JP2000034174A - Manufacturing method of ceramic composite material - Google Patents
Manufacturing method of ceramic composite materialInfo
- Publication number
- JP2000034174A JP2000034174A JP10202485A JP20248598A JP2000034174A JP 2000034174 A JP2000034174 A JP 2000034174A JP 10202485 A JP10202485 A JP 10202485A JP 20248598 A JP20248598 A JP 20248598A JP 2000034174 A JP2000034174 A JP 2000034174A
- Authority
- JP
- Japan
- Prior art keywords
- particles
- sintering
- ceramic
- composite material
- ceramic composite
- 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
Links
- 239000000919 ceramic Substances 0.000 title claims abstract description 55
- 239000002131 composite material Substances 0.000 title claims abstract description 34
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 11
- 239000002245 particle Substances 0.000 claims abstract description 118
- 238000005245 sintering Methods 0.000 claims abstract description 98
- 239000011159 matrix material Substances 0.000 claims abstract description 26
- 238000000034 method Methods 0.000 claims description 22
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims description 12
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 8
- 239000001301 oxygen Substances 0.000 claims description 8
- 229910052760 oxygen Inorganic materials 0.000 claims description 8
- 239000011225 non-oxide ceramic Substances 0.000 claims description 4
- 229910052575 non-oxide ceramic Inorganic materials 0.000 claims description 4
- -1 Mg O Inorganic materials 0.000 claims 1
- 239000012298 atmosphere Substances 0.000 abstract description 5
- 239000006185 dispersion Substances 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052718 tin Inorganic materials 0.000 abstract description 2
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 abstract 1
- 229910052581 Si3N4 Inorganic materials 0.000 abstract 1
- 229910033181 TiB2 Inorganic materials 0.000 abstract 1
- 229910034327 TiC Inorganic materials 0.000 abstract 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 abstract 1
- 229910052593 corundum Inorganic materials 0.000 abstract 1
- 229910003465 moissanite Inorganic materials 0.000 abstract 1
- 229910010271 silicon carbide Inorganic materials 0.000 abstract 1
- 229910001845 yogo sapphire Inorganic materials 0.000 abstract 1
- 239000011148 porous material Substances 0.000 description 16
- 238000005452 bending Methods 0.000 description 12
- 239000007791 liquid phase Substances 0.000 description 7
- 238000000280 densification Methods 0.000 description 6
- 238000013001 point bending Methods 0.000 description 6
- 238000007731 hot pressing Methods 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 230000002159 abnormal effect Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 239000012299 nitrogen atmosphere Substances 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000012071 phase Substances 0.000 description 2
- 102100036738 Guanine nucleotide-binding protein subunit alpha-11 Human genes 0.000 description 1
- 101100283445 Homo sapiens GNA11 gene Proteins 0.000 description 1
- 229910004298 SiO 2 Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
Landscapes
- Compositions Of Oxide Ceramics (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、優れた機械的特性
を示すセラミックス複合材料の製造方法、特に複雑形状
のセラミックス複合材料の製造に好適な方法に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing a ceramic composite material having excellent mechanical properties, and more particularly to a method suitable for producing a ceramic composite material having a complicated shape.
【0002】[0002]
【従来の技術】従来から、セラミックスは集積回路の基
板やパッケージ、切削工具用チップ、耐摩耗材料等に幅
広く使用されている。しかし、セラミックスは金属材料
と比べてコストが高い、信頼性に劣る、製造プロセスが
複雑である等の理由から、エンジン部品等の構造材料へ
の適用は困難であった。2. Description of the Related Art Conventionally, ceramics have been widely used for substrates and packages of integrated circuits, chips for cutting tools, wear-resistant materials, and the like. However, ceramics have been difficult to apply to structural materials such as engine parts because of their higher cost, lower reliability, and more complicated manufacturing process than metal materials.
【0003】このようなセラミックスの問題点を解決す
るために、異なる第2相を分散させる複合化によって、
その機械的特性を改善し、信頼性を向上させる試みがな
されてきた。例えば、特許第2507479号公報に
は、マトリックスのAl2O3粒子にSiC粒子及びSi
Cウイスカーを分散させた、強度及び靭性に優れた複合
焼結体が開示されている。[0003] In order to solve such problems of ceramics, a composite in which different second phases are dispersed is used.
Attempts have been made to improve its mechanical properties and improve its reliability. For example, Japanese Patent No. 2507479 discloses that AlC particles and SiC particles are used as matrix Al 2 O 3 particles.
A composite sintered body having excellent strength and toughness in which C whiskers are dispersed is disclosed.
【0004】また、特開昭59−3766号公報、特開
昭61−21964号公報、特開昭61−174165
号公報等には、マトリックスであるAl2O3粒子にSi
C粒子を分散させることによって、Al2O3焼結体の強
度及び靭性を向上させることが記載されている。Further, JP-A-59-3766, JP-A-61-21964, and JP-A-61-174165.
Japanese Patent Application Laid-Open Publication No. H10-15064 discloses that Al 2 O 3 particles serving as a matrix have Si
It is described that the strength and toughness of an Al 2 O 3 sintered body are improved by dispersing C particles.
【0005】[0005]
【発明が解決しようとする課題】上記したような複合材
料は、一般的に緻密化が困難であるため、その製造方法
としては機械的加圧を行うホットプレス焼結か、或いは
ホットプレス焼結に続いて雰囲気加圧焼結する方法に限
定される。そのため、平板のような単純形状の製品の製
造に限られ、複雑形状の製品への適用が困難であった。Since the above-mentioned composite materials are generally difficult to densify, they can be produced by hot press sintering under mechanical pressure or hot press sintering. Subsequently, the method is limited to a method of sintering under an atmospheric pressure. Therefore, it is limited to the manufacture of a product having a simple shape such as a flat plate, and it is difficult to apply the method to a product having a complicated shape.
【0006】また、ミクロンサイズの粒子を含むセラミ
ックス複合材料では、常圧焼結に続いて雰囲気加圧焼結
を行う2段階焼結の場合、二次焼結で緻密な焼結体を得
るためには、一次焼結体の相対密度を95%以上とする
必要があった。しかし、一次焼結の常圧焼結において9
5%以上の相対密度を達成するには、焼結温度を高くす
る必要があるため、粒成長が促進されて粒径が大きくな
り、最終的な複合材料の曲げ強度が低下するという問題
点があった。In the case of a two-stage sintering in which a ceramic composite material containing micron-sized particles is subjected to atmospheric pressure sintering followed by atmospheric pressure sintering, a dense sintered body is obtained by secondary sintering. Requires that the relative density of the primary sintered body be 95% or more. However, in normal pressure sintering of primary sintering, 9
In order to achieve a relative density of 5% or more, it is necessary to increase the sintering temperature, so that the grain growth is promoted, the grain size increases, and the bending strength of the final composite material decreases. there were.
【0007】本発明は、このような従来の事情に鑑み、
複雑形状を持つ製品への適用が可能であって、エンジン
部品等の構造材料として実用可能な高い強度を有するセ
ラミックス複合材料の製造方法を提供することを目的と
する。The present invention has been made in view of such a conventional situation,
An object of the present invention is to provide a method for producing a ceramic composite material having a high strength, which can be applied to a product having a complicated shape and can be practically used as a structural material for an engine part or the like.
【0008】[0008]
【課題を解決するための手段】上記目的を達成するた
め、本発明が提供するセラミックス複合材料の製造方法
は、マトリックスとなるセラミックス粒子に、表面酸化
物層を有する最大粒径1μm以下且つ平均粒径0.5μ
m以下の非酸化物系セラミックスの分散粒子を添加混合
し、常圧焼結により相対密度90%以上95%未満とし
た後、雰囲気加圧焼結により相対密度99%以上に緻密
化して、前記分散粒子の一部がマトリックス粒子内に分
散したセラミックス複合材料を得ることを特徴とする。Means for Solving the Problems In order to achieve the above object, the present invention provides a method for producing a ceramic composite material, wherein a ceramic particle serving as a matrix has a surface oxide layer having a maximum particle size of 1 μm or less and an average particle size. 0.5μ diameter
m and less than 90% and less than 95% relative density by atmospheric pressure sintering, and then densified to a relative density of 99% or more by atmospheric pressure sintering. It is characterized in that a ceramic composite material in which a part of dispersed particles is dispersed in matrix particles is obtained.
【0009】上記本発明においては、非酸化物系セラミ
ックスからなる分散粒子の添加量が0.5〜10体積%
の範囲内であることが好ましい。また、この分散粒子は
表面酸化物層による酸素量が0.15重量%以上である
ことが好ましい。かかる分散粒子の好ましい例として
は、Si3N4、SiC、TiN、TiC、TiB2から
選ばれた少なくとも1種がある。In the present invention, the amount of the dispersed particles made of non-oxide ceramics is 0.5 to 10% by volume.
Is preferably within the range. The dispersed particles preferably have an oxygen content of 0.15% by weight or more due to the surface oxide layer. Preferred examples of such dispersed particles include at least one selected from Si 3 N 4 , SiC, TiN, TiC, and TiB 2 .
【0010】[0010]
【発明の実施の形態】本発明においては、マトリックス
となるセラミックス粒子に、最大粒径が1μm以下であ
って平均粒径が0.5μm以下の微細な非酸化物系セラ
ミックスからなる分散粒子(以下単に分散粒子とも言
う)を添加混合する。かかる微細な分散粒子の添加混合
によって、常圧焼結での閉気孔化が促進され、開気孔を
飛躍的に低減させた一次焼結体を簡単に得ることがで
き、しかもこの開気孔の少ない一次焼結体は二次焼結の
雰囲気加圧焼結によって緻密化することができる。BEST MODE FOR CARRYING OUT THE INVENTION In the present invention, dispersed ceramic particles (hereinafter, referred to as fine particles) composed of fine non-oxide ceramics having a maximum particle size of 1 μm or less and an average particle size of 0.5 μm or less are used as matrix particles. (Also simply referred to as dispersed particles). By the addition and mixing of such fine dispersed particles, closed porosity in normal pressure sintering is promoted, and it is possible to easily obtain a primary sintered body in which the open pores are drastically reduced, and furthermore, there are few open pores. The primary sintered body can be densified by atmospheric pressure sintering of secondary sintering.
【0011】本発明方法における一次焼結過程を、図1
を参照して説明する。即ち、本発明方法では、焼結助剤
を添加しなくても、分散粒子1の表面酸化物層とマトリ
ックスとなるセラミックス粒子2の表面との反応により
液相3が形成され、且つその際に微細な分散粒子1がセ
ラミックス粒子2の間に存在するため、気孔近傍や3重
点及び粒界に存在する液相3の閉気孔化が促進される。
従って、閉気孔4は形成されるものの、開気孔が形成さ
れる割合は小さくなり、相対密度90%以上95%未満
まで常圧焼結したとき、開気孔率が10体積%以下の一
次焼結体が得られる。The primary sintering process in the method of the present invention is shown in FIG.
This will be described with reference to FIG. That is, in the method of the present invention, the liquid phase 3 is formed by the reaction between the surface oxide layer of the dispersed particles 1 and the surface of the ceramic particles 2 serving as a matrix without adding a sintering aid. Since the fine dispersed particles 1 exist between the ceramic particles 2, the closed phase of the liquid phase 3 existing near the pores, at the triple point and at the grain boundary is promoted.
Therefore, although the closed pores 4 are formed, the proportion of the open pores formed is small, and when normal pressure sintering is performed to a relative density of 90% or more and less than 95%, the primary sintering is performed with an open porosity of 10% by volume or less. The body is obtained.
【0012】一方、分散粒子を添加しない場合には、図
2に示すように、常圧焼結によりマトリックスとなるセ
ラミックス粒子2が互いに接触した地点で互いの反応
(物質移動)が生じ、若干の液相3が形成されることも
あるが、液相3がセラミックス粒子2の間の空隙を充分
に埋めることができないため、開気孔5の多い一次焼結
体となる。On the other hand, when the dispersed particles are not added, mutual reaction (mass transfer) occurs at a point where the ceramic particles 2 serving as a matrix come into contact with each other by normal pressure sintering, as shown in FIG. Although the liquid phase 3 may be formed, the liquid phase 3 cannot sufficiently fill the gaps between the ceramic particles 2, so that a primary sintered body having many open pores 5 is obtained.
【0013】このような場合に開気孔5を潰して緻密化
するためには、常圧焼結において更に昇温するか又は焼
結時間を延長する方法、若しくは後の二次焼結において
ホットプレス法のような型内で機械的に加圧する方法の
いずれかを採用する必要があり、二次焼結で雰囲気加圧
焼成を行っても緻密な焼結体は得られない。尚、通常の
焼結のように、焼結助剤を添加して液相量を増やすこと
によっても開気孔を低減することができるが、その場合
には異常な粒成長が生じ易くなる。In such a case, in order to crush the open pores 5 and make them denser, a method of further raising the temperature in normal pressure sintering or extending the sintering time, or hot pressing in subsequent secondary sintering is used. It is necessary to employ any of the methods of mechanically pressing in a mold such as the method, and a dense sintered body cannot be obtained even if the atmosphere is pressed and sintered in the secondary sintering. As in the case of ordinary sintering, open pores can be reduced by adding a sintering aid to increase the amount of liquid phase, but in this case, abnormal grain growth is likely to occur.
【0014】このように、本発明方法によれば、焼結助
剤を添加せず又は焼結助剤の添加量が少なくても、一次
焼結の常圧焼結によって、後の雰囲気加圧焼結での緻密
化を阻害する要因となる開気孔の割合を小さくすること
ができ、セラミックス粒子又はマトリックス粒子(焼結
後のセラミックス粒子)の異常な粒成長が無く、相対密
度が90%以上95%未満の一次焼結体を得ることがで
きる。この一次焼結体は開気孔率が10体積%以下と小
さいため、相対密度が95%未満であっても、二次焼結
で雰囲気加圧焼結を行うことにより相対密度99%以上
に緻密化できる。また、二次焼結では雰囲気加圧焼結に
より緻密化でき、型内での機械的な加圧を加える必要が
ないので、複雑な形状の製品にも適用が可能である。As described above, according to the method of the present invention, even if the sintering aid is not added or the addition amount of the sintering aid is small, the atmospheric pressure sintering of the primary sintering allows the subsequent atmospheric pressure sintering. The ratio of open pores, which is a factor that hinders densification in sintering, can be reduced, and there is no abnormal grain growth of ceramic particles or matrix particles (ceramic particles after sintering), and the relative density is 90% or more. A primary sintered body of less than 95% can be obtained. Since the primary sintered body has a small open porosity of 10% by volume or less, even if the relative density is less than 95%, the relative density is increased to 99% or more by performing atmospheric pressure sintering in the secondary sintering. Can be In the secondary sintering, densification can be performed by atmospheric pressure sintering, and there is no need to apply mechanical pressure in a mold. Therefore, the present invention can be applied to products having complicated shapes.
【0015】一次焼結体の相対密度が90%未満では、
開気孔率が増えるため、雰囲気加圧焼結の二次焼結によ
る緻密化が難しくなる。また、相対密度が95%以上で
あっても雰囲気加圧焼結は可能であるが、95%以上の
密度に到達させるためには常圧焼結の温度を高めねばな
らないため、結果的にマトリックス粒子の異常な粒成長
のために、得られる焼結体の曲げ強度が低下する。ま
た、二次焼結の際の雰囲気圧力としては、10MPa以
上が好ましいが、経済的にも実用可能な圧力域である2
00MPa以下で焼結することが望ましい。When the relative density of the primary sintered body is less than 90%,
Since the open porosity increases, densification by secondary sintering in atmospheric pressure sintering becomes difficult. Atmospheric pressure sintering is possible even if the relative density is 95% or more. However, in order to reach a density of 95% or more, the temperature of normal pressure sintering must be increased. Due to the abnormal grain growth of the grains, the bending strength of the obtained sintered body decreases. The atmosphere pressure during the secondary sintering is preferably 10 MPa or more, but is a pressure range that is economically practical.
Desirably, sintering is performed at a pressure of 00 MPa or less.
【0016】また、本発明方法によれば 常圧焼結の一
次焼結過程や雰囲気加圧焼結の二次焼結過程において、
セラミックス粒子又はマトリックス粒子は一部の分散粒
子を粒内に取り込み、若干粒成長をする。その結果、焼
結完了後の二次焼結体(セラミックス複合材料)には、
一部の分散粒子がマトリックス粒子の粒内に存在し、マ
トリックス粒子を強化する働きをする。このように、最
大粒径が1μm以下で平均粒径が0.5μm以下の分散
粒子を分散させることにより、前述のごとく分散粒子が
焼結性及び開気孔率の低減に寄与すると共に、分散粒子
が殆ど粒成長せずにマトリックス粒子内に分散してマト
リックス自体を強化し、曲げ強度の向上を達成すること
ができるのである。Further, according to the method of the present invention, in the primary sintering step of normal pressure sintering and the secondary sintering step of atmospheric pressure sintering,
The ceramic particles or matrix particles take some of the dispersed particles into the grains and grow slightly. As a result, the secondary sintered body (ceramic composite material) after sintering is completed
Some dispersed particles are present within the grains of the matrix particles and serve to strengthen the matrix particles. Thus, by dispersing the dispersed particles having a maximum particle size of 1 μm or less and an average particle size of 0.5 μm or less, the dispersed particles contribute to the reduction of the sinterability and the open porosity as described above. Can be dispersed in the matrix particles with almost no grain growth, strengthening the matrix itself, and achieving an improvement in bending strength.
【0017】本発明における分散粒子の添加量又は分散
量は、0.5〜10体積%の範囲が好ましく、1〜10
体積%が更に好ましい。この添加量又は分散量が0.5
体積%未満では、セラミックス複合材料の粒径が不均一
になるため、常温での曲げ強度が低下し易くなるほか、
ピン止め効果が小さくなるため、高温での曲げ強度も低
下する。逆に添加量又は分散量が10体積%を越える
と、焼結性が低下して緻密化が阻害されるので、高い曲
げ強度が得られない。In the present invention, the added or dispersed amount of the dispersed particles is preferably in the range of 0.5 to 10% by volume, and 1 to 10% by volume.
% By volume is more preferred. The amount of addition or dispersion is 0.5
If the content is less than the volume%, the particle size of the ceramic composite material becomes non-uniform, so that the bending strength at room temperature tends to decrease,
Since the pinning effect is reduced, the bending strength at high temperatures is also reduced. Conversely, if the amount of addition or dispersion exceeds 10% by volume, sinterability is reduced and densification is inhibited, so that high bending strength cannot be obtained.
【0018】本発明方法は、Al2O3、MgO、Si3
N4、SiC、AlN等の代表的なセラミックス粒子に
適用が可能であり、それぞれ適切な非酸化物系セラミッ
クスからなる分散粒子を選択することによって、強度等
の機械的特性を向上させたセラミックス複合材料を提供
することができる。また、好ましい分散粒子としては、
マトリックス中で粒成長しないSi3N4、SiC、Ti
N、TiC、TiB2等が挙げられる。According to the method of the present invention, Al 2 O 3 , MgO, Si 3
It is applicable to typical ceramic particles such as N 4 , SiC, AlN, etc. Ceramic composites with improved mechanical properties such as strength by selecting appropriate dispersed particles composed of non-oxide ceramics Material can be provided. Further, as preferred dispersed particles,
Si 3 N 4 , SiC, Ti that does not grow in the matrix
N, TiC, TiB 2 and the like.
【0019】これら分散粒子の表面には通常表面酸化物
層が存在し、この表面酸化物層が前述のごとくマトリッ
クスとなるセラミックス粒子と反応して液相を形成し
て、閉気孔化を促進する。従って、分散粒子の表面酸化
物層の酸素量は、0.15重量%以上であることが望ま
しい。この酸素量より低い場合には、開気孔の低減効果
が少なくなるので、相対密度90%以上95%未満に一
次焼結するため高温又は長時間を要することとなり、マ
トリックス粒子が粒成長して強度特性が低下するからで
ある。A surface oxide layer usually exists on the surface of these dispersed particles, and the surface oxide layer reacts with the ceramic particles serving as a matrix as described above to form a liquid phase, thereby promoting closed pores. . Therefore, the oxygen content of the surface oxide layer of the dispersed particles is desirably 0.15% by weight or more. When the oxygen content is lower than this, the effect of reducing the open pores is reduced, so that the primary sintering to a relative density of 90% or more and less than 95% requires a high temperature or a long time. This is because the characteristics deteriorate.
【0020】また、本発明方法は基本的には焼結助剤が
不要であるが、焼結助剤を加えると効果がより顕著にな
り、通常は焼結助剤が不要であるマトリックスに対して
も同様である。これらの焼結助剤は焼結温度で液相化を
助長し、その際粒界にある分散粒子周辺に毛細管現象に
より集結する。その結果、開気孔の閉気孔化が一層促進
され、開気孔の割合が更に減少するため、低密度の一次
焼結体でも雰囲気加圧焼結による二次焼結が可能であ
る。Although the method of the present invention basically does not require a sintering aid, the effect becomes more remarkable when a sintering aid is added. It is the same as above. These sintering aids promote liquefaction at the sintering temperature, in which case the sintering agents gather around the dispersed particles at the grain boundaries by capillary action. As a result, the closed pores of the open pores are further promoted and the ratio of the open pores is further reduced, so that the secondary sintering by the atmospheric pressure sintering is possible even with a low-density primary sintered body.
【0021】このような焼結助剤としては、セラミック
ス粒子が通常用いられるAl2O3の場合は、MgO等を
0.5重量%以下を加えることが有効である。また、セ
ラミックス粒子がSi3N4系(サイアロンを含む)の場
合にはAl2O3、Y2O3、MgO等を10体積%程度、
セラミックス粒子がSiCの場合にはY2O3、Yb2O3
等を5体積%程度、セラミックス粒子がAlN粒子の場
合にはY2O3、Yb2O3等を2体積%程度、及びセラミ
ックス粒子がMgO粒子の場合にはSiO2等を0.5体
積%程度加えることが有効である。尚、これ以上の焼結
助剤を添加することも可能であるが、粒成長が起こりや
すくなり、焼結体の高温強度が低下するので好ましくな
い。As such a sintering aid, in the case of Al 2 O 3 in which ceramic particles are usually used, it is effective to add 0.5% by weight or less of MgO or the like. When the ceramic particles are Si 3 N 4 (including sialon), Al 2 O 3 , Y 2 O 3 , MgO, etc. are about 10% by volume,
When the ceramic particles are SiC, Y 2 O 3 , Yb 2 O 3
About 5% by volume or the like, 0.5 volume of SiO 2 or the like in the case of Y 2 O 3, Yb 2 O 3 or the like for about 2 vol%, and the ceramic particles are MgO particles in the case of ceramic particles AlN particles It is effective to add about%. Although it is possible to add more sintering aids, it is not preferable because grain growth is likely to occur and the high-temperature strength of the sintered body is reduced.
【0022】[0022]
【実施例】実施例1 マトリックスとなるSi3N4粒子、SiC粒子、AlN
粒子、MgO粒子に、それぞれ下記表1に示す分散粒子
を所定量混合した。また、焼結助剤として、Si3N4粒
子には5重量%のY2O3−2重量%Al2O3を、SiC
粒子には2重量%のY2O3を、AlN粒子には2重量%
のY2O3を添加した。尚、各セラミックス粒子及び焼結
助剤の平均粒径は、Si3N4粒子、AlN粒子、MgO
粒子、Al2O3粒子がそれぞれ0.1μm、及びSiC
粒子、Y2O3粒子がそれぞれ0.3μmであった。尚、
平均粒径は線密度から算出した。EXAMPLES Example 1 Si 3 N 4 particles, SiC particles and AlN serving as a matrix
Predetermined amounts of the dispersed particles shown in Table 1 below were mixed with the particles and the MgO particles. As a sintering aid, Si 3 N 4 particles contain 5% by weight of Y 2 O 3 -2% by weight Al 2 O 3 and SiC
2% by weight of Y 2 O 3 for the particles and 2% by weight for the AlN particles
Of Y 2 O 3 was added. The average particle size of each of the ceramic particles and the sintering aid is Si 3 N 4 particles, AlN particles, MgO
Particles, Al 2 O 3 particles of 0.1 μm each, and SiC
Particles and Y 2 O 3 particles were each 0.3 μm. still,
The average particle size was calculated from the linear density.
【0023】その後、各試料の混合粉末を成形し、下記
表2に示す条件で一次焼結及び二次焼結を行って、それ
ぞれセラミックス複合材料を製造した。一次焼結は常圧
窒素雰囲気中で4時間保持する常圧焼結とし、及び二次
焼結は100MPaの窒素雰囲気中にて1時間保持する
雰囲気加圧焼結(以後HIPとも称する)とした。ただ
し、試料9については一次焼結を行わず、二次焼結は機
械的加圧を行うホットプレス(HP)とした。Thereafter, the mixed powder of each sample was molded and subjected to primary sintering and secondary sintering under the conditions shown in Table 2 below to produce ceramic composite materials. The primary sintering was normal pressure sintering for 4 hours in a normal pressure nitrogen atmosphere, and the secondary sintering was atmospheric pressure sintering (hereinafter also referred to as HIP) for 1 hour in a 100 MPa nitrogen atmosphere. . However, the primary sintering was not performed for Sample 9, and the secondary sintering was performed by hot pressing (HP) in which mechanical pressure was applied.
【0024】得られた各試料のセラミックス複合材料に
ついて、JIS R 1601に従った曲げ試験片を切り
出し、室温で3点曲げ強度を測定した。これらの結果
を、一次焼結体の相対密度と開気孔率、及び二次焼結体
(セラミックス複合材料)の相対密度とマトリックス粒
子の平均粒径と共に、下記表2に示した。With respect to the obtained ceramic composite material of each sample, a bending test piece in accordance with JIS R 1601 was cut out, and the three-point bending strength was measured at room temperature. The results are shown in Table 2 below, together with the relative density and open porosity of the primary sintered body, the relative density of the secondary sintered body (ceramic composite material) and the average particle size of the matrix particles.
【0025】[0025]
【表1】 マトリックス 分 散 粒 子 試料 粒 子 種 類 最大粒径(μm) 平均粒径(μm) 添加量(wt%) 1 Si3N4 SiC 1.0 0.5 5 2* Si3N4 SiC 3.0 1.0 5 3* Si3N4 SiC 0.8 0.3 0.1 4 Si3N4 SiC 0.8 0.3 0.5 5 Si3N4 SiC 0.8 0.3 1 6 Si3N4 SiC 0.8 0.3 10 7* Si3N4 SiC 0.8 0.3 15 8* Si3N4 SiC 0.8 0.3 1 9* Si3N4 SiC 0.8 0.3 5 10 MgO SiC 0.8 0.3 5 11 SiC TiB2 0.9 0.5 5 12 AlN SiC 0.8 0.3 5 (注)表中の*を付した試料は比較例である。TABLE 1 Matrix partial dispersion particle child sample particle child species such maximum particle diameter ([mu] m) average particle size ([mu] m) amount (wt%) 1 Si 3 N 4 SiC 1.0 0.5 5 2 * Si 3 N 4 SiC 3.0 1.0 5 3 * Si 3 N 4 SiC 0.8 0.3 0.1 4 Si 3 N 4 SiC 0.8 0.3 0.5 5 Si 3 N 4 SiC 0.8 0.3 16 Si 3 N 4 SiC 0.8 0.3 10 7 * Si 3 N 4 SiC 0.8 0.3 15 8 * Si 3 N 4 SiC 0.8 0.3 1 9 * Si 3 N 4 SiC 0.8 0.3 5 10 MgO SiC 0.8 0.3 5 11 SiC TiB 2 0.9 0.5 5 12 AlN SiC 0.8 0.35 Note: Samples marked with * in the table are compared It is an example.
【0026】[0026]
【表2】 一 次 焼 結 開気孔率 二 次 焼 結 マトリックス 曲げ強度試料 温度(℃) 密度(%) (vol%) 温度(℃) 密度(%) 粒径(μm) (MPa) 1 1750 92 9 1650 99.5 1.7 1200 2* 1750 88 15 1650 96 1.7 560 3* 1700 95 5 1650 99.9 2.2 600 4 1700 94 8 1650 99.5 2.0 900 5 1750 92 7 1650 99.8 1.9 1020 6 1850 90 9 1700 99.1 1.1 1100 7* 1850 85 25 1850 89 0.8 640 8* 1800 96 4 1650 99.9 2.8 620 9* 一次焼結なし − 1750/HP 99.5 1.7 1200 10 1750 92 8 1650 99.2 2.5 650 11 1900 91 9 1850 99 3.0 500 12 1750 92 10 1650 99.5 3.5 450 (注)表中の*を付した試料は比較例である。Table 2 primary sintered open porosity secondary sintering matrix flexural strength sample temperature (℃) Density (%) (vol%) Temperature (℃) Density (%) particle diameter ([mu] m) (MPa) 1 1750 92 9 1650 99.5 1.7 1200 2 * 1750 88 15 1650 96 1.7 560 3 * 1700 95 5 1650 99.9 2.2 600 4 1700 94 8 1650 99.5 2.0 900 5 1750 92 7 1650 99.8 1.9 1020 6 1850 90 9 1700 99.1 1.1 1100 7 * 1850 85 25 1850 89 0.8 640 8 * 1800 96 4 1650 99.9 2.8 620 9 * No primary sintering-1750 / HP 99.5 1.7 1200 10 1750 92 8 1650 99.2 2.5 650 11 1900 91 9 1850 99 3.0 500 12 1750 92 10 1650 99.5 3.5 450 (Note) Samples marked with * in the table are comparative examples.
【0027】上記の結果から、各試料において分散粒子
の最大粒径1μm以下且つ平均粒径0.5μm以下の場
合、一次焼結での相対密度が90%以上であれば、HI
Pによる二次焼結で相対密度99%以下の緻密化を達成
できることが分かる。また、二次焼結後の各試料はHP
による試料9と同等の曲げ強度を有し、特に分散粒子の
添加量が1〜10体積%の場合に高い曲げ強度が得られ
ることが分かる。尚、一次焼結において相対密度を95
%以上にした試料3と試料8では、異常な粒成長が起こ
るため、二次焼結においてHIPで緻密化させても、高
い曲げ強度が得られないことが理解される。From the above results, in each sample, when the maximum particle size of the dispersed particles is 1 μm or less and the average particle size is 0.5 μm or less, if the relative density in the primary sintering is 90% or more, HI
It is understood that densification with a relative density of 99% or less can be achieved by secondary sintering with P. Each sample after secondary sintering is HP
It can be seen that the sample has a bending strength equivalent to that of Sample 9 and that a high bending strength can be obtained particularly when the added amount of the dispersed particles is 1 to 10% by volume. In the primary sintering, the relative density was 95
%, Sample 3 and sample 8 exhibit abnormal grain growth, so that it is understood that high bending strength cannot be obtained even when densification by HIP in secondary sintering.
【0028】実施例2 前記実施例1の試料5と同様に、しかし二次焼結のHI
Pにおける雰囲気圧力と焼結温度を下記表3のごとく変
化させて、セラミックス複合材料を製造した。得られた
各試料のセラミックス複合材料について、実施例1と同
様に相対密度、マトリックス粒子の平均粒径、室温での
3点曲げ強度を測定し、その結果を下記表3に示した。 Example 2 As in the case of the sample 5 of the above-mentioned Example 1, but the HI of the secondary sintering was used.
By changing the atmosphere pressure and sintering temperature in P as shown in Table 3 below, a ceramic composite material was manufactured. The relative density, the average particle size of the matrix particles, and the three-point bending strength at room temperature of the obtained ceramic composite material of each sample were measured in the same manner as in Example 1. The results are shown in Table 3 below.
【0029】[0029]
【表3】 二 次 焼 結 マトリックス 曲げ強度試料 圧力(MPa) 温度(℃) 密度(%) 粒径(μm) (MPa) 13 5 1700 99.1 2.3 850 14 10 1700 99.4 2.3 920 15 50 1650 99.5 1.9 1000 5 100 1650 99.8 1.9 1020 16 200 1650 99.9 1.9 1050 (注)表中の試料5は実施例1の試料5と同じである。[Table 3] Secondary sintered matrix Flexural strength Sample pressure (MPa) Temperature (° C) Density (%) Particle size (μm) (MPa) 13 5 1700 99.1 2.3 850 14 10 1700 99.4 2.3 920 15 50 1650 99.5 1.9 1000 5 100 1650 99.8 1.9 1020 16 200 1650 99.9 1.9 1050 (Note) Sample 5 in the table is the same as Sample 5 in Example 1.
【0030】実施例3 代表的なセラミックス複合材料であるAl2O3−SiC
複合材料を以下のごとく製造した。即ち、平均粒径0.
1μmのα−Al2O3粒子に、最大粒径0.8μm且つ
平均粒径0.3μmで酸素量0.2重量%のSiC分散粒
子と、焼結助剤として平均粒径0.1μmのMgOを下
記表4に示す割合で添加し、混合及び成形した。次に、
各成形体を焼結温度1600℃〜1800℃の常圧窒素
雰囲気下で一次焼結した後、1600℃及び窒素圧力1
00MPaのHIPにより二次焼結した。 Example 3 Al 2 O 3 —SiC which is a representative ceramic composite material
A composite material was produced as follows. That is, the average particle size is 0.
1 μm α-Al 2 O 3 particles, SiC dispersed particles having a maximum particle diameter of 0.8 μm, an average particle diameter of 0.3 μm and an oxygen content of 0.2% by weight, and an average particle diameter of 0.1 μm as a sintering aid. MgO was added at the ratio shown in Table 4 below, and mixed and molded. next,
After primary sintering of each compact under a normal pressure nitrogen atmosphere at a sintering temperature of 1600 ° C. to 1800 ° C., 1600 ° C. and a nitrogen pressure of 1
Secondary sintering was performed using a HIP of 00 MPa.
【0031】得られた各セラミックス複合材料につい
て、実施例1と同様に3点曲げ試験を行い、室温と12
00℃で3点曲げ強度を測定し、その結果を表4に併せ
て示した。SiC分散粒子の添加量が1〜10体積%の
範囲において、高い強度を示すことが分かる。また、こ
の場合の試料18〜22のセラミックス複合材料の相対
密度は全て99%以上であった。ただし、試料23は焼
結助剤であるMgOの添加量が0.5体積%を越えるた
め、高温での強度が低下した。Each of the obtained ceramic composite materials was subjected to a three-point bending test in the same manner as in Example 1.
The three-point bending strength was measured at 00 ° C., and the results are shown in Table 4. It can be seen that high strength is exhibited when the added amount of the SiC dispersed particles is in the range of 1 to 10% by volume. In this case, the relative densities of the ceramic composite materials of Samples 18 to 22 were all 99% or more. However, in Sample 23, the amount of MgO as a sintering aid exceeded 0.5% by volume, so that the strength at high temperatures was reduced.
【0032】[0032]
【表4】 SiC添加量 MgO添加量 一次焼結 曲げ強度(MPa) 試料 (vol%) (vol%) 温度(℃) 室 温 1200℃ 17* 0 0 1600 600 400 18 1 0 1600 900 780 19 5 0 1800 1100 900 20 5 0.1 1800 1150 850 21 10 0.1 1800 1120 850 22 10 0.5 1800 1200 850 23* 10 0.6 1800 1200 650 (注)表中の*を付した試料は比較例である。[Table 4] Addition amount of SiC Addition amount of MgO Primary sintering bending strength (MPa) Sample (vol%) (vol%) Temperature (° C) Room temperature 1200 ° C 17 * 0 0 1600 600 400 18 1 0 1600 900 780 19 5 0 1800 1100 900 20 5 0.1 1800 1150 850 21 10 0.1 1800 1120 850 22 10 0.5 1800 1200 850 23 * 10 0.6 1800 1200 650 Note: Samples marked with * in the table are comparative examples.
【0033】また、上記各試料のうちの代表的な試料1
7、試料19、試料20、及び試料21について、HI
P前の一次焼結体の相対密度と、HIP後の二次焼結体
(セラミックス複合材料)の相対密度との関係を、グラ
フにして図3に示した。この図3から、分散粒子を含ま
ない試料17では、HIP前密度が95%を越えなけれ
ば二次焼結で密度99%以上に緻密化できないのに対し
て、分散粒子を含む本発明の各試料では、HIP前密度
が95%未満であっても二次焼結で密度99%以上に緻
密化されることが分かる。A representative sample 1 of the above samples
7, Sample 19, Sample 20, and Sample 21
FIG. 3 is a graph showing the relationship between the relative density of the primary sintered body before P and the relative density of the secondary sintered body (ceramic composite material) after HIP. From FIG. 3, it can be seen that, in the sample 17 containing no dispersed particles, the density before the HIP cannot be increased to 99% or more by the secondary sintering unless the pre-HIP density exceeds 95%. In the sample, it can be seen that even if the pre-HIP density is less than 95%, the density is increased to 99% or more by the secondary sintering.
【0034】実施例4 前記実施例3の試料19と同様に、しかし下記表5に示
すごとく酸素量の異なるSiC分散粒子をそれぞれ5重
量%添加混合して、表5に示す各温度にて常圧雰囲気下
で一次焼結した後、1600℃及び窒素圧力100MP
aのHIPにて二次焼結した。 Example 4 In the same manner as in Sample 19 of Example 3 above, but as shown in Table 5 below, 5% by weight of SiC-dispersed particles having different oxygen contents were added and mixed. After primary sintering under pressure atmosphere, 1600 ° C and nitrogen pressure 100MP
The secondary sintering was performed by the HIP of a.
【0035】得られた各セラミックス複合材料につい
て、JIS R 1601に従った曲げ試験により3点曲
げ強度を室温にて測定し、その結果を表5に併せて示し
た。この結果から、分散粒子の酸素量が0.15重量%
以下の試料24と試料25では、一次焼結の際に高温で
焼結する必要があるためマトリックス粒子の粒成長が起
こり、二次焼結後の3点曲げ強度が低下したことが分か
る。For each of the obtained ceramic composite materials, a three-point bending strength was measured at room temperature by a bending test according to JIS R 1601, and the results are shown in Table 5. From this result, the oxygen content of the dispersed particles was 0.15% by weight.
In the following Samples 24 and 25, it is necessary to perform sintering at a high temperature during the primary sintering, so that the growth of matrix particles occurred, and the three-point bending strength after the secondary sintering was reduced.
【0036】[0036]
【表5】 酸素量 一 次 焼 結 二次焼結 曲げ強度試料 (wt%) 温度(℃) 密度(%) 密度(%) (MPa) 24 0.1 1800 93 99 700 25 0.1 1850 94 99 750 26 0.15 1800 91 99 1080 19 0.2 1800 92 99 1100 27 0.3 1750 92 99 1250 (注)表中の試料19は実施例3の試料19と同じである。[Table 5] Oxygen content Primary sintering Secondary sintering Flexural strength sample (wt%) Temperature (° C) Density (%) Density (%) (MPa) 24 0.1 1800 93 99 700 25 0.1 1850 94 99 750 26 0.15 1800 91 99 1080 19 0.2 1800 92 99 1100 27 0.3 1750 92 99 1250 (Note) Sample 19 in the table is the same as Sample 19 of Example 3.
【0037】[0037]
【発明の効果】本発明によれば、高い強度を有するセラ
ミックス複合材料を、常圧焼結と雰囲気加圧焼結による
簡便な方法で製造できるので、エンジン部品等の複雑形
状を持つ製品への適用が可能となる。According to the present invention, a ceramic composite material having a high strength can be manufactured by a simple method using normal pressure sintering and atmospheric pressure sintering, so that it can be applied to products having complicated shapes such as engine parts. Applicable.
【図1】本発明方法の分散粒子を含む一次焼結過程を説
明するための模式的な断面図である。FIG. 1 is a schematic cross-sectional view for explaining a primary sintering process including dispersed particles according to a method of the present invention.
【図2】分散粒子を含まない場合の一次焼結過程を説明
するための模式的な断面図である。FIG. 2 is a schematic cross-sectional view for explaining a primary sintering process when no dispersed particles are included.
【図3】実施例3の各試料におけるHIP前密度とHI
P後密度の関係を示すグラフである。FIG. 3 shows pre-HIP density and HI for each sample of Example 3.
It is a graph which shows the relationship of density after P.
1 分散粒子 2 セラミックス粒子 3 液相 4 閉気孔 5 開気孔 1 dispersed particles 2 ceramic particles 3 liquid phase 4 closed pores 5 open pores
───────────────────────────────────────────────────── フロントページの続き Fターム(参考) 4G030 AA07 AA36 AA45 AA47 AA49 AA51 AA52 AA54 BA20 GA11 GA23 GA24 GA28 ──────────────────────────────────────────────────続 き Continued on the front page F term (reference) 4G030 AA07 AA36 AA45 AA47 AA49 AA51 AA52 AA54 BA20 GA11 GA23 GA24 GA28
Claims (6)
に、表面酸化物層を有する最大粒径1μm以下且つ平均
粒径0.5μm以下の非酸化物系セラミックスの分散粒
子を添加混合し、常圧焼結により相対密度90%以上9
5%未満とした後、雰囲気加圧焼結により相対密度99
%以上に緻密化して、前記分散粒子の一部がマトリック
ス粒子内に分散したセラミックス複合材料を得ることを
特徴とするセラミックス複合材料の製造方法。1. A non-oxide ceramic dispersed particle having a surface oxide layer and having a maximum particle size of 1 μm or less and an average particle size of 0.5 μm or less is added to and mixed with ceramic particles serving as a matrix. Relative density 90% or more 9
After reducing to less than 5%, the relative density was 99
%, Thereby obtaining a ceramic composite material in which a part of the dispersed particles is dispersed in matrix particles.
積%の範囲内であることを特徴とする、請求項1に記載
のセラミックス複合材料の製造方法。2. The method for producing a ceramic composite material according to claim 1, wherein the amount of the dispersed particles is in the range of 0.5 to 10% by volume.
量が0.15重量%以上であることを特徴とする、請求
項1又は2に記載のセラミックス複合材料の製造方法。3. The method for producing a ceramic composite material according to claim 1, wherein the amount of oxygen in the surface oxide layer of the dispersed particles is 0.15% by weight or more.
O、Si3N4、SiC、AlNから選ばれた少なくとも
1種であることを特徴とする、請求項1〜3のいずれか
に記載のセラミックス複合材料の製造方法。4. The method according to claim 1, wherein the ceramic particles are Al 2 O 3 , Mg
O, Si 3 N 4, SiC , and wherein the at least one selected from AlN, method of producing a ceramic composite material according to claim 1.
N、TiC、TiB2から選ばれた少なくとも1種であ
ることを特徴とする、請求項1〜4に記載のセラミック
ス複合材料の製造方法。5. The method according to claim 1, wherein the dispersed particles are Si 3 N 4 , SiC, Ti
N, TiC, and wherein the at least one selected from TiB 2, method of producing a ceramic composite material according to claims 1-4.
り、焼結助剤として0.5重量%以下のMgOを添加す
ることを特徴とする、請求項1〜5のいずれかに記載の
セラミックス複合材料の製造方法。6. The ceramic according to claim 1, wherein said ceramic particles are Al 2 O 3 , and 0.5% by weight or less of MgO is added as a sintering aid. Manufacturing method of composite material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10202485A JP2000034174A (en) | 1998-07-17 | 1998-07-17 | Manufacturing method of ceramic composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10202485A JP2000034174A (en) | 1998-07-17 | 1998-07-17 | Manufacturing method of ceramic composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JP2000034174A true JP2000034174A (en) | 2000-02-02 |
Family
ID=16458295
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| Application Number | Title | Priority Date | Filing Date |
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| JP10202485A Pending JP2000034174A (en) | 1998-07-17 | 1998-07-17 | Manufacturing method of ceramic composite material |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012087045A (en) * | 2011-11-14 | 2012-05-10 | Nippon Tokushu Gokin Kk | Method for producing binderless alloy |
| WO2019163710A1 (en) * | 2018-02-20 | 2019-08-29 | 日本碍子株式会社 | Composite sintered body, component of semiconductor manufacturing device and method for manufacturing composite sintered body |
-
1998
- 1998-07-17 JP JP10202485A patent/JP2000034174A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012087045A (en) * | 2011-11-14 | 2012-05-10 | Nippon Tokushu Gokin Kk | Method for producing binderless alloy |
| WO2019163710A1 (en) * | 2018-02-20 | 2019-08-29 | 日本碍子株式会社 | Composite sintered body, component of semiconductor manufacturing device and method for manufacturing composite sintered body |
| KR20200106180A (en) * | 2018-02-20 | 2020-09-11 | 엔지케이 인슐레이터 엘티디 | Composite sintered body, semiconductor manufacturing device member, and manufacturing method of composite sintered body |
| JPWO2019163710A1 (en) * | 2018-02-20 | 2021-03-04 | 日本碍子株式会社 | Manufacturing method of composite sintered body, semiconductor manufacturing equipment member and composite sintered body |
| KR102432509B1 (en) | 2018-02-20 | 2022-08-12 | 엔지케이 인슐레이터 엘티디 | Composite sintered body, semiconductor manufacturing apparatus member, and manufacturing method of composite sintered body |
| JP7227954B2 (en) | 2018-02-20 | 2023-02-22 | 日本碍子株式会社 | Composite sintered body, semiconductor manufacturing device member, and manufacturing method of composite sintered body |
| US11837488B2 (en) | 2018-02-20 | 2023-12-05 | Ngk Insulators, Ltd. | Composite sintered body, semiconductor manufacturing apparatus member, and method of manufacturing composite sintered body |
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