Abstract:
The present invention relates to a sintered product containing silicon carbide as a main component which comprises a phase(a) containing at least one metal selected from among Al, Sc, Y and rare earth elements and oxygen, a particle phase(b) comprising at least one metal carbide selected from among carbides of Ti, Zr, Hf, Va, Nb, Ta, W and the like, a composite particle phase(c) comprising said phase(a) and said phase(b) surrounding the phase(a) and silicon carbide matrix(d) in which the above phase(a), (b) and (c) are dispersed. 
     The silicon carbide sintered product of the present invention exhibits a remarkably high strength and a remarkably high toughness which have not been attained up to this time, so that it can form various heat-resistant structural materials having a high reliability.

Description:
BACKGROUND OF THE INVENTION 
     The present invention relates to novel silicon carbide ceramics. Particularly, it relates to a toughened silicon carbide which is useful as structural materials. 
     A silicon carbide exhibits a high heat resistance, a high oxidation resistance and an excellent high-temperature strength, so that it is expected to be widely used as a heat-resistant structural material. However, a sintered silicon carbide is fragile (i.e. the toughness is low), so that it has only a low reliability as a structural material, which is the greatest barrier for the practical use of silicon carbide ceramics. 
     To overcome this disadvantage, it was reported in, for example, Journal of the American Ceramic Society, 67, 571 (1984) that titanium carbide particles are dispersed in silicon carbide matrix to thereby prevent the propagation of crack in a sintered body thus improving the toughness. However, the sintered materials obtained by this method has a structure where titanium carbide particles are only dispersed in silicon carbide matrix and exhibit a fracture toughness of at most 6MN/m 3/2 , so that they cannot be used without anxiety as a structural material which requires a high reliability. 
     SUMMARY OF THE INVENTION 
     An object of the present invention is to provide silicon carbide ceramics having a high reliability which are tough enough to be used as various structural materials. 
     The present invention provides silicon carbide sintered materials having a structure where a phase (a) containing at least one metallic element selected from among aluminum, scandium, yttrium and rare earth elements and oxygen, a particle phase(b) comprising at least one metal carbide other than silicon carbide, such as titanium, zirconium, hafnium, vanadium, niobium, tantalum or wolfram carbide, and a composite particle phase(c) comprising such a phase(a) and such a particle phase(b) surrounding the phase(a) are dispersed in a matrix(d) comprising silicon carbide. 
     As described above, the particle phase(b) is formed around the phase(a) in the sintered silicon carbide of the present invention. In other words, the sintered silicon carbide of the present invention has a structure where the composite particle phases(c) having a structure where the grain boundary between the metal carbide particle phases(b) is filled with the phase(a) comprising at least one metallic element selected from among aluminum, scandium, yttrium and rare earth elements and oxygen (that is to say, the particle phases(b) are bonded with each other via the phase(a)), are dispersed in a matrix(d) comprising silicon carbide. It has been found that the presence of the above structure remarkably enhances the fracture toughness of a sintered silicon carbide. 
     FIG. 1 shows the scheme of a structure of the high toughness ceramic of the present invention. In this figure, numeral 1 refers to a phase(a) containing at least one metallic element selected from among aluminum, scandium, yttrium and rare earth elements and oxygen, these metals being generally present as an oxide. 2 is a metal carbide particle phase(b) surrounding the phase(a) and forms a composite particle phase(c) 10 together with the phase(a). 
     The phase(b)-constituting metal carbide must have a high melting point and be stable in silicon carbide and is preferably at least one carbide selected from among titanium, zirconium, hafnium, vanadium, niobium, tantalum and wolfram carbides. Among them, titanium or vanadium carbide or a mixture thereof are particularly preferred as a particle phase(b)-constituting metal carbide, because they are relatively light, exhibit a relatively high oxidation resistance at a high temperature and are particularly effective in enhancing the toughness of sintered silicon carbide. 3 is a silicon carbide particle which is a main component of the high toughness ceramic of the present invention and forms a matrix(d), in which the above phases are dispersed. 
     4 and 5 are phases comprising the same components as the ones of phase 1 and 2, respectively. That is to say, 4 and 5 show the phases(a) and (b) which are alone dispersed in the silicon carbide matrix (d). 
     As described above, a high toughness ceramic having a high reliability can be obtained for the first time by dispersing composite particle phases(10) having a structure where phases(1) comprising a metallic element selected from among aluminum, scandium, yttrium and rare earth elements and oxygen are present among metal carbide particles(2) to bond the particles(2) with each other via phase(1) in a silicon carbide matrix. 
     The reasons why the ceramic of the present invention exhibits an improved toughness are thought to be the branching and termination of crack. That is to say, the difference in thermal expansion coefficient and Young&#39;s modulus between the silicon carbide particles of the matrix and the composite particle phase causes stress around and in the composite particle phase. Crack propagating in the ceramic is deflected by this stress to be taken into the composite particle. Then, the crack generally branches, propagates on the interface between the phases(a) and (b) and is terminated in the composite particles. In some cases, the crack propagates inside of the phase(b) and deflects in the direction of cleavage of the metal carbide particle and is terminated also in the composite particle. As described above, the composite particle acts as a crack energy absorber, so that crack propagation becomes difficult in the ceramic, thus enhancing the toughness. 
     The high toughness ceramic of the present invention can be prepared by adding at least one metal or its compound selected from among aluminum, scandium, yttrium rare earth elements and hydride, carbide, nitride, silicide and oxide thereof, and a metal (for example, titanium, zirconium, hafnium, vanadium, niobium, tantalum or wolfram) or alloy, hydride, nitride or silicide thereof which can form a carbide in silicon carbide to silicon carbide powders and by firing the mixture at 1900° to 2300° C. either under vacuum or in an inert atmosphere. 
     In the firing step, a metal selected from among aluminum, scandium, yttrium and rare earth elements or a compound thereof acts as a sintering aid to give a dense sintered product. At the same time, the metals or metal compounds other than oxides react with oxygen or surface oxide film adhering to the surface of silicon carbide particle or oxygen or surface oxide film adhering to the added particle of titanium, zirconium, hafnium, vanadium, niobium, tantalum, wolfram or the like to form an oxide, thus forming an oxide phase of aluminum, scandium, yttrium or rare earth elements in the sintered product. 
     The average particle size of the silicon carbide to be used as a raw material is preferably from 0.1 to 2μm. If the particle size is less than 0.1μm, the handling of the raw material becomes difficult and a homogeneous sintered product is not obtained. If the particle size is more than 2μm, the dense sintering is difficult and a sintered product having a high density and a high strength is not obtained. 
     Preferred examples of the sintering aid include metallic aluminum and aluminum carbide, nitride and oxide and metallic yttrium and yttrium hydride. The use of these sintering aids can give a dense sintered product. When a sintering aid containing yttrium is used, the generated yttrium oxide(Y 2  O 3 ) has a high melting point of 2410° C., so that the obtained high toughness ceramic is advantageous in that the mechanical properties do not change until a high temperature is reached. In this connection, melting points are Al 2  O 3  : 2054° C., La 2  O 3  : 2307° C., CeO 2  : 1950° C. 
     Further, in the firing step, a metal such as titanium, zirconium, hafnium, vanadium, niobium, tantalum, wolfram or a compound thereof such as hydride, nitride or silicide is reacted with silicon carbide to be converted into the corresponding carbide. At the same time, an aggregate structure of the carbide particles is formed, thus forming the above-described composite particle phase(c) which is effective in enhancing the toughness. In some cases, the silicon generated by this reaction is taken into the phase(a) comprising an oxide of aluminum, scandium, yttrium or rare earth metal and is present in the phase(a) as a simple substance, silicate or silicate glass under certain conditions. 
     As described above, the composition of the phase(a) varies depending upon the kind of raw materials used or the sintering conditions, and can be selected from among Al 2  O 3 , Y 2  O 3 , La 2  O 3 , CeO 2 , Y 4  Al 2  O 3 , Al 2  SiO 5 , Y 2  SiO 5 , alumino silicate glass, yttrium-silicate glass and the like. 
     In the above case, where the phase(a) contains silicon, even if all of the phases(a) and (b) are homogeneously dispersed in the silicon carbide matrix(d), so that the above-described composite particle phase(c) is not formed, the enhancement in the toughness of the sintered product is observed, though slightly lower than in the case where the phase(c) is formed. 
     It is preferred that the above composite particle(c) has a diameter of about 30 to 150 μm. If the diameter is less than 30 μm, the particle is only slightly effective in preventing crack propagation. On the contrary, if the composite particle is too large, the difference in thermal expansion coefficient between the silicon carbide matrix and the composite particle causes cracks and these cracks become defects, thus decreasing the strength of the sintered product. Further, to prepare a ceramic having a sufficiently high strength and a sufficiently high toughness, it is preferred that at least 50% by volume of the total composite particles has a diameter of 30 to 150 μm. 
     To form the above composite particle, it is preferred that the metal, alloy or metal hydride to be used as a raw material for the phase(b) has an average particle size of 5 to 100 μm. Such a material is treated with silicon carbide during sintering to form a fine metal carbide particle and this particle forms the composite particle phase(c) effective in enhancing the toughness together with the phase(a) containing a sintering aid as a main component. If the particle size of the metal, alloy or hydride to be used as a raw material is too small or too large, the formation of the composite particle having a diameter of 30 to 150 μm is difficult. 
     Further, it is preferred that the metal carbide particle phase(b) which constitutes the composite particle pahse(c) has an average particle size of 1 to 20 μm. If the metal carbide particle is too small, it will not be effective in terminating crack, while if it is too large, it will not be effective in branching crack. 
     The preferred amount of the phase (a) is 0.05 to 10% by volume. If the amount is too small, a sufficiently dense sintered product is not obtained and the bonding of the composite particle(c)-constituting metal carbide particles(b) with each other becomes weak. If the amount is too large, the excellent characteristics inherent to silicon carbide are lost. 
     The amount of the composite particle(c) as calculated from an area ratio of the section of the sintered product is preferably from 5 to 30% by volume. 
     The amount of the metal carbide present in the sintered product is preferably 5 to 40% by volume If the amount is too small, the toughness ia not sufficiently improved, while if it is too large, the excellent properties inherent to silicon carbide are lost. 
     It is preferred that a ceramic to be used as a structural material requiring a high reliability, such as a turbocharger rotor or a gas turbine rotor, has a toughness of 10MN/m 3/2  or above in terms of critical stress intensity factor KIc. The ceramic of the present invention exhibits a strength of 30 kg/mm 2  or above, even if defects of about 100 μm are present on the surface of the ceramic or within the ceramic, thus satisfying the tolerance strength for design of the above rotors. Defects having a size of more than 100 μm which are present in the ceramic can be non-destructively found by X-ray penetration method, supersonic flaw detection method, viewing method or the like and can be removed. 
     The use of a ceramic having a KIc of 10MN/m 3/2  or above can prevent the breakage caused by very small, unavoidable internal defects or surface flaws. Much energy is required for cracks to grow in a ceramic having a high Kic, therefore preventing the growth of the cracks, which is thought to be the reason why the characteristics of the ceramic are stable and highly reliable for a long period. 
     The high toughness ceramic of the present invention exhibits a high KIc of more than 10MN/m 3/2 , when it contains the phase(a) in an amount of 0.05 to 10% by volume and the composite particle phase(c) in an amount of 5 to 30% by volume. The growth of cracks in a ceramic having such a high KIc requires 3 to 10 times as much energy as that required in a ceramic of the prior art having a KIc of about 3 to 6MN/m 3/2 , so that the ceramic having such a high KIc becomes more reliable as a structural material. It is preferred that the particle size of the particle phase(b) is larger than that of the SiC matrix(d). 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a scheme showing a structure of the high toughness ceramic of the present invention. 
     FIG. 2 shows a cross-section of the piping valve for atomic energy which is an example of the present invention. 
    
    
     DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS 
     The present invention will be described by the following Examples, but is not limited thereby. 
     EXAMPLE 1 
     A hydride YHx (wherein x is 1 or 2) having an average particle size of 0.7 μm or a metal Y having an average particle size of 3 μm and a carbide-formable metal or hydride thereof having a particle size of 5 to 100 μm, which will be shown in Table 1, were added to α-type of SiC powder having an average particle size of 0.5 μm, in an amount of 3 to 70% by volume in terms of metal carbide, followed by mixing. 5% by volume of a silicone resin was added as a binder to the obtained powdery mixture. The obtained mixture was passed through a 16-mesh screen and granulated. The resulting granulated mixture was placed in a metal mold and molded under a pressure of 500 kg/cm 2  into a circular plate having a diameter of 60 mm and a thickness of 10 mm. The molded product was placed in a mold made of graphite and hot-pressed by induction heating under vacuum. The hot pressing was carried out under a pressure of 300 kg/cm 2  and according to a temperature profile which comprises heating at a heating rate of 20° to 40° C./minute to a temperature of 2000° to 2200° C. and cooling immediately at the same rate. 
     A column sample (3 mm X 4 mm X 45 mm) was prepared from the obtained sintered product and examined for strength according to JIS three-point bending test (with a span of 30 mm). The bending strength at 1200° C. under vacuum, the bending strength at the same temperature after the treatment at 1000° C. in air for 1000 hours and the bending strength after giving a Vickers indentation flaw on the surface of the sample with a load of 20 to 50 kg were measured. The fracture toughness (critical stress intensity factor KIc calculated from the area of Vickers indentation flaw and the bending strength is shown in Table 1. The KIc values were calculated according to the following equation: ##EQU1## 
     wherein σ is bending strength and s is area of indentation flaw. 
     The X-ray diffraction analysis of the samples shown in Table 1 showed that all of the added YHx were present as Y 2  O 3  in the sintered product, while all of the carbide-formable metals were present as metal carbide. In the sintered product obtained under the above conditions, 30 to 70% of the Y 2  O 3  was present in the grain boundary of the composite particle phase(c) and about 50 to 75% of the metal carbide was dispersed as a sole particle, while the balance, i.e. about 25 to 50%, of the metal carbide was dispersed as an aggregate of the particles among which Y 2  O 3  phase was present, thus forming the composite particle phase(c). Further, the X-ray microanalysis of the Y 2  O 3  phase of the sample obtained by using Ti as a carbide-formable metal showed that the Y 2  O 3  phase contained not only Y and O but also Si and that Y 2  SiO 5  was present in the phase. This Si is thought to be generated by the reaction between Ti and SiC. 
     The raw material having the same composition as the one of the sample shown in Table 1 was sintered at a hot pressing temperature of 2200° C. with a retention time of 2 hours to obtain a sample. In this sample, all of the carbide-formable metal was converted into the corresponding metal carbide, about 50% of which was dispersed as an aggregate thereof. However, no Y 2  O 3  phase was present among the metal carbide particles in the sample and the sample exhibited a KIc of 3 to 4MN/m 3/2  which is about equal to that of the sintered silicon carbide of the prior art, which may be because Y 2  O 3  was evaporated during the holding of 2 hours at 2200° C. It seems necessary that the mixture of raw materials is immediately cooled to lower the temperature after sintering, though the condition may be varied depending upon the kind of additive. However, rapid cooling may cause breakage. 
     
                                           TABLE 1__________________________________________________________________________                                   Bending strengthPhase (a) in sintered product             Phase (c) in sintered product                             Bending                                   after treat-        Amt. of        Amt. of                             strength                                   ment at 1000° C.        phase (a)      phase (c)                             at 1200° C.                                   for 1000 hrNo.   Additive   Phase (a)        (Vol %)             Additive                  Phase (b)                       (Vol %)                             (MPa) (MPa)    K.sub.Ic (MN/m.sup.3/2)__________________________________________________________________________ 1 YHx  Y.sub.2 O.sub.3        0.02 VH.sub.2                  VC   15     720  700       8 2 &#34;    &#34;    0.05 &#34;    &#34;    &#34;     1050  1040     12 3 &#34;    &#34;    2    &#34;    &#34;    &#34;     1200  1150     15 4 &#34;    &#34;    5    &#34;    &#34;    &#34;     1250  1200     16 5 &#34;    &#34;    10   &#34;    &#34;    &#34;     1100  1010     14 6 &#34;    &#34;    15   &#34;    &#34;    &#34;      610  600       9 7 &#34;    &#34;    5    &#34;    &#34;     2    1100  1100      7 8 &#34;    &#34;    &#34;    &#34;    &#34;     5    1270  1250     13 9 &#34;    &#34;    &#34;    &#34;    &#34;    10    1250  1230     1610 &#34;    &#34;    &#34;    &#34;    &#34;    30    1000  910      1611 &#34;    &#34;    &#34;    &#34;    &#34;    50     400  150      1412 &#34;    &#34;    0.05 &#34;    &#34;     5    1000  1010     1213 &#34;    &#34;    10   &#34;    &#34;    30    1100  990      1614 &#34;    Y.sub.2 SiO.sub.5        0.02 Ti   TiC  15     500  480       715 &#34;    &#34;    0.05 &#34;    &#34;    &#34;      760  740      1116 &#34;    &#34;    2    &#34;    &#34;    &#34;      850  810      1517 &#34;    &#34;    5    &#34;    &#34;    &#34;      900  850      1618 &#34;    &#34;    10   &#34;    &#34;    &#34;      810  800      1519 &#34;    &#34;    15   &#34;    &#34;    &#34;      400  380      1120 &#34;    &#34;    5    &#34;    &#34;     2     700  700       821 &#34;    &#34;    &#34;    &#34;    &#34;     5     830  800      1222 &#34;    &#34;    &#34;    &#34;    &#34;    10     910  900      1623 &#34;    &#34;    &#34;    &#34;    &#34;    30     750  610      1724 &#34;    &#34;    &#34;    &#34;    &#34;    50     320  140      1525 &#34;    Y.sub.2 O.sub.3        0.05 Zr   ZrC   5    1020  820      1026 &#34;    &#34;    5    &#34;    &#34;    15    1100  510      1127 &#34;    &#34;    10   &#34;    &#34;    30    1000  --*      1128 Y    Y.sub.2 O.sub.3        0.05 Hf   HfC   5     980  800      1029 &#34;    &#34;    5    &#34;    &#34;    15    1050  620      1130 &#34;    &#34;    10   &#34;    &#34;    30    1010  --*      1031 &#34;    &#34;    0.05 Nb   NbC   5    1100  910      1032 &#34;    &#34;    5    &#34;    &#34;    15    1210  480      1233 &#34;    &#34;    10   &#34;    &#34;    30    1030  --*      1234 &#34;    &#34;    0.05 TaH.sub.2                  TaC   5    1000  850      1135 &#34;    &#34;    5    &#34;    &#34;    15    1050  500      1136 &#34;    &#34;    10   &#34;    &#34;    30    1050  --*      1037 &#34;    &#34;    0.02 W    WC, W.sub.2 C                       15     680  310       838 &#34;    &#34;    0.05 &#34;    &#34;    &#34;      970  420      1239 &#34;    &#34;    2    &#34;    &#34;    &#34;     1020  450      1540 &#34;    &#34;    5    &#34;    &#34;    &#34;     1100  500      1541 &#34;    &#34;    10   &#34;    &#34;    &#34;     1010  480      1642 &#34;    &#34;    15   &#34;    &#34;    &#34;      500  380      1343 &#34;    &#34;    5    &#34;    &#34;     2    1050  920       744 &#34;    &#34;    &#34;    &#34;    &#34;     5    1100  1010     1145 &#34;    &#34;    &#34;    &#34;    &#34;    10    1110  800      1546 &#34;    &#34;    &#34;    &#34;    &#34;    30     980  --*      1647 &#34;    &#34;    &#34;    &#34;    &#34;    50     420  --*      14__________________________________________________________________________ *decomp. 
    
     It is apparent from Table 1 that a ceramic exhibits a high KIc and a high bending strength, particularly when it contains 0.05 to 10% by volume of the Y 2  O 3  phase(a) and 5 to 30% by volume of the composite particle phase(c), which are calculated from the area ratio of the section. Particularly, a ceramic having a bending strength at 1200° C. of 400 MPa or above and a KIc 10MN/mm 3/2  or above can be obtained. 
     The samples Nos. 10 and 12 shown in Table 1 were examined for their structure. This examination showed that the total amount of VC present in the sintered products were 40 and 7% by volume, respectively, about 75% of which was present as the composite particle and that both particle sizes of VC were 5 to 20 μm, while those of the composite particle varied widely over the range of 10 to 150 μm and 70% of the composite particle had a particle size of 30 to 150 μm. 
     The sample No. 16 shown in Table 1 was examined in a similar manner a above. The total amount of TiC present in the sintered product was 20% by volume, 75% of which was present as the composite particle. The particle size of TiC which was the phase(b) was 1 to 10 μm. The size of the composite particle(c) varied over the range of 3 to 100 μm and 50% of the particle(c) had a size of 30 to 100 μm. 
     EXAMPLE 2 
     A mixture of SiC having a particle size of 0.5 to 1.0 μm and additives having a particle size of 0.7 to 100 μm was treated according to the same procedure as the one described in Example 1 to prepare a sample shown in Table 2. These samples were examined for characteristics. In these samples, all of the added sintering aid was present as an oxide in the sintered product, about 30 to 70% of which was present in the grain boundary of the composite particle phase(c) as the phase(a). All of the added carbide-formable metal was present in the sintered product as a metal carbide, 25 to 75% of which formed the composite particle phase(c). 
     
                                           TABLE 2__________________________________________________________________________                                          Bending strengthPhase (a) in sintered product                 Phase (c) in sintered product                                    Bending                                          after the treat-          Amt. of             Amt. of                                    strength                                          ment at 1000° C.          phase (a)           phase (c)                                    at 1200° C.                                          for 1000                                                   K.sub.IcNo.   Additive     Phase (a)          (Vol %)                 Additive                        Phase (b)                              (Vol %)                                    (MPa) (MPa)    (MN/m.sup.3/2)__________________________________________________________________________ 1 Al     A.sub.2 O.sub.3          0.05   V      VC     5    620   600      13 2 &#34;      &#34;    5      &#34;      &#34;     15    800   800      15 3 &#34;      &#34;    10     &#34;      &#34;     30    840   820      15 4 AlN    &#34;    0.05   &#34;      &#34;      5    700   700      14 5 &#34;      &#34;    5      &#34;      &#34;     15    900   890      17 6 &#34;      &#34;    10     &#34;      &#34;     30    850   790      16 7 Al.sub.2 O.sub.3     &#34;    0.02   VH.sub. 2                        &#34;      2    400   380       9 8 &#34;      &#34;    0.05   &#34;      &#34;      5    770   750      11 9 &#34;      &#34;    5      &#34;      &#34;     15    810   780      1510 &#34;      &#34;    10     &#34;      &#34;     30    720   570      1511 &#34;      &#34;    15     &#34;      &#34;     50    230   110      1312 &#34;      Al.sub.2 SiO.sub.5          10     Ti     TiC    5    680   650      1513 &#34;      &#34;    &#34;      &#34;      &#34;     30    610   500      1414 &#34;      &#34;    0.05   &#34;      &#34;     &#34;     570   500      1415 &#34;      &#34;    &#34;      &#34;      &#34;      5    520   510      1316 &#34;      &#34;    0.02   &#34;      &#34;     50    310   160       817 Sc.sub.2 O.sub.3     Sc.sub.2 O.sub.3          0.05   &#34;      &#34;      5    530   520      1018 &#34;      &#34;    5      &#34;      &#34;     15    550   530      1219 &#34;      &#34;    10     &#34;      &#34;     30    500   380      1120 Y.sub.2 O.sub.3     Y.sub.2 SiO.sub.5          0.05   &#34;      &#34;     30    600   410      1521 &#34;      &#34;    5      &#34;      &#34;     15    680   610      1622 &#34;      &#34;    10     &#34;      &#34;      5    730   730      1523 LaH.sub.3     La.sub.2 O.sub.3          0.05   &#34;      &#34;      5    510   500      1124 &#34;      &#34;    5      &#34;      &#34;     15    600   600      1125 &#34;      &#34;    10     &#34;      &#34;     30    490   380      1026 &#34;      La.sub.2 SiO.sub.5          0.05   WSi.sub.2                        WC, W.sub.2 C                               5    400   270      1027 &#34;      &#34;    5      &#34;      &#34;     15    450   330      1128 LaH.sub.3     La.sub.2 SiO.sub.5          10     &#34;      &#34;     30    370   --*      1129 LaC.sub.2     La.sub.2 O.sub.3          0.02   TaN    TaC   15    270   120       830 &#34;      &#34;    0.05   &#34;      &#34;     15    440   210      1231 &#34;      &#34;    10     &#34;      &#34;     15    530   330      1132 La.sub.2 O.sub.3     &#34;    15     VN     VC     5    430   420      1033 &#34;      &#34;    10     &#34;      &#34;     30    620   400      1034 &#34;      &#34;    5      &#34;      &#34;     50    310   180       735 LaSi.sub.2     La.sub.2 SiO.sub.5          0.02   TiH.sub.2                        TiC    2    420   420       8     glass36 &#34;      La.sub.2 SiO.sub.5          0.05   &#34;      &#34;      5    500   510      10     glass37 &#34;      La.sub.2 SiO.sub.5          5      &#34;      &#34;     15    520   490      11     glass38 &#34;      La.sub.2 SiO.sub.5          10     &#34;      &#34;     30    490   400      12     glass39 &#34;      La.sub.2 SiO.sub.5          15     &#34;      &#34;     50    330   190      12     glass40 CeH.sub.2     CeO.sub.2          0.05   VH.sub.2                        VC     5    540   530      1041 &#34;      &#34;    5      &#34;      &#34;     15    650   620      1042 &#34;      &#34;    10     &#34;      &#34;     30    500   370      1143 Y.sub.5 Si.sub.3     Y.sub.2 SiO.sub.5          0.05   Ti     TiC    5    600   600      13     glass44 &#34;      Y.sub.2 SiO.sub.5          5      &#34;      &#34;     15    670   650      15     glass45 &#34;      Y.sub.2 SiO.sub.5          10     &#34;      &#34;     30    640   570      16     glass46 Al.sub.5 Si.sub.3     Al.sub.2 SiO.sub.5          10     &#34;      &#34;      5    520   530      16     glass47 &#34;      Al.sub.2 SiO.sub.5          5      &#34;      &#34;     15    570   550      15     glass48 &#34;      Al.sub.2 SiO.sub.5          0.05   &#34;      &#34;     30    500   400      12     glass49 Y + Al (2:1)     Y.sub.4 Al.sub.2 O.sub.9          0.05   VH.sub.2                        VC     5    1010  1000     1450 &#34;      &#34;    5      &#34;      &#34;     15    1210  1200     1651 &#34;      &#34;    10     &#34;      &#34;     30    1070  880      1652 YH.sub.2     Y.sub.2 O.sub.3          0.05   V + Ti (1:1)                        VC + TiC                               5    1100  1050     1353 &#34;      &#34;    5      &#34;      &#34;     15    1270  1180     1554 &#34;      &#34;    10     &#34;      &#34;     30    1230  990      16__________________________________________________________________________ *decomp. 
    
     The sample No. 1 shown in Table 2 was examined for structure. The total amount of VC present in the sintered product was 5.5% by volume, about 90% of which was present as the composite particle (c). The particle size of VC was 1 to 20 μm and the size of the composite particle varied over the range of 3 to 150 μm, while 50% of the composite particle had a particle size of 30 to 150 μm. 
     The sample No. 14 shown in Table 2 was examined in a similar manner as above. The total amount of TiC present in the sintered product was 40% by volume, about 75% of which was present as the composite particle (c). The particle size of TiC was 7 to 20 μm. The size of the composite particle varied over the range of 20 to 200 μm, while about 90% of the composite particle had a size of 30 to 150 μm. 
     Particularly, a sintered product having a KIc of 10 MN/mm 3/2  or above and a bending strength at 1200° C. of 400 MPa or above, can be obtained. 
     EXAMPLE 3 
     60% by volume of a silicon carbide powder having an average particle size of 0.5 μm, 15% by volume of a titanium carbide powder having an average particle size of 2 μm, 23% by volume (in terms of the amount in the inorganic substance comprising silicon carbide as a main component obtained by firing) of a polycarbosilane having a number-average molecular weight of 1850 which is solid at room temperature and 2% by volume of an aluminum nitride powder as a sintering aid were mixed in an attritor. Xylene was added to the obtained powder in an amount of 10 to 15 ml per 50 g of the powder, followed by mixing. The obtained powdery mixture was granulated and molded in a metal mold. The obtained molded product was heattreated in air at 350° C. for 3 hours, held at 2050° C. for 30 min and hot-pressed under a pressure of 30 MPa under vacuum. 
     The surface of the obtained sintered product was subjected to mirror polishing and etched, followed by the observation of the microstructure thereof. A phase in which Al, Si and 0 were detectable with a wavelength dispersion X-ray analyzer was present among crystalline particles of silicon carbide and titanium carbide. The Si contained in this phase is thought to be generated during the pyrolysis of the polycarbosilane. Further, the titanium carbide particle phase(b) was not agglomerated but dispersed uniformly. 
     The sintered product exhibited a bending strength of 540 MPa at 1200° C. under vacuum and a bending strength of 510 MPa at the same temperature after the treatment at 1000° C. for 1000 hr in air and had a KIc of 8 MN/m 3/2   
     As described above, the high toughness ceramic of the present invention has a high fracture energy, so that it is highly resistant against mechanical and heat-shock. Therefore, the ceramic of the present invention can be used as gas turbine components (nozzle or rotor), turbocharger rotor, ball bearing, cutting machine (cutting tool or saw or), piping valve which operates with a high shock or the like. 
     FIG. 2 shows a case where the high toughness ceramic of the present invention is used as the disc head of a piping valve for atomic energy (section) which requires wear resistance and shock resistance. 
     In FIG. 2, the ceramic of the present invention was applied to a disc head 11 which requires the highest strength in a piping valve for atomic energy comprising a disc head 11, a disc 12, a cylinder 13, a shaft 14, a bonnet 15 and a pipe 16, thus obtaining a piping valve for atomic energy having a longer life and a higher operating reliability as compared with piping valves of the prior art. 
     As described above, the ceramic of the present invention has a remarkably high toughness and can be therefore used as a structural material, particularly as a component of an apparatus requiring heat resistance and high strength.