JP2005133141A - Metal based carbon fiber-reinforced composite material, and production method therefor - Google Patents
Metal based carbon fiber-reinforced composite material, and production method therefor Download PDFInfo
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本発明は、航空宇宙等の極限環境、あるいは半導体や液晶パネル等の超精密産業機械用途に適用可能な、高弾性、低熱膨張、耐熱性に優れた産業用部材である金属基炭素繊維強化複合材料およびその製造方法に関する。 The present invention is a metal-based carbon fiber reinforced composite that is an industrial member with excellent elasticity, low thermal expansion, and excellent heat resistance, applicable to extreme environments such as aerospace, or ultra-precision industrial machinery applications such as semiconductors and liquid crystal panels. The present invention relates to a material and a manufacturing method thereof.
惑星探査衛星がおかれる宇宙空間では、その惑星探査衛星を構成する使用部材が、高真空、高温、低温、に同時にさらされる。そのような極限環境で、強度、剛性、低熱膨張性を満足し得る材料として、近年、金属基炭素繊維強化複合材料が認知されている。 In the outer space where the planetary exploration satellite is placed, the members that make up the planetary exploration satellite are simultaneously exposed to high vacuum, high temperature, and low temperature. In recent years, metal-based carbon fiber reinforced composite materials have been recognized as materials that can satisfy strength, rigidity, and low thermal expansion in such extreme environments.
この金属基炭素繊維強化複合材料とは、弾性率が高く且つ熱膨張のほとんどない炭素繊維が強化材として使用され、母材にアルミニウム、銅、マグネシウムおよびそれらの合金などが用いられている。(例えば特許文献1参照)。 As this metal-based carbon fiber reinforced composite material, a carbon fiber having a high elastic modulus and almost no thermal expansion is used as a reinforcing material, and aluminum, copper, magnesium and alloys thereof are used as a base material. (For example, refer to Patent Document 1).
また、この金属基炭素繊維強化複合材料は、温度変化に対する寸法安定性、高弾性が必要であることから、半導体製造装置や液晶パネル製造装置、各種ロボットアームなどの用途としても、現在、注目されている。
しかしながら、前述したような衛星用途としては、金属材料、炭素繊維強化樹脂複合材料などが用いられているが、熱膨張、真空下での脱ガス特性、弾性率などの欠点があるため、従来、設計が困難であった。 However, for satellite applications as described above, metal materials, carbon fiber reinforced resin composite materials, etc. are used, but due to drawbacks such as thermal expansion, degassing characteristics under vacuum, and elastic modulus, It was difficult to design.
また後述したような産業用途である、半導体製造装置や液晶パネル製造装置などは、従来はアルミナなどのセラミックを主体とした部品で構成されてきたが、半導体の集積化、液晶パネルの大型化に対応した製造装置の大型化、高加工化の面では、加工性、重量、強度面から限界に来ていると言われており、かかる構成材料を、金属基炭素繊維強化複合材料に置き換えようとしている。 In addition, semiconductor manufacturing equipment and liquid crystal panel manufacturing equipment, etc., which are industrial applications as described later, have conventionally been composed of parts mainly made of ceramics such as alumina. In terms of increasing the size and processing capability of the corresponding manufacturing equipment, it is said that it has reached the limit in terms of workability, weight, and strength, and we are trying to replace such constituent materials with metal-based carbon fiber reinforced composite materials. Yes.
このように、最近性能面から注目されている金属基炭素繊維強化複合材料ではあるが、今まではその製造方法が難しく広く普及するまでには至らなかった。
すなわち、従来は、通常強化材となる炭素繊維強化炭素複合材料(以下C/C材と略する)を溶融状態の金属中に浸漬することにより金属成分を含浸させていたが、これによると、金属が溶融する高温状態が必要となるが、アルミニウムのような金属によっては、炭素とカーバイド生成反応が起こるため、均質な複合化が難しい。
As described above, although it is a metal-based carbon fiber reinforced composite material that has recently been attracting attention in terms of performance, its production method has been difficult so far and has not been widely spread.
That is, conventionally, a carbon fiber reinforced carbon composite material (hereinafter abbreviated as C / C material), which is a normal reinforcing material, was impregnated with a metal component by immersing it in a molten metal. Although a high temperature state in which the metal melts is necessary, depending on a metal such as aluminum, a carbon and carbide formation reaction occurs, so that it is difficult to form a homogeneous composite.
そこで、本発明は、従来材料に比較して高弾性、低熱膨張、耐熱性に優れ、且つ目的に応じた材料設計の自由度が高い金属基炭素繊維強化複合材料およびその製造方法を提供することを目的とする。 Therefore, the present invention provides a metal-based carbon fiber reinforced composite material that is excellent in high elasticity, low thermal expansion, and heat resistance as compared with conventional materials and has a high degree of freedom in material design according to the purpose, and a method for producing the same. With the goal.
上記課題を達成するために、本件発明者は、鋭意研究した結果、炭素繊維と等方性炭素材がサンドイッチ構造をなす炭素部材に金属マトリックスを含浸することを知見した。
すなわち、請求項1にかかる金属基炭素繊維強化複合材料は、炭素部分が、等方性炭素材を中央部のコア材とし、外側に炭素繊維を配する3層構造により構成されるサンドイッチ構造をとることを特徴とする。
請求項2にかかる金属基炭素繊維強化複合材料は、請求項1において、前記等方性炭素材が、CIP材、押出材、型込材、短繊維成型体などの炭素粉粒体を成型して製作した炭素材であることを特徴とする。
請求項3にかかる金属基炭素繊維強化複合材料は、請求項1または2において、前記炭素繊維が、織物材、0/90度積層材、一方向積層材、チョップ材およびそれを組み合わせたものであることを特徴とする。
請求項4にかかる金属基炭素繊維強化複合材料は、請求項1〜3の何れか1項において、金属基が、アルミニウム、銅、マグネシウム、およびそれらの合金であることを特徴とする。
請求項5にかかる金属基炭素繊維強化複合材料の製造方法は、炭素部分が、CIP材、押出材、型込材、短繊維成型体などの炭素粉粒体を成型して製作した炭素材を有した等方性炭素材を中央部のコア材とし、外側に炭素繊維を配する3層構造により構成されるサンドイッチ構造とし、前記炭素材に対して金属を溶融状態で高圧で圧入することを特徴とする。
請求項6にかかる金属基炭素繊維強化複合材料の製造方法は、請求項5において、前記炭素繊維が、織物材、0/90度積層材、一方向積層材、チョップ材およびそれを組み合わせたものであることを特徴とする。
請求項7にかかる金属基炭素繊維強化複合材料の製造方法は、請求項5または6において、金属基が、アルミニウム、銅、マグネシウム、およびそれらの合金を用いたことを特徴とする。
In order to achieve the above object, the present inventor has intensively studied, and as a result, has found that the carbon matrix and the isotropic carbon material are impregnated with a metal matrix in a carbon member having a sandwich structure.
That is, the metal-based carbon fiber reinforced composite material according to
A metal-based carbon fiber reinforced composite material according to
A metal-based carbon fiber reinforced composite material according to claim 3 is the composite material according to
The metal-based carbon fiber reinforced composite material according to claim 4 is characterized in that, in any one of
In the method for producing a metal-based carbon fiber reinforced composite material according to claim 5, a carbon material is produced by molding a carbon powder such as a CIP material, an extruded material, a molding material, and a short fiber molded body. It is a sandwich structure composed of a three-layer structure in which an isotropic carbon material having a central core material and carbon fibers are arranged on the outside, and metal is pressed into the carbon material at a high pressure in a molten state. Features.
The method for producing a metal-based carbon fiber reinforced composite material according to claim 6 is the method according to claim 5, wherein the carbon fiber is a woven material, a 0/90 degree laminated material, a unidirectional laminated material, a chop material, and a combination thereof. It is characterized by being.
The method for producing a metal-based carbon fiber reinforced composite material according to claim 7 is characterized in that, in claim 5 or 6, the metal group uses aluminum, copper, magnesium, and alloys thereof.
本発明によれば、炭素繊維と等方性炭素材がサンドイッチ構造をなす炭素部材に金属マトリックスを有効に含浸するため、従来の金属基炭素複合材料の欠点を改善して、高弾性、低熱膨張、耐熱性に優れ、且つ目的に応じた材料設計の自由度が高い高性能な金属基炭素繊維強化複合材料が提供できる。
また、本製造法によれば、金属と炭素がカーバイド生成反応を起こすことなく、金属基炭素繊維強化複合材料が容易に製造でき、したがって、産業界に広く普及することができる。
According to the present invention, a carbon member having a sandwich structure of carbon fibers and an isotropic carbon material is effectively impregnated with a metal matrix, thereby improving the disadvantages of the conventional metal-based carbon composite material, and having high elasticity and low thermal expansion. It is possible to provide a high-performance metal-based carbon fiber reinforced composite material that is excellent in heat resistance and has a high degree of freedom in material design according to the purpose.
Further, according to this production method, the metal-based carbon fiber reinforced composite material can be easily produced without causing a carbide-forming reaction between the metal and carbon, and thus can be widely spread in the industry.
次に本実施の形態にかかる金属基炭素繊維強化複合材料と、その製造方法を説明する。
本実施の形態にかかる金属基炭素繊維強化複合材料は、その炭素部分が中心を形成する中央部のコア材2及びその外周あるいは上下面に配するスキン材1からなり、全体に金属が含浸されている。
Next, a metal-based carbon fiber reinforced composite material according to the present embodiment and a manufacturing method thereof will be described.
The metal-based carbon fiber reinforced composite material according to the present embodiment includes a
中央部のコア材2は、各種の等方性炭素材を用いるが、その役割は材料全体の芯材として、また適度な気孔を有するため金属を材料中心まで均一に含浸せしめる役割を持っている。適用し得る等方性炭素材料としては、その製造方法により、型込材、押出材、CIP材、短繊維成型材等がいずれも好適に用いられるが、気孔率、密度、熱膨張係数、強度、価格などの面から型込材、押出材がより好ましい。
The
外側に配するスキン材1は、炭素繊維からなり、その用途に応じて織物材、0/90度積層材、一方向材、チョップ材およびそれらを組み合わせたものを使い分けることができる。特に、熱膨張、弾性率の性能設計の観点では、外側の炭素繊維材を選ぶことで材料性能設計の自由度が従来のC/C材に比較して格段に広がっている。
The
例えば、機械的特性や熱膨張に方向性を持たせる用途に対しては、0/90度積層材や一方向積層材、等方的に特性を出したい場合には織物材やチョップ材を用いることが望ましい。 For example, for applications that give directionality to mechanical properties and thermal expansion, use 0/90 degree laminated materials or unidirectional laminated materials, and use woven materials or chopping materials when isotropic properties are desired. It is desirable.
炭素繊維を等方性炭素に接合する方法として、エポキシ樹脂やフェノール樹脂などの樹脂系接着剤を用いて接着する方法、タールピッチや自己焼結性炭素などの炭素質バインダーを用いた炭素結合による方法、あるいは型枠に填め込み、金属含浸時に接着させるなどの方法がとられる。 As a method of bonding carbon fibers to isotropic carbon, a method of bonding using a resin adhesive such as an epoxy resin or a phenol resin, or a carbon bond using a carbonaceous binder such as tar pitch or self-sintering carbon. A method such as a method or a method of filling in a mold and adhering at the time of metal impregnation is employed.
全体に含浸させた金属、すなわち、マトリックス金属は、前述のように、アルミニウム、銅、マグネシウムおよびそれらの合金などが適用可能だが、溶融温度が低いなどの理由から、アルミニウムがもっとも好ましい。 As described above, aluminum, copper, magnesium and alloys thereof can be applied to the metal impregnated in the whole, that is, matrix metal, but aluminum is most preferable because of its low melting temperature.
その含浸方法として、金型容器内に置いた等方性炭素/炭素繊維複合材をあらかじめ含浸温度まで加熱し、そこへ別に加熱溶融させた金属を流し込む。同時に1cm2あたり500kg以上の圧力をかけ、瞬時に炭素繊維間、等方性炭素細孔内部まで金属を圧入する。 As an impregnation method, an isotropic carbon / carbon fiber composite material placed in a mold container is heated to an impregnation temperature in advance, and separately heated and melted metal is poured therein. At the same time, a pressure of 500 kg or more per 1 cm 2 is applied, and the metal is instantaneously pressed between the carbon fibers and inside the isotropic carbon pores.
この製造方法により、金属と炭素がカーバイド生成反応を起こすことなく、金属基炭素繊維強化複合材料が製造できるが、上記金属含浸方法を可能にしたのは、含浸される炭素材料部分が、等方性炭素材と炭素繊維のサンドイッチ構造を成しているからである。 With this manufacturing method, a metal-based carbon fiber reinforced composite material can be manufactured without causing a carbide-forming reaction between the metal and carbon. However, the metal impregnation method enables the carbon material portion to be impregnated to be isotropic. This is because it has a sandwich structure of carbonaceous material and carbon fiber.
以上、本実施の形態及び本実施例にかかる金属基炭素繊維強化複合材料と、その製造方法を説明したが、上述した実施の形態及び実施例は、本発明の好適な実施の形態の一例を示すものであり、本発明はそれに限定されるものではなく、その要旨を逸脱しない範囲内において、種々変形実施が可能である。 The metal-based carbon fiber reinforced composite material and the manufacturing method thereof according to this embodiment and this example have been described above. However, the above-described embodiment and example are examples of the preferred embodiment of the present invention. The present invention is not limited thereto, and various modifications can be made without departing from the scope of the invention.
1 スキン材
2 コア材
1
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US7942637B2 (en) | 2008-12-11 | 2011-05-17 | General Electric Company | Sparcap for wind turbine rotor blade and method of fabricating wind turbine rotor blade |
CN104120457A (en) * | 2014-07-10 | 2014-10-29 | 上海大学 | Preparing method of metal-carbide-containing multi-layer multi-component composite material |
WO2018088045A1 (en) * | 2016-11-11 | 2018-05-17 | 昭和電工株式会社 | Metal-carbon particle composite material and method for manufacturing same |
JP2018075617A (en) * | 2016-11-11 | 2018-05-17 | 昭和電工株式会社 | Metal-carbon particle composite material and its manufacturing method |
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US7942637B2 (en) | 2008-12-11 | 2011-05-17 | General Electric Company | Sparcap for wind turbine rotor blade and method of fabricating wind turbine rotor blade |
CN104120457A (en) * | 2014-07-10 | 2014-10-29 | 上海大学 | Preparing method of metal-carbide-containing multi-layer multi-component composite material |
WO2018088045A1 (en) * | 2016-11-11 | 2018-05-17 | 昭和電工株式会社 | Metal-carbon particle composite material and method for manufacturing same |
JP2018075617A (en) * | 2016-11-11 | 2018-05-17 | 昭和電工株式会社 | Metal-carbon particle composite material and its manufacturing method |
JP2018075802A (en) * | 2016-11-11 | 2018-05-17 | 昭和電工株式会社 | Metal-carbon particle composite and production method of the same |
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