JPS5935841B2 - Tansozairiyounoseizohou - Google Patents

Tansozairiyounoseizohou

Info

Publication number
JPS5935841B2
JPS5935841B2 JP50128570A JP12857075A JPS5935841B2 JP S5935841 B2 JPS5935841 B2 JP S5935841B2 JP 50128570 A JP50128570 A JP 50128570A JP 12857075 A JP12857075 A JP 12857075A JP S5935841 B2 JPS5935841 B2 JP S5935841B2
Authority
JP
Japan
Prior art keywords
carbon
fibers
binder
fiber
coated
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
JP50128570A
Other languages
Japanese (ja)
Other versions
JPS5252912A (en
Inventor
登久治 早瀬
淳一 田中
洋一郎 富永
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.)
Nippon Carbon Co Ltd
Original Assignee
Nippon Carbon 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 Nippon Carbon Co Ltd filed Critical Nippon Carbon Co Ltd
Priority to JP50128570A priority Critical patent/JPS5935841B2/en
Publication of JPS5252912A publication Critical patent/JPS5252912A/en
Publication of JPS5935841B2 publication Critical patent/JPS5935841B2/en
Expired legal-status Critical Current

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Description

【発明の詳細な説明】 本発明は炭素材料、と(に高強度の炭素繊維強化炭素材
料の製造法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a carbon material and a method for producing a high strength carbon fiber reinforced carbon material.

従来、炭素繊維強化炭素材料の製造法として、数枚の黒
鉛化されたセルロース性織布にフルフラール・ケトン縮
合生成物、フェノールホルムアルデヒド樹脂等を噴務又
は塗布して被覆し、こうして被覆したシートを積み重ね
て積層物を形成させ、この積層物を圧力下で加熱して結
合剤を硬化させ、ついで非酸化性雰囲気中で加熱・して
炭素化する方法が知られているが、この方法によって製
造する場合、結合剤の厚さの変動に起因する結合剤の不
均一な膨張及び収縮があり、変形や内部に割れが生じ易
い。
Conventionally, as a manufacturing method for carbon fiber-reinforced carbon materials, several sheets of graphitized cellulosic woven fabric are coated with furfural-ketone condensation products, phenol formaldehyde resin, etc. by spraying or coating, and the thus coated sheets are coated. A known method is to stack the laminate to form a laminate, heat the laminate under pressure to harden the binder, and then heat it in a non-oxidizing atmosphere to carbonize it. In this case, there is non-uniform expansion and contraction of the binder due to variations in the thickness of the binder, which tends to cause deformation and internal cracks.

この他の方法として、炭素又はグラファイト繊維をある
型に成形し、フェノール性縮合生成物、尿素縮合生成物
、エポキシ樹脂、デクストロズ、コールタールピッチの
如き結合剤を加圧浸透させた後、成形品を圧縮して過剰
な結合剤を除去し、ついで加圧硬化させ、硬化後保護雰
囲気中で焼成され、焼成品は最終製品に期待される密度
によって再び含浸及び焼成の工程を何回か繰返す方法が
知られている。
Another method is to mold carbon or graphite fibers into a mold, infiltrate the molded product under pressure with a binder such as a phenolic condensation product, a urea condensation product, an epoxy resin, Dextroz, or coal tar pitch. The product is compressed to remove excess binder, then pressure-cured, and after curing is fired in a protective atmosphere, and the fired product undergoes the impregnation and firing process several times again depending on the density desired for the final product. It has been known.

この方法によれば、製品の密度が少なくとも1.4f/
Ceのものを得るには含浸及び焼成サイクルを6回以上
も必要であり、製造に長時間装した。
According to this method, the density of the product is at least 1.4 f/
Obtaining the Ce version required more than six impregnation and firing cycles, which required a long manufacturing time.

又、結合剤は炭素又はグラファイト繊維の成形品に含浸
する方法がとられているが、結合剤と繊維との濡れ性が
悪(、特に大型成形品の場合内部までの浸透が不完全と
なり欠陥となって残り易い等の問題があった。
In addition, a method of impregnating a molded product made of carbon or graphite fibers with a binder is used, but the wettability of the binder and the fibers is poor (particularly in the case of large molded products, penetration into the interior is incomplete, resulting in defects). There was a problem that it was easy to leave a residue.

本発明の目的は、従来における前記のような問題点を解
決して繊維と結合剤との結合が良好で、欠陥がな(、か
つ製造時間の短縮ができる炭素材料の製造法を実現する
にある。
The purpose of the present invention is to solve the above-mentioned conventional problems and to realize a method for manufacturing carbon materials that has good bonding between fibers and binders, is free from defects (and can shorten manufacturing time). be.

前記目的を達成するための、本発明の要旨とするところ
は、炭素繊維に有機質結合剤を被覆し、得られた繊維で
所望の形状に成形したのち、その成形体を加圧しながら
加熱して炭素化し、更に必要に応じて黒鉛化することを
特徴とする炭素材料の製造法に存する。
In order to achieve the above object, the gist of the present invention is to coat carbon fibers with an organic binder, mold the obtained fibers into a desired shape, and then heat the molded product while applying pressure. The present invention resides in a method for producing a carbon material, characterized by carbonizing it and further graphitizing it as necessary.

前記において述べる炭素繊維とは再生セルロース、ポリ
アクリロニトリル、ビニロン、リグニンポバール、ピッ
チ系(例えば、ポリ塩化ビニルピッチ、石油アスファル
ト、原油分解ピッチ、石油スラッジ、テトラベンゾフェ
ナジンピッチ、コールタールピッチなど)、耐熱性有機
高分子系(例えば、ポリアミド、ポリイミド、ホリヘン
ズイミダゾール、ポリベンゾオサジノン、ポリキナゾリ
ンジオン、ポリオキシジアゾール、ポリベンゾオキサジ
オン、ポリオキシジアゾール、ポリベンゾチアゾールな
ど)、フェノール樹脂、塩化ビニリデンとポリ塩化ビニ
ルの共重合物、フラン系樹脂等の有機高分子物質を紡糸
したものを製造用原料繊維として用いて、これを必要に
応じて不融化処理を行なった後、炭素化温度(即ち80
0〜3000°C)以上まで加熱処理して得られるもの
で、通常加熱処理温度が8oO〜1500℃のものを炭
素質繊維、2000℃以上のものを黒鉛質繊維を称して
いるものを全て含む。
The carbon fibers mentioned above are regenerated cellulose, polyacrylonitrile, vinylon, lignin poval, pitch-based (e.g., polyvinyl chloride pitch, petroleum asphalt, crude oil cracked pitch, petroleum sludge, tetrabenzophenazine pitch, coal tar pitch, etc.), heat-resistant organic polymers (e.g., polyamide, polyimide, polyhenzimidazole, polybenzoosazinone, polyquinazolinedione, polyoxydiazole, polybenzoxadione, polyoxydiazole, polybenzothiazole, etc.), phenolic resin, chloride Copolymers of vinylidene and polyvinyl chloride, furan-based resins, and other organic polymers are used as raw material fibers for production, and if necessary, they are treated to make them infusible, and then the carbonization temperature ( That is 80
0 to 3,000°C) or higher, including all those obtained by heat treatment at a temperature of 8oO to 1,500°C, which are referred to as carbonaceous fibers, and those whose heat treatment temperature is 2,000°C or higher are called graphite fibers. .

又、炭素繊維は布、テープ、糸、フェルト、編組品、チ
ョップ、紙等の任意の形状で用いられる。
Further, carbon fibers can be used in any form such as cloth, tape, thread, felt, braided product, chopped, paper, etc.

本発明に述べる有機質結合剤には、炭素繊維製造用原料
繊維の紡糸に用いられる上記に記載の有機高分子物質を
適宜選択して単独又は混合して使用される。
As the organic binder described in the present invention, the above-mentioned organic polymer substances used for spinning raw material fibers for producing carbon fibers are appropriately selected and used alone or in combination.

有機高分子物質のうち、とくにピッチ系、ポリアクリロ
ニトリル系のものは被覆に先立ち、200〜500℃に
乾留して低分子成分を留出し炭素含有率を増加させるこ
とが望ましい。
Among organic polymeric substances, it is preferable that pitch-based and polyacrylonitrile-based substances in particular be carbonized at 200 to 500° C. to distill off low-molecular components and increase the carbon content prior to coating.

有機質結合剤は炭素繊維との濡れを良好とするために必
要があれば有機溶剤を加え、適宜粘度に調整し、浸漬又
は含浸等の方法で炭素繊維に被覆する。
If necessary, an organic solvent is added to the organic binder to improve wetting with the carbon fibers, the viscosity is adjusted appropriately, and the carbon fibers are coated by dipping or impregnation.

浸漬又は含浸された繊維は、ついで洗浄又は乾燥して有
機溶剤を除去或いは揮発させることにより均一に有機質
結合剤を被覆した炭素繊維が得られる。
The soaked or impregnated fibers are then washed or dried to remove or volatilize the organic solvent, thereby obtaining carbon fibers uniformly coated with the organic binder.

被覆した炭素繊維は積層法、フィラメントワインド法等
により成形する。
The coated carbon fiber is molded by a lamination method, a filament winding method, or the like.

成形は必要があれば加熱し、加圧又は解圧しながら充分
にガス抜きをしながら行なうとよりち密なものとなる。
The molding can be made more compact if it is heated if necessary, and the gas is thoroughly degassed while pressurizing or depressurizing.

ピッチ系又はポリアクリロニトリル系の有機結合剤を用
いた成形体は、そのま\或いは過マンガン酸カリウム、
重クロム酸カリウム等の酸化剤を含む溶液に浸した後、
これを空気、酸素、オゾン、酸化窒素、硝酸ガス、酸化
イオウ、ハロゲン等の酸化性雰囲気中で200〜300
℃に加熱し不融化処理を行なうことが好ましい。
Molded products using pitch-based or polyacrylonitrile-based organic binders can be used as is or with potassium permanganate,
After soaking in a solution containing an oxidizing agent such as potassium dichromate,
This is heated in an oxidizing atmosphere such as air, oxygen, ozone, nitrogen oxide, nitric acid gas, sulfur oxide, halogen, etc.
It is preferable to perform the infusibility treatment by heating to ℃.

未処理又は不融化処理後の成形体は成形鋳型内で直接プ
レスするか、或いは粉末を圧力媒体として加圧、或いは
窒素、アルゴン等の不活性ガス圧等により加圧しながら
外部加熱、直接通電加熱、誘導加熱等により300〜5
00°Cまで加熱し、ついで800〜1500℃まで焼
成し、炭化して炭素繊維−炭素結合剤からなる炭素材料
を、更に必要に応じて2400〜3000℃まで加熱し
て黒鉛質繊維−黒鉛結合剤からなる炭素材料を得る。
The untreated or infusible molded product is directly pressed in a mold, or it is heated externally or directly heated while being pressurized by using powder as a pressure medium, or by inert gas pressure such as nitrogen or argon. , 300-5 by induction heating etc.
00°C, then fired to 800-1500°C, carbonized to form a carbon fiber-carbon binder carbon material, and further heated to 2400-3000°C as necessary to form a graphite fiber-graphite bond. A carbon material consisting of a carbonaceous agent is obtained.

炭素繊維の製造用原料繊維と同種の有機質高分子物質を
有機結合剤として使用した場合(例えばピッチ系炭素繊
維−ピッチ系結合剤、ポリアクリロニトリル系炭素繊維
−ポリアクリロニトリル系結合剤)有機質結合剤が炭化
して得られる炭素結合剤と炭素繊維とがほとんど同一性
質を示すため特に有効である。
When an organic polymer substance of the same type as the raw material fiber for manufacturing carbon fiber is used as an organic binder (for example, pitch-based carbon fiber-pitch-based binder, polyacrylonitrile-based carbon fiber-polyacrylonitrile-based binder), the organic binder This is particularly effective because the carbon binder obtained by carbonization and the carbon fibers exhibit almost the same properties.

と(に両者の熱膨張率の差が非常に小さく、又加熱処理
時及び処理後の冷却時に発生する熱応力も小さい為、こ
の間の剥離、クラック、変形等の発生は大巾に減少させ
ることが可能となった。
The difference in the coefficient of thermal expansion between the two is very small, and the thermal stress generated during heat treatment and cooling after treatment is also small, so the occurrence of peeling, cracks, deformation, etc. during this time can be greatly reduced. became possible.

上記により得られた焼成体はより高密度化、高強度化及
び不浸透化をはかるため再含浸、再焼成を行なうことは
勿論できるが、従来法のものにくらべ一次焼成体の強度
が高いため、従来の如く6回も必要とせず1〜2回程度
で充分であった。
The fired body obtained by the above method can of course be re-impregnated and re-fired in order to achieve higher density, higher strength, and impermeability, but since the strength of the primary fired body is higher than that of the conventional method, , it was sufficient to do it about 1 to 2 times, instead of 6 times as in the conventional case.

以下実施例により本発明の詳細な説明する。The present invention will be explained in detail below with reference to Examples.

実施例 1 強化繊維材として直径5μm、引張強度320kg/m
4、弾性率21 t /maのポリアクリロニトリル系
炭素繊維を用い、ポリアクリロニトリル有機質結合剤と
して被覆繊維を作った。
Example 1 Reinforced fiber material with a diameter of 5 μm and a tensile strength of 320 kg/m
4. A coated fiber was made using polyacrylonitrile carbon fiber with an elastic modulus of 21 t/ma as a polyacrylonitrile organic binder.

ポリアクリロニトリルの溶剤としてDMSO(ジメチル
スルホオキサイド)を使用し、その量は、ポリアクリロ
ニトリル5部に対してジメチルスルホオキサイド95部
とした。
DMSO (dimethyl sulfoxide) was used as a solvent for polyacrylonitrile, and the amount thereof was 95 parts of dimethyl sulfoxide per 5 parts of polyacrylonitrile.

被覆繊維をマンドレルに巻きつけた後、溶剤を除去する
ため水洗後、ロールを掛け、ついで熱風乾燥炉内150
℃で1時間加熱した。
After the coated fibers are wound around a mandrel, they are washed with water to remove the solvent, rolled, and then placed in a hot air drying oven at 150°C.
Heated at ℃ for 1 hour.

乾燥後、被覆繊維を裁断し、一方向に積層して、金型を
用いて50WX200LX5 を龍の形状に成形した。
After drying, the coated fibers were cut, laminated in one direction, and molded into a dragon shape of 50Wx200Lx5 using a mold.

成形は220℃で10分間予備加熱し、20ky/ca
rの圧力で加圧して行なった。
The molding is preheated at 220℃ for 10 minutes and the molding is performed at 20ky/ca.
The test was carried out under pressure of r.

成形体の繊維含有率は60容量%であった。The fiber content of the molded body was 60% by volume.

この成形体を空気中で250℃で6時間加熱し不融化処
理を行なった。
This molded body was heated in air at 250° C. for 6 hours to perform infusibility treatment.

不融化処理後、鋳型焼結炉で50kg/cntの圧力を
かげながら、100℃/Hrの昇温速度で250〜90
0℃まで加熱し炭素質繊維−炭素結合剤からなる炭素材
料を得た。
After the infusibility treatment, while applying a pressure of 50 kg/cnt in a mold sintering furnace, the heating rate was 250 to 90°C at a temperature increase rate of 100°C/Hr.
It was heated to 0°C to obtain a carbon material consisting of carbon fiber-carbon binder.

得られた炭素材料の特性を次に示す。The properties of the obtained carbon material are shown below.

比重 ・・・・・・ 1.40 曲げ強さ ・・・・・・37kg/ra弾性率
・・・・・・12 t/ma層間剪断強度・・・・
・・ 3、Okg/rna実施例 2 実施例1で得られた炭素材料に軟化点80℃のコールタ
ールピッチを150°C11〜1o7rL11LHgの
減圧下浸漬し、ついで10kg/cn’tの圧力下で1
時間含浸した。
Specific gravity: 1.40 Bending strength: 37kg/ra Modulus of elasticity
...12 t/ma interlaminar shear strength...
... 3.Okg/rna Example 2 The carbon material obtained in Example 1 was immersed in coal tar pitch with a softening point of 80°C under a reduced pressure of 150°C11~1o7rL11LHg, and then under a pressure of 10kg/cn't. 1
Impregnated for hours.

金製品は塩素ガス中で200 ’Cに2時間保持し、つ
いで窒素雰囲気中で900℃まで焼成した。
The gold products were held at 200'C in chlorine gas for 2 hours and then fired to 900'C in a nitrogen atmosphere.

この含浸再焼成のサイクルを2回行なって炭素材料を得
た。
This impregnation and re-firing cycle was repeated twice to obtain a carbon material.

その特性値は次に示すと#″’C−,b9“・
) 比重 ・・・・・・1.45 曲げ強さ ・・・・・・42 kg/mi弾性率
−12,5t /m4 層間剪断強度・・・・・・ 3.5kg/ma実施例
3 実施例2で得られた炭素材料を、2400℃に加熱黒鉛
化して黒鉛質繊維−黒鉛結合剤の炭素材料を得た。
Its characteristic values are shown below: #'''C-, b9''・
) Specific gravity: 1.45 Bending strength: 42 kg/mi Elastic modulus -12,5t/m4 Interlaminar shear strength: 3.5 kg/ma Example
3 The carbon material obtained in Example 2 was graphitized by heating at 2400°C to obtain a carbon material of a graphite fiber-graphite binder.

その特性を下に示す。比重 ・・・・・・ 1.
47
Its characteristics are shown below. Specific gravity 1.
47

Claims (1)

【特許請求の範囲】[Claims] 1 炭素繊維に該炭素繊維の製造用原料繊維と同種の有
機質高分子物質を結合剤として被覆し、得られた繊維で
所望の形状に成形したのち、その成形体を加圧しながら
加熱して炭素化し、更に必要に応じて黒鉛化することを
特徴とする炭素材料の製造法。
1 Carbon fibers are coated with an organic polymer substance of the same type as the raw material fiber for manufacturing the carbon fibers as a binder, the obtained fibers are molded into a desired shape, and the molded body is heated under pressure to form carbon fibers. 1. A method for producing a carbon material, which is characterized by graphitizing the carbon material and, if necessary, graphitizing the material.
JP50128570A 1975-10-25 1975-10-25 Tansozairiyounoseizohou Expired JPS5935841B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP50128570A JPS5935841B2 (en) 1975-10-25 1975-10-25 Tansozairiyounoseizohou

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP50128570A JPS5935841B2 (en) 1975-10-25 1975-10-25 Tansozairiyounoseizohou

Publications (2)

Publication Number Publication Date
JPS5252912A JPS5252912A (en) 1977-04-28
JPS5935841B2 true JPS5935841B2 (en) 1984-08-31

Family

ID=14988010

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50128570A Expired JPS5935841B2 (en) 1975-10-25 1975-10-25 Tansozairiyounoseizohou

Country Status (1)

Country Link
JP (1) JPS5935841B2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6054270B2 (en) * 1978-08-23 1985-11-29 東邦レーヨン株式会社 Carbon fiber reinforced carbon friction material
JPS5734085A (en) * 1980-08-06 1982-02-24 Toho Beslon Co Manufacture of carbon fiber reinforced carbon composite material
JPS57110751A (en) * 1980-12-27 1982-07-09 Toho Rayon Co Ltd Rocket nozzle
JPS60127265A (en) * 1983-12-15 1985-07-06 旭有機材工業株式会社 Pitch modified phenol resin coated carbon fiber for sintering body
JPS60127264A (en) * 1983-12-15 1985-07-06 旭有機材工業株式会社 Phenol resin coated carbonaceous fiber
US5246639A (en) * 1987-02-20 1993-09-21 Petoca Ltd. Method for producing carbon-carbon composite materials
JPS63215564A (en) * 1987-03-04 1988-09-08 日石三菱株式会社 Manufacture of carbon/carbon composite material
JPS63248770A (en) * 1987-04-03 1988-10-17 日石三菱株式会社 Manufacture of carbon/carbon composite material
JPH0533263A (en) * 1990-11-30 1993-02-09 Petoca:Kk Reinforcing fiber for carbon-carbon composite material and method for manufacturing composite material
CN121554302B (en) * 2026-01-23 2026-05-05 诸暨市幄肯中智新材料有限公司 Carbon-carbon composite cylinders, their preparation methods and applications

Also Published As

Publication number Publication date
JPS5252912A (en) 1977-04-28

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