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JPH0116927B2 - - Google Patents
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JPH0116927B2 - - Google Patents

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Publication number
JPH0116927B2
JPH0116927B2 JP59108534A JP10853484A JPH0116927B2 JP H0116927 B2 JPH0116927 B2 JP H0116927B2 JP 59108534 A JP59108534 A JP 59108534A JP 10853484 A JP10853484 A JP 10853484A JP H0116927 B2 JPH0116927 B2 JP H0116927B2
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JP
Japan
Prior art keywords
fibers
elongation
gas
fiber
strength
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
JP59108534A
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Japanese (ja)
Other versions
JPS60252719A (en
Inventor
Akitaka Kikuchi
Keizo Hosoi
Tsutomu Hiseki
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 JP10853484A priority Critical patent/JPS60252719A/en
Publication of JPS60252719A publication Critical patent/JPS60252719A/en
Publication of JPH0116927B2 publication Critical patent/JPH0116927B2/ja
Granted legal-status Critical Current

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  • Chemical Treatment Of Fibers During Manufacturing Processes (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • 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、高伸度炭素繊維の製造方法に関し、
さらに詳細には、耐炎化繊維を原料として炭素繊
維を製造する工程において少なくとも一度、酸化
剤による酸化作用を受けた炭素繊維を特定の雰囲
気中において、1200℃〜1600℃の温度でさらに熱
処理することによつて、高伸度炭素繊維を製造す
る方法に関する。 一般に炭素繊維は、比強度、比弾性率等の機械
的特性に優れており、そのため、この炭素繊維を
強化材とした複合材料は、航空機の構造材をはじ
め宇宙開発機器、自動車部品およびスポーツ用品
にまで広く利用されつつある。この複合材料は、
主として炭素繊維で補強したプラスチツクより構
成されており、従つて、この炭素繊維とプラスチ
ツクとの接着性は複合材料の機械的特性に大きく
影響を与える事が知られている。 従来の技術 近年、高伸度炭素繊維と呼ばれる引張破断伸度
及び強度が高い炭素繊維の開発が進められ、従来
汎用されている炭素繊維と比較して強度に於て約
50Kg/mm2以上向上し、かつ破断伸度が2%近いも
のまで開発されてきている。ここに於て、炭素繊
維の高伸度化の効果を複合材料として充分に発揮
させるに当つて、炭素繊維とプラスチツクとの接
着性を改善させるための製造方法の研究が従来に
も増して、重要なものとなつてきている。 従来、炭素繊維とプラスチツクとの接着性を向
上させるための技法として、炭素繊維を酸化処理
する方法が知られている。そのような酸化処理方
法としては、日本公開特許公報昭52−25119号に
記載されている様に酸化剤を含む溶液中で炭素繊
維表面を酸化する方法(液相酸化法)、日本公開
特許公報昭58−104222号に記載されている様に、
電極ローラーを介して炭素繊維に直接通電し、電
解液中にて炭素繊維の表面を酸化する方法(電解
酸化法)、ならびに、日本公開特許公報昭52−
40662号および昭52−53092号に記載されている様
に、酸化性のガス雰囲気中にて耐炎化繊維または
炭素繊維を熱処理し、該繊維維の表面を酸化する
方法ならびに、耐炎化繊維を炭素化する際炭素化
と同時に表面を酸化する方法(気相酸化法)など
が知られている。 発明が解決しようとする問題点 上述の酸化処理を施した被酸化処理繊維は、繊
維自身の強度および伸度は、ともに未酸化処理繊
維よりは大きいが、被酸化処理繊維から生成され
る複合材料の特性は未酸化処理繊維から生成され
た同様な複合材料と比較して劣るという事が報告
されている(K.Morita etal International
Carbon Conference Baden、Baden1976)。この
ような酸化処理技術を改善すべく日本公開特許公
報昭50−145696号、昭54−59497号、および昭58
−214527号等の報告がなされている。 しかし、近年の多分野に亘る炭素繊維複合材料
の開発に伴い、その用途によつて様々な種類のプ
ラスチツクがマトリツクスとして用いられてお
り、その多様化はますます進展しつつある。そし
て、同一の被酸化処理繊維を用いたにもかかわら
ず、このプラスチツクの組成に依存して該複合材
料の引張破断伸度が著しく低下する場合がある。 問題点を解決するための手段 本発明者らは、プラスチツクをマトリツクスと
する炭素繊維複合材料の機械的破壊機構について
鋭意研究を重ねた結果、該炭素繊維複合材料の引
張破壊は、炭素繊維と、マトリツクスプラスチツ
ク間の界面状態と密接な関係があるとの知見を
得、この知見に基づいて高伸度炭素繊維の製造に
成功した。 本発明に係る高伸度炭素繊維の製造方法は、ア
クリロニトリル系合成繊維を、酸化性雰囲気中で
熱処理することによつて得られた耐炎化繊維を原
料として、炭素繊維を製造する工程において、炭
素化と同時に気相にて表面酸化処理するかまたは
炭素化の後に気相にて表面酸化処理を施し、しか
る後得られた炭素繊維を不活性ガスまたは/およ
びハロゲン化水素ガスから構成される雰囲気中に
おいて1200℃〜1600℃の温度で1〜80秒間さらに
熱処理することを特徴とする。 本発明において、高伸度炭素繊維とは、引張破
断伸度1.5%以上、かつ引張破断強度400Kg/mm2
上の炭素質繊維をさす。 本発明の方法において、プリカーサとしては、
アクリロニトリル系合成繊維が用いられ、中で
も、少くとも90重量%、のアクリロニトリル単位
を含有するアクリロニトリル系重合体から、周知
の方法によつて製造された繊維が好ましい。特
に、単糸繊度0.5〜1.5デニール、単糸本数1000〜
12000本の繊維束が好ましく、不純物や欠陥が少
なく、緻密な構造を有し、かつ高配向の繊維束が
さらに好ましい。 本発明の方法において、耐炎化繊維は、上述の
ようなプリカーサを空気で代表される酸化性雰囲
気中で熱風循環炉または/および加熱ローラーを
用いて200〜400℃、好ましくは、240〜350℃で所
定の時間熱処理することによつて得ることができ
る。 本発明方法に従つて、炭素繊維を製造する工程
において、繊維に表面酸化処理を施す方法として
は、前記耐炎化繊維を非酸化性雰囲気中1200〜
1450℃、好ましくは1300〜1400℃の温度で炭素化
処理し、しかる後、気相の状態に於て、酸化処理
を施す方法と、前記耐炎化繊維を酸化性のガス雰
囲気中1200〜1450℃、好ましくは1300〜1400℃の
温度で炭素化すると同時に繊維表面を気相酸化す
る方法などがある。 一方、本発明方法の表面酸化処理において使用
する酸化剤としては、酸素、オゾン、酸化窒素、
酸化イオウ、酸化炭素などがあるが、実用上酸素
が好ましい。これらの酸化剤を含む酸化性ガス雰
囲気の組成としては、酸化剤の種類によつて異な
るが、一般に、酸化剤濃度が500ppm〜40容量%
である不活性ガスとの混合ガスが用いられる。 一般に、炭素化後、気相で酸化処理する場合に
は、酸化性ガス雰囲気中約600〜1400℃において
約5〜120秒間加熱すればよい。また、炭素化と
同時に表面酸化処理する場合は、酸化性ガス雰囲
気中で前述のように1200〜1450℃で約5〜60秒間
加熱すればよい。 上記の酸化剤は、繊維表面に対して含酸素官能
基の導入または/および該繊維表面のエツチング
を行い得るものである。 本発明の方法のように、炭素化の後または炭素
化と同時に表面酸化処理を受けた被酸化処理繊維
は、不活性ガスまたは/およびハロゲン化水素ガ
スからなる雰囲気中で熱処理される。 ハロゲン化水素としてはフツ化水素、塩化水
素、臭化水素等を用いることができるが、実用
上、塩化水素の使用が好ましい。また、不活性ガ
スとしては、ヘリウム、アルゴン、窒素等を用い
ることができるが、コスト面から窒素が有利であ
る。 この場合、不活性ガスのみでも使用する事は可
能であるが、ハロゲン化水素が存在する方が被酸
化処理繊維の表面の改良には、より効果がある。
この事から、使用する雰囲気としては不活性ガス
およびハロゲン化水素の混合ガスの使用が好まし
い。この場合、ハロゲン化水素を0.1容量%以上
含有する不活性ガスとハロゲン化水素の混合ガス
の使用がさらに好ましい。混合ガス中のハロゲン
化水素の含有量の上限は、格別限定されないが、
コスト面からあまり高くない方がよい。 また、熱処理条件は、1200℃〜1600℃にて、1
〜80秒であり、1200〜1400℃で、秒が特に好まし
い。 1200℃未満の温度又は1秒未満の時間では、酸
化処理を施された被酸化処理繊維の表面が改善さ
れず、従つて該被酸化処理繊維をプラスチツクマ
トリツクスに配合して、複合材料とした際、ある
種のプラスチツクに対して、十分に該被酸化処理
繊維の高伸度物性が発揮されない場合が生じる。 また、1600℃を超える温度では、該被酸化処理
繊維の本体の構造に変化を生じ始め、該繊維の内
部に微細な空孔を生成し、結果として該繊維の物
性が低下し始めるので好ましくない。さらに、80
秒を超える時間では、該被酸化処理繊維を用いた
複合材料の引張破断伸度及び強度については、高
い値を示すものの、該繊維とプラスチツクマトリ
ツクスとの接着性の尺度の1つである層間せん断
強度(ILSS)が激減し、このため、高性能の複
合材料は得られない。 発明の効果 本発明の方法によつて得られる高伸度炭素繊維
を用いた複合材料は、引張破断伸度及び強度が、
そのマトリツクスを構成するプラスチツクの種類
に関係なく高い値を示し、しかも、層間せん断強
度(ILSS)についても実用に耐えうるに充分な
値を保持している。 また、X線光電子分光法(ESCA)による酸素
濃度O1S/C1Sも酸化処理糸に対して、1200℃以上
の加熱によつて若干減小しているものの、未酸化
処理繊維に比べれば、かなりの量の酸素が残存し
ており、この事から、該繊維表面には、高性能複
合材料を形成するに十分な表面官能基が、均一に
存在していると考えられる。また、クリプトンガ
スを用いたBET法比表面積測定の結果、被酸化
処理繊維に比べて、該繊維を1000℃以上の温度で
熱処理を施した方が、表面積が小さく、この事か
ら、酸化処理の際生じた表面の微細な空孔などが
少なくなつた事が考えられる。 実施例 以下、本発明を以下の実施例について具体的に
説明する。 実施例 1 アクリロニトリル系合成繊維(単糸デニール
1.3d、フイラメント数6000)を空気中240℃にお
いて40分間、さらに260℃において20分間加熱し
て耐炎化繊維を得、さらに非酸化性雰囲気中、最
高処理温度1300℃で炭素化し未酸化処理繊維を得
た。この未酸化処理繊維を用い、気相にて、塩化
水素ガスが1.0容量%、酸素ガスが0.5容量%、窒
素ガスが98.5容量%から成る雰囲気中、1000℃に
て40秒間酸化処理を行つた。得られた被酸化処理
繊維を、塩化水素ガスが1.0容量%、窒素ガスが
99.0容量%から成る雰囲気中、1200℃にて7秒
間、熱処理を行ない、高伸度炭素繊維を得た。得
られた高伸度炭素繊維から、JIS−R−7601−
1980−5・3・2に記載の方法に準じてストラン
ドを作製し、引張破断強伸度を測定した。ストラ
ンドは、2つの種類のものを作製した。即ち、エ
ポキシ樹脂(油化シエルエポキシ社製エピコート
828)100重量部、無水メチルナジツク酸90重量部
及びベンジルジメチルアミン2重量部をメチルエ
チルケトン(以下、「MEK」という。)に溶解し
た混合液に該繊維を含浸し、150℃1時間の条件
で硬化したもの(以下、「ストランドA」とい
う。)及び、前記エポキシ樹脂脂100重量部、3フ
ツ化ほう素モノエチルアミン3重量部をMEKに
溶解した混合液に同様に含浸し、130℃、1時間、
さらに180℃、2時間の条件で硬化したもの「以
下、「ストランドB」という。)である。 測定の結果、ストランドAでは引張破断伸度
(以下、「伸度」という。)1.78%、引張破断強度
(以下、「強度」という。)435Kg/mm2、ストランド
Bでは引張破断伸度1.72%、強度421Kg/mm2であ
つた。 また、前記高伸度炭素繊維を、エポキシ樹脂
(チバガイギー社製アラルダイド MY720)100
重量部、4,4′−ジアミノジフエニルスルホン20
重量部、3フツ化ほう素モノエチルアミン1.5重
量部をMEKに溶解した混合液に含浸し、プレプ
リグを作製し、これを積層し加熱硬化させること
によつて平板状の成形物を作成し、層間せん断強
度(ILSS)を測定したところ、12.7Kg/mm2であ
つた。 またESCAによるO1S/C1Sは0.15であり、クリ
プトンによるBET比表面積は、0.34m2/gであ
つた。 一方、耐炎化繊維を原料として、炭素繊維を製
造する際、一度も酸化処理を施さなかつた未酸化
処理繊維を使つて作製したストランド及び平板状
成型物についての結果を第1表に示す。 実施例 2 実施例1において、被酸化処理繊維を熱処理す
る雰囲気が、窒素100容量%で、該熱処理温度及
び時間をそれぞれ1350℃、15秒間とした以外は全
て同様な処理を行ない、同様にしてストランド及
び成型物を作製した。物性測定の結果、ストラン
ドAでは、伸度1.79%、強度440Kg/mm2であり、
ストランドBでは、伸度1.64、強度403Kg/mm2
ILSSは12.3Kg/mm2であつた。 実施例 3 実施例1において、被酸化処理繊維を熱処理す
る雰囲気が、塩化水素ガス3.0容量%、窒素ガス
97.0容量%からなる混合ガスとし、また熱処理温
度及び時間を1400℃、10秒間とした以外は全て同
様な処理を行ない、同様にしてストランド及び、
成型物を作製した。物性測定の結果、ストランド
Aでは伸度1.77%、強度433Kg/mm2、ストランド
Bでは、伸度1.76%、強度430Kg/mm2、ILSSは
12.1Kg/mm2であつた。 実施例 4 実施例1において、耐炎化繊維を原料として塩
化水素ガス5容量%、酸素ガス2.0容量%、窒素
ガス93.0容量%から成る雰囲気中、最高処理温度
1300℃で炭素化して、被酸化処理繊維を作製し、
得られた被酸化処理繊維を塩化水素ガスが1.0容
量%、窒素ガス99.0容量%から成る雰囲気中1400
℃、10秒間熱処理を行なつた以外は全て同様な処
理を行ない、同様にしてストランド及び成型物を
作製した。物性測定の結果、ストランドAでは、
伸度1.78%、強度436Kg/mm2、ストランドBでは、
伸度1.73%、強度425Kg/mm2、ILSSは、12.1Kg/
mm2であつた。 比較例 1 実施例1において、被酸化処理繊維に対して熱
処理を実施しなかつた以外は、全て同様な処理を
行つたところ、ストランドAでは伸度1.75%、強
度428Kg/mm2、ストランドBでは伸度1.20%、強
度295Kg/mm2、ILSSは12.7Kg/mm2であつた。 比較例 2 実施例1において、被酸化処理繊維を塩化水素
ガス1.0容量%、窒素ガス99.0容量%から成る雰
囲気中、500℃にて30秒間、熱処理を施した以外
は全て同様な処理を行つたところ、ストランドA
では、伸度1.78%、強度435Kg/mm2、ストランド
Bでは伸度1.23%、強度302Kg/mm2、ILSSは12.6
Kg/mm2であつた。 比較例 3 実施例4において、被酸化処理繊維に対して、
熱処理を実施しなかつた以外は全て同様な処理を
行つたところ、ストランドAでは伸度1.79%、強
度439Kg/mm2、ストランドBでは伸度1.22、強度
298Kg/mm2、ILSSは12.8Kg/mm2であつた。 比較例 4 実施例1と同様な手法により、炭素繊維を製造
し、さらに、この炭素繊維から同様に2種のスト
ランドAおよびBを製造した。但し、被酸化処理
繊維の熱処理を、塩化水素1.0容量%、酸素0.5容
量%および窒素98.5容量%から成る雰囲気中、
1350℃にて、15秒間行つた以外は全て同様な処理
法および条件を採用した。ストランドAは、伸度
1.79%および強度430Kg/mm2であり、ストランド
Bは伸度1.25%、強度305Kg/mm2、およびILSSは
12.6Kg/mm2であつた。
INDUSTRIAL APPLICATION FIELD The present invention relates to a method for producing high elongation carbon fiber,
More specifically, in the process of manufacturing carbon fibers using flame-resistant fibers as raw materials, carbon fibers that have been oxidized by an oxidizing agent are further heat-treated at a temperature of 1200°C to 1600°C in a specific atmosphere at least once. The present invention relates to a method for producing high elongation carbon fiber. In general, carbon fiber has excellent mechanical properties such as specific strength and specific modulus. Therefore, composite materials reinforced with carbon fiber are used in structural materials for aircraft, space development equipment, automobile parts, and sporting goods. It is becoming widely used. This composite material is
It is mainly composed of plastic reinforced with carbon fibers, and it is therefore known that the adhesiveness between the carbon fibers and the plastics has a large effect on the mechanical properties of the composite material. Conventional technology In recent years, the development of carbon fibers with high tensile elongation at break and strength, called high elongation carbon fibers, has been progressing.
Products with improved elongation of more than 50 kg/mm 2 and elongation at break of nearly 2% have been developed. In order to fully utilize the effect of increasing the elongation of carbon fiber as a composite material, research into manufacturing methods to improve the adhesion between carbon fiber and plastic has increased more than ever before. It is becoming important. Conventionally, a method of oxidizing carbon fibers has been known as a technique for improving the adhesiveness between carbon fibers and plastic. Such oxidation treatment methods include a method of oxidizing the carbon fiber surface in a solution containing an oxidizing agent (liquid phase oxidation method) as described in Japanese Patent Publication No. 52-25119; As stated in No. 58-104222,
A method of oxidizing the surface of carbon fibers in an electrolytic solution by applying electricity directly to carbon fibers through an electrode roller (electrolytic oxidation method), and Japanese Patent Application Publication No. 1982-
As described in No. 40662 and No. 52-53092, there is a method in which flame-resistant fibers or carbon fibers are heat-treated in an oxidizing gas atmosphere to oxidize the surface of the fibers, and flame-resistant fibers are treated with carbon fibers. A method of oxidizing the surface at the same time as carbonization (vapor phase oxidation method) is known. Problems to be Solved by the Invention Although the oxidized fibers subjected to the above oxidation treatment have higher strength and elongation than non-oxidized fibers, the composite material produced from the oxidized fibers have been reported to have inferior properties compared to similar composites made from unoxidized fibers (K.Morita etal International
Carbon Conference Baden, Baden1976). In order to improve such oxidation treatment technology, Japanese Patent Publications No. 145696/1982, No. 59497/1982, and No. 58
−214527, etc. have been reported. However, with the recent development of carbon fiber composite materials in many fields, various types of plastics are used as matrices depending on the application, and their diversification is progressing more and more. Even though the same oxidized fibers are used, the tensile elongation at break of the composite material may be significantly reduced depending on the composition of the plastic. Means for Solving the Problems The present inventors have conducted extensive research on the mechanical fracture mechanism of carbon fiber composite materials having plastic as a matrix, and have found that the tensile fracture of carbon fiber composite materials is We obtained the knowledge that there is a close relationship with the interfacial state between matrix plastics, and based on this knowledge, we succeeded in producing high elongation carbon fiber. The method for producing high elongation carbon fibers according to the present invention includes a step of producing carbon fibers using flame-resistant fibers obtained by heat-treating acrylonitrile-based synthetic fibers in an oxidizing atmosphere. At the same time as carbonization, surface oxidation treatment is performed in the gas phase, or after carbonization, surface oxidation treatment is performed in the gas phase, and then the obtained carbon fiber is placed in an atmosphere consisting of an inert gas and/or a hydrogen halide gas. It is characterized by further heat treatment at a temperature of 1200°C to 1600°C for 1 to 80 seconds. In the present invention, high elongation carbon fibers refer to carbonaceous fibers with a tensile elongation at break of 1.5% or more and a tensile strength at break of 400 Kg/mm 2 or more. In the method of the present invention, the precursor is
Synthetic acrylonitrile fibers are used, especially fibers produced by known methods from acrylonitrile polymers containing at least 90% by weight of acrylonitrile units. In particular, the single yarn fineness is 0.5 to 1.5 denier, and the number of single yarns is 1000 or more.
A fiber bundle of 12,000 fibers is preferred, and a fiber bundle with few impurities and defects, a dense structure, and a highly oriented fiber bundle is more preferred. In the method of the present invention, the flame-resistant fibers are prepared by heating the precursor as described above at 200 to 400°C, preferably 240 to 350°C, using a hot air circulation furnace or/and heating roller in an oxidizing atmosphere represented by air. It can be obtained by heat treatment for a predetermined period of time. In the process of producing carbon fibers according to the method of the present invention, the method of subjecting the fibers to surface oxidation treatment includes heating the flame-retardant fibers in a non-oxidizing atmosphere at
A method of carbonizing at a temperature of 1450°C, preferably 1300 to 1400°C, and then oxidizing in a gas phase; There is a method in which the fiber surface is simultaneously carbonized, preferably at a temperature of 1300 to 1400°C, and oxidized in a vapor phase. On the other hand, the oxidizing agents used in the surface oxidation treatment of the method of the present invention include oxygen, ozone, nitrogen oxide,
Examples include sulfur oxide and carbon oxide, but oxygen is preferred in practice. The composition of the oxidizing gas atmosphere containing these oxidizing agents varies depending on the type of oxidizing agent, but generally the oxidizing agent concentration is 500 ppm to 40% by volume.
A mixed gas with an inert gas is used. Generally, in the case of oxidation treatment in the gas phase after carbonization, heating may be performed at about 600 to 1400° C. for about 5 to 120 seconds in an oxidizing gas atmosphere. Moreover, when carrying out surface oxidation treatment at the same time as carbonization, heating may be performed at 1200 to 1450° C. for about 5 to 60 seconds in an oxidizing gas atmosphere as described above. The above-mentioned oxidizing agent is capable of introducing oxygen-containing functional groups onto the fiber surface and/or etching the fiber surface. As in the method of the present invention, the fiber to be oxidized which has undergone surface oxidation treatment after carbonization or simultaneously with carbonization is heat treated in an atmosphere consisting of an inert gas and/or hydrogen halide gas. As the hydrogen halide, hydrogen fluoride, hydrogen chloride, hydrogen bromide, etc. can be used, but it is practically preferable to use hydrogen chloride. Further, as the inert gas, helium, argon, nitrogen, etc. can be used, but nitrogen is advantageous in terms of cost. In this case, it is possible to use an inert gas alone, but the presence of hydrogen halide is more effective in improving the surface of the fiber to be oxidized.
For this reason, it is preferable to use a mixed gas of an inert gas and hydrogen halide as the atmosphere used. In this case, it is more preferable to use a mixed gas of hydrogen halide and an inert gas containing 0.1% by volume or more of hydrogen halide. The upper limit of the content of hydrogen halide in the mixed gas is not particularly limited, but
It is better not to be too expensive from a cost standpoint. In addition, the heat treatment conditions were 1200℃ to 1600℃.
~80 seconds, at 1200-1400°C, with seconds being particularly preferred. If the temperature is less than 1200°C or the time is less than 1 second, the surface of the oxidized fibers will not be improved, so the oxidized fibers will not be blended into a plastic matrix to form a composite material. In some cases, the high elongation properties of the oxidized fibers are not fully exhibited for certain types of plastics. Furthermore, at temperatures exceeding 1600°C, the structure of the main body of the fiber to be oxidized begins to change, fine pores are generated inside the fiber, and as a result, the physical properties of the fiber begin to deteriorate, which is undesirable. . In addition, 80
When the time exceeds seconds, the tensile elongation at break and the strength of the composite material using the oxidized fibers show high values, but the The shear strength (ILSS) is drastically reduced, and therefore a high-performance composite material cannot be obtained. Effects of the Invention The composite material using high elongation carbon fiber obtained by the method of the present invention has tensile elongation at break and strength of
It exhibits a high value regardless of the type of plastic that makes up the matrix, and also maintains a sufficient value for interlaminar shear strength (ILSS) to withstand practical use. In addition, the oxygen concentration O 1S /C 1S determined by X-ray photoelectron spectroscopy (ESCA) was slightly reduced for oxidized fibers by heating above 1200°C, but compared to non-oxidized fibers, A considerable amount of oxygen remains, which suggests that sufficient surface functional groups are uniformly present on the fiber surface to form a high-performance composite material. In addition, as a result of BET specific surface area measurement using krypton gas, the surface area of the fibers heat-treated at a temperature of 1000°C or higher was smaller than that of the fibers subjected to oxidation treatment. This is thought to be due to the fact that the number of fine pores that appeared on the surface decreased. EXAMPLES Hereinafter, the present invention will be specifically described with reference to the following examples. Example 1 Acrylonitrile synthetic fiber (single denier
1.3d, 6000 filaments) was heated in air at 240°C for 40 minutes and then at 260°C for 20 minutes to obtain flame-resistant fibers, and then carbonized in a non-oxidizing atmosphere at a maximum treatment temperature of 1300°C to obtain non-oxidized fibers. I got it. Using this unoxidized fiber, oxidation treatment was performed in the gas phase at 1000°C for 40 seconds in an atmosphere consisting of 1.0% by volume of hydrogen chloride gas, 0.5% by volume of oxygen gas, and 98.5% by volume of nitrogen gas. . The obtained oxidized fibers were treated with 1.0% by volume of hydrogen chloride gas and 1.0% by volume of nitrogen gas.
Heat treatment was performed at 1200° C. for 7 seconds in an atmosphere consisting of 99.0% by volume to obtain high elongation carbon fibers. From the obtained high elongation carbon fiber, JIS-R-7601-
Strands were prepared according to the method described in 1980-5.3.2, and the tensile strength and elongation at break were measured. Two types of strands were produced. That is, epoxy resin (Epicoat manufactured by Yuka Ciel Epoxy Co., Ltd.)
828) The fibers were impregnated in a mixture of 100 parts by weight, 90 parts by weight of methylnadic anhydride, and 2 parts by weight of benzyldimethylamine dissolved in methyl ethyl ketone (hereinafter referred to as "MEK"), and cured at 150°C for 1 hour. (hereinafter referred to as "Strand A"), 100 parts by weight of the epoxy resin, and 3 parts by weight of boron trifluoride monoethylamine were similarly impregnated in a mixed solution in MEK, and heated at 130°C for 1 hour. ,
The strand was further cured at 180°C for 2 hours (hereinafter referred to as ``Strand B''). ). As a result of the measurement, strand A had a tensile elongation at break (hereinafter referred to as "elongation") of 1.78% and tensile strength at break (hereinafter referred to as "strength") of 435 Kg/mm 2 , and strand B had a tensile elongation at break of 1.72%. The strength was 421Kg/ mm2 . In addition, the high elongation carbon fiber was coated with epoxy resin (Araldide MY720 manufactured by Ciba Geigy) 100%
Parts by weight, 4,4'-diaminodiphenylsulfone 20
A prepreg is prepared by impregnating a mixture of MEK with 1.5 parts by weight of boron trifluoride monoethylamine, which is then laminated and cured by heating to create a flat plate-like molded product. When the shear strength (ILSS) was measured, it was 12.7Kg/ mm2 . Further, O 1S /C 1S by ESCA was 0.15, and BET specific surface area by krypton was 0.34 m 2 /g. On the other hand, Table 1 shows the results for strands and plate-shaped molded products made using unoxidized fibers that were never oxidized when producing carbon fibers using flame-resistant fibers as raw materials. Example 2 The same treatment as in Example 1 was carried out except that the atmosphere in which the fibers to be oxidized were heat treated was 100% nitrogen by volume, and the heat treatment temperature and time were 1350°C and 15 seconds, respectively. A strand and a molded article were produced. As a result of physical property measurements, strand A has an elongation of 1.79% and a strength of 440 kg/ mm2 .
Strand B has an elongation of 1.64 and a strength of 403 Kg/mm 2 .
ILSS was 12.3Kg/ mm2 . Example 3 In Example 1, the atmosphere in which the fibers to be oxidized were heat treated was hydrogen chloride gas 3.0% by volume and nitrogen gas.
The same treatment was carried out except that a mixed gas consisting of 97.0% by volume was used, and the heat treatment temperature and time were 1400°C and 10 seconds, and strands and
A molded article was produced. As a result of physical property measurements, strand A has an elongation of 1.77% and a strength of 433 Kg/mm 2 , strand B has an elongation of 1.76% and a strength of 430 Kg/mm 2 , and ILSS is
It was 12.1Kg/ mm2 . Example 4 In Example 1, flame-resistant fibers were used as raw materials in an atmosphere consisting of 5% by volume of hydrogen chloride gas, 2.0% by volume of oxygen gas, and 93.0% by volume of nitrogen gas at the maximum treatment temperature.
Carbonize at 1300℃ to produce oxidized fibers,
The obtained oxidized fibers were heated at 1,400 °C in an atmosphere containing 1.0% by volume of hydrogen chloride gas and 99.0% by volume of nitrogen gas.
Strands and molded products were produced in the same manner, except that the heat treatment was performed at ℃ for 10 seconds. As a result of physical property measurements, in strand A,
Strand B has an elongation of 1.78% and a strength of 436Kg/ mm2 .
Elongation 1.73%, strength 425Kg/mm 2 , ILSS 12.1Kg/
It was warm in mm2 . Comparative Example 1 In Example 1, except that the oxidized fibers were not heat-treated, all the same treatments were performed. Strand A had an elongation of 1.75% and a strength of 428 Kg/mm 2 , and Strand B had an elongation of 1.75% and a strength of 428 Kg/mm 2 . The elongation was 1.20%, the strength was 295 Kg/mm 2 , and the ILSS was 12.7 Kg/mm 2 . Comparative Example 2 The same treatment as in Example 1 was carried out except that the fibers to be oxidized were heat-treated at 500°C for 30 seconds in an atmosphere consisting of 1.0% by volume of hydrogen chloride gas and 99.0% by volume of nitrogen gas. However, strand A
Strand B has an elongation of 1.78%, a strength of 435 Kg/mm 2 , and an elongation of strand B of 1.23%, a strength of 302 Kg/mm 2 , and an ILSS of 12.6.
It was Kg/ mm2 . Comparative Example 3 In Example 4, for the oxidized fiber,
When all the same treatments were performed except that no heat treatment was performed, Strand A had an elongation of 1.79% and a strength of 439 Kg/mm 2 , and Strand B had an elongation of 1.22 and a strength of 439 Kg/mm 2
298Kg/mm 2 and ILSS was 12.8Kg/mm 2 . Comparative Example 4 Carbon fibers were produced in the same manner as in Example 1, and two types of strands A and B were produced from these carbon fibers in the same manner. However, the heat treatment of the fibers to be oxidized is carried out in an atmosphere consisting of 1.0% by volume of hydrogen chloride, 0.5% by volume of oxygen, and 98.5% by volume of nitrogen.
Similar treatment methods and conditions were used except that the treatment was carried out at 1350°C for 15 seconds. Strand A has elongation
Strand B has an elongation of 1.25% and a strength of 305Kg/mm 2 , and the ILSS has a
It was 12.6Kg/ mm2 .

【表】【table】

【表】 実施例5および比較例5 実施例4と同一の方法で得た被酸化処理繊維
を、塩化水素ガス1.0容量%と窒素ガス99.0容量
%からなる雰囲気中で熱処理した。熱処理温度は
1000℃(比較例6)および1200℃(実施例6)と
し、熱処理時間は5、10および20秒間とした。得
られた繊維のストランドBの引張強度を測定した
結果を第1図に示す。
[Table] Example 5 and Comparative Example 5 The oxidized fibers obtained in the same manner as in Example 4 were heat treated in an atmosphere containing 1.0% by volume of hydrogen chloride gas and 99.0% by volume of nitrogen gas. The heat treatment temperature is
The temperature was 1000°C (Comparative Example 6) and 1200°C (Example 6), and the heat treatment times were 5, 10, and 20 seconds. The results of measuring the tensile strength of the obtained fiber strand B are shown in FIG.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は、実施例5および比較例5における熱
処理条件と、得られた繊維のストランドBの引張
強度との関係を示す。
FIG. 1 shows the relationship between the heat treatment conditions in Example 5 and Comparative Example 5 and the tensile strength of the obtained fiber strand B.

Claims (1)

【特許請求の範囲】[Claims] 1 アクリロニトリル系合成繊維を、酸化性雰囲
気中で熱処理することによつて得られた耐炎化繊
維を原料として、炭素繊維を製造する工程におい
て、炭素化と同時に気相にて表面酸化処理するか
または炭素化の後に気相にて表面酸化処理を施
し、しかる後得られた炭素繊維を不活性ガスまた
は/およびハロゲン化水素ガスから構成される雰
囲気中において1200℃〜1600℃の温度で1〜80秒
間さらに熱処理することを特徴とする高伸度炭素
繊維の製造方法。
1. In the process of manufacturing carbon fiber using flame-resistant fiber obtained by heat-treating acrylonitrile-based synthetic fiber in an oxidizing atmosphere as a raw material, surface oxidation treatment is carried out in the gas phase at the same time as carbonization, or After carbonization, surface oxidation treatment is performed in the gas phase, and then the obtained carbon fiber is heated at a temperature of 1200°C to 1600°C for 1 to 80°C in an atmosphere consisting of an inert gas and/or hydrogen halide gas. A method for producing high elongation carbon fiber, characterized by further heat treatment for seconds.
JP10853484A 1984-05-30 1984-05-30 Production of carbon fiber having high elongation Granted JPS60252719A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10853484A JPS60252719A (en) 1984-05-30 1984-05-30 Production of carbon fiber having high elongation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10853484A JPS60252719A (en) 1984-05-30 1984-05-30 Production of carbon fiber having high elongation

Publications (2)

Publication Number Publication Date
JPS60252719A JPS60252719A (en) 1985-12-13
JPH0116927B2 true JPH0116927B2 (en) 1989-03-28

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Country Link
JP (1) JPS60252719A (en)

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Publication number Priority date Publication date Assignee Title
JP2961274B2 (en) * 1988-12-27 1999-10-12 大阪瓦斯株式会社 High modulus pitch-based carbon fiber and method for producing the same
JP2004277192A (en) * 2003-03-13 2004-10-07 Toray Ind Inc Carbon fiber for carbon fiber reinforced carbon composite material and method for producing the same
JP4674066B2 (en) * 2004-08-05 2011-04-20 帝人化成株式会社 Electromagnetic wave shielding thermoplastic resin composition
CN105714412A (en) * 2016-04-23 2016-06-29 北京化工大学 Preparation method of electrospun polyacrylonitrile pre-oxidized fiber and carbon fiber

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JPS58214527A (en) * 1982-06-08 1983-12-13 Toray Ind Inc Carbon fiber bundle of high strength and elongation
JPS59168129A (en) * 1983-03-10 1984-09-21 Nippon Carbon Co Ltd Production of carbon fiber
JPS60110925A (en) * 1983-11-15 1985-06-17 Asahi Chem Ind Co Ltd Manufacture of high-performance carbon fiber

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