JPH0798682B2 - Method for producing high-density carbon composite material - Google Patents
Method for producing high-density carbon composite materialInfo
- Publication number
- JPH0798682B2 JPH0798682B2 JP63115471A JP11547188A JPH0798682B2 JP H0798682 B2 JPH0798682 B2 JP H0798682B2 JP 63115471 A JP63115471 A JP 63115471A JP 11547188 A JP11547188 A JP 11547188A JP H0798682 B2 JPH0798682 B2 JP H0798682B2
- Authority
- JP
- Japan
- Prior art keywords
- container
- impregnating
- pressure
- carbon composite
- molded body
- 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 - Lifetime
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims description 15
- 229910052799 carbon Inorganic materials 0.000 title claims description 15
- 239000002131 composite material Substances 0.000 title claims description 13
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 239000000463 material Substances 0.000 claims description 47
- 239000007789 gas Substances 0.000 claims description 21
- 239000003575 carbonaceous material Substances 0.000 claims description 14
- 229910052739 hydrogen Inorganic materials 0.000 claims description 7
- 239000011347 resin Substances 0.000 claims description 7
- 229920005989 resin Polymers 0.000 claims description 7
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 6
- 239000001257 hydrogen Substances 0.000 claims description 6
- 238000010000 carbonizing Methods 0.000 claims description 5
- 239000007769 metal material Substances 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims 2
- 239000002184 metal Substances 0.000 claims 2
- 239000000956 alloy Substances 0.000 claims 1
- 229910045601 alloy Inorganic materials 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 14
- 238000005470 impregnation Methods 0.000 description 11
- 239000011295 pitch Substances 0.000 description 11
- 239000002775 capsule Substances 0.000 description 10
- 238000003763 carbonization Methods 0.000 description 10
- 238000003466 welding Methods 0.000 description 10
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 4
- 239000011148 porous material Substances 0.000 description 4
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000007667 floating Methods 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000007872 degassing Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 239000011301 petroleum pitch Substances 0.000 description 2
- 239000011271 tar pitch Substances 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000007770 graphite material Substances 0.000 description 1
- 238000005087 graphitization Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000001513 hot isostatic pressing Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 125000001997 phenyl group Chemical group [H]C1=C([H])C([H])=C(*)C([H])=C1[H] 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
- C04B35/521—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite obtained by impregnation of carbon products with a carbonisable material
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
Description
【発明の詳細な説明】 (産業上の利用分野) 本発明は、ポーラスなカーボン成形体に、タール・ピッ
チや樹脂などを含浸し、これを炭化させてより高密度の
カーボン材料を製造する技術に関するものであり、ロケ
ットノズルや航空機用ブレーキなど航空宇宙産業などの
新材料として用いられる。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention is a technique for producing a higher density carbon material by impregnating a porous carbon molded body with tar / pitch, resin or the like and carbonizing the same. It is used as a new material for the aerospace industry such as rocket nozzles and aircraft brakes.
(従来の技術) 近年、炭素繊維と炭素材料の複合材料(C/Cコンポジッ
ト)は、ロケットノズルや航空機用ブレーキなど航空宇
宙産業における新しい材料として急速に普及しつつあ
る。またこのC/Cコンポジットは軽量・高強度でかつ熱
容量が小さいことや、衝撃強度に優れていることから、
不活性雰囲気で使用される高温炉の炉構造材料や棚板材
としてもその利用が進みつつある。(Prior Art) In recent years, a composite material of carbon fiber and a carbon material (C / C composite) is rapidly spreading as a new material in the aerospace industry such as a rocket nozzle and an aircraft brake. In addition, because this C / C composite is lightweight, has high strength, has a small heat capacity, and has excellent impact strength,
It is also being used as a furnace structural material for high temperature furnaces used in an inert atmosphere and as a shelf board material.
また、従来の黒鉛材料についても、近年、高品質化が進
み、結晶粉が微細でかつ気孔の少ない緻密な材料の需要
が増加しつつある。Further, the quality of conventional graphite materials has been improved in recent years, and the demand for dense materials having fine crystal powder and few pores is increasing.
これらカーボン材料の製造における最大の技術的課題
は、いかにして高密度にするかということにある。特に
工業規模での高密度化の技術確立が業界における大きな
課題となっている。The biggest technical challenge in the production of these carbon materials is how to achieve high density. In particular, the establishment of high-density technology on an industrial scale has become a major issue in the industry.
これら材料の高密度化の技術として、ポーラスな成形体
にタール・ピッチや樹脂などの炭化性物質を含浸した
後、炭化させる技術があり、通常、真空下で含浸して、
これを大気圧下で焼成する方法が用いられている。As a technology for increasing the density of these materials, there is a technology of impregnating a porous molded body with a carbonaceous substance such as tar / pitch or a resin, and then carbonizing the same.
A method of firing this under atmospheric pressure is used.
高圧ガスの圧力下で、タール・ピッチを含浸し、炭化す
る技術としては例えば、第7図に示す如き、Fiber Mate
rials Inc社(米国)の技術が公知である。この場合、C
/Cコンポジットが対象となっており、この成形体はカー
ボン繊維を主体とするものである。As a technique for impregnating tar / pitch and carbonizing under the pressure of high-pressure gas, for example, as shown in FIG.
The technology of rials Inc (USA) is known. In this case C
The target is the / C composite, and this molded body is mainly composed of carbon fiber.
成形体中にタール・ピッチを200℃で真空含浸した後、
大気圧下850℃でタール・ピッチを炭化させる。得られ
た成形体の外面を荒加工した後、気密性のカンの中にタ
ール・ピッチと共に入れ、再び真空含浸した後、カンを
密封する。密封したカンを高温・高圧炉中に入れ、カン
の外側から、アルゴンガスの圧力をかけた状態で昇温・
加圧して最終的に650℃,10,000psi(約700kg f/cm2)の
温度・圧力で炭化させる。炭化処理後、カンを除去し黒
鉛化処理を行う。After vacuum impregnating the molded product with tar and pitch at 200 ° C,
Carbonizes tar pitch at 850 ° C under atmospheric pressure. After rough-processing the outer surface of the obtained molded body, it is put together with tar pitch in an airtight can, vacuum impregnated again, and then the can is sealed. Place the sealed can in a high-temperature, high-pressure furnace and raise the temperature with the pressure of argon gas applied from the outside of the can.
Pressurize and finally carbonize at 650 ° C and 10,000 psi (about 700 kg f / cm 2 ) temperature and pressure. After carbonization, the can is removed and graphitization is performed.
(発明が解決しようとする課題) 前記の第7図に示された技術については、図に示された
カンの材質や形状、さらには真空封入の方法などで公開
されたものはなく、第7図に模式的に示されたカンを本
発明者らが製作して実際に処理を行ったところ、次のよ
うな問題点が見出された。(Problems to be Solved by the Invention) With regard to the technique shown in FIG. 7, there is no disclosure of the material and shape of the can shown in the diagram, and further, the method of vacuum sealing, etc. When the present inventors produced a can schematically shown in the figure and actually processed it, the following problems were found.
1) 本含浸に用いるタール・ピッチや樹脂は炭素収率
をかせぐ意味から、高分子量のすなわち室温では固形の
ものが用いられるが、固形のタール・ピッチ等の塊や粉
を容器に充填すると、嵩密度が低く、含浸操作時のガス
圧での圧縮で容器が大変形を生じ、気密性が損われた
り、処理材がイビツになる。1) The tar / pitch and the resin used for the main impregnation have a high molecular weight, that is, a solid one at room temperature from the meaning of increasing the carbon yield. However, if solid lumps or powders such as tar / pitch are filled in a container, The bulk density is low, and the container is largely deformed by the compression with the gas pressure during the impregnation operation, and the airtightness is impaired, or the treatment material becomes irritated.
2) 通常のHIPで使用される鋼製の容器(カプセル)
は、第6図のような形状で、その肉厚は直径の1〜2.5
%であるが、このようなカプセルを用いると、含浸操作
時は200〜300℃という比較的低温で、数100〜2000kg f/
cm2のガス圧力での圧縮に対し、十分な変形能をもって
おらず、容器がイビツに変形したり、破れたりして、所
期の効果が得られない。2) Steel container (capsule) used in normal HIP
Has a shape as shown in Fig. 6, and its wall thickness is 1 to 2.5 of the diameter.
%, But when such a capsule is used, the impregnation operation is carried out at a relatively low temperature of 200 to 300 ° C. and several hundred to 2000 kg f /
It does not have sufficient deformability with respect to compression at a gas pressure of cm 2 , and the container is deformed or broken, and the desired effect cannot be obtained.
なお、第6図において、1は底1Aを有するカプセル胴部
(容器)、2はカプセル蓋、3は脱気管、4は処理物
(炭素材料成形体)である。In FIG. 6, 1 is a capsule body (container) having a bottom 1A, 2 is a capsule lid, 3 is a deaeration tube, and 4 is a treated product (carbon material molded body).
本発明は、この含浸に高圧力を用いて微細な気孔にまで
含浸材を含浸し、かつ、これを高圧ガス雰囲気下で炭化
させて第5図に示すように炭素の収率を向上して、効率
良く高密度の炭素材料を製造しようとすることが目的で
ある。In the present invention, high pressure is used for this impregnation to impregnate the impregnating material into even fine pores, and the impregnating material is carbonized in a high pressure gas atmosphere to improve the carbon yield as shown in FIG. The purpose is to efficiently produce a high-density carbon material.
(課題を解決するための手段) 本発明は、ポーラスな炭素材料成形体に、タール・ピッ
チや樹脂などの炭化性物質を含浸し、この含浸材を炭化
して高密度の炭素複合材料を製造する方法において、叙
述の目的を達成するために、次の技術的手段を講じたの
である。(Means for Solving the Problems) According to the present invention, a porous carbon material compact is impregnated with a carbonaceous substance such as tar / pitch or resin, and the impregnated material is carbonized to produce a high-density carbon composite material. In order to achieve the stated purpose, the following technical measures were taken.
すなわち、本発明は、気密性の金属材料からなる薄肉の
容器中に、隙間をもたせて炭素材料成形体を収め、大気
圧下または減圧下にて容器と炭素材料成形体の前記隙間
を溶融したタール・ピッチなどの含浸材で充填して成形
体全体を覆うようにした後、気密性の金属材料からなる
蓋を容器に気密に結合し、この容器全体を熱間静水圧プ
レス装置内に装入し、該装置内部の圧媒ガス置換操作を
行った後、タール・ピッチなどの含浸材が溶融して液状
となる温度に昇温し、圧媒ガスを加えて容器ごと圧縮す
ることで含浸材を成形体に含浸し、次いで昇温して高圧
力下で含浸材の一部もしくは全部を炭化することを特徴
とするのである。That is, the present invention, in a thin container made of an airtight metal material, the carbon material compact is placed with a gap, and the gap between the container and the carbon material compact is melted under atmospheric pressure or reduced pressure. After filling with an impregnating material such as tar and pitch to cover the entire molded body, a lid made of an airtight metallic material is airtightly connected to the container, and the entire container is mounted in a hot isostatic press. After performing the pressure medium gas replacement operation inside the device, the temperature is raised to a temperature at which the impregnating material such as tar and pitch melts and becomes a liquid, and the pressure medium gas is added to compress the whole container to impregnate. It is characterized in that the material is impregnated into the molded body, and then the temperature is raised to carbonize a part or all of the impregnated material under high pressure.
(作 用) 前記の1)の問題点を解決する方法(手段)としては、
含浸材の嵩密度向上の観点から、粉末あるいは塊状のタ
ール・ピッチや樹脂などの含浸材を一旦、加熱して溶融
させて、容器と成形体の隙間を充填する方法が最も好ま
しい。この場合、固形状の含浸材を成形体と共に容器中
に配置した後、全体を加熱して含浸材を溶融せしめても
良いし、含浸材を別途加熱溶融せしめて、これを成形体
が収納された容器中に静かに注ぎ込んでも良い。(Operation) As a method (means) for solving the problem of 1) above,
From the viewpoint of improving the bulk density of the impregnating material, the most preferable method is to heat and melt the impregnating material such as powder or lump tar / pitch or resin to fill the gap between the container and the molded body. In this case, after the solid impregnating material is placed in the container together with the molded body, the entire body may be heated to melt the impregnating material, or the impregnating material may be separately heated and melted to store the molded body in the container. You can pour it gently into the container.
このような操作は、大気中で実施しても良いが、溶融し
た含浸材と成形体が共存している状態で真空引きして減
圧下においてやると、含浸材中の気泡が効率良く除去で
きて嵩密度を大きく向上できるばかりか、一部の含浸材
はこの時点で成形体に含浸されるので成形体のみかけの
密度が上がり、浮力による成形体の浮上を防止すること
ができる。特に、ポアの量の多い成形体に本発明を適用
する際に効果的である。また、この操作の時にしばしば
経験される成形体の浮上りに対しては、容器に成形体の
浮上防止用の押さえを設けておくことが好ましい。Such an operation may be performed in the atmosphere, but if the molten impregnated material and the molded body are coexistent and the vacuum is applied and the pressure is reduced, the bubbles in the impregnated material can be efficiently removed. Thus, not only the bulk density can be greatly improved, but also a part of the impregnating material is impregnated in the molded body at this point, so that the apparent density of the molded body is increased and the floating of the molded body due to buoyancy can be prevented. In particular, it is effective when the present invention is applied to a molded product having a large amount of pores. In addition, it is preferable to provide a container with a presser for preventing the floating of the molded body against the floating of the molded body which is often experienced during this operation.
2)の問題点の解決には、容器の材質、形状、肉厚の最
適化が必要である。これらは、熱間静水圧プレス装置内
での温度および圧力の操作に依存する。第4図に本発明
者らが実験的に行った温度、圧力のパターンの例を示
す。In order to solve the problem 2), it is necessary to optimize the material, shape, and thickness of the container. These depend on the manipulation of temperature and pressure within the hot isostatic press. FIG. 4 shows an example of temperature and pressure patterns experimentally conducted by the present inventors.
ここで、含浸工程の温度は含浸材が溶融して液状を呈
し、かつ含浸材が分解・炭化しない温度で、この温度は
含浸材の種類により異るが、通常200〜300℃である。こ
の含浸工程では、徐々に容器外部の圧力を増加し、容器
全体を圧縮して容器内の溶融した含浸材を成形体の気孔
中に押し込む訳であるが、圧力により溶融した含浸材の
体積が収縮することと併わせ、場合によっては容器は大
きく収縮する。Here, the temperature of the impregnating step is a temperature at which the impregnating material melts to give a liquid state, and the impregnating material does not decompose or carbonize. In this impregnation step, the pressure outside the container is gradually increased, the entire container is compressed and the molten impregnating material in the container is pushed into the pores of the molded body. Combined with shrinking, in some cases the container shrinks significantly.
したがって、容器はこのような圧力の作用に対し、柔軟
に変形してくれることが好ましい。200〜300℃で、柔軟
に変形してくれる金属材料としては、アルミ,銅,鉛,
亜鉛などがあげられるが、肉厚によっては鋼も十分使用
可能である。含浸工程後の炭化工程で曝される温度は、
含浸材をどの程度炭化させるかに依存する通常600℃以
上であり、600℃でも溶融しないアルミ,銅,鋼が本発
明には好適である。Therefore, it is preferable that the container flexibly deforms under the action of such pressure. Aluminum, copper, lead, and metallic materials that flexibly deform at 200-300 ℃
Examples include zinc, but depending on the wall thickness, steel can also be used. The temperature exposed in the carbonization process after the impregnation process is
Aluminum, copper, and steel, which usually have a temperature of 600 ° C. or higher, which does not melt even at 600 ° C., are suitable for the present invention, depending on how much the impregnating material is carbonized.
また、肉厚は用いる材料の変形能にもよるが、前記の通
常のカプセルより薄い方が好ましく、円柱状の場合に
も、直径の0.2〜1%程度が適している。薄い方が良い
理由は、前記の変形能のほか、炭化工程後の減圧時に、
カプセル内に充満した炭化反応で発生したメタンや水素
などのガス圧力によりカプセルが膨れた際に延性的に破
断して、カプセルが爆発的に破裂するのを防ぐことがで
きるからである。Although the wall thickness depends on the deformability of the material used, it is preferably thinner than the above-mentioned ordinary capsules, and even in the case of a cylindrical shape, about 0.2 to 1% of the diameter is suitable. The reason why it is better to be thin is that, in addition to the deformability described above, during depressurization after the carbonization step,
This is because it is possible to prevent the capsule from explosively bursting due to ductile fracture when the capsule is swollen due to gas pressure of methane or hydrogen generated by the carbonization reaction filled in the capsule.
さらに、容器の形状については、第1図に示すように胴
部をベローズ状に形成すると、前記の含浸工程での大き
な収縮を容易に対応できる。特に円板状の成形体を重ね
た場合等に適している。Further, regarding the shape of the container, if the body portion is formed into a bellows shape as shown in FIG. 1, it is possible to easily cope with the large shrinkage in the impregnation step. It is particularly suitable for stacking disc-shaped compacts.
なお、第1図において、1は容器で、その胴部にベロー
ズ形状部1Aを有し、この容器1中に、隙間を有して炭素
材料成形体4が収められており、隙間はタール・ピッチ
や樹脂などの炭化性物質5で充填され、脱気管3を有す
る蓋2で施蓋されている。In FIG. 1, reference numeral 1 denotes a container, which has a bellows-shaped portion 1A in its body, and a carbon material molded body 4 is accommodated in this container 1 with a gap, and the gap is made of tar. It is filled with a carbonizable substance 5 such as pitch or resin, and is covered with a lid 2 having a degassing pipe 3.
以上のほか、容器と蓋の結合についても通常、溶接が用
いられることから、溶接時の熱による含浸材の分解変質
や分解時に発生するガスによる溶接部分の欠陥発生防止
などに配慮が必要である。In addition to the above, welding is usually used to connect the container and the lid, so it is necessary to consider measures such as decomposition and alteration of the impregnated material due to heat during welding and prevention of defects in the welded part due to gas generated during decomposition. .
第2図は、このような配慮を行った容器と蓋の結合方法
の例である。容器1中に前述の如き方法で成形体4と含
浸材5を充填した後、含浸材が溶融したまゝでも、冷却
固化した状態でも良いが、脱気管3のついた蓋2を容器
1に装着し端部を溶接6により結合する。溶接時の熱に
よる含浸材5の分解を防ぐため溶接部位と含浸材の間の
距離を通常のカプセルより長くとることが好ましい。溶
接後、脱気管から内部を真空に引きつつ、脱気管を圧着
7する。この圧着部分は余分な管を切断除去したのち、
溶接により気密性を完全にすることも推奨される。この
ように最後に封着する部分は、溶接する場合には溶接の
熱で、内部の含浸材が過熱されないようなところにする
ことが気密性確保の点から好ましい。FIG. 2 shows an example of a method of connecting the container and the lid, in which such consideration is taken. After filling the molded body 4 and the impregnating material 5 into the container 1 by the above-mentioned method, the impregnating material may be melted or cooled and solidified, but the lid 2 with the degassing pipe 3 is attached to the container 1. It is attached and the ends are joined by welding 6. In order to prevent the impregnated material 5 from being decomposed by heat during welding, it is preferable to make the distance between the welded portion and the impregnated material longer than that of a normal capsule. After welding, the deaeration tube is pressure-bonded 7 while the inside of the deaeration tube is evacuated. For this crimped part, after cutting and removing excess pipe,
It is also recommended to complete the hermeticity by welding. In this way, it is preferable from the viewpoint of ensuring airtightness that the portion to be finally sealed is a place where the impregnating material inside is not overheated by the heat of welding when welding.
このようにして準備した容器を図示していないが、熱間
静水圧プレス装置に装入し、装置内の空気を、圧媒ガス
によるガス置換などにより除去した後、第4図に示した
ような温度、圧力パターンにて含浸炭化処理を行う。炭
化工程では含浸材の分解により炭化が進むが、この時に
発生するガスは、温度が上昇するにつれてベンゼン環を
含む炭化水素から、メタン,水素へと分解してゆく。含
浸材中の水素が全てH2OやH2など分子量の小さな物質に
変化した時が、固定炭素の収率が高くなるので、このよ
うな反応が推奨されて、かつ容器内の発生ガスの圧力が
容器外の圧媒ガスの圧力より高くならないようにする目
的で、水素を吸収するゲッター材を予め容器内にセット
しておくことも推奨される。Although not shown, the container prepared in this manner was charged into a hot isostatic press, and after the air in the device was removed by gas replacement with a pressure medium gas, as shown in FIG. Impregnation carbonization is performed at various temperatures and pressure patterns. In the carbonization process, carbonization proceeds due to the decomposition of the impregnated material, but the gas generated at this time decomposes from the hydrocarbon containing the benzene ring into methane and hydrogen as the temperature rises. When all the hydrogen in the impregnated material changes to a substance with a small molecular weight such as H 2 O or H 2 , the yield of fixed carbon increases, so such a reaction is recommended and the gas generated in the container is In order to prevent the pressure from becoming higher than the pressure of the pressure medium gas outside the container, it is also recommended to previously set a getter material that absorbs hydrogen in the container.
炭化工程後の減圧工程では、このようにして発生したガ
スが容器内に溜っているため、この圧力によっては容器
外側の圧媒ガスの圧力が容器内の圧力より低くなると、
容器は膨れて最後には一番弱い部分に亀裂が入り、内部
のガスが抜ける。この亀裂が急激に生じると急激に容器
内からガスが放出され、内部の成形体を割ったり、熱間
静水圧プレス装置のヒータを破損したりする。前記の如
く、変形能が大きな材料で、かつ薄肉の容器を用いる
と、この亀裂は小さな穴が発生するような形態で生じる
ので好適である。In the depressurizing step after the carbonization step, since the gas thus generated is accumulated in the container, depending on this pressure, when the pressure of the pressure medium gas outside the container becomes lower than the pressure in the container,
The container swells and finally the weakest part cracks and the gas inside escapes. When this crack is suddenly generated, gas is suddenly released from the container, the molded body inside is cracked, and the heater of the hot isostatic pressing device is damaged. As described above, when a thin container having a large deformability is used, this crack is suitable because a small hole is formed.
(実施例) PAN系の炭素繊維30体積パーセント、カーボン30体積パ
ーセントを含む開気孔率、約35パーセントの成形体を第
3図(a)に示したように形状の銅製の容器1内に配置
し、容器1と成形体4の隙間に平均粒径3mm程度に粉砕
した石油ピッチ5Aを充填し、この容器1を真空中で300
℃まで加熱昇温し、石油ピッチを溶融し、成形体4の全
体を含浸材5で覆った。この時の状態は、第3図(b)
の如くである。次いで水素ゲッターとしてのチタン箔8
を入れた後、第3図(c)の如く脱気管3の付いた蓋2
を容器1にはめ込み、端部を溶接6により結合した。脱
気管3に真空ポンプを接続し、真空引きしながら脱気管
3を潰し圧接した。余分な脱気管を切断し、切断口を溶
接によりシールした。この容器1を図示省略したが熱間
静水圧プレス装置内に入れ、第4図に示した温度、圧力
パターンにて含浸炭化処理を行った。処理後、容器を熱
間静水圧プレス装置から取り出し、容器を切断して中の
成形体を回収した。開気孔率は約13%で、十分炭化され
ていることが判明した。比重は約1.4g/ccから約1.58g/c
cに増加し、十分な密度向上効果が確認された。(Example) A molded body having 30% by volume of PAN-based carbon fiber and about 35% open porosity containing 30% by volume of carbon was placed in a copper container 1 having a shape as shown in FIG. 3 (a). Then, the space between the container 1 and the molded body 4 is filled with petroleum pitch 5A crushed to an average particle size of about 3 mm.
The temperature was raised to 0 ° C., the petroleum pitch was melted, and the entire molded body 4 was covered with the impregnating material 5. The state at this time is shown in FIG. 3 (b).
Is like. Then titanium foil 8 as a hydrogen getter
After putting in, the lid 2 with the deaeration pipe 3 as shown in FIG. 3 (c)
Was fitted into the container 1 and the ends were joined by welding 6. A vacuum pump was connected to the deaeration pipe 3, and the deaeration pipe 3 was crushed and pressed while vacuuming. The excess deaeration pipe was cut, and the cutting opening was sealed by welding. Although not shown, this container 1 was placed in a hot isostatic press and impregnated and carbonized at the temperature and pressure pattern shown in FIG. After the treatment, the container was taken out from the hot isostatic press, the container was cut, and the molded body inside was collected. The open porosity was about 13%, which proved to be fully carbonized. Specific gravity is about 1.4g / cc to about 1.58g / c
It was confirmed that the density was increased to c and a sufficient density improving effect was obtained.
(発明の効果) 本発明は以上の通りであり、高圧ガス圧力を利用した含
浸炭化法による高密度炭素複合材の製造が簡便に、かつ
含浸工程で容器が破損する確率が低減されるので、通常
の熱間静水圧プレス装置を用いても、装置内部をほとん
ど汚染することなく処理が可能となり、特殊な装置を用
いることなく、1000〜2000kg f/cm2の高圧含浸炭化処理
でき、高密度炭素複合化の新しい製造法を与えるものと
して、その寄与は極めて大きい。(Effects of the Invention) The present invention is as described above, and since the production of the high-density carbon composite material by the impregnation carbonization method using high-pressure gas pressure is simple, and the probability that the container is damaged in the impregnation step is reduced, Even if a normal hot isostatic press is used, it can be processed with almost no contamination inside the device, and high pressure impregnation carbonization of 1000 to 2000 kg f / cm 2 can be performed without using a special device, resulting in high density. The contribution is extremely large as it gives a new manufacturing method of carbon composite.
第1図と第2図はいずれも本発明に用いる容器とその中
に収めた成形体を示す断面図であり、第3図(a)
(b)(c)は本発明実施例の工程一部を示す各断面図
であり、第4図はHIP処理を示すグラフであり、第5図
は炭素の収率と圧力との関係を示すグラフを示し、第6
図は従来例のカプセル(容器)を示し、第7図は従来例
のフローチャートである。 1……容器、2……蓋、4……成形体、5……含浸材。1 and 2 are sectional views showing a container used in the present invention and a molded body housed therein, and FIG. 3 (a).
(B) and (c) are cross-sectional views showing a part of the process of the embodiment of the present invention, FIG. 4 is a graph showing HIP treatment, and FIG. 5 shows the relationship between carbon yield and pressure. Shows the graph, 6th
FIG. 7 shows a conventional capsule (container), and FIG. 7 is a flowchart of the conventional example. 1 ... container, 2 ... lid, 4 ... molded body, 5 ... impregnated material.
Claims (4)
ッチや樹脂などの炭化性物質を含浸し、この含浸材を炭
化して高密度の炭素複合材料を製造する方法において、 気密性の金属材料からなる薄肉の容器中に、隙間をもた
せて炭素材料成形体を収め、大気圧下または減圧下にて
容器と炭素材料成形体の前記隙間を溶融したタール・ピ
ッチなどの含浸材で充填して成形体全体を覆うようにし
た後、気密性の金属材料からなる蓋を容器に気密に結合
し、この容器全体を熱間静水圧プレス装置内に装入し、
該装置内部の圧媒ガス置換操作を行った後、タール・ピ
ッチなどの含浸材が溶融して液状となる温度に昇温し、
圧媒ガスを加えて容器ごと圧縮することで含浸材を成形
体に含浸し、次いで昇温して高圧力下で含浸材の一部も
しくは全部を炭化することを特徴とする高密度炭素複合
材料の製造方法。1. A method for producing a high-density carbon composite material by impregnating a porous carbon material compact with a carbonizing substance such as tar / pitch or resin, and carbonizing the impregnating material to obtain a gas-tight metal. A carbon material compact is placed in a thin container made of material with a gap, and the gap between the container and the carbon material compact is filled with molten impregnating material such as tar and pitch under atmospheric pressure or reduced pressure. After covering the entire molded body by air-tightly, a lid made of an airtight metal material is airtightly coupled to the container, and the entire container is placed in a hot isostatic press.
After performing the pressure medium gas replacement operation inside the apparatus, the temperature is raised to a temperature at which the impregnating material such as tar and pitch is melted and becomes liquid.
A high-density carbon composite material characterized by impregnating a molded body with an impregnating material by adding a pressure medium gas and compressing the whole container, and then heating the temperature to carbonize a part or all of the impregnating material under high pressure. Manufacturing method.
アルミもしくはこれら金属系の合金であることを特徴と
する請求項(1)の高密度炭素複合材料の製造方法。2. The method for producing a high-density carbon composite material according to claim 1, wherein the metal material of the container and the lid is copper, steel, aluminum or an alloy of these metal systems.
とを特徴とする請求項(1)(2)記載の高密度炭素複
合材料の製造方法。3. The method for producing a high-density carbon composite material according to claim 1, wherein the container is formed in a bellows shape.
置することを特徴とする請求項(1)(2)(3)記載
の高密度炭素複合材料の製造方法。4. The method for producing a high-density carbon composite material according to claim 1, wherein a getter material that absorbs hydrogen is arranged in the container.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63115471A JPH0798682B2 (en) | 1988-05-11 | 1988-05-11 | Method for producing high-density carbon composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63115471A JPH0798682B2 (en) | 1988-05-11 | 1988-05-11 | Method for producing high-density carbon composite material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH01286963A JPH01286963A (en) | 1989-11-17 |
| JPH0798682B2 true JPH0798682B2 (en) | 1995-10-25 |
Family
ID=14663362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63115471A Expired - Lifetime JPH0798682B2 (en) | 1988-05-11 | 1988-05-11 | Method for producing high-density carbon composite material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0798682B2 (en) |
-
1988
- 1988-05-11 JP JP63115471A patent/JPH0798682B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH01286963A (en) | 1989-11-17 |
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