US3215510A - Alloy - Google Patents
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- US3215510A US3215510A US313185A US31318563A US3215510A US 3215510 A US3215510 A US 3215510A US 313185 A US313185 A US 313185A US 31318563 A US31318563 A US 31318563A US 3215510 A US3215510 A US 3215510A
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- chromium
- alloy
- carbide
- binder
- nickel
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- 229910045601 alloy Inorganic materials 0.000 title claims description 30
- 239000000956 alloy Substances 0.000 title claims description 30
- 239000011651 chromium Substances 0.000 claims description 35
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 28
- 229910052804 chromium Inorganic materials 0.000 claims description 28
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 13
- 238000005260 corrosion Methods 0.000 claims description 12
- 230000007797 corrosion Effects 0.000 claims description 12
- 229910000599 Cr alloy Inorganic materials 0.000 claims description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 39
- 235000012721 chromium Nutrition 0.000 description 26
- 239000011230 binding agent Substances 0.000 description 23
- 229910052759 nickel Inorganic materials 0.000 description 18
- 239000000203 mixture Substances 0.000 description 16
- 238000005245 sintering Methods 0.000 description 9
- 229910017052 cobalt Inorganic materials 0.000 description 7
- 239000010941 cobalt Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 238000007792 addition Methods 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 239000000843 powder Substances 0.000 description 6
- 229910000990 Ni alloy Inorganic materials 0.000 description 5
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 5
- 229910052721 tungsten Inorganic materials 0.000 description 5
- 239000010937 tungsten Substances 0.000 description 5
- 229910009043 WC-Co Inorganic materials 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 150000001247 metal acetylides Chemical class 0.000 description 4
- 239000002253 acid Substances 0.000 description 3
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 3
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 3
- 239000012071 phase Substances 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 229910003470 tongbaite Inorganic materials 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 229910001339 C alloy Inorganic materials 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910018487 Ni—Cr Inorganic materials 0.000 description 2
- 150000007513 acids Chemical class 0.000 description 2
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 description 2
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 241000288673 Chiroptera Species 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- -1 iron group metals Chemical class 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910001120 nichrome Inorganic materials 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000007665 sagging Methods 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical group C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/067—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds comprising a particular metallic binder
Definitions
- Cemented carbides are well known for their unique combination of hardness, strength and abrasion resistance and are accordingly extensively used in industry as cutting tools, drawing 'dies and wear parts. They are produced by powder metallurgy techniques from one or more refractory carbides of groups 1V, V and VI of the periodic table, bonded or cemented together, by liquid phase sintering, with one or more of the iron group metals.
- the binder metal or alloy must possess a number of important properties and must meet a number of demanding requirements, among which are the following.
- the binder must have, or possess the ability to produce with the carbide through eutectic formation, a reasonable melting point. It must adequately Wet the carbide to produce 'a dense body.
- the binder should not to any material extent enter into an irreversible reaction with the carbide.
- the binder should impart reasonable strength to the cemented carbide alloy.
- tungsten carbidecobalt system Of the possible carbide-binder combinations, the best known and most extensively .used is the tungsten carbidecobalt system.
- a second useful system is titanium carbide in which nickel is the binder. Nickel can also be used in place of cobalt with tungsten carbide but with a 2 generation of strength normally observed makes such WCNiCr C alloys of little value.
- compositions which consist essentially of tungsten carbide and about 10 to about 25%, and not more than 30%, by weight, of a binder of chromium and nickel, the ratio of the weight of chromium to the combined weight of nickel and chromium ranging from about 0.015 to about 0.15.
- the compositions of the invention are prepared by pressing a powdered mixture of tungsten carbide, chromium and nickel within the foregoing ranges, the chromium being present in chemically uncombined form, and then sintering the pressed mixture in a carbon-free atmosphere.
- compositions of the invention possess outstanding corrosion resistance, particularly to acids and alkalis, combined with hardness and strength comparable, or in some instances superior, to tungsten carbide compositions having a cobalt binder. Moreover, it is superior in corrosion resistance to WC-Ni alloys and is vastly superior to WC-Ni alloys in hardness and strength. In addition, the present compositions can be made nonmagnetic, an important advantage over WC-Co alloys in certain applications.
- tungsten carbide-cobalt systems are their relatively poor corrosion resistance, particularly 'to acids which readily attack the cobalt binder.
- the corrosion resistance of WC-Co alloys can be somewhat improved by the addition of small amounts of chromium carbide, but only at the sacrifice of strength and metallurgical soundness.
- WCCo-Cr C alloys of suflicient corrosion resistance for most applications are not useful because of low strength. Chromium additions to WC Co behave similarly to chromium carbide additions and thus have limited usefulness.
- Alloys of the WC-Ni system have superior corrosion resistance properties in certain mild acid environments, and are therefore of some limited use. However, as indicated above they do not possess the strength and hardness properties of equivalent WC-Co alloys. Chromium carbide additions to WC-Ni further improve the corrosion resistance of WC-Ni alloys, but the accompanying de- Compositions of thepresent invention exhibit superior properties over rather narrow compositional limits of alloy-binder contents.
- the alloy binder content range should be from 10to 30%, by weight, of'the total weight of the alloy, and preferably from 1625%, the latter range being that of optimum properties. Compositions containing less than about 10% binder do not provide consistently dense pieces.
- the upper alloy binder limit of 30% isbased upon the sagging characteristics shared by all cemented carbide bodies of high binder content prepared by powder metallurgy.
- the upper useful binder content'limit of the alloys of the invention is thus approximately the same as that of conventional tungsten carbide-cobalt systems.
- Tables II and III compare the properties of the present alloy with those of WCCo over the binder content range of 825%, the range most frequently used in known commercially available WCCo alloys.
- the ratio of the weight of chromium to the combined weight of nickel and chromium was 0.058 in all samples.
- the corresponding ratio was 0.111 for all samples.
- Strength and hardness were measured as in Table I.
- Tungsten carbide (1 micron) 415 /20 Ni/Cr master alloy (-325 mesh) 25 Nickel, carbonyl (325 mesh) 60
- the charge was introduced into a tungsten carbide lined ball mill containing tungsten carbide-cobalt balls and milled in an acetone vehicle for 24 hours.
- the powder was then dried in a reducing atmosphere and paraffin was added as a pressing lubricant.
- the powder was pressed into a compact under 20 t.s.i. (tons per square inch) pressure in a carbide lined die and presintered in a hydrogen atmosphere for 3 hours at a peak temperature of 600 C.
- the presintered compact was then loaded into a vacuum furnace and sintered at 1450 C. for two hours at one to ten microns pressure.
- the sintered carbide was then cooled in the furnace.
- Example 2 The procedure of Example 1 was followed except that an alloy containing 16% Ni, 2% chromium and 82% WC was prepared from the following 500 gram charge:
- the chromium will enter the refractorycarbide phase in sufficient quantities to form, with the other components of the system, a complex carbide with resulting losses in properties of the final product.
- chromium is concentrated in the binder phase as a NiCr alloy, and the chromiums carbide forming tendencies must be suppressed.
- the chromium is introduced in chemically uncombined form as a high purity metal powder or as a nickel-chromium master alloy powder.
- the addition of chromium as an alloy is preferred but not essential.
- the tungsten carbide powders used should contain a high combined carbon content and a low free carbon content. Combined carbon contents of 6.10% with free carbon contents of .02% are preferred.
- Process conditions are chosen to isolate the powdered al loys from outside carbon sources to ensure the ultimate deposition of chromium principally as a nickel-chromium alloy.
- vacuum sintering does an excellent job of maintaining the neutral or slightly decarburizing atmosphere conditions needed and is preferred over other forms of sintering.
- other forms of sintering such as hydrogen atmosphere sintering, can be used. It is only essential that a non-carburizing atmosphere be used during sintering. Sintering temperatures of 13501500 C. are employed.
- a corrosion resistant, cemented carbide alloy consisting essentially of tungsten carbide and about to 30%, by weight, of a binder of an alloy of chromium and nickel, the ratio of the weight of chromium to the combined weight of nickel and chromium ranging from about 0.015 to about 0.15.
- the alloy of claim 1 containing 16 to 25%, by weight, of a binder.
- a process for the preparation of a corrosion resistant, cemented carbide alloy comprising pressing a powder mixture of tungsten carbide, chromium and nickel, said mixture containing about 10 to 30%, by weight, of chromium and nickel and a weight ratio of chromium to combined nickel and chromium of from about 0.015 to about 0.15, said 10 carried out at subatmospheric pressures.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
United States Patent 3,215,510 ALLOY Frederick J. Kelly, Grosse Pointe Woods, and Keith H. McKee, St. Clair Shores, Miclr, assignors to General Electric Company, a corporation of New York No Drawing. Filed Oct. 2, 19163, Ser. No. 313,185 '6 Claims. '(Cl. 29-1818) This invention relates to cemented carbide compositions combining corrosion resistance with high hardness and strength and to a process for preparing such compositions.
Cemented carbides are well known for their unique combination of hardness, strength and abrasion resistance and are accordingly extensively used in industry as cutting tools, drawing 'dies and wear parts. They are produced by powder metallurgy techniques from one or more refractory carbides of groups 1V, V and VI of the periodic table, bonded or cemented together, by liquid phase sintering, with one or more of the iron group metals.
The binder metal or alloy must possess a number of important properties and must meet a number of demanding requirements, among which are the following. The binder must have, or possess the ability to produce with the carbide through eutectic formation, a reasonable melting point. It must adequately Wet the carbide to produce 'a dense body. The binder should not to any material extent enter into an irreversible reaction with the carbide. Finally, the binder should impart reasonable strength to the cemented carbide alloy.
Of the possible carbide-binder combinations, the best known and most extensively .used is the tungsten carbidecobalt system. A second useful system is titanium carbide in which nickel is the binder. Nickel can also be used in place of cobalt with tungsten carbide but with a 2 generation of strength normally observed makes such WCNiCr C alloys of little value.
It is accordingly a principal object of the present invention to provide cemented carbide compositions combining corrosion resistance with high hardness and strength.
It is an additional object of this invention to provide a process for preparing cemented carbide compositions having the foregoing corrosion-resistance, hardness and strength properties. .Other objects will become apparent from the description of the invention which follows:
We have now found that the foregoing objects may be achieved in compositions which consist essentially of tungsten carbide and about 10 to about 25%, and not more than 30%, by weight, of a binder of chromium and nickel, the ratio of the weight of chromium to the combined weight of nickel and chromium ranging from about 0.015 to about 0.15. The compositions of the invention are prepared by pressing a powdered mixture of tungsten carbide, chromium and nickel within the foregoing ranges, the chromium being present in chemically uncombined form, and then sintering the pressed mixture in a carbon-free atmosphere.
The compositions of the invention possess outstanding corrosion resistance, particularly to acids and alkalis, combined with hardness and strength comparable, or in some instances superior, to tungsten carbide compositions having a cobalt binder. Moreover, it is superior in corrosion resistance to WC-Ni alloys and is vastly superior to WC-Ni alloys in hardness and strength. In addition, the present compositions can be made nonmagnetic, an important advantage over WC-Co alloys in certain applications.
A comparison of the properties of WC-Co and WC-Ni alloys with those of the present WC-Ni-Cr alloys is shown in the following Table I.
1 Rockwell A. 2 P.s.i., centers.
' At pH=1, 40-60" C. for 100 hrs.
4 Agitated abrasive. 100 hrs.
decided sacrifice in hardness and strength.
One of the principal disadvantages of tungsten carbide-cobalt systems is their relatively poor corrosion resistance, particularly 'to acids which readily attack the cobalt binder. The corrosion resistance of WC-Co alloys can be somewhat improved by the addition of small amounts of chromium carbide, but only at the sacrifice of strength and metallurgical soundness. As a result, WCCo-Cr C alloys of suflicient corrosion resistance for most applications are not useful because of low strength. Chromium additions to WC Co behave similarly to chromium carbide additions and thus have limited usefulness.
Alloys of the WC-Ni system have superior corrosion resistance properties in certain mild acid environments, and are therefore of some limited use. However, as indicated above they do not possess the strength and hardness properties of equivalent WC-Co alloys. Chromium carbide additions to WC-Ni further improve the corrosion resistance of WC-Ni alloys, but the accompanying de- Compositions of thepresent invention exhibit superior properties over rather narrow compositional limits of alloy-binder contents. The alloy binder content range should be from 10to 30%, by weight, of'the total weight of the alloy, and preferably from 1625%, the latter range being that of optimum properties. Compositions containing less than about 10% binder do not provide consistently dense pieces. It is believed that this is due to the poorer wettability of the nickel-chromium alloy binders for tungsten carbide as compared to pure nickel or cobalt binders. This results in the presence of insufiicient active liquid phase in the tungsten carbide-nickelchromium alloy below the 10% binder content.
The upper alloy binder limit of 30% isbased upon the sagging characteristics shared by all cemented carbide bodies of high binder content prepared by powder metallurgy. The upper useful binder content'limit of the alloys of the invention is thus approximately the same as that of conventional tungsten carbide-cobalt systems.
Tables II and III compare the properties of the present alloy with those of WCCo over the binder content range of 825%, the range most frequently used in known commercially available WCCo alloys. In Table II, the ratio of the weight of chromium to the combined weight of nickel and chromium was 0.058 in all samples. In Table III, the corresponding ratio was 0.111 for all samples. Strength and hardness were measured as in Table I.
TABLE II Transverse Percent Binder Type Alloy Rupture Hardness,
Strength R A WCNi-Cr Not measure ZOO-300,000 91 310,000 89.5 300-400,000.-. 90 70 000 89 88 87. 5 87 86 86 84 84 For footnotes see Table III.
TABLE III Transverse Percent Binder Type Alloy Rupture Hardness,
Strength R A Not measweight ratio, have been found to exhibit generally low strength. Examples of the properties of WCNi-Cr alloys showing a fixed nickel content and a variable chromium content within the specified limits are given in the following Table IV.
TABLE IV Hard- Transverse WC Ni Cr CrlNi+Cr ness, Density Rupture RA Strength The process of the invention is carried out by first mixing tungsten carbide, nickel and chromium powder Example 1 A cemented carbide alloy containing 16% Ni, 1% Cr and 83% WC was prepared from the following 500 gram charge:
Gm. Tungsten carbide (1 micron) 415 /20 Ni/Cr master alloy (-325 mesh) 25 Nickel, carbonyl (325 mesh) 60 The charge was introduced into a tungsten carbide lined ball mill containing tungsten carbide-cobalt balls and milled in an acetone vehicle for 24 hours. The powder was then dried in a reducing atmosphere and paraffin was added as a pressing lubricant. The powder was pressed into a compact under 20 t.s.i. (tons per square inch) pressure in a carbide lined die and presintered in a hydrogen atmosphere for 3 hours at a peak temperature of 600 C. The presintered compact was then loaded into a vacuum furnace and sintered at 1450 C. for two hours at one to ten microns pressure. The sintered carbide was then cooled in the furnace.
Example 2 The procedure of Example 1 was followed except that an alloy containing 16% Ni, 2% chromium and 82% WC was prepared from the following 500 gram charge:
Gm. Tungsten carbide (1 micron) 410 Chromium, electrolytic (325 mesh) -I 10 Nickel, carbonyl (325 mesh) 80 The technical explanation for the unique combination of properties obtained with WCNi-Cr alloys, within the specified compositional range, appears to be complex. A plausible explanation, supported by the process conditions found necessary to achieve the superior properties is as follows: It is believed that chromium additions to WCNi alloys will tend to partition between the metal binder and the refractory carbide phase during sintering. Moreover, chromium is well known to be a strong carbide former as compared to WC and will scavenge carbon to form simple and/or complex carbides. Above the approximate upper Cr/Ni-]Cr ratio limit of 0.15, the chromium will enter the refractorycarbide phase in sufficient quantities to form, with the other components of the system, a complex carbide with resulting losses in properties of the final product.
In preparing the composition, steps must accordingly be taken to insure that the chromium is concentrated in the binder phase as a NiCr alloy, and the chromiums carbide forming tendencies must be suppressed. To ac complish this the chromium is introduced in chemically uncombined form as a high purity metal powder or as a nickel-chromium master alloy powder. The addition of chromium as an alloy is preferred but not essential. The tungsten carbide powders used should contain a high combined carbon content and a low free carbon content. Combined carbon contents of 6.10% with free carbon contents of .02% are preferred. Process conditions are chosen to isolate the powdered al loys from outside carbon sources to ensure the ultimate deposition of chromium principally as a nickel-chromium alloy. We have found that vacuum sintering does an excellent job of maintaining the neutral or slightly decarburizing atmosphere conditions needed and is preferred over other forms of sintering. However, other forms of sintering, such as hydrogen atmosphere sintering, can be used. It is only essential that a non-carburizing atmosphere be used during sintering. Sintering temperatures of 13501500 C. are employed.
What we claim as new and desire to secure by Letters Patent of the United States is:
1. A corrosion resistant, cemented carbide alloy consisting essentially of tungsten carbide and about to 30%, by weight, of a binder of an alloy of chromium and nickel, the ratio of the weight of chromium to the combined weight of nickel and chromium ranging from about 0.015 to about 0.15.
2. The alloy of claim 1 containing 16 to 25%, by weight, of a binder.
3. The alloy of claim 2 in which the chromium content is 1 to 2% and the nickel content is to 17%, both 20 by weight, based on the total weight of the alloy.
4. A process for the preparation of a corrosion resistant, cemented carbide alloy comprising pressing a powder mixture of tungsten carbide, chromium and nickel, said mixture containing about 10 to 30%, by weight, of chromium and nickel and a weight ratio of chromium to combined nickel and chromium of from about 0.015 to about 0.15, said 10 carried out at subatmospheric pressures.
References Cited by the Examiner UNITED STATES PATENTS 15 2,147,329 2/39 Willey 29182.8 2,313,227 3/43 De Bats 29-1828 3,109,917 11/63 Schmidt et al. 29-182] Schwarzkopf, Paul and Kiefler, Richard: Cemented Carbides, New York, The Macmillan Co., 1960, pages CARL D. QUARFORTH, Primary Examiner. REUBEN EPSTEIN, Examiner.
Claims (1)
1. A CORROSION RESISTANT, CEMENTED CARBIDE ALLOY CONSISTING ESSENTIALLY OF TUNGSTEN CARBIDE AND ABOUT 10 TO 30%, BY WEIGHT OF A BINDER OF AN ALLOY OF CHROMIUM AND NICKEL, THE RATIO OF THE WEIGHT OF CHROMIUM TO THE COMBINED WEIGHT OF NICKEL AND CHROMIUM RANGING FROM ABOUT 0.015 TO ABOUT 0.15.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US313185A US3215510A (en) | 1963-10-02 | 1963-10-02 | Alloy |
| GB36532/64A GB1013328A (en) | 1963-10-02 | 1964-09-07 | Improvements in cemented carbide alloys |
| FR988088A FR1407611A (en) | 1963-10-02 | 1964-09-14 | Sintered carbides and method of manufacturing said carbides |
| BE653503D BE653503A (en) | 1963-10-02 | 1964-09-24 | |
| NL646411185A NL151442B (en) | 1963-10-02 | 1964-09-25 | PROCESS FOR THE PREPARATION OF A TUNGSTEN CARBIDE, CONTAINING CHROME AND NICKEL HARD METAL, AND OBJECTS CONSISTING WHOLLY OR LARGE PART OF A HARD METAL PREPARED THEREFORE. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US313185A US3215510A (en) | 1963-10-02 | 1963-10-02 | Alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3215510A true US3215510A (en) | 1965-11-02 |
Family
ID=23214714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US313185A Expired - Lifetime US3215510A (en) | 1963-10-02 | 1963-10-02 | Alloy |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3215510A (en) |
| BE (1) | BE653503A (en) |
| GB (1) | GB1013328A (en) |
| NL (1) | NL151442B (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3878592A (en) * | 1971-12-22 | 1975-04-22 | Ford Motor Co | Molybdenum nickel chromium bonded titanium carbide |
| US3989554A (en) * | 1973-06-18 | 1976-11-02 | Hughes Tool Company | Composite hardfacing of air hardening steel and particles of tungsten carbide |
| WO1980002569A1 (en) * | 1979-05-17 | 1980-11-27 | Sandvik Ab | Cemented carbide |
| US4430389A (en) | 1982-03-01 | 1984-02-07 | Wexco Corporation | Composite cylinder and casting alloy for use therein |
| EP0195965A2 (en) | 1985-03-28 | 1986-10-01 | Fried. Krupp Gesellschaft mit beschränkter Haftung | Hard metal and process for its manufacture |
| AT385775B (en) * | 1985-08-08 | 1988-05-10 | Plansee Metallwerk | CORROSION-RESISTANT CARBIDE ALLOY |
| US4961780A (en) * | 1988-06-29 | 1990-10-09 | Vermont American Corporation | Boron-treated hard metal |
| US5116416A (en) * | 1988-03-11 | 1992-05-26 | Vermont American Corporation | Boron-treated hard metal |
| WO1992018656A1 (en) * | 1991-04-10 | 1992-10-29 | Sandvik Ab | Method of making cemented carbide articles |
| US5223020A (en) * | 1988-10-31 | 1993-06-29 | Krupp Widia Gmbh | Hard-metal body |
| US5470807A (en) * | 1995-03-17 | 1995-11-28 | Industrial Technology Research Institute | Chromium carbide based ceramics composite block gauge |
| US5651808A (en) * | 1989-11-09 | 1997-07-29 | Rutgers, The State University Of New Jersey | Carbothermic reaction process for making nanophase WC-Co powders |
| US5736658A (en) * | 1994-09-30 | 1998-04-07 | Valenite Inc. | Low density, nonmagnetic and corrosion resistant cemented carbides |
| US5841045A (en) * | 1995-08-23 | 1998-11-24 | Nanodyne Incorporated | Cemented carbide articles and master alloy composition |
| US6368377B1 (en) * | 1999-02-23 | 2002-04-09 | Kennametal Pc Inc. | Tungsten carbide nickel-chromium alloy hard member and tools using the same |
| WO2002063054A3 (en) * | 2001-02-02 | 2002-10-24 | Boart Longyear Gmbh & Co Kg | Soil processing tool comprising a working element made of hard metal |
| US20080202191A1 (en) * | 2006-12-27 | 2008-08-28 | Sandvik Intellectual Property Ab | Corrosion resistant tool |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB395721A (en) * | 1931-11-16 | 1933-07-17 | Molybdenum Co Nv | An improved material for tool or tool parts |
| US2147329A (en) * | 1937-07-21 | 1939-02-14 | Fay H Willey | Wear-resistant metal alloy |
| US2313227A (en) * | 1938-08-04 | 1943-03-09 | Metal Carbides Corp | Roll for metal-rolling mills |
| US3109917A (en) * | 1959-04-18 | 1963-11-05 | Boehler & Co Ag Geb | Hard facing |
-
1963
- 1963-10-02 US US313185A patent/US3215510A/en not_active Expired - Lifetime
-
1964
- 1964-09-07 GB GB36532/64A patent/GB1013328A/en not_active Expired
- 1964-09-24 BE BE653503D patent/BE653503A/xx unknown
- 1964-09-25 NL NL646411185A patent/NL151442B/en not_active IP Right Cessation
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB395721A (en) * | 1931-11-16 | 1933-07-17 | Molybdenum Co Nv | An improved material for tool or tool parts |
| US2147329A (en) * | 1937-07-21 | 1939-02-14 | Fay H Willey | Wear-resistant metal alloy |
| US2313227A (en) * | 1938-08-04 | 1943-03-09 | Metal Carbides Corp | Roll for metal-rolling mills |
| US3109917A (en) * | 1959-04-18 | 1963-11-05 | Boehler & Co Ag Geb | Hard facing |
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3878592A (en) * | 1971-12-22 | 1975-04-22 | Ford Motor Co | Molybdenum nickel chromium bonded titanium carbide |
| US3989554A (en) * | 1973-06-18 | 1976-11-02 | Hughes Tool Company | Composite hardfacing of air hardening steel and particles of tungsten carbide |
| WO1980002569A1 (en) * | 1979-05-17 | 1980-11-27 | Sandvik Ab | Cemented carbide |
| US4497660A (en) * | 1979-05-17 | 1985-02-05 | Santrade Limited | Cemented carbide |
| US4430389A (en) | 1982-03-01 | 1984-02-07 | Wexco Corporation | Composite cylinder and casting alloy for use therein |
| DE3511220A1 (en) * | 1985-03-28 | 1986-10-09 | Fried. Krupp Gmbh, 4300 Essen | HARD METAL AND METHOD FOR THE PRODUCTION THEREOF |
| US4684405A (en) * | 1985-03-28 | 1987-08-04 | Fried. Krupp Gmbh | Sintered tungsten carbide material and manufacturing method |
| EP0195965A3 (en) * | 1985-03-28 | 1988-09-21 | Fried. Krupp Gesellschaft Mit Beschrankter Haftung | Hard metal and process for its manufacture |
| EP0195965A2 (en) | 1985-03-28 | 1986-10-01 | Fried. Krupp Gesellschaft mit beschränkter Haftung | Hard metal and process for its manufacture |
| AT385775B (en) * | 1985-08-08 | 1988-05-10 | Plansee Metallwerk | CORROSION-RESISTANT CARBIDE ALLOY |
| US5116416A (en) * | 1988-03-11 | 1992-05-26 | Vermont American Corporation | Boron-treated hard metal |
| US4961780A (en) * | 1988-06-29 | 1990-10-09 | Vermont American Corporation | Boron-treated hard metal |
| US5223020A (en) * | 1988-10-31 | 1993-06-29 | Krupp Widia Gmbh | Hard-metal body |
| US5651808A (en) * | 1989-11-09 | 1997-07-29 | Rutgers, The State University Of New Jersey | Carbothermic reaction process for making nanophase WC-Co powders |
| WO1992018656A1 (en) * | 1991-04-10 | 1992-10-29 | Sandvik Ab | Method of making cemented carbide articles |
| US5619000A (en) * | 1991-04-10 | 1997-04-08 | Sandvik Ab | Method of making cemented carbide articles and the resulting articles |
| US5441693A (en) * | 1991-04-10 | 1995-08-15 | Sandvik Ab | Method of making cemented carbide articles and the resulting articles |
| US5736658A (en) * | 1994-09-30 | 1998-04-07 | Valenite Inc. | Low density, nonmagnetic and corrosion resistant cemented carbides |
| US5470807A (en) * | 1995-03-17 | 1995-11-28 | Industrial Technology Research Institute | Chromium carbide based ceramics composite block gauge |
| US5841045A (en) * | 1995-08-23 | 1998-11-24 | Nanodyne Incorporated | Cemented carbide articles and master alloy composition |
| US6368377B1 (en) * | 1999-02-23 | 2002-04-09 | Kennametal Pc Inc. | Tungsten carbide nickel-chromium alloy hard member and tools using the same |
| WO2002063054A3 (en) * | 2001-02-02 | 2002-10-24 | Boart Longyear Gmbh & Co Kg | Soil processing tool comprising a working element made of hard metal |
| US20080202191A1 (en) * | 2006-12-27 | 2008-08-28 | Sandvik Intellectual Property Ab | Corrosion resistant tool |
| US8057571B2 (en) * | 2006-12-27 | 2011-11-15 | Sandvik Intellectual Property Ab | Corrosion resistant tool |
Also Published As
| Publication number | Publication date |
|---|---|
| BE653503A (en) | 1965-01-18 |
| NL151442B (en) | 1976-11-15 |
| GB1013328A (en) | 1965-12-15 |
| NL6411185A (en) | 1965-04-05 |
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