GB2276376A - Ceramic-metal composites - Google Patents
Ceramic-metal composites Download PDFInfo
- Publication number
- GB2276376A GB2276376A GB9410517A GB9410517A GB2276376A GB 2276376 A GB2276376 A GB 2276376A GB 9410517 A GB9410517 A GB 9410517A GB 9410517 A GB9410517 A GB 9410517A GB 2276376 A GB2276376 A GB 2276376A
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- Prior art keywords
- ceramic
- metal
- powder
- sintered
- powder mixture
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- 239000002905 metal composite material Substances 0.000 title claims abstract description 43
- 239000000203 mixture Substances 0.000 claims abstract description 165
- 239000000919 ceramic Substances 0.000 claims abstract description 118
- 229910052751 metal Inorganic materials 0.000 claims abstract description 100
- 239000002184 metal Substances 0.000 claims abstract description 98
- 238000005245 sintering Methods 0.000 claims abstract description 66
- 150000004706 metal oxides Chemical class 0.000 claims abstract description 27
- 150000004703 alkoxides Chemical class 0.000 claims abstract description 26
- 229910044991 metal oxide Inorganic materials 0.000 claims abstract description 24
- 230000000737 periodic effect Effects 0.000 claims abstract description 16
- 229910052987 metal hydride Inorganic materials 0.000 claims abstract description 11
- 239000000843 powder Substances 0.000 claims description 228
- 239000002245 particle Substances 0.000 claims description 131
- 239000002131 composite material Substances 0.000 claims description 46
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 44
- 238000010438 heat treatment Methods 0.000 claims description 13
- 238000004519 manufacturing process Methods 0.000 claims description 10
- 230000003301 hydrolyzing effect Effects 0.000 claims description 4
- 238000003801 milling Methods 0.000 claims description 4
- 150000004681 metal hydrides Chemical class 0.000 claims description 2
- 239000011159 matrix material Substances 0.000 abstract description 71
- 238000000034 method Methods 0.000 abstract description 25
- 230000001976 improved effect Effects 0.000 abstract description 14
- 150000004678 hydrides Chemical class 0.000 abstract description 9
- 239000000047 product Substances 0.000 description 180
- 230000000052 comparative effect Effects 0.000 description 62
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 46
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 44
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 40
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 39
- 229910052593 corundum Inorganic materials 0.000 description 36
- 229910001845 yogo sapphire Inorganic materials 0.000 description 36
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 28
- 238000002441 X-ray diffraction Methods 0.000 description 27
- 238000004445 quantitative analysis Methods 0.000 description 27
- 239000000126 substance Substances 0.000 description 27
- 239000002923 metal particle Substances 0.000 description 26
- 239000007789 gas Substances 0.000 description 25
- 229910052786 argon Inorganic materials 0.000 description 23
- 239000001257 hydrogen Substances 0.000 description 22
- 229910052739 hydrogen Inorganic materials 0.000 description 22
- 239000002904 solvent Substances 0.000 description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 16
- 239000006185 dispersion Substances 0.000 description 16
- 239000000395 magnesium oxide Substances 0.000 description 15
- CETPSERCERDGAM-UHFFFAOYSA-N ceric oxide Chemical compound O=[Ce]=O CETPSERCERDGAM-UHFFFAOYSA-N 0.000 description 14
- 229910000422 cerium(IV) oxide Inorganic materials 0.000 description 14
- 229910002077 partially stabilized zirconia Inorganic materials 0.000 description 14
- 229910052581 Si3N4 Inorganic materials 0.000 description 12
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 12
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 12
- 239000010955 niobium Substances 0.000 description 12
- 239000000243 solution Substances 0.000 description 12
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 9
- 229910052863 mullite Inorganic materials 0.000 description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 229910001111 Fine metal Inorganic materials 0.000 description 8
- 229910052742 iron Inorganic materials 0.000 description 8
- JKQOBWVOAYFWKG-UHFFFAOYSA-N molybdenum trioxide Chemical compound O=[Mo](=O)=O JKQOBWVOAYFWKG-UHFFFAOYSA-N 0.000 description 8
- 239000004698 Polyethylene Substances 0.000 description 7
- RKTYLMNFRDHKIL-UHFFFAOYSA-N copper;5,10,15,20-tetraphenylporphyrin-22,24-diide Chemical compound [Cu+2].C1=CC(C(=C2C=CC([N-]2)=C(C=2C=CC=CC=2)C=2C=CC(N=2)=C(C=2C=CC=CC=2)C2=CC=C3[N-]2)C=2C=CC=CC=2)=NC1=C3C1=CC=CC=C1 RKTYLMNFRDHKIL-UHFFFAOYSA-N 0.000 description 7
- 230000000694 effects Effects 0.000 description 7
- 239000010419 fine particle Substances 0.000 description 7
- -1 polyethylene Polymers 0.000 description 7
- 229920000573 polyethylene Polymers 0.000 description 7
- 229910052721 tungsten Inorganic materials 0.000 description 7
- 239000011261 inert gas Substances 0.000 description 6
- 229920003023 plastic Polymers 0.000 description 6
- 239000004033 plastic Substances 0.000 description 6
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 6
- 239000010937 tungsten Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 229910052750 molybdenum Inorganic materials 0.000 description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 4
- 229910017878 a-Si3N4 Inorganic materials 0.000 description 4
- 239000011153 ceramic matrix composite Substances 0.000 description 4
- 239000011521 glass Substances 0.000 description 4
- 238000001746 injection moulding Methods 0.000 description 4
- 239000011733 molybdenum Substances 0.000 description 4
- ZKATWMILCYLAPD-UHFFFAOYSA-N niobium pentoxide Chemical compound O=[Nb](=O)O[Nb](=O)=O ZKATWMILCYLAPD-UHFFFAOYSA-N 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 238000005240 physical vapour deposition Methods 0.000 description 4
- 239000011148 porous material Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 229910052878 cordierite Inorganic materials 0.000 description 3
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 3
- 239000008187 granular material Substances 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 230000001737 promoting effect Effects 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 239000004372 Polyvinyl alcohol Substances 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 2
- 238000005229 chemical vapour deposition Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- AWXKYODXCCJWNF-UHFFFAOYSA-N ethanol tungsten Chemical compound [W].CCO.CCO.CCO.CCO.CCO AWXKYODXCCJWNF-UHFFFAOYSA-N 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000007676 flexural strength test Methods 0.000 description 2
- 230000007062 hydrolysis Effects 0.000 description 2
- 238000006460 hydrolysis reaction Methods 0.000 description 2
- 238000010348 incorporation Methods 0.000 description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 229910052575 non-oxide ceramic Inorganic materials 0.000 description 2
- 239000011225 non-oxide ceramic Substances 0.000 description 2
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 2
- 229920002451 polyvinyl alcohol Polymers 0.000 description 2
- 230000008093 supporting effect Effects 0.000 description 2
- 229910000048 titanium hydride Inorganic materials 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 229910015667 MoO4 Inorganic materials 0.000 description 1
- 229910019651 Nb(OC2H5)5 Inorganic materials 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000007931 coated granule Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- ABGLZESYHATICB-UHFFFAOYSA-N ethanol;molybdenum Chemical compound [Mo].CCO.CCO.CCO.CCO.CCO ABGLZESYHATICB-UHFFFAOYSA-N 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910003465 moissanite Inorganic materials 0.000 description 1
- ZTILUDNICMILKJ-UHFFFAOYSA-N niobium(v) ethoxide Chemical compound CCO[Nb](OCC)(OCC)(OCC)OCC ZTILUDNICMILKJ-UHFFFAOYSA-N 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 229910052574 oxide ceramic Inorganic materials 0.000 description 1
- 239000011224 oxide ceramic Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000000644 propagated effect Effects 0.000 description 1
- 230000001902 propagating effect Effects 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/74—Ceramic products containing macroscopic reinforcing agents containing shaped metallic materials
- C04B35/76—Fibres, filaments, whiskers, platelets, or the like
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
A sintered ceramic-metal composite product has a ceramic matrix of polycrystalline ceramic in which a metal phase is dispersed for adding improved toughness. The metal phase comprises at least one metal selected from the groups IVa, Va and VIa of the periodic table. The ceramic-metal composite product is fabricated by several methods utilizing a mixture of the ceramic, or alkoxide of ceramic constituting element, and metal oxide, hydride or alkoxide. The final step of the methods is sintering in a reducing environment.
Description
SPECIFICATION
SINTERED CERAMIC-METAL COMPOSITE PRODUCT AND METHOD OF
FABRICATING THE SAME
BACKGROUND OF THE INVENTION 1. Field of the Invention
The present invention is directed to a sintered ceramicmetal composite product and a method of fabricating the same.
2. Description of the Prior Art
Sintered polycrystalline ceramic products, due to their excellent heat, wear and corrosion resistance, are currently expected to have a wide variety of applications for use as storming turbo-charger rotors of automobiles, various cutting tools and tool bits, mechanical seals, and even sporting and leisure goods. However, because of inherently strong covalent and ionic bond that permit no substantial dislocation or plastic deformation as opposed to metallic materials, the ceramics fail to alleviate stress concentration occurring at a leading end of a crack and are therefore easily fractured as a consequence of that the crack proceeds as started from a minute internal defect or a surface scratch.Thus, the ceramics exhibit poor toughness with attendant brittleness which excludes the application of the ceramics for making large parts or parts of complicated shapes and therefore restricts the application only to parts of limited dimensions and shapes.
In order to overcome the brittleness, attempts have been made to provide a ceramic matrix composite of improved toughness and strength in which minute particles or whiskers of one ceramic material are dispersed into a matrix of another ceramic material. Such ceramic matrix composite strengthening has advanced from the ceramic particle dispersion to whisker or fibre dispersion, and from a micro-order inter-granular dispersion to a nano-order intra-granular dispersion.
Particularly, the ceramic matrix composite of the nano-order dispersion Fhereinafter referred to simply as nano-order ceramic composite] is reported to show remarkable improvement in mechanical strength, particularly at high temperature, for example, as disclosed in Japanese patent non-examined early publication (KOKAI) No. 64-87552. The patent teaches to strengthen a-alumina matrix by dispersing minute SiC particles within the granules of the alumina matrix. Besides, it is also known that improved mechanical strength is achieved in other nano-order ceramics composites of A1203/Si3N4 where Si3N4 is an intra-granular phase in the matrix of A1203 and MgO/SiC where SiC is an intra-granular phase in MgO matrix.As for a non-oxide ceramic matrix, a like nano-order ceramic composite of Si3N4/SiC is known to exhibit improved strength, as described in the publication "Powder and Powder Metallurgy
Vol. 1.36 page 243, 1989". The publication teaches to react [Si(CH)3]2NH in an atmosphere of ammonia and hydrogen through chemical vapor deposition (CVD) technique to obtain amorphous composite powder of Si-C-N which is subsequently processed to present the corresponding ceramic composite Si3N4/SiC in which
SiC particles are dispersed within the granules of the Si3N4 matrix.
With regard to the toughness, the ceramic matrix composite of the micro-order dispersion [hereinafter referred to simply as micro-order ceramic composite] can exhibit an improved fracture toughness of about 10 MPamV2 for a ceramic matrix in which ZrO2 particles or whiskers are dispersed and an even more improved fracture toughness of about 20 to 30 MPaml2 for a ceramic matrix in which long fibers of SiC are dispersed. While, on the other hand, the nano-order ceramic composite is found to exhibit the fracture toughness which is only about 30 to 40 % of that for the micro-order ceramic composite. Despite the poor fracture toughness, the nanoorder ceramic composite has an improved mechanical strength of as much as 160 to 200 % of that of the micro-order ceramic composite.Consequently, it is most desirous to further improve fracture toughness of the nano-order ceramic composite so that the nano-order ceramic composite can combine excellent toughness and fracture strength.
SUMMARY OF THE INVENTION
The present invention has been achieved in view of the above, and has a primary object of presenting a sintered ceramic-metal composite product which combines excellent mechanical strength as well as fracture toughness sufficient for use as a structural material. The sintered ceramic-metal composite product in accordance with the present invention comprises a ceramic matrix of polycrystalline ceramic and a metal phase or constituent having a melting temperature higher than a sintering temperature of the ceramic matrix. The metal phase is dispersed within the grains of the ceramic matrix to effect nano-order intra-granular dispersion. Such dispersed metal phase, or metal constituent acts to inhibit crack propagation in the grains of the ceramic matrix to thereby attain greatly improved toughness while retaining excellent mechanical strength.
Another object of the present invention is to provide several methods of successfully fabricating the ceramic-metal composite product in which the metal phase is dispersed intragranular within the grains of the ceramic matrix. Included in the methods are: 1) to prepare a powder mixture containing a ceramic powder
having an average particle size of 0.5 pm or less, and 5
to 50% by volume of at least one metal element selected
from groups IVa, Va, and VIa of the periodic table, and
sinter the powder mixture.
2) to prepare a powder mixture containing a ceramic powder
having an average particle size of 0.5 m or less, and a
metal or metal oxide of at least one metal element
selected from groups IVa, Va, and VIa of the periodic
table, and sinter the powder mixture firstly in an
atmospheric environment followed by sintering in a
reducing environment.
3) to prepare a powder mixture of a ceramic powder having an
average particle size of 0.5 pm or less, and a metal
oxide or hydride of at least one metal element selected
from groups IVa, Va and VIa of the periodic table, and
sinter the powder mixture in a reducing environment.
4) to prepare a mixture of a ceramic powder having an
average particle size of 0.5 pm or less, a metal alkoxide
of at least one metal element selected from groups IVa,
Va and VIa of the periodic table, and an alcohol;
hydrolyze and heat the mixture into a resulting powder
mixture, and subsequently sinter the powder mixture in a
reducing environment.
5) to dissolve a metal alkoxide of at least one metal
element selected from groups IVa, Va and VIa of the
periodic table together with an alkoxide of a ceramic
constituting element into an alcohol to obtain an alcohol
solution thereof, hydrolyze and heat the alcohol solution
into a resulting powder mixture, and sinter the power
mixture in a reducing environment.
6) to dissolve a metal alkoxide of at least one metal
element selected from groups IVa, Va and VIa of the
periodic table together with an alkoxide of a ceramic
constituting element into an alcohol to provide an
alcohol solution thereof, heat the solution to provide a
composite alkoxide followed by hydrolyzing and heating
the resulting composite alkoxide into a corresponding
powder mixture, and subsequently sinter the powder
mixture in a reducing environment.
With the above methods, the metal phase can be readily and successfully incorporated in the ceramic matrix during the sintering so as to precipitate as finely dispersed metal particles within the grains of the ceramic matrix, effecting nano-order dispersion of the metal particles responsible for remarkably improved toughness while retaining the excellent strength inherent to-the ceramics, which is therefore a further object of the present invention.
These and still other objects and advantageous features of the present invention will become more apparent from the following description and examples of the present invention when taken in conjunction with the attached drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a graph illustrating three-point flexural strength (MPa) over a temperature range from a room temperature up to 1400 C for a ceramic-metal composite product obtained in
Example 1 of the present invention;
FIG. 2 is a transmission-type electron photomicrograph showing the grain structure of the composite product of Example 1;
FIG. 3 is a scan-type electron photomicrograph showing the grain structure at the fractured face of the composite product of Example 1;
FIG. 4 is a graph illustrating three-point flexural strength (MPa) over a temperature range from a room temperature up to 1400 C for a ceramic-metal composite product obtained in comparative Example 3;
FIG. 5 is a transmission-type electron photomicrograph showing the grain structure of the composite product of Example 7; and
FIG. 6 is a scan-type electron photomicrograph showing the grain structure at the fractured face of the composite product of Example 7.
DESCRIPTION OF THE INVENTION
The present invention will be described hereinafter in more detail. The ceramic matrix utilized in the present invention may be oxides or non-oxides of a suitable metal, for example, A1203, MgO, partially stabilized zirconia, mullite, cordierite, Si3N4, SiC, and A1N, which can 'be sintered either at an atmospheric or increased pressure into a closely packed structure. In order to successfully migrate majority of the metal element into the grains of the ceramic matrix during the sintering process, the ceramic should be in the form of a powder having an average particle size of 0.5 p or less and be of such kind as to effect grain growth during the sintering.
When the partially stabilized zirconia is selected as the ceramic matrix, the zirconia is preferred to incorporate CeO2 as a stabilizing agent, and particularly in 5 to 30 mol %.
Within this incorporation range, the partially stabilized zirconia can have a structure substantially made of tetragonal system or a mixed phase of tetragonal and cubic systems, which are responsible for imparting improved mechanical strength to the partially stabilized zirconia matrix. When CeO2 is incorporated in less than 0.5 mol %, there occurs insufficient formation of tetragonal system of a metastable phase. Above 30 mol % of CeO2, the cubic system predominates to lower the strength of the zirconia matrix.
The metal phase is limited to have a melting temperature higher than the sintering temperature of the ceramic matrix and is also limited to be made into a such a fine particle that can be incorporated within the grains of the ceramic matrix during the sintering. When the metal powder is utilized, its average particle size is preferred to be 1 Fm.
The metal phase may partially remain in the grain boundaries, but is preferred to be all dispersed within the grains of the ceramic matrix. In this regard, the metal phase is preferably contained in 0.5 to 50 vol %, and more preferably 2.5 to 30 vol %, based upon the ceramic-metal composite product. Below 0.5 vol % of the metal phase, no substantial improvement is expected as to the toughness. As the metal phase increases above 30 vol %, the metal phase has an increased chance of contacting to each other to thereby bring about correspondingly large grain growth of the metal phase during the sintering to such an extent as not to successfully migrate the metal particles into the grains of the ceramic matrix, whereby exhibiting gradual lowering of the toughness with the increase of the metal phase.When exceeding 50 mol %, the metal phase is inhibited from migrating into the grains of the ceramic matrix during the sintering to be thereby left in the grain boundaries of the ceramic matrix, resulting in a critical strength drop.
The metal element constituting the metal phase is selected in consideration of the sintering compatibility with the ceramic matrix, and includes Ti, Zr, Hf from group IVa, V,
Nb, Ta from group Va, and Cr, Mo, W from group VIa of the periodic table. One or more of such metal element can be selected as constituting the metal phase. The metal phase may be obtained from a starting material of either metal element itself, metal oxide, metal hydride, or metal alkoxide.
Considering the sintering compatibility between the ceramic matrix and the metal phase in terms of coefficient of expansion, it is preferred to disperse the metal phase having coefficient of expansion less than that of the ceramic matrix since it will contribute to effectively improving the toughness of the ceramic matrix, although the present invention is not limited thereto. When the ceramic matrix is formed form the metal oxide including A1203, MgO, and partially stabilized zirconia. but excluding mullite and cordierite, the above listed metal elements are all found satisfactory as they have individual melting points greater than the sintering temperature of the ceramic -matrix as well as individual coefficients of expansion less than that of the ceramic matrix. When, on the other hand, oxide ceramics of mullite and cordierite as well as non-oxide ceramics of Si3N4, SiC, and
A1N are known to have coefficients of expansion nearly equal to that of the above listed metal elements and are found nevertheless to be improved in toughness by the incorporation of the metal element or elements.
Now, discussion will be made as to a mechanism of improving the toughness and high temperature strength of the ceramic-metal composite product of the present invention. The metal phase or metal particles, which are dispersed within the grains of the ceramic matrix and partially in the grain boundaries thereof, will act to inhibit abnormal grain growth of the ceramic matrix during the sintering and therefore provide a fine structure, thereby minimizing origins of fracture and therefore improve the strength remarkably, in addition to that the dispersed metal particles, due to the inherent plastic deformability, improve the toughness. Such improved toughness is attributed to the behavior of the dispersed metal particles which will blunt or pin the leading edge of a crack being propagated so as to relieve stress concentration at the leading edge of the crack.
In a ceramic-metal composite product incorporating the metal phase having coefficient of expansion less than that of the ceramic matrix, the metal phase acts to improve the toughness more effectively. Discrepancy in expansion coefficient between the metal phase and the ceramic matrix will leave residual stress fields in the ceramic matrix and around the metal phase during cooling of the ceramic-metal composite product subsequent to the sintering, which residual stress fields act on the propagation path of the cracks to block further crack propagation. That is, during the cooling process the metal phase of less expansion coefficient will cause therearound tensile stress and therefore the residual stress fields by the presence of which the cracks are caused to propagate in such a manner as to be attracted to the metal phase, thereby inducing transgranular fracture.Thus, the crack will have an increased chance of colliding against the metal phase having plastic deformability to be thereby effectively blocked from further propagating. Considering the improvement in toughness in terms of effective fracture energy, the blocking of the crack propagation is expected to yield an increased surface energy of about 0.5 to 6 J/m2, while the plastic deformation of metal phase is expected to absorb the energy as much as about 2000 to 3000 J/m2. Thus, the metal phase of plastic deformability can give rise to a stress relief mechanism at the leading end of the crack to thereby remarkably improve the toughness to such an extent that has not been expected.In addition, during the cooling of the ceramic-metal composite product subsequent to the sintering, the metal phase dispersed in the ceramic matrix will cause in its axial directions residual compression stress fields which strengthen the grains of the ceramic matrix itself to fuhrer improve the strength of the composite product. It is noted at this time that the remarkably improved toughness is also attributed to the fact that the leading end of the crack is caused to bow or deflect between the adjacent metal particles of the metal phase as the crack propagates.
As to the high temperature strength, the metal phase dispersed within the grains of the ceramic matrix provides the following effects which are available even at high temperatures to give an improved high temperature strength to the ceramic-metal composite product. One effect is that the metal phase will inhibit matrix dislocation and therefore restrain plastic deformation at high temperatures, thereby improving creep strength. Another effect is that the residual compression stress produced in the axial directions of the metal phase will act to restrain grain boundary sliding or cavity formation which would otherwise lower the high temperature strength. The other effect is that the residual tensile stress produced around the metal phase will act to induce the transgranular fracture even at the high temperature.By reason of the above, the ceramic-metal composite product is expected to exhibit no critical lowering in strength even at an elevated temperature of 1000 "C.
In the first method 1) of fabricating the ceramic-metal composite product from a powder mixture containing a ceramic powder and at least one metal element selected from groups
IVa, Va, and VIa of the periodic table, the powder mixture is prepared as a blend of the ceramic power having an average particle size of 0.5 ym or less and a metal powder having an average particle size of 1 im or less.Alternately, the powder mixture may be prepared by coating the ceramic powder of an average particle size of 0.5 ssm or less with the metal and milling a resulting composite powder into a fine particle size, or may be prepared by coating granules of the aggregated ceramic powder of an average particle size of 0.5 4m or less with the metal and milling resulting coated granules into a fine particle size. The blend of the powder mixture is carried out, for example, by placing a suitable proportion of ceramic powder and the metal powder together with a suitable solvent such as ethanol, acetone, toluene into a wet ball-mill in order to mill the mixture followed by heating it to provide a fine composite powder.The powder mixture may be alternately intermixed and milled in an inert gas atmosphere such as argon or the like by means of a dry ball mill. The resulting blend or fine composite powder is pressed or molded by means of the. conventional shape forming presses such as a dry press or injection molding into a compact of desired shape. Subsequently, the compact is sintered either at atmospheric pressure or vacuum condition with a gas-pressure press, hot-press, or hot hydraulic press [HIP] to obtain a sintered ceramic-metal composite product of fine structure.
The sintering and compact forming may be made simultaneously.
In order to avoid oxidization of the ceramic powder and the metal powder, the sintering is preferably made in a vacuum, inert gas atmosphere of nitrogen and argon, or in a reducing gas atmosphere of hydrogen. When sintering by the use of the hot hydraulic press, the compact may be preliminary heated at atmospheric pressure or with the use of the hot-press into a preliminary heated product with a reduced number of open pores, or the compact may be capsulized by means of airtight metal or glass seal prior to being sintered in the hydraulic press.
In the second method 2) of fabricating the ceramic-metal composite product from the powder mixture of the ceramic powder and the metal or oxide thereof, the powder mixture is preliminary heated in an atmospheric environment in order to produce composite oxides of the ceramic and the metal. The resulting composite oxides of the ceramic and the metal will allow the corresponding metal to precipitate as very fine particles in the ceramic matrix during the subsequent sintering in the reducing gas environment, thereby enabling to effect nano-order intragranular dispersion of the metal particles within the grains of the ceramic matrix. In thus obtained nano-order ceramic composite, the interface between the metal particles and the ceramic matrix is very activated to provide a strong interface bonding force responsible for excellent toughness as well as strength.The powder mixture of ceramic and metal and/or metal oxide is prepared as a blend of the ceramic powder-and a metal and/or metal oxide powder in suitable proportions, and is placed together with a suitable solvent such as ethanol, acetone, toluene into a wet ball-mill to mill the mixture followed by heating it to provide a fine composite powder. The powder mixture may be alternately milled in a dry condition in the presence of an inert gas such as argon or the like by means of a dry ball mill.
The preliminary heating is carried out, preferably but not limited to, at a temperature of 500 to 1200 C for 1 to 24 hours in the presence of oxygen in-order to produce the composite oxides of the ceramic and the metal. Further, it is also preferable to again mil the preliminary heated product into a corresponding powder for use in the subsequent sintering. Such milling may be carried out by the use of a dry ball mill or alternately by placing the preliminary heated product together with the solvent such as ethanol, acetone or toluene into a wet ball mill and drying the resulting powder.
The resulting powder is pressed or molded by means of the conventional shape forming presses such as a dry press or injection molding into a compact of desired shape.
Subsequently, the compact is sintered either at atmospheric pressure or vacuum condition with a gas-pressure press, hotpress, or hot hydraulic press [HIP] to obtain a sintered ceramic-metal composite product of fine structure. The sintering and compact forming may be made simultaneously. The sintering should be carried out in the reduced gas atmosphere such as hydrogen until the metal oxide is reduced to the metal particles to be dispersed in the ceramic matrix. Once the reduction of the metal oxide is achieved, the subsequent sintering is carried out preferably in a vacuum, inert gas atmosphere of nitrogen and argon, or in a reducing gas atmosphere of hydrogen in order to avoid oxidization of the ceramic powder and the metal powder.When sintering with the hot hydraulic press, the compact may be preliminary heated at atmospheric pressure or with the use of the hot-press into a preliminary heated product with a reduced number of open pores, or the compact may be capsulized by means of airtight metal or glass seal prior to being sintered in the hydraulic press.
In the third method 3) of fabricating the ceramic-metal composite product from the powder mixture of the ceramic powder and the metal oxide or hydride, the powder mixture is sintered in a reducing environment such that the metal oxide or hydride will precipitate as very fine metal particles in the ceramic matrix, thereby activating energetically the interfaces between the metal particles and the ceramic matrix and therefore giving a very strong interface bonding force responsible for excellent toughness as well as strength. The powder mixture is prepared as a blend of the ceramic powder and a metal oxide or hydride in suitable proportions, and is placed together with a suitable solvent such as ethanol, acetone, toluene into a wet ball-mill to mill the mixture followed by heating it to provide a fine composite powder.
Alternately, the powder mixture of the ceramic powder and metal oxide or hydride may be pulverized mechanochemically in a dry condition by the use of a ball mill, planetary ball mill, or high energy ball mill [known as the Attoritor" available from Union Process Corp.] into a very fine powder mixture in which the metal oxide or hydride is pulverized into substantially amorphous state. With such fine powder mixture, it is possible to precipitate an extremely fine metal particles in the ceramic matrix during the sintering in the reducing environment to thereby effect nano-order intragranular dispersion of the metal particles in the grains of the ceramic matrix.
The powder mixture is pressed or molded by means of the conventional shape forming presses such as a dry press or injection molding into a compact of desired shape.
Subsequently, the compact is sintered either at atmospheric pressure or vacuum condition with a gas-pressure press, hotpress, or hot hydraulic press [HIP] to obtain a sintered ceramic-metal composite product of fine structure. The sintering and compact forming may be made simultaneously. The sintering should be carried out in the reduced gas atmosphere such as hydrogen until the metal oxide or hydride is reduced to the metal particles dispersed in the ceramic matrix. Once the reduction of the metal oxide or hydride is achieved, the subsequent sintering is carried out preferably in a vacuum, inert gas atmosphere of nitrogen and argon, or in a reducing gas atmosphere of hydrogen in order to avoid oxidization of the ceramic powder and the metal powder.When sintering with the hot hydraulic press, the compact may be preliminary heated at atmospheric pressure or with the use of the hot-press into a preliminary heated product with a reduced number of open pores, or the compact may be capsulized by means of airtight metal or glass seal prior to being sintered in the hydraulic press.
In the fourth method 4) of fabricating the ceramic-metal composite product from the mixture of the ceramic powder, metal alkoxide, and alcohol, the mixture is firstly hydrolyzed to provide fine particles of the corresponding metal oxide dispersed in the alcohol and is then heated to obtain the fine metal oxide. During the subsequent sintering in a reducing environment, such fine metal oxide can be reduced to the corresponding metal such that the metal can precipice as very fine metal particles in the ceramic matrix, thereby effecting nano-order intragranular dispersion of the metal particles in the grains of the ceramic matrix.Such nano-order dispersion will activate energetically the interfaces between the metal particles and the ceramic matrix and therefore giving to the ceramic-metal composite product a very strong interface bonding force responsible for excellent toughness as well as strength.
The heating of the ceramic and metal oxide mixture after the hydrolysis is carried out, for example, preferably but not limited to, at a temperature of 800 C for several hours. The resulting powder mixture is pressed or molded by means of the conventional shape forming presses such as a dry press or injection molding into a compact of desired shape.
Subsequently, the compact is sintered either at atmospheric pressure or vacuum condition with a gas-pressure press, hotpress, or hot hydraulic press [HIP] to obtain a sintered ceramic-metal composite product of fine structure. The sintering and compact forming may be made simultaneously. The sintering should be carried out in the reduced gas atmosphere such as hydrogen until the metal oxide is reduced to the metal particles dispersed in the ceramic matrix. Once the reduction of the metal oxide is achieved, the subsequent sintering is carried out preferably in a vacuum, inert gas atmosphere of nitrogen and argon, or in a reducing gas atmosphere of hydrogen in order to avoid oxidization of the ceramic powder and the metal powder.When sintering with the hot hydraulic press, the compact may be preliminary heated at atmospheric pressure or with the use of the hot-press into a preliminary heated product with a reduced number of open pores, or the compact may be capsulized by means of airtight metal or glass seal prior to being sintered in the hydraulic press.
In the fifth method 5) of fabricating the ceramic-metal composite product from the mixture of a metal alkoxide and the alkoxide of a ceramic constituting element in an alcohol, the mixture or alcohol solution is firstly hydrolyzed to provide fine particles of the ceramic and metal oxide dispersed in the alcohol and is then heated to obtain the fine particles.
During the subsequent sintering in a reducing environment, the fine metal oxide can be reduced to the corresponding metal such that the metal can precipice as very fine metal particles in the ceramic matrix, thereby effecting nano-order intragranular dispersion of the metal particles in the grains of the ceramic matrix. Such nano-order dispersion will activate energetically the interfaces between the metal particles and the ceramic matrix and therefore giving to the ceramic-metal composite product a very strong interface bonding force responsible for excellent toughness as well as strength. This method is basically identical to the above fourth method 4) except that the alkoxide of a ceramic constituting element is utilized instead of the ceramic powder. Therefore, the compact forming and the sintering can be made in the identical manner as in the fourth 4) method.
In the fifth method 6) of fabricating the ceramic-metal composite product from the mixture of a metal alkoxide and the alkoxide of a ceramic constituting element in an alcohol, the mixture or alcohol solution is firstly heated to provide a composite alkoxide which is subsequently hydrolyzed to give rise to a correspondingly composite oxide particle of the ceramic and the metal dispersed in the alcohol and is then heated to obtain the fine composite oxide particles. During the subsequent sintering in a reducing environment, the fine composite oxide particles are converted into the corresponding ceramic matrix and the metal phase which is caused to precipitate as very fine metal particles in the resulting ceramic matrix, thereby effecting nano-order intragranular dispersion of the metal particles in the grains of the ceramic matrix.Such nano-order dispersion will activate energetically the interfaces between the metal particles and the ceramic matrix and therefore giving to the ceramic-metal composite product a very strong interface bonding force responsible for excellent toughness as well as strength.
The heating for providing the composite alkoxide is carried out, preferably but not limited thereto, at a temperature of 100 C for several hours. This method is basically identical to the above fourth method 5) except that the composite alkoxide is additionally provided by heating prior to the hydrolysis. Therefore, the compact forming and the sintering can be made in the identical manner as in the fourth 5) method.
The following examples and comparative examples show the comparative results with the metal particles dispersed in varying proportions in the ceramic matrix, but it is to be understood that these examples are given by way of illustration and not of limitation.
Examples 1 to 6 and comparative Examples 1 to 2
A 99.9% or more pure alumina powder [a-A1203] having an average particle size of 0.2 Mm was blended with a 99.9 % or more pure tungsten [W] powder having an average particle size of 0.35 pm in added proportions of O to 60 % by volume based upon the total volume, as listed in Table 1, to prepare a powder mixture or pure alumina powder. The resulting powder mixture or pure powder was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 104 Torr or more at a temperature of 1400 "C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 1 to 6 containing added volume of 50 % or less of W were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that W particles are certainly present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in Table 1, that the ratio of W present at the grain boundaries increased with the increased amount of W added, and that substantially all of W particles were seen at the grain boundaries for the sintered product of comparative Example 2 containing 60 % by volume of
W.
Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm. The test specimens were tested with respect to three-point flexural strength at room temperature in accordance with Japanese Industrial Standard (JIS) R-1601. In addition, the test specimens were mirror-polished to be tested with respect to Vickers hardness and to fracture toughness at room temperature in accordance with JIS R-1607, SEPB (single edge precracked beam) method. The test results are listed in
Table 1. The three-point flexural strength is defined to be a strength at which the specimen supported at two spaced supporting points breaks with such strength applied midway between the supporting points.The fracture toughness was measured for the specimen in which a crack had been made midway thereof prior to being subjected to the test.
Table 1
Incorporated Proportion of W Three-point Fracture Vickers amount of W partlcles in the flexural strength toughness Hardness [vol%] matrix graln [%] [MPa] [MPam1/2] [GPa] Example 1 5 85 1125 7.2 18.5 Example 2 10 83 1235 7.7 18.3 Example 3 20 80 1315 8.2 18.0 Example 4 30 70 1310 8.4 17.6 Example 5 40 52 1050 8.6 17.3 Example 6 50 25 705 9.0 16.9 Comparative Example 1 0 . 500 3.0 18.8 Comparative Example 2 60 0 410 9.3 16.5 Table 2
Incorporated Average particle Three-point Fracture Vickers amount of W size of W particles flexural strength toughness Hardness [vol%] [ m] [MPa] [MPam1/2] [GPa] Example 1 5 0.35 1125 7.2 18.5 Comparative Example 3 5 3 525 8.3 18.0 The specimens of Example 1 were also tested with regard to the three-point flexural strength [MPa] over a temperature range of from room temperature to 1400 C to examine the temperature-dependent strength [MPa], which is illustrated in
FIG. 1. As apparent from FIG. 1, the product of Example 1 maintains the flexural strength at the room temperature up to about 1000 C, as opposed to that pure alumina will exhibit critical drop in the flexural strength at about 800 C due to slow crack growth (SCG).
FIG. 2 is a transmission-type electron photomicrograph illustrating a grain structure of the sintered product of
Example 1 in which black dots represent W particles. From the figure, it is confirmed that W particles are dispersed within the grains of a-A1203 and that no reactive phase appears at the interface between Also, and W particles.
FIG. 3 is a scan-type electron photomicrograph illustrating the grain structure in fractured face of the sintered product of Example 1 after subjected to the threepoint flexural strength test in which white dots represent W particles. From this figure, it is confirmed that W particles are present within the grains of the a-Al203 and that the fractured face is rather flat which demonstrates the occurrence of transgranular fracture.
Comparative Example 3
A 99.9 % or more pure alumina powder [a-Al203] having an average particle size of 0.2 tm was blended with 5 % by volume, based upon the total volume, of 99.9 % or more pure tungsten [W] powder having an average particle size of 3 ssm to prepare a powder mixture. The powder mixture was processed in the identical manner as in Example 1 to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the W particles are present in the grain boundaries of a-A12O3 from a scan-type electron photomicrograph.Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 2 together with those of Example 1 for comparison.
The specimens of comparative Example 3 were also tested with regard to the three-point flexural strength [MPa] over a temperature range of from room temperature to 1400 C to examine the temperature-dependent strength [MPa], which is illustrated in FIG. 4. As apparent from FIG. 4, comparative
Example 3 shows an abrupt drop in the flexural strength before reaching 1000 C. Also from Table 2, it is known that comparative Example 3 utilizing the W particles of average particle size of 3 ssm show a less three-point flexural strength than Example 1.
Examples 7 to 12 and comParative Examples 4 and 5
A 99.9 % or more pure alumina powder [a-Al203] having an average particle size of 0.2 im was blended with a 99.9 % or more pure molybdenum [Mo] powder having an average particle size of 0.65 ssm in added proportions of O to 60 % by volume based upon the total volume, as listed in Table 1, to prepare a powder mixture. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 "C followed by being sintered in a vacuum of 10-4 Torr or more at a temperature of 1500 "C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 7 to 12 containing added volume of 50 % or less of Mo were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that Mo particles are certainly present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in Table 3, that the ratio of Mo present at the grain boundaries increased with the increased amount of Mo added, and that substantially all of Mo particles were seen at the grain boundaries for the sintered product of comparative Example 5 containing 60 % by volume of
Mo.
Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 3.
Table 3
Incorporated Proportion of Mo Three-point Fracture Vickers amount of W partlcles in the flexural strength toughness Hardness [vol%] matrix grain [%] [MPa] [MPam1/2] [GPa] Example 7 5 70 1220 7.8 18.0 Example 8 10 68 1315 8.3 17.8 Example 9 20 65 1430 8.8 17.5 Example 10 30 60 1425 9.0 17.1 Example 11 40 46 1150 9.2 16.8 Example 12 50 25 710 9.6 16.4 Comparative Example 4 0 . 500 3.0 18.8 Comparative Example 5 60 0 415 9.9 16.0 Table 4
Incorporated Average particle Three-point Fracture Vickers amount of Mo size of Mo flexural strength toughness Hardness [vol%] Particles [ m] [MPa] [MPam1/2] [GPa] Example 7 5 0.65 1220 7.8 18.0 Comparative Example 6 5 3 570 8.7 17.7 FIG. 5 is a transmission-type electron photomicrograph illustrating a grain structure of the sintered product cf Example 7 in which black dots represent Mo particles.From the figure, it is confirmed that Mo particles are dispersed within the grains of a-Al 203 and that no reactive phase appears at the interface between Al203 and Mo particles.
FIG. 3 is a scan-type electron photomicrograph illustrating the grain structure in fractured face of the sintered product of Example 7 after subjected to the threepoint flexural strength test in which white dots represent Mo particles. From this figure, it is confirmed that Mo particles are present within the grains of the a-Al203 and that the fractured face is rather flat which demonstrates the occurrence of transgranular fracture.
Comparative Example 6
A 99.9 % or more pure alumina powder [a-Al203] having an average particle size of 0.2 /m was blended with 5 % by volume, based upon the total volume, of 99.9 % or more pure molybdenum [Mo] powder having an average particle size of 3 ssm to prepare a powder mixture. The powder mixture was processed in the identical manner as in Example 7 to obtain a diskshaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the Mo particles are present in the grain boundaries of a-Al2O3 by scan-type electron photomicrograph.Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in
Table 4 together with those of Example 7 for comparison. As apparent from Table 4, the-sintered product of comparative
Example 6 has three-point flexural strength less than that of
Example 7.
Examples 13 to 18 and Comparative Examples 7 and 8
A 99.9 % or more pure magnesium oxide powder [MgO3 having an average particle size of 0.1 ssm was blended with a 99.9 % or more pure tungsten [W] powder having an average particle size of 0.35 tm in added proportions of O to 60 % by volume based upon the total volume, as listed in Table 5, to prepare a powder mixture. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 e C followed by being sintered in an argon gas environment at a temperature of 1450 "C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 13 to 18 containing added volume of 50 % or less of W were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that W particles are certainly present within the grains of MgO. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in Table 5, that the ratio of W present at the grain boundaries increased with the increased amount of W added, and that substantially all of W particles were seen at the grain boundaries for the sintered product of comparative Example 8 containing 60 % by volume of
W.
Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 5.
Table 5
Incorporated Proportion of W Three-point Fracture Vickers amount of W partlcles in the flexural strength toughness Hardness [vol%] matrix graln [%] [MPa] [MPam1/2] [GPa] Example 13 5 83 995 6.5 8.0 Example 14 10 81 1100 7.0 7.8 Example 15 20 78 1215 7.5 7.5 Example 16 30 68 1210 7.7 7.1 Example 17 40 50 935 7.9 6.8 Example 18 50 25 495 8.3 6.4 Comparative Example 7 0 . 400 2.5 8.8 Comparative Example 8 60 0 205 8.6 6.0 Table 6
Incorporated Average prticle Three-point Fracture Vickers amount of W size of W particles flexural strength toughness Hardness [vol%] [ m] [MPa] [MPam1/2] [GPa] Example 13 5 0.35 995 6.5 8.0 Comparative Example 9 5 3 460 7.8 7.5 ComParative ExamPle 9
A 99.9 % or more pure magnesium oxide [a-Al203] powder having an average particle size of 0.1 pm was blended with 5 % by volume, based upon the total volume, of 99.9 % or more pure tungsten [W] powder having an average particle size of 3.5 pm to prepare a powder mixture. The powder mixture was processed in the identical manner as in Example 13 to obtain a diskshaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the W particles are present in the grain boundaries of MgO by scan-type electron photomicrograph. Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 6 together with those of Example 13 for comparison. As apparent from
Table 6, the sintered product of comparative Example 9 has three-point flexural strength less than that of Example 13.
ExamPles 19 to 24 and Comnarative Examples 10 and 11
A 98% or more pure a-Si3N4 powder having an average particle size of 0.2 pm was blended with a 99.9 % or more pure molybdenum [Mo] powder having an average particle size of 0.65 pm in added proportions of O to 60 % by volume based upon the total volume, as listed in Table 7, together with 5 % by weight of A1203 and 5% by weight of Y203 to prepare a powder mixture additionally including A1203 and Y203 as sintering promoting agents. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 "C followed by being sintered in an argon gas environment at a temperature of 1800 C for 3 hours as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 19 to 24 containing added volume of 50 % or less of Mo were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that Mo particles are certainly present within the grains of B-SN4. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in Table 7, that the ratio of Mo present at the grain boundaries increased with the increased amount of Mo added, and that substantially all of Mo particles were seen at the grain boundaries for the sintered product of comparative Example 11 containing 60 % by volume of
Mo.
Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 7.
Table 7
Incorporated Proportion of Mo Three-point Fracture Vickers amount of Mo partlcles in the flexural strength toughness Hardness [vol%] matrix grain [%] [MPa] [MPam1/2] [GPa] Example 19 5 72 1210 7.0 14.5 Example 20 10 70 1320 7.5 14.3 Example 21 20 67 1400 8.0 14.0 Example 22 30 62 1395 8.2 13.6 Example 23 40 48 1135 8.4 13.3 Example 24 50 25 790 8.8 12.9 Comparative Example 10 0 . 600 4.0 15.3 Comparative Example 11 60 0 495 9.1 12.5 Table 8
Incorporated Average particle Three-point Fracture Vickers amount of Mo size of Mo flexural strength toughness Hardness [vol%] Praticles [ m] [MPa] [MPam1/2] [GPa] Example 19 5 0.65 1210 7.0 14.5 Comparative Example 12 5 3.5 575 8.0 14.0 Comparative Example 12
A powder mixture was prepared in the identical manner as in Example 19 except that Mo powder having a larger average particle size of 3.5 ssm was utilized instead of the Mo particles having the average particle size of 0.65 Um. The powder mixture was processed in the identical manner as in
Example 19 to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the
Mo particles are present in the grain boundaries of ss-Si3N4 by scan-type electron photomicrograph. Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in
Table 8 together with those of Example 19 for comparison.As apparent from Table 8, the sintered product of comparative
Example 12 has three-point flexural strength less than that of
Example 19.
Examples 25 to 30 and Comparative Examples 13 and 14
A 99.9 % or more pure mullite [3Alz03 2SiO2] powder having an average particle size of 0.2 ssm was blended with a 99.9 % or more pure tungsten [W] powder having an average particle size of 0.35 pm in added proportions of 0 to 60 % by volume based upon the total volume, as listed in Table 9, to prepare a powder mixture. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment at a temperature of 1600 "C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 25 to 30 containing added volume of 50 % or less of W were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that W particles are certainly present within the grains of mullite. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in Table 9, that the ratio of W present at the grain boundaries increased with the increased amount of W added, and that substantially all of W particles were seen at the grain boundaries for the sintered product of comparative Example 14 containing 60 % by volume of
W.
Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 9.
Table 9
Incorporated Proportion of W Three-point Fracture Vickers amount of W partlcles in the flexural strength toughness Hardness [vol%] matrix graln [%] [MPa] [MPam1/2] [GPa] Example 25 5 85 750 4.7 11.5 Example 26 10 83 825 5.1 11.2 Example 27 20 79 905 5.5 10.8 Example 28 30 72 900 5.7 10.2 Example 29 40 50 705 5.9 9.7 Example 30 50 25 370 6.3 9.2 Comparative Example 13 0 . 300 1.8 11.6 Comparative Example 14 60 0 155 6.6 8.7 Table 10
Incorporated Average prticle Three-point Fracture Vickers amount of W size of W Particles flexural strength toughness Hardness [vol%] [ m] [MPa] [MPam1/2] [GPa] Example 25 5 0.35 750 4.7 11.5 Comparative Example 15 5 3.5 345 5.6 10.7 Comnarative ExamPle 15
A powder mixture was prepared in the identical manner as in Example 25 except that W powder having a larger average particle size of 3.5 pm was utilized instead of the W particles having the average particle size of 0.35 ssm. The powder mixture was processed in the identical manner as in
Example 25 to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the
W particles are present in the grain boundaries of mullite by scan-type electron photomicrograph. Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in
Table 10 together with those of Example 25 for comparison.As apparent from Table 10, the sintered product of comparative
Example 15 has three-point flexural strength less than that of
Example 25.
ExamPles 31 to 36 and comParative Examples 16 and 17
A partially stabilized zirconia powder having an average particle size of 0.2 ssm and containing 12 mol % of CeO2 was blended with a 99.9 % or more pure tungsten [W] powder having an average particle size of 0.35 ssm in added proportions of 0 to 60 % by volume based upon the total volume, as listed in
Table 11, to prepare a powder mixture. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene-coated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a highpure alumina-made mold and sintered in an argon gas environment at a temperature of 1400 C for 2 hours as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product of Examples 31 to 36 containing added volume of 50 % or less of W were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that W particles are certainly present within the grains of partially stabilized zirconia. By chemical and
X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions as listed in
Table 11. Also it was confirmed that the ratio of minute W particles present at the grain boundaries increased with the increased amount of W added, and that substantially all of W particles were seen at the grain boundaries for the sintered product of comparative Example 17 containing 60 % by volume of
W.Further, it was seen that all the sintered products of
Examples 31 to 36 and comparative Examples 16 and 17 have a crystalline structure of cubic system. Then, the disk-shaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 11.
Table 11
Incorporated Proportion of W Three-point Fracture Vickers amount of W partlcles in the flexural strength toughness Hardness [vol%] matrix graln [%] [MPa] [MPam1/2] [GPa] Example 31 5 84 1390 12.8 10.9 Example 32 10 82 1470 13.2 10.6 Example 33 20 79 1590 13.5 10.2 Example 34 30 70 1570 13.8 9.6 Example 35 40 53 1320 14.0 9.1 Example 36 50 25 990 14.3 8.6 Comparative Example 16 0 . 700 8.0 11.0 Comparative Example 17 60 0 605 14.5 8.1 Table 12
Incorporated Average particle Three-point Fracture Vickers amount of W size of W Particles flexural strength toughness Hardness [vol%] [ m] [MPa] [MPam1/2] [GPa] Example 31 5 0.35 1390 12.6 10.9 Comparative Example 18 5 3.5 840 13.3 10.2 Comparative Example 18
A powder mixture was prepared in the identical manner as in Example 31 except that W powder having a larger average particle size of 3.5 ssm was utilized instead of the W particles of 0.35 ttm average particle size. The powder mixture was processed in the identical manner as in Example 31 to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the W particles are present in the grain boundaries of partially stabilized zirconia by scan-type electron photomicrograph. Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 12 together with those of
Example 31 for comparison.As apparent from Table 12, the sintered product of comparative Example 18 has three-point flexural strength less than that of Example 31.
Examples 37 to 42 and Comparative ExamPles 19 and 20
5% by volume of 99.9 % or more pure molybdenum [Mo] powder having an average particle size of 0.65 ssm was blended with a partially stabilized zirconia powder having an average particle size of 0.2 ssm and containing CeO2 in proportions from 0 to 35 mol %, as listed in Table 13, to prepare a powder mixture. The resulting power mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylenecoated iron balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was then molded in a high-pure alumina-made mold and sintered in an argon gas environment at a temperature of 1400 "C for 2 hours as being compressed at a pressure of 30 MPa to obtain a diskshaped sintered product of 50 mm diameter and 4 mm thick.
The sintered products of Examples 37 to 42 and comparative Examples 19 and 20 were all found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and were also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that Mo particles are certainly present within the grains of partially stabilized. zirconia.By X-ray diffraction analysis for crystalline identification, the zirconia was found to have all the crystal structures of tetragonal system for Examples 37 to 41 containing 5 to 20 mol % of CeO2, to have a mixed structure of tetragonal system partially mixed with cubic system for Example 42 containing 30 mol % of CeO2, to have all the structure of cubic system for comparative Example 20 containing 35 mol % of CeO2, and to have all the structure of orthorhombic system for comparative
Example 19 containing no CeO2. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions.Then, the diskshaped sintered product were all cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 13.
Table 13
Incorporated Average particle Three-point Fracture Vickers amount of size of Mo flexural strength toughness Hardness CeO2[mol%] Particles[ m] [MPa] [MPam1/2] [GPa] Example 37 5.0 0.65 1080 14.8 10.0 Example 38 8.0 0.65 1260 14.4 10.3 Example 39 12.0 0.65 1380 12.6 10.8 Example 40 16.0 0.65 1280 12.1 11.2 Example 41 20.0 0.65 1030 11.7 11.3 Example 42 30.0 0.65 980 9.6 11.5 Comparative Example 19 0.0 0.65 200 1.5 9.5 Comparative Example 20 35.0 0.65 300 2.0 11.8 Table 14
Incorporated Average particle Three-point Fracture Vickers amount of size of Mo flexural strength toughness Hardness CeO2[mol%] Particles[ m] [MPa] [MPam1/2] [GPa] Comparative Example 21 5.0 3.5 645 15.8 9.4 Comparative Example 22 8.0 3.5 755 15.4 9.6 Comparative Example 23 12.0 3.5 830 13.3 10.1 Comparative Example 24 16.0 3.5 737 12.7 10.5 Comparative Example 25 20.0 3.5 615 12.3 10.6 Comparative Example 26 30.0 3.5 585 10.1 10.8 ComParative Examples 21 to 26
A powder mixture was prepared in the identical manner as in Example 37 except that Mo powder having a larger average particle size of 3.5 m was utilized instead of the Mo particles of 0.65 pm average particle size with the partially stabilized zirconia containing CeO2 in proportions, as listed in Table 14.The powder mixture was processed in the identical manner as in Example 37 to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick, which was found to be of fine structure having relative density of 99 % or more and porosity of 1 % or less, but was observed to have substantially all the Mo particles are present in the grain boundaries of partially stabilized zirconia by scan-type electron photomicrograph. By X-ray diffraction analysis for crystalline identification, the zirconia was found to have all the crystal structures of tetragonal system for comparative
Examples 21 to 25 containing 5 to 20 mol % of CeO2, and to have a mixed structure of tetragonal system partially mixed with cubic system for comparative Example 26 containing 30 mol % of
CeO2. By chemical and X-ray diffraction quantitative analysis it was confirmed that the individual sintered products had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered product were cut and grounded into corresponding test specimens measuring 4 x 3 x 35 mm and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature,
Vickers hardness, and fracture toughness at room temperature.
The test results are listed in Table 14. As apparent from
Tables 13 and 14, the sintered product of comparative Examples 21 to 26 incorporating the coarse Mo powder of an average particle size of 3.5 Mm show three-point flexural strength less than that of Examples 37 to 42 incorporating the minute
Mo powder of an average particle size of 0.65 ssm.
Example 43
A 99.9 % or more pure a-Al203 powder having an average particle size of 0.2 tm was coated by the physical vapor deposition (PVD) technique with vanadium layer to prepare a composite powder containing 5 % by volume, based upon the total volume, of vanadium [V]. The resulting composite powder was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone-and was milled for 48 hours. The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10-4 Torr at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 70 % or more of plate-like and granular V phase are present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 15.
Example 44
A 99.9 % or more pure a-Al203 powder having an average particle size of 0.2 pm was blended with polyvinylalcohol to prepare a powder mixture containing 3 % by weight of polyvinylalcohol. The resulting powder was pelletized by the spray-and-dry technique to provide a pelletized powder which was then coated by the physical vapor deposition (PVD) technique with niobium layer to prepare a composite pelletized powder containing 5 % by volume, based upon the total volume, of niobium [Nb]. The resulting composite pelletized powder was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours.The resulting fine powder was then molded in a graphite-made mold and sintered in a hydrogen reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10 Torr at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 70 % or more of plate-like and granular Nb phase are present within the grains of a-A1203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 15.
Table 15
Incorporated Metal Three-point Fracture Vickers amount of Incorporated flexural toughness Hardness Metal [volO/o] strength [MPamyl [GPa] [MPa] Example 43 5 V 1185 7.6 17.8 Example 44 5 Nb 1200 7.5 18.0 ExamPle 45
A 99.9 % or more pure y-Al203 powder having a BET specific surface area of 200 m2/g was blended with a 99.9 % or more pure W03 powder having an average particle size of 0.35 m in such proportions as to prepare a powder mixture which, after sintering, produces a-A1203 and W in a volume ratio of 95 to 5.
The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 24 hours. The resulting fine powder was heated preliminary in an atmospheric environment at a temperature of 900 C for 8 hours to obtain a preliminary product composed of Al203 and a composite oxide
AlWO4.Thus obtained preliminary product was milled in a dry ball mill in an argon gas environment to provide a fine composite powder which was then molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment containing 10 % by volume of hydrogen at a temperature of 1400 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick. The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type-electron photomicrograph and transmission-type electron photomicrograph that about 80 % or more of W phase were present within the grains of all203. By chemical and Xray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 16.
Example 46
A 99.9 % or more pure a-A12O3 powder having an average particle size of 0.2 pm was blended with a 99.9 % or more pure
MoO3 powder having an average particle size of 0.65 m in such proportions as to prepare a powder mixture which, after sintering, produces a-Al203 and Mo in a volume ratio of 95 to 5. The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 24 hours.The resulting fine powder was heated preliminary in an atmospheric environment at a temperature of 900 0C for 8 hours to obtain a preliminary product composed of Al203 and a composite oxide A12 (MoO4) 3. Thus obtained preliminary product was milled in a dry ball mill in an argon gas environment to provide a fine composite powder which was then molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10 4 Torr at a temperature of 1500 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 80 % or more of Mo phase were present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions. Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 16.
Table 16
Three-point Fracture Vickers flexural strength toughness Hardness [MPa] [MPamh] [GPa] Example 45 1350 7.1 18.5 Example 46 1380 8.2 18.0 Example 47
A 99.9 % or more pure a-Al203 powder having an average particle size of 0.2 m was blended with a 99.9 % or more pure WO3 powder having an average particle size of 0.35 tm in such proportion as to prepare a powder mixture which, after sintering produces t-Al203 and W in volume ratio of 95 to 5.
The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours. The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 "C followed by being sintered in a vacuum of 10-4 Torr at a temperature of 1400 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 80 % or more of W phase were present within the grains of a-A1203. By chemical and Xray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 48
A 99.9 % or more pure a-Al203 powder having an average particle size of 0.2 pm was blended with a 99.9 % or more pure
MoO3 powder having an average particle size of 0.65 ym in such proportions as to prepare a powder mixture which, after sintering produces Al203 and Mo in a volume ratio of 95 to 5.
The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours. The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10 4 Torr at a temperature of 1500 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 70 % or more of Mo phase were present within the grains of a-Al2O3. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 49
A 99.9 % or more pure a-Al2O3 powder having an average particle size of 0.2 ssm was blended with a 99.9 % or more pure Nb2O5 powder having an average particle size of 0.5 tm in such proportions as to prepare a powder mixture which, after sintering, produces A1203 and Nb in a volume ratio of 95 to 5.
The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours. The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10-4 Torr at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 70 % or more of Nb phase were present within the grains of a-A1203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 50
A 99.9 % or more pure mullite [3Al203 2SiO2] powder having an average particle size of 0.2 pm was blended with a 99.9 % or more pure W03 powder having an average particle size of 0.35 pm in such proportions as to prepare a powder mixture which, after sintering, produces 3Al203 2SiO2 and W in a volume ratio of 95 to 5. The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours.The resulting fine powder was molded in a graphitemade mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment at a temperature of 1600 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 80 % or more of W phase were present within the grains of mullite. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 51
A 99.9 % or more pure a-Si3N4 powder having an average particle size of 0.2 pm was intermingled with 5 % by weight of
Al203 and 5 % by weight of Yz05 to prepare a mixture containing Awl203 and Y205 as sintering promoting agents. The mixture was blended with a 99.9 % or more pure V205 powder having an average particle size of 0.4 ssm in such proportions as to prepare powder mixture which, after sintering, produces ss-Si3N4 and V in a volume ratio of 95 to 5. The powder mixture was placed in a wet ball mill, composed of alumina-made vessel and alumina-made balls, together with a solvent of acetone and was milled for 48 hours.The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 "C followed by being sintered in an argon gas environment at a temperature of 1800 C for 3 hours as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 70 % or more of V phase were present within the grains of ss-Si3N4. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 52
A 99.9 % or more pure MgO powder having an average particle size of 0.1 ssm was blended with a TiH2 powder having an average particle size of 30 ssm in such proportions as to prepare a powder mixture which, after sintering, produces MgO and T in a volume ratio of 95 to 5.The powder mixture was placed in a wet ball mill, composed of polyethylene-made vessel and polyethylene coated iron balls, together with a solvent of acetone and was milled for 72 hours to such an extent that TiH2 powder was milled into an average particle size of about 0.2 ssm. The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 80 % or more of Ti phase were present within the grains of MgO. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 53
A 99.9 % or more pure a-A1203 powder having an average particle size of 0.2 ssm was blended with a WO3 powder having an average particle size of 0.35 Um in such proportions as to prepare a powder mixture which, after sintering, produces a Awl203 and W in a volume ratio of 95 to 5. The powder mixture was placed in a planetary ball mill, composed of a pot and balls both made of partially stabilized zirconia, and was milled in a dry condition for 24 hours.The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in a vacuum of 10-4 Torr at a temperature of 1400 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1.% or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that-about 90 % or more of W phase were present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 54
A 99.9 % or more pure a-Al2O3 powder having an average particle size of 0.2 tm was blended with a MoO3 powder having an average particle size of 0.65 ssm in such proportions as to prepare a powder mixture which, after sintering, produces a Awl203 and Mo in a volume ratio of 95 to 5. The powder mixture was placed in a high energy ball mill known as the Attoritor, composed of a pot and balls both made of partially stabilized zirconia, and was milled in a dry condition for 24 hours.The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 "C followed by being sintered in a vacuum of 10-4 Torr at a temperature of 1500 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 -% or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of Mo phase were present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Example 55
A 99.9 % or more pure a-AlQ powder having an average particle size of 0.2 ssm was blended with a Nb2O5 powder having an average particle size of 0.5 jim in such proportions as to prepare a powder mixture which, after sintering, produces a
Al203 and Nb in a volume ratio of 95 to 5. The powder mixture was placed in a ball mill, composed of a pot and balls both made of partially stabilized zirconia, and was milled in a dry condition for 480 hours.The resulting fine powder was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 e C followed by being sintered in a vacuum of 10 Torr at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of Nb phase were present within the grains of a-Al2O3. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 17.
Table 17
Three-point Fracture Vickers flexural strength toughness Hardness [MPa] [MPam"l [GPa] Example 47 1300 7.9 18.5 Example 48 1355 8.6 18.0 Example 49 1330 8.3 18.5 Example 50 880 5.3 11.5 Example 51 1380 8.3 14.5 Example 52 1000 6.8 7.5 Example 53 1330 7.7 18.5 Example 54 1375 8.3 18.0 Example 55 1350 8.2 18.5 Example 56
A 99.9 % or more pure a-A1203 powder having an average particle size of 0.2 jim was dispersed in an ethanol solution containing tri-ethoxy-vanadyl [VO(OC2H5)] to provide a mixture which, after sintering, produces a-Al203 and V in a volume ratio of 95 to 5. The mixture was hydrolyzed by addition of water and was then dried followed by being heated in an atmospheric environment at a temperature of 800 C for 4 hours to obtain a powder mixture of Al203 and V205. The resulting powder mixture was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1500 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of V phase were present within the grains of a-Al203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Example 57
A 99.9 % or more pure MgO powder having an average particle size of 0.1 jim was dispersed in an ethanol solution containing tetra-ethoxy-titan [Ti(OC2H5)4] to provide a mixture which, after sintering, produces MgO and Ti in a volume ratio of 95 to 5.The mixture was hydrolyzed by addition of water and was then dried followed by being heated in an atmospheric environment at a temperature of 800 C for 4 hours to obtain a powder mixture of MgO and TiO2. The resulting powder mixture was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of Ti phase were present within the grains of MgO. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Example 58
A 98 % or more pure a-Si3N4 powder having an average particle size of 0.2 jim was dispersed in an ethanol solution containing penta-ethoxy-tungsten [W(OC2H5)5] together with 5 % by weight of A1203 and 5 % by weight of Y203, to provide a mixture which, after sintering, produces ss-Si3N4 and W in a volume ratio of 95 to 5 and additionally containing Al203 and
Y203 as sintering promoting agents. The mixture was hydrolyzed by addition of water and was then dried followed by being heated in an atmospheric environment at a temperature of 800 C for 4 hours to obtain a powder mixture of a-Si3N4 and W03.
The resulting powder mixture was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1800 "C for 3 hours as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of W phase were present within the grains of ss-Si3N4. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Example 59
A 99.9 % or more pure mullite [3Al203 2SiO2] powder having an average particle size of 0.2 Am was dispersed in an ethanol solution containing penta-ethoxy-tungsten [W(OC2H5)5] to provide a mixture which, after sintering, produces 3Al203 2SiO2 and W in a volume ratio of 95 to 5.The mixture was hydrolyzed by addition of water and was then dried followed by being heated in an atmospheric environment at a temperature of 800 C for 4 hours to obtain a powder mixture of 3A1203.2SiO2 and W03. The resulting powder mixture was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1600 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of W phase were present within the grains of 3Al203 2SiO2. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Example 60
Tri-i-propoxyl-aluminum [Al (O-i-C3H7) 3] and penta-ethoxy
Niobium [Nb(OC2H5)5] were dissolved in ethanol in such proportions as to provide, after sintering, Al203 and Nb in a volume ratio of 95 to 5. Thus prepared ethanol solution was hydrolyzed by addition of water and was then dried followed by being heated in an atmospheric environment at a temperature of 800 "C for 4 hours to obtain a powder mixture of A1203 and Nub205. The resulting powder mixture was molded in a graphitemade mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of Nb phase were present within the grains of a-A1203. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Example 61
Tri-i-propoxyl-aluminum [Al (O-i-C3H7) 3] and penta-ethoxy
Molybdenum tMo(oc2H5) 5] were dissolved in ethanol in such proportions as to produce, after sintering, A1203 and Mo in a volume ratio of 95 to 5. Thus prepared ethanol solution was kept at a temperature of 100 C for 8 hours and was hydrolyzed by addition of water. Then, it was dried followed by being heated in an atmospheric environment at a temperature of 800 C for 4 hours to obtain a powder mixture of Alp03 and MoO3.
The resulting powder mixture was molded in a graphite-made mold and sintered in a hydrogen gas reducing environment up to a temperature of 1000 C followed by being sintered in an argon gas environment including 10 % by volume of hydrogen at a temperature of 1450 C for 1 hour as being compressed at a pressure of 30 MPa to obtain a disk-shaped sintered product of 50 mm diameter and 4 mm thick.
The sintered product was found to have fine structure with relative density of 99 % or more and with porosity of 1 % or less, and was also observed by scan-type electron photomicrograph and transmission-type electron photomicrograph that about 90 % or more of Mo phase were present within the grains of a-Al2O3. By chemical and X-ray diffraction quantitative analysis it was confirmed that the sintered product had the same component proportions as the initial blend proportions.
Then, the disk-shaped sintered products were cut and grounded into corresponding test specimens each measuring 4 x 3 x 35 mm, and were subjected to the same tests as in Example 1 to obtain the three-point flexural strength at room temperature, Vickers hardness, and fracture toughness at room temperature. The test results are listed in Table 18.
Table 18
Three-point Fracture Vickers flexural strength toughness Hardness [MPa] [MPamy2] [GPa] Example 56 1370 7.4 18.0 Example 57 1190 6.6 7.7 Example 58 1400 8.1 14.6 Example 59 905 5.0 11.5 Example 60 1380 8.0 18.5 Example 61 1390 8.1 18.0
Claims (8)
- CLAIMS 1. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: preparing a powder mixture of a ceramic powder having an average particle size of 0.5 gm or less and a metal oxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table; and sintering said powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 2. A method of fabricating a sintered-ceramic-metal composite product comprising the steps of: preparing a powder mixture of a ceramic powder having an average particle size of 0.5 zm or less and a metal oxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table; and heating said powder mixture preliminary in an atmospheric environment to provide a preliminary heated product; and sintering said preliminary product in a reducing environment to obtain said ceramic-metal composite product.
- 3. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: preparing a powder mixture of a ceramic powder having an average particle size of 0.5 zm or less and a metal hydride of at least one metal element selected from groups IVa, Va and VIa of the periodic table; and sintering said powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 4. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: preparing a powder mixture of a ceramic powder having an average particle size of 0.5 Rm or less and a metal oxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table; milling said powder mixture under a dry condition into a fine powder mixture; and sintering said fine powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 5. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: preparing a mixture of a ceramic powder having an average particle size of 0.5 zm or less, a metal alkoxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table, and an alcohol; hydrolysing and heating said mixture into a corresponding powder mixture; and sintering said powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 6. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: dissolving a metal alkoxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table together with an alkoxide of a ceramic constituting element into an alcohol to obtain an alcohol solution thereof; hydrolysing and heating said alcohol solution into a resulting powder mixture; and sintering said powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 7. A method of fabricating a sintered ceramic-metal composite product comprising the steps of: dissolving a metal alkoxide of at least one metal element selected from groups IVa, Va and VIa of the periodic table together with an alkoxide of a ceramic constituting element into an alcohol to provide an alcohol solution thereof; heating said solution to provide a composite alkoxide followed by hydrolysing and heating the resulting composite alkoxide into a powder mixture; and sintering said powder mixture in a reducing environment to obtain said ceramic-metal composite product.
- 8. A method of fabricating a sintered metal-ceramic composite substantially as described in any of the Examples.
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB949785A (en) * | ||||
GB220301A (en) * | 1923-08-09 | 1925-11-02 | Philips Nv | Improved manufacture of highly refractory bodies |
GB741721A (en) * | 1950-11-08 | 1955-12-14 | Onera (Off Nat Aerospatiale) | Improvements in or relating to the production of refractory materials |
GB941886A (en) * | 1960-06-13 | 1963-11-13 | Du Pont | Improvements in or relating to metalliferous compositions |
GB949569A (en) * | 1960-06-13 | 1964-02-12 | E I Du Font De Nemours And Com | Improvements in or relating to metalliferous compositions |
GB985174A (en) * | 1960-08-31 | 1965-03-03 | Ass Elect Ind | Preparation of cermets |
WO1992001645A1 (en) * | 1990-07-24 | 1992-02-06 | Centre National De La Recherche Scientifique (Cnrs) | Composite alumina/metal powders, cermets made from such powders and production methods |
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GB2245557A (en) * | 1990-06-27 | 1992-01-08 | Johnson Matthey Plc | Metal-ceramic composites |
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1991
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Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB949785A (en) * | ||||
GB220301A (en) * | 1923-08-09 | 1925-11-02 | Philips Nv | Improved manufacture of highly refractory bodies |
GB741721A (en) * | 1950-11-08 | 1955-12-14 | Onera (Off Nat Aerospatiale) | Improvements in or relating to the production of refractory materials |
GB941886A (en) * | 1960-06-13 | 1963-11-13 | Du Pont | Improvements in or relating to metalliferous compositions |
GB949569A (en) * | 1960-06-13 | 1964-02-12 | E I Du Font De Nemours And Com | Improvements in or relating to metalliferous compositions |
GB985174A (en) * | 1960-08-31 | 1965-03-03 | Ass Elect Ind | Preparation of cermets |
WO1992001645A1 (en) * | 1990-07-24 | 1992-02-06 | Centre National De La Recherche Scientifique (Cnrs) | Composite alumina/metal powders, cermets made from such powders and production methods |
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GB2276376B (en) | 1995-07-05 |
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