JP3098478B2 - Manufacturing method of carbon fiber composite molded product - Google Patents
Manufacturing method of carbon fiber composite molded productInfo
- Publication number
- JP3098478B2 JP3098478B2 JP09326197A JP32619797A JP3098478B2 JP 3098478 B2 JP3098478 B2 JP 3098478B2 JP 09326197 A JP09326197 A JP 09326197A JP 32619797 A JP32619797 A JP 32619797A JP 3098478 B2 JP3098478 B2 JP 3098478B2
- Authority
- JP
- Japan
- Prior art keywords
- carbon fiber
- fiber composite
- composite material
- resin
- thickness
- 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
Links
Classifications
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/71—General 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
【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、連続した炭素繊維からなる、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、第2の要旨は、2枚の連続した炭素繊維
からなる、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。That is, the first aspect of the present invention is as follows.
The gist is composed of continuous carbon fiber and has a thickness of 0.01 to
The thickness of the carbon fiber composite material plate of 2.0 mm
A method for producing a carbon fiber composite molded article characterized in that a thermoplastic resin is injection-molded so as to have a thickness of 30 mm and bonded and integrated, and a second point is that a thickness is formed of two continuous carbon fibers. A carbon fiber composite molded product characterized by injection-molding a thermoplastic resin in the middle 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 and joining and integrating the thermoplastic resin. Recipe.
【0005】[0005]
【発明の実施の形態】炭素繊維複合材料板としては、炭
素繊維を一方向に引き揃えてシート状にし、公知の熱硬
化性樹脂(エポキシ、ポリエステル、フェノール、ビニ
ルエステル、ポリイミド等)および、公知の熱可塑性樹
脂(ナイロン、ABS、ポリカーボネート、アクリル
等)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2−418525号,
同4−32344号,同4−32345号明細書に記
載)。BEST MODE FOR CARRYING OUT THE INVENTION As a carbon fiber composite material plate, carbon fibers are aligned in one direction to form a sheet, and a known thermosetting resin (epoxy, polyester, phenol, vinyl ester, polyimide, etc.) and a known resin are used. A carbon fiber composite material plate obtained by appropriately laminating a unidirectional prepreg impregnated with a thermoplastic resin (nylon, ABS, polycarbonate, acrylic, or the like) and heating and pressing the resin as a representative example (Japanese Patent Application Hei 2-418525,
Nos. 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。Further, a woven fabric or a knitted fabric made of carbon fibers is appropriately impregnated with a thermosetting resin or a thermoplastic resin by a known method in place of the one-way prepreg, laminated as necessary, and laminated by heating and pressing. Carbon fiber composite boards of 0.01-2.0 mm are also used.
【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 in the middle of the two carbon fiber composite material plates may be nylon, ABS, polycarbonate, acrylic, or any other resin that can be injection molded. Any known thermoplastic resin or reinforced thermoplastic resin can be appropriately selected and used in consideration of the adhesion 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]エポキシ樹脂をマトリックス
樹脂とする炭素繊維クロスプリプレグ(三菱レイヨン社
製TR3110 340)1層を硬化したシートを用い
るほかは、実施例1と同様な方法によって、外層に炭素
繊維複合材料層をもつ、3mm厚の成形品を得た。[Example 2] A carbon fiber cloth prepreg using an epoxy resin as a matrix resin (TR3110 340 manufactured by Mitsubishi Rayon Co., Ltd.) was used. A 3 mm thick molded article having a fiber composite material layer was obtained.
【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]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 3 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.
【0020】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.
【0021】[実施例4]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 4] 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.
【0022】[実施例5]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 5] In the portion corresponding to the gate portion, 13
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.
【0023】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るものであった。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 peculiar to the carbon fiber composite material, and could be effectively used for daily necessities and automobile interior parts.
【0024】[0024]
【表1】 [Table 1]
【0025】[0025]
【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 (58)調査した分野(Int.Cl.7,DB名) B29C 45/00 - 45/84 ──────────────────────────────────────────────────続 き Continued on front page (58) Field surveyed (Int. Cl. 7 , DB name) B29C 45/00-45/84
Claims (5)
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。1. It has flexibility made of continuous carbon fiber.
A thermoplastic resin 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, and bonded and integrated. Manufacturing method for composite molded products.
を有する、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。2. A flexible sheet made of two continuous carbon fibers, having a thickness of 0.01 to 2.0 mm, and being heated to a thickness of 0.01 to 30 mm in the middle of a carbon fiber composite material plate. A method for producing a carbon fiber composite molded article, comprising injection-molding a plastic resin and bonding and integrating the same.
が、アクリル系樹脂である請求項1又は2記載の炭素繊
維複合成形品の製法。Wherein the matrix resin in the carbon fiber composite material plate according to claim 1 or 2 Preparation of carbon fiber composite molded article, wherein the acrylic resin.
リル系樹脂である請求項1又は2記載の炭素繊維複合成
形品の製法。4. A resin forming the thermoplastic resin layer method according to claim 1 or 2, wherein the carbon fiber composite moldings is an acrylic resin.
り行う請求項1項又は2記載の炭素繊維複合成形品の製
法。5. A method according to claim 1 1 or 2 Preparation of carbon fiber composite moldings according performing injection molding by injection press.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP09326197A JP3098478B2 (en) | 1997-11-27 | 1997-11-27 | Manufacturing method of carbon fiber composite molded product |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP09326197A JP3098478B2 (en) | 1997-11-27 | 1997-11-27 | Manufacturing method of carbon fiber composite molded product |
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 |
---|---|
JPH10156881A JPH10156881A (en) | 1998-06-16 |
JP3098478B2 true JP3098478B2 (en) | 2000-10-16 |
Family
ID=18185106
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP09326197A Expired - Lifetime JP3098478B2 (en) | 1997-11-27 | 1997-11-27 | Manufacturing method of carbon fiber composite molded product |
Country Status (1)
Country | Link |
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JP (1) | JP3098478B2 (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
JP5098132B2 (en) * | 2004-03-29 | 2012-12-12 | 東レ株式会社 | Fiber reinforced resin sandwich panel |
DE102004051334A1 (en) * | 2004-10-21 | 2006-05-04 | Christian Fuchs | Process for producing a dimensionally stable object coated with a textile fabric, in particular a fiber composite structure |
JP4973745B2 (en) * | 2010-02-01 | 2012-07-11 | トヨタ自動車株式会社 | Method for forming continuous fiber prepreg |
JP5565566B2 (en) * | 2010-03-04 | 2014-08-06 | Jx日鉱日石エネルギー株式会社 | Carbon fiber reinforced plastic molding |
JP5565565B2 (en) * | 2010-03-04 | 2014-08-06 | Jx日鉱日石エネルギー株式会社 | Carbon fiber reinforced plastic molding |
KR101537862B1 (en) * | 2013-11-27 | 2015-07-17 | 롯데케미칼 주식회사 | Hybrid seat frame for vehicle |
JP2017144567A (en) * | 2016-02-15 | 2017-08-24 | 東レ株式会社 | Thermoplastic resin molded body |
-
1997
- 1997-11-27 JP JP09326197A patent/JP3098478B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH10156881A (en) | 1998-06-16 |
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