Sintered Si.sub.3 N.sub.4 body

Information

  • Patent Grant
  • 4412009
  • Patent Number
    4,412,009
  • Date Filed
    Wednesday, September 23, 1981
    43 years ago
  • Date Issued
    Tuesday, October 25, 1983
    40 years ago
Abstract
Disclosed is a method of producing a sintered body of ceramics, wherein a powder mixture consisting, essentially of at most 10%, exclusive of 0%, by weight of yttrium oxide, at most 10%, exclusive of 0%, by weight of aluminum oxide, at most 10%, exclusive of 0%, by weight of aluminum nitride, at most 5%, exclusive of 0%, by weight of at least one material selected from the group consisting of titanium oxide, magnesium oxide and zirconium oxide, and the balance essentially of silicon nitride is sintered under a non-oxidizing atmosphere.
Description

This invention relates to a method of producing a sintered body of silicon nitride-based ceramics.
A sintered body of silicon nitride-based ceramics exhibits an excellent heat resistance; it is resistant to the heat of up to 1,900.degree. C. In addition, the sintered body mentioned has a low thermal expansion coefficient, leading to an excellent thermal shock resistance. Thus, researches are being made in an attempt to use a sintered body of silicon nitride-based ceramics for forming machine parts requiring a high mechanical strength under high temperatures such as a gas turbine blade and nozzle. In general, such a sintered body is produced from a mixted powder of silicon nitride-yttrium oxide-aluminum oxide by a so-called "hot press method" or "normal sintering". The normal sintering is advantageous over the hot press method in that the former permits producing a sintered body of any desired shape and is suitable for mass production of a sintered body. However, it is difficult to produce dense sintered body exhibiting a satisfactory mechanical strength and heat resistance by the normal sintering. Naturally, it is a matter of serious concern in this field to develop a method which permits producing, even by the normal sintering a dense sintered body of silicon nitride-based ceramics exhibiting a high mechanical strength and heat resistance.
An object of this invention is to provide a method which does not necessitate pressurizing in the sintering step, of producing a dense sintered body of silicon nitride-based ceramics exhibiting a high mechanical strength under high temperatures and a high thermal shock resistance.
According to this invention, there is provided a method of producing a sintered body of ceramics, wherein a powder mixture consisting essentially of at most 10%, exclusive of 0%, by weight of yttrium oxide at most 10%, exclusive of 0%, by weight of aluminum oxide, at most 10%, exclusive of 0%, by weight of aluminum nitride, at most 5%, exclusive of 0%, by weight of at least one material selected from the group consisting of titanium oxide, magnesium oxide and zirconium oxide, and the balance essentially of silicon nitride is sintered under a non-oxidizing atmosphere.
Each of yttrium oxide and aluminum oxide used in this invention acts as a sintering accelerator and should be used in an amount of at most 10%, exclusive of 0%, by weight. Preferably, the total amount of these materials should range between 3 and 15% by weight. If the amount of any of these materials exceeds 10% by weight, the produced sintered body fails to exhibit satisfactory mechanical strength and thermal shock resistance.
Aluminum nitride used in this invention serves to suppress evaporation of silicon nitride in the sintering process. Also, aluminum nitride reacts with the other additives so as to form a liquid phase serving to promote the sintering process. The amount of aluminum nitride should be at most 10%, exclusive of 0% by weight. If aluminum nitride is used in an amount larger than 10% by weight, the product sintered body is rendered unsatisfactory in mechanical strength and thermal shock resistance. Preferably, the total amount of aluminum nitride and aluminum oxide should be at most 15% by weight, more preferably, should range between 2 and 15% by weight.
Any of titanium oxide, magnesium oxide and zirconium oxide used in this invention serves to assist the function of the sintering accelerator mentioned previously. The amount of any of these materials, or the total amount of these materials, if used in combination, should be at most 5%, exclusive of 0%, by weight, preferably, should range between 0.05 and 3% by weight. Specifically, any of these materials contributes to the sintering acceleration together with yttrium oxide and aluminum oxide and, in addition, serves to improve the wettability between the main component of silicon nitride and the additives. As a result, the sintered body is enabled to exhibit a high density and the sintering time can be shortened. Further, the sintering temperature can be lowered. However, if the amount of these material 5% by weight, the produced sintered body tends to be unsatisfactory in mechanical strength under high temperatures.
In this invention, it is possible to use silicon nitride of either .alpha.-type or .beta.-type as the main component of the raw material, though .alpha.-silicon nitride is desirable. The amount of silicon nitride, which is the balance between the total amount of the raw material and the total amount of the additives described above, should be more than 65% by weight, preferably, should range between 70 and 94% by weight.
A powder mixture of the composition described above is shaped as desired by using a binder and, then, sintered under a non-oxidizing atmosphere at 1,500.degree. to 1,900.degree. C. preferably, at 1,600.degree. to 1,800.degree. C. A rare gas like argon gas or nitrogen gas can be used as the nonoxidizing atmosphere. It is also possible to carry out the sintering under vacuum. If the sintering is carried out under an oxygen-containing atmosphere, silicon nitride is oxidized into silicon dioxide, failing to obtain a sintered body exhibiting a high mechanical strength under high temperatures. A so-called "normal sintering" which does not involve pressurizing can be employed for producing a silicon nitride-based sintered body having a high density and exhibiting a high mechanical strength and thermal shock resistance under high temperatures. Of course, the sintering can be carried out under a pressure of, for example, 50 to 500 Kg/cm.sup.2, i.e., hot press method, for producing a sintered body of satisfactory properties.





EXAMPLES AND CONTROLS
Used in the experiment as the raw material were a Si.sub.3 N.sub.4 power containing 85% of .alpha.-Si.sub.3 N.sub.4 and having an average particle size of 1.2 .mu., a Y.sub.2 O.sub.3 powder having an average particle size of 1 .mu., an Al.sub.2 O.sub.3 powder having an average particle size of 0.5 .mu., and an AlN powder having an average particle size of 1.5 .mu. as well as TiO.sub.2 powder, MgO powder and ZrO.sub.2 powder each having an average particle size of 1 .mu.. Various ratios of these powdery materials as shown in the following Table were mixed for 10 hours, with n-butylalcohol used as a solvent, by using a ball mill of rubber-coated balls so as to prepare 53 samples of powder mixture including Control cases.
Each powder mixture sample thus prepared was kneaded with 7% by weight of stearic acid added thereto as a binder, followed by shaping the kneaded mass under a pressure of 700 Kg/cm.sup.2 into a plate 60 mm long, 40 mm wide and 10 mm thick and into disc 30 mm in diameter and 10 mm in thickness. Each of the plate and disc thus prepared was heated at 700.degree. C. so as to remove the binder and, then, sintered at 1,700.degree. C. under nitrogen gas atmosphere so as to obtain a silicon nitride-based sintered body of ceramics.
The following Table shows the relative density (%), flexural strength and thermal shock resistance of the sintered body. The relative density mentioned above represents the percentage of the actual density of the sintered body relative to the theoretical density thereof. The flexural strength represents the value obtained by applying a three point bend strength test to a specimen sized at 3.times.3.times.30 (mm), which was cut out from the plate-like sintered body, under a crosshead speed of 0.5 mm/min and a span of 20 mm. The flexural strength was measured at a room temperature, at 1,000.degree. C. and at 1,200.degree. C. The value shown in the Table represents the average of four specimens. Further, the critical thermal shock temperature (.DELTA.T.sub.C) was measured by a so-called "water quenching method" in which a sample heated to a predetermined temperature is immersed in water so as to rapidly cool the sample, namely, the value of .DELTA.T.sub.C shown in the Table represents the difference between the temperature of the sample at which the sample begins to be cracked and the water temperature.
TABLE__________________________________________________________________________ Flexural strength kg/mm.sup.2 RoomComponent (%) Relative temper- .DELTA.TcSample Si.sub.3 N.sub.4 Y.sub.2 O.sub.3 Al.sub.2 O.sub.3 AlN TiO.sub.2 MgO ZrO.sub.2 density ature 1,000.degree. C. 1,200.degree. C. (.degree.C.)__________________________________________________________________________Control A 70 10 10 10 -- -- -- 98.5 75 59 40 300Control B 85 5 5 5 -- -- -- 95.8 83 70 60 400Control C 90 5 5 10 -- -- -- 96.4 60 65 54 350Control D 88 5 2 5 -- -- -- 92.0 45 47 50 450Control E 94 2 2 2 -- -- -- 85.2 30 30 28 500Control F 80 10 5 5 -- -- -- 98.0 65 60 52 400Control G 80 5 3.5 3.5 8 -- -- 99.8 90 69 45 375Control H 80 5 3.5 3.5 -- 8 -- 99.6 88 64 40 375Example 1 75 10 5 5 5 -- -- 99.5 80 70 60 400Example 2 82 10 2 5 1 -- -- 98.8 75 72 65 475Example 3 78 5 2 10 5 -- -- 97.5 85 75 61 450Example 4 89 5 2 2 2 -- -- 96.2 91 75 67 475Example 5 87.5 5 2 3.5 2 -- -- 99.0 100 80 68 475Example 6 89 5 2 3.5 0.5 -- -- 96.1 90 80 78 550Example 7 87 5 3.5 3.5 1 -- -- 99.4 102 90 75 500Example 8 86 5 3.5 3.5 2 -- -- 99.6 99 80 67 450Example 9 87.5 5 3.5 3.5 0.5 -- -- 98.7 100 95 82 525Example 10 87.5 2 3.5 2 5 -- -- 96.2 85 70 60 400Example 11 78 10 2 5 -- 5 -- 99.0 90 75 60 400Example 12 80 5 5 5 -- 5 -- 99.8 95 80 62 400Example 13 89 5 2 2 -- 2 -- 97.7 91 74 63 500Example 14 87.5 5 2 3.5 -- 2 -- 96.6 96 72 66 550Example 15 88.5 5 3.5 2 -- 1 -- 97.3 92 86 75 550Example 16 87.5 5 3.5 3.5 -- 0.5 -- 98.9 95 90 80 500Example 17 76 10 2 10 -- -- 2 99.0 88 72 60 400Example 18 88.5 5 2 3.5 -- -- 1 97.5 95 93 70 525Example 19 79.5 5 10 5 -- -- 0.5 99.8 100 82 68 400Example 20 83 5 3.5 3.5 -- -- 5 98.5 99 85 62 450Example 21 87.5 5 3.5 3.5 -- -- 0.5 98.0 90 88 75 500Example 22 89 2 5 2 -- -- 2 95.8 80 78 68 475Control I 88 5 5 -- 2 -- -- 95.2 63 57 46 400Control J 88 5 5 -- -- 2 -- 96.0 63 59 47 400Control K 88 5 5 -- -- -- 2 92.6 59 54 49 400Example 23 77 10 5 5 1 1 1 99.2 89 72 60 400Example 24 87 2 5 2 -- 2 2 99.0 80 70 62 450Example 25 85 5 2 5 2 1 -- 98.5 95 83 70 425Example 26 85 5 3.5 3.5 1 1 1 98.7 100 80 64 450Example 27 87.75 5 3.5 3.5 0.25 -- -- 97.5 98 95 82 550Example 28 87.9 5 3.5 3.5 0.1 -- -- 96.0 84 80 72 550Example 29 87.75 5 2 5 0.25 -- -- 98.2 105 99 81 550Example 30 90.95 5 2 2 0.05 -- -- 95.0 80 78 73 600Example 31 87.75 5 3.5 3.5 -- 0.25 -- 97.8 100 84 70 500Example 32 87.9 5 3.5 3.5 -- -- 0.1 96.4 86 80 75 525Example 33 87.85 5 3.5 3.5 0.05 0.05 0.05 95.9 88 84 76 575Example 34 87.80 5 3.5 3.5 0.1 0.05 0.05 98.0 103 90 79 550Example 35 93.9 2 2 2 0.1 -- -- 95.0 80 78 70 600Example 36 89 5 5 0.5 0.5 -- -- 97.2 95 83 72 600Example 37 87 3 0.5 7 -- 0.5 -- 95.1 80 80 70 525Example 38 87.9 2 8 0.1 -- -- 2 96.8 88 79 62 475Example 39 88 0.5 7 3.5 1 -- -- 95.9 81 78 65 500Example 40 87.9 7 0.1 3 2 -- -- 95.0 80 75 60 525Example 41 90.5 5 1.5 1 -- 2 -- 95.2 79 74 68 500Control L 92 5 0.5 0.5 -- -- 2 86.3 50 42 30 475__________________________________________________________________________
The above Table shows that the method of this invention permits producing a sintered body of ceramics having a relatively density of at least 95%, a flexural strength of at least 70 Kg/mm.sup.2 at a room temperature and at least 60 Kg/mm.sub.2 at 1,200.degree. C., and a critical thermal shock temperature of at least 400.degree. C. It is important to note that the normal sintering was employed in the experiment described above. Nevertheless, the produced sintered body exhibits properties fully comparable with those of the sintered body produced by employing the hot press method.
As described above in detail, this invention provides a method of producing a dense sintered body of silicon nitride-based ceramics exhibiting a high mechanical strength and thermal shock resistance under high temperature. Particularly, the normal sintering, not the hot press method, can be employed for obtaining a desired sintered body.
Claims
  • 1. A sintered ceramic body consisting essentially of at most 10%, exclusive of 0%, by weight of yttrium oxide; at most 10%, exclusive of 0%, by weight of aluminum nitride; at most 10%, exclusive of 0%, by weight of aluminum nitride; at most 5%, exclusive of 0%, by weight of at least one material selected from the group consisting of titanium oxide, magnesium oxide and zirconium oxide; and the balance essentially of silicon nitride; wherein said sintered ceramic body has a relative density of at least 95.1%.
  • 2. The sintered ceramic body according to claim 1, wherein the total amount of yttrium oxide and aluminum oxide ranges between 3 and 15% by weight.
  • 3. The sintered ceramic body according to claim 1 or 2, wherein the total amount of aluminum nitride and aluminum oxide ranges between 2 and 15% by weight.
  • 4. The sintered ceramic body according to claim 3, wherein the amount of at least one material selected from the group consisting of titanium oxide, magnesium oxide and zirconium oxide ranges between 0.05 and 3% by weight.
  • 5. The sintered ceramic body according to claim 1, wherein the amount of silicon nitride ranges between 70 and 94% by weight.
Priority Claims (1)
Number Date Country Kind
54-19013 Feb 1979 JPX
Parent Case Info

This is a continuation of application Ser. No. 122,659, filed Feb. 19, 1980 now U.S. Pat. No. 4,327,187.

US Referenced Citations (8)
Number Name Date Kind
3830652 Gazza Aug 1974
3953221 Lange Apr 1976
3969125 Komeya et al. Jul 1976
3991148 Lumby et al. Nov 1976
4066468 Kamigaito et al. Jan 1978
4113503 Lumby et al. Sep 1978
4127416 Lumby et al. Nov 1978
4143107 Ishii et al. Mar 1979
Foreign Referenced Citations (2)
Number Date Country
4988917 Dec 1972 JPX
49-128915 Dec 1974 JPX
Continuations (1)
Number Date Country
Parent 122659 Feb 1980