JPH01234367A - Production of carbon/carbon composite material - Google Patents
Production of carbon/carbon composite materialInfo
- Publication number
- JPH01234367A JPH01234367A JP63058367A JP5836788A JPH01234367A JP H01234367 A JPH01234367 A JP H01234367A JP 63058367 A JP63058367 A JP 63058367A JP 5836788 A JP5836788 A JP 5836788A JP H01234367 A JPH01234367 A JP H01234367A
- Authority
- JP
- Japan
- Prior art keywords
- pitch
- fiber
- carbon
- fibers
- parts
- 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
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 20
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 20
- 239000002131 composite material Substances 0.000 title claims abstract description 10
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 239000000835 fiber Substances 0.000 claims abstract description 56
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 15
- 239000004917 carbon fiber Substances 0.000 claims abstract description 15
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000012298 atmosphere Substances 0.000 claims abstract description 9
- 238000010000 carbonizing Methods 0.000 claims abstract description 9
- 238000009987 spinning Methods 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 abstract description 7
- 239000000203 mixture Substances 0.000 abstract description 4
- 239000011295 pitch Substances 0.000 description 31
- 238000003763 carbonization Methods 0.000 description 10
- 239000000463 material Substances 0.000 description 8
- 239000011301 petroleum pitch Substances 0.000 description 7
- 239000011261 inert gas Substances 0.000 description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000007731 hot pressing Methods 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 239000003575 carbonaceous material Substances 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 239000012299 nitrogen atmosphere Substances 0.000 description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 3
- 238000010298 pulverizing process Methods 0.000 description 3
- 239000011337 anisotropic pitch Substances 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000005087 graphitization Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000002074 melt spinning Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 241000219112 Cucumis Species 0.000 description 1
- 235000015510 Cucumis melo subsp melo Nutrition 0.000 description 1
- FJJCIZWZNKZHII-UHFFFAOYSA-N [4,6-bis(cyanoamino)-1,3,5-triazin-2-yl]cyanamide Chemical compound N#CNC1=NC(NC#N)=NC(NC#N)=N1 FJJCIZWZNKZHII-UHFFFAOYSA-N 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000011300 coal pitch Substances 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000009656 pre-carbonization Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- XTQHKBHJIVJGKJ-UHFFFAOYSA-N sulfur monoxide Chemical class S=O XTQHKBHJIVJGKJ-UHFFFAOYSA-N 0.000 description 1
- 229910052815 sulfur oxide Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Composite Materials (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
Abstract
Description
【発明の詳細な説明】 産業上の利用分野 本発明は、炭素/炭素複合材料の製造法に関する。[Detailed description of the invention] Industrial applications The present invention relates to a method for manufacturing carbon/carbon composite materials.
従来の および発明が解決しようとする問題点炭素/
炭素複合材料は、1000℃以上の高温においても高強
度、高弾性率を維持し、かつ熱膨張率が小さい等の特異
な性質を有する材料であり、航空宇宙機器の部品、ブレ
ーキ、炉材等への利用が期待されている。しかしながら
、マトリックスと炭素繊維とを複合化する製造プロセス
は複雑であり、かつ長い日数を要するためコストがかか
っている。本発明は簡便な方法で炭素/炭素複合材料を
製造する方法を提供することにある。Conventional problems and problems to be solved by the invention Carbon/
Carbon composite materials are materials that have unique properties such as maintaining high strength and high modulus of elasticity even at high temperatures of 1000°C or higher, and a low coefficient of thermal expansion, and are used as parts of aerospace equipment, brakes, furnace materials, etc. It is expected that it will be used for However, the manufacturing process for compositing the matrix and carbon fibers is complicated and takes a long time, resulting in high costs. An object of the present invention is to provide a method for producing a carbon/carbon composite material using a simple method.
問題点を解決するための手段
本発明者らは、前記問題点を解決した簡便な製造プロセ
スを開発すべく研究した結果、本発明の完成に至った。Means for Solving the Problems The present inventors conducted research to develop a simple manufacturing process that solved the above-mentioned problems, and as a result, they completed the present invention.
本発明は、(A)軟化点150〜400℃を有する炭素
質ピッチ5〜50重量部、(B)炭素質ピッチを紡糸し
て得られるピッチ繊維の不融化処理により得られる不融
化繊維およびこれらの不融化繊維をさらに不活性雰囲気
下、350〜800℃で前炭化処理して得られろ前炭化
m維からなる群より選ばれる1種または2種以上のm、
5t20〜95重量部、および(C)ピッチ系炭素wi
A維5〜80!を置部をプレス下あるいは加圧下で炭化
することを特徴とする炭素/炭素複合材料の製造法に関
する。The present invention relates to (A) 5 to 50 parts by weight of carbonaceous pitch having a softening point of 150 to 400°C, (B) infusible fibers obtained by infusible treatment of pitch fibers obtained by spinning carbonaceous pitch, and these infusible fibers. One or more types of m selected from the group consisting of pre-carbonized m fibers obtained by further pre-carbonizing the infusible fibers at 350 to 800°C in an inert atmosphere,
5t20 to 95 parts by weight, and (C) pitch-based carbon wi
Awei 5-80! The present invention relates to a method for producing a carbon/carbon composite material, which comprises carbonizing the deposited part under a press or under pressure.
以下、本発明について詳述する。The present invention will be explained in detail below.
本発明でいう、(^)炭素質ピッチとは、軟化点150
〜400℃好ましくは200〜350℃を有する石炭系
あるいは石油系のピッチである。炭素質ピッチは、光学
的に等方性のピッチあるいは異方性のピッチのいずれも
使用できるが、光学的異方性相の含量が60〜100v
o I%、好ましくは80〜100vo1%の光学的異
方性ピッチが特に好ましく用いられる。In the present invention, (^) carbonaceous pitch has a softening point of 150
It is a coal-based or petroleum-based pitch having a temperature of -400°C, preferably 200-350°C. As the carbonaceous pitch, either optically isotropic pitch or anisotropic pitch can be used, but the content of the optically anisotropic phase is 60 to 100v.
o I%, preferably 80 to 100 vol. optically anisotropic pitch is particularly preferably used.
本発明でいう、(B)ピッチ繊維とは、前記の炭素質ピ
ッチを公知の方法で溶融紡糸することにより得られる平
均直径5〜100μ転好ましくは7〜30μmの繊維で
ある。本発明でいう不融化m維とは、前記ピッチ!a雄
を不融化処理して得られる繊維である。不融化処理は、
酸化性ガス雰囲気下、50〜400℃、好ましくは10
0〜350℃で行うことができる。酸化性ガスとしては
、空気、酸素、窒素酸化物、硫黄酸化物、ハロゲン、あ
るいはこれらの混合物等が使用できる。不融化処理は通
常10分〜20時間実施する。一方、本発明でいう前炭
化繊維とは、前記不融化繊維をさらに前炭化処理して得
られるm維をいう。前炭化処理は、不活性ガス雰囲気下
、350〜800℃、好ましくは400〜700℃で行
い、通常10分〜5時間実施する。In the present invention, the pitch fiber (B) is a fiber having an average diameter of 5 to 100 μm, preferably 7 to 30 μm, obtained by melt-spinning the above-mentioned carbonaceous pitch by a known method. The infusible m-fiber referred to in the present invention refers to the pitch! It is a fiber obtained by infusible treatment of a male. The infusible treatment is
Under an oxidizing gas atmosphere, 50 to 400°C, preferably 10
It can be carried out at 0 to 350°C. As the oxidizing gas, air, oxygen, nitrogen oxides, sulfur oxides, halogens, or mixtures thereof can be used. The infusibility treatment is usually carried out for 10 minutes to 20 hours. On the other hand, the pre-carbonized fiber in the present invention refers to m-fiber obtained by further pre-carbonizing the infusible fiber. The pre-carbonization treatment is carried out under an inert gas atmosphere at 350 to 800°C, preferably 400 to 700°C, and is usually carried out for 10 minutes to 5 hours.
本発明でいう、(C)ピッチ系炭素1維とは、前記前炭
化繊維をさらに炭化あるいは黒鉛化処理して得られる繊
維をいう。In the present invention, (C) pitch-based carbon fiber refers to a fiber obtained by further carbonizing or graphitizing the pre-carbonized fiber.
炭化処理は、不活性ガス雰囲気下、700〜2000℃
で通常10分〜5時間実施する。また黒鉛化処理は、不
活性ガス雰囲気下、2000〜3000℃で通常1秒〜
5時間実施する。Carbonization treatment is performed at 700-2000℃ under an inert gas atmosphere.
It is usually carried out for 10 minutes to 5 hours. In addition, graphitization treatment is usually performed at 2000 to 3000°C for 1 second or more under an inert gas atmosphere.
It will be held for 5 hours.
本発明においては、(人)炭素質ピッチ5〜50重量部
、好ましくは10〜40重量部、CB)不融化繊維およ
び前炭化繊維からなる群より選ばれる1種または2種以
上の繊維20〜95重旦部、皿部しくは25〜50重量
部、および(C)ピッチ系炭素繊維5〜3000部、好
ましくは10〜7Ofi量部をプレス下あるいは加圧下
で炭化する。In the present invention, (human) 5 to 50 parts by weight of carbonaceous pitch, preferably 10 to 40 parts by weight, CB) 20 to 20 parts of one or more types of fibers selected from the group consisting of infusible fibers and pre-carbonized fibers. 95 parts by weight, 25 to 50 parts by weight, and (C) 5 to 3,000 parts of pitch-based carbon fiber, preferably 10 to 7 parts by weight, are carbonized under a press or under pressure.
プレス下の炭化は、ホットプレスにより不活性ガス雰囲
気下、5〜500kg/ct/、好ましくは10〜30
0kg/cd、400〜2000℃、好ましくは500
〜1500℃において実施する。加圧下の炭化は、不活
性ガスにより50〜10000kg/cd、好ましくは
100〜3000kg / crlに加圧し、400〜
2000℃、好ましくは500〜1500℃において実
施する。また、プレス下あるいは加圧下で炭化するに先
たち、繊維を室温において予備成型することもできる。Carbonization under press is performed by hot pressing under an inert gas atmosphere at 5 to 500 kg/ct/, preferably 10 to 30 kg/ct/
0kg/cd, 400-2000℃, preferably 500
Perform at ~1500°C. Carbonization under pressure is performed by pressurizing with an inert gas to 50 to 10,000 kg/cd, preferably 100 to 3,000 kg/crl, and
It is carried out at 2000°C, preferably 500-1500°C. The fibers can also be preformed at room temperature prior to carbonization under press or pressure.
加圧下あるいはプレス下での炭化の後に、必要に応じて
常圧下、不活性ガス雰囲気下400〜3000℃におい
て炭化あるいは黒鉛化してもよい。After carbonization under pressure or press, carbonization or graphitization may be carried out at 400 to 3000° C. under normal pressure and an inert gas atmosphere, if necessary.
(^)および(B)成分のみでは補強効果が不十分であ
り、(B)および(C)成分のみでは成形性が不足し、
補強材成分のアスペクト比を大きくすることが出来ない
。さらに(人)および(B)成分のみでは成形時に流動
性が過大となり、バインダー成分が流出して炭化装置の
汚染につながる。Components (^) and (B) alone have insufficient reinforcing effect, and components (B) and (C) alone have insufficient moldability.
It is not possible to increase the aspect ratio of the reinforcing material component. Furthermore, if only the (human) and (B) components are used, the fluidity will be excessive during molding, and the binder component will flow out, leading to contamination of the carbonization equipment.
(^)、 (Blおよび(C)の3成分を複合化する方
法としては、例えばこれらの成分を混合粉砕し、あるい
はこれらを個々に粉砕した後混合し、プレス下あるいは
加圧下で炭化する方法がある。混合粉砕は少なくとも繊
維の形状をとどめる程度までとし、それぞれのm維の1
/d(アスペクト比)は、2〜5000、好ましくは5
〜3000である。通常は不融化繊維あるいは前炭化繊
維の1/dをピッチ系炭素繊維のl/dよりも小さくす
る。(^), (A method for compounding the three components Bl and (C) is, for example, by mixing and pulverizing these components, or by pulverizing them individually, mixing them, and carbonizing them under a press or pressure. Mixing and crushing should be done at least to the extent that the fibers retain their shape, and 1 m fibers of each
/d (aspect ratio) is 2 to 5000, preferably 5
~3000. Usually, 1/d of the infusible fiber or pre-carbonized fiber is smaller than 1/d of the pitch-based carbon fiber.
他の例としては、(A)および(B)の2成分を混合粉
砕し、これを(C)成分であるピッチ系炭素!!維の織
物内あるいは織物間に充填し、ともにプレス下あるいは
加圧下で炭化する方法がある。As another example, the two components (A) and (B) are mixed and ground, and this is mixed with pitch-based carbon, which is the component (C)! ! There is a method of filling the fibers into or between the fibers and carbonizing both under a press or under pressure.
衷塵男 以下に実施例をあげ、本発明を具体的に説明する。man in the dust EXAMPLES The present invention will be specifically explained below with reference to Examples.
(実施例1)
(入)軟化点280℃を有する光学的異方性相100v
o1%の石油系ピッチ、(B)前記石油系ピッチを溶融
紡糸し、平均直径13μmのピッチ繊維とし、さらにこ
のピッチ繊維を空気中240℃で不融化処理して得た不
融化繊維および(C)アスペクト比が300のピッチ系
炭素繊維の3成分を、33重皿部、33瓜量部および3
3重量部の割合で混合、粉砕し、ホットプレスにより1
00kg/c+/の圧力下、1000℃において30分
プレス炭化し、かさ密度1.6g/ccの炭素/炭素複
合材料を製造した。ホットプレス装置内のよごれは極め
て軽微であり、得られた材料の空隙率は10%未満であ
った。偏光顕微鏡あるいは電子顕微鏡を用いた観察によ
り、繊維組織がきわめて均一に分布していることも明ら
かとなった。(Example 1) (Enter) Optically anisotropic phase with a softening point of 280°C 100v
o 1% petroleum pitch, (B) the above petroleum pitch was melt-spun to produce pitch fibers with an average diameter of 13 μm, and the pitch fibers were further infusible treated in air at 240°C; ) Three components of pitch-based carbon fiber with an aspect ratio of 300 were mixed into a 33-layer plate portion, 33 melon portion, and 3
Mix 3 parts by weight, crush, and hot press to 1
Press carbonization was performed at 1000° C. for 30 minutes under a pressure of 00 kg/c+/ to produce a carbon/carbon composite material with a bulk density of 1.6 g/cc. There was very little dirt in the hot press equipment, and the resulting material had a porosity of less than 10%. Observation using a polarizing microscope or an electron microscope revealed that the fiber structure was extremely uniformly distributed.
(比較例1)
実施例1の不融化m維を粉砕し、アスペクト比が300
のピッチ系炭素繊維と共に、ホットプレスによりIQO
kg/cfの圧力下、1000℃において30分プレス
炭化し、かき密度1.6g/ ecの材料を製造した。(Comparative Example 1) The infusible m-fiber of Example 1 was pulverized and the aspect ratio was 300.
IQO is made by hot pressing with pitch-based carbon fiber.
Press carbonization was performed at 1000° C. for 30 minutes under a pressure of kg/cf to produce a material with a scraping density of 1.6 g/ec.
得られた材料の空隙率は10%未満であったが成形性が
不十分であった。The porosity of the obtained material was less than 10%, but the moldability was insufficient.
(比較例2)
実施例1のピッチ系炭素m維を、ホットプレスにより1
00kg/c+/の圧力下、1000℃において30分
プレス炭化したところ、得られたものは成形性が悪く、
機械加工ができなかった。(Comparative Example 2) The pitch-based carbon m fibers of Example 1 were heated to 1
When press carbonized at 1000°C for 30 minutes under a pressure of 00 kg/c+/, the obtained product had poor moldability.
Machine processing was not possible.
(比較例3)
実施例1のピッチおよびピッチ系炭素繊維を、ホットプ
レスにより100kg/at/の圧力下、1000℃に
おいて30分プレス炭化したところ、ピッチが流出し良
好に成形できなかった。(Comparative Example 3) When the pitch and pitch-based carbon fiber of Example 1 were press-carbonized by hot pressing at 1000° C. for 30 minutes under a pressure of 100 kg/at/, the pitch flowed out and could not be molded well.
また炉内が汚染された。The inside of the furnace was also contaminated.
(実施例2)
(八)軟化点280℃を有する光学的異方性相100v
o1%の石油系ピッチの粉末、(B)前記石油系ピッチ
を溶融紡糸し、平均直径13μmのピッチ繊維とし、こ
れを空気中300℃で1時間不融化処理した後、窒素中
、400℃で1時間処理して前炭化繊維を得た。この前
炭化繊維トウ375重量部を粉砕してl/dが10の繊
維とし、これに前記ピッチの粉砕物375重量部および
(C)ピッチ系炭素m維を粉砕して得たl/dが50の
繊維25重量部を混合し、ホットプレスにより100k
g / c+/の圧力下、600℃において1時間プレ
ス炭化した。この炭化物を窒素雰囲気下1200℃30
分焼成しかさ密度1.6g/ccの炭素繊維含有材料を
製造した。得られた炭素材料の空隙率は10%未満であ
った。偏光顕微鏡あるいは電子顕微鏡を用いた観察によ
り、m維組造がきわめて均一に分布していることも明ら
かとなった。(Example 2) (8) Optically anisotropic phase with a softening point of 280°C 100v
o1% petroleum pitch powder, (B) The petroleum pitch was melt-spun to form pitch fibers with an average diameter of 13 μm, which was infusible in air at 300°C for 1 hour, and then in nitrogen at 400°C. After processing for 1 hour, pre-carbonized fibers were obtained. 375 parts by weight of the pre-carbonized fiber tow was pulverized into fibers with an l/d of 10, and 375 parts by weight of the pulverized pitch product and (C) the l/d obtained by pulverizing the pitch-based carbon fibers were added to the fibers. Mix 25 parts by weight of fibers of 50% and make 100k by hot pressing.
Press carbonized for 1 hour at 600 °C under a pressure of g/c+/. This carbide was heated at 1200℃30 in a nitrogen atmosphere.
A separately fired carbon fiber-containing material with a bulk density of 1.6 g/cc was produced. The porosity of the obtained carbon material was less than 10%. Observation using a polarizing microscope or an electron microscope revealed that the m-fiber structure was extremely uniformly distributed.
(実施例3)
軟化点280℃を有する光学的異方性相90vo I%
の石油系ピッチを溶融紡糸し、平均直径13μmのピッ
チ繊維とし、これを空気中300℃で1時間不融化処理
して不融化m維を得た。この不融化繊維25重丘部と前
記ピッチ繊維25重量部を混合粉砕し、ピッチ系炭素m
維の平織50重厘部のあいだに充填して、ホットプレス
により50kg/cdの圧力下、窒素雰囲気中1200
℃30分焼成し、かさ密度1.7g/ccの炭素繊維含
有材料を製造した。得られた炭素材料の空隙率は10%
未満であった。偏光1黴鏡あるいは電子顕微鏡を用いた
観察により、繊維組織がきわめて均一に分布しているこ
とも明らかとなった。(Example 3) Optically anisotropic phase with a softening point of 280°C 90vo I%
The petroleum-based pitch was melt-spun to obtain pitch fibers with an average diameter of 13 μm, which were then treated to be infusible in air at 300° C. for 1 hour to obtain infusible m-fibers. 25 parts by weight of this infusible fiber and 25 parts by weight of the pitch fiber were mixed and pulverized, and pitch-based carbon m
Filled between 50 layers of plain weave fiber, and hot pressed under a pressure of 50 kg/cd in a nitrogen atmosphere at 1200 kg/cm.
C. for 30 minutes to produce a carbon fiber-containing material with a bulk density of 1.7 g/cc. The porosity of the obtained carbon material is 10%
It was less than Observation using a polarized light mirror or an electron microscope revealed that the fiber structure was extremely uniformly distributed.
(実施例4)
軟化点280℃を有する光学的異方性相100vo1%
の石油系ピッチを溶融紡糸して得た平均直径13μmの
ピッチ繊維を空気中300℃で1時間不融化処理した後
、窒素中、350℃で1時間処理して、前炭化繊維を得
た。この前炭化繊維トウを粉砕して1/dが10の繊維
とし、乙の!!を維24重量部に前記ピッチの粉砕物1
6重量部を混合し、ピッチ系炭素繊維の平織60重量部
のあいだに充填したのち、ステンレス容器中に入れ、2
00kg/ctの圧力下、窒素雰囲気中1000℃30
分加圧炭化しかぎ密度1.5g/ccの炭素繊維含有材
料を製造した。得られた炭素材料の空隙率は5%未満で
あった。偏光!a徹鏡あるいは電子顕微鏡を用いた観察
により、繊維組織マトリックスがきわめて均一に分布し
ていることも明らかとなった。(Example 4) 100vo1% optically anisotropic phase with a softening point of 280°C
Pitch fibers having an average diameter of 13 μm obtained by melt-spinning petroleum-based pitch were treated to be infusible in air at 300° C. for 1 hour, and then treated in nitrogen at 350° C. for 1 hour to obtain pre-carbonized fibers. Before this, the carbonized fiber tow was crushed into fibers with a 1/d ratio of 10. ! 24 parts by weight of the pulverized pitch
After mixing 6 parts by weight and filling it between 60 parts by weight of plain weave pitch-based carbon fibers, it was placed in a stainless steel container and 2 parts by weight were mixed.
1000℃30 in a nitrogen atmosphere under a pressure of 00kg/ct
A carbon fiber-containing material having a partial pressure carbonization key density of 1.5 g/cc was produced. The porosity of the obtained carbon material was less than 5%. Polarization! Observation using a speculum or electron microscope revealed that the fibrous tissue matrix was extremely uniformly distributed.
Claims (1)
ッチ5〜50重量部、(B)炭素質ピッチを紡糸して得
られるピッチ繊維の不融化処理により得られる不融化繊
維およびこれらの不融化繊維をさらに不活性雰囲気下、
350〜800℃で前炭化処理して得られる前炭化繊維
からなる群より選ばれる1種または2種以上の繊維20
〜95重量部、および(C)ピッチ系炭素繊維5〜80
重量部をプレス下あるいは加圧下で炭化することを特徴
とする炭素/炭素複合材料の製造法。(1) (A) 5 to 50 parts by weight of carbonaceous pitch having a softening point of 150 to 400°C, (B) Infusible fibers obtained by infusibility treatment of pitch fibers obtained by spinning carbonaceous pitch, and these The infusible fibers are further heated under an inert atmosphere.
One or more types of fibers selected from the group consisting of pre-carbonized fibers obtained by pre-carbonizing at 350 to 800°C 20
~95 parts by weight, and (C) 5 to 80 parts by weight of pitch-based carbon fiber
A method for producing a carbon/carbon composite material characterized by carbonizing a weight part under a press or under pressure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63058367A JPH07100630B2 (en) | 1988-03-14 | 1988-03-14 | Method for manufacturing carbon / carbon composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63058367A JPH07100630B2 (en) | 1988-03-14 | 1988-03-14 | Method for manufacturing carbon / carbon composite material |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH01234367A true JPH01234367A (en) | 1989-09-19 |
JPH07100630B2 JPH07100630B2 (en) | 1995-11-01 |
Family
ID=13082355
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63058367A Expired - Lifetime JPH07100630B2 (en) | 1988-03-14 | 1988-03-14 | Method for manufacturing carbon / carbon composite material |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07100630B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0477359A (en) * | 1990-07-17 | 1992-03-11 | Toyota Motor Corp | Carbon fiber reinforced carbon sintered body |
JPH06501232A (en) * | 1990-07-19 | 1994-02-10 | イギリス国ロンドン エスダブリュー 1ピー・2ピーエル,ビンセント・スクウェアー,シルバータウン・ハウス | Carbon-carbon composite material |
-
1988
- 1988-03-14 JP JP63058367A patent/JPH07100630B2/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0477359A (en) * | 1990-07-17 | 1992-03-11 | Toyota Motor Corp | Carbon fiber reinforced carbon sintered body |
JPH06501232A (en) * | 1990-07-19 | 1994-02-10 | イギリス国ロンドン エスダブリュー 1ピー・2ピーエル,ビンセント・スクウェアー,シルバータウン・ハウス | Carbon-carbon composite material |
Also Published As
Publication number | Publication date |
---|---|
JPH07100630B2 (en) | 1995-11-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4849200A (en) | Process for fabricating carbon/carbon composite | |
JPH01252577A (en) | Production of carbon/carbon composite material | |
US3943213A (en) | Method for manufacturing high temperature graphite fiber-graphite composites | |
WO1999061390A1 (en) | Method for producing shaped bodies on the basis of carbon, carbides and/or carbonitrides | |
US3719452A (en) | Carbonaceous material and method of preparation | |
JPH01234367A (en) | Production of carbon/carbon composite material | |
JPH06183835A (en) | Production of preform body for staple fiber-reinforced c/c composite and preform body production by the same method | |
JPH05330915A (en) | Production of carbon/carbon composite material | |
JPH0768064B2 (en) | Carbon fiber reinforced composite material | |
JP2635634B2 (en) | Method for producing carbon fiber reinforced carbon material | |
JPH04370223A (en) | Carbon fiber and its production | |
JPH01203267A (en) | Production of carbon/carbon composite material | |
JPH0569061B2 (en) | ||
JP2676211B2 (en) | Method for manufacturing carbon / carbon composite material | |
JPH0559863B2 (en) | ||
JP2566555B2 (en) | Method for producing carbon fiber reinforced carbon composite material | |
JPH0647497B2 (en) | Carbon material manufacturing method | |
KR970008693B1 (en) | Process for the preparation of carbon composite material | |
JPH06321633A (en) | Shock-resistant carbon-carbon composite material and its production | |
JPS63215565A (en) | Manufacture of carbon/carbon composite material | |
JPH0569060B2 (en) | ||
JP3138939B2 (en) | Method for producing carbon / carbon composite material | |
EP0656331A2 (en) | A method for preparing a carbon/carbon composite material | |
JPH01145373A (en) | Production of carbon fiber-reinforced carbonaceous material | |
JPS6153104A (en) | Production of high-strength carbon material |