US2568251A - Process for refining refractory carbides - Google Patents
Process for refining refractory carbides Download PDFInfo
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- US2568251A US2568251A US780998A US78099847A US2568251A US 2568251 A US2568251 A US 2568251A US 780998 A US780998 A US 780998A US 78099847 A US78099847 A US 78099847A US 2568251 A US2568251 A US 2568251A
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- 150000001247 metal acetylides Chemical class 0.000 title claims description 28
- 238000007670 refining Methods 0.000 title claims description 22
- 238000000034 method Methods 0.000 title claims description 17
- 230000008569 process Effects 0.000 title description 7
- 239000000203 mixture Substances 0.000 claims description 24
- 229910052751 metal Inorganic materials 0.000 claims description 23
- 239000002184 metal Substances 0.000 claims description 23
- 239000006104 solid solution Substances 0.000 claims description 19
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 18
- 229910052799 carbon Inorganic materials 0.000 claims description 17
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 15
- 229910052760 oxygen Inorganic materials 0.000 claims description 15
- 239000001301 oxygen Substances 0.000 claims description 15
- 229910052721 tungsten Inorganic materials 0.000 claims description 13
- 239000010937 tungsten Substances 0.000 claims description 13
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 12
- 229910052750 molybdenum Inorganic materials 0.000 claims description 11
- 239000011733 molybdenum Substances 0.000 claims description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 9
- 239000012535 impurity Substances 0.000 claims description 9
- 239000010936 titanium Substances 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 6
- 239000000843 powder Substances 0.000 claims description 6
- 229910052719 titanium Inorganic materials 0.000 claims description 6
- 150000002739 metals Chemical class 0.000 claims description 5
- 239000010955 niobium Substances 0.000 claims description 5
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 5
- 229910052715 tantalum Inorganic materials 0.000 claims description 5
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 5
- -1 ZIRCONIM Chemical compound 0.000 claims description 4
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 14
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 12
- 230000004907 flux Effects 0.000 description 9
- 239000000047 product Substances 0.000 description 8
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 8
- 239000000956 alloy Substances 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 7
- 238000001816 cooling Methods 0.000 description 6
- 229910052757 nitrogen Inorganic materials 0.000 description 6
- QIJNJJZPYXGIQM-UHFFFAOYSA-N 1lambda4,2lambda4-dimolybdacyclopropa-1,2,3-triene Chemical compound [Mo]=C=[Mo] QIJNJJZPYXGIQM-UHFFFAOYSA-N 0.000 description 4
- 229910039444 MoC Inorganic materials 0.000 description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 4
- 230000009471 action Effects 0.000 description 4
- 238000011109 contamination Methods 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 239000003870 refractory metal Substances 0.000 description 4
- 229910052726 zirconium Inorganic materials 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 3
- 229910017052 cobalt Inorganic materials 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 239000011872 intimate mixture Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000006233 lamp black Substances 0.000 description 1
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000001546 nitrifying effect Effects 0.000 description 1
- 239000011541 reaction mixture Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
- 229910003468 tantalcarbide Inorganic materials 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 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
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/65—Reaction sintering of free metal- or free silicon-containing compositions
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B32/00—Carbon; Compounds thereof
- C01B32/90—Carbides
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/5607—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on refractory metal carbides
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/5607—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on refractory metal carbides
- C04B35/5611—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on refractory metal carbides based on titanium carbides
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/5607—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on refractory metal carbides
- C04B35/5626—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on refractory metal carbides based on tungsten carbides
Definitions
- This invention relates to refining process for deoxidizing and/or denitrifying carbides or mixtures of carbides of refractory metals of the fourth and fifth periodic groups.
- Refractory carbides of transition metals are generally prepared by reducing the corresponding oxides in the presence of a carburising substance and in a neutral or reducing atmosphere or in vacuum.
- oxides are very difficultly reducible, solid solutions of the protoxides in the carbides, for instance of the type Ti (C. O.) in the case of titanium carbide, are frequently obtained. If, furthermore, the nitrifying action of the nitrogen has not been avoided, ternary solid solutions of carbide, nitride and oxide, particularly Ti (C. N. 0.), are obtained.
- carbides of the group VI are associated with the carbides of the groups IV and V.
- the tungsten carbide enters into solid solution in the carbides of the other groups, but its diffusion is very much delayed by the presence of nitrogen and/or oxygen.
- Attempts have, therefore, been made to heat-treat the alloys at a very high temperature in order to facilitate diffusion, but the final product is found to contain blow-holes which areall the larger and the more numerous as the carbide of the groups IV and V include a larger percentage of foreign elements, such as oxygen and nitrogen, and the operation has been carried out at a higher temperature.
- the process which forms the subject matter of the invention makes it possible to refine impure carbides and to incorporate them in sintered alloys, provided the latter also contain tungsten carbide and/or molybdenum carbide.
- the diffusion of tungsten carbide or molybdenum carbide, or of these two carbides is set up in the carbide, or the mixture of carbides, to be refined.
- This preliminary operation carried out at a high temperature, produces a solid solution of a carbide of the Vlth group in the carbide or carbides subjected to refining.
- Example 1 For refining titanium carbide containing 1% of oxygen, tungsten carbide is used as a reducing agent. Reduction by tungsten carbide follows the reaction 2WC+O CO+WzC and requires 24.5 parts of tungsten carbide for combination with the oxygen in parts of titanium carbide containing 1% oxygen. But it is much better to use an excess of tungsten carbide relatively to the above-indicated stoichiometrically calculated quantity, as, for instance, about 50 to about parts of tungsten carbide per unit of oxygen in the carbide to be refined. According to the invention, the proportion preferred in this case comprises the quantity of tungsten carbide,
- the refining mixture is as follows:
- the constituent powders are intimately mixed.
- the mixture is heated in a gastight' vessel and a vacuum is kept up during the whole operation and during the subsequent cooling.
- the temperature is raised to 1600 C. to 2000 C., and it is kept at the higher temperature for from one to three hours.
- 3 solid solution is .produced which has substantially the composipending upon the temperature above 1300 C. to
- Example II In the presence of a flux, the refining is more rapid. The most convenient way is to use as flux the auxiliary metal which is to serve as a binder during the sintering or else one of the metals incorporated with the auxiliary alloy. The presence of the flux makes it possible to shorten the refining time at constant temperature or to lower the refining temperature with constant time, A metal of the iron family is preferably chosen in the proportion of less than of the weight of the carbides to be treated, usually comprising between about 0.5 and 4%. The correct dispersion of the flux requires some care.
- Example 1 For instance, with the composition shown in Example 1, may be incorporated 3 parts of cobalt to 100 parts of mixture of carbides, the mixture being as follows:
- the refining is carried out at a temperature of 14001700 C. for from one to four hours, in a maintained vacuum. A part of the cobalt distils towards the cold parts of the oven. It is, therefore, necessary to analyse the refined product in order to calculate the supplemental quantity of auxiliary metal to be incorporated with the mixture for the purpose of sintering.
- the carbides to be refined, or their solid solutions must allow the diffusion of one at least of the tungsten or molybdenum carbides in solid solution; it is, therefore, necessary that the products to be refined should retain a solvent power adequate for the molybdenum and tungsten carbides.
- the invention comprises different variants.
- the carbide of tungsten and the carbide of molybdenum can be made to act in their nascent state, for instance by mixing pulverulent tungsten or molybdenum with carbon in a calculated quantity, and with the carbide to be refined, or else it is possible to associate with the reaction mixture carbide of tungsten or of molybdenum, metallic tungsten or molybdenum, and carbon, with the eventual addition of a flux.
- the nascent carbide then becomes more rapidly diffused, and often the refining action is improved.
- Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, said carbide being preformed and contaminated with oxygen as an impurity comprising forming an intimate powder mixture of said impure carbide with carbide of metal selected from the group consisting of tungsten and molybdenum and with added free carbon, and heating said mixture to substantially eliminate said impurity and simultaneously produce a solid solution of carbides of the selected metals.
- Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, said carbide being preformed and having a non-metallic contamination including oxygen chemically com bined with said metal comprising eliminating said contamination and substituting carbon therefor by heating said impure carbide in the presence of carbide of metal selected from the group consisting of tungsten and molybdenum and free carbon in an amount of stoichiometrically equivalent to that of said non-metallic contamination in said impure carbide, to substantially eliminate said contamination and substitute said carbon therefor and simultaneously produce a solid solution of carbides of the selected metals.
- Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium comprising determining the impurity content of oxygen and nitrogen in said carbide, forming an intimate powder mixture of said carbide with carbide of metal selected from the group consisting of tungsten and molybdenum, and with added free carbon in an amount stoichiometrically equivalent to that of said impurity content, heating said mixture to a temperature ranging from about 1600 C. to about 2000C. in vacuo to substantially eliminate said impurity content and substitute said carbon therefor in said impure carbide and simultaneously produce a solid solution of said carbides.
- Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium comprising determining the impurity content of oxygen and nitrogen in said carbide, forming an intimate powder mixture of said carbide with carbide of metal selected from the group consisting of tung- ,n f-i-s sten and molybdenum ⁇ : and with added free carbon in an amount stoichiometrically equivalent to that of saidirnpurity content, heating said mixture to ateinperature ranging from about 1600 C. to about 2000C.
- Method of refining impure titanium carbide containing about 1% of oxygen impurity chemically combined with titanium comprising heating an intimate powder mixture of about 100 parts of titanium carbide with about 108 parts of tungsten carbide and about 1.5 parts of carbon for about one to three hours at about 1600 to 6 2000 C. in vacuo, cooling the product thereby formed while still under vacuum, and subjecting said product to a heat treatment comprising bringing said product to a temperature at least about 1300 C. and thereafter slowly cooling to about 1000 C. in about two to four hours.
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Description
Patented Sept. 18, 1951 PROCESS FOR REFINING REFRACTORY CARBIDES Marcel Oswald, Paris, France, assignor to Societe Le Carbone-Lorraine, Paris, France No Drawing. Application October 20, 1947, SerialNo. 780,998. In France August 4, 1941 Claims. l 1
This invention relates to refining process for deoxidizing and/or denitrifying carbides or mixtures of carbides of refractory metals of the fourth and fifth periodic groups.
Refractory carbides of transition metals are generally prepared by reducing the corresponding oxides in the presence of a carburising substance and in a neutral or reducing atmosphere or in vacuum. When the oxides are very difficultly reducible, solid solutions of the protoxides in the carbides, for instance of the type Ti (C. O.) in the case of titanium carbide, are frequently obtained. If, furthermore, the nitrifying action of the nitrogen has not been avoided, ternary solid solutions of carbide, nitride and oxide, particularly Ti (C. N. 0.), are obtained. Experience has shown that solid solutions of oxides and/or of nitrides in the carbides derived from the metals of the periodic groups IV and V are difficult to sinter with a more fusible auxiliary metal or alloy, because these solutions are not weLted by the melted auxiliary constituent. Instead of obtaining a hard tough alloy withstanding wear, a badly agglomerated substance full of blow-holes, fragile and hardly usable is produced.
Frequently, carbides of the group VI, particularly tungsten carbide, are associated with the carbides of the groups IV and V. The tungsten carbide enters into solid solution in the carbides of the other groups, but its diffusion is very much delayed by the presence of nitrogen and/or oxygen. Attempts have, therefore, been made to heat-treat the alloys at a very high temperature in order to facilitate diffusion, but the final product is found to contain blow-holes which areall the larger and the more numerous as the carbide of the groups IV and V include a larger percentage of foreign elements, such as oxygen and nitrogen, and the operation has been carried out at a higher temperature. In conclusion, it has not been possible to prepare good heat-treated alloys by starting from carbides comprising oxygen and/or nitrogen.
The process which forms the subject matter of the invention makes it possible to refine impure carbides and to incorporate them in sintered alloys, provided the latter also contain tungsten carbide and/or molybdenum carbide. To that end, the diffusion of tungsten carbide or molybdenum carbide, or of these two carbides, is set up in the carbide, or the mixture of carbides, to be refined. This preliminary operation, carried out at a high temperature, produces a solid solution of a carbide of the Vlth group in the carbide or carbides subjected to refining. Accord- Section 1, Public Law 690, August 8, 1946 Patent expires August 4, 1961 ing to a variant, the refining is carried out in the presence of a more fusible metal, which serves as a flux. It is important to incorporate with the pulverulent mixture intended for refining, the
quantity of free carbon calculated according to the composition to be refined, and according to the proportion of carbon which it is desired to leave in the refined product.
The two examples below, referred to each of the main modes of operation, explain the invention. The proportions given are by weight.
Example 1 For refining titanium carbide containing 1% of oxygen, tungsten carbide is used as a reducing agent. Reduction by tungsten carbide follows the reaction 2WC+O CO+WzC and requires 24.5 parts of tungsten carbide for combination with the oxygen in parts of titanium carbide containing 1% oxygen. But it is much better to use an excess of tungsten carbide relatively to the above-indicated stoichiometrically calculated quantity, as, for instance, about 50 to about parts of tungsten carbide per unit of oxygen in the carbide to be refined. According to the invention, the proportion preferred in this case comprises the quantity of tungsten carbide,
which makes it possible to obtain the composition of the double carbide Ti3WC4. In these conditions, the refining mixture is as follows:
Parts Titanium carbide with 1% of oxygen 100 Tungsten carbide 108 Carbon (lamp-black) 1.5
The constituent powders are intimately mixed. The mixture is heated in a gastight' vessel and a vacuum is kept up during the whole operation and during the subsequent cooling. The temperature is raised to 1600 C. to 2000 C., and it is kept at the higher temperature for from one to three hours. After cooling, 3, solid solution is .produced which has substantially the composipending upon the temperature above 1300 C. to
which the solid solution has been brought.
According to the proportion, the nature of the primary substances and the treatment chosen, it is possible to obtain a solid solution or compound such as Ti3WC4 or ZI3WC4 sufiiciently refined for use.
Example II In the presence of a flux, the refining is more rapid. The most convenient way is to use as flux the auxiliary metal which is to serve as a binder during the sintering or else one of the metals incorporated with the auxiliary alloy. The presence of the flux makes it possible to shorten the refining time at constant temperature or to lower the refining temperature with constant time, A metal of the iron family is preferably chosen in the proportion of less than of the weight of the carbides to be treated, usually comprising between about 0.5 and 4%. The correct dispersion of the flux requires some care. It is convenient to prepare beforehand an intimate mixture of the flux and the tungsten or molybdenum carbide by liberating the auxiliary metal and the refractory metal simultaneously in the nascent state by the action of a reducing and carburising gas such as town gas on an intimate mixture of reducible compounds of the auxiliary and refractory metals, so as simultaneously to produce powdered carbon which is distributed between the metallic grains and prevents them from growing. The further carbon necessary to carburise the refractory metal as required is then added and the mixturecarburised to-produce an intimatemixture of the auxiliary metal and the refractor metal carbide.
For instance, with the composition shown in Example 1, may be incorporated 3 parts of cobalt to 100 parts of mixture of carbides, the mixture being as follows:
Parts Titanium carbide with 1% of oxygen 100 Tungsten carbide 108 Cobalt 6.24 Carbon 1.5
The refining is carried out at a temperature of 14001700 C. for from one to four hours, in a maintained vacuum. A part of the cobalt distils towards the cold parts of the oven. It is, therefore, necessary to analyse the refined product in order to calculate the supplemental quantity of auxiliary metal to be incorporated with the mixture for the purpose of sintering.
B refining with manganese, or an alloy rich in manganese, it is possible more easily to distil this very volatile metal under chosen operative conditions. Whatever the flux is, its amount must remain insufficient to cause the binding of. the mixture. In the particular case chosen, the operation may be concluded by the heat treatment described in the aforesaid application Serial No. 764,900 and the double carbide TiaWC-i, correctly refined, may be obtained.
The processes described in Examples I and II apply, without any notable modifications, to the refining of several carbides, either mixed or already in solid solutions, under the action of tungsten or molybdenum carbide. It is possible, for example, to refine by this process mixtures of titanium carbide and tantalum carbide, or of solid solutions of both these carbides, using tungsten carbide for the refining. Finally, it is possible to refine a carbide, a mixture of carbides, a solid solution of carbides, or a mixture of solid solutions of carbides, by the simultaneous action of tungsten and molybdenum carbides, or by the gotion of a solid solution of these carbides with or without a flux.
The only limit to the application of the process is as follows: the carbides to be refined, or their solid solutions, must allow the diffusion of one at least of the tungsten or molybdenum carbides in solid solution; it is, therefore, necessary that the products to be refined should retain a solvent power adequate for the molybdenum and tungsten carbides.
Apart from the above-described methods of execution, the invention comprises different variants. Particularly, the carbide of tungsten and the carbide of molybdenum can be made to act in their nascent state, for instance by mixing pulverulent tungsten or molybdenum with carbon in a calculated quantity, and with the carbide to be refined, or else it is possible to associate with the reaction mixture carbide of tungsten or of molybdenum, metallic tungsten or molybdenum, and carbon, with the eventual addition of a flux. The nascent carbide then becomes more rapidly diffused, and often the refining action is improved.
I claim:
1. Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, said carbide being preformed and contaminated with oxygen as an impurity, the method comprising forming an intimate powder mixture of said impure carbide with carbide of metal selected from the group consisting of tungsten and molybdenum and with added free carbon, and heating said mixture to substantially eliminate said impurity and simultaneously produce a solid solution of carbides of the selected metals.
2, Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, said carbide being preformed and having a non-metallic contamination including oxygen chemically com bined with said metal, the method comprising eliminating said contamination and substituting carbon therefor by heating said impure carbide in the presence of carbide of metal selected from the group consisting of tungsten and molybdenum and free carbon in an amount of stoichiometrically equivalent to that of said non-metallic contamination in said impure carbide, to substantially eliminate said contamination and substitute said carbon therefor and simultaneously produce a solid solution of carbides of the selected metals.
3. Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, comprising determining the impurity content of oxygen and nitrogen in said carbide, forming an intimate powder mixture of said carbide with carbide of metal selected from the group consisting of tungsten and molybdenum, and with added free carbon in an amount stoichiometrically equivalent to that of said impurity content, heating said mixture to a temperature ranging from about 1600 C. to about 2000C. in vacuo to substantially eliminate said impurity content and substitute said carbon therefor in said impure carbide and simultaneously produce a solid solution of said carbides.
4. Method of refining impure carbide of metal selected from the group consisting of titanium, zirconium, tantalum and columbium, comprising determining the impurity content of oxygen and nitrogen in said carbide, forming an intimate powder mixture of said carbide with carbide of metal selected from the group consisting of tung- ,n f-i-s sten and molybdenum}: and with added free carbon in an amount stoichiometrically equivalent to that of saidirnpurity content, heating said mixture to ateinperature ranging from about 1600 C. to about 2000C. in vacuo for about one to three hours, cooling the resultant product while still under vacuo, and fsubjecting said product to a heat treatment comprising bringing said prodnot to a temperature at least about 1300 C. and thereafter slowly cooling to about 1000 C. in about two to four hours.
5. Method of refining impure titanium carbide containing about 1% of oxygen impurity chemically combined with titanium, comprising heating an intimate powder mixture of about 100 parts of titanium carbide with about 108 parts of tungsten carbide and about 1.5 parts of carbon for about one to three hours at about 1600 to 6 2000 C. in vacuo, cooling the product thereby formed while still under vacuum, and subjecting said product to a heat treatment comprising bringing said product to a temperature at least about 1300 C. and thereafter slowly cooling to about 1000 C. in about two to four hours.
MARCEL OSWALD.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Name Date 2,119,489 Beer May 31, 1938 2,289,104 Dawihl et a1. 'July '7, 1942 $2,300,558 Driggs Nov. 3, 1942 2,356,009 Schwartzkopf Aug. 15, 1944
Claims (1)
1. METHOD OF REFINING IMPURE CARBIDE OF METAL SELECTED FROM THE GROUP CONSISTING OF TITANIUM, ZIRCONIM, TANTALUM AND COLUMBIUM, SAID CARBIDE BEING PREFORMED AND CONTAMINATED WITH OXYGEN AS AN IMPURITY, THE METHOD COMPRISING FORMING AN INTIMATE POWDER MIXTURE OF SAID IMPURE CARBIDE WITH CARBIDE OF METAL SELECTED FROM THE GROUP CONSISTING OF TUNGSTEN AND MOLYBDENUM AND WITH ADDED FREE CARBON, AND HEATING SAID MIXTURE TO SUBSTANTIALLY ELIMINATE SAID IMPURITY AND SIMULTANEOUSLY PRODUCE A SOLID SOLUTION OF CARBIDES OF THE SELECTED METALS.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2568251X | 1941-08-04 |
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| Publication Number | Publication Date |
|---|---|
| US2568251A true US2568251A (en) | 1951-09-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US780998A Expired - Lifetime US2568251A (en) | 1941-08-04 | 1947-10-20 | Process for refining refractory carbides |
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| Country | Link |
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| US (1) | US2568251A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3535132A (en) * | 1967-12-15 | 1970-10-20 | Atomic Energy Commission | Titanium carbide molten metal barrier and method of production |
| US4046517A (en) * | 1975-02-14 | 1977-09-06 | Ltd. Dijet Industrial Co | Cemented carbide material for cutting operation |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2119489A (en) * | 1936-07-29 | 1938-05-31 | Sirian Wire And Contact Compan | Refractory metal alloys and method of making same |
| US2289104A (en) * | 1940-06-11 | 1942-07-07 | Gen Electric | Method for the production of hardmetal alloys |
| US2300558A (en) * | 1940-07-22 | 1942-11-03 | Fansteel Metallurgical Corp | Contact alloys |
| US2356009A (en) * | 1929-05-16 | 1944-08-15 | American Cutting Alloys Inc | Process for manufacturing hard metal compositions |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2356009A (en) * | 1929-05-16 | 1944-08-15 | American Cutting Alloys Inc | Process for manufacturing hard metal compositions |
| US2119489A (en) * | 1936-07-29 | 1938-05-31 | Sirian Wire And Contact Compan | Refractory metal alloys and method of making same |
| US2289104A (en) * | 1940-06-11 | 1942-07-07 | Gen Electric | Method for the production of hardmetal alloys |
| US2300558A (en) * | 1940-07-22 | 1942-11-03 | Fansteel Metallurgical Corp | Contact alloys |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3535132A (en) * | 1967-12-15 | 1970-10-20 | Atomic Energy Commission | Titanium carbide molten metal barrier and method of production |
| US4046517A (en) * | 1975-02-14 | 1977-09-06 | Ltd. Dijet Industrial Co | Cemented carbide material for cutting operation |
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