JPH0544429B2 - - Google Patents
Info
- Publication number
- JPH0544429B2 JPH0544429B2 JP61018689A JP1868986A JPH0544429B2 JP H0544429 B2 JPH0544429 B2 JP H0544429B2 JP 61018689 A JP61018689 A JP 61018689A JP 1868986 A JP1868986 A JP 1868986A JP H0544429 B2 JPH0544429 B2 JP H0544429B2
- Authority
- JP
- Japan
- Prior art keywords
- mullite
- fibers
- strength
- silicon carbide
- present
- 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
- 239000000835 fiber Substances 0.000 claims description 42
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 claims description 41
- 229910052863 mullite Inorganic materials 0.000 claims description 41
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 37
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 35
- 239000000919 ceramic Substances 0.000 claims description 30
- 239000013078 crystal Substances 0.000 claims description 16
- 239000002131 composite material Substances 0.000 claims description 8
- 239000012071 phase Substances 0.000 description 31
- 239000000463 material Substances 0.000 description 16
- 238000000034 method Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 10
- 238000005245 sintering Methods 0.000 description 9
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 6
- 150000001875 compounds Chemical class 0.000 description 6
- 230000007423 decrease Effects 0.000 description 6
- 239000011148 porous material Substances 0.000 description 6
- 239000002994 raw material Substances 0.000 description 6
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 238000010304 firing Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 229910052581 Si3N4 Inorganic materials 0.000 description 3
- 229910004298 SiO 2 Inorganic materials 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 150000004649 carbonic acid derivatives Chemical class 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 238000000280 densification Methods 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011268 mixed slurry Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 239000005995 Aluminium silicate Substances 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 235000012211 aluminium silicate Nutrition 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 150000004679 hydroxides Chemical class 0.000 description 1
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000013001 point bending Methods 0.000 description 1
- 238000000634 powder X-ray diffraction Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000001238 wet grinding Methods 0.000 description 1
Landscapes
- Compositions Of Oxide Ceramics (AREA)
Description
産業上の利用分野
本発明は、炭化珪素繊維を含有するムライト質
複合セラミツクスに関する。
従来の技術及びその問題点
アルミナ、ジルコニア、窒化珪素、炭化珪素等
の焼結体は、高強度かつ高硬度であり、更に耐熱
性、耐食性、耐摩耗性等に優れたものであり、構
造材として有望視され、エンジン部材等にその利
用が試みられつつある。しかしながら、アルミ
ナ、ジルコニア等の酸化物系焼結体は、高温強度
や熱衝撃抵抗性が悪く、また窒化珪素や炭化珪素
等は靭性や耐酸化性が悪いという欠点があり、高
温構造材料として広くの利用されるには至つてい
ない。
そこで近年セラミツクスの機械的性質を改善す
るため、アルミナ、ジルコニア、窒化珪素などの
単相セラミツクスに炭化珪素(SiC)繊維を含有
させて靭性の改善を行なうことが研究されてい
る。これらのうちアルミナ−SiCセラミツクス
は、SiC繊維の複合による靭性の改善効果は認め
られているものの、高温強度などの機械的性質が
不充分であり、また、窒化珪素−SiCセラミツク
スは高温強度は優れているものの、低温における
強度の改善に難点があり、また高温での耐酸化性
も悪く、これらの理由により高温構造材料への利
用の拡大が妨げられている。
問題点を解決するための手段
本発明者は、上記した如き現状に鑑みて高温構
造材料として優れた特性を有するセラミツクス材
料を見出すべく鋭意研究を重ねてきた。その結
果、ムライトを母材とし、SiC繊維を均一に分散
させた緻密な焼結体であつて、特定量のガラス質
相を含み、かつ特定値以上の密度を有するセラミ
ツクスが、室温及び高温において、高い強度及び
靭性を有し、かつ耐熱性に優れたものであること
を見出し、ここに本発明を完成した。
即ち本発明は、炭化珪素繊維5〜30容積%及び
ガラス質相0.5〜8容積%を含み、残部の95容積
%以上がムライト晶である焼結体であつて、対論
理密度が90%以上であることを特徴とする炭化水
素珪素繊維含有ムライト質複合セラミツクスに係
る。
本発明複合セラミツクスは、耐熱性に優れた酸
化物であるムライトを主とする母材中に、高温ま
で高強度であるSiC繊維を均一に分散させた構造
である。本発明者の研究によれば、SiC繊維を複
合させることによる効果を有効に発揮させるため
には、セラミツクスの微構造を適切に制御するこ
とか重要であることが見出された。特に、従来は
高温強度低下やSiCの酸化の原因となると考えら
れていたガラス質相を特定範囲の量存在させるこ
とが必要であることが判かつた。本発明セラミツ
クスは、具体的には以下に示す条件を満足するこ
とが必要である。
(a) 炭化珪素繊維及びガラス質相を除いた部分の
95容積%以上をムライト晶とする。
本発明てでは、セラミツクスの母材としては
耐熱性に優れた酸化物であるムライトを用い
る。本発明においてムライト晶とは、
3Al2O3・2SiO2(Al2O371.8重量%、SiO228.2重
量%)で表わされるムライト結晶だけでなく、
そのムライトの固溶体も含む。更に、ムライト
中のAlの30%程度までをCrで置換固溶しても
良い。特に、Alの一部をCrで置換固溶した焼
結体は靭性、耐食性等の改善に寄与する。ムラ
イト晶の平均粒径は8μm以下であることが好
ましく、5μm以下がより好ましい。ムライト
晶の粒径が大きすぎると母材自体の強度が低い
ものとなると共に、粒界にできるガラス質相の
巾が大きくなり、高温強度が低下し易くなるの
で好ましくない。
本発明セラミツクスでは、ムライト晶は、炭
化珪素繊維及びガラス質相を除いた部分の95容
積%以上とする。5容積%未満であれば、
Al2O3、Cr2O3、ZrO2等(粉末X線回折法によ
る)が存在してもよいが、多くなりすぎるとム
ライト晶が粒状結晶となつて、高温強度が低く
なる。このため、ムライト晶単相であることが
好ましい。
(b) 炭化珪素繊維量を5〜30容積%とする。
本発明セラミツクスは炭化珪素繊維(SiCウ
イスカー、SiC多結晶体からなるフアイバー
等)が繊維の形態のままセラミツクス中に均一
に分散した構造である。炭化珪素繊維は、焼結
体中に二次元又は三次元的に分散して、強度、
靭性等を向上させる。繊維が大き過ぎると、緻
密な焼結体においてもこの繊維とムライトとの
粒界が破壊の応力集中源となり、強度の低下を
もたらす。また、繊維のアスペクト比(長さ/
直径)は大きいことが望ましいが、大き過ぎる
と母材の緻密化を阻害することとなる。このた
め繊維の平均直径は、0.05〜20μm程度とし、
好ましくはムライト結晶粒と同程度の0.1〜8μ
m程度とし、更に好ましくは0.3〜4μm程度と
する。また繊維の平均長さは、好ましくは、2
〜30μm程度とし、より好ましくは3〜15μm
程度とする。
セラミツクス中の炭化珪素繊維量は、5〜30
容積%とし、好ましくは10〜25容積%とする。
繊維量が5容積%未満では、強度や靭性を向上
させる効果が少なく、一方30容積%を上回る
と、焼結過程における物質移動が繊維により阻
害されて母材の焼結性が悪くなり、多量の空孔
が存在して焼結体密度が低くなり、その結果常
温における強度も低いものとなる。
(c) ガラス質相を0.5〜8容積%とする。
本発明において、ガラス質相とは、ムライト
結晶、炭化珪素繊維等の粒界に存在する非晶質
相をいう。ガラス質相は、セラミツクス中に
0.5〜8容積%存在することが必要であり、1
〜5容積%存在することがより好ましい。ガラ
ス質相の存在により、ムライトの拡散焼結に加
えて、液相焼結が生じるので、セラミツクスを
低温で緻密に焼結させることが可能となる。こ
のため焼結過程における母材のムライトの分解
や炭化珪素繊維の酸化が防止される。また、ガ
ラス質相は、ムライトの粒成長を抑制する効果
があり、緻密で均質なムライト多結晶体からな
る母材を形成させる働きをする。更に、ムライ
ト晶の柱状化にも寄与し、強度、靭性を向上さ
せる。
ガラス質相量が少なすぎると、上記効果が充
分に奏されず、且つ母材のムライトと炭化珪素
との熱膨脹の差が小さいために、焼結体中の繊
維に母材からの応力効果がわずかしか寄与せ
ず、引張り応力場で繊維の引抜きが生じ易く、
強度の向上効果が小さくなる。一方ガラス質相
が多すぎる場合には、高温の応力場でガラス質
相の塑性変形と粘性低下によりガラス質相から
の破壊の進展と繊維の引抜きが容易に生じ、強
度の急激な低下を起し易い。
ガラス質相としては、特に限定されず、例え
ばNa2O−Al2O3−SiO2系のものでも良いが、
K、Li、B、Mg、Cr及びYの少なくとも1種
の化合物、例えばこれらの炭酸塩、水酸化物、
塩化物、酸化物等の焼成過程において酸化物と
なる化合物を添加して、これらの成分と、ムラ
イトの構成成分であるAl、Si、O及び炭化珪
素繊維のSiとを主とするガラス質相を形成させ
ることが好ましい。上記成分は、焼結効果の他
に、Kはガラス質相の粘性増加による高温強度
の向上、Liはガラス質相の耐熱衝撃性向上、B
はSiCとムライトとの焼結性向上、Mg、Cr、
Yは靭性の向上に寄与する。
(d) 焼結体の対理論密度を90%以上とする。
本発明では、対理論密度とは、焼結体中に空
孔の存在しない100%緻密な焼結体の密度を理
論密度とし、焼結体密度をこの理論密度に対す
る百分率で表わしたものをいう。対理論密度が
90%未満では、焼結体に空孔が多く存在し、連
続孔を生成して、強度の低下や耐食性の低下の
原因となる。しかし、空孔が微細で小容積存在
する場合には、応力場において、空孔が応力分
散効果に寄与する。好ましくは、対理論密度は
92%以上とする。
本発明複合セラミツクスは、例えば以下の方法
によつて製造することができる。
ムライトとしては、溶液又はゾル状のSi、Al
含有化合物をAl/Si比がムライトの組成となる
ように混合した後、溶媒を飛散させ、焼成して、
予めムライト結晶化したものを用いることが好ま
しいが、カオリン(Al2O3・2SiO2・2H2O)とア
ルミナなどを用いて、セラミツクスの焼成中にム
ライトを反応析出させる反応焼結法により形成さ
せてもよい。ガラス質相を形成させるための化合
物は、ムライト結晶を予め形成させる際に加えて
おくことが好ましいが、ムライト原料にSiC繊維
を添加する際に加えてもよい。
炭化珪素繊維は、湿式でほぐし、繊維の塊とな
つているものを除去した後、ムライト原料及びガ
ラス質相を形成させる化合物からなる混合物に
徐々に加えながら湿式で混合することが望ましい
が、ムライト原料及びガラス質相を形成させるた
めの化合物と同時に配合して湿式粉砕混合しても
良い。
このようにして必要原料を加えた混合物を調整
した後、湿式で成形するか、或いは大気中又は減
圧中で炭化珪素繊維が分離しないよう乾燥させて
成形用原料としたものを常法に従い成形加工し、
次いで成形体を焼成することにより本発明複合セ
ラミツクスが得られる。本発明セラミツクスで
は、ガラス質相がセラミツクスの緻密化に寄与す
るため、加圧焼結法だけでなく、常圧焼結法も可
能であり、例えばN2、Ar等の常圧雰囲気下や真
空中で焼成するか、或いはこれらの雰囲気中又は
非酸化雰囲気中でホツトプレス、ホツトアイソス
タテイツクプレス等で焼成すればよい。焼成条件
は、1500〜1700℃程度で0.5〜10時間程度とすれ
ばよい。
発明の効果
本発明複合セラミツクスは、高強度の炭化珪素
繊維をムライトの緻密な焼結体中に包み込んだ構
造であり、室温及び1400℃程度の高温における強
度が共に30Kgf/mm2以上と高く、且つ繊維強化に
よつて靭性も高いものである。また高温の酸素雰
囲気下において安定なムライトに、炭化珪素繊維
が包み込まれているため、セラミツクス全体とし
ての耐酸化性も良好である。
本発明セラミツクスは、このような優れた特性
を有するものであり、エンジン部材、熱交換器部
材、高温の搬送用ロール、バーナーノズル、均熱
管、熱処理用部材など高温における耐久性が要求
される部材として極めて有用である。
実施例
以下に実施例を示して本発明を詳細に説明す
る。
実施例 1
下記第1表に示す原料のうちSiC繊維を除く原
料を、ボールミルで24時間湿式粉砕し、混合し
た。ムライトとしては、(Al2O3+SiO2)分99.99
%、比表面積5m2/gで結晶相がムライトからな
るものを用いた。ガラス質相形成物としては、
Na及びKの炭酸塩の1:2(モル比)混合粉末を
用いた。
得られた混合スラリーをミキサーで撹拌しなが
ら、平均直径0.4μm、平均長さ15μmのβ−SiCウ
イスカーを第1表に示す配合割合となるように
徐々に添加して混合した。次いで、この混合スラ
リーをスプレードライヤーにて乾燥、造粒し、第
1表に示す各温度で、カーボン型を用いて200
Kg/cm2でホツトプレス焼結させて板状の複合セラ
ミツクスを得た。
得られたセラミツクスのムライト量、ガラス質
相量及びSiC量を第2表に示す。また、JIS−R
−1601による3点曲げ強さの測定結果及びMI法
による靭性値(KIC)の測定結果を第2表に示
す。
INDUSTRIAL APPLICATION FIELD The present invention relates to mullite composite ceramics containing silicon carbide fibers. Prior art and its problems Sintered bodies of alumina, zirconia, silicon nitride, silicon carbide, etc. have high strength and hardness, and also have excellent heat resistance, corrosion resistance, abrasion resistance, etc., and are used as structural materials. It is seen as a promising material, and attempts are being made to use it in engine parts, etc. However, oxide-based sintered bodies such as alumina and zirconia have poor high-temperature strength and thermal shock resistance, and silicon nitride and silicon carbide have poor toughness and oxidation resistance, so they are widely used as high-temperature structural materials. However, it has not yet been fully utilized. Therefore, in recent years, in order to improve the mechanical properties of ceramics, research has been carried out on improving the toughness by incorporating silicon carbide (SiC) fibers into single-phase ceramics such as alumina, zirconia, and silicon nitride. Among these, alumina-SiC ceramics have been recognized to have an effect of improving toughness by combining SiC fibers, but have insufficient mechanical properties such as high-temperature strength, and silicon nitride-SiC ceramics have excellent high-temperature strength. However, there are difficulties in improving the strength at low temperatures, and the oxidation resistance at high temperatures is also poor, and these reasons are preventing the expansion of its use in high-temperature structural materials. Means for Solving the Problems In view of the current situation as described above, the present inventor has conducted extensive research in order to find a ceramic material that has excellent properties as a high-temperature structural material. As a result, ceramics, which are dense sintered bodies made of mullite as a base material and uniformly dispersed SiC fibers, contain a specific amount of glassy phase, and have a density above a specific value, can be produced at room and high temperatures. It was discovered that this material has high strength and toughness, and excellent heat resistance, and the present invention has now been completed. That is, the present invention provides a sintered body containing 5 to 30 volume % of silicon carbide fibers and 0.5 to 8 volume % of a glassy phase, with the remaining 95 volume % or more being mullite crystal, and having a theoretical density of 90% or more. The present invention relates to a mullite composite ceramic containing hydrocarbon silicon fibers. The composite ceramic of the present invention has a structure in which SiC fibers, which have high strength up to high temperatures, are uniformly dispersed in a matrix mainly composed of mullite, which is an oxide with excellent heat resistance. According to the research conducted by the present inventors, it has been found that in order to effectively exhibit the effects of combining SiC fibers, it is important to appropriately control the microstructure of ceramics. In particular, it has been found that it is necessary to have a glassy phase present in a specific range of amount, which was conventionally thought to cause a decrease in high-temperature strength and oxidation of SiC. Specifically, the ceramics of the present invention must satisfy the following conditions. (a) Part excluding silicon carbide fibers and glassy phase
More than 95% by volume is mullite crystal. In the present invention, mullite, which is an oxide with excellent heat resistance, is used as the ceramic base material. In the present invention, mullite crystals are
As well as mullite crystals represented by 3Al 2 O 3 2SiO 2 (71.8% by weight of Al 2 O 3 and 28.2% by weight of SiO 2 ),
It also includes solid solutions of mullite. Furthermore, up to about 30% of the Al in the mullite may be replaced with Cr as a solid solution. In particular, a sintered body in which a part of Al is replaced with Cr as a solid solution contributes to improvements in toughness, corrosion resistance, etc. The average particle size of the mullite crystals is preferably 8 μm or less, more preferably 5 μm or less. If the grain size of the mullite crystals is too large, the strength of the base material itself will be low, and the width of the glassy phase formed at the grain boundaries will become large, making it easy to reduce the high-temperature strength, which is not preferable. In the ceramics of the present invention, mullite crystals account for 95% or more by volume of the area excluding silicon carbide fibers and the glassy phase. If it is less than 5% by volume,
Al 2 O 3 , Cr 2 O 3 , ZrO 2 , etc. (according to powder X-ray diffraction method) may be present, but if too much, the mullite crystals become granular crystals and the high temperature strength decreases. For this reason, it is preferable to have a single phase of mullite crystal. (b) The amount of silicon carbide fiber is 5 to 30% by volume. The ceramic of the present invention has a structure in which silicon carbide fibers (SiC whiskers, fibers made of SiC polycrystals, etc.) are uniformly dispersed in the ceramic in the form of fibers. Silicon carbide fibers are dispersed two-dimensionally or three-dimensionally in a sintered body to improve strength,
Improves toughness etc. If the fibers are too large, even in a dense sintered body, the grain boundaries between the fibers and mullite become a stress concentration source for fracture, resulting in a decrease in strength. In addition, the aspect ratio of the fiber (length/
Although it is desirable that the diameter (diameter) is large, if it is too large, it will hinder the densification of the base material. For this reason, the average diameter of the fibers should be approximately 0.05 to 20 μm,
Preferably 0.1 to 8μ, which is the same as mullite crystal grains.
The thickness is preferably about 0.3 to 4 μm. Further, the average length of the fibers is preferably 2
~30μm, more preferably 3~15μm
degree. The amount of silicon carbide fiber in ceramics is 5 to 30
% by volume, preferably 10-25% by volume.
If the amount of fibers is less than 5% by volume, the effect of improving strength and toughness will be small, while if it exceeds 30% by volume, the fibers will inhibit mass transfer during the sintering process, resulting in poor sinterability of the base material, Due to the presence of pores, the density of the sintered body is low, and as a result, the strength at room temperature is also low. (c) The glassy phase is 0.5 to 8% by volume. In the present invention, the glassy phase refers to an amorphous phase existing at grain boundaries of mullite crystals, silicon carbide fibers, and the like. The glassy phase is present in ceramics.
It is necessary to be present at 0.5 to 8% by volume, and 1
More preferably, it is present in an amount of ~5% by volume. Due to the presence of the glassy phase, liquid phase sintering occurs in addition to diffusion sintering of mullite, making it possible to sinter ceramics densely at low temperatures. This prevents the decomposition of mullite as a base material and the oxidation of silicon carbide fibers during the sintering process. Further, the glassy phase has the effect of suppressing grain growth of mullite, and functions to form a base material consisting of dense and homogeneous mullite polycrystals. Furthermore, it also contributes to columnarization of mullite crystals, improving strength and toughness. If the amount of glassy phase is too small, the above effects will not be sufficiently achieved, and the difference in thermal expansion between the base material mullite and silicon carbide will be small, so the stress effect from the base material will be applied to the fibers in the sintered body. It contributes only a small amount and is prone to fiber pull-out in the tensile stress field.
The strength improvement effect becomes smaller. On the other hand, if there is too much vitreous phase, the plastic deformation and viscosity reduction of the vitreous phase in the high-temperature stress field will easily cause the propagation of fracture and the pulling out of fibers from the vitreous phase, resulting in a rapid decrease in strength. Easy to do. The glassy phase is not particularly limited, and may be, for example, a Na 2 O−Al 2 O 3 −SiO 2 type, but
at least one compound of K, Li, B, Mg, Cr and Y, such as their carbonates, hydroxides,
Compounds that become oxides in the firing process, such as chlorides and oxides, are added to form a glassy phase consisting mainly of these components, Al, Si, and O, which are the constituent components of mullite, and Si of silicon carbide fibers. It is preferable to form. In addition to the sintering effect, the above components have the following properties: K improves high-temperature strength by increasing the viscosity of the glassy phase, Li improves the thermal shock resistance of the glassy phase, and B
improves the sinterability of SiC and mullite, Mg, Cr,
Y contributes to improving toughness. (d) The theoretical density of the sintered body is 90% or more. In the present invention, the theoretical density refers to the theoretical density of a 100% dense sintered body with no pores, and the density of the sintered body is expressed as a percentage of this theoretical density. . The theoretical density is
If it is less than 90%, there are many pores in the sintered body, forming continuous pores, which causes a decrease in strength and corrosion resistance. However, when the pores are minute and exist in a small volume, the pores contribute to the stress dispersion effect in the stress field. Preferably, the theoretical density is
Must be 92% or more. The composite ceramics of the present invention can be produced, for example, by the following method. Mullite is Si, Al in solution or sol form.
After mixing the containing compounds so that the Al/Si ratio has the composition of mullite, the solvent is scattered, and the material is fired.
It is preferable to use mullite that has been crystallized in advance, but it can also be formed by a reaction sintering method in which mullite is reacted and precipitated during firing of ceramics using kaolin (Al 2 O 3 2SiO 2 2H 2 O) and alumina. You may let them. The compound for forming a glassy phase is preferably added when forming mullite crystals in advance, but may be added when adding SiC fibers to the mullite raw material. It is preferable to loosen the silicon carbide fibers in a wet process and remove any fiber clumps, and then gradually add the silicon carbide fibers to a mixture consisting of a mullite raw material and a compound that forms a glassy phase and mix them in a wet process. It may be mixed together with the raw material and the compound for forming the glassy phase by wet grinding. After preparing the mixture with the necessary raw materials in this way, it is either wet molded or dried in the atmosphere or under reduced pressure so that the silicon carbide fibers do not separate, and the raw material for molding is then molded according to a conventional method. death,
The composite ceramic of the present invention is then obtained by firing the molded body. In the ceramics of the present invention, since the glassy phase contributes to densification of the ceramic, not only pressure sintering method but also normal pressure sintering method is possible. Alternatively, it may be fired in these atmospheres or in a non-oxidizing atmosphere using a hot press, a hot isostatic press, or the like. The firing conditions may be approximately 1500 to 1700°C for approximately 0.5 to 10 hours. Effects of the Invention The composite ceramics of the present invention has a structure in which high-strength silicon carbide fibers are wrapped in a dense sintered body of mullite, and its strength at room temperature and high temperature of about 1400°C is as high as 30 Kgf/mm 2 or more. In addition, it has high toughness due to fiber reinforcement. Furthermore, since the silicon carbide fibers are wrapped in mullite, which is stable in a high-temperature oxygen atmosphere, the ceramic as a whole has good oxidation resistance. The ceramics of the present invention have such excellent properties and can be used in parts that require durability at high temperatures, such as engine parts, heat exchanger parts, high-temperature conveying rolls, burner nozzles, soaking tubes, and heat treatment parts. It is extremely useful as a EXAMPLES The present invention will be described in detail with reference to Examples below. Example 1 The raw materials shown in Table 1 below, excluding SiC fibers, were wet-pulverized for 24 hours in a ball mill and mixed. As mullite, (Al 2 O 3 + SiO 2 ) min 99.99
%, a specific surface area of 5 m 2 /g, and a crystal phase consisting of mullite. As a glassy phase formation product,
A 1:2 (mole ratio) mixed powder of Na and K carbonates was used. While stirring the obtained mixed slurry with a mixer, β-SiC whiskers having an average diameter of 0.4 μm and an average length of 15 μm were gradually added and mixed in the proportions shown in Table 1. Next, this mixed slurry was dried and granulated using a spray dryer, and then granulated using a carbon mold at each temperature shown in Table 1.
A plate-shaped composite ceramic was obtained by hot press sintering at Kg/cm 2 . Table 2 shows the amount of mullite, the amount of glassy phase, and the amount of SiC in the obtained ceramics. Also, JIS-R
Table 2 shows the results of measuring the three-point bending strength using -1601 and the toughness value (KIC) using the MI method.
【表】【table】
【表】【table】
【表】
第2表から明らかな様に、本発明セラミツクス
は、室温及び高温における強度、並びに靭性が高
い値を示す。これに対してSiC繊維が5%未満の
セラミツクス(比較品1,2)では靭性値が3.0
以下と低くなり、またSiC繊維が30%を上回る場
合(比較品3)及びガラス質相が0.5%未満の場
合(比較品4)には焼結性が悪く対理論密度が低
くなり、室温及び高温における強度が低くなる。
ガラス質相が8%を上回る場合(比較品5)に
は、高温強度が特に低いものとなる。[Table] As is clear from Table 2, the ceramics of the present invention exhibit high values of strength and toughness at room and high temperatures. On the other hand, ceramics containing less than 5% SiC fibers (comparative products 1 and 2) have a toughness value of 3.0.
In addition, when the SiC fiber content exceeds 30% (comparative product 3) and when the glassy phase content is less than 0.5% (comparative product 4), the sinterability is poor and the theoretical density is low. Strength at high temperatures decreases.
When the glassy phase exceeds 8% (comparative product 5), the high temperature strength becomes particularly low.
Claims (1)
0.5〜8容積%を含み、残部の95容積%以上がム
ライト晶である焼結体であつて、対理論密度が90
%以上であることを特徴とする炭化珪素繊維含有
ムライト質複合セラミツクス。1 5-30% by volume of silicon carbide fibers and glassy phase
A sintered body containing 0.5 to 8% by volume, with the remaining 95% or more by volume being mullite crystals, and having a theoretical density of 90
% or more of mullite composite ceramics containing silicon carbide fibers.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61018689A JPS62176964A (en) | 1986-01-30 | 1986-01-30 | Silicon carbide fiber-containing mullite base composite ceramics |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61018689A JPS62176964A (en) | 1986-01-30 | 1986-01-30 | Silicon carbide fiber-containing mullite base composite ceramics |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62176964A JPS62176964A (en) | 1987-08-03 |
| JPH0544429B2 true JPH0544429B2 (en) | 1993-07-06 |
Family
ID=11978581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP61018689A Granted JPS62176964A (en) | 1986-01-30 | 1986-01-30 | Silicon carbide fiber-containing mullite base composite ceramics |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62176964A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BR9708819A (en) * | 1996-04-26 | 1999-08-03 | Asea Brown Bover Ab | Varistor block |
-
1986
- 1986-01-30 JP JP61018689A patent/JPS62176964A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62176964A (en) | 1987-08-03 |
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