。また、前記上型43には、前記下型41の深絞り成形用凹部42と対向する深絞り成形用凸部44が形成されている。なお、前記下型41の型面で賦形される面が意匠面となる場合(第1実施形態の炭素繊維複合化粧板10Aの場合)には、前記下型41の深絞り成形用凹部42は、頂部の曲率半径が3mm以上に設定される。一方、前記上型43の型面で賦形される面が意匠面となる場合(第2実施形態の炭素繊維複合化粧板10Bの場合)には、前記上型43の深絞り成形用凸部44は、頂部の曲率半径が3mm以上に設定される。   In the deep drawing step (4-3) shown in FIG. 4, the laminate 100C is three-dimensionally shaped by deep drawing with a lower die 41 and an upper die 43 of a press molding die, Compress and heat. The lower die 41 is formed with a deep drawing recess 42. Further, the upper die 43 is formed with a deep drawing convex portion 44 that faces the deep drawing concave portion 42 of the lower die 41. In addition, when the surface shaped by the mold surface of the lower mold 41 is a design surface (in the case of the carbon fiber composite decorative board 10A of the first embodiment), the deep drawing concave portion 42 of the lower mold 41 is used. The curvature radius of the top is set to 3 mm or more. On the other hand, when the surface formed by the mold surface of the upper mold 43 is a design surface (in the case of the carbon fiber composite decorative board 10B of the second embodiment), the deep-drawing convex portion of the upper mold 43 No. 44 is set such that the radius of curvature of the top is 3 mm or more.

前記深絞り成形工程における圧縮率は、200〜1500%、特に好ましくは300〜1000%となるようにする。なお、圧縮率は、{(圧縮前のメラミン樹脂発泡体の厚み−芯材の厚み)÷芯材の厚み}×100で規定される。芯材の厚みは、製造された炭素繊維複合化粧板における芯材の厚みである。
なお、前記下型41と上型43間の間隔を変化させて炭素繊維複合化粧板を実際に製造し、得られた炭素繊維複合化粧板から圧縮率を計算して目的の圧縮率となる前記下型41と上型43間の間隔を見つけておく。前記深絞り成形工程時、前記下型41と上型43間には適宜の位置にスペーサを設置して、前記下型41と上型43間が所定間隔(積層体の所定圧縮厚み)となるようにする。
また、加熱方法は特に限定されないが、前記下型41と上型43にヒーター等の加熱手段を設けて、前記下型41と上型43を介して行うのが簡単である。加熱温度は、含浸しているフェノール樹脂の硬化反応温度以上とされる。
The compression ratio in the deep drawing step is 200 to 1500%, particularly preferably 300 to 1000%. The compression rate is defined as {(thickness of melamine resin foam before compression−thickness of core material) ÷ thickness of core material} × 100. The thickness of the core material is the thickness of the core material in the produced carbon fiber composite decorative board.
In addition, the carbon fiber composite decorative board is actually manufactured by changing the interval between the lower mold 41 and the upper mold 43, and the compression ratio is calculated from the obtained carbon fiber composite decorative board to obtain the target compression ratio. Find the space between the lower mold 41 and the upper mold 43. During the deep drawing process, a spacer is installed at an appropriate position between the lower die 41 and the upper die 43, and a predetermined interval (predetermined compression thickness of the laminate) is provided between the lower die 41 and the upper die 43. Like that.
The heating method is not particularly limited, but it is easy to perform heating through the lower mold 41 and the upper mold 43 by providing heating means such as a heater in the lower mold 41 and the upper mold 43. The heating temperature is set to be equal to or higher than the curing reaction temperature of the impregnated phenol resin.

前記深絞り成形工程における圧縮により、前記含浸済み炭素繊維織物210Cのフェノール樹脂と前記含浸済みメラミン樹脂発泡体110Cのフェノール樹脂が確実に接触する。そして前記深絞り成形工程における加熱により、前記含浸済みメラミン樹脂発泡体110Cのフェノール樹脂と前記含浸済み炭素繊維織物210Cのフェノール樹脂がそれぞれ硬化反応を開始し、前記積層体100Cの圧縮状態、すなわち前記含浸済みメラミン樹脂発泡体110Cが圧縮された状態で硬化する。それにより、前記含浸済みメラミン樹脂発泡体110Cから前記芯材110が形成され、また、前記含浸済み炭素繊維織物210Cから前記繊維補強材210が形成され、前記芯材11と前記繊維補強材21と面材31が前記フェノール樹脂の硬化により一体化する。その後、加熱圧縮を解除して前記炭素繊維複合化粧板10を得る。   By the compression in the deep drawing process, the phenol resin of the impregnated carbon fiber fabric 210C and the phenol resin of the impregnated melamine resin foam 110C are reliably in contact. And by the heating in the deep drawing process, the phenol resin of the impregnated melamine resin foam 110C and the phenol resin of the impregnated carbon fiber fabric 210C start a curing reaction, respectively, the compressed state of the laminate 100C, that is, the The impregnated melamine resin foam 110C is cured in a compressed state. Thereby, the core material 110 is formed from the impregnated melamine resin foam 110C, and the fiber reinforcing material 210 is formed from the impregnated carbon fiber fabric 210C. The core material 11 and the fiber reinforcing material 21 The face material 31 is integrated by curing the phenol resin. Thereafter, the heat compression is released to obtain the carbon fiber composite decorative board 10.

さらに本発明は、その課題について、面材を織布とする三次元的な曲げ形状の賦形が良好で、かつ軽量な炭素繊維複合化粧板の提供とする場合、以下のようにも表現される。すなわち、本発明の別の態様は、少なくとも一面に加飾可能な面材が積層された繊維強化成形体において、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布の面材と、前記面材の片面に積層され炭素繊維織布からなる第一の繊維補強材と、前記繊維補強材の前記面材が積層されていない面に積層される発泡体が圧縮賦形されて気泡がないメラミン樹脂層からなる芯材と、前記芯材の前記繊維補強材が積層されていない面に積層され、炭素繊維織布からなる第二の繊維補強材とからなり、
前記面材と前記第一の繊維補強材と前記芯材と前記第二の繊維補強材は、フェノール樹脂接着剤により含浸硬化されている炭素繊維複合化粧板である。
さらに、前記フェノール樹脂接着剤は、前記面材に浸みだすことなく、前記第一の繊維補強材と前記面材との間で接着層を形成する上記炭素繊維複合化粧板である。また、上記炭素繊維複合化粧板には、面材により覆われた、少なくとも3平面から形成される頂部もしくは凹部が、少なくとも一つ備えている炭素繊維複合化粧板である。
Furthermore, the present invention is expressed as follows when providing the carbon fiber composite decorative board having a good three-dimensional bending shape with a woven cloth as a face material and a lightweight carbon fiber composite decorative board. The That is, according to another aspect of the present invention, there is provided a fiber reinforced molded body in which a surface material that can be decorated is laminated on at least one surface, a surface material of a woven fabric made of a heat-resistant long fiber yarn coated with a fluororesin, and The first fiber reinforcing material made of carbon fiber woven fabric laminated on one side of the face material and the foam laminated on the surface of the fiber reinforcing material on which the face material is not laminated are compression-shaped and free of bubbles. A core material composed of a melamine resin layer, and a second fiber reinforcement material composed of a carbon fiber woven fabric, laminated on a surface of the core material on which the fiber reinforcement material is not laminated,
The face material, the first fiber reinforcing material, the core material, and the second fiber reinforcing material are carbon fiber composite decorative boards that are impregnated and cured with a phenol resin adhesive.
Furthermore, the said phenol resin adhesive is the said carbon fiber composite decorative board which forms an adhesive layer between said 1st fiber reinforcement material and the said face material, without oozing out into the said face material. The carbon fiber composite decorative board is a carbon fiber composite decorative board provided with at least one top portion or concave portion formed of at least three planes and covered with a face material.

フェノール樹脂は、住友ベークライト株式会社製、品名;PR−55791B、樹脂濃度60wt%エタノール溶液を用いた。このフェノール樹脂に平織の炭素繊維織物(東邦テックス株式会社製、品名;W−3101、繊維重さ200g/m)を漬け、取り出した後に25℃の室温にて2時間自然乾燥し、更に60℃の雰囲気下にて1時間乾燥させて含浸済み炭素繊維織物を、図5の表に示す各実施例及び各比較例の繊維補強材の積層枚数に応じて形成した。なお、図5の表における[繊維補強材の積層枚数]は、表裏均等に配列した、成形体の総積層枚数である。炭素繊維織物は、200×300mmの平面サイズに裁断したもの(重量12g/枚、厚み0.23mm)を使用した。乾燥後の含浸済み炭素繊維織物は、1枚当たり22gであった。なお、含浸量の調節は、フェノール樹脂から取り出した炭素繊維織物を、隙間を調整した二本の絞りローラーに通すことにより行った。 As the phenol resin, Sumitomo Bakelite Co., Ltd., product name: PR-55791B, resin concentration 60 wt% ethanol solution was used. A plain-woven carbon fiber fabric (manufactured by Toho Tex Co., Ltd., product name; W-3101, fiber weight 200 g / m 2 ) is soaked in this phenolic resin, taken out, air-dried at room temperature of 25 ° C. for 2 hours, and further 60 The carbon fiber woven fabric impregnated by drying for 1 hour in an atmosphere at 0 ° C. was formed in accordance with the number of laminated fiber reinforcing materials in the examples and comparative examples shown in the table of FIG. In addition, [the number of laminated fiber reinforcing materials] in the table of FIG. 5 is the total number of laminated laminates of the molded bodies arranged evenly on the front and back sides. The carbon fiber woven fabric was cut into a plane size of 200 × 300 mm (weight 12 g / sheet, thickness 0.23 mm). The impregnated carbon fiber fabric after drying was 22 g per sheet. The amount of impregnation was adjusted by passing the carbon fiber woven fabric taken out from the phenol resin through two squeezing rollers with adjusted gaps.

また、厚みを5mmとした連続気泡を有するメラミン樹脂発泡体(BASF社製、品名:バソテクトG、密度9kg/m)を、平面サイズ200×300mmに切り出し、前記炭素繊維織物と同様にしてフェノール樹脂溶液に漬け、取り出した後に25℃の室温にて2時間自然乾燥し、更に60℃の雰囲気下にて1時間乾燥させて含浸済みメラミン樹脂発泡体を形成した。
フッ素樹脂で被覆された耐熱性長繊維糸からなる織布からなる面材として、株式会社I.S.T製、イストフロン不燃クロスを用いた。
含浸前のメラミン樹脂発泡体の重量、含浸前の炭素繊維織物全体(全積層数)の重量、含浸後(乾燥後)のメラミン樹脂発泡体の重量、含浸後(乾燥後)の炭素繊維織物全体(全積層数)の重量、及び面材の重量を測定し、測定値を用いて計算した樹脂比率を図5の表に示す。
Further, a melamine resin foam having an open cell thickness of 5 mm (manufactured by BASF, product name: Bathotect G, density 9 kg / m 3 ) was cut into a plane size of 200 × 300 mm, and phenol was obtained in the same manner as the carbon fiber fabric. After being immersed in the resin solution and taken out, it was naturally dried at room temperature of 25 ° C. for 2 hours and further dried in an atmosphere of 60 ° C. for 1 hour to form an impregnated melamine resin foam.
As a face material made of a woven fabric made of heat-resistant long fiber yarn coated with a fluororesin, I.K. S. T-made, Istoflon non-combustible cloth was used.
Weight of melamine resin foam before impregnation, weight of entire carbon fiber fabric before impregnation (total number of laminated layers), weight of melamine resin foam after impregnation (after drying), whole carbon fiber fabric after impregnation (after drying) The weight of (total number of layers) and the weight of the face material are measured, and the resin ratio calculated using the measured values is shown in the table of FIG.

次に、予め離型剤を表面に塗布した鉄製のプレス成形用の金型として、頂部の曲率半径が3mm(比較例4では曲率半径1.5mm)からなる三次元形状の深絞り成形用凹部を四隅に有する凹形状の型面を有する下型と、該下型に対応した上型を用い、含浸後(乾燥後)のメラミン樹脂発泡体と、含浸後(乾燥後)炭素繊維織物と、面材とを、図4の(4−3)のように積層した状態で、下型と上型により深絞り成形した。深絞り成形は、前記積層体を下型と上型により、150℃で10分間、10MPaの面圧をかけて押圧し、圧縮して三次元的に賦形すると共に加熱を行ない、前記圧縮状態でフェノール樹脂を反応硬化させた。その際の加熱は、下型及び上型に取り付けられた鋳込みヒーターにより行なった。また、下型と上型間には、図5の表に示す[製品板厚]と等しい厚みの鉄製スペーサを介在させて下型と上型間の間隔、すなわち積層体の圧縮厚みを調整した。その後、下型と上型を開き、芯材の両面に繊維補強材と面材が積層一体化した各実施例及び各比較例の炭素繊維複合化粧板を得た。得られた炭素繊維複合化粧板は、一面が開口した箱状(深さ10mm×縦150×横250mm)であり、四隅に三次元的に賦形された賦形部(深絞り成形部)を有する。   Next, as a die for iron press molding in which a mold release agent is previously applied to the surface, a three-dimensional deep drawing concave portion having a top radius of curvature of 3 mm (in the comparative example 4, a radius of curvature of 1.5 mm). A lower mold having concave mold surfaces at four corners, an upper mold corresponding to the lower mold, a melamine resin foam after impregnation (after drying), a carbon fiber fabric after impregnation (after drying), The face material was deep-drawn with a lower mold and an upper mold in a state of being laminated as shown in (4-3) of FIG. Deep drawing is performed by pressing the laminated body with a lower mold and an upper mold at a surface pressure of 10 MPa at 150 ° C. for 10 minutes, compressing to form three-dimensionally and heating, The phenolic resin was reacted and cured. The heating at that time was performed by a cast heater attached to the lower mold and the upper mold. Further, an iron spacer having a thickness equal to the [product plate thickness] shown in the table of FIG. 5 is interposed between the lower mold and the upper mold to adjust the interval between the lower mold and the upper mold, that is, the compression thickness of the laminate. . Thereafter, the lower mold and the upper mold were opened, and carbon fiber composite decorative boards of Examples and Comparative Examples in which the fiber reinforcing material and the face material were laminated and integrated on both surfaces of the core material were obtained. The obtained carbon fiber composite decorative board has a box shape (depth 10 mm × length 150 × width 250 mm) with one side opened, and three-dimensionally shaped portions (deep-drawn molded portions) are formed at the four corners. Have.

各実施例及び各比較例について、繊維補強材比率(%)と前記圧縮率(%)を計算した。補強材比率(%)は、前記炭素繊維複合化粧板に対する繊維補強材全体の厚みの割合(%)である。
各実施例及び各比較例の炭素繊維複合化粧板について、金型の曲率半径3.0mmで賦形された賦形部(深絞り成形部)の外観の目視観察、厚み(製品板厚)、比重(JIS K7112準拠)、曲げ弾性率(JIS K7074−1988 A法)、破壊荷重(JIS K7074準拠)の測定、鉄道車両用材料燃焼性試験を行った。測定結果は図5の表に示す。
For each example and each comparative example, the fiber reinforcement ratio (%) and the compression ratio (%) were calculated. The reinforcing material ratio (%) is the ratio (%) of the thickness of the entire fiber reinforcing material to the carbon fiber composite decorative board.
About the carbon fiber composite decorative board of each example and each comparative example, visual observation of the appearance of the shaped part (deep drawing molded part) shaped with a curvature radius of the mold of 3.0 mm, thickness (product thickness), Specific gravity (JIS K7112 compliant), flexural modulus (JIS K7074-1988 A method), fracture load (JIS K7074 compliant) were measured, and railcar material flammability tests were performed. The measurement results are shown in the table of FIG.

外観の目視観察では、炭素繊維複合化粧板の賦形部(深絞り成形部)を含む外面及び内面の外観に対して、皺、亀裂、フェノール樹脂の染み出しの有無を判断した。
炭素繊維複合化粧板の厚み(製品板厚)は平面部の厚みをデジタルマイクロメーターにより測定した。炭素繊維複合化粧板の厚み(製品板厚)は、前記プレス成形用下型と上型間の間隔と等しかった。
鉄道車両用材料燃焼性試験は、平成28年度新方式に従って行った。
In the visual observation of the appearance, the presence or absence of wrinkles, cracks, or phenol resin exudation was determined with respect to the appearance of the outer surface and the inner surface including the shaped portion (deep drawing portion) of the carbon fiber composite decorative board.
As for the thickness of the carbon fiber composite decorative board (product board thickness), the thickness of the flat portion was measured with a digital micrometer. The thickness of the carbon fiber composite decorative board (product board thickness) was equal to the distance between the lower mold for press molding and the upper mold.
The rail vehicle material flammability test was conducted according to the 2016 new method.

実施例1は、炭素繊維複合化粧板の板厚が2mm、芯材両面各々の繊維補強材の積層枚数が2枚、表裏合計4枚、繊維補強材比率が46.0%、圧縮率363%、樹脂比率60.0%、金型の曲率半径が3.0mmであり、賦形部(深絞り成形部)の外観問題無し、弾性率20GPa、破壊荷重210N、燃焼性試験が不燃合格、比重が0.81であった。   In Example 1, the thickness of the carbon fiber composite decorative board is 2 mm, the number of laminated fiber reinforcements on each side of the core material is 2, the total number of front and back is 4, the fiber reinforcement ratio is 46.0%, and the compression ratio is 363%. , Resin ratio 60.0%, mold radius of curvature is 3.0mm, no appearance problem of shaped part (deep drawing part), elastic modulus 20GPa, breaking load 210N, flammability test passed nonflammable, specific gravity Was 0.81.

実施例2は、樹脂比率が68.0%である点を除き、他は実施例1と同様の製造条件であり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率24GPa、破壊荷重230N、燃焼性試験が不燃合格、比重が1.08であった。   Example 2 is the same production conditions as in Example 1 except that the resin ratio is 68.0%, and the measurement results show no appearance problem of the shaped part (deep-drawn part), elastic modulus 24 GPa, breaking load 230 N, flammability test passed nonflammability, specific gravity was 1.08.

実施例3は、樹脂比率が42.9%である点を除き、他は実施例1と同様の製造条件であり、測定結果は賦形部(絞り部深絞り成形部)の外観問題無し、弾性率15GPa、破壊荷重170N、燃焼性試験が不燃合格、比重が0.60であった。   Example 3 is the same production conditions as in Example 1 except that the resin ratio is 42.9%, and the measurement result is no appearance problem of the shaped part (drawing part deep drawing part), The elastic modulus was 15 GPa, the breaking load was 170 N, the flammability test was non-combustible, and the specific gravity was 0.60.

実施例4は、炭素繊維複合化粧板の板厚が3mm、芯材両面各々の繊維補強材の積層枚数が2枚、表裏合計4枚、繊維補強材比率30.7%、圧縮率381%、樹脂比率66.7%、金型の曲率半径が3.0mmであり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率17GPa、破壊荷重180N、燃焼性試験が不燃合格、比重が0.65であった。   In Example 4, the thickness of the carbon fiber composite decorative board is 3 mm, the number of laminated fiber reinforcements on each side of the core material is 2, the total number of front and back is 4, the fiber reinforcement ratio is 30.7%, the compression ratio is 381%, The resin ratio is 66.7%, the radius of curvature of the mold is 3.0 mm, the measurement result is no appearance problem of the shaped part (deep drawing part), the elastic modulus is 17 GPa, the breaking load is 180 N, and the flammability test is nonflammable. The specific gravity was 0.65.

実施例5は、炭素繊維複合化粧板の板厚が3mm、芯材両面各々の繊維補強材の積層枚数が5枚、表裏合計10枚、繊維補強材比率76.7%、圧縮率614%、樹脂比率44.4%、金型の曲率半径が3.0mmであり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率25GPa、破壊荷重520N、燃焼性試験が不燃合格、比重が0.98であった。   In Example 5, the thickness of the carbon fiber composite decorative board is 3 mm, the number of laminated fiber reinforcements on each side of the core material is 5, the total number of front and back 10 sheets, fiber reinforcement ratio 76.7%, compression ratio 614%, The resin ratio is 44.4%, the radius of curvature of the mold is 3.0 mm, the measurement results are no appearance problems of the shaped part (deep drawing part), the elastic modulus is 25 GPa, the breaking load is 520 N, and the flammability test is nonflammable. The specific gravity was 0.98.

実施例6は、炭素繊維複合化粧板の板厚が3mm、芯材両面各々の繊維補強材の積層枚数が3枚、表裏合計6枚、繊維補強材比率46.0%、圧縮率209%、樹脂比率60.0%、金型の曲率半径が3.0mmであり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率18GPa、破壊荷重300N、燃焼性試験が不燃合格、比重が0.81であった。   In Example 6, the thickness of the carbon fiber composite decorative board is 3 mm, the number of laminated fiber reinforcements on each side of the core material is 3, the total number of front and back is 6, fiber reinforcement ratio is 46.0%, compression rate is 209%, The resin ratio is 60.0%, the radius of curvature of the mold is 3.0 mm, the measurement results are no appearance problems of the shaped part (deep drawing part), the elastic modulus is 18 GPa, the breaking load is 300 N, and the flammability test is nonflammable. The specific gravity was 0.81.

実施例7は、炭素繊維複合化粧板の板厚が5mm、芯材両面各々の繊維補強材の積層枚数が5枚、表裏合計10枚、繊維補強材比率46.0%、圧縮率270%、樹脂比率60.0%、金型の曲率半径が3.0mmであり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率20GPa、破壊荷重840N、燃焼性試験が不燃合格、比重が0.83であった。   In Example 7, the thickness of the carbon fiber composite decorative board is 5 mm, the number of laminated fiber reinforcements on each side of the core material is 5, the total number of front and back 10 sheets, the fiber reinforcement ratio 46.0%, the compression ratio 270%, The resin ratio is 60.0%, the radius of curvature of the mold is 3.0 mm, the measurement results are no appearance problems of the shaped part (deep drawing part), the elastic modulus is 20 GPa, the breaking load is 840 N, and the flammability test is nonflammable The specific gravity was 0.83.

実施例8は、炭素繊維複合化粧板の板厚が1mm、芯材両面各々の繊維補強材の積層枚数が1枚、表裏合計2枚、繊維補強材比率46.0%、圧縮率826%、樹脂比率66.7%、金型の曲率半径が3.0mmであり、測定結果は賦形部(深絞り成形部)の外観問題無し、弾性率20GPa、破壊荷重110N、燃焼性試験が不燃合格、比重が1.06であった。   In Example 8, the thickness of the carbon fiber composite decorative board is 1 mm, the number of laminated fiber reinforcements on each side of the core material is 1, the total number of front and back is 2, the fiber reinforcement ratio is 46.0%, the compression ratio is 826%, The resin ratio is 66.7%, the radius of curvature of the mold is 3.0 mm, the measurement results are no appearance problems of the shaped part (deep drawing part), the elastic modulus is 20 GPa, the breaking load is 110 N, and the flammability test is nonflammable. The specific gravity was 1.06.

このように、実施例1〜8の炭素繊維複合化粧板は、何れも不燃試験に合格し、かつ賦形部(深絞り成形部)において外観が良好であると共に、比重が0.60〜1.08で軽量なものであった。なお、金型の曲率半径が3mmより大の場合の例については示していないが、金型の曲率半径が大になれば、皺や破れなどが生じ難くなるのは周知であり、実施例1〜8において、金型の曲率半径を3mm以上としても得られる炭素繊維複合化粧板は、賦形部(深絞り成形部)において外観が良好なものになる。   Thus, each of the carbon fiber composite decorative boards of Examples 1 to 8 passed the non-flammability test, had a good appearance at the shaped part (deep drawing part), and had a specific gravity of 0.60 to 1. .08 and light weight. Although an example where the radius of curvature of the mold is larger than 3 mm is not shown, it is well known that if the radius of curvature of the mold is increased, wrinkles and tears are less likely to occur. -8, the carbon fiber composite decorative board obtained even if the radius of curvature of the mold is 3 mm or more has a good appearance in the shaped part (deep drawing part).

比較例1は、樹脂比率が71.4%である以外は、実施例1と同様の条件で製造されたものであり、測定結果は賦形部(深絞り成形部)で面材に樹脂が染み出しており、外観不良であった。なお外観不良であったため、他の試験項目については試験を行わなかった。   Comparative Example 1 was manufactured under the same conditions as in Example 1 except that the resin ratio was 71.4%, and the measurement result was a molded part (deep drawing part) and the resin was applied to the face material. It exuded and had a poor appearance. Since the appearance was poor, other tests were not tested.

比較例2は、樹脂比率が38.4%である以外は、実施例1と同様の条件で製造されたものであり、測定結果は賦形部(深絞り成形部)で面材に樹脂が染み出しており、外観不良であった。なお外観不良であったため、他の試験項目については試験を行わなかった。   Comparative Example 2 was manufactured under the same conditions as in Example 1 except that the resin ratio was 38.4%, and the measurement result was that the resin was applied to the face material at the shaped part (deep drawing part). It exuded and had a poor appearance. Since the appearance was poor, other tests were not tested.

比較例3は、炭素繊維複合化粧板の板厚が2mm、芯材両面各々の繊維補強材の積層枚数が1枚、表裏合計2枚、繊維補強材比率が23.0%、圧縮率225%、樹脂比率71.4%、金型の曲率半径が3.0mmであり、賦形部(深絞り成形部)で面材に樹脂が染み出しており、外観不良であった。なお外観不良であったため、他の試験項目については試験を行わなかった。   In Comparative Example 3, the thickness of the carbon fiber composite decorative board is 2 mm, the number of laminated fiber reinforcements on each side of the core material is 1, the total number of front and back is 2, the fiber reinforcement ratio is 23.0%, and the compression ratio is 225% The resin ratio was 71.4%, the radius of curvature of the mold was 3.0 mm, and the resin exuded into the face material at the shaped part (deep drawing part), resulting in poor appearance. Since the appearance was poor, other tests were not tested.

比較例1〜3は、樹脂比率が本発明の範囲を外れるものであるため、賦形部(深絞り成形部)で面材に樹脂が染み出した外観不良のものであり、車両用部材において美観が求められる部材には適さないものである。   In Comparative Examples 1 to 3, since the resin ratio is out of the range of the present invention, the resin exudes to the face material at the shaping part (deep drawing part). It is not suitable for members that require aesthetics.

このように、本発明の炭素繊維複合化粧板は、鉄道車両用材料燃焼性試験に不燃合格でき、かつ三次元的な曲げ形状の賦形が良好で、軽量なものである。   As described above, the carbon fiber composite decorative board of the present invention can pass the noncombustibility of the material flammability test for railway vehicles, has a good three-dimensional bent shape, and is lightweight.

10A、10B 炭素繊維複合化粧板
11A、11B 三次元的に賦形された賦形部
11 芯材
21 繊維補強材
31 面材
41 下型
43 上型
100C 積層体
110A メラミン樹脂発泡体
110B フェノール樹脂
110C 含浸済みメラミン樹脂発泡体
210A 炭素繊維織物
210B フェノール樹脂
210C 含浸済み炭素繊維織物
10A, 10B Carbon fiber composite decorative plate 11A, 11B Three-dimensionally shaped shaped part 11 Core material 21 Fiber reinforcing material 31 Face material 41 Lower mold 43 Upper mold 100C Laminate 110A Melamine resin foam 110B Phenolic resin 110C Impregnated melamine resin foam 210A Carbon fiber fabric 210B Phenolic resin 210C Impregnated carbon fiber fabric

Claims (6)

芯材と、前記芯材の両面に積層された繊維補強材と、前記両面の繊維補強材の少なくとも一方の繊維補強材の表面に積層された面材とからなる炭素繊維複合化粧板において、
前記芯材は、連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸して前記メラミン樹脂発泡体の圧縮状態で前記フェノール樹脂が硬化したものであり、
前記繊維補強材は、炭素繊維織物にフェノール樹脂が含浸硬化したものからなり、
前記面材は、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布であり、
前記芯材は一つの層を形成しており、
前記芯材と前記繊維補強材と前記面材は、前記芯材のメラミン樹脂発泡体に含浸したフェノール樹脂と、前記繊維補強材の炭素繊維織物に含浸したフェノール樹脂の硬化によって接着しており、
樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100で規定される樹脂比率が40〜70%であることを特徴とする炭素繊維複合化粧板。
In a carbon fiber composite decorative board comprising a core, a fiber reinforcement laminated on both sides of the core, and a face laminated on the surface of at least one of the fiber reinforcements on both sides,
The core material is obtained by impregnating a melamine resin foam having open cells with a phenol resin and curing the phenol resin in a compressed state of the melamine resin foam,
The fiber reinforcing material consists of a carbon fiber fabric impregnated and cured with a phenol resin,
The face material is a woven fabric made of heat-resistant long fiber yarns coated with a fluorine resin,
The core material forms one layer,
The core material, the fiber reinforcing material, and the face material are bonded by curing the phenol resin impregnated in the melamine resin foam of the core material and the phenol resin impregnated in the carbon fiber fabric of the fiber reinforcing material,
Resin ratio = {(weight of melamine resin foam + weight of phenol resin in carbon fiber composite decorative board) ÷ (weight of carbon fiber composite decorative board excluding weight of face material)} × 100 A carbon fiber composite decorative board characterized by being 40 to 70%.
前記芯材の両面に積層された前記繊維補強材のすべての積層枚数は、2枚〜10枚であることを特徴とする請求項1に記載の炭素繊維複合化粧板。   2. The carbon fiber composite decorative board according to claim 1, wherein the number of all the fiber reinforcements laminated on both surfaces of the core material is 2 to 10 sheets. 前記炭素繊維複合化粧板の破壊荷重(JIS K7074準拠)は100N以上850N以下であり、比重(JIS K7112準拠)は0.50〜1.10である請求項1または2に記載の炭素繊維複合化粧板   The carbon fiber composite makeup according to claim 1 or 2, wherein the carbon fiber composite decorative board has a breaking load (conforming to JIS K7074) of 100N or more and 850N or less and a specific gravity (conforming to JIS K7112) of 0.50 to 1.10. Board 前記炭素繊維複合化粧板には三次元的に賦形された賦形部を有し、前記賦形部の凸部又は凹部の頂部における曲率半径が3mm以上であることを特徴とする請求項1から3のいずれか一項に記載の炭素繊維複合化粧板。   The carbon fiber composite decorative board has a three-dimensionally shaped shaping portion, and a curvature radius at a top of the convex portion or the concave portion of the shaping portion is 3 mm or more. To 5. The carbon fiber composite decorative board according to any one of 3 to 4. 鉄道車両用材料燃焼性試験に不燃合格することを特徴とする請求項1から4の何れか一項に記載の炭素繊維複合化粧板。   The carbon fiber composite decorative board according to any one of claims 1 to 4, wherein the carbon fiber composite decorative board passes the nonflammability test of the material flammability test for railway vehicles. 連続気泡を有するメラミン樹脂発泡体にフェノール樹脂が含浸し、前記メラミン樹脂発泡体が圧縮された状態で前記フェノール樹脂が硬化した芯材と、炭素繊維織物にフェノール樹脂が含浸硬化した繊維補強材と、フッ素樹脂で被覆された耐熱性長繊維糸からなる織布で構成された面材とよりなって、前記芯材の両面には前記繊維補強材が一枚以上積層され、前記両面の繊維補強材の少なくとも一方の繊維補強材の表面には前記面材が積層され、前記芯材と前記繊維補強材と前記面材が積層一体化している炭素繊維複合化粧板の製造方法であって、
連続気泡を有するメラミン樹脂発泡体と炭素繊維織物の何れか一方または両方にフェノール樹脂を、樹脂比率={(メラミン樹脂発泡体の重量+炭素繊維複合化粧板中のフェノール樹脂の重量)÷(面材の重量を除く炭素繊維複合化粧板の重量)}×100で規定される樹脂比率が40〜70%の範囲となるように含浸させる含浸工程と、
前記含浸工程後に前記メラミン樹脂発泡体の両面に、それぞれ前記炭素繊維織物を複数積層配置し、前記メラミン樹脂発泡体の両面に積層配置された炭素繊維織物の少なくとも一方の炭素繊維織物に面材を積層する積層工程と、
前記積層工程で得られた積層体を金型で深絞り成形して三次元的に賦形すると共に、前記積層体を圧縮状態で加熱して前記フェノール樹脂を硬化させ、前記フェノール樹脂の硬化によって前記メラミン樹脂発泡体と前記炭素繊維織物と前記面材を一体化させる深絞り成形工程と、
を行うことを特徴とする炭素繊維複合化粧板の製造方法。
A core material in which a phenol resin is impregnated in a melamine resin foam having open cells, and the phenol resin is cured in a state in which the melamine resin foam is compressed, and a fiber reinforcing material in which a carbon fiber fabric is impregnated and cured with a phenol resin; And a face material composed of a woven fabric made of heat-resistant long fiber yarns coated with a fluororesin, and at least one fiber reinforcing material is laminated on both sides of the core material, A method for producing a carbon fiber composite decorative board in which the face material is laminated on the surface of at least one fiber reinforcing material of the material, and the core material, the fiber reinforcing material, and the face material are laminated and integrated,
Either one or both of the melamine resin foam and carbon fiber woven fabric having open cells, the resin ratio = {(weight of melamine resin foam + weight of phenol resin in the carbon fiber composite decorative board) / (surface The weight of the carbon fiber composite decorative board excluding the weight of the material)} impregnation step for impregnation so that the resin ratio defined by × 100 is in the range of 40 to 70%;
After the impregnation step, a plurality of the carbon fiber fabrics are laminated on both sides of the melamine resin foam, and a face material is applied to at least one of the carbon fiber fabrics arranged on both sides of the melamine resin foam. A laminating process for laminating;
The laminate obtained in the laminating step is deep-drawn with a mold and shaped three-dimensionally, and the laminate is heated in a compressed state to cure the phenol resin, and by curing the phenol resin A deep drawing process for integrating the melamine resin foam, the carbon fiber fabric and the face material;
A method for producing a carbon fiber composite decorative board, comprising:
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CN110549691A (en) * 2019-09-29 2019-12-10 佛山市西钢装饰材料有限公司 Melamine veneer for metal plate and manufacturing process thereof
JP6764179B1 (en) * 2020-05-28 2020-09-30 株式会社The MOT Company Mold

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