JP3065974B2 - Carbon fiber composite molded article and method for producing the same - Google Patents

Carbon fiber composite molded article and method for producing the same

Info

Publication number
JP3065974B2
JP3065974B2 JP9326198A JP32619897A JP3065974B2 JP 3065974 B2 JP3065974 B2 JP 3065974B2 JP 9326198 A JP9326198 A JP 9326198A JP 32619897 A JP32619897 A JP 32619897A JP 3065974 B2 JP3065974 B2 JP 3065974B2
Authority
JP
Japan
Prior art keywords
carbon fiber
fiber composite
resin
composite material
molded article
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP9326198A
Other languages
Japanese (ja)
Other versions
JPH10151708A (en
Inventor
学 安田
稔之 伊藤
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Chemical Corp
Mitsubishi Rayon Co Ltd
Original Assignee
Mitsubishi Chemical Corp
Mitsubishi Rayon Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Chemical Corp, Mitsubishi Rayon Co Ltd filed Critical Mitsubishi Chemical Corp
Priority to JP9326198A priority Critical patent/JP3065974B2/en
Publication of JPH10151708A publication Critical patent/JPH10151708A/en
Application granted granted Critical
Publication of JP3065974B2 publication Critical patent/JP3065974B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined

Landscapes

  • Laminated Bodies (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、軽量で、強度、剛
性、寸法安定性、及び耐久性に優れ、かつ特徴ある異方
性光沢を有する炭素繊維複合成形品の製法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing a carbon fiber composite molded article that is lightweight, has excellent strength, rigidity, dimensional stability, and durability, and has a characteristic anisotropic gloss.

【0002】[0002]

【従来の技術】炭素繊維複合材料は、軽量で且つ高強度
であると云う特徴から航空機、自動車、スポーツ、レジ
ャー、その他各種工業用途に利用されている。一方、炭
素繊維複合材料は、それを構成する炭素繊維集束体の配
向性によって特徴ある異方性光沢を有し、更に表面に塗
装等の処理を施すことによって深みのある重厚な外観を
与え、また導電性、X線透過性、電磁波遮蔽性等の特徴
を有している。
2. Description of the Related Art Carbon fiber composite materials are used for aircraft, automobiles, sports, leisure and various other industrial applications because of their characteristics of being lightweight and having high strength. On the other hand, the carbon fiber composite material has a characteristic anisotropic luster due to the orientation of the carbon fiber bundle constituting the carbon fiber composite material, and gives a deep and solid appearance by applying a treatment such as painting to the surface, Further, it has characteristics such as conductivity, X-ray transparency, and electromagnetic wave shielding properties.

【0003】[0003]

【発明が解決しようとする課題】本発明は、かかる特性
を有する炭素繊維複合材料を用いて、外観及び物性の優
れた炭素繊維複合成形品を簡易且つ効率的に製造し得る
方法を提供するものである。
SUMMARY OF THE INVENTION The present invention provides a method for easily and efficiently producing a carbon fiber composite molded article having excellent appearance and physical properties using a carbon fiber composite material having such properties. It is.

【0004】[0004]

【課題を解決するための手段】すなわち、本発明の第1
の要旨は、熱可塑性樹脂の表面にアクリル系樹脂をマト
リックス樹脂とする、厚さ0.01〜2.0mmの炭素繊
維複合材料層を有する炭素繊維複合成形品にあり、第2
の要旨は、アクリル系樹脂をマトリックス樹脂とする、
厚さ0.01〜2.0mmの炭素繊維複合材料板の表面に
厚み0.01〜30mmとなるように熱可塑性樹脂を射
出成形して、結合一体化せしめることを特徴とする炭素
繊維複合成形品の製法にあり、さらに第3の要旨は、2
枚のアクリル系樹脂をマトリックス樹脂とする、厚さ
0.01〜2.0mmの炭素繊維複合材料板の中間に厚み
0.01〜30mmとなるように熱可塑性樹脂を射出成
形して、結合一体化せしめることを特徴とする炭素繊維
複合成形品の製法にある。
That is, the first aspect of the present invention is as follows.
The gist of the present invention resides in a carbon fiber composite molded product having a carbon fiber composite material layer having a thickness of 0.01 to 2.0 mm and having an acrylic resin as a matrix resin on the surface of a thermoplastic resin.
The gist of the acrylic resin as the matrix resin,
A carbon fiber composite molding characterized in that a thermoplastic resin is injection-molded on a surface of a carbon fiber composite material plate having a thickness of 0.01 to 2.0 mm so as to have a thickness of 0.01 to 30 mm so as to be integrated. The third point is in the manufacturing method of the product.
A thermoplastic resin is injection-molded so as to have a thickness of 0.01 to 30 mm in the middle of a carbon fiber composite material plate having a thickness of 0.01 to 2.0 mm using a piece of acrylic resin as a matrix resin. And a method for producing a carbon fiber composite molded article characterized in that

【0005】[0005]

【発明の実施の形態】炭素繊維複合材料板としては、ア
クリル系樹脂を含浸せしめた一方向プリプレグを必要に
応じて適宜積層し、加熱加圧して得られる炭素繊維複合
材料板が代表例として挙げられる(特願平2−4185
25号,同4−32344号,同4−32345号明細
書に記載)。
DESCRIPTION OF THE PREFERRED EMBODIMENTS As a carbon fiber composite material plate, a carbon fiber composite material plate obtained by appropriately laminating a unidirectional prepreg impregnated with an acrylic resin as necessary and heating and pressing is exemplified. RU (Japanese Patent Application No. 2-4185)
Nos. 25, 4-32344 and 4-32345).

【0006】さらに、一方向プリプレグの代わりに炭素
繊維からなる織物、編み物、不織布、マット等に公知の
方法で適宜、熱硬化性樹脂または熱可塑性樹脂を含浸せ
しめ、必要に応じて積層し、加熱加圧せしめた厚み0.
01〜2.0mmの炭素繊維複合材料板も使用される。
炭素繊維複合材料板のマトリックス樹脂をアクリル系樹
脂とすることにより、炭素繊維に独特の深みのある光
沢、模様がより鮮やかに現れ、意匠効果を発揮する。
Further, a woven fabric, a knitted fabric, a nonwoven fabric, a mat or the like made of carbon fibers are appropriately impregnated with a thermosetting resin or a thermoplastic resin in place of the one-way prepreg by a known method, laminated as necessary, and laminated by heating. Pressurized thickness 0.
Carbon fiber composite plates of 01-2.0 mm are also used.
By using an acrylic resin as the matrix resin of the carbon fiber composite material plate, a unique deep luster and pattern appear more vividly on the carbon fiber, and the design effect is exhibited.

【0007】本発明で用いる炭素繊維複合材料板の厚み
は0.01〜2.0mmである。5〜10μ径をもつ通常
の炭素繊維フィラメントの場合、厚み0.01mm未満
の複合材料板またはフィルムを製作することは困難であ
り、逆に厚み2.0mmを越える複合材料板は、射出成
形金型内に入れるために必要な曲げ及び撓み変形に乏し
くなるので好ましくない。
The thickness of the carbon fiber composite material plate used in the present invention is 0.01 to 2.0 mm. In the case of ordinary carbon fiber filaments having a diameter of 5 to 10 μm, it is difficult to produce a composite material plate or a film having a thickness of less than 0.01 mm. It is not preferable because bending and bending deformations required for putting in the mold are poor.

【0008】なお、本発明の趣旨に従って、炭素繊維複
合材料の成形に際し、ガラス繊維、アラミド繊維、その
ほかの有機または無機繊維をハイブリッドとして併用す
ることは何ら差し支えない。また、取扱い性を改良する
ために積極的にハイブリッド材とすることも可能であ
る。
In the meantime, according to the gist of the present invention, glass fibers, aramid fibers, and other organic or inorganic fibers may be used in combination as a hybrid when forming the carbon fiber composite material. It is also possible to positively use a hybrid material in order to improve the handleability.

【0009】炭素繊維複合材料板の表面または2枚の炭
素繊維複合材料板の中間に樹脂層を形成する熱可塑樹脂
としては、ナイロン、ABS、ポリカーボネート、アク
リル、その他、射出成形できる樹脂であればよく、公知
の熱可塑性樹脂または、強化熱可塑性樹脂から、マトリ
ックス樹脂との接着性、劣化温度等を考慮にいれ、適宜
選定使用することが可能である。樹脂層の厚み、すなわ
ち、炭素繊維複合材料板との厚み比率は、性能発揮効率
と材料費のバランスから決定される。
The thermoplastic resin forming the resin layer on the surface of the carbon fiber composite material plate or between the two carbon fiber composite material plates may be nylon, ABS, polycarbonate, acrylic, or any other resin that can be injection molded. A well-known thermoplastic resin or reinforced thermoplastic resin can be appropriately selected and used in consideration of the adhesiveness to the matrix resin, the deterioration temperature, and the like. The thickness of the resin layer, that is, the ratio of the thickness to the carbon fiber composite material plate, is determined from the balance between the performance demonstrating efficiency and the material cost.

【0010】軽量かつ高剛性の材料を得るためには、2
枚の炭素繊維複合材料板の中間層に熱可塑性樹脂層を形
成して、サンドイッチ構造体とするのが効果的である。
また、炭素繊維の特徴ある異方性光沢を成形品外観に生
かすためには、外層を炭素繊維複合材料にすることが効
果的である。これらの方法により、軽量、高性能、好外
観の成形品が得られる。
In order to obtain a lightweight and highly rigid material,
It is effective to form a sandwich structure by forming a thermoplastic resin layer on an intermediate layer of two carbon fiber composite material plates.
In order to make use of the characteristic anisotropic luster of carbon fibers in the appearance of a molded product, it is effective to use a carbon fiber composite material for the outer layer. By these methods, lightweight, high-performance, and good-looking molded articles can be obtained.

【0011】さらに、炭素繊維複合材料板を表面に出し
た成形品では、炭素繊維複合材料板のマトリックスと樹
脂層を形成する樹脂をともにアクリル系樹脂とすること
により、炭素繊維に独特の深みのある光沢、模様がより
鮮やかに現れ、意匠効果を発揮する。
Further, in the molded article having the carbon fiber composite material plate exposed on the surface, the resin forming the matrix and the resin layer of the carbon fiber composite material plate is made of an acrylic resin, so that the carbon fiber composite plate has a unique depth to carbon fiber. A certain luster and pattern appear more vividly and exhibit a design effect.

【0012】本発明の炭素繊維複合成形品は、既存の射
出成形機を用いても製造することができるが、インジェ
クションプレスを用いることで、大型成形品の成形が可
能となり、また、炭素繊維複合材料板と樹脂層との接着
が強固なものとなる。
Although the carbon fiber composite molded article of the present invention can be produced by using an existing injection molding machine, a large molded article can be molded by using an injection press. The adhesion between the material plate and the resin layer becomes strong.

【0013】[0013]

【実施例】以下、本発明を実施例によって更に具体的に
説明する。
EXAMPLES The present invention will be described more specifically below with reference to examples.

【0014】[実施例1]炭素繊維3000本を集束し
た炭素繊維トウ(三菱レイヨン社製パイロフィルTR4
0)を用いて製織(経緯とも12.5本/インチ)した
炭素繊維織布に、アクリル系樹脂を含浸して0.3mm
厚のシート状物を形成した。
[Example 1] Carbon fiber tow (Pyrofil TR4 manufactured by Mitsubishi Rayon Co., Ltd.) bundled with 3000 carbon fibers
0) is impregnated with an acrylic resin into a woven carbon fiber woven fabric (12.5 lines / inch for both processes) and 0.3 mm
A thick sheet was formed.

【0015】次に、このシート状物を95×520mm
に切断して皿金型底部にセットし、ポリメチルメタクリ
レート(三菱レイヨン社製アクリライトVH)を、シリ
ンダー温度250℃,金型温度60℃の条件で射出成形
して、外層に炭素繊維複合材料層をもつ、3mm厚の成
形品を得た。
Next, this sheet-shaped material is 95 × 520 mm
, Set on the bottom of a dish mold, and injection-molded polymethyl methacrylate (Acrylite VH manufactured by Mitsubishi Rayon Co., Ltd.) at a cylinder temperature of 250 ° C. and a mold temperature of 60 ° C. to form a carbon fiber composite material on the outer layer. A 3 mm thick molded article with layers was obtained.

【0016】これから切り出した試験片に対して、AS
TM D−790に準じた曲げ試験を実施したところ、
表1の如く優れた特性を示した。また表面は炭素繊維複
合材料特有の高級重厚感をもち、日用品、自動車内装品
へ有効に利用できるものであった。
The test piece cut out from this was subjected to AS
When a bending test according to TM D-790 was performed,
Excellent characteristics are shown in Table 1. In addition, the surface had a high-grade profound feeling peculiar to the carbon fiber composite material, and could be effectively used for daily necessities and automobile interior parts.

【0017】[実施例2]射出する樹脂を炭素繊維強化
ポリカーボネート樹脂(三菱レイヨン社製パイロフィル
ペレットPC−C−20)に、シリンダー平均温度を3
00℃、金型温度80℃にかえた他は、実施例1と同様
の操作を行って、3mm厚の成形品を得た。
Example 2 The resin to be injected was carbon fiber reinforced polycarbonate resin (Pyrofil Pellets PC-C-20 manufactured by Mitsubishi Rayon Co., Ltd.) and the average cylinder temperature was 3
A molded product having a thickness of 3 mm was obtained by performing the same operation as in Example 1 except that the temperature was changed to 00 ° C and the mold temperature was changed to 80 ° C.

【0018】これから切り出した試験片に対して、AS
TM D−790に準じた曲げ試験を実施を実施したと
ころ、表1の如く優れた特性を示した。
The test piece cut out from this was subjected to AS
When a bending test was performed in accordance with TMD-790, excellent characteristics were shown in Table 1.

【0019】[実施例3]シートの切断寸法を145×
520mmに変更したほかは、実施例1と同様な方法で
トレー壁面にも炭素繊維複合材料層のある3mm厚の成
形品を得た。断面観察を行ったところ、角部の炭素繊維
に座屈等の欠陥はなく良好な成形品であった。
[Embodiment 3] The cut size of the sheet is 145 ×
A 3 mm-thick molded product having a carbon fiber composite material layer on the tray wall was obtained in the same manner as in Example 1 except that the thickness was changed to 520 mm. When the cross section was observed, it was a good molded product without any defect such as buckling in the carbon fiber at the corner.

【0020】[実施例4]ゲート部に当たる部分に13
mmφの穴を開けたシートと穴を開けないシートを重ね
て金型内にセットしたほかは実施例1と同様の操作を行
って、樹脂層の両面に炭素繊維複合材料層をもつ3mm
厚のサンドイッチ成形品を得た。
[Embodiment 4] 13 is applied to a portion corresponding to a gate portion.
The same operation as in Example 1 was carried out except that the sheet with the hole of mmφ and the sheet without the hole were set in a mold by superimposing the sheet, and the sheet having the carbon fiber composite material layer on both surfaces of the resin layer was 3 mm.
A thick sandwich molded product was obtained.

【0021】これから切り出した試験片に対して、AS
TM D−790に準じた曲げ試験を実施を実施したと
ころ、表1の如く特に優れた特性を示した。また表面は
炭素繊維複合材料特有の高級重厚感をもち、日用品、自
動車内装品へ有効に利用できものであった。
The test piece cut out from this was subjected to AS
When a bending test was performed according to TMD-790, particularly excellent characteristics were shown in Table 1. In addition, the surface had a high-grade profound feeling unique to carbon fiber composite materials, and could be effectively used for daily necessities and automobile interior parts.

【0022】[0022]

【表1】 [Table 1]

【0023】[0023]

【発明の効果】上述の如く構成された本発明によれば、
外観及び物性の優れた炭素繊維複合成形品を極めて簡易
且つ効率的に得ることが出来る。
According to the present invention configured as described above,
A carbon fiber composite molded product having excellent appearance and physical properties can be obtained extremely easily and efficiently.

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI B29L 9:00 (58)調査した分野(Int.Cl.7,DB名) B29C 45/00 - 45/84 B32B 5/28 B32B 27/30 ──────────────────────────────────────────────────の Continued on the front page (51) Int.Cl. 7 identification code FI B29L 9:00 (58) Field surveyed (Int.Cl. 7 , DB name) B29C 45/00-45/84 B32B 5/28 B32B 27/30

Claims (6)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 厚さ0.01〜30mmの熱可塑性樹脂
の表面にアクリル系樹脂をマトリックス樹脂とする、厚
さ0.01〜2.0mmの炭素繊維複合材料層を有する炭
素繊維複合成形品。
1. A carbon fiber composite molded article having a carbon fiber composite material layer having a thickness of 0.01 to 2.0 mm using an acrylic resin as a matrix resin on a surface of a thermoplastic resin having a thickness of 0.01 to 30 mm. .
【請求項2】 アクリル系樹脂をマトリックス樹脂とす
る、厚さ0.01〜2.0mmの炭素繊維複合材料板の表
面に厚み0.01〜30mmとなるように熱可塑性樹脂
を射出成形して、結合一体化せしめることを特徴とする
炭素繊維複合成形品の製法。
2. A thermoplastic resin is injection-molded to a thickness of 0.01 to 30 mm on the surface of a carbon fiber composite material plate having a thickness of 0.01 to 2.0 mm using an acrylic resin as a matrix resin. And a method for producing a carbon fiber composite molded article characterized by being integrated.
【請求項3】 2枚のアクリル系樹脂をマトリックス樹
脂とする、厚さ0.01〜2.0mmの炭素繊維複合材料
板の中間に厚み0.01〜30mmとなるように熱可塑
性樹脂を射出成形して、結合一体化せしめることを特徴
とする炭素繊維複合成形品の製法。
3. A thermoplastic resin is injected into the middle of a 0.01 to 2.0 mm thick carbon fiber composite material plate having a thickness of 0.01 to 30 mm using two acrylic resins as a matrix resin. A method for producing a carbon fiber composite molded article, which is molded and bonded and integrated.
【請求項4】 熱可塑性樹脂層を形成する樹脂が、アク
リル系樹脂である請求項1記載の炭素繊維複合成形品の
製法。
4. The method for producing a carbon fiber composite molded article according to claim 1, wherein the resin forming the thermoplastic resin layer is an acrylic resin.
【請求項5】 ゲート部に当たる部分に穴を開けたシー
トと穴を開けないシートを重ねて金型内にセットし熱可
塑性樹脂を射出成形する請求項3記載の炭素繊維複合成
形品の製法。
5. The method for producing a carbon fiber composite molded product according to claim 3, wherein a sheet having a hole at a portion corresponding to a gate portion and a sheet having no hole are overlapped, set in a mold, and injection molded with a thermoplastic resin.
【請求項6】 射出成形をインジェクションプレスによ
り行う請求項1項記載の炭素繊維複合成形品の製法。
6. The method according to claim 1, wherein the injection molding is performed by an injection press.
JP9326198A 1997-11-27 1997-11-27 Carbon fiber composite molded article and method for producing the same Expired - Lifetime JP3065974B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9326198A JP3065974B2 (en) 1997-11-27 1997-11-27 Carbon fiber composite molded article and method for producing the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9326198A JP3065974B2 (en) 1997-11-27 1997-11-27 Carbon fiber composite molded article and method for producing the same

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP4173296A Division JP3035409B2 (en) 1992-06-30 1992-06-30 Manufacturing method of carbon fiber composite molded product

Publications (2)

Publication Number Publication Date
JPH10151708A JPH10151708A (en) 1998-06-09
JP3065974B2 true JP3065974B2 (en) 2000-07-17

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JP4107709B2 (en) * 1998-04-20 2008-06-25 三菱レイヨン株式会社 Evaluation method of fiber reinforced plastic sandwich board
JP5355803B1 (en) * 2013-01-18 2013-11-27 日新製鋼株式会社 Painted metal preform, composite, and production method thereof
JP7046711B2 (en) * 2018-05-21 2022-04-04 株式会社水田製作所 Wood grain pattern molded building material, wood grain pattern carbon fiber composite thin body and its manufacturing method
CN116034028A (en) * 2020-08-21 2023-04-28 巴斯夫欧洲公司 Materials, compositions, and methods for forming composite articles

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