JPH02124766A - Production of carbon fiber reinforced carbonaceous material - Google Patents
Production of carbon fiber reinforced carbonaceous materialInfo
- Publication number
- JPH02124766A JPH02124766A JP63277348A JP27734888A JPH02124766A JP H02124766 A JPH02124766 A JP H02124766A JP 63277348 A JP63277348 A JP 63277348A JP 27734888 A JP27734888 A JP 27734888A JP H02124766 A JPH02124766 A JP H02124766A
- Authority
- JP
- Japan
- Prior art keywords
- binder
- carbon
- cured
- carbon fiber
- laminating
- 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.)
- Pending
Links
- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 14
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 14
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims description 9
- 239000003575 carbonaceous material Substances 0.000 title claims description 6
- 239000011230 binding agent Substances 0.000 claims abstract description 21
- 239000011159 matrix material Substances 0.000 claims abstract description 19
- 229920005989 resin Polymers 0.000 claims abstract description 18
- 239000011347 resin Substances 0.000 claims abstract description 18
- 239000006229 carbon black Substances 0.000 claims abstract description 14
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 12
- 238000010030 laminating Methods 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 238000002156 mixing Methods 0.000 claims description 8
- 238000003763 carbonization Methods 0.000 claims description 4
- 239000003960 organic solvent Substances 0.000 claims description 4
- 238000007731 hot pressing Methods 0.000 claims description 3
- 239000011344 liquid material Substances 0.000 claims description 2
- 238000005245 sintering Methods 0.000 claims 1
- 239000002245 particle Substances 0.000 abstract description 10
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 abstract description 8
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 abstract description 4
- 238000000465 moulding Methods 0.000 abstract description 4
- 238000010521 absorption reaction Methods 0.000 abstract description 3
- 238000001354 calcination Methods 0.000 abstract description 3
- 238000010000 carbonizing Methods 0.000 abstract description 3
- 239000011248 coating agent Substances 0.000 abstract description 3
- 238000000576 coating method Methods 0.000 abstract description 3
- 239000005011 phenolic resin Substances 0.000 abstract description 3
- 239000002904 solvent Substances 0.000 abstract description 3
- 239000012298 atmosphere Substances 0.000 abstract description 2
- 238000010438 heat treatment Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 18
- 238000010304 firing Methods 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- YLQBMQCUIZJEEH-UHFFFAOYSA-N Furan Chemical compound C=1C=COC=1 YLQBMQCUIZJEEH-UHFFFAOYSA-N 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 241000872198 Serjania polyphylla Species 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005470 impregnation Methods 0.000 description 2
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 2
- 239000002759 woven fabric Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000007770 graphite material Substances 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 238000010299 mechanically pulverizing process Methods 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229920002239 polyacrylonitrile Polymers 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 239000002296 pyrolytic carbon Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 239000011882 ultra-fine particle Substances 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Landscapes
- Ceramic Products (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、高密度性を備える炭素繊維強化炭素材(以下
、rC/CC/C材う)の製造方法に関する。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a method for manufacturing a carbon fiber reinforced carbon material (hereinafter referred to as rC/CC/C material) having high density.
〔従来の技術]
通常、C/C材は炭素繊維の織布、フェルト、トウなど
に熱硬化性樹脂に代表される低粘度のマトリックス結合
材を含浸または塗布し、これを積層熱圧成形したのち、
硬化および焼成炭化する工程によって製造される。とこ
ろが、この製造方法では、マトリックス結合材がプリプ
レグ化または積層熱圧成形の過程において外部に圧出、
逸散したり、焼成炭化時に揮散したりしてmm密度の低
下を招く問題点がある。このため、実用上十分な密度と
強度を付与するためには、−旦、製造したC/C材に炭
化性の樹脂を強制含浸して炭化するプロセスを繰り返す
か、CVD法により熱分解炭素を沈着する等の二次的な
補強処理を施す必要があり、工程の煩雑性と製造原価の
高騰をもたらす原因となっていた。[Prior art] C/C materials are usually made by impregnating or coating a carbon fiber woven fabric, felt, tow, etc. with a low-viscosity matrix binder represented by a thermosetting resin, and then laminating and hot-pressing the materials. after,
Manufactured by hardening and calcination carbonization processes. However, in this manufacturing method, the matrix binder is extruded to the outside during the prepreg formation or laminated hot press molding process.
There is a problem that it escapes or volatilizes during firing and carbonization, resulting in a decrease in mm density. Therefore, in order to impart sufficient density and strength for practical use, it is necessary to first repeat the process of forcibly impregnating the manufactured C/C material with carbonizable resin and carbonizing it, or to add pyrolytic carbon using the CVD method. It is necessary to perform secondary reinforcing treatment such as depositing, which makes the process complicated and increases manufacturing costs.
このような問題を解決するための手段として、炭素質も
しくは炭化性物質の微粉末をマトリックス結合材に混合
することによってtu織の高密度化と強度性能の向上を
図る方法が知られている。As a means for solving such problems, a method is known in which fine powder of carbonaceous or carbonizable material is mixed into a matrix binder to increase the density and improve the strength performance of the tu weave.
例えば、本出願人による特公昭60−52103号の発
明は、炭素質もしくは炭化性物質として粒度80−以下
のカーボンブラック、炭素、黒鉛あるいはフェノール系
、フラン系、ジヒニルベンゼンなどの硬化樹脂から選択
された微粉末を、マトリックス結合材に対して10〜6
0重世%の範囲で添加混合する点を特徴とするC/C材
の製造技術であり、その後にもピッチ生コークスのよう
な焼結可能な炭素の微粉末を熱可塑性樹脂からなる7ト
リノクス結合材に混合する方法(特開昭62−8336
9号公報)などが提案されている。For example, in the invention of Japanese Patent Publication No. 60-52103 by the present applicant, the carbonaceous or carbonizable material is selected from carbon black with a particle size of 80 or less, carbon, graphite, or cured resins such as phenolic, furan, and dihinylbenzene. fine powder to matrix binder at a ratio of 10 to 6
This is a C/C material manufacturing technology characterized by addition and mixing in the range of 0 weight percent, and after that, sinterable carbon fine powder such as pitch raw coke is added to 7 trinox made of thermoplastic resin. Method of mixing with binding material (Japanese Patent Application Laid-Open No. 62-8336
9) have been proposed.
〔発明が解決しようとする課題]
上記の方法においては、マトリックス結合材に混合する
炭素質もしくは炭化性物質の粉末粒度を可及的に小さく
することが望ましい。しかしながら、固形の炭素材、黒
鉛材などを機械的に粉砕して微粉化するには限界があり
、工業的粉砕ではせいぜい平均粒径としてII!mまで
が限度である。この点、カーボンブラックは生成段階で
の粒径(アグリゲート単位)が数+n+aという超微粉
末であって粉砕する必要がないため、本目的に適用する
ためには有利である。[Problems to be Solved by the Invention] In the above method, it is desirable to make the particle size of the powder of the carbonaceous or carbonizable substance mixed in the matrix binder as small as possible. However, there are limits to mechanically pulverizing solid carbon materials, graphite materials, etc., and in industrial pulverization, the average particle size is at most II! The limit is up to m. In this respect, carbon black is advantageous for application to this purpose because it is an ultrafine powder with a particle size (aggregate unit) of several +n+a at the production stage and does not need to be pulverized.
本発明は、このような観点からカーボンブランクのマト
リックス配合について再検討し、この使用に関する最適
な条件を見出して開発に至ったものである。The present invention was developed by reexamining the matrix composition of carbon blank from this viewpoint and finding the optimal conditions for its use.
〔課題を解決するための手段]
本発明に係るC/C材の製造方法は、炭素繊維にマトリ
ックス結合材を含浸または塗布して形成したプリプレグ
を積層熱圧成形したのち、硬化および焼成炭化して炭素
繊維強化炭素材を製造する方法において、カーボンブラ
ンクを10重世%以下の配合量で予め有機溶媒に均一分
散し、ついで熱硬化性樹脂を混合して形成した液状体を
マl−IJソクス結合材として用いることを構成上の特
徴とする。[Means for Solving the Problems] The method for manufacturing a C/C material according to the present invention involves laminating and hot-pressing a prepreg formed by impregnating or applying a matrix binder to carbon fibers, and then hardening and firing carbonization. In a method for producing a carbon fiber reinforced carbon material, a carbon blank is uniformly dispersed in an organic solvent in an amount of 10% or less, and then a thermosetting resin is mixed to form a liquid material, which is then mixed with a thermosetting resin. Its structural feature is that it is used as a sox binding material.
強化材となる炭素繊維は、目的に応じ平繊、綾織などの
織布、フェルトまたはトウの形態で用いれ、また、マト
リックス結合材の主成分となる熱硬化性樹脂としては、
フェノール系あるいはフラン系のような炭化性の高い液
状樹脂が使用される。Carbon fiber, which serves as a reinforcing material, is used in the form of plain fiber, woven fabric such as twill weave, felt, or tow, depending on the purpose, and the thermosetting resin, which is the main component of the matrix binding material, is
A highly carbonizable liquid resin such as a phenol-based or furan-based resin is used.
上記熱硬化性樹脂に混合されるカーボンブラックの種類
、性状等にはとくに制約はないが、出来るだけ粒径が大
きく、ストラフチャーの小さい性状のものを選定するこ
とが望ましい。好適な粒性状は、粒子径50nm以上、
DBP吸油1100m1/100g以下である。There are no particular restrictions on the type, properties, etc. of the carbon black to be mixed into the thermosetting resin, but it is desirable to select carbon black that has as large a particle size as possible and as small a structure as possible. Suitable particle properties include a particle size of 50 nm or more;
DBP oil absorption is 1100ml/100g or less.
カーボンブラックを熱硬化性樹脂に混合するには、まず
、カーボンブラックをエタノール、アセトンなどの有機
溶媒に添加し例えば超音波などの振動を与えて均一に分
散したのち、熱硬化性樹脂の初期縮合物を加える方法が
採られる。To mix carbon black with a thermosetting resin, first add carbon black to an organic solvent such as ethanol or acetone, apply vibrations such as ultrasonic waves to uniformly disperse it, and then perform initial condensation of the thermosetting resin. The method of adding things is adopted.
この際、カーボンブラックの配合量は、有機溶媒に対し
10重量%以下、好ましくは5〜10重璽%の範囲内に
設定することが重要で、これがlO重装置を越えると得
られるC/C材の組織密度が急激に低下する。また、熱
硬化性樹脂の混合量は、有i熔媒100重量部に対し1
00〜400重量部の範囲で設定することが望ましい。At this time, it is important to set the blending amount of carbon black to 10% by weight or less, preferably within the range of 5 to 10% by weight, based on the organic solvent. The tissue density of the wood decreases rapidly. In addition, the mixing amount of the thermosetting resin is 1 part by weight for 100 parts by weight of the solvent.
It is desirable to set it in the range of 00 to 400 parts by weight.
上記の混合順序と配合比率を併用することにより、熱硬
化性樹脂中にカーボンブラックが均質に分散した液状の
マトリックス結合材を形成することができる。By using the above mixing order and blending ratio in combination, it is possible to form a liquid matrix binder in which carbon black is homogeneously dispersed in the thermosetting resin.
このようにして形成されたカーボンブラックを含有する
マトリックス結合材を炭素繊維に含浸または塗布し、半
硬化してプリプレグを形成する。The carbon black-containing matrix binder thus formed is impregnated or applied onto carbon fibers and semi-cured to form a prepreg.
ついで、プリプレグを積層して熱圧成形したのち、マト
リックス結合材を加熱硬化し、更に非酸化性雰囲気中で
焼成炭化してC/C材を製造する。Next, prepregs are laminated and hot-press molded, and then the matrix binding material is heated and hardened, and then fired and carbonized in a non-oxidizing atmosphere to produce a C/C material.
なお、製造されたC/C材に、上記のカーボンブラック
含有マトリックス結合材を含浸もしくは塗布して焼成炭
化する処理を反復することもでき、こうすることにより
表面層部分の組織を一層緻密化することができる。Incidentally, it is also possible to repeat the process of impregnating or coating the manufactured C/C material with the carbon black-containing matrix binder and firing and carbonizing it, thereby further densifying the structure of the surface layer portion. be able to.
上記の製造過程で、マトリックス結合材中に介在するカ
ーボンブラックは熱硬化性樹脂と同伴して炭素繊維の編
目内部に容易に充填保持され、プリプレグ化または積層
熱圧工程における樹脂成分の圧出現象を阻止するととも
に、その超微粒特性により焼成炭化時に樹脂成分がtt
i散して生じる空隙の減少ならびに補填するために有効
作用する。In the above manufacturing process, the carbon black interposed in the matrix binder is easily filled and retained inside the carbon fiber mesh along with the thermosetting resin, and the resin component is squeezed out during the prepreg or lamination heat-pressing process. In addition, due to its ultra-fine particle characteristics, the resin component is
It acts effectively to reduce and compensate for voids caused by scattering.
これらの作用を介して組織の高密度化と強度の向上がも
たらされる。Through these actions, tissue densification and strength improvement are brought about.
以下、本発明を実施例に基づいて説明する。 Hereinafter, the present invention will be explained based on examples.
実施例1〜2、比較例1〜2
粒子径62n+a、 D B P吸油量87iffi/
100gの粒子性状を有するカーボンブラック〔東海カ
ーボン■製、5east V )を、0.5.10およ
び20重量%の各配合量でアセトンに加え、超音波装置
にかけて均一に分散させた。ついで、これにフェノール
樹脂液〔大日本インキ工業■製、P 5900)をアセ
トン100重量部に対し230重量部の割合で加え、超
音波装置により十分混合して懸濁させた。Examples 1-2, Comparative Examples 1-2 Particle size 62n+a, DBP oil absorption amount 87iffi/
100 g of carbon black (manufactured by Tokai Carbon ■, 5east V) having particle properties was added to acetone in amounts of 0.5, 10 and 20% by weight, and uniformly dispersed using an ultrasonic device. Next, a phenol resin liquid (manufactured by Dainippon Ink Industries, Inc., P5900) was added thereto at a ratio of 230 parts by weight to 100 parts by weight of acetone, and the mixture was thoroughly mixed and suspended using an ultrasonic device.
このようにして形成したマトリックス結合材に平織炭素
繊維布(ポリアクリロニトリル系高弾性タイプ)を浸漬
して含浸処理した。これを半硬化して得たプリプレグ(
FTi横150鰭、厚さ0.38mm)を14枚M層し
てモールドに入れ、加熱温度110 ’C1適用圧力2
0kg / cdの条件で熱圧成形した。A plain-woven carbon fiber cloth (highly elastic polyacrylonitrile type) was immersed into the matrix binding material thus formed for impregnation treatment. Prepreg obtained by semi-curing this (
14 M layers of FTi (150 fins horizontally, 0.38 mm thick) were placed in a mold, heating temperature 110'C1 applied pressure 2
Hot pressure molding was carried out under the condition of 0 kg/cd.
成形物を250°Cで完全に硬化したのち、窒素雰囲気
に保持した焼成炉に移し、5°C/hrの上昇速度で1
000°Cまで昇温し5時間に亘り焼成炭化した。After the molded product was completely cured at 250°C, it was transferred to a firing furnace maintained in a nitrogen atmosphere and heated at a rate of 5°C/hr for 1 hour.
The temperature was raised to 000°C and the mixture was fired and carbonized for 5 hours.
得られたC/C材にフェノール樹脂液を真空加圧下に含
浸して上記同様に1000°C再焼成する処理(再含浸
)を3回反復した。The process of impregnating the obtained C/C material with a phenol resin liquid under vacuum pressure and re-firing at 1000°C (re-impregnation) in the same manner as above was repeated three times.
このようにして製造したC/C材を、空気中10oo’
cの温度に30分間曝してそれぞれの重量減少の度合を
測定した。その結果を表1に示した。The C/C material manufactured in this way was
The degree of weight loss of each sample was measured by exposing it to a temperature of c for 30 minutes. The results are shown in Table 1.
表 1
表1の結果から、本発明のカーボンブランク含有マトリ
ックス結合材を用いた実施例1.2は、比較例に比べて
著しく組織密度が高く、酸化速度も大幅に低減している
ことが認められる。Table 1 From the results in Table 1, it was found that Example 1.2 using the carbon blank-containing matrix binder of the present invention had a significantly higher tissue density and a significantly lower oxidation rate than the comparative example. It will be done.
〔発明の効果]
以上のとおり、本発明によれば高密度、高強度のC/C
材を安価に製造することができるから、工業生産上の効
果は頗る大である。[Effect of the invention] As described above, according to the present invention, high-density, high-strength C/C
Since the material can be manufactured at low cost, the effect on industrial production is extremely large.
特許出願人 東海カーボン株式会社Patent applicant: Tokai Carbon Co., Ltd.
Claims (1)
て形成したプリプレグを積層熱圧成形したのち、硬化お
よび焼成炭化して炭素繊維強化炭素材を製造する方法に
おいて、カーボンブラックを10重量%以下の配合量で
予め有機溶媒に均一分散し、ついで熱硬化性樹脂を混合
して形成した液状体をマトリックス結合材として用いる
ことを特徴とする炭素繊維強化炭素材の製造方法。1. In a method of producing a carbon fiber reinforced carbon material by laminating and hot-pressing a prepreg formed by impregnating or applying a matrix binder to carbon fibers, and then curing and sintering carbonization, the blending amount of carbon black is 10% by weight or less. A method for producing a carbon fiber-reinforced carbon material, characterized in that a liquid material formed by uniformly dispersing carbon fiber in an organic solvent in advance and then mixing with a thermosetting resin is used as a matrix binder.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63277348A JPH02124766A (en) | 1988-11-04 | 1988-11-04 | Production of carbon fiber reinforced carbonaceous material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63277348A JPH02124766A (en) | 1988-11-04 | 1988-11-04 | Production of carbon fiber reinforced carbonaceous material |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH02124766A true JPH02124766A (en) | 1990-05-14 |
Family
ID=17582275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63277348A Pending JPH02124766A (en) | 1988-11-04 | 1988-11-04 | Production of carbon fiber reinforced carbonaceous material |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH02124766A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100565385B1 (en) * | 1998-10-28 | 2006-05-29 | 영성산업 주식회사 | Manufacturing method of light weight high strength carbon composite material |
US8137798B2 (en) * | 2006-08-07 | 2012-03-20 | Toray Industries, Inc. | Prepreg and carbon fiber reinforced composite materials |
JP2012218954A (en) * | 2011-04-05 | 2012-11-12 | Osaka Gas Chem Kk | Surface treated molded insulation material, method for producing the same, and surface coating agent used for this |
-
1988
- 1988-11-04 JP JP63277348A patent/JPH02124766A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100565385B1 (en) * | 1998-10-28 | 2006-05-29 | 영성산업 주식회사 | Manufacturing method of light weight high strength carbon composite material |
US8137798B2 (en) * | 2006-08-07 | 2012-03-20 | Toray Industries, Inc. | Prepreg and carbon fiber reinforced composite materials |
JP2012218954A (en) * | 2011-04-05 | 2012-11-12 | Osaka Gas Chem Kk | Surface treated molded insulation material, method for producing the same, and surface coating agent used for this |
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