JP3756583B2 - Ceramic-based fiber composite material and manufacturing method thereof - Google Patents
Ceramic-based fiber composite material and manufacturing method thereof Download PDFInfo
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- JP3756583B2 JP3756583B2 JP21882696A JP21882696A JP3756583B2 JP 3756583 B2 JP3756583 B2 JP 3756583B2 JP 21882696 A JP21882696 A JP 21882696A JP 21882696 A JP21882696 A JP 21882696A JP 3756583 B2 JP3756583 B2 JP 3756583B2
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Description
【0001】
【発明の属する技術分野】
この発明は、セラミックス基繊維複合材料およびその製造方法に係り、とくにマトリックスとして反応焼結法で形成された緻密質の炭化ケイ素(SiC)を用いた複合材の改善に関する。
【0002】
【従来の技術】
一般に、セラミックス焼結体は、高温までの強度低下が少なく、硬度、電気絶縁性、耐摩耗性、耐腐食性、軽量性等の諸特性が従来の金属材と比較して優れているため、重電設備部品、航空機部品、自動車部品、電子機器、精密機械部品、半導体装置材料などの電子用材料や構造用材料として広い分野において使用されている。
【0003】
しかし、このセラミックス焼結体は、圧縮応力に比べて引張り応力に弱く、この引張り応力下で破壊が一気に進行する、いわゆる脆性という欠点を有しているため、このような脆性を改善して高靭性化や破壊エネルギーの増大を図ることが適用対象によっては必要となる。このような脆性改善の試みは、耐熱性及び高温強度に加え、特に高信頼性が要求されるガスタービン部品、航空機部品、自動車部品等のセラミックス構造部品への適用に際し、強く要請されている。
【0004】
そこで、このような要請を受けて、破壊靭性値、破壊エネルギー値、耐熱衝撃性等を高めたセラミックス焼結体として、無機物質や金属からなる繊維、ウィスカー、プレート、粒子等の複合素材をマトリックス中に分散複合化させて形成したセラミックス基複合材料が脚光を浴び、この実用化研究が内外の研究機関等において精力的に進められている。特に、繊維を複合化させてセラミックス基繊維複合材料とした場合には、破壊抵抗の改良効果が大きいため、その実用化が期待されている。
【0005】
このようなセラミックス基繊維複合材料の中でも、特に高温材料としてSiCをマトリックスとする複合材が脚光を浴びている。この複合材のSiCマトリックスの合成法の一例としては、繊維耐熱性を考慮に入れると、比較的合成温度の低いCVI法(Chemical Vapor Infiltration :化学蒸気含浸法)、PC(プリカーサ)法、反応焼結法などが挙げられるが、この中でも特に初期破壊強度特性を改良しやすく、高い信頼性を得ることができる代表例として、緻密質なSiCマトリックスを形成する反応焼結法が注目されている。
【0006】
ところで一方、上記のようなセラミックス基繊維複合材料においては、繊維の複合効果を発揮させるため、特にマトリックスと繊維との界面での結合状態を適正に制御することが極めて重要なテーマとなっている。繊維とセラミックスとが強固に結合すれば、ブリッジングやプルアウト等の複合効果が十分に発揮されず、脆性破壊しやすくなるためである。その対策として、繊維とマトリックスとの結合を弱めてマトリックスに対する繊維のすべりを発現させる窒化ホウ素(BN)等のすべり層を繊維表面にコーティングする方法が知られている。
【0007】
【発明が解決しようとする課題】
しかしながら、上述したすべり層は、反応焼結法を適用した場合にマトリックス形成材料との反応等により変質したり、分解、消失してしまうといった問題があった。例えば、セラミックスの繊維で形成したプリフォームに溶融Siを含浸させてSiCマトリックスを形成する反応焼結法を適用する場合には、含浸させられる溶融Siは反応性が高いため、すべり層や繊維自体と反応しやすく、その結果、上述した繊維の複合効果を十分に発揮させることができないといった不具合が生じることがあった。
【0008】
この発明は、このような従来の問題を考慮してなされたもので、緻密質なSiCマトリックスを形成する反応焼結法を適用し、このマトリックスと繊維との界面に形成する繊維コート層として少なくともすべり層が存在するものを対象とし、焼結時に反応性が高いSiと繊維又はすべり層との反応をより有効に抑制して、得られたマトリックス中に繊維及びすべり層を健全な状態で存在させることを、目的とする。
【0009】
【課題を解決するための手段】
上記目的を達成するため、本発明者は、マトリックス形成材料である反応性が高い溶融Siと繊維又はすべり層との反応抑制策について種々の研究を行ってきたところ、繊維を複合した成形体において乾燥収縮に伴って発生する亀裂を有効に防止するため、乾燥収縮がほぼ0のマトリックス組成としなければならない制約があり、そのためマトリックス中には強度や耐熱性等の面ではネックとなる焼結後の遊離Siを所定量含有することとなり、このことが反応焼結時の溶融Siと繊維等との接触機会を増やしている事実に着目した。溶融Siと繊維等との接触機会が増加することは、両者の間で反応がより進行しやすいことを意味する。
【0010】
このことから、得られたマトリックス中に所定量の遊離Siを含有しつつ、そのSiと繊維等との反応を有効に抑制する対策として、複合させる繊維に繊維束で構成された構造体を使用し、その繊維束の内部とその近傍とのマトリックス部分については、乾燥収縮に伴って発生する亀裂による強度劣化等の影響が繊維束の外部のマトリックス部分よりも少ないことから、乾燥収縮があっても残留する遊離Siが少なくなる組成として繊維等と溶融Siの接触機会を減らすことが有効であるとの考えに至った。
【0011】
即ち、本発明者は、繊維束の外部のマトリックス部分では遊離Siを所定量含有することを許容することにより、乾燥収縮に伴う亀裂発生による強度劣化を十分に防止できると共に、繊維束の内部とその近傍とのマトリックス部分で遊離Siを少ない組成とすることにより、反応焼結時に含浸させられる溶融Siと繊維等との反応を有効に抑制できるとの知見を得て、以下の発明を完成するに至った。
【0012】
この発明に係るセラミックス基繊維複合材料は、反応焼結で形成されたSiCを主相とするマトリックス及びこのマトリックス中に複合化させたセラミックスの繊維で成り、この繊維及びマトリックスの界面に少なくとも当該マトリックスに対して上記繊維のすべりを発現可能なすべり層が存在するセラミックス基繊維複合材料であって、上記繊維は、繊維束で構成された構造体で成り、上記マトリックスは、その遊離Si量は上記繊維束の内部とその近傍では16乃至18 vol %の範囲にあり、当該繊維束の外部においては21乃至26 vol% の範囲にあって、上記繊維束の内部とその近傍とで当該繊維束の外部よりも実質的に少ない組成を有することを特徴とする。
【0013】
前記マトリックスは、望ましくは前記繊維束の外部における遊離Si量が25体積%よりも小さい組成を有するものとする。繊維束の外部における遊離Si量が25体積%以上となると、SiCに対するSiの占める割合が増加して強度低下が見られるためである。
【0014】
前記マトリックスは、更に望ましくは前記繊維束の内部及びその近傍における遊離Si量をa(体積%)とし、上記繊維束の外部における遊離Si量をb(体積%)としたときに上記aに対するbの比率(b/a)が1.25以上の組成を有するものとする。このような遊離Si量でマトリックスの組成を調整すれば、上述した反応抑制効果をより確実に発揮させることができるためである。
【0015】
前記すべり層は、望ましくはB、N、Si、C、及びOの少なくとも1種を含む材料からなるものとする。例えば、すべりを発現可能な成分としてBN、C等が望ましく、またBN、C等の成分にSiC、SiO2 、Si3 N4 、非晶質成分(Si−C−N−O化合物)等を複合介在させて耐酸化性等の機能を分担させたものでもよい。
【0016】
上記のセラミックス基繊維複合材料は、以下の方法を用いて製造できる。
【0017】
即ち、この発明に係るセラミックス基繊維複合材料の製造方法は、セラミックスの繊維で構造体を形成し、この構造体にC成分を含む反応焼結用原料を含浸させ、その後に溶融Siを含浸させて上記C成分と溶融Siとの反応焼結を行わせることにより、SiCを主相とするマトリックス中に上記繊維を複合化させるセラミックス基繊維複合材料の製造方法であって、上記反応焼結後のマトリックス中の遊離Si量を制御する方法として、上記反応焼結前に上記マトリックス中のSi残留量に基づいて組成を予め調整した第1の反応焼結用原料を上記繊維を束ねた繊維束の内部とその近傍とに含浸させ、その後に上記第1の反応焼結用原料よりも上記Si残留量が多くなるように組成を予め調整した第2の反応焼結用原料を上記繊維束の外部に含浸させる方法を用いることを特徴とする。
【0018】
また、前記第1及び第2の反応焼結原料として、望ましくはSiC粉末、C粉末、セラミックスプリカーサ、及び樹脂の少なくとも1種を主成分としたスラリーを用いる。
【0019】
例えば、C粉末を含むスラリーを用いる場合には、例えば粒径(粒度特性)が異なる2種のC粉末を用意し、粒径が小さいC粉末を多く含むスラリーを第1の反応焼結用原料とし、粒径が大きいC粉末を多く含むスラリーを第2の反応焼結用原料とすればよい。
【0020】
また、セラミックスプリカーサ(セラミックス前駆体)を用いる場合には、ポリカルボシランとC粉末の混合物を第1の反応焼結用原料とし、ポリカルボシランとC粉末及びSiC粉末の混合物を第2の反応焼結用原料とすればよい。
【0021】
樹脂を用いる場合には、フェノール樹脂を第1の反応焼結用原料とし、フェノール樹脂とSiC粉末の混合物を第2の反応焼結用原料とすればよい。
【0022】
【発明の実施の形態】
以下、この発明に係るセラミックス基繊維複合材料およびその製造方法の実施形態を具体的に説明する。
【0023】
この実施形態では、繊維として直径14μmのSiC系セラミックス繊維(日本カーボン株式会社製、商品名:ハイニカロン)を500本、束ねてヤーンとした繊維束(500F/Y)で、そのモノフィラメントの表面にBNをコーティングして所定厚さのすべり層を形成したものを準備し、この繊維束から平織クロスを製織した。
【0024】
この平織クロスを第1のスラリー(スリップ)1に浸積して含浸させた。第1のスラリー1としては、中心粒径が30nm程度の粒状カーボン粉末(30wt%)に純水(65wt%)及び界面活性剤(5wt%)を混合したものを使用した。
【0025】
続いて、この平織クロスを乾燥後に積層してプリフォームとし、これを多孔質樹脂製成形型にセットして(繊維体積率(Vf=27%))、第2のスラリー
(スリップ)2を含浸させ、成形して乾燥させることにより、成形体を得た。ここで、第2のスラリー2としては、SiC粉末(70wt%)及び中心粒径が85nm程度の粒状カーボン粉末(30wt%)を固形分とし、この固形分(50wt%)に純水(47wt%)及び界面活性剤(3wt%)を混合したものを使用した。
【0026】
上記のように2種のスラリーを夫々分けて繊維束及びプリフォームに含浸させることにより、その含浸粉末の粒径分布及び組成に基づくC充填量に応じて、反応焼結で得られるマトリックス中のSi残留量を繊維束の内部(近傍を含む)と外部とで制御する方法を用いた。ここで、SiC粉末の充填部分を除く空隙単位体積当たりのC充填量が増加することは、溶融Siとの反応焼結時に未反応として残るSi量が少なくなることを意味する。
【0027】
そこで、上記のようにSi残留量を制御して作製した成形体をSi溶融金属 (純度99.9wt%)に接触させ、真空中で5hr、1430℃に加熱して溶融含浸させることにより、マトリックスに反応焼結SiCを合成させると共に、そのマトリックス中の遊離Si量が繊維束の内部とその近傍とで繊維束の外部よりも少ない組成をもつセラミックス基繊維複合材料を得た。
【0028】
従って、この複合材では、反応焼結時に反応性が高い溶融Siと繊維又はすべり層との反応が繊維束の内部とその近傍とでより有効に抑制されるため、すべり層及び繊維をマトリックス中により健全な状態で存在させることができる。
【0029】
次に、このセラミックス基繊維複合材料の特性を検証するため、マトリックス中の遊離Si量を変え、それ以外は上記と略同様の製造プロセスで複数のセラミックス基繊維複合材料を取得し、これらから所定サイズの試験片(「実施例1〜3」)を切り出して、下記の表1に示す各種試験を行った。
【0030】
以下、この実施形態のセラミックス基繊維複合材料の特性を表1に基づいて説明する。
【0031】
実施例1
実施例1は、表1に示すように、得られた複合材の密度は3.0g/cm3 であり、マトリックス中の遊離Si量(以下、繊維束の内部とその近傍をaとし、繊維束の外部をbとする)については、aが16vol%、bが21vol%、両者の比率(b/a)は1.31であった。
【0032】
室温3点曲げ強度については、初期マトリックス破壊強度σ1が200MPa、最大強度σ2が490MPaであり、3点曲げ試験の荷重変位曲線に基づいて破壊エネルギーを調べたところ、有効破壊エネルギーγが6.9kJ/m2 であり、破壊は完全な破断まで一気に至らない複合材料特有の安定的な破壊挙動を示した。また、破面をSEM(走査電子顕微鏡)で観察したところ、単繊維1本1本の表面にBN層が均質に且つ健全に存在し、繊維の引き抜けが顕著であることが明瞭に確認された。
【0033】
実施例2
実施例2は、表1に示すように、得られた複合材の密度は3.0g/cm3 であり、マトリックス中の遊離Si量については、aが18vol%、bが21vol%、両者の比率(b/a)は1.17であった。
【0034】
室温3点曲げ強度については、σ1が210MPa、σ2が410MPaであり、有効破壊エネルギーγが5.8kJ/m2 であり、破壊は完全な破断まで一気に至らない複合材料特有の安定的な破壊挙動を示した。また、破面のSEM観察では、単繊維1本1本の表面にBN層が均質に且つ健全に存在し、繊維の引き抜けが顕著であることが明瞭に確認された。
【0035】
実施例3
実施例3は、表1に示すように、得られた複合材の密度は3.0g/cm3 であり、マトリックス中の遊離Si量については、aが17vol%、bが26vol%、両者の比率(b/a)は1.53であった。
【0036】
室温3点曲げ強度については、σ1が200MPa、σ2が440MPaであり、有効破壊エネルギーγが6.1kJ/m2 であり、破壊は完全な破断まで一気に至らない複合材料特有の安定的な破壊挙動を示した。また、破面のSEM観察では、単繊維1本1本の表面にBN層が均質に且つ健全に存在し、繊維の引き抜けが顕著であることが明瞭に確認された。
【0037】
比較例1
比較例1では、上記の第1のスラリーを使用せずに、プリフォームに第2のスラリーを含浸させ、その他については上記と略同様の製造プロセスでセラミックス基複合材料を取得し、この切り出し試験片に対して上記と同様の試験を行った。
【0038】
その結果、表1に示すように、得られた複合材の密度は3.0g/cm3 であり、マトリックス中の遊離Si量については、aが22vol%、bが21vol%で、両者の比率(b/a)は0.95であった。
【0039】
室温3点曲げ強度については、σ1が280MPa、σ2が290MPaであり、有効破壊エネルギーγについては3.6kJ/m2 と上記各実施例と比べて小さく、破断は一気に至るものではないものの、より脆性的な破壊挙動を示した。また、破面のSEM観察では、溶融Siとの反応によりBN層が一部の箇所で消失し、その消失箇所で繊維とマトリックスとが一体化した状況が明瞭に認められた。
【0040】
比較例2
比較例2では、bを26vol%とし、その他については上記比較例1と略同様の製造プロセスでセラミックス基複合材料を取得し、この切り出し試験片に対して試験を行った。その結果、表1に示すように、得られた複合材の密度は3.0g/cm3 であり、マトリックス中の遊離Si量については、aが26vol%、bが26vol%で、両者の比率(b/a)は1.00であった。
【0041】
室温3点曲げ強度については、σ1が290MPa、σ2が最大強度σ2 については脆性的で確認できず、有効破壊エネルギーγについては0.7kJ/m2 と上記各実施例と比べて小さく、破断は一気に至るものではないものの、より脆性的な破壊挙動を示した。また、破面のSEM観察では、上記比較例1と同様に溶融Siとの反応によりBN層が一部の箇所で消失し、その消失箇所で繊維とマトリックスとが一体化した状況が明瞭に認められた。
【0042】
【表1】
【0043】
なお、その他として、1):すべり層として、BNのほかにB、N、C、Si、Oの少なくとも1種の材料からなるものを用いた場合、2):製造方法として、セラミックスプリカーサを主成分としたスラリーを用いた場合と樹脂を主成分としたスラリーを用いた場合においても、上記と略同様の結果であった。
【0044】
【発明の効果】
以上説明したように、この発明によれば、マトリックスは、その遊離Si量が繊維束の内部とその近傍とで繊維束の外部よりも実質的に少ない組成を有しているため、反応焼結時に反応性が高い溶融Siと繊維又はすべり層との反応を繊維束の縁部近傍を含む内側でより有効に抑制でき、マトリックス中に繊維及びすべり層を健全な状態で存在させることができる。従って、耐酸化性に優れた緻密質な反応焼結SiCをマトリックスとするセラミックス基繊維複合材料を、繊維及び界面の特性を殆ど劣化させることなく取得できる。[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a ceramic matrix fiber composite material and a method for producing the same, and more particularly to improvement of a composite material using dense silicon carbide (SiC) formed by a reactive sintering method as a matrix.
[0002]
[Prior art]
Generally, ceramic sintered bodies are less susceptible to strength reduction to high temperatures, and have superior properties such as hardness, electrical insulation, wear resistance, corrosion resistance, and light weight compared to conventional metal materials. It is used in a wide range of fields as electronic materials and structural materials such as heavy electrical equipment parts, aircraft parts, automobile parts, electronic equipment, precision machine parts, and semiconductor device materials.
[0003]
However, this ceramic sintered body is weaker in tensile stress than compressive stress, and has a drawback of so-called brittleness in which fracture proceeds at a stretch under this tensile stress. Depending on the application target, it is necessary to increase toughness and increase fracture energy. Such attempts to improve brittleness are strongly demanded when applied to ceramic structural parts such as gas turbine parts, aircraft parts, automobile parts and the like, which require particularly high reliability in addition to heat resistance and high temperature strength.
[0004]
Therefore, in response to such a request, as a ceramic sintered body with improved fracture toughness value, fracture energy value, thermal shock resistance, etc., composite materials such as fibers, whiskers, plates and particles made of inorganic substances and metals are matrixed. The ceramic matrix composite material formed by dispersing and compounding in the spotlight has attracted attention, and this practical research has been energetically promoted in domestic and foreign research institutions. In particular, when a fiber is composited to make a ceramic-based fiber composite material, since the effect of improving the fracture resistance is great, its practical application is expected.
[0005]
Among these ceramic-based fiber composite materials, composite materials using SiC as a matrix as a high-temperature material are particularly in the spotlight. As an example of a method for synthesizing the SiC matrix of this composite material, taking into account the heat resistance of the fiber, the CVI method (Chemical Vapor Infiltration), PC (Precursor) method, reaction firing, which have a relatively low synthesis temperature, are considered. Among them, a reactive sintering method for forming a dense SiC matrix has attracted attention as a typical example in which the initial fracture strength characteristics can be easily improved and high reliability can be obtained.
[0006]
On the other hand, in the ceramic-based fiber composite material as described above, it is an extremely important theme to appropriately control the bonding state at the interface between the matrix and the fiber in order to exert the fiber composite effect. . This is because if the fiber and the ceramic are firmly bonded, the combined effects such as bridging and pullout are not sufficiently exhibited, and brittle fracture is likely to occur. As a countermeasure, a method of coating the fiber surface with a slip layer such as boron nitride (BN) that weakens the bond between the fiber and the matrix and causes the fiber to slide against the matrix is known.
[0007]
[Problems to be solved by the invention]
However, the above-described sliding layer has a problem that, when the reaction sintering method is applied, the slip layer is deteriorated due to a reaction with the matrix forming material or the like, or decomposes and disappears. For example, when applying a reactive sintering method in which a preform formed of ceramic fibers is impregnated with molten Si to form a SiC matrix, the impregnated molten Si is highly reactive, so the slip layer or the fiber itself As a result, there may be a problem that the above-mentioned combined effect of fibers cannot be sufficiently exhibited.
[0008]
The present invention has been made in view of such conventional problems, and applies a reaction sintering method for forming a dense SiC matrix, and at least as a fiber coat layer formed at the interface between the matrix and the fibers. Targeting the presence of slip layers, the reaction between Si, which is highly reactive during sintering, and the fiber or slip layer is more effectively suppressed, and the fibers and slip layers are present in a healthy state in the resulting matrix. The purpose is to make it.
[0009]
[Means for Solving the Problems]
In order to achieve the above-mentioned object, the present inventor has conducted various studies on a reaction suppression measure between molten Si having a high reactivity as a matrix forming material and a fiber or a sliding layer. In order to effectively prevent cracks caused by drying shrinkage, there is a restriction that the matrix composition must have almost zero drying shrinkage. Therefore, in the matrix after sintering, which becomes a bottleneck in terms of strength and heat resistance Attention was paid to the fact that this increased the chance of contact between molten Si and fibers during reaction sintering. An increase in the chance of contact between molten Si and fibers means that the reaction is more likely to proceed between the two.
[0010]
For this reason, a structure composed of fiber bundles for fibers to be combined is used as a measure for effectively suppressing the reaction between Si and fibers while containing a predetermined amount of free Si in the obtained matrix. However, the matrix portion between the inside and the vicinity of the fiber bundle has a drying shrinkage because the influence of the strength deterioration due to the cracks generated by the drying shrinkage is less than the matrix portion outside the fiber bundle. However, the present inventors have come up with the idea that it is effective to reduce the chance of contact between the fibers and the molten Si as a composition that reduces the residual free Si.
[0011]
That is, the present inventor can sufficiently prevent the deterioration of strength due to cracking due to drying shrinkage by allowing a predetermined amount of free Si to be contained in the matrix portion outside the fiber bundle, and the inside of the fiber bundle. Obtaining the knowledge that the reaction between molten Si impregnated at the time of reaction sintering and fibers, etc. can be effectively suppressed by making the composition of the free Si in the matrix portion in the vicinity thereof, and the following invention is completed. It came to.
[0012]
The ceramic-based fiber composite material according to the present invention comprises a matrix mainly composed of SiC formed by reactive sintering and ceramic fibers composited in the matrix, and at least the matrix is present at the interface between the fibers and the matrix. A ceramic-based fiber composite material in which a slip layer capable of expressing the slip of the fiber is present, wherein the fiber is a structure composed of fiber bundles, and the matrix has a free Si amount of is within the vicinity of the fiber bundle is in the range of 16 to 18 vol%, the outside of the fiber bundle in the range of 21 to 26 vol%, of the fiber bundle between the inside and the vicinity thereof of the fiber bundle It has a composition substantially smaller than that of the outside.
[0013]
The matrix desirably has a composition in which the amount of free Si outside the fiber bundle is smaller than 25% by volume. This is because when the amount of free Si outside the fiber bundle is 25% by volume or more, the ratio of Si to SiC increases and a decrease in strength is observed.
[0014]
More preferably, the matrix has a free b amount relative to a when the free Si amount inside and near the fiber bundle is a (volume%), and the free Si amount outside the fiber bundle is b (volume%). The ratio (b / a) of 1.25 shall be 1.25 or more. This is because the reaction suppression effect described above can be more reliably exhibited by adjusting the composition of the matrix with such an amount of free Si.
[0015]
The sliding layer is preferably made of a material containing at least one of B, N, Si, C, and O. For example, BN, C, etc. are desirable as components capable of developing slip, and SiC, SiO 2 , Si 3 N 4 , amorphous components (Si—C—N—O compounds), etc. are used as components such as BN, C, etc. A combination of functions such as oxidation resistance may be used in combination.
[0016]
The ceramic-based fiber composite material can be manufactured using the following method.
[0017]
That is, in the method for producing a ceramic-based fiber composite material according to the present invention, a structure is formed with ceramic fibers, the structure is impregnated with a raw material for reactive sintering containing a C component, and then molten Si is impregnated. A method for producing a ceramic-based fiber composite material in which the fibers are combined in a matrix having SiC as a main phase by causing reaction sintering of the C component and molten Si, and after the reaction sintering As a method for controlling the amount of free Si in the matrix, a fiber bundle obtained by bundling the first reactive sintering raw material whose composition is adjusted in advance based on the residual amount of Si in the matrix before the reaction sintering. Then, the second reactive sintering raw material whose composition is adjusted in advance so that the residual amount of Si is larger than that of the first reactive sintering raw material is impregnated in and near the inside of the fiber bundle. Outside Characterized by using the method of impregnating.
[0018]
Further, as the first and second reaction sintering raw materials, preferably, a slurry mainly containing at least one of SiC powder, C powder, ceramic precursor, and resin is used.
[0019]
For example, when a slurry containing C powder is used, for example, two types of C powder having different particle sizes (particle size characteristics) are prepared, and a slurry containing a large amount of C powder having a small particle size is used as the first reaction sintering raw material. A slurry containing a large amount of C powder having a large particle size may be used as the second reaction sintering raw material.
[0020]
When a ceramic precursor (ceramic precursor) is used, a mixture of polycarbosilane and C powder is used as a first reaction sintering raw material, and a mixture of polycarbosilane, C powder and SiC powder is used as a second reaction. A raw material for sintering may be used.
[0021]
When the resin is used, the phenol resin may be used as the first reaction sintering material, and the mixture of the phenol resin and SiC powder may be used as the second reaction sintering material.
[0022]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, embodiments of the ceramic-based fiber composite material and the manufacturing method thereof according to the present invention will be specifically described.
[0023]
In this embodiment, a fiber bundle (500 F / Y) of 500 SiC-ceramic fibers (manufactured by Nippon Carbon Co., Ltd., trade name: Hynicalon) having a diameter of 14 μm is used as the fiber, and BN is formed on the surface of the monofilament. Was prepared by forming a sliding layer having a predetermined thickness, and a plain woven cloth was woven from this fiber bundle.
[0024]
This plain weave cloth was immersed in the first slurry (slip) 1 and impregnated. As the first slurry 1, a mixture of granular carbon powder (30 wt%) having a center particle diameter of about 30 nm and pure water (65 wt%) and a surfactant (5 wt%) was used.
[0025]
Subsequently, the plain woven cloth is dried and laminated to form a preform, which is set in a porous resin mold (fiber volume ratio (Vf = 27%)) and impregnated with the second slurry (slip) 2. , Molded and dried to obtain a molded body. Here, as the second slurry 2, SiC powder (70 wt%) and granular carbon powder (30 wt%) having a central particle size of about 85 nm are used as solid contents, and pure water (47 wt%) is added to the solid contents (50 wt%). ) And a surfactant (3 wt%) were used.
[0026]
As described above, the two types of slurry are separately impregnated into the fiber bundle and the preform, so that depending on the C filling amount based on the particle size distribution and composition of the impregnated powder, A method of controlling the residual amount of Si between the inside (including the vicinity) and outside of the fiber bundle was used. Here, an increase in the C filling amount per unit volume of the void excluding the filling portion of the SiC powder means that the amount of Si remaining as unreacted during reaction sintering with molten Si is reduced.
[0027]
Therefore, the molded body produced by controlling the amount of residual Si as described above is brought into contact with Si molten metal (purity 99.9 wt%), heated to 1430 ° C. in vacuum for 5 hours, and melt impregnated to form a matrix. Then, a sintered ceramic composite material having a composition in which the amount of free Si in the matrix is less in the inside and in the vicinity of the fiber bundle than in the outside of the fiber bundle was obtained.
[0028]
Therefore, in this composite material, the reaction between the molten Si, which has high reactivity during reaction sintering, and the fiber or the slip layer is more effectively suppressed in and near the fiber bundle. It can exist in a healthy state.
[0029]
Next, in order to verify the characteristics of this ceramic matrix fiber composite material, the amount of free Si in the matrix is changed, and other than that, a plurality of ceramic matrix fiber composite materials are obtained by a manufacturing process substantially the same as described above. A test piece of size (“Examples 1 to 3”) was cut out and subjected to various tests shown in Table 1 below.
[0030]
Hereinafter, the characteristics of the ceramic-based fiber composite material of this embodiment will be described based on Table 1.
[0031]
Example 1
In Example 1, as shown in Table 1, the density of the obtained composite material is 3.0 g / cm 3 , the amount of free Si in the matrix (hereinafter, the inside and the vicinity of the fiber bundle is a, As for b), a was 16 vol%, b was 21 vol%, and the ratio (b / a) between them was 1.31.
[0032]
As for the room temperature three-point bending strength, the initial matrix breaking strength σ1 is 200 MPa and the maximum strength σ2 is 490 MPa. When the breaking energy is examined based on the load displacement curve of the three-point bending test, the effective breaking energy γ is 6.9 kJ. / M 2 , and the fracture showed a stable fracture behavior peculiar to a composite material that does not reach a complete fracture at a stretch. Further, when the fracture surface was observed with an SEM (scanning electron microscope), it was clearly confirmed that the BN layer was present uniformly and soundly on the surface of each single fiber, and the fiber pullout was remarkable. It was.
[0033]
Example 2
In Example 2, as shown in Table 1, the density of the obtained composite material was 3.0 g / cm 3. Regarding the amount of free Si in the matrix, a was 18 vol%, b was 21 vol%, both The ratio (b / a) was 1.17.
[0034]
As for the room temperature three-point bending strength, σ1 is 210 MPa, σ2 is 410 MPa, the effective fracture energy γ is 5.8 kJ / m 2 , and the fracture does not reach a complete fracture at all. showed that. Further, SEM observation of the fracture surface clearly confirmed that the BN layer was present uniformly and soundly on the surface of each single fiber, and that the pull-out of the fiber was remarkable.
[0035]
Example 3
In Example 3, as shown in Table 1, the density of the obtained composite material is 3.0 g / cm 3. Regarding the amount of free Si in the matrix, a is 17 vol%, b is 26 vol%, both The ratio (b / a) was 1.53.
[0036]
As for the room temperature three-point bending strength, σ1 is 200 MPa, σ2 is 440 MPa, the effective fracture energy γ is 6.1 kJ / m 2 , and the fracture does not reach a complete fracture at all. showed that. Further, SEM observation of the fracture surface clearly confirmed that the BN layer was present uniformly and soundly on the surface of each single fiber, and that the pull-out of the fiber was remarkable.
[0037]
Comparative Example 1
In Comparative Example 1, the preform was impregnated with the second slurry without using the first slurry, and the ceramic matrix composite material was obtained by a manufacturing process substantially similar to the above for the others. A test similar to the above was performed on the piece.
[0038]
As a result, as shown in Table 1, the density of the obtained composite material was 3.0 g / cm 3 , and the amount of free Si in the matrix was 22 vol% for a and 21 vol% for b, and the ratio of both (B / a) was 0.95.
[0039]
As for the room temperature three-point bending strength, σ1 is 280 MPa, σ2 is 290 MPa, and the effective fracture energy γ is 3.6 kJ / m 2 , which is smaller than those in each of the above examples. It showed brittle fracture behavior. Further, in the SEM observation of the fracture surface, it was clearly recognized that the BN layer disappeared at some locations due to the reaction with molten Si, and the fibers and the matrix were integrated at the disappeared locations.
[0040]
Comparative Example 2
In Comparative Example 2, b was set to 26 vol%, and the others were obtained by a manufacturing process substantially similar to that of Comparative Example 1 above, and a test was performed on this cut-out specimen. As a result, as shown in Table 1, the density of the obtained composite material was 3.0 g / cm 3 , and the amount of free Si in the matrix was 26 vol% for a and 26 vol% for b, and the ratio of the two (B / a) was 1.00.
[0041]
Regarding the room temperature three-point bending strength, σ1 is 290 MPa and σ2 is brittle when the maximum strength σ 2 is brittle, and the effective fracture energy γ is 0.7 kJ / m 2 , which is small compared to the above examples, Although not at a stretch, it showed more brittle fracture behavior. Further, in the SEM observation of the fracture surface, the situation where the BN layer disappeared in some places due to the reaction with molten Si in the same manner as in Comparative Example 1 above, and the situation where the fibers and the matrix were integrated at the disappeared places was clearly recognized. It was.
[0042]
[Table 1]
[0043]
In addition, 1): In the case of using at least one material of B, N, C, Si, O in addition to BN as the sliding layer, 2): The ceramic precursor is mainly used as the manufacturing method. The results were almost the same as above when the slurry as the component was used and when the slurry containing the resin as the main component was used.
[0044]
【The invention's effect】
As described above, according to the present invention, the matrix has a composition in which the amount of free Si is substantially less in the inside and in the vicinity of the fiber bundle than in the outside of the fiber bundle. At times, the reaction between molten Si having high reactivity and the fiber or the slip layer can be more effectively suppressed on the inside including the vicinity of the edge of the fiber bundle, and the fiber and the slip layer can be present in a healthy state in the matrix. Therefore, it is possible to obtain a ceramic-based fiber composite material having a dense reaction-sintered SiC excellent in oxidation resistance as a matrix without substantially deteriorating the properties of the fiber and the interface.
Claims (6)
この繊維及びマトリックスの界面に少なくとも当該マトリックスに対して上記繊維のすべりを発現可能なすべり層が存在するセラミックス基繊維複合材料であって、
上記繊維は、繊維束で構成された構造体で成り、
上記マトリックスは、その遊離Si量は上記繊維束の内部とその近傍では16乃至18 vol %の範囲にあり、当該繊維束の外部においては21乃至26 vol% の範囲にあって、
上記繊維束の内部とその近傍とで当該繊維束の外部よりも実質的に少ない組成を有することを特徴とするセラミックス基繊維複合材料。It consists of a matrix mainly composed of SiC formed by reactive sintering and ceramic fibers compounded in this matrix.
A ceramic-based fiber composite material in which a slip layer capable of expressing at least the slip of the fiber with respect to the matrix exists at the interface between the fiber and the matrix,
The fiber is a structure composed of fiber bundles,
The amount of free Si in the matrix is in the range of 16 to 18 vol % inside and in the vicinity of the fiber bundle, and in the range of 21 to 26 vol% outside the fiber bundle ,
A ceramic-based fiber composite material characterized in that the inside and the vicinity of the fiber bundle have substantially less composition than the outside of the fiber bundle.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
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| JP21882696A JP3756583B2 (en) | 1996-08-20 | 1996-08-20 | Ceramic-based fiber composite material and manufacturing method thereof |
| US08/914,245 US6235379B1 (en) | 1996-08-20 | 1997-08-19 | Ceramic matrix composite and method of manufacturing the same |
| EP19970114371 EP0825163B1 (en) | 1996-08-20 | 1997-08-20 | Ceramic matrix composite and method of manufacturing the same |
| DE69703471T DE69703471T2 (en) | 1996-08-20 | 1997-08-20 | Ceramic matrix composite and method for producing the same |
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| JP21882696A JP3756583B2 (en) | 1996-08-20 | 1996-08-20 | Ceramic-based fiber composite material and manufacturing method thereof |
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| JP3756583B2 true JP3756583B2 (en) | 2006-03-15 |
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