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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US313185A
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Frederick J Kelly
Keith H Mckee
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General Electric Co
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General Electric Co
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Priority to US313185A priority Critical patent/US3215510A/en
Priority to GB36532/64A priority patent/GB1013328A/en
Priority to FR988088A priority patent/FR1407611A/en
Priority to BE653503D priority patent/BE653503A/xx
Priority to NL646411185A priority patent/NL151442B/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06Alloys 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
    • C22C29/08Alloys 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06Alloys 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
    • C22C29/067Alloys 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.
US313185A 1963-10-02 1963-10-02 Alloy Expired - Lifetime US3215510A (en)

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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.

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Cited By (17)

* Cited by examiner, † Cited by third party
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
WO2002063054A2 (en) * 2001-02-02 2002-08-15 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)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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 (25)

* Cited by examiner, † Cited by third party
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
WO2002063054A2 (en) * 2001-02-02 2002-08-15 Boart Longyear Gmbh & Co. Kg Soil processing tool comprising a working element made of hard metal
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

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BE653503A (en) 1965-01-18
GB1013328A (en) 1965-12-15
NL6411185A (en) 1965-04-05

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