JPH05345670A - Carbon fiber-reinforced carbon composite material and sliding material produced therewith - Google Patents

Carbon fiber-reinforced carbon composite material and sliding material produced therewith

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Publication number
JPH05345670A
JPH05345670A JP4158284A JP15828492A JPH05345670A JP H05345670 A JPH05345670 A JP H05345670A JP 4158284 A JP4158284 A JP 4158284A JP 15828492 A JP15828492 A JP 15828492A JP H05345670 A JPH05345670 A JP H05345670A
Authority
JP
Japan
Prior art keywords
carbon fiber
composite material
carbon
impregnated
sheet
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.)
Granted
Application number
JP4158284A
Other languages
Japanese (ja)
Other versions
JP3383992B2 (en
Inventor
Kazuo Niwa
一夫 丹羽
Toshihiro Fukagawa
敏弘 深川
Hitoshi Seki
均 関
Takeo Matsui
丈雄 松井
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 Kasei Corp
Original Assignee
Mitsubishi Kasei 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 Kasei Corp filed Critical Mitsubishi Kasei Corp
Priority to JP15828492A priority Critical patent/JP3383992B2/en
Priority to EP93913533A priority patent/EP0598923B1/en
Priority to DE69324105T priority patent/DE69324105T2/en
Priority to US08/196,140 priority patent/US5525558A/en
Priority to PCT/JP1993/000812 priority patent/WO1993025493A1/en
Publication of JPH05345670A publication Critical patent/JPH05345670A/en
Application granted granted Critical
Publication of JP3383992B2 publication Critical patent/JP3383992B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE:To provide a carbon fiber-reinforced carbon composite material having excellent abrasion resistance. CONSTITUTION:A short carbon fiber bundle composed of plural single fibers and free from collecting agent is opened to obtain a sheet containing fibers randomly oriented in two dimensions. The sheet is impregnated with a resin and the impregnated sheets are laminated, formed, baked and finally densified with an impregnating pitch having a softening point of 70-120 deg.C, a toluene insoluble content of 10-30%, a quinoline insoluble content of <=1% and a fixed carbon content of >=40% to obtain the carbon fiber-reinforced carbon composite material.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、摩擦、摺動特性に優れ
た炭素繊維強化炭素複合材(以下、C/C複合材とい
う)及びそれを用いた摺動材に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a carbon fiber reinforced carbon composite material (hereinafter referred to as C / C composite material) having excellent friction and sliding characteristics, and a sliding material using the same.

【0002】[0002]

【従来の技術】炭素繊維炭素複合材は機械特性、耐熱特
性、摩擦制動特性に優れており、航空機、レース用四輪
車、二輪車などのブレーキ摺動部のディスクやパッドへ
の実用化が進んでいる。一般的にC/C複合材は、PA
N系、ピッチ系、あるいはレーヨン系などの長短炭素繊
維に熱硬化性樹脂を含浸させ、プリプレグをつくり、こ
れらを積層、硬化させて成形体にし、不活性雰囲気にお
いて600〜2500℃で焼成することにより製造され
ている。
2. Description of the Related Art Carbon fiber-carbon composite materials have excellent mechanical properties, heat resistance properties, and friction braking properties, and are being put to practical use as disks and pads for brake sliding parts of aircraft, racing four-wheeled vehicles, two-wheeled vehicles, etc. I'm out. Generally C / C composites are PA
N-type, pitch-type, or rayon-type long and short carbon fibers are impregnated with a thermosetting resin to form a prepreg, which are laminated and cured to form a molded body, which is fired at 600 to 2500 ° C. in an inert atmosphere. Are manufactured by.

【0003】この段階ではかさ密度が低く、強度的には
非常に不十分である。そのため、フェノール樹脂、フラ
ン樹脂などの熱硬化性樹脂もしくはピッチ類などの熱可
塑性樹脂等を含浸またはメタン、プロパン、ジクロロエ
チレン等の有機物ガスを原料としたCVD法により緻密
化処理を繰り返し行い高緻密化(低気孔率化)、高強度
化する。
At this stage, the bulk density is low and the strength is very insufficient. Therefore, it is highly densified by impregnating thermosetting resin such as phenol resin or furan resin or thermoplastic resin such as pitches or by repeating the densification process by the CVD method using organic gas such as methane, propane, dichloroethylene as a raw material. (Lower porosity) and higher strength.

【0004】[0004]

【発明が解決しようとする課題】しかし、フェノール樹
脂、フラン樹脂などの熱硬化性樹脂を用いた場合、含
浸、硬化、焼成させる工程を繰り返す間に気孔を閉気孔
化しやすく、気孔が内部に残り低気孔率化しにくい。
又、メタン、プロパン、ジクロロエチレン等の有機物ガ
スを原料としたCVD法を用いた場合、炭素繊維との接
着性が悪く、ブレーキ摺動部への適用時に摩耗による消
耗が激しくなる。
However, when a thermosetting resin such as a phenol resin or a furan resin is used, it is easy to close the pores while repeating the steps of impregnation, curing and firing, and the pores remain inside. It is difficult to reduce porosity.
Further, when the CVD method using an organic gas such as methane, propane, or dichloroethylene as a raw material is used, the adhesiveness with the carbon fiber is poor and the wear due to abrasion becomes large when applied to the brake sliding portion.

【0005】そして、ピッチ類などの熱可塑性樹脂等を
用いた場合、高炭化収率とするために軟化点の高いもの
を用いるのが一般的である。しかしながら、軟化点の高
いピッチは含浸性に劣り、また高温処理を要するため
に、C/C複合材を作るための設備が過大となり、取扱
いも煩雑になる。すなわち、どの方法にも一長一短があ
り満足なものではなかった。
When a thermoplastic resin such as pitch is used, it is common to use one having a high softening point in order to obtain a high carbonization yield. However, pitch having a high softening point is inferior in impregnation property and requires high temperature treatment, so that equipment for producing a C / C composite material becomes excessive and handling becomes complicated. In other words, each method has advantages and disadvantages and is not satisfactory.

【0006】[0006]

【問題を解決するための手段】そこで、本発明者等は、
かかる課題を解決するために、C/C複合材の緻密化方
法について鋭意検討したところ、ある特定の性質を持つ
ピッチを含浸ピッチとして用いて緻密化処理を施すこと
により、上記課題が解決できることを知得し、本発明を
完成するに至った。即ち、本発明の目的は、低い摩耗率
を示すC/C複合材を提案することであり、その目的は
軟化点70〜120℃好ましくは80〜90℃、トルエ
ン不溶分10〜30好ましくは13〜20%、キノリン
不溶分1%以下、固定炭素が40%以上好ましくは50
%以上である含浸ピッチを用いて緻密化処理を施すこと
により達成される。
[Means for Solving the Problem] Therefore, the present inventors
In order to solve such a problem, as a result of extensive studies on a densification method of a C / C composite material, it was found that the above problems can be solved by performing a densification treatment using a pitch having a specific property as an impregnated pitch. After knowing it, the present invention was completed. That is, an object of the present invention is to propose a C / C composite material exhibiting a low wear rate, the object of which is a softening point of 70 to 120 ° C, preferably 80 to 90 ° C, and a toluene insoluble content of 10 to 30 and preferably 13 ~ 20%, quinoline insoluble content 1% or less, fixed carbon 40% or more, preferably 50
It is achieved by performing a densification treatment using an impregnated pitch that is at least%.

【0007】以下、本発明につき詳細に説明する。本発
明で用いる炭素繊維としては、ピッチ系、PAN系ある
いはレーヨン系炭素繊維等の公知のいずれのものも使用
でき、さらに必要に応じてSiC、Al23、カーボン
ブラックなどの無機繊維、無機物などを添加してもよ
い。これらの炭素繊維の形態は通常2000本〜800
0本の単繊維の束からなるトウ、ストランド、ロービン
グ、ヤーン等で、これらをカッティングすることによっ
て得られる短繊維状のものを用いる。本発明について
は、通常0.3〜100mm、好ましくは5〜50mm
程度の短繊維を使用する。炭素繊維自体の径や弾性率
は、一般に複合材として用いられる範囲で特に限定はさ
れない。
The present invention will be described in detail below. As the carbon fiber used in the present invention, any known carbon fiber such as pitch-based, PAN-based or rayon-based carbon fiber can be used, and if necessary, SiC, Al 2 O 3 , an inorganic fiber such as carbon black, or an inorganic substance. Etc. may be added. The form of these carbon fibers is usually 2000 to 800
A tow, a strand, a roving, a yarn, or the like, which is a bundle of 0 single fibers, and a short fiber-like one obtained by cutting these is used. For the present invention, usually 0.3 to 100 mm, preferably 5 to 50 mm
Use only short fibers. The diameter and elastic modulus of the carbon fiber itself are not particularly limited within the range generally used as a composite material.

【0008】C/C複合材とする際に例えば特開昭62
−96364号、特開平1−176273号公報等に記
載の方法で解繊・分散してシートとする。具体的な解繊
及び二次元ランダムなシートの作製方法の一例として
は、例えば紡績において一般的な機械的に炭素繊維をモ
ノフィラメント化し、シートを作製するランダムウェバ
ーを使用して製造したり、またはエアーにより解繊し、
シートを製造する方法などがある。
In forming a C / C composite material, for example, JP-A-62-62
-96364, JP-A-1-176273, and other methods to defibrate and disperse a sheet. As an example of a concrete defibration and a method for producing a two-dimensional random sheet, for example, a carbon fiber is mechanically made into a monofilament commonly used in spinning, and a sheet is produced using a random webber, or air is used. Disentangled by
There is a method of manufacturing a sheet.

【0009】また湿式解繊し、二次元ランダムに配向し
たシートを製造する方法としては、例えばパルプ等の叩
解処理に通常使用されているビーターや解繊処理に用い
られるパルパーを使用し、溶媒中で短繊維状炭素繊維を
解繊後、例えば底部にスクリーンを有する型枠等に少量
ずつ供給したり、解繊後撹拌等の手段で均一に分散さ
せ、金網等で抄紙後、乾燥させて作製する方法がある。
短繊維状の炭素繊維を均一に分散させる溶媒としては、
好ましくは水、あるいはアセトン、炭素数1〜5のアル
コール、アントラセン油等を用いるがその他の有機溶剤
を用いてもよい。又該溶媒中にフェノール樹脂、フラン
樹脂あるいはピッチ等を分散もしくは溶解させておく
と、炭素繊維同志が接着された状態となり、次工程での
取り扱いをより容易とするので好ましい。更に、繊維素
グリコール酸ナトリウム、ポリビニルアルコール、ヒド
ロキシセルロース等の増粘剤を溶媒中に加えておくと、
その効果が更に増大するので好ましい。
As a method for wet-defibration to produce a two-dimensional randomly oriented sheet, for example, a beater usually used for beating of pulp or the like or a pulper used for defibration is used in a solvent. After defibrating the short fibrous carbon fibers with, for example, supply them little by little to a mold having a screen at the bottom, or evenly disperse them by means such as stirring after defibration, make paper with a wire mesh, etc., and then make by drying There is a way to do it.
As a solvent for uniformly dispersing short fiber carbon fibers,
Preferably, water, acetone, alcohol having 1 to 5 carbon atoms, anthracene oil, or the like is used, but other organic solvent may be used. Further, it is preferable to disperse or dissolve a phenol resin, a furan resin, pitch or the like in the solvent, because the carbon fibers are adhered to each other and the handling in the next step becomes easier. Furthermore, if a thickening agent such as sodium fibrin glycolate, polyvinyl alcohol, or hydroxycellulose is added to the solvent,
This is preferable because the effect is further increased.

【0010】シートの目付(1m2当りの重量)として
は、種々のものが取り得るが、取り扱い性、含浸性、均
一性を考えると10〜500g/m2が最適である。こ
の様にして得られた二次元ランダムに配向したシートに
フェノール樹脂、フラン樹脂、あるいは石油系、石炭系
ピッチ等のマトリックスを含浸させた後乾燥する。その
際、マトリックスはアルコール、アセトン、アントラセ
ン油等の溶媒に溶解して適正な粘度に調整したものを使
用する。
Although various weights (weight per 1 m 2 ) of the sheet can be taken, 10-500 g / m 2 is optimal in view of handleability, impregnation property and uniformity. The two-dimensional randomly oriented sheet thus obtained is impregnated with a phenol resin, furan resin, or a matrix such as petroleum-based or coal-based pitch and then dried. At this time, the matrix used is one that is dissolved in a solvent such as alcohol, acetone, or anthracene oil and adjusted to have an appropriate viscosity.

【0011】次いで、この乾燥したシートを積層して金
型に充填し、100〜500℃の温度で加圧成形してV
f(繊維体積含有率)が5〜65%、好ましくは10〜
55%の成形体を得る、その後、N2ガスなどの不活性
ガス雰囲気中で1〜200℃/hrの昇温速度で800
〜2500℃まで昇温し、焼成した後、軟化点70〜1
20℃好ましくは80〜90℃、トルエン不溶分10〜
30%好ましくは13〜20%、キノリン不溶分1%以
下、固定炭素が40%以上好ましくは50%以上である
含浸ピッチを用いて緻密化処理を施す、または、より一
層緻密化効果を発揮する特開平1−298013号公報
等に記載の方法で含浸炭化する緻密化処理を行うことに
よりC/C複合材を得る。以下具体的な緻密処理を説明
する。
Then, the dried sheets are laminated, filled in a mold, and pressure-molded at a temperature of 100 to 500 ° C. to obtain V.
f (fiber volume content) is 5 to 65%, preferably 10
A 55% compact is obtained, and then 800 at a temperature rising rate of 1 to 200 ° C./hr in an inert gas atmosphere such as N 2 gas.
Up to 2500 ° C and after firing, softening point 70-1
20 ° C., preferably 80 to 90 ° C., toluene insoluble content 10 to
30%, preferably 13 to 20%, quinoline insoluble matter 1% or less, fixed carbon is 40% or more, preferably 50% or more, is used for densification treatment, or further densification effect is exhibited. A C / C composite material is obtained by performing a densification treatment for impregnating and carbonizing by a method described in JP-A-1-298013 or the like. The specific dense processing will be described below.

【0012】所定温度に加熱された槽に上記C/C複合
材を載置し、槽内を真空とした後、樹脂又は溶融ピッチ
を供給し、焼成により生じた空隙にマトリックスを含浸
する。この後再度800〜2500℃の温度で焼成す
る。上記工程を繰り返すことにより目的のC/C複合材
の緻密化処理を行う。
The above C / C composite material is placed in a bath heated to a predetermined temperature, the interior of the bath is evacuated, and then resin or molten pitch is supplied, and the voids formed by firing are impregnated with a matrix. After that, it is fired again at a temperature of 800 to 2500 ° C. By repeating the above steps, the target C / C composite material is densified.

【0013】[0013]

【実施例】以下、本発明を実施例により具体的に説明す
るが、本発明はその要旨を越えない限り、下記実施例に
よって限定されるものではない。
EXAMPLES The present invention will be specifically described below with reference to examples, but the present invention is not limited to the following examples as long as the gist thereof is not exceeded.

【0014】製造例1 30mm長でフィラメント数4000本のピッチ系炭素
繊維束をランダムウェッバーにて解繊し、二次元ランダ
ムに配向した目付200g/m2のシートを得る。この
シートヘエタノールで希釈したフェノール樹脂を含浸さ
せた後乾燥し、200g/m2の炭素繊維に対し、13
0g/m2のフェノール樹脂を含浸したシートを作製し
た。このシートを金型内へ積層し、250℃にて加圧成
形し、Vf〜50%の成形体を得た。この成形体を加熱
炉で2000℃まで焼成した後、軟化点85℃、トルエ
ン不溶分15%、実質的にキノリン不溶分を含まず、固
定炭素が55%であるピッチを含浸した状態で500℃
で、5時間、6kg/cm2の加圧下で加熱処理した
後、加熱炉で1000℃で焼成した。さらに同様の含浸
−固化−焼成の操作を4回繰り返しその後に2000℃
の処理を行って本発明の気孔率6%のC/C複合材を得
た。このC/Cを使って回転数7000rpm面圧12
kg/cm2の条件下で摩耗率を調べたところ0.5×
10-4mm/stop・surfであった。
Production Example 1 A pitch-based carbon fiber bundle having a length of 30 mm and 4000 filaments is defibrated by a random webber to obtain a sheet having a basis weight of 200 g / m 2 which is two-dimensionally randomly oriented. This sheet was impregnated with a phenol resin diluted with ethanol and then dried to obtain 200 g / m 2 of carbon fiber,
A sheet impregnated with 0 g / m 2 of phenol resin was prepared. This sheet was laminated in a mold and pressure-molded at 250 ° C. to obtain a molded body having Vf of 50%. After the molded body was fired to 2000 ° C. in a heating furnace, the softening point was 85 ° C., the toluene insoluble content was 15%, the quinoline insoluble content was not substantially contained, and the pitch in which fixed carbon was 55% was impregnated at 500 ° C.
Then, after heat treatment under a pressure of 6 kg / cm 2 for 5 hours, it was fired at 1000 ° C. in a heating furnace. Further, the same operation of impregnation-solidification-firing is repeated 4 times, and thereafter 2000 °
Was performed to obtain a C / C composite material of the present invention having a porosity of 6%. Using this C / C, the rotation speed is 7,000 rpm and the surface pressure is 12
When the wear rate was examined under the condition of kg / cm 2 , it was 0.5 ×
It was 10 −4 mm / stop · surf.

【0015】[0015]

【発明の効果】本発明は以上のように軟化点70〜12
0℃、トルエン不溶分10〜30%、キノリン不溶分1
%以下、固定炭素が40%以上である含浸ピッチを用い
て緻密化処理をすることにより、摩耗量が少ないブレー
キ摺動部を得ることができる。
As described above, the present invention has a softening point of 70-12.
0 ° C, toluene insoluble matter 10 to 30%, quinoline insoluble matter 1
%, The densification treatment is performed using an impregnated pitch having a fixed carbon content of 40% or more, whereby a brake sliding portion with a small amount of wear can be obtained.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 松井 丈雄 香川県坂出市番の州1番地 三菱化成株式 会社坂出工場内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Takeo Matsui No. 1 state in Sakaide city, Kagawa Prefecture Mitsubishi Kasei Corporation Sakaide factory

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 複数の単繊維からなる短繊維状の炭素
繊維束を解繊し、繊維が二次元ランダムに配向したシー
トを作製、樹脂を含浸後、積層して成形し、焼成した後
に、軟化点70〜120℃、トルエン不溶液10〜30
%、キノリン不溶分1%以下、固定炭素が40%以上で
ある含浸ピッチにより緻密化処理して得られることを特
徴とする炭素繊維強化炭素複合材。
1. A short fiber-like carbon fiber bundle composed of a plurality of single fibers is defibrated to prepare a sheet in which the fibers are two-dimensionally randomly oriented, impregnated with a resin, laminated and molded, and fired, Softening point 70-120 ° C, toluene non-solution 10-30
%, A quinoline insoluble content of 1% or less, and a fixed carbon of 40% or more obtained by a densification treatment with a carbon fiber-reinforced carbon composite material.
【請求項2】 複数の単繊維からなる短繊維状の炭素
繊維束を解繊し、繊維が二次元ランダムに配向したシー
トを作製、樹脂を含浸後、積層して成形し、焼成した後
に、軟化点70〜120℃、トルエン不溶液10〜30
%、キノリン不溶分1%以下、固定炭素が40%以上で
ある含浸ピッチにより緻密化処理して得られる炭素繊維
強化炭素複合材から構成されてなる摺動材。
2. A short fibrous carbon fiber bundle composed of a plurality of single fibers is defibrated to prepare a sheet in which the fibers are two-dimensionally randomly oriented, impregnated with a resin, laminated and molded, and fired, Softening point 70-120 ° C, toluene non-solution 10-30
%, Quinoline insoluble content of 1% or less, and fixed carbon of 40% or more, a sliding material composed of a carbon fiber reinforced carbon composite material obtained by a densification treatment with an impregnated pitch.
JP15828492A 1992-06-16 1992-06-17 Carbon fiber reinforced carbon composite and sliding material using the same Expired - Lifetime JP3383992B2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP15828492A JP3383992B2 (en) 1992-06-17 1992-06-17 Carbon fiber reinforced carbon composite and sliding material using the same
EP93913533A EP0598923B1 (en) 1992-06-16 1993-06-16 Method of manufacturing carbon fiber-reinforced composite carbon material, carbon fiber-reinforced composite carbon material, and sliding material
DE69324105T DE69324105T2 (en) 1992-06-16 1993-06-16 METHOD FOR PRODUCING CARBON FIBER ARMED CARBON COMPOSITE MATERIAL, CARBON FIBER ARMORED CARBON COMPOUND MATERIAL AND SLIDING MATERIAL
US08/196,140 US5525558A (en) 1992-06-16 1993-06-16 Process for producing carbon fiber reinforced carbon composite material, carbon fiber reinforced carbon composite material and sliding material
PCT/JP1993/000812 WO1993025493A1 (en) 1992-06-16 1993-06-16 Method of manufacturing carbon fiber-reinforced composite carbon material, carbon fiber-reinforced composite carbon material, and sliding material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15828492A JP3383992B2 (en) 1992-06-17 1992-06-17 Carbon fiber reinforced carbon composite and sliding material using the same

Publications (2)

Publication Number Publication Date
JPH05345670A true JPH05345670A (en) 1993-12-27
JP3383992B2 JP3383992B2 (en) 2003-03-10

Family

ID=15668237

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007004482A1 (en) * 2005-07-05 2007-01-11 Mitsubishi Chemical Functional Products, Inc. CARBON-FIBER-REINFORCED SiC COMPOSITE MATERIAL AND SLIDE MEMBER
JP2020040862A (en) * 2018-09-12 2020-03-19 大陽日酸株式会社 Method for producing carbon dense fine particles and carbon dense fine particles

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007004482A1 (en) * 2005-07-05 2007-01-11 Mitsubishi Chemical Functional Products, Inc. CARBON-FIBER-REINFORCED SiC COMPOSITE MATERIAL AND SLIDE MEMBER
US7794826B2 (en) 2005-07-05 2010-09-14 Mitsubishi Plastics, Inc. Carbon-fiber-reinforced SiC composite material and slide member
JP2020040862A (en) * 2018-09-12 2020-03-19 大陽日酸株式会社 Method for producing carbon dense fine particles and carbon dense fine particles

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