JP2000026170A - Ceramic composite material - Google Patents

Ceramic composite material

Info

Publication number
JP2000026170A
JP2000026170A JP10191417A JP19141798A JP2000026170A JP 2000026170 A JP2000026170 A JP 2000026170A JP 10191417 A JP10191417 A JP 10191417A JP 19141798 A JP19141798 A JP 19141798A JP 2000026170 A JP2000026170 A JP 2000026170A
Authority
JP
Japan
Prior art keywords
yarn
composite material
ceramic composite
reinforcing
ceramic
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP10191417A
Other languages
Japanese (ja)
Other versions
JP2000026170A5 (en
Inventor
Takeshi Nakamura
武志 中村
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Corp
Original Assignee
IHI Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by IHI Corp filed Critical IHI Corp
Priority to JP10191417A priority Critical patent/JP2000026170A/en
Publication of JP2000026170A publication Critical patent/JP2000026170A/en
Publication of JP2000026170A5 publication Critical patent/JP2000026170A5/ja
Pending legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To obtain a ceramic composite material having high strength and airtightness without forming a porous part that causes defects. SOLUTION: The reinforcing material forming body of the ceramic composite material 1 comprises a three-dimensional rectangular solid formed by laminating two-dimensional fabrics 11 woven from yarn obtd. by twisting ceramic fibers in the Z-axis direction. In each two-dimensional fabric 11C disposed at the central part of the solid, both the warp 10B and the woof 10H are close woven at the central part and are loosen toward the edges. In the upper two-dimensional fabric 11U and the lower two-dimensional fabric 11L, the warp 10B and the woof 10H are loosely woven all over the entire surface.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、セラミックス母材
をセラミックス繊維織物による補強材によって補強して
成るセラミックス複合材料に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a ceramic composite material obtained by reinforcing a ceramic base material with a reinforcing material made of a ceramic fiber fabric.

【0002】[0002]

【従来の技術】セラミックス母材をセラミックス繊維を
撚り合わせて成る糸を製織して成る補強材によって補強
して成るセラミックス複合材料(CMC:Ceramic Matr
ix Composites)を製造する方法として、ポリマー含浸
焼成法:PIP(Polymer Impregnation and Pirolysis)
と、気相含浸法:CVI(Chemical Vapor Infiltratio
n)が知られている。
2. Description of the Related Art A ceramic composite material (CMC) formed by reinforcing a ceramic base material with a reinforcing material formed by weaving a yarn formed by twisting ceramic fibers.
ix Composites) is manufactured by polymer impregnation and firing method: PIP (Polymer Impregnation and Pirolysis).
And gas phase impregnation method: CVI (Chemical Vapor Infiltratio)
n) is known.

【0003】ポリマー含浸焼成法は、例えばポリカルボ
シラン等の有機ケイ素ポリマーをキシレン等の溶媒に溶
解させて成る溶液に、セラミックス繊維製の補強材を浸
してその織糸間にポリマーを含浸させ、乾燥させた後、
高温で焼成して炭化ケイ素の母材を成形するものであ
る。
In the polymer impregnation firing method, for example, a reinforcing material made of ceramic fibers is immersed in a solution obtained by dissolving an organosilicon polymer such as polycarbosilane in a solvent such as xylene to impregnate the polymer between the woven yarns. After drying,
It is to be fired at a high temperature to form a silicon carbide base material.

【0004】また、気相含浸法は、補強材であるセラミ
ックス繊維による織物を炉内で高温に加熱し、減圧雰囲
気にて炭化ケイ素の母材を形成するものである。例えば
炭化ケイ素の析出には、メチルトリクロロシランガスの
熱分解等を用いている。
[0004] In the gas phase impregnation method, a fabric made of ceramic fibers as a reinforcing material is heated to a high temperature in a furnace, and a silicon carbide base material is formed in a reduced pressure atmosphere. For example, thermal decomposition of methyltrichlorosilane gas is used for the deposition of silicon carbide.

【0005】[0005]

【発明が解決しようとする課題】しかしながら、上記の
ごとき方法によって形成されるセラミックス複合材料で
は、強度や気密性の向上を目的として補強材の織糸間隔
を狭く密に形成すると、母材の含浸性が悪化して内部に
母相の形成されない気孔部を残すという問題がある。こ
のような気孔部は、使用中に欠陥発生を誘発する虞を有
する。
However, in the case of the ceramic composite material formed by the above-described method, if the reinforcing material is formed with a narrow and dense yarn interval for the purpose of improving the strength and airtightness, the impregnation of the base material is prevented. However, there is a problem that pores in which a parent phase is not formed remain inside due to deterioration of properties. Such pores may cause defects during use.

【0006】本発明は、上記問題に鑑みてなされたもの
であって、欠陥を誘発する気孔部の形成がなく強度や気
密性の高いセラミックス複合材料を提供することを目的
とする。
SUMMARY OF THE INVENTION The present invention has been made in view of the above problems, and has as its object to provide a ceramic composite material having high strength and airtightness without formation of pores which induce defects.

【0007】[0007]

【課題を解決する為の手段】上記目的を達成する本発明
のセラミックス複合材料は、セラミックス母材をセラミ
ックス繊維織物による補強材によって補強して成るセラ
ミックス複合材料において、前記補強材の織糸間隔が、
気密性を要する部位は密に、その他の部位は粗く設定さ
れていることを特徴とする。
A ceramic composite material according to the present invention, which achieves the above object, is a ceramic composite material comprising a ceramic base material reinforced by a reinforcing material made of a ceramic fiber woven fabric, wherein the yarn spacing of the reinforcing material is reduced. ,
It is characterized in that the parts requiring airtightness are set densely and the other parts are set roughly.

【0008】また、セラミックス母材をセラミックス繊
維織物による補強材によって補強して成るセラミックス
複合材料において、前記補強材の織糸間隔が、内部は密
に、外面側は粗く設定されていることを特徴とする。
Further, in a ceramic composite material obtained by reinforcing a ceramic base material with a reinforcing material made of a ceramic fiber fabric, the yarn spacing of the reinforcing material is set densely on the inside and coarse on the outer surface. And

【0009】更に、上記構成に加え、その補強材は、少
なくとも一方向の織糸の太さが上記織糸間隔に対応して
織糸間隔が粗い部位では太く設定されていることを特徴
とする。
Further, in addition to the above configuration, the reinforcing member is characterized in that the thickness of the yarn in at least one direction is set to be thick at a portion where the yarn interval is coarse, corresponding to the yarn interval. .

【0010】また、セラミックス母材をセラミックス繊
維織物による補強材によって補強して円筒状に形成され
るセラミックス複合材料において、前記補強材はブレー
ド織りによって肉厚方向に多重に形成され、その織糸の
間隔が、内周面側は密に、外周面側は粗く設定されてい
ることを特徴とする。
In a ceramic composite material which is formed in a cylindrical shape by reinforcing a ceramic base material with a reinforcing material made of a ceramic fiber woven fabric, the reinforcing material is formed in multiple layers in the thickness direction by blade weaving. The interval is set densely on the inner peripheral surface side and coarsely set on the outer peripheral surface side.

【0011】また、上記織糸の太さはその間隔の粗密に
対応し、当該織糸間隔が粗い部位では太く設定されてい
ることを特徴とする。
The thickness of the yarn corresponds to the density of the yarn, and the yarn is set to be thick at a portion where the yarn is coarse.

【0012】[0012]

【発明の実施の形態】以下、添付図面を参照して本願発
明の実施の形態について説明する。図1は、本願発明に
係るセラミックス複合材の一構成例におけるセラミック
ス繊維織物による補強材としての補強材成形体10を概
念的に示す斜視図である。尚、本構成例は三次元織りの
例であるが、二次元織りである積層材や儒子織り材に適
用可能なものである。
Embodiments of the present invention will be described below with reference to the accompanying drawings. FIG. 1 is a perspective view conceptually showing a reinforcing material molded body 10 as a reinforcing material made of a ceramic fiber fabric in one configuration example of the ceramic composite material according to the present invention. Note that this configuration example is an example of three-dimensional weaving, but can be applied to a laminated material or two-dimensional weaving material that is two-dimensional weaving.

【0013】図示補強材形成体10は、炭化ケイ素等の
セラミックス繊維を撚り合わせて成る糸を平織りした
(織糸がX軸及びY軸方向に直交配置された)布状の二
次元織物11をZ軸方向に積層し、図示しない高さ方向
の織糸で結合して三次元立体(直方体)に形成されてい
る。このような補強材成形体10の織糸間空隙にポリマ
ー含浸焼成法(PIP)又は気相含浸法(CVI)によ
って炭化ケイ素等のセラミックス母材を含浸させて母相
を形成し、ダイヤモンド砥石等によって外形を所定形状
に加工して完成されたセラミックス複合材1を得るもの
である。
The illustrated reinforcing material forming body 10 is made of a cloth-shaped two-dimensional woven fabric 11 in which yarns formed by twisting ceramic fibers such as silicon carbide are plain-woven (woven yarns are arranged orthogonally in the X-axis and Y-axis directions). The layers are stacked in the Z-axis direction and connected by a weaving thread (not shown) in the height direction to form a three-dimensional solid (a rectangular parallelepiped). A matrix is formed by impregnating a ceramic base material such as silicon carbide into the voids between the yarns of the reinforcing material molded body 10 by a polymer impregnation firing method (PIP) or a gas phase impregnation method (CVI), and forming a diamond grindstone or the like. The outer shape is processed into a predetermined shape to obtain a completed ceramic composite material 1.

【0014】ここで、補強材成形体10のZ軸方向に積
層される各二次元織物11は、その経糸10Bと緯糸1
0Hの間隔がそのZ軸方向の位置に対応して異なってい
る。即ち、中央に配設された二次元織物11Cは、図2
(A)に示すように経糸10B及び緯糸10H共中央部
位が密で外縁側に行くに従って粗く形成され、上下の外
面に配設された二次元織物11U,11Lは、図2
(B)に示すように経糸10B及び緯糸10Hの間隔が
全面にわたって粗く形成されている。それらの中間に位
置する二次元織物11M…は、その経糸及び緯糸の織糸
間の間隔が両者の中間状態で漸次変化するように(中央
部が徐々に粗くなるように)形成されている。また、二
次元織物11のZ軸方向の配置は、その中央が密で上下
外面に至るほど粗くなるように設定されている。
Here, each two-dimensional fabric 11 laminated in the Z-axis direction of the reinforcing material molded body 10 has its warp 10B and weft 1
The interval of 0H differs according to the position in the Z-axis direction. That is, the two-dimensional fabric 11C disposed at the center is the same as that of FIG.
As shown in (A), the two-dimensional fabrics 11U and 11L in which the central portions of both the warp 10B and the weft 10H are denser and coarser toward the outer edge side and are disposed on the upper and lower outer surfaces are shown in FIG.
As shown in (B), the interval between the warp yarn 10B and the weft yarn 10H is formed coarsely over the entire surface. The two-dimensional woven fabrics 11M... Located between them are formed such that the interval between the warp yarns and the weft yarns gradually changes in an intermediate state between the two (so that the central portion gradually becomes coarser). Further, the arrangement of the two-dimensional fabric 11 in the Z-axis direction is set such that the center thereof is dense and the two-dimensional fabric 11 is roughened toward the upper and lower outer surfaces.

【0015】而して、上記のごとく構成された補強材成
形体10では、織糸の配置は、X,Y,Z軸の何れの方
向においても織糸が中心部が密で外周面側程粗くなって
いる。このため、織糸間の隙間が外周面では大きく中心
部では小さくなっており、母材含浸の際には中央部の織
糸間の小さな空間から順次外周面側の大きな空間に母相
が形成されることとなり、内部に気孔部を残すことがな
く、残存する気孔に起因する欠陥を防ぐことができると
共に強度や気密性の高いセラミックス複合材1を得るこ
とができるものである。
Thus, in the reinforcing material molded body 10 configured as described above, the arrangement of the yarns is such that the center of the yarns is denser in any direction of the X, Y, and Z axes, and is closer to the outer peripheral surface. It is rough. For this reason, the gap between the yarns is large on the outer peripheral surface and small at the center, and when impregnating the base material, a matrix is formed in a small space between the yarns in the central portion and sequentially in a large space on the outer peripheral surface side. As a result, it is possible to prevent the defects caused by the remaining pores without leaving any pores inside, and to obtain the ceramic composite material 1 having high strength and high airtightness.

【0016】尚、上記構成例では、補強材成形体10は
平織りの二次元織物11を積層して形成されているが、
補強材成形体10の組織は平織りに限るものではなく、
また、粗密にする織糸は経糸と緯糸の何れか一方のみで
あっても良いものである。
In the above configuration example, the reinforcing material molded body 10 is formed by laminating two-dimensional plain woven fabrics 11.
The structure of the reinforcing material molded body 10 is not limited to plain weave,
Further, the woven yarn to be made dense and coarse may be only one of the warp and the weft.

【0017】更に、上記構成では、全ての二次元織物1
1を同一の太さ織糸を用いて形成した場合、織糸間隔の
粗い部位では補強材密度が小さくなるためにセラミック
ス複合材1の当該部位の強度が低下することとなるが、
これは織糸の径を部位毎で変化させる(即ち織糸間隔の
粗い部位では織糸の径を太くする)ことで解消できる。
つまり、織糸の間隔が粗く織糸密度が小さい部位では当
該織糸を形成する繊維数を増やして(織糸を太くして)
繊維密度を高めることで、セラミックス複合材1全体の
強度の一定化が可能となるものである。
Further, in the above configuration, all the two-dimensional fabrics 1
When 1 is formed by using the same thickness woven yarn, the strength of the ceramic composite material 1 is reduced at a portion where the yarn spacing is coarse because the reinforcing material density is low,
This can be solved by changing the diameter of the yarn at each portion (that is, increasing the diameter of the yarn at a portion where the yarn interval is coarse).
In other words, in a portion where the yarn interval is coarse and the yarn density is low, the number of fibers forming the yarn is increased (the yarn is made thicker).
By increasing the fiber density, the strength of the entire ceramic composite material 1 can be made constant.

【0018】図3は、上記と異なる構成例のセラミック
ス複合材の補強材成形体を概念的に示す斜視図であり、
図示補強材成形体10′は、その下面側に高い気密性を
求められるセラミックス複合材1′の例である。
FIG. 3 is a perspective view conceptually showing a reinforcing material molded body of a ceramic composite material having a configuration example different from the above.
The illustrated reinforcing material molded body 10 'is an example of a ceramic composite material 1' which requires high airtightness on the lower surface side.

【0019】補強材成形体10′は、上記構成例と同様
に、炭化ケイ素等のセラミックス繊維を撚り合わせて成
る糸を平織りした二次元織物11′をZ軸方向に積層す
ると共に図示しない高さ方向の織糸で結合して三次元立
体(直方体)に形成されている。
The reinforcing material molded body 10 'is formed by laminating a two-dimensional woven fabric 11' formed by plain weaving a yarn formed by twisting ceramic fibers such as silicon carbide in the Z-axis direction and having a height (not shown), as in the above configuration example. It is formed into a three-dimensional solid (rectangular parallelepiped) by binding with the weaving yarns in the directions.

【0020】その下面側に位置する二次元織物11L′
は、図4(A)に示すように経糸及び緯糸の両方共密に
形成され、上面側に位置する二次元織物11U′は、図
4(B)に示すように経糸10B及び緯糸10Hの両方
共粗く形成され、それらの中間に位置する二次元織物1
1M′は、その経糸10B及び緯糸10Hの織糸間の間
隔が両者の中間状態で漸次変化するように形成されてい
る。また、各二次元織物11′のz軸方向の配設間隔は
上面側程粗く配置されているものである。更に、各二次
元織物11′の織糸の太さ(補強繊維数)はその織糸間
間隔の粗密に対応して、組織が密なものは細く、組織が
粗いものは太く(補強繊維量が多く)、単位体積当たり
の補強繊維量が一定となるように設定されている。
The two-dimensional woven fabric 11L 'located on the lower surface side
4A, both the warp and the weft are formed densely as shown in FIG. 4 (A), and the two-dimensional woven fabric 11U ′ located on the upper surface side has both the warp 10B and the weft 10H as shown in FIG. 4 (B). Two-dimensional fabric 1 which is formed coarsely and is located between them
1M 'is formed such that the spacing between the warp yarns of the warp yarn 10B and the weft yarn 10H gradually changes in an intermediate state between them. Further, the arrangement intervals in the z-axis direction of the two-dimensional fabrics 11 'are arranged to be coarser toward the upper surface side. Furthermore, the thickness (the number of reinforcing fibers) of the yarns of each two-dimensional woven fabric 11 'corresponds to the density of the inter-woven yarns. ), And the amount of reinforcing fibers per unit volume is set to be constant.

【0021】上記のごとく構成された補強材成形体1
1′では、母材含浸の際に、密な二次元織物11L′が
配設されている下面側には初期に母相が形成されて当該
下面側からの母材の含浸はなくなるが、粗い二次元織物
11U′が配設された上面側から母材が含浸し、全体に
母相が形成されたセラミックス複合材1′を得ることが
できる。これにより、下面側は平滑で気密性が高く、そ
の単位体積当たりの補強繊維量は各部位において等しい
ため、強度も一定のセラミックス複合材1′を構成でき
るものである。尚、経糸及び緯糸が密に形成された面
(二次元織物11L′)は、下面に限らず高さ方向の何
れの位置に設けてもかまわないものである。
Reinforcement molding 1 constructed as described above
In 1 ', when the base material is impregnated, a matrix phase is initially formed on the lower surface side where the dense two-dimensional fabric 11L' is disposed, and the base material is not impregnated from the lower surface side, but is coarse. The base material is impregnated from the upper surface side on which the two-dimensional fabric 11U 'is disposed, and the ceramic composite material 1' in which the base phase is formed as a whole can be obtained. Thereby, the lower surface side is smooth and highly airtight, and the amount of reinforcing fibers per unit volume is equal in each part, so that the ceramic composite material 1 'having a constant strength can be constituted. The surface on which the warp and the weft are densely formed (the two-dimensional fabric 11L ') is not limited to the lower surface and may be provided at any position in the height direction.

【0022】図5は、内周面に平滑で高い気密性が求め
られる円筒状のセラミックス複合材2を形成する構成例
の補強材形成体の横断面図を示す。
FIG. 5 is a cross-sectional view of a reinforcing material forming body of a configuration example in which a cylindrical ceramic composite material 2 requiring smooth and high airtightness on the inner peripheral surface is formed.

【0023】図示補強材形成体20は、図6に概念的に
示すように、周方向に複数配設された軸方向に延びる中
央糸21に対して左右の組み糸22が互いに逆勾配に斜
めに織られて成るブレード織りによる組織が、同心状に
二重に設けられて(内周側組織20A及び外周側組織2
0B)形成されているものである。
As shown conceptually in FIG. 6, the illustrated reinforcing material forming body 20 has left and right braided yarns 22 obliquely inclined in opposite directions with respect to a plurality of axially extending central yarns 21 arranged in the circumferential direction. The tissue by blade weaving that is woven in two is provided concentrically and double (the inner peripheral tissue 20A and the outer peripheral tissue 2A).
0B) is formed.

【0024】組み糸22の太さは、内周側組織20Aと
外周側組織20Bで等しく、これに対し、内周側組織2
0Aの中央糸21Aは細く密に配設され、外周側組織2
0Bの中央糸21Bは太く周方向に粗く配設されてい
る。即ち、中央糸21の太さ(補強繊維数)はその周方
向の粗密に対応しており、密な内周側組織20Aでは細
く補強繊維量が少なく)、粗い外周側組織20Bでは太
く(補強繊維量が多く)、単位体積当たりの補強繊維量
が一定となるように設定されている。
The thickness of the braided yarn 22 is equal in the inner circumferential side structure 20A and the outer circumferential side structure 20B.
0A central thread 21A is arranged finely and densely,
The central thread 21B of 0B is thickly and coarsely arranged in the circumferential direction. That is, the thickness (the number of reinforcing fibers) of the center yarn 21 corresponds to the density in the circumferential direction, and is thin (the reinforcing fiber amount is small in the dense inner peripheral structure 20A) and thick (reinforcement) in the coarse outer structure 20B. (The amount of fibers is large) and the amount of reinforcing fibers per unit volume is set to be constant.

【0025】上記のごとく形成された補強材形成体20
では、母材含浸の際に、中央糸21Aが密な内周側組織
20Aには初期に母相が形成されて内周側からの母材の
含浸はなくなるが、中央糸21Bが粗い外周側(外周側
組織20Bの側)から母材が含浸し、全体に母相が形成
された円筒状のセラミックス複合材2を得ることができ
る。これにより、内周面側は平滑で気密性が高く、その
単位体積当たりの補強繊維量は各部位において等しく強
度一定のセラミックス複合材2を構成できるものであ
る。
The reinforcing member formed body 20 formed as described above
Then, when the base material is impregnated, a matrix phase is initially formed in the inner circumferential side structure 20A where the central yarn 21A is dense, and the base material is not impregnated from the inner circumferential side. The base material is impregnated with the base material from the (outer side structure 20B side), and the cylindrical ceramic composite material 2 in which the whole parent phase is formed can be obtained. Thereby, the inner peripheral surface side is smooth and has high airtightness, and the amount of reinforcing fibers per unit volume can form the ceramic composite material 2 having the same strength at each portion.

【0026】尚、本構成例は内周面側を平滑で高い気密
性を得るために内周側組織20Aの中央糸21Aを密に
配置したものであるが、必要によりこれとは逆に外周側
組織20Bの中央糸21Bを密に配置すれば外周面側を
平滑で高い気密性を得るように構成できる。また、上記
構成例はブレード織りの組織(内周側組織20A及び外
周側組織20B)を二重に重合したものであるが、これ
に限らず三重以上であっても良いものである。更に、円
筒状の補強材形成体の組織構造としては、ブレード織り
に限らず、例えば前述の構成例のように平織りの二次元
織物を積層したものを屈曲させて両端を接合することで
円筒状に形成しても良いものである。
In this embodiment, the central thread 21A of the inner side structure 20A is densely arranged in order to obtain a smooth and high air-tightness on the inner peripheral surface side. If the central thread 21B of the side structure 20B is densely arranged, the outer peripheral surface side can be configured to be smooth and highly airtight. In the above configuration example, the structure of the blade weave (the inner circumferential structure 20A and the outer circumferential structure 20B) is double-polymerized, but the present invention is not limited to this, and the structure may be triple or more. Further, the tissue structure of the cylindrical reinforcing material formed body is not limited to blade weave, for example, by bending a two-dimensional woven fabric of plain weave as in the above configuration example and joining both ends to form a cylindrical structure. It may be formed in the form.

【0027】[0027]

【発明の効果】以上述べたように、本願発明に係るセラ
ミックス複合材料によれば、補強材の織糸間隔が、気密
性を要する部位は密に、その他の部位は粗く設定されて
いることにより、母材の含浸が、織糸間隔が粗い部位を
介して密な部位に行われ、密な部位から粗い部位に進行
する。このため、織糸間隔が密な部位でも気孔を残すこ
となく強度や気密性の高いセラミックス複合材料と成し
得るものである。
As described above, according to the ceramic composite material according to the present invention, the space between the reinforcing yarns is set so that the portion requiring airtightness is set densely and the other portions are set coarse. Then, the impregnation of the base material is performed in the dense portion through the portion in which the yarn spacing is coarse, and progresses from the dense portion to the coarse portion. For this reason, a ceramic composite material having high strength and airtightness can be formed without leaving pores even in a portion where the yarn spacing is close.

【0028】また、補強材の織糸間隔が、内部は密に、
外面側は粗く設定されていることにより、外部から内部
への母材の含浸が容易となり、欠陥を誘発する気孔部の
残存のない強度や気密性の高いセラミックス複合材料と
成しを得るものである。
Further, the weaving yarn spacing of the reinforcing material is dense inside,
By setting the outer surface to be rough, it is easy to impregnate the base material from the outside to the inside, and it is possible to obtain a ceramic composite material with high strength and airtightness without residual pores that induce defects. is there.

【0029】また、補強材は、少なくとも一方向の織糸
の太さが織糸間隔に対応して織糸間隔が粗い部位では太
く設定されていることにより、単位体積当たりの補強繊
維量を各部位において等しく設定することが可能とな
り、全体の強度を一定に構成できるものである。
The reinforcing material has a thickness of the weaving yarn in at least one direction corresponding to the yarn spacing, and is set thick at a portion where the yarn spacing is coarse. The same strength can be set in each part, and the entire strength can be configured to be constant.

【0030】また、円筒状の補強材がブレード織りによ
って肉厚方向に多重に形成され、その織糸の間隔が、内
周面側は密に、外周面側は粗く設定されていることによ
り、母材の含浸が、織糸間隔が粗い外周面側を介して密
な内周面側に行われ、織糸間隔が密な内周面側でも気孔
のない気密的な母相が形成された円筒状のセラミックス
複合材料と成し得るものである。
Further, the cylindrical reinforcing material is formed in multiple layers in the thickness direction by blade weaving, and the spacing between the yarns is set densely on the inner peripheral surface side and coarsely on the outer peripheral surface side. The impregnation of the base material was performed on the dense inner peripheral surface side via the outer peripheral surface side where the weave yarn interval was coarse, and an airtight parent phase without pores was formed even on the inner peripheral surface side where the weave yarn interval was dense. It can be made of a cylindrical ceramic composite material.

【0031】また、織糸の太さはその間隔の粗密に対応
し、当該織糸間隔が粗い部位では太く設定されているこ
とにより、単位体積当たりの補強繊維量を各部位におい
て等しく設定することが可能となり、全体の強度を一定
に構成できるものである。
Further, the thickness of the weaving yarn corresponds to the density of the interval, and the amount of the reinforcing fiber per unit volume is set to be equal at each portion by setting the thickness at the portion where the interval between the yarns is coarse. And the strength of the whole can be made constant.

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

【図1】本願発明に係るセラミックス複合材の一構成例
における補強材成形体を概念的に示す斜視図である。
FIG. 1 is a perspective view conceptually showing a reinforcing material molded body in one configuration example of a ceramic composite material according to the present invention.

【図2】図1の補強材成形体を形成する二次元織物の平
面図であって、(A)は中央に配設された二次元織物,
(B)は上下の外面に配設された二次元織物である。
FIG. 2 is a plan view of a two-dimensional fabric forming the reinforcing material molded body of FIG. 1, wherein (A) is a two-dimensional fabric disposed in the center,
(B) is a two-dimensional woven fabric disposed on the upper and lower outer surfaces.

【図3】他の構成例における補強材成形体を概念的に示
す図である。
FIG. 3 is a view conceptually showing a reinforcing material molded body in another configuration example.

【図4】図1の補強材成形体を形成する二次元織物の平
面図であって、(A)は下面側に配設された二次元織
物,(B)は下面側に配設された二次元織物である。
FIGS. 4A and 4B are plan views of a two-dimensional fabric forming the reinforcing material molded body of FIG. 1, wherein FIG. 4A is a two-dimensional fabric disposed on the lower surface side, and FIG. It is a two-dimensional fabric.

【図5】円筒状のセラミックス複合材を形成する構成例
の補強材形成体の横断面図である。
FIG. 5 is a cross-sectional view of a reinforcing member forming body of a configuration example for forming a cylindrical ceramic composite material.

【図6】ブレード織りを説明する概念図である。FIG. 6 is a conceptual diagram illustrating blade weaving.

【符号の説明】[Explanation of symbols]

1 セラミックス複合材料 2 セラミックス複合材料 10 補強材成形体(補強材) 10B 経糸(織糸) 10H 緯糸(織糸) 10′ 補強材成形体(補強材) 20 補強材形成体(補強材) 21 中央糸(織糸) 22 組み糸(織糸) DESCRIPTION OF SYMBOLS 1 Ceramic composite material 2 Ceramic composite material 10 Reinforcement molding (reinforcement) 10B Warp (woven yarn) 10H Weft (woven yarn) 10 'Reinforcement molding (reinforcement) 20 Reinforcement formation (reinforcement) 21 Center Yarn (woven yarn) 22 Braided yarn (woven yarn)

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 セラミックス母材をセラミックス繊維織
物による補強材によって補強して成るセラミックス複合
材料において、 前記補強材の織糸間隔が、気密性を要する部位は密に、
その他の部位は粗く設定されていることを特徴とするセ
ラミックス複合材料。
1. A ceramic composite material obtained by reinforcing a ceramic base material with a reinforcing material made of a ceramic fiber woven fabric, wherein the yarn spacing of the reinforcing material is tight in a portion requiring airtightness,
A ceramic composite material characterized in that other parts are roughly set.
【請求項2】 セラミックス母材をセラミックス繊維織
物による補強材によって補強して成るセラミックス複合
材料において、 前記補強材の織糸間隔が、内部は密に、外面側は粗く設
定されていることを特徴とするセラミックス複合材料。
2. A ceramic composite material in which a ceramic base material is reinforced by a reinforcing material made of a ceramic fiber woven fabric, wherein the yarn spacing of the reinforcing material is set densely on the inside and coarse on the outer surface side. Ceramic composite material.
【請求項3】 上記補強材は、少なくとも一方向の織糸
の太さが上記織糸間隔に対応して織糸間隔が粗い部位で
は太く設定されてい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。
3. The reinforcing material according to claim 1, wherein the thickness of the weaving yarn in at least one direction is set to be thick at a portion where the yarn yarn interval is coarse, corresponding to the yarn yarn interval.
2. The ceramic composite material according to item 1.
【請求項4】 セラミックス母材をセラミックス繊維織
物による補強材によって補強して円筒状に形成されるセ
ラミックス複合材料において、 前記補強材はブレード織りによって肉厚方向に多重に形
成され、その織糸の間隔が、内周面側は密に、外周面側
は粗く設定されていることを特徴とするセラミックス複
合材料。
4. A ceramic composite material formed into a cylindrical shape by reinforcing a ceramic base material with a reinforcing material made of a ceramic fiber woven fabric, wherein the reinforcing material is formed in multiple layers in the thickness direction by blade weaving. A ceramic composite material, wherein the interval is set densely on the inner peripheral side and coarsely set on the outer peripheral side.
【請求項5】 上記織糸の太さはその間隔の粗密に対応
し、当該織糸間隔が粗い部位では太く設定されているこ
とを特徴とする請求項4に記載のセラミックス複合材
料。
5. The ceramic composite material according to claim 4, wherein the thickness of the yarn corresponds to the density of the yarn, and the yarn is set thick at a portion where the yarn is coarse.
JP10191417A 1998-07-07 1998-07-07 Ceramic composite material Pending JP2000026170A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10191417A JP2000026170A (en) 1998-07-07 1998-07-07 Ceramic composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10191417A JP2000026170A (en) 1998-07-07 1998-07-07 Ceramic composite material

Publications (2)

Publication Number Publication Date
JP2000026170A true JP2000026170A (en) 2000-01-25
JP2000026170A5 JP2000026170A5 (en) 2005-09-02

Family

ID=16274273

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10191417A Pending JP2000026170A (en) 1998-07-07 1998-07-07 Ceramic composite material

Country Status (1)

Country Link
JP (1) JP2000026170A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005201241A (en) * 2003-11-07 2005-07-28 General Electric Co <Ge> Method and device for deterring crack inside body

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005201241A (en) * 2003-11-07 2005-07-28 General Electric Co <Ge> Method and device for deterring crack inside body
JP4559191B2 (en) * 2003-11-07 2010-10-06 ゼネラル・エレクトリック・カンパニイ Method and apparatus for suppressing cracks inside the body

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