JPH0114340B2 - - Google Patents

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Publication number
JPH0114340B2
JPH0114340B2 JP60067781A JP6778185A JPH0114340B2 JP H0114340 B2 JPH0114340 B2 JP H0114340B2 JP 60067781 A JP60067781 A JP 60067781A JP 6778185 A JP6778185 A JP 6778185A JP H0114340 B2 JPH0114340 B2 JP H0114340B2
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JP
Japan
Prior art keywords
carbon fibers
fibers
strength
resin
minutes
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
Application number
JP60067781A
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Japanese (ja)
Other versions
JPS61231265A (en
Inventor
Toshio Iharaki
Hiroshi Tanji
Hiroto Imamura
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.)
Asahi Chemical Industry Co Ltd
Original Assignee
Asahi Chemical Industry 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 Asahi Chemical Industry Co Ltd filed Critical Asahi Chemical Industry Co Ltd
Priority to JP6778185A priority Critical patent/JPS61231265A/en
Publication of JPS61231265A publication Critical patent/JPS61231265A/en
Publication of JPH0114340B2 publication Critical patent/JPH0114340B2/ja
Granted legal-status Critical Current

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  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Inorganic Fibers (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

(産業上の利用分野) 本発明は、高強度でかつ樹脂との接着性の優れ
たアクリル系繊維を前駆体とする高性能炭素繊維
の製造法に関する。 (従来の技術) 炭素繊維は、強度、弾性率等に優るため、各種
複合材料の強化繊維として、航空宇宙用途、工業
用材料、スポーツ用品等に使用されている。しか
しながら、炭素繊維をこれら複合材料として使用
する場合、炭素繊維自体の強度、弾性率等の他に
樹脂等マトリツクス材料との接着性が重要であ
り、これら諸特性が兼ね具わつて始めて有用な複
合材料が得られる。従つて、市販される炭素繊維
は何らかの方法で表面処理されているのが通例で
ある。 一方、強度がより向上した炭素繊維を製造する
方法としては、前駆体の製造工程における改良と
炭素化工程における改良とが数多く提案されてい
る。炭素化工程における改良の中には、炭素化を
特殊な雰囲気中で行う方法が提案されている(特
公昭47−7686号、特公昭47−29935号、特開昭59
−168129号)。特に、特開昭59−168129号には耐
炎化処理したアクリル系繊維を、塩化水素0.2〜
10容量%、酸素0.2〜4容量%および不活性ガス
を含有する雰囲気中で加熱することによつて高強
度を有する炭素繊維を得ることを記載している。
この公報によれば、上記の雰囲気中で加熱して得
た炭素繊維は、塩化水素と不活性ガスとからなる
雰囲気(酸素を含まない)中で加熱したものおよ
び塩化水素と不活性ガスと多量の酸素とからなる
雰囲気中で加熱したものと比較して、引張強さお
よび曲げ強度に優れ、また、製造工程での単糸切
れも少ないとされている。しかしながら、上記公
報に記載される雰囲気中で加熱処理して得た炭素
繊維を複合材料として使用する場合、マトリツク
ス樹脂との接着性に劣り、複合材料の層間剪断強
度および耐疲労性が劣る。 他方、特公昭48−42812号には、無機酸およ
び/または有機酸の水溶液中で炭素繊維を陽極酸
化することによつて表面積が増大した炭素繊維が
得られ、ひいては、剪断力および屈曲力に優れた
複合材を得ることができると記載されている。し
かしながら、得られる複合材料の層間剪断強度お
よび耐疲労性は十分満足できるものではない。 〔発明が解決しようとする問題点〕 本発明者らは、高強度でしかも樹脂との接着性
に優れた高性能炭素繊維を製造する方法について
鋭意検討した結果、炭素化工程で得られる原料炭
素繊維と表面処理工程との関係が密接に関係する
との知見を得、さらに検討を重ねた結果、意外に
も、上記特開昭59−168129号において、高強度炭
素繊維を得るのに好ましくないとされている。塩
化水素を不活性ガスをからなる雰囲気(酸素を含
まない)中で熱処理して得た炭素繊維に特定の条
件下に電解処理することによつて、高強度で、し
かも層間剪断強度および耐疲労性に優れた複合材
料を提供し得る炭素繊維が得られることを見出し
た。 (問題点を解決するための手段) 本発明は、アクリル系繊維を前駆体として高強
度でかつ樹脂との接着性に優れた炭素繊維を製造
するに際し、アクリル系繊維を耐炎化処理後、塩
化水素を少くとも1容量%以上含み実質的に酸素
を含まない不活性ガス雰囲気中600〜1600℃で炭
素化し、続いて、アルカリ金属及び塩素を含まな
い電解質中で10mA〜3Aの電流を0.1〜10分間適
用して炭素繊維を陽極とし電解処理することを特
徴とする高性能炭素繊維の製造法である。 本発明におけるアクリル系繊維とは、ポリアク
リロニトリルまたは、少くとも90重量%以上のア
クリロニトリルと他の共重合し得る単量体、例え
ばアクリル酸メチル等のアクリル酸エステル、ア
クリル酸、メタクリル酸、イタコン酸等のカルボ
ン酸、更にはアクリルアミド、アリルスルフオン
酸等との共重合体からなる繊維を指す。これらの
繊維は、湿式紡糸法、乾式紡糸法、乾−湿式紡糸
法等で得られる長繊維であつて、それらの製法は
特に限定されず、従来公知の方法を採ることがで
きる。このアクリル系繊維を耐炎化処理する方法
についても従来公知の方法を採ることができる。
一般には、200℃ないし350℃の範囲で低温側から
徐々に高温側へと何段かに分けて空気中で熱処理
するのが通例である。 本発明において炭素化工程は600℃ないし1600
℃の温度領域で塩化水素を少くとも1容量%含
み、実質的に酸素を含まない不活性ガス雰囲気中
で行なう。600℃未満の温度領域で塩化水素ガス
を供給しても強度向上が実質的に認められず、ま
た、600℃ないし1600℃の温度領域で塩化水素の
含有量が1容量%より少ないと得られる炭素繊維
に強度向上効果がみられない。また塩化水素含有
量の上限は20%程度であり、これを超えて含有さ
せてもそれに見合う効果が得難く、また、使用済
み排ガスの処理のため多額の費用を要するので工
業的に不利である。この炭素化時の雰囲気ガス中
に若干の酸素ガスが混入しても0.1容量%程度以
下であればさしつかえない。これは、工業的に実
施する場合供給糸によつて炭素化炉内にもち込ま
れる酸素量および炭素化装置のシール部分から若
干混入する酸素量にほぼ相当する。 上述のようにして得られる高強度の炭素繊維
は、そのままでは層間剪断強度で示される樹脂と
の接着性に劣る。従つて、本発明においてはアル
カリ金属及び塩素を含まない電解質中で炭素繊維
を陽極として電解処理する。電解質としてアルカ
リ金属または塩素を含むものを用いた場合は樹脂
との接着性が不充分であり、また、バラツキの大
きいものとなる。この理由は明確ではないが、炭
素化工程で炭素繊維表面に付着した塩化水素また
は塩素が何らかの悪影響を及ぼしているものと推
定される。 本発明で使用される電解質としては強酸、弱酸
及びそれらのアンモニウム塩等が挙げられる。例
えば、硫酸、硝酸、リン酸、硫酸アンモニウム、
硝酸アンモニウム、炭酸アンモニウム、及びこれ
らの混合物等が有用であつて、特に硝酸が最も好
ましい。 これら電解質の濃度は通常0.1%ないし10%程
度である。電解液の温度は一般に70℃以下であ
る。電解時間は0.1分ないし10分間程度である。
また、電解条件としては一般に電流が10mAない
し3A程度で、電解電圧は0.5ないし20ボルトで行
なわれ、好ましくは電流が50mAないし1A、電
解電圧は1ないし5ボルトである。これらの範囲
より低い電解条件では樹脂との接着性に劣り、他
方、電解時間および電流がそれぞれ過大になると
電解による表面処理が過剰になり、炭素繊維の強
度の低下量が著しく大きくなるとともに、樹脂と
の接着性も低下し始める。 (発明の効果) 上述のように特定の炭素化条件下に炭素化し、
さらに特定の表面処理(電解処理)条件下に処理
して得られる炭素繊維は、高強度でしかも樹脂と
の接着性に優れたバランスのとれた高性能炭素繊
維である。 (実施例) 以下に実施例を挙げて本発明の方法を具体的に
説明する。 実施例 1 アクリロニトリル97重量%を含むポリマーを常
法に従つて硝酸を溶媒として湿式紡糸し、単糸繊
度1.3デニール、12000フイラメントの長繊維を得
た。このプリカーサーを240℃の空気中で30分さ
らに260℃の空気中で40分かけて熱処理し、耐炎
化糸を得た。この耐炎化糸を用いて表―1に示す
ような各種炭素化及び表面処理条件で炭素繊維を
得た。なお、電解時間は1分であつた。これらの
炭素繊維ストランドの強度は、JISR7601に示さ
れる樹脂含浸ストランド試験法に準拠して測定し
た。樹脂処方は同解説例2を用いた。層間剪断強
度は次の方法で測定した。先ず、テトラグリシジ
ルジアミノジフエニルメタン100重量部、ジアミ
ノジフエニルスルホン35重量部、三弗化ホウソモ
ノメチルアミン1.5重量部を加えたメチルエチル
ケトン溶液中に炭素繊維を含浸させて、一方向の
プリプレグを作成した。このプリプレグを130℃
×60分、次いで、180℃×120分で加熱硬化させて
平板状複合材を作成した。次いで、インストロン
を用いてL/D=4の条件で三点曲げシヨートビ
ーム法で層間剪断強度を測定した。
(Industrial Application Field) The present invention relates to a method for producing high-performance carbon fibers using acrylic fibers having high strength and excellent adhesiveness to resin as a precursor. (Prior Art) Carbon fibers have excellent strength, elastic modulus, etc., and are therefore used as reinforcing fibers in various composite materials for aerospace applications, industrial materials, sporting goods, and the like. However, when carbon fibers are used as these composite materials, in addition to the strength and elastic modulus of the carbon fibers themselves, adhesion with matrix materials such as resins is important. Materials are obtained. Therefore, commercially available carbon fibers are usually surface-treated in some way. On the other hand, as a method for producing carbon fibers with further improved strength, many improvements in the precursor production process and in the carbonization process have been proposed. Among the improvements in the carbonization process, a method of carrying out carbonization in a special atmosphere has been proposed (Japanese Patent Publication No. 47-7686, Japanese Patent Publication No. 47-29935, Japanese Unexamined Patent Application Publication No. 1987-59).
−168129). In particular, in JP-A-59-168129, flame-retardant acrylic fibers are made with hydrogen chloride of 0.2~
It is described that carbon fibers having high strength can be obtained by heating in an atmosphere containing 10% by volume, 0.2 to 4% by volume of oxygen, and an inert gas.
According to this publication, carbon fibers obtained by heating in the above atmosphere include those heated in an atmosphere (not containing oxygen) consisting of hydrogen chloride and an inert gas, and those heated in an atmosphere consisting of hydrogen chloride and an inert gas (not containing oxygen), and carbon fibers obtained by heating in the above atmosphere. It is said that it has superior tensile strength and bending strength, and is less likely to break single filaments during the manufacturing process, compared to those heated in an atmosphere consisting of oxygen. However, when carbon fibers obtained by heat treatment in the atmosphere described in the above-mentioned publication are used as a composite material, the adhesion with the matrix resin is poor, and the interlaminar shear strength and fatigue resistance of the composite material are poor. On the other hand, Japanese Patent Publication No. 48-42812 discloses that by anodizing carbon fibers in an aqueous solution of an inorganic acid and/or an organic acid, carbon fibers with increased surface area are obtained, and as a result, carbon fibers with increased shear and bending forces are obtained. It is stated that an excellent composite material can be obtained. However, the interlaminar shear strength and fatigue resistance of the resulting composite material are not fully satisfactory. [Problems to be Solved by the Invention] As a result of extensive research into a method for producing high-performance carbon fibers that have high strength and excellent adhesion to resin, the present inventors found that the raw material carbon obtained in the carbonization process After finding out that there is a close relationship between fibers and the surface treatment process, and as a result of further investigation, we unexpectedly found that the above-mentioned Japanese Patent Application Laid-Open No. 59-168129 found that it was not desirable for obtaining high-strength carbon fibers. has been done. Carbon fibers obtained by heat-treating hydrogen chloride in an inert gas atmosphere (no oxygen) are electrolytically treated under specific conditions to achieve high strength, interlaminar shear strength, and fatigue resistance. It has been discovered that carbon fiber can be obtained that can provide a composite material with excellent properties. (Means for Solving the Problems) The present invention, when producing carbon fibers having high strength and excellent adhesion to resin using acrylic fibers as a precursor, the acrylic fibers are subjected to flame-retardant treatment and then chlorinated. Carbonization at 600-1600°C in an inert gas atmosphere containing at least 1% by volume of hydrogen and substantially oxygen-free, followed by a current of 10mA-3A at 0.1-1600°C in an alkali metal- and chlorine-free electrolyte. This is a method for producing high-performance carbon fiber, which is characterized by applying electrolytic treatment for 10 minutes and using the carbon fiber as an anode. The acrylic fiber in the present invention refers to polyacrylonitrile or other monomers that can be copolymerized with at least 90% by weight of acrylonitrile, such as acrylic esters such as methyl acrylate, acrylic acid, methacrylic acid, and itaconic acid. It refers to fibers made of copolymers with carboxylic acids such as acrylamide, allylsulfonic acid, etc. These fibers are long fibers obtained by a wet spinning method, a dry spinning method, a dry-wet spinning method, etc., and the manufacturing method thereof is not particularly limited, and conventionally known methods can be used. Conventionally known methods can be used for flame-proofing the acrylic fibers.
Generally, the heat treatment is carried out in air in several stages from a low temperature side to a gradually high temperature side within the range of 200°C to 350°C. In the present invention, the carbonization step is carried out at temperatures ranging from 600℃ to 1600℃.
C. in an inert gas atmosphere containing at least 1% by volume of hydrogen chloride and substantially free of oxygen. Even if hydrogen chloride gas is supplied in a temperature range below 600°C, no substantial improvement in strength is observed, and in a temperature range between 600°C and 1600°C, strength improvement is obtained when the hydrogen chloride content is less than 1% by volume. Carbon fiber does not show any strength improvement effect. Furthermore, the upper limit of the hydrogen chloride content is approximately 20%, and even if it is contained in excess of this, it is difficult to obtain a commensurate effect, and a large amount of cost is required to treat the used exhaust gas, which is industrially disadvantageous. . Even if a small amount of oxygen gas is mixed into the atmospheric gas during carbonization, there is no problem as long as it is about 0.1% by volume or less. This approximately corresponds to the amount of oxygen brought into the carbonization furnace by the supply thread and the amount of oxygen slightly mixed in from the sealing part of the carbonization device in the case of industrial implementation. The high-strength carbon fibers obtained as described above have poor adhesion to resin as indicated by interlaminar shear strength. Therefore, in the present invention, electrolytic treatment is performed using carbon fiber as an anode in an electrolyte that does not contain alkali metals and chlorine. If an electrolyte containing an alkali metal or chlorine is used, the adhesion to the resin will be insufficient and will be highly variable. Although the reason for this is not clear, it is presumed that hydrogen chloride or chlorine adhering to the carbon fiber surface during the carbonization process has some adverse effect. Electrolytes used in the present invention include strong acids, weak acids, ammonium salts thereof, and the like. For example, sulfuric acid, nitric acid, phosphoric acid, ammonium sulfate,
Ammonium nitrate, ammonium carbonate, and mixtures thereof are useful, with nitric acid being most preferred. The concentration of these electrolytes is usually about 0.1% to 10%. The temperature of the electrolyte is generally below 70°C. Electrolysis time is about 0.1 to 10 minutes.
The electrolysis conditions are generally about 10 mA to 3 A and an electrolytic voltage of 0.5 to 20 volts, preferably a current of 50 mA to 1 A and an electrolytic voltage of 1 to 5 volts. Electrolytic conditions lower than these ranges will result in poor adhesion to the resin. On the other hand, if the electrolytic time and current are excessive, the surface treatment by electrolysis will be excessive, resulting in a significant decrease in the strength of the carbon fiber, and The adhesion with the material also begins to deteriorate. (Effect of the invention) Carbonized under specific carbonization conditions as described above,
Further, the carbon fiber obtained by processing under specific surface treatment (electrolytic treatment) conditions is a well-balanced high-performance carbon fiber that has high strength and excellent adhesiveness to resin. (Example) The method of the present invention will be specifically explained below with reference to Examples. Example 1 A polymer containing 97% by weight of acrylonitrile was wet-spun using nitric acid as a solvent according to a conventional method to obtain long fibers with a single fiber fineness of 1.3 denier and 12,000 filaments. This precursor was heat-treated in air at 240°C for 30 minutes and then in air at 260°C for 40 minutes to obtain a flame-resistant yarn. Using this flame-resistant yarn, carbon fibers were obtained under various carbonization and surface treatment conditions as shown in Table 1. Note that the electrolysis time was 1 minute. The strength of these carbon fiber strands was measured in accordance with the resin-impregnated strand test method specified in JISR7601. The same Explanation Example 2 was used for the resin formulation. The interlaminar shear strength was measured by the following method. First, carbon fibers were impregnated in a methyl ethyl ketone solution containing 100 parts by weight of tetraglycidyl diaminodiphenylmethane, 35 parts by weight of diaminodiphenyl sulfone, and 1.5 parts by weight of borosomonomethylamine trifluoride to create a unidirectional prepreg. . This prepreg is heated to 130℃.
x 60 minutes, then heated and cured at 180°C x 120 minutes to create a flat composite material. Next, the interlaminar shear strength was measured using an Instron and a three-point bending short beam method under the condition of L/D=4.

【表】 表―1から明きらかなように、本発明の方法に
よつて得られる炭素繊維は高強度でしかも樹脂と
の接着性にも優れたものであるが、炭素化を塩化
水素ガスを含まない雰囲気で行つた場合、および
アルカリ金属および/または塩酸等を電解質とし
て用いて陽極酸化した場合には、強度または樹脂
との接着性のいずれかまたは両方が劣つたものし
か得られない。 実施例 2 実施例1にポリマーを用いて、単糸繊度0.8デ
ニール、6000フイラメントの長繊維を得、実施例
1の条件で耐炎化糸を得た。この耐炎化糸を窒素
ガス中500℃で2分、さらに塩化水素ガス7容量
%を含む窒素ガス中1300℃で炭素化し、続いて5
%硝酸を電解質として120mAの電流を1分間流
して陽極酸化した。得られた炭素繊維の強度は
520Kg/mm2で、層間剪断強度は14.1Kg/mm2であつ
た。 比較例 1 実施例1の耐炎化糸を用い、炭素化ガス雰囲気
を塩化水素/酸素/窒素とした以外は実施例1―
実験番号2と同一条件で炭素化、電解処理し、ス
トランド強度及び層間剪断強度を測定した。結果
を表―2に示す。 さらに、これらの繊維の接着性の差をより明ら
かにするために、複合材の疲労試験を行つた。 実施例1と同一の樹脂を用いて、これらの繊維
より一方向プリプレグを作成し、67.5度及び−
67.5度の方向に交互に10枚づつ積層し、実施例1
と同じ条件で加熱硬化し、平板状積層材を成形し
た。これを所定の寸法に切り出して試験片を作
り、定荷重−四点曲げ疲労試験を実施した。荷重
を変えた8回の試験結果よりS―N(応力−疲労
回数)曲線を得、これより応力5.5Kg/mm2に於け
る疲労回数を求め、耐疲労性を評価した。結果を
表―2に示す。
[Table] As is clear from Table 1, the carbon fibers obtained by the method of the present invention have high strength and excellent adhesion to resin. If anodization is carried out in a non-containing atmosphere, or if anodic oxidation is carried out using an alkali metal and/or hydrochloric acid as an electrolyte, only a product with poor strength and/or adhesion to the resin will be obtained. Example 2 Using the same polymer as in Example 1, a long fiber of 6000 filaments with a single yarn fineness of 0.8 denier was obtained, and a flame-resistant yarn was obtained under the conditions of Example 1. This flame-resistant yarn was carbonized at 500℃ for 2 minutes in nitrogen gas, then carbonized at 1300℃ in nitrogen gas containing 7% by volume of hydrogen chloride gas, and then carbonized for 5 minutes.
% nitric acid as an electrolyte and a current of 120 mA was applied for 1 minute to carry out anodic oxidation. The strength of the obtained carbon fiber is
The interlaminar shear strength was 520Kg/mm 2 and 14.1Kg/mm 2 . Comparative Example 1 Example 1 except that the flame-resistant yarn of Example 1 was used and the carbonizing gas atmosphere was hydrogen chloride/oxygen/nitrogen.
Carbonization and electrolytic treatment were performed under the same conditions as in Experiment No. 2, and the strand strength and interlaminar shear strength were measured. The results are shown in Table-2. Furthermore, in order to clarify the differences in adhesion between these fibers, fatigue tests were conducted on the composite material. A unidirectional prepreg was made from these fibers using the same resin as in Example 1, and the angle of 67.5 degrees and -
Example 1: 10 sheets were laminated alternately in the direction of 67.5 degrees.
It was heated and cured under the same conditions as above to form a flat plate-like laminate. This was cut to a predetermined size to make a test piece, and a constant load four-point bending fatigue test was conducted. An SN (stress-fatigue frequency) curve was obtained from the results of eight tests with varying loads, and from this the fatigue frequency at a stress of 5.5 Kg/mm 2 was determined to evaluate fatigue resistance. The results are shown in Table-2.

【表】 表―2より明らかなように、本発明の繊維は秀
れた接着性および耐疲労性を示すのに対し、炭素
化ガス雰囲気として酸素を含むものは、それ自身
及び表面処理後の繊維とも接着性が劣り、耐疲労
性も低い。 比較例 2 表面処理時間を30分とした以外は、実施例1―
実験番号2と同様の方法で炭素繊維を得た。この
炭素繊維の強度及び層間剪断強度は、それぞれ
371Kg/mm2および10.4Kg/mm2であり、実施例1―
実験番号2に比し、極めて低い値であつた。 比較例 3 実施例1―実験番号11の炭素繊維について比較
例2に記載した方法で複合材の疲労試験を行つた
ところ、耐疲労性(疲労回数)は39000回であつ
た。
[Table] As is clear from Table 2, the fibers of the present invention exhibit excellent adhesion and fatigue resistance, whereas those containing oxygen as a carbonizing gas atmosphere both themselves and after surface treatment. It has poor adhesion to fibers and low fatigue resistance. Comparative Example 2 Example 1 except that the surface treatment time was 30 minutes.
Carbon fibers were obtained in the same manner as in Experiment No. 2. The strength and interlaminar shear strength of this carbon fiber are
371Kg/mm 2 and 10.4Kg/mm 2 , and Example 1-
Compared to Experiment No. 2, this value was extremely low. Comparative Example 3 A composite material fatigue test was conducted on the carbon fiber of Example 1-Experiment No. 11 by the method described in Comparative Example 2, and the fatigue resistance (number of fatigue cycles) was 39,000 times.

Claims (1)

【特許請求の範囲】[Claims] 1 アクリル系繊維を前駆体として高強度でかつ
樹脂との接着性に優れた炭素繊維を製造するに際
し、アクリル系繊維を耐炎化処理後、塩化水素を
少くとも1容量%以上含み実質的に酸素を含まな
い不活性ガス雰囲気中600〜1600℃で炭素化し、
続いて、アルカリ金属及び塩素を含まない電解質
中で10mA〜3Aの電流を0.1分〜10分間適用して
炭素繊維を陽極とし電解処理することを特徴とす
る高性能炭素繊維の製造法。
1. When producing carbon fibers with high strength and excellent adhesion to resin using acrylic fibers as a precursor, the acrylic fibers are flame-retardantly treated and then treated to contain at least 1% by volume of hydrogen chloride and substantially oxygen. Carbonized at 600-1600℃ in an inert gas atmosphere free of
Subsequently, a method for producing high-performance carbon fibers is characterized in that the carbon fibers are electrolytically treated by applying a current of 10 mA to 3 A for 0.1 minutes to 10 minutes in an electrolyte that does not contain alkali metals and chlorine, using the carbon fibers as anodes.
JP6778185A 1985-03-30 1985-03-30 Production of high performance carbon fiber Granted JPS61231265A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6778185A JPS61231265A (en) 1985-03-30 1985-03-30 Production of high performance carbon fiber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6778185A JPS61231265A (en) 1985-03-30 1985-03-30 Production of high performance carbon fiber

Publications (2)

Publication Number Publication Date
JPS61231265A JPS61231265A (en) 1986-10-15
JPH0114340B2 true JPH0114340B2 (en) 1989-03-10

Family

ID=13354840

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6778185A Granted JPS61231265A (en) 1985-03-30 1985-03-30 Production of high performance carbon fiber

Country Status (1)

Country Link
JP (1) JPS61231265A (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS542123B2 (en) * 1971-09-30 1979-02-02
JPS59168129A (en) * 1983-03-10 1984-09-21 Nippon Carbon Co Ltd Production of carbon fiber

Also Published As

Publication number Publication date
JPS61231265A (en) 1986-10-15

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