US20130184141A1

US20130184141A1 - Process for producing ceramic fiber-reinforced composite material and ceramic fiber-reinforced composite material

Info

Publication number: US20130184141A1
Application number: US13/743,293
Authority: US
Inventors: Toshio Ogasawara; Takuya Aoki; Masaki Kotani
Original assignee: Japan Aerospace Exploration Agency JAXA
Current assignee: Japan Aerospace Exploration Agency JAXA
Priority date: 2012-01-18
Filing date: 2013-01-16
Publication date: 2013-07-18
Also published as: EP2617694A1; US10597333B2; US20160145158A1; JP2013147366A; EP2617694B1; JP5916088B2

Abstract

To obtain a ceramic fiber-reinforced composite material, by melt-infiltrating a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals that belong to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, and having the silicon content ratio of 66.7 at % or more.

Description

BACKGROUND

1. Technical Field
The present invention relates to a process for producing a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix (base material) formed of an inorganic substance, with an infiltrating material, and can be used at a high temperature, and to a ceramic fiber-reinforced composite material.
2. Related Art
Generally, in ceramic fiber-reinforced composite materials, a special interface layer is required for an interface between ceramic fibers and a matrix so as to control the adhesion strength between the ceramic fibers and matrix, and interface layers of hexagonal boron nitride (h-BN) or carbon (c) are most frequently used.
However, oxidation by water vapor in a temperature range of 800 to 1,000° C. generates in boron nitride and oxidation by air in a temperature range of 800° C. or more generates in carbon, to thereby inhibit the high temperature properties of the ceramic fiber-reinforced composite material.
Furthermore, formation of a matrix in a ceramic fiber-reinforced composite material is conducted by a chemical vapor deposition process (CVD), a chemical vapor infiltration process (CVI), a ceramic precursor infiltration-pyrolysis process (PIP), a reactive sintering process (RS) or the like, but pores (voids) remain in either process.
For example, in the infiltration-pyrolysis process of a ceramic precursor, decrease of weight and volume generates in the process of forming a ceramic by heat decomposition of the precursor.
In the chemical vapor deposition process and chemical vapor infiltration process, the diffusion of reaction gas into the inside of a preform of ceramic fibers is inhibited according to the growth of a matrix, and thereby pores remain.
In the reactive sintering process, remaining of pores in accordance with the volumetric shrinkage during reactive sintering occurs.
Due to such phenomena, it is impossible to completely fill a matrix in a ceramic fiber-reinforced composite material, and generally, pores of at least several percent by volume to several ten percent by volume or more remain.
These pores become entry pathways for gases (air and water vapor) that oxidize the interface layer to thereby cause decrease of the adhesion strength between the ceramic fibers and matrix, and the residual pores themselves become one of the causes of the deterioration of the mechanistic properties of the ceramic fiber-reinforced composite material.
In order to solve these problems, for example, a technique including infiltrating pores of a ceramic-based composite material with glass to thereby suppress oxidation at an interface layer is known (see Japanese Patent Application Laid-Open (JP-A) No. 10-259070 and the like).
Furthermore, a technique including forming a silicon carbide matrix by a reactive sintering process by infiltrating a preform of ceramic fibers with a carbon powder, and melt-infiltrating the preform with metallic silicon, to thereby suppress the deterioration of an interface layer is known (see JP-A Nos. 10-59780, 11-263668 and the like).
Furthermore, a technique including obtaining a silicon carbide fibers/silicon-silicon carbide composite material by molding a molded article including silicon carbide fibers and silicon carbide particles by using metallic silicon as a binder to thereby suppress the deterioration of an interface layer and improve the mechanistic properties is known (see JP-A No. 10-167831 and the like).

SUMMARY

However, the technique known in the above-mentioned JP-A No. 10-259070 has a problem that, since the glass is chemically unstable in a temperature range of 1,000° C. or more, the material is deteriorated over time by use in that temperature range and thus has low durability.
Furthermore, the technique also has a problem that the material cannot be applied in a high temperature range over 1,300° C. since melting and vaporization of the glass generate.
The techniques known in the above-mentioned JP-A Nos. 10-59780 and 11-263668 have a problem that it is necessary to form a reaction protective layer by a chemical vapor deposition process (CVD process) or the like on the surface of the ceramic fibers so as to prevent the deterioration of the ceramic fibers and interface layer due to direct contact of the molten silicon with the ceramic fibers or interface layer during the production process, thereby the production steps become complex.
Furthermore, in melt infiltration of silicon, it is necessary to heat to a temperature equal to or more than 1,414° C. that is the melting point of silicon, generally to 1450° C. or more, but there is a problem that heat decomposition occurs in this temperature range in many ceramic fibers, and thus the strength of the ceramic fibers is significantly decreased.
For example, it is known that, when a heat treatment of amorphous silicon carbide (SiC) fibers, amorphous alumina fibers or the like, which are generally used as ceramic fibers, is conducted at a temperature equal to or more than the production temperature of these ceramic fibers, heat decomposition proceeds and the mechanistic properties are significantly inhibited.
Therefore, in the case when silicon is melt-infiltrated, there was a problem that special ceramic fibers that are excellent in chemical stability at a high temperature and extremely expensive (for example, Tyranno SA fibers (trade name: Ube Industries, Ltd.) and Hi-Nicalon Type S fibers (trade name: Nippon Carbon Co., Ltd.), which are crystalline silicon carbide fibers, and the like) may be used.
The technique known in the above-mentioned JP-A No. 10-167831 has a problem that the strength property of the composite material significantly decreases in a temperature range over 1,300° C. since the strength property significantly depends on the metallic silicon as a binder.
Therefore, the present invention aims at providing a ceramic fiber-reinforced composite material obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, which suppresses the deterioration of an interface layer, improves mechanistic properties and has excellent durability even under a high temperature, even general ceramic fibers are used, without complicating the production steps.
A first aspect of the invention solves the above-mentioned problem by providing a process for producing a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or apart of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material, wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon, and the process comprises melt-infiltrating the pores that are present in the composite material substrate with the infiltrating material under a temperature environment at a temperature equal to or more than the melting point of the alloy as the infiltrating material.
A second aspect of the invention solves the above-mentioned problem by providing the entirety or a part of the pores that are present in the composite material substrate with free carbon prior to the melt infiltration, and reacting the alloy as the infiltrating material and the free carbon in the pores during the melt infiltration to generate silicon carbide and a carbide of the transition metal, besides the constitution of the process for producing a ceramic fiber-reinforced composite material of the first aspect.
Third and fourth aspects of the invention solve the above-mentioned problem by that the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration, besides the constitutions of the processes for producing a ceramic fiber-reinforced composite material of the first and second aspects.
Fifth, sixth, seventh and eighth aspects of the invention solve the above-mentioned problem by that the above-mentioned ceramic fibers are silicon carbide fibers, besides the constitutions of the processes for producing a ceramic fiber-reinforced composite material of the first, second, third and fourth aspects.
A ninth aspect of the invention solves the above-mentioned problem by providing a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material, wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon.
A tenth aspect of the invention solves the above-mentioned problem by that silicon carbide and a carbide of the transition metal are present in interface regions between the pores and the infiltrating material, besides the constitution of the ceramic fiber-reinforced composite material of the ninth aspect.
Eleventh and twelfth aspects of the invention solve the above-mentioned problem by that the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration, besides the constitutions of the ceramic fiber-reinforced composite materials of the ninth and tenth aspects.
Thirteenth, fourteenth, fifteenth and sixteenth aspects of the invention solve the above-mentioned problem by that the above-mentioned ceramic fibers are silicon carbide fibers, besides the constitutions of the ceramic fiber-reinforced composite materials of the ninth, tenth, eleventh and twelfth aspects.
According to the process for producing a ceramic fiber-reinforced composite material of the first aspect and the ceramic fiber-reinforced composite material of the ninth aspect, the melting point of the alloy as the infiltrating material becomes lower than 1,414° C. that is the melting point of silicon, by adjusting the silicon content ratio (including the silicon in the transition metal disilicate) of the alloy to 66.7 at % or more, thereby the temperature of the alloy as the infiltrating material during the melt infiltration can be suppressed to be low during the melt infiltration treatment of the infiltrating material.
By this way, exposure of the ceramic fibers to a high temperature for a long time can be suppressed, and decrease in the strength and durability of the ceramic fibers by heat can also be suppressed without complicating the production steps, even general ceramic fibers are used, and thus a ceramic fiber-reinforced composite material having excellent durability even under a high temperature can be provided.
Furthermore, the alloy as the infiltrating material has a property that the melting point of the alloy simply decreases from 1,414° C. that is the melting point of silicon as the silicon content ratio decreases from 100 at %, and becomes the lowest at 85 to 95 at %, and the melting point simply increases in the range of 66.7 at % or more as the content ratio further decreases, and the melting points of the alloy are relatively linear at the both sides of the lowest point and do not have extreme flexion point and singular point. Therefore, the melting point of the alloy during the melt infiltration treatment can be stably retained in a region lower than the melting point of silicon.
Furthermore, by forming the ceramic fibers into a composite with a matrix formed of an inorganic substance in the step prior to the melt infiltration of the infiltrating material, the effect of the direct contact of the alloy as the molten infiltrating material with the ceramic fibers and interface layer can be completely prevented.
Moreover, since the treatment is a sealing treatment on the pores that are present in the composite material substrate, heat treatment distortion of the ceramic fibers which accompanies the melt infiltration of the alloy as the infiltrating material generates significantly little, and thus the obtained ceramic fiber-reinforced composite material has a high dimensional accuracy.
Furthermore, the pores that are present in the composite material substrate are sealed by the silicon alloy as the infiltrating material, and the like, and thus entry of gases (air and water vapor) that oxidize the interface layer of the composite material substrate, thereby the oxidation resistance at the interface is significantly improved.
Furthermore, since a large amount of the transition metal disilicate remains together with metallic silicon after the infiltration, much metal oxide is generated even oxygen and water vapor that are present in the environment enter, and thus more excellent oxidation resistance is shown than in the case when only silicon dioxide is generated. Therefore, an excellent effect is exerted also from the viewpoint of improvement of oxidation resistance.
According to the constitutions of the second and tenth aspects, since the silicon carbide and a carbide of the transition metal are generated on the interface regions between the infiltrating material and pores during the melt infiltration of the infiltrating material, the carbides function as a reaction protective layer for the interface region to thereby suppress the deterioration of the interface layer and improve the mechanistic properties of the ceramic fiber-reinforced composite material.
Furthermore, since the silicon carbide and carbide of the transition metal are generated, the amount of the residual alloy that remains after the solidification is decreased, and thus the mechanistic properties can be improved.
In addition, it becomes possible to change the ratio of the silicon and other transition metal in the residual alloy that remains after the solidification from the ratio prior to the infiltration, by utilizing the difference in the generation velocities of the silicon carbide and the carbide of the transition metal according to temperature conditions.
According to the constitutions of the third, fourth, eleventh and twelfth aspects, it becomes possible to accommodate up to the heat resistance limit of the composite material substrate itself without being affected by the melting point of the residual alloy that remains after the solidification in the practical use of the ceramic fiber-reinforced composite material, by increasing the melting point of the residual alloy that remains after the solidification by changing the ratio of the silicon and other transition metal in the residual alloy.
According to the constitutions recited of the fifth, sixth, seventh, eighth, thirteenth, fourteenth, fifteenth and sixteenth aspects, the interface regions between the pores in the composite material substrate and the infiltrating material are reinforced more, thereby the deterioration of the interface layer is suppressed more and the mechanistic properties of the ceramic fiber-reinforced composite material are improved more.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 is the phase diagram (schematic view) of an exemplary embodiment of the alloy as the infiltrating material used in the present invention; and

FIG. 2 is the micrograph of the cross-sectional surface of the ceramic fiber-reinforced composite material of the present invention.

DETAILED DESCRIPTION

The specific embodiment of the process for producing a ceramic fiber-reinforced composite material of the present invention may be any one as long as it is a process for producing a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material, wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon, and the process includes melt-infiltrating the pores that are present in the composite material substrate with the infiltrating material under a temperature environment at a temperature equal to or more than the melting point of the alloy as the infiltrating material.
Furthermore, the specific embodiment of the ceramic fiber-reinforced composite material of the present invention may be any one as long as it is a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material, wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon.
Namely, the ceramic fiber-reinforced composite material according to the present invention is obtained by pre-forming a composite material base material obtained by forming ceramic fibers as reinforcing fibers into a composite with an oxide or an inorganic substance such as carbon as a matrix (base material), and melt-infiltrating pores or voids that remain in the composite material substrate with a transition metal disilicate/silicon alloy as the infiltrating material.
The composite material substrate is preformed by forming a preform of ceramic fibers into a composite with an inorganic material as a matrix (base material) by a chemical vapor deposition process (CVD), a chemical vapor infiltration process (CVI), a ceramic precursor infiltration-pyrolysis process (PIP), a reactive sintering process (RS) or the like.
As the inorganic substance that forms the matrix, carbon, a nitride, a carbide, an oxide, a phosphate, a boride, crystallized glass or the like can be applied.
The ceramic fibers can be applied to either long fibers or short fibers, and as reinforced forms of the preforms thereof, various states of arrangement such as unidirectional reinforcement, woven fabric lamination, three-dimensional woven fabric and woven fabric lamination/suturation can be applied.
In order to react the melt-infiltrated transition metal disilicate/silicon alloy and the free carbon in the pores to generate carbides, as processes for providing free carbon to the inside of the pores in the composite material substrate prior to the infiltration, there are many techniques such as a chemical vapor deposition process (CVD), a chemical vapor infiltration process (CVI), an infiltration-pyrolysis process (PIP) for a carbon precursor resin and a process for slurry infiltration of a carbon powder, and the free carbon as formed can also have various forms such as amorphous carbon, crystalline carbon, graphite, carbon nanotube and graphene.
A schematic drawing of a representative phase diagram of the transition metal disilicate/silicon alloy as the infiltrating material is shown in FIG. 1.
Here, T_mp1is the temperature at which the melting point of the silicon alloy is the lowest, and T_mp2is the melting point of the transition metal disilicate, and a predetermined component ratio within the composition range A is used as the composition of the transition metal disilicate/silicon alloy in the present invention.
These transition metal disilicate/silicon alloys have significant features that the transition metal disilicates have melting points (T_mp2) that are higher than the melting point of silicon (1,414° C.), the transition metal disilicate/silicon alloys have melting points that are lower than the melting point of silicon (1,414° C.), and the like.
The features of the transition metal disilicate/silicon alloys in a binary system, which are summarized for every transition metal, are shown in the following Table 1.

TABLE 1

	Amount of		Specific
Lowest	silicon (at %)	Melting	gravity of
melting	(at lowest	point of	transition
point (° C.)	melting point)	disilicate (° C.)	metal (g/cc)

None	1414
Scandium	1000	84-86	(1230)	3.0
Yttrium	1260	85-87	1850	4.5
Titanium	1330	84-86	1478	4.5
Zirconium	1370	87-89	1620	6.5
Hafnium	1330	91-93	1543	13.3
Vanadium	1400	95-97	1677	6.0
Niobium	1400	96-98	1940	8.6
Tantalum	1375	92-94	2200	16.7

In general, an alloy having a low lowest melting point and containing a transition metal disilicate having a high melting point is desirable, and it is found that titanium, zirconium and hafnium, which are transition metals in Group 4A of the Periodic Table, are preferable.
In vanadium, niobium and tantalum, which are transition metals in Group 5A of the Periodic Table, the transition metal disilicate has a high melting point, whereas the transition metal disilicate/silicon alloy has a slightly high melting point. Conversely, in the cases of scandium and yttrium, which are transition metals in Group 3A of the Periodic Table, the transition metal disilicate/silicon alloy has a low melting point, whereas the transition metal disilicate tends to show a slightly low melting point.
Among these, hafnium, zirconium and yttrium can be preferably used as the transition metal disilicate/silicon alloy for infiltration since the transition metal disilicate/silicon alloy has a low melting point, the transition metal disilicate has a high melting point, and the transition metal disilicate has relatively excellent oxidation resistance.
For example, in the case of a hafnium disilicate/silicon alloy containing 8 to 9 at % of hafnium, the melting point is decreased to about 1,330° C. at the lowest, and thus it becomes possible to decrease the melt infiltration temperature to about 1,380° C.
At this temperature, for example, even general silicon carbide fibers (Tyranno ZMI fibers and Lox-M fibers (trade names: Ube Industries, Ltd.)) or the like are applied as ceramic fibers, it becomes possible to significantly suppress the decrease in the strength of the fibers in the melt infiltration step.
By providing the entirety or a part of the pores that are present in the composite material substrate with free carbon prior to the melt infiltration, for example, when the pores are melt-infiltrated with the hafnium disilicate/silicon alloy containing 8 to 9 at % of hafnium, the silicon in the alloy reacts with the free carbon present in the pores to generate silicon carbide, whereas the reaction amounts of the hafnium and free carbon in the alloy is relatively small, and thus the amount of the hafnium in the hafnium disilicate/silicon alloy changes little.
Therefore, the silicon on the hafnium disilicate/silicon alloy decreases, and the melting point in the hafnium disilicate/silicon alloy consequently increases according to the phase diagram shown in FIG. 1.
It is also possible to bring the melting point of the residual hafnium disilicate/silicon alloy after the infiltration close to the melting point (T_mp2) of hafnium disilicate by suitably adjusting the amount of the free carbon, the infiltration temperature and the infiltration time, and the melting point of the residual hafnium disilicate/silicon alloy can be increased to about 1,400° C. that is the melting point of silicon.

EXAMPLES

Next, the exemplary embodiments of the process for the production of a ceramic fiber-reinforced composite material and the ceramic fiber-reinforced composite material of the present invention will be explained in more detail.
As the ceramic fibers, amorphous silicon carbide fibers formed of a chemical composition of Si—Zr—C—O (Tyrrano ZMI fiber (trade name: Ube Industries, Ltd.) which had been woven into an orthogonal three-dimensional woven fabric having a shape of about 120 mm×120 mm×4 mm was used as a preform.
The fiber volume fractions of the woven fabric are 20%, 20% and 0.3%, respectively, in the X, Y and Z directions.
A carbon layer having a thickness of about 0.1 to 0.3 μm was first formed on the fiber surface on the preform of the amorphous silicon carbide fibers by a chemical vapor deposition process (CVI process) using propane (C₃H₈).
Furthermore, SiC having a thickness of 5 to 10 μm was deposited on the fiber surface by a CVI process using silicon tetrachloride (SiCl₄) and propane (C₃H₈) to form a matrix, to thereby form a composite material substrate that is a premolded product. The composite material substrate has a bulk density of about 1.8 g/cc and a pore rate of about 25%.
The composite material substrate that had been pre-formed in this way was cut into about a width of 30 mm×a thickness of 4 mm×a length 50 mm and used as a sample, and the powders of the transition metal disilicate/silicon alloys having the respective composition shown in Examples 1 to 6 in the following Table 2 were each applied thereto by using a spray glue (Spray Glue 77 (trade name: manufactured by 3M)).
The powder was applied five times to every surface of the sample, and the sample to which the transition metal disilicate/silicon alloy had been applied was put into a carbon crucible and heated in vacuum by using a carbon heater furnace to infiltrate the pores in the composite material substrate with the transition metal disilicate/silicon alloy to give a ceramic fiber-reinforced composite material (Examples 1 to 6).
The temperatures for the infiltration treatment were each preset to a temperature that is about 50° C. higher than the melting point, as shown in the following Table 2, and the heat treatment time was 1 hour.
Furthermore, an example in which the infiltration treatment with the infiltrating material was not conducted (Comparative Example 1), an example in which silicon was melt-infiltrated in vacuum at 1,430° C. (Comparative Example 2), and an example in which silicon was melt-infiltrated in vacuum at 1,470° C. (Comparative Example 3) were defined as comparative examples.

TABLE 2

				Matrix
	Free	Content ratio of	Impregnation	composition
	carbon	infiltrating	tempreature	after infiltration
	in pores	material (at %)	(° C.)	(pore parts)

Comparative	None	(Impregnation
Example 1		material was
		absent)
Comparative	None	Si(100)	1470	Si
Example 2
Comparative	None	Si(100)	1430	Si
Example 3
Example 1	None	Si(92)—Hf(8)	1380	HfSi₂+ Si
Example 2	None	Si(88)—Hf(12)	1380	HfSi₂+ Si
Example 3	None	Si(88)—Zr(12)	1420	ZrSi₂+ Si
Example 4	None	Si(86)—Y(14)	1310	YSi₂+ Si
Example 5	None	Si(85)—Ti(15)	1380	TiSi₂+ Si
Example 6	None	Si(93)—Ta(7)	1420	TaSi₂+ Si
Example 7	Present	Si(88)—Hf(12)	1420	HfSi₂+ Si +
	(carbon			SiC
	black)
Example 8	Present	Si(88)—Hf(12)	1420	HfSi₂+ Si +
	(phenol			SiC
	resin char)

A bending test piece of 4×4×length 50 mm was processed from each ceramic fiber-reinforced composite material, and bending tests and measurements of pore rates at 1,200° C. and 1,300° C. under room temperature in argon were conducted.
Furthermore, a sample of 4×4×4 mm was cut out, and the change in the weight by oxidation was measured by a thermal gravimetry in the air.
The measurement conditions were an airflow amount of 100 mL/min and a temperature raising velocity of 10° C./min, and the temperature was retained at 1,200° C. for 5 hours and the change in the weight during that time (increase in amount by oxidation) was measured.
The obtained results are shown in the following Table 3.

	TABLE 3

	Increase in
	amount by

Bending strength (MPa)

oxidation

Density	Pore rate	Room			(mg/mm²)
(g/cc)	(vol. %)	temperature	1200° C.	1300° C.	—

Comparative	1.80	24.1	253	172	124	0.06
Example 1
Comparative	2.45	2.9	85	45	38	0.06
Example 2
Comparative	2.10	16.7	140	65	35	0.06
Example 3
Example 1	2.60	3.4	250	188	162	0.02
Example 2	2.75	2.0	255	197	175	0.02
Example 3	2.55	1.8	180	160	142	0.05
Example 4	2.50	2.6	245	185	162	0.01
Example 5	2.45	3.1	249	175	151	0.06
Example 6	2.62	2.2	170	146	121	0.07
Example 7	2.65	2.0	242	206	181	0.02
Example 8	2.60	3.9	248	210	175	0.02

In Comparative Example 1 in which the infiltration treatment with the infiltrating material was not conducted, the pore rate was high as 24.1%, whereas the bending strength was a tolerable value of about 253 MPa.
In Comparative Example 2 in which the sample was melt-infiltrated with silicon (Si: 100%) under vacuum at 1,470° C., the bending strength was decreased to 85 MPa in accordance with the decrease in the strength due to thermal decomposition of the ceramic fibers during the infiltration treatment.
In the case of Comparative Example 3 in which the infiltration temperature was set to 1,430° C. that is slightly higher than the melting point of silicon (1,414° C.) so as to suppress the decrease in the strength of the ceramic fibers, the pore rate was slightly high as about 16.7% due to the high viscosity of the molten silicon, i.e., infiltration could not be sufficiently conducted.
Furthermore, even the heat treatment temperature was decreased to 1,430° C., slight decrease in the strength due to thermal decomposition of the ceramic fibers was also observed.
On the other hand, in either of Examples 1 to 6 of the present invention, since the melt infiltration temperature could be suppressed to 1,420° C. or less at most, thermal decomposition of the ceramic fibers was significantly suppressed, and thus a ceramic fiber-reinforced composite material having a high bending strength could be obtained.
Furthermore, the pore rate was 4% or less at the most and thus the infiltration property was extremely fine. Specifically, it is understood that, in the cases of the transition metal disilicate/silicon alloys containing hafnium and yttrium, respectively, the increase in amount by oxidation at 1,200° C. is also decreased, and thus materials also having excellent oxidation resistance can be obtained.
As Example 7 in the present invention, a pre-formed composite material substrate as in the above-mentioned Examples 1 to 6 was subjected to a vacuum infiltration treatment and a dry-curing treatment at 120° C., by using an aqueous solution containing 19.2 wt % of carbon black had been dispersed therein (Aqua-Black 162 (trade name: Tokai Carbon Co., Ltd.)) to which 0.5 wt % of an acrylic resin-based binder (Merposol (trade name: Matsumoto Yushi-Seiyaku Co., Ltd.) had been added.
These vacuum infiltration/drying/curing treatments were repeatedly conducted five times to thereby disperse carbon black in the pores to give a composite material substrate, and the composite material substrate was melt-infiltrated with a hafnium disilicate/silicon alloy having a composition of Si (88 at %)-Hf (12 at %) in vacuum at 1,380° C. to give a ceramic fiber-reinforced composite material.
FIG. 2 is the micrograph of the cross-sectional surface of the obtained ceramic fiber-reinforced composite material.
Most of the pores became SiC that was generated by the reaction between the filled carbon and the silicon in the melt-infiltrated hafnium disilicate/silicon alloy, and the gaps thereof were filled with the residual hafnium disilicate/silicon alloy.
As a result of an analysis of the crystal phase of this by an X-ray diffractometry, the peak of HfSi₂was not changed whereas the peak of metallic Si was extremely small.
Furthermore, the peak of crystalline SiC was significantly increased, whereas the peak of HfC was observed little.
Accordingly, it was found that a considerable part of Si in the hafnium disilicate/silicon alloy became SiC by the reaction with the free carbon in the pores, and most of the hafnium disilicate/silicon alloy phase remaining in the material was HfSi₂.
Furthermore, no decrease in the bending strength due to metal infiltration was observed, and thus a fine composite material could be obtained.
As Example 8 in the present invention, a pre-formed composite material substrate as in the above-mentioned Examples 1 to 6 was soaked in a solution obtained by diluting a novolak-type phenol resin (J-325 (trade name: DIC Corporation)) with a solvent (methyl alcohol) at a ratio of 1:1, vacuum deaeration for about 24 hours was conducted to infiltrate the pores with the phenol resin, the solvent was removed in a vacuum drier at 100° C. for 5 hours, and the phenol resin was cured in the air at 160° C.
These vacuum infiltration/drying/curing treatments were repeatedly conducted four times, and a heat treatment at 800° C. for 1 hour in an argon atmosphere was conducted to thereby carbonize the phenol resin to give a composite material substrate having pores containing carbon, and the composite material substrate was melt-infiltrated with a hafnium disilicate/silicon alloy having a composition of Si (88 at %)-Hf (12 at %) in vacuum at 1,380° C. to give a ceramic fiber-reinforced composite material.
Also in this Example 8, a ceramic fiber-reinforced composite material having an excellent bending strength and contains a small amount of the residual hafnium disilicate/silicon alloy could be obtained as in Example 7.
The ceramic fiber-reinforced composite material of the present invention can prevent the alloy as the infiltrating material, and the like from melting at a high temperature and partially scattering to thereby inhibit the oxidation resistance, and thus is preferable for, for example, movable parts that are used under high temperatures such as moving blades in gas turbines, and also exerts excellent performances in any use such as improvement of bending strength and improvement of anticorrosive property.

Claims

What is claimed is:

1. A process for producing a ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material,

wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon, and

the process comprises melt-infiltrating the pores that are present in the composite material substrate with the infiltrating material under a temperature environment at a temperature equal to or more than the melting point of the alloy as the infiltrating material.

2. The process for producing a ceramic fiber-reinforced composite material according to claim 1, comprising:

providing the entirety or a part of the pores that are present in the composite material substrate with free carbon prior to the melt infiltration; and

reacting the alloy as the infiltrating material and the free carbon in the pores during the melt infiltration to generate silicon carbide and a carbide of the transition metal.

3. The process for producing a ceramic fiber-reinforced composite material according to claim 1, wherein the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration.

4. The process for producing a ceramic fiber-reinforced composite material according to claim 2, wherein the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration.

5. The process for producing a ceramic fiber-reinforced composite material according to claim 1, wherein the ceramic fibers are silicon carbide fibers.

6. The process for producing a ceramic fiber-reinforced composite material according to claim 2, wherein the ceramic fibers are silicon carbide fibers.

7. The process for producing a ceramic fiber-reinforced composite material according to claim 3, wherein the ceramic fibers are silicon carbide fibers.

8. The process for producing a ceramic fiber-reinforced composite material according to claim 4, wherein the ceramic fibers are silicon carbide fibers.

9. A ceramic fiber-reinforced composite material that is formed by infiltrating the entirety or a part of pores that are present in a composite material substrate obtained by forming ceramic fibers into a composite with a matrix formed of an inorganic substance, with an infiltrating material,

wherein the infiltrating material is an alloy having a composition that is constituted by a disilicate of at least one or more transition metal among transition metals selected from scandium, yttrium, titanium, zirconium, hafnium, vanadium, niobium and tantalum belonging to Group 3A, Group 4A or Group 5A of the Periodic Table and silicon as the remainder, has a silicon content ratio (including the silicon in the transition metal disilicate) of 66.7 at % or more, and gives a melting point that is lower than that of a single body of silicon.

10. The ceramic fiber-reinforced composite material according to claim 9, wherein silicon carbide and a carbide of the transition metal are present in interface regions between the pores and the infiltrating material.

11. The ceramic fiber-reinforced composite material according to claim 9, wherein the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration.

12. The ceramic fiber-reinforced composite material according to claim 10, wherein the melting point of the residual alloy that is solidified in the pores after the melt infiltration is higher than the melting point of the alloy as the infiltrating material prior to the melt infiltration.

13. The ceramic fiber-reinforced composite material according to claim 9, wherein the ceramic fibers are silicon carbide fibers.

14. The ceramic fiber-reinforced composite material according to claim 10, wherein the ceramic fibers are silicon carbide fibers.

15. The ceramic fiber-reinforced composite material according to claim 11, wherein the ceramic fibers are silicon carbide fibers.

16. The ceramic fiber-reinforced composite material according to claim 12, wherein the ceramic fibers are silicon carbide fibers.