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JPH0788261B2 - Method for producing carbon fiber reinforced carbon composite material - Google Patents
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JPH0788261B2 - Method for producing carbon fiber reinforced carbon composite material - Google Patents

Method for producing carbon fiber reinforced carbon composite material

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Publication number
JPH0788261B2
JPH0788261B2 JP61095263A JP9526386A JPH0788261B2 JP H0788261 B2 JPH0788261 B2 JP H0788261B2 JP 61095263 A JP61095263 A JP 61095263A JP 9526386 A JP9526386 A JP 9526386A JP H0788261 B2 JPH0788261 B2 JP H0788261B2
Authority
JP
Japan
Prior art keywords
composite material
temperature
carbon fiber
pitches
pressure
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
JP61095263A
Other languages
Japanese (ja)
Other versions
JPS62252371A (en
Inventor
公平 奥山
明男 加藤
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
Original Assignee
Mitsubishi Chemical Corp
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 filed Critical Mitsubishi Chemical Corp
Priority to JP61095263A priority Critical patent/JPH0788261B2/en
Publication of JPS62252371A publication Critical patent/JPS62252371A/en
Publication of JPH0788261B2 publication Critical patent/JPH0788261B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は炭素繊維強化炭素複合材料に関するものであ
る。詳しくはピツチ類をマトリツクス原料として優れた
特性を有する炭素繊維強化炭素複合材料を製造する方法
に関するものである。
TECHNICAL FIELD The present invention relates to a carbon fiber reinforced carbon composite material. More specifically, the present invention relates to a method for producing a carbon fiber reinforced carbon composite material having excellent properties by using pitches as a matrix raw material.

(従来の技術) 炭素繊維強化炭素複合材料(以下C/C複合材と略す)は
軽量、高強度であり耐熱、耐食性に優れているという特
徴を活してロケツトノズル、ノーズコーン、航空機のデ
イスクブレーキなどの航空宇宙材料や発熱体、ホツトプ
レス鋳型、その他の機械部品、原子炉用部材等に用いら
れている。
(Prior Art) Carbon fiber reinforced carbon composite materials (hereinafter abbreviated as C / C composite materials) are lightweight, high-strength, and have excellent heat resistance and corrosion resistance, making use of rocket nozzles, nose cones, and aircraft disks. It is used for aerospace materials such as brakes, heating elements, hot press molds, other mechanical parts, and reactor components.

従来C/C複合材は予め炭素繊維に樹脂、ピツチ等の有機
物マトリツクスを含浸しておき、成型・硬化させた後炭
化・黒鉛化する方法、あるいは科学気相蒸着法により炭
素繊維間に熱分解炭素を充填する方法で製造されてい
る。
In the conventional C / C composite material, carbon fibers have been impregnated in advance with an organic matrix such as resin or pitch, and they are molded / cured and then carbonized / graphitized, or they are thermally decomposed between carbon fibers by a chemical vapor deposition method. It is manufactured by the method of filling carbon.

これらの方法のうち、ピツチ類をマトリツクス原料とす
る方法は原料が安価であること、炭化収率が高いこと、
炭化の結果得られる炭素質が易黒鉛化性物質であり、C/
C複合材の性能発現上好ましいものであること、さらに
は用いる炭素繊維がピツチを原料とするものである場合
には繊維とのなじみが良く繊維とマトリツクスの接着性
が良くなる等の利点を有している。しかしながら、一方
ではピツチ類は炭化時の膨張が著しくそのためC/C複合
材のマトリツクスとして使用した場合にはC/C複合材に
焼きあげた時の保形性、寸法安定性が不良である、ある
いはC/C複合材の内部に多量の気孔、亀裂が発生し、そ
の後ピツチ含浸あるいは樹脂含浸一炭化の緻密化工程を
多数回繰返さなければ充分な特性を発現するに至らない
といつた欠点があつた。
Among these methods, the method of using Pitches as a matrix raw material is inexpensive raw material, high carbonization yield,
The carbonaceous material obtained as a result of carbonization is a graphitizable substance, and C /
C has the advantages that it is preferable in terms of performance manifestation, and that the carbon fiber used is made of pitch as the raw material, it has good compatibility with the fiber and good adhesion between the fiber and matrix. is doing. However, on the other hand, pits have a significant expansion during carbonization, and therefore when used as a matrix for C / C composites, the shape retention and dimensional stability when baked into C / C composites are poor. Alternatively, a large number of pores and cracks are generated inside the C / C composite material, and if the densification process of pitch-impregnated or resin-impregnated monocarbonization is not repeated many times, sufficient characteristics will not be expressed, which is a drawback. Atsuta

(発明が解決しようとする問題点) そこで従来は、ピツチ類をマトリツクス原料とした場合
のかかる欠点を回避する方法として成型後の炭化を、少
なくともピツチ類が炭素質化して強度を発現し始める60
0〜700℃の温度まではオートクレーブ中で加圧下に行な
う、いわゆる加圧炭化と称される方法が採用されてい
た。しかしながら、かかる方法においてもピツチ類の膨
張が完全に抑制されるわけではなく、また炭化のための
装置が大規模、複雑なものになるといつた問題を有して
いた。
(Problems to be solved by the invention) Therefore, in the past, as a method of avoiding such a drawback in the case where the pits were used as a matrix raw material, carbonization after molding was started, and at least the pits were carbonized to start developing strength.
A method called so-called carbonization under pressure, which is performed under pressure in an autoclave up to a temperature of 0 to 700 ° C, has been adopted. However, even in such a method, the expansion of pits is not completely suppressed, and there is always a problem when the apparatus for carbonization becomes large-scale and complicated.

(問題点を解決するための手段) そこで、本発明者はかかる問題点を解決すべく鋭意検討
した結果、炭素繊維にピツチ類を含浸した成型した後、
特定の処理を施すことにより上記の問題点を解決できる
ことを見い出し本発明に到達した。
(Means for Solving Problems) Therefore, the present inventor has made diligent studies to solve such problems, and after molding by impregnating carbon fibers with pitches,
The inventors have found that the above problems can be solved by performing a specific treatment, and have reached the present invention.

すなわち、本発明の目的は、簡便かつ安定して優れた特
性を有するピツチ類をマトリツクスとしたC/C複合材を
製造する方法を提供するものである。そしてその目的
は、ピツチ類をマトリツクス原料として炭素繊維強化炭
素複合材料を製造する方法において、炭素繊維にピッチ
類を含浸して加熱加圧成型し、引続いて、加圧状態のま
ま、成型温度より高く500℃以下の温度で成型体を保持
した後、炭化処理を行なうことを特徴とする炭素繊維強
化炭素複合材料の製造方法により容易に達成される。
That is, an object of the present invention is to provide a method for producing a C / C composite material which is simple and stable, and has excellent characteristics and has a matrix of pitches. And the purpose is a method for producing a carbon fiber reinforced carbon composite material using pitches as a matrix raw material, in which carbon fibers are impregnated with pitches and heated and pressure molded, and subsequently, in a pressurized state, at a molding temperature. This is easily achieved by a method for producing a carbon fiber-reinforced carbon composite material, which comprises performing carbonization treatment after holding the molded body at a higher temperature of 500 ° C. or less.

以下本発明を詳細に説明する。The present invention will be described in detail below.

本発明で使用されるマトリツクス原料としてのピツチ類
とは石炭タールピツチ、石油系残渣ピツチあるいは各種
合成ピツチ等から蒸留、熱処理、エアブローイングある
いは溶剤処理、沈降分離による特定成分の抽出等で得ら
れる成型に適した軟化温度を有する炭素質歴青物質であ
る。更に具体的にはメトラー法によつて得られる軟化点
が80℃以上、好ましくは200〜350℃の範囲にあり、かつ
300℃における留出分が10%未満である様なピツチ類が
好ましい。
Pits as a matrix raw material used in the present invention are coal tar pitch, petroleum-based residue pitch or various synthetic pitch, and the like, which are obtained by distillation, heat treatment, air blowing or solvent treatment, extraction of specific components by sedimentation separation, etc. A carbonaceous bituminous material having a suitable softening temperature. More specifically, the softening point obtained by the Mettler method is 80 ° C. or higher, preferably in the range of 200 to 350 ° C., and
Pitches having a distillate content of less than 10% at 300 ° C. are preferred.

また用いられる炭素繊維としては特に限定されるもので
はなくポリアクリロニトリル系、ピツチ系、炭素繊維、
あるいは気相熱分解法により得られる炭素繊維等であ
る。さらに繊維の形態としては、連続繊維、短繊維、フ
エルト状のものが用いられる。
The carbon fiber used is not particularly limited, but polyacrylonitrile-based, pitch-based, carbon fiber,
Alternatively, it is a carbon fiber or the like obtained by a vapor phase pyrolysis method. Further, as the form of the fibers, continuous fibers, short fibers, and felt-like ones are used.

炭素繊維は熔融状態のピツチ類を含浸した後に成型金型
中に配列させるか、あるいは金型中に繊維とピツチ類の
粉末を交互に積層してゆく方法等で配列される。
The carbon fibers are arranged by impregnating the melted pitches and then arranged in a molding die, or by alternately laminating fibers and powders of the pitches in the molding die.

繊維の使用量は適宜決定されるが、成型体の体積に対し
て通常20〜75%、好ましくは30〜60%となる様にするの
がよい。
The amount of the fiber used is appropriately determined, but it is usually 20 to 75%, preferably 30 to 60% with respect to the volume of the molded product.

炭素繊維およびマトリツクスとしてのピツチ類が充填さ
れた金型はその後加熱ヒータを備えた加圧機に載置さ
れ、まず無加圧状態でピツチ類を加熱熔融する。加熱の
程度は使用するピツチ類の軟化温度によつて異なつてく
るものであるが、ピツチ類が炭素繊維間に充分に浸透し
うる様な低粘度を示すまで、通常ピツチ類の軟化点より
も50〜150℃高い温度まで加熱されるべきである。ピツ
チ類が熔融した後加圧によつて所定の圧力通常5〜100k
g/cm2の圧力が印加され所定の形状に成型される。従来
では、成型後、金型は冷却され充分冷却された常圧に戻
して成型体を得ていたが、本発明では上記の成型処理に
引続いて成型温度より高い温度での保持を行なうことが
重要である。
The mold filled with carbon fibers and pitches as a matrix is then placed on a pressurizing machine equipped with a heater, and first, the pitches are heated and melted in a non-pressurized state. The degree of heating varies depending on the softening temperature of the pits used, but it is usually lower than the softening point of the pits until the pits show a low viscosity so that they can sufficiently penetrate between the carbon fibers. It should be heated to 50-150 ° C higher temperature. After the pitches are melted, pressurize to a predetermined pressure, usually 5 to 100k
A pressure of g / cm 2 is applied and it is molded into a predetermined shape. In the past, after molding, the mold was cooled and returned to a sufficiently cooled normal pressure to obtain a molded body, but in the present invention, following the above-mentioned molding treatment, holding at a temperature higher than the molding temperature is performed. is important.

すなわち、所定形状への成型が行なわれた後、加圧状態
のまま成型温度よりは高い温度すなわち、使用するピツ
チの軟化点により多少異なるが、通常50℃以上高い温度
へと移行される。この温度は実質的に炭化が起らない温
度であればよく、通常、300℃以上500℃以下の温度であ
り好ましくは380℃〜500℃の範囲である。500℃をこえ
る加熱温度では使用する材質によるが金型の劣化を引き
おこし、また得られる成型体が金型から脱離しがたくな
るという問題が生じ好ましくない。加熱処理は成型温度
から段階的あるいは連続的に徐々に昇温することが望ま
しいが成型温度から直ちに所定の保持温度まで昇温して
も本発明の効果が失なわれることはない。
That is, after being molded into a predetermined shape, the temperature is usually higher than the molding temperature in a pressurized state, that is, the temperature is higher by 50 ° C. or more, though it is somewhat different depending on the softening point of the pitch used. This temperature may be a temperature at which carbonization does not substantially occur, and is usually a temperature of 300 ° C. or higher and 500 ° C. or lower, preferably 380 ° C. to 500 ° C. A heating temperature of more than 500 ° C. is not preferable because it causes deterioration of the mold depending on the material used and the molded body obtained is difficult to separate from the mold. It is desirable that the heat treatment be gradually raised from the molding temperature stepwise or continuously, but the effect of the present invention is not lost even if the temperature is immediately raised from the molding temperature to a predetermined holding temperature.

保持時間としては使用されるピツチ類の軟化温度および
保持温度によつても異なつて来るが通常0.5〜100時間、
好ましくは3〜20時間の範囲である。
As the holding time, it depends on the softening temperature and holding temperature of the Pitches used, but usually 0.5 to 100 hours,
It is preferably in the range of 3 to 20 hours.

また成型体を保持する間の加圧状態は完全に無加圧でな
ければ加えられる圧力は特に限定されるものではない
が、成型時の圧力状態を維持するのが加圧操作等の点か
ら好ましい。
The pressure applied while holding the molded body is not particularly limited unless it is completely unpressurized, but maintaining the pressure during molding is in view of pressure operation and the like. preferable.

なお、成型体を保持する間にマトリツクスとしてのピツ
チ類の膨張による昇圧があるので保圧機構等を作動させ
危険な程に圧力が上昇しない様に注意することが必要で
ある。
It should be noted that while holding the molded body, there is a pressure increase due to the expansion of the pitches as a matrix, so it is necessary to operate the pressure maintaining mechanism and the like so that the pressure does not rise dangerously.

このようにして所定の温度、時間の保持が終了した後金
型を冷却し、常圧に戻して成型体を得、炭化処理を行な
う。炭化処理は常法に従つて行なわれ、例えば成型体を
パツキングコース中に埋め込んで行なう様な方法がなさ
れる。さらに必要ならばピツチ含浸あるいは樹脂含浸−
再炭化の緻密化処理を繰返して行ない、あるいは更に黒
鉛化処理を行なつてC/C複合材を得ることが出来る。
After the holding of the predetermined temperature and time is completed in this way, the mold is cooled and returned to normal pressure to obtain a molded body, and carbonized. The carbonization treatment is performed according to a conventional method, for example, a method in which the molded body is embedded in a packing course. If necessary, pitch impregnation or resin impregnation-
It is possible to obtain a C / C composite material by repeating the densification treatment of recarbonization or further performing graphitization treatment.

(効 果) 本発明によれば得られるC/C複合材は炭化処理による形
の崩れや、寸法の変化も小さく、また気孔・亀裂の発生
が少ないため充分に高密度であり、従つて優れた特性を
示すものである。
(Effect) The C / C composite material obtained according to the present invention is small in shape change and dimensional change due to carbonization treatment, and has sufficiently few densities of pores and cracks to have a sufficiently high density, which is excellent. It shows the characteristics.

以下、本発明を実施例でもつてより具体的に説明する
が、本発明はその要旨をこえない限り下記の実施例に限
定されるものではない。
Hereinafter, the present invention will be described in more detail with reference to Examples, but the present invention is not limited to the following Examples unless it exceeds the gist.

実施例1 厚さ2mm、幅10mm、長さ230mmの金型中に3000フイラメン
トの炭素繊維束(引張強度200kg/mm2、同弾性率15ton/m
m2)とコールタールピツチから熱処理によつて得た軟化
点240℃のピツチの60メツシユ篩下の微粉とを交互に積
層した。次いで加熱ヒータを備えた加圧機にこの金型を
載置し330℃まで加熱した。金型が330℃に達してから15
分後に加圧を開始し50kg/cm2の圧力下に30分間保持し成
型を行なつた。引続いてその加圧状態を維持したまま20
℃/Hrの割合で450℃まで昇温し、さらに450℃に到達後1
0時間そのままの状態で保持した。なお、この際加圧機
の保圧機構を作動させ圧力が200kg/cm2を越えない様に
した。その後金型を冷却し、常圧に戻して成型体を得
た。得られた成型体の繊維体積含有率は約50%であり、
嵩密度は1.52g/cm8であつた。
Example 1 A carbon fiber bundle of 3000 filaments (tensile strength 200 kg / mm 2 , elastic modulus 15 ton / m) in a mold having a thickness of 2 mm, a width of 10 mm and a length of 230 mm.
m 2 ) and fine powder obtained by heat treatment from coal tar pits and having a softening point of 240 ° C. under the 60 mesh mesh sieve were alternately laminated. Then, this mold was placed on a pressurizing machine equipped with a heater and heated to 330 ° C. 15 after the mold reaches 330 ℃
After a lapse of minutes, pressurization was started, and the pressure was maintained at 50 kg / cm 2 for 30 minutes for molding. Continue to maintain the pressurized state 20
The temperature was raised to 450 ° C at the ratio of ℃ / Hr, and after reaching 450 ° C 1
It was kept as it was for 0 hours. At this time, the pressure holding mechanism of the pressurizer was operated so that the pressure did not exceed 200 kg / cm 2 . After that, the mold was cooled and returned to normal pressure to obtain a molded body. The fiber volume content of the obtained molded body is about 50%,
The bulk density was 1.52 g / cm 8 .

次いでこの成型体をパツキングコークス中に埋め込み60
0℃までは10℃/Hr、その後1000℃までは30℃/Hrの割合
で昇温して炭化処理した。炭化処理による成型体の体積
変化は−3.3%であり、また得られたC/C複合材の嵩密度
は1.54g/cm8であつた。
Then, this molded body was embedded in packing coke 60
Carbonization treatment was performed by raising the temperature up to 0 ° C at a rate of 10 ° C / Hr and then up to 1000 ° C at a rate of 30 ° C / Hr. The change in volume of the molded body due to carbonization was -3.3%, and the bulk density of the obtained C / C composite material was 1.54 g / cm 8 .

さらに、このC/C複合材をピツチ含浸し、再炭化するプ
ロセスを4回繰返し緻密化処理されたC/C複合材を得
た。このC/C複合材の嵩密度は1.72g/cm8であつた。ま
た、緻密化処理によるC/C複合材の体積変化はほとんど
なかつた。このC/C複合材を長さ45mmの試験片に切断
し、スパン間距離40mm、歪速度1mm/minで3点曲げ試験
を行い曲げ強度、同弾性率の測定を行なつた。その結果
4点の試験片の平均値として曲げ強度55kg/mm2、同弾性
率13.5ton/mm2であつた。
Further, the process of impregnating the C / C composite material with pitch was repeated four times to obtain a densified C / C composite material. The bulk density of this C / C composite material was 1.72 g / cm 8 . In addition, the volume change of the C / C composite material due to the densification treatment was almost nonexistent. This C / C composite material was cut into a test piece having a length of 45 mm, and a three-point bending test was performed at a span distance of 40 mm and a strain rate of 1 mm / min to measure the bending strength and the same elastic modulus. As a result, the bending strength was 55 kg / mm 2 and the elastic modulus was 13.5 ton / mm 2 as an average value of the four test pieces.

実施例2 実施例1と同様にして厚さ2mm、幅10mm、長さ230mmの金
型中に3000フイラメントの炭素繊維束と軟化点240℃の
ピツチ粉とを交互に積層し、次いで加圧機に載置した後
330℃まで加熱した。金型が330℃に達してから15分後に
加圧を開始し50kg/cm2でもつて30分間保持し成型を行な
つた。引続いてその加圧状態のまま、380℃まで昇温
し、5時間保持した。さらに430℃に昇温して3時間、4
80℃に昇温して2時間保持した。なおこの際圧力は200k
g/cm2を越えない様にした。得られた成型体の繊維体積
含有率は約50%であり、嵩密度は1.54g/cm8であつた。
Example 2 Similar to Example 1, carbon fiber bundles of 3000 filaments and Pitch powder having a softening point of 240 ° C. were alternately laminated in a mold having a thickness of 2 mm, a width of 10 mm and a length of 230 mm, and then placed in a press. After placing
Heated to 330 ° C. Pressing was started 15 minutes after the temperature of the mold reached 330 ° C., the pressure was kept at 50 kg / cm 2 and was held for 30 minutes to perform molding. Subsequently, in the pressurized state, the temperature was raised to 380 ° C. and kept for 5 hours. Further raise the temperature to 430 ° C for 3 hours, 4
The temperature was raised to 80 ° C. and kept for 2 hours. At this time, the pressure is 200k
I tried not to exceed g / cm 2 . The fiber volume content of the obtained molded product was about 50%, and the bulk density was 1.54 g / cm 8 .

次いで実施例1と同様にこの成型体を炭化処理した結
果、嵩密度1.56g/cm8のC/C複合材が得られた。また炭化
処理による成型体の体積変化は−2.7%であつた。
Next, as a result of carbonizing this molded body as in Example 1, a C / C composite material having a bulk density of 1.56 g / cm 8 was obtained. The volume change of the molded product due to carbonization was -2.7%.

さらにこのC/C複合材をピツチ含浸し、再炭化するプロ
セスを4回繰返し緻密化処理されたC/C複合材を得た。
このC/C複合材の嵩密度は1.73g/cm8であつた。また、緻
密化処理によるC/C複合材の体積変化はほとんどなかつ
た。
Further, this C / C composite material was impregnated with pitch and recarbonization was repeated 4 times to obtain a densified C / C composite material.
The bulk density of this C / C composite material was 1.73 g / cm 8 . In addition, the volume change of the C / C composite material due to the densification treatment was almost nonexistent.

このC/C複合材の曲げ強度、同弾性率を実施例1と同様
にして測定した結果4点の試験片の平均値としてそれぞ
れ59kg/mm2、14.0ton/mm2であつた。
The flexural strength and the elastic modulus of this C / C composite material were measured in the same manner as in Example 1, and the average values of the four test pieces were 59 kg / mm 2 and 14.0 ton / mm 2 , respectively.

比較例 実施例1と同様にして厚さ2mm、幅10mm、長さ230mmの金
型中に3000フイラメントの炭素繊維束と軟化点240℃の
ピツチ粉とを交互に積層し、次いで加圧機に載置した後
330℃まで加熱した。金型が330℃に達してから15分後に
加圧を開始し50kg/cm2でもつて30分間保持し成型を行な
つた。その後金型を冷却し、常圧に戻して成型体を得
た。得られた成型体の繊維体積含有率は約50%であり、
嵩密度は1.47g/cm8であつた。
Comparative Example Similar to Example 1, a carbon fiber bundle of 3000 filaments and pitch powder having a softening point of 240 ° C. were alternately laminated in a mold having a thickness of 2 mm, a width of 10 mm and a length of 230 mm, and then placed on a press. After placing
Heated to 330 ° C. Pressing was started 15 minutes after the temperature of the mold reached 330 ° C., the pressure was kept at 50 kg / cm 2 and was held for 30 minutes to perform molding. After that, the mold was cooled and returned to normal pressure to obtain a molded body. The fiber volume content of the obtained molded body is about 50%,
The bulk density was 1.47 g / cm 8 .

次いで実施例1と同様にこの成型体を炭化処理した結
果、嵩密度1.18g/cm8のC/C複合材が得られた。また炭化
処理による成型体の体積変化は+22.8%であつた。さら
にこのC/C複合材をピツチ含浸し、再炭化するプロセス
を4回繰返し緻密化処理されたC/C複合材を得た。このC
/C複合材の嵩密度は1.38g/cm8であつた。また、緻密化
処理によるC/C複合材の体積変化はほとんどなかつた。
Next, as a result of carbonizing this molded body in the same manner as in Example 1, a C / C composite material having a bulk density of 1.18 g / cm 8 was obtained. The volume change of the molded product due to carbonization was + 22.8%. Further, this C / C composite material was impregnated with pitch and recarbonization was repeated 4 times to obtain a densified C / C composite material. This C
The bulk density of the / C composite material was 1.38 g / cm 8 . In addition, the volume change of the C / C composite material due to the densification treatment was almost nonexistent.

このC/C複合材の曲げ強度、同弾性率を実施例1と同様
にして測定した結果4点の試験片の平均値としてそれぞ
れ21kg/mm2、5.7ton/mm2であつた。
The flexural strength and elastic modulus of this C / C composite material were measured in the same manner as in Example 1, and the average values of the four test pieces were 21 kg / mm 2 and 5.7 ton / mm 2 , respectively.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】ピッチ類をマトリックス原料として炭素繊
維強化炭素複合材料を製造する方法において、炭素繊維
にピッチ類を含浸して加熱加圧成型し、引続いて、加圧
状態のまま、成型温度より高く500℃以下の温度で成型
体を保持した後、炭化処理を行なうことを特徴とする炭
素繊維強化炭素複合材料の製造方法。
1. A method for producing a carbon fiber-reinforced carbon composite material using pitches as a matrix raw material, wherein carbon fibers are impregnated with pitches and heated and pressure-molded, and subsequently, at a molding temperature in a pressurized state. A method for producing a carbon fiber-reinforced carbon composite material, which comprises performing a carbonization treatment after holding a molded body at a temperature higher than or equal to 500 ° C.
JP61095263A 1986-04-24 1986-04-24 Method for producing carbon fiber reinforced carbon composite material Expired - Lifetime JPH0788261B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61095263A JPH0788261B2 (en) 1986-04-24 1986-04-24 Method for producing carbon fiber reinforced carbon composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61095263A JPH0788261B2 (en) 1986-04-24 1986-04-24 Method for producing carbon fiber reinforced carbon composite material

Publications (2)

Publication Number Publication Date
JPS62252371A JPS62252371A (en) 1987-11-04
JPH0788261B2 true JPH0788261B2 (en) 1995-09-27

Family

ID=14132877

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61095263A Expired - Lifetime JPH0788261B2 (en) 1986-04-24 1986-04-24 Method for producing carbon fiber reinforced carbon composite material

Country Status (1)

Country Link
JP (1) JPH0788261B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01264966A (en) * 1987-12-28 1989-10-23 Kawasaki Heavy Ind Ltd Production of carbon material and carbon/carbon composite material
JPH02129069A (en) * 1988-11-10 1990-05-17 Kawasaki Heavy Ind Ltd Production of carbon material and carbon/carbon composite material
JPH01305857A (en) * 1988-06-03 1989-12-11 Nippon Oil Co Ltd Production of carbon/carbon composite material
JPH02258676A (en) * 1989-03-31 1990-10-19 Kawasaki Heavy Ind Ltd Production of carbon/carbon composite material

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62212263A (en) * 1986-03-13 1987-09-18 日本鉱業株式会社 Manufacture of carbon-carbon fiber composite material

Also Published As

Publication number Publication date
JPS62252371A (en) 1987-11-04

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