JPH03290367A - Production of carbon/silicon carbide composite material - Google Patents

Production of carbon/silicon carbide composite material

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Publication number
JPH03290367A
JPH03290367A JP2088641A JP8864190A JPH03290367A JP H03290367 A JPH03290367 A JP H03290367A JP 2088641 A JP2088641 A JP 2088641A JP 8864190 A JP8864190 A JP 8864190A JP H03290367 A JPH03290367 A JP H03290367A
Authority
JP
Japan
Prior art keywords
alloy
silicon carbide
silicon
eutectic
intermetallic compound
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.)
Pending
Application number
JP2088641A
Other languages
Japanese (ja)
Inventor
Tsutomu Iikawa
勤 飯川
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.)
Fujitsu Ltd
Original Assignee
Fujitsu 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 Fujitsu Ltd filed Critical Fujitsu Ltd
Priority to JP2088641A priority Critical patent/JPH03290367A/en
Publication of JPH03290367A publication Critical patent/JPH03290367A/en
Pending legal-status Critical Current

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  • Ceramic Products (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

PURPOSE:To obtain a composite ceramic structural material having high and stable strength and good lubricity by reacting a green compact composed of graphite powder with a eutectic alloy composed mainly of silicon. CONSTITUTION:A eutectic alloy 2 containing silicon accounting for the major part of the alloy is impregnated under pressure into a green compact 1 composed of graphite powder and made to react with each other to form a silicon carbide layer 3 at the interface between the green compact 1 and the alloy 2 and precipitate an intermetallic compound 2 composed mainly of silicon. The eutectic alloy 2 is e.g. Si-Mo alloy, Si-Nb alloy and Si-Ta alloy and the content of Si is preferably >=80wt.%. The eutectic composition is used in order to lower the melting point and form the intermetallic compound.

Description

【発明の詳細な説明】 〔概要〕 黒鉛−炭化硅素系複合材料の製造方法に関し、機械的強
度が高く、潤滑性を有する成型体を製造することを目的
とし、 黒鉛粉末からなる圧粉成型体に硅素が組成比の大部分を
占める共晶合金を加圧溶浸して反応せしめ、前記圧粉成
型体との界面に炭化硅素層を形成すると共に、硅素を主
成分とする金属間化合物を析出させることを特徴として
黒鉛−炭化硅素系複合材料の製造方法を構成する。
[Detailed Description of the Invention] [Summary] The purpose of the present invention is to produce a molded body having high mechanical strength and lubricity with respect to a method for producing a graphite-silicon carbide-based composite material. A eutectic alloy in which silicon accounts for most of the composition ratio is infiltrated under pressure and reacted to form a silicon carbide layer at the interface with the powder compact, and an intermetallic compound mainly composed of silicon is precipitated. A method for producing a graphite-silicon carbide composite material is characterized in that:

〔産業上の利用分野〕[Industrial application field]

本発明は黒鉛−炭化硅素系複合材料の製造方法に関する
The present invention relates to a method for producing a graphite-silicon carbide composite material.

機械装置において回転軸を支える軸受なとの材料には金
属やセラミックスが使用されており、金属の場合は減摩
合金あるいは耐摩合金とも言われ、摩擦係数が小なく、
摩減量が少なく、潤滑油などに対する耐蝕性が優れた材
料が使用されている。
Metals and ceramics are used as materials for bearings that support rotating shafts in mechanical devices. Metals are also called anti-friction alloys or anti-friction alloys, and have a low coefficient of friction.
Materials used are low in wear and have excellent corrosion resistance against lubricating oil and the like.

そして、青銅系や鉄系の焼結体が用いられ、潤滑油を含
浸して使用されている。
Bronze-based or iron-based sintered bodies are used and impregnated with lubricating oil.

また、グラファイトなどを含ませて構威し、自己潤滑性
をもたせた無給油軸受もある。
There are also oil-free bearings that contain graphite or the like to provide self-lubricating properties.

本発明はこのように機械的強度が高く、且つ潤滑性が必
要な用途に使用するセラミックス構造体に関するもので
ある。
The present invention relates to a ceramic structure that is used in applications that require high mechanical strength and lubricity.

〔従来の技術〕[Conventional technology]

軸受など機械的強度が高く、且つ潤滑性が必要な用途に
は上記の合金以外に複合セラミックスが使用されている
In addition to the above-mentioned alloys, composite ceramics are used in applications such as bearings that require high mechanical strength and lubricity.

例えば、アルミナ(Aj!203)や炭化硅素(SiC
)などのセラミックスよりなるマトリックスの内部にチ
タン(Ti)やアルミニウム(^Il)のような金属粒
子を強化物質として分散した材料が知られている。
For example, alumina (Aj!203) and silicon carbide (SiC)
) Materials are known in which metal particles such as titanium (Ti) or aluminum (^Il) are dispersed as reinforcing substances inside a matrix made of ceramics such as ceramics.

そして、強化用の金属粒子を分散させたセラ旦ツク材料
粉末を成型し焼結を行うことにより複合セラミックスが
作られている。
Composite ceramics are produced by molding and sintering ceramic material powder in which reinforcing metal particles are dispersed.

然し、焼結体であるために孔(ポア)が多く存在し、こ
れが原因で強度の変動が大きく、実用に供するには高い
安全係数の確保が必要である。
However, since it is a sintered body, there are many pores, which causes large fluctuations in strength, and it is necessary to ensure a high safety factor for practical use.

また、セラミックスの焼結温度は1500℃以上の高温
となることから強化用金属粒子の酸化が起こり易く、こ
れも強度の変動が大きい原因となっている。
Furthermore, since the sintering temperature of ceramics is as high as 1500° C. or higher, oxidation of reinforcing metal particles is likely to occur, which is also a cause of large fluctuations in strength.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

以上のように、従来よりセラミックス複合材料が知られ
ているが、強度の変動が大きいなどの理由から余り使用
されていない。
As described above, ceramic composite materials have been known for some time, but they are not used much because of large fluctuations in strength.

そこで、強度が高くて変動が少なく、更に潤滑性を備え
た新規の複合セラくソクス構造材料を提供することが課
題である。
Therefore, it is an issue to provide a new composite ceramic structure material that has high strength, little fluctuation, and has lubricity.

〔課題を解決するための手段〕[Means to solve the problem]

上記の課題は黒鉛(以下略してC)粉末からなる圧粉成
型体に硅素(以下Si)が組成比の大部分を占める共晶
合金を加圧溶浸して反応せしめ、圧粉成型体との接合面
に炭化硅素(以下5iC)層を形成すると共に、硅素を
主成分とする金属間化合物を析出させることを特徴とし
てC−5i系複合材料の製造方法を構成することにより
解決することができる。
The above problem was solved by pressure infiltrating a eutectic alloy, in which silicon (hereinafter referred to as Si) accounts for the majority of the composition, into a powder compact made of graphite (hereinafter abbreviated as C) powder and reacting it with the powder compact. This problem can be solved by configuring a method for producing a C-5i composite material characterized by forming a silicon carbide (hereinafter referred to as 5iC) layer on the joint surface and precipitating an intermetallic compound whose main component is silicon. .

〔作用〕[Effect]

本発明は圧粉成型したCと溶融したSi合金とを反応さ
せることによりCよりなり多孔質である圧粉成型体の表
面に強度の高いSiC皮膜を形成すると共に、その隙間
をSiを主成分とする金属間化合物で充填する方法をと
ることにより機械的強度が高く、且つ潤滑性をもつ複合
セラミックスを実現するものである。
The present invention forms a strong SiC film on the surface of a porous powder compact made of C by reacting compacted C with a molten Si alloy. By using a method of filling with intermetallic compounds, composite ceramics with high mechanical strength and lubricity can be realized.

第1図はこの原理図であって、圧粉成型したC1には各
粒子間に隙間があるが、この隙間に高温でSiの組成比
が大部分(80重量%以上)を占める共晶合金2の溶融
体を浸透させることにより、C1と共晶合金2を構成す
るSiとを反応させて炭化硅素(SiC)層3を形成し
つ覧、未反応のSiによって金属間化合物を析出させる
ものである。
Figure 1 is a diagram of this principle, and shows that C1 that has been compacted has gaps between each particle, and these gaps are filled with eutectic alloy in which the composition ratio of Si is mostly (80% by weight or more) at high temperatures. By infiltrating the melt of No. 2, C1 reacts with the Si constituting the eutectic alloy 2 to form a silicon carbide (SiC) layer 3, and the unreacted Si precipitates an intermetallic compound. It is.

こ覧で、本発明に通用可能の共晶合金としてはSi−M
o(モリブデン)合金、5i−Nb(ニオブ)合金。
From this table, Si-M is a eutectic alloy that can be used in the present invention.
o (molybdenum) alloy, 5i-Nb (niobium) alloy.

5i−Ta(タンタル)合金などがある。Examples include 5i-Ta (tantalum) alloy.

参考として第2図に5t−1’lo合金の状態図を、ま
た第3図に5i−Nb合金の状態図を示した。
For reference, FIG. 2 shows a phase diagram of the 5t-1'lo alloy, and FIG. 3 shows a phase diagram of the 5i-Nb alloy.

こ−で共晶組成を用いる理由は融点が低下すると共に、
金属間化合物を形成させるためであり、これにより作業
性が改善できること\、Siの酸化を少なくする点に特
徴がある。
The reason for using the eutectic composition is that the melting point decreases and
This is to form an intermetallic compound, which is characterized by improving workability and reducing oxidation of Si.

次に、使用する共晶合金のSi含有料が80重量%以上
とする理由は、実験の結果、これ以下の含有量の場合は
Cとの反応が不充分でSiCの形成量が不足し、強度が
低下するためである。
Next, the reason why the Si content of the eutectic alloy used is 80% by weight or more is that as a result of experiments, if the content is less than this, the reaction with C is insufficient and the amount of SiC formed is insufficient. This is because the strength decreases.

本発明は第2図においては5ieJo++組成(融点1
410″C)の共晶合金を、また第3図においては51
aeNb+z(融点1300℃)の共晶合金を使用する
The present invention has a 5ieJo++ composition (melting point 1
410″C) and 51″C) in Figure 3.
A eutectic alloy of aeNb+z (melting point 1300°C) is used.

このような共晶合金をCよりなる圧粉成型体の中に溶浸
させて表面層をSiCに変えると、共晶合金の組成はs
in戒比の少ない方にずれ、X5iz(XはMo或いは
Nb)の金属間化合物が生威し、この金属間化合物が強
度の向上に寄与する。
When such a eutectic alloy is infiltrated into a powder compact made of C to change the surface layer to SiC, the composition of the eutectic alloy becomes s
As the in-force ratio shifts to the smaller side, an intermetallic compound of X5iz (X is Mo or Nb) flourishes, and this intermetallic compound contributes to improving the strength.

なお、成型体の中に溶浸させるためには加圧雰囲気を使
用する必要がある。
Note that it is necessary to use a pressurized atmosphere to infiltrate into the molded body.

本発明は硬度の低いCの表面に硬度の高いSiCを被覆
すると共に、粒子間の隙間を硬度の高い金属間化合物2
で充填するもので、この材料を用いて例えば軸受を構成
する場合、摩耗によって部分的に中のCが現れることか
ら、強度が高く、かつ潤滑性のよい複合セラミックスを
実現するものである。
The present invention coats the surface of C with low hardness with SiC with high hardness, and fills the gaps between particles with an intermetallic compound 2 with high hardness.
When this material is used to construct, for example, a bearing, the C inside will partially appear due to wear, resulting in a composite ceramic with high strength and good lubricity.

〔実施例〕〔Example〕

Cとしては平均粒径が10μmの鱗片状のものを用い、
この粉末を成型圧力3融/cm”の条件で5X 10 
X 50mの板状にプレス底形した。
As C, a scale-like material with an average particle size of 10 μm was used.
This powder was 5
The bottom of the press was formed into a plate shape of 50 m x 50 m.

この密度は78%であった。This density was 78%.

次に、重量U威がSiavMo+sとなるようにSiと
M。
Next, Si and M so that the weight U becomes SiavMo+s.

を混合した後、アルミナ坩堝に入れ、高周波溶解炉を用
い、窒素(N、)気流中で共晶温度である1300℃よ
りも20℃高い1320℃に加熱して溶解し、均一な合
金とした。
After mixing, the mixture was placed in an alumina crucible and heated to 1320°C, which is 20°C higher than the eutectic temperature of 1300°C, in a nitrogen (N) stream using a high-frequency melting furnace to form a uniform alloy. .

この溶解した合金を鋳型に鋳造し、CtF、型体と同一
寸法に切り出した。
This molten alloy was cast into a mold, and the CtF mold was cut into the same dimensions as the mold body.

この合金をC成型体の上に置き、圧力100気圧のN2
雰囲気中で1300℃で10分間加熱することにより内
部へ溶浸させると共にCと反応させてSiCを形成した
This alloy was placed on top of the C molded body, and N2 was placed at a pressure of 100 atm.
By heating at 1300° C. for 10 minutes in an atmosphere, it was infiltrated into the interior and reacted with C to form SiC.

得られた試料の断面観察を行った結果、気孔率は0%で
あり、成型体の気孔部には総て溶融合金が含浸されてお
り、Cの表面にはSiCが一様に形成され、気孔部に残
存した溶融合金はMo5izとして析出していた。
As a result of cross-sectional observation of the obtained sample, the porosity was 0%, all the pores of the molded body were impregnated with molten alloy, and SiC was uniformly formed on the surface of C. The molten alloy remaining in the pores was precipitated as Mo5iz.

次に、この試料について曲げ強度を測定したところ、約
80 Kg/m”の値を示し、値の変動は僅かであった
Next, when the bending strength of this sample was measured, it showed a value of about 80 Kg/m'', and the variation in the value was slight.

また、摩耗試験を行った結果、SiC単体と比較して摩
耗量は約1/8に減少していた。
Further, as a result of a wear test, the amount of wear was reduced to about 1/8 compared to SiC alone.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、強度が高く、その変動が少なく、また
潤滑性に富んだ複合セラG 7クスを作ることができ、
構造用部品への適用が可能である。
According to the present invention, it is possible to make a composite Cera G7 that has high strength, little variation in strength, and rich lubricity.
It can be applied to structural parts.

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

第1図は本発明に係る複合セラミ・ノクス材料の原理図
、 第2図はSt−Mo合金の状態図、 第3図は5i−Nb合金の状態図、 である。 図において、 1はC(グラファイト)、 2は共晶合金(金属間化合物)、 3はSiC層、 である。 ベニ=シ1 重 量 (’/、)S M。 昂千量(X) Si S;−Mo合金の状態図 兜2図 1 415−
Fig. 1 is a principle diagram of the composite ceramic-nox material according to the present invention, Fig. 2 is a phase diagram of the St-Mo alloy, and Fig. 3 is a phase diagram of the 5i-Nb alloy. In the figure, 1 is C (graphite), 2 is a eutectic alloy (intermetallic compound), and 3 is a SiC layer. Beni-shi1 Weight ('/,) S M. Phase diagram of Mo alloy (X) Si S;

Claims (1)

【特許請求の範囲】[Claims]  黒鉛粉末からなる圧粉成型体に硅素が組成比の大部分
を占める共晶合金を加圧溶浸して反応せしめ、前記圧粉
成型体との界面に炭化硅素層を形成すると共に、硅素を
主成分とする金属間化合物を析出させることを特徴とす
る黒鉛−炭化硅素系複合材料の製造方法。
A compact made of graphite powder is infiltrated with a eutectic alloy in which silicon accounts for most of the composition ratio under pressure to cause a reaction, forming a silicon carbide layer at the interface with the compact, and at the same time forming a silicon carbide layer mainly containing silicon. A method for producing a graphite-silicon carbide composite material, which comprises precipitating an intermetallic compound as a component.
JP2088641A 1990-04-03 1990-04-03 Production of carbon/silicon carbide composite material Pending JPH03290367A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2088641A JPH03290367A (en) 1990-04-03 1990-04-03 Production of carbon/silicon carbide composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2088641A JPH03290367A (en) 1990-04-03 1990-04-03 Production of carbon/silicon carbide composite material

Publications (1)

Publication Number Publication Date
JPH03290367A true JPH03290367A (en) 1991-12-20

Family

ID=13948448

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2088641A Pending JPH03290367A (en) 1990-04-03 1990-04-03 Production of carbon/silicon carbide composite material

Country Status (1)

Country Link
JP (1) JPH03290367A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2413794A (en) * 2004-05-03 2005-11-09 Snecma Propulsion Solide A method of manufacturing an impervious thermostructural composite material
US10040724B2 (en) * 2015-12-11 2018-08-07 University Of The Witwatersrand, Johannesburg Ceramic composite and method to prepare the composite

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2413794A (en) * 2004-05-03 2005-11-09 Snecma Propulsion Solide A method of manufacturing an impervious thermostructural composite material
GB2413794B (en) * 2004-05-03 2009-07-01 Snecma Propulsion Solide A method of manufacturing a part out of impervious thermostructural composite material
US7736554B2 (en) 2004-05-03 2010-06-15 Snecma Propulsion Solide Method of manufacturing a part out of impervious thermostructural composite material
US10040724B2 (en) * 2015-12-11 2018-08-07 University Of The Witwatersrand, Johannesburg Ceramic composite and method to prepare the composite

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