US3369891A - Heat-treatable nickel-containing refractory carbide tool steel - Google Patents

Heat-treatable nickel-containing refractory carbide tool steel Download PDF

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US3369891A
US3369891A US481386A US48138665A US3369891A US 3369891 A US3369891 A US 3369891A US 481386 A US481386 A US 481386A US 48138665 A US48138665 A US 48138665A US 3369891 A US3369891 A US 3369891A
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matrix
titanium
steel
carbide
nickel
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Stuart E Tarkan
John L Ellis
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Alloy Technology International Inc
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Chromalloy American Corp
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Priority to US481386A priority Critical patent/US3369891A/en
Priority to US481416A priority patent/US3369892A/en
Priority to GB31392/66A priority patent/GB1094829A/en
Priority to DEC39812A priority patent/DE1298293B/de
Priority to CH1136966A priority patent/CH465242A/fr
Priority to FR72922A priority patent/FR1489454A/fr
Priority to SE6611130A priority patent/SE370959B/xx
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Assigned to ALLOY TECHNOLOGY INTERNATIONAL, INC. reassignment ALLOY TECHNOLOGY INTERNATIONAL, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: CHROMALLOY AMERICAN CORPORATION
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/10Ferrous alloys, e.g. steel alloys containing cobalt
    • C22C38/105Ferrous alloys, e.g. steel alloys containing cobalt containing Co and Ni
    • 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

  • a refractory carbide tool steel comprising about 20 to 80% by volume of titanium carbide distributed through a low carbon allow steel matrix making up substantially the balance, the matrix being characterized in the solution annealed state by a microstructure of soft martensite containing at least one age hardening element.
  • the matrix may contain by weight about 10 to 30% nickel, about 0.2 to 9% titanium, up to about 5% aluminum, the sum of the titanium and aluminum not exceeding about 9%, up to about 25% cobalt, up to about 10% molybdenum, substantially the balance of the matrix being at least 50% iron.
  • This invention relates to a nickel-containing refractory carbide tool steel and, in particular, to a nickel-containing titanium carbide tool steel bar stock capable of being precision machined into desired shapes in the martensitic condition and of being thereafter heat treated to high hardeness while maintaining close dimensional tolerances.
  • the composition is formed by employing titanium and carbon together in a combinedform as titanium carbide as an alloying ingredient together with a steel matrix utilizing powder metallurgy methods of fabrication.
  • the steel employed in forming the matrix contains iron as the major alloying element which generally comprises at least about 60% by Weight of the steel matrix composition.
  • the amount of titanium may range from about 10% to 70% by weight (about 20 to 90% by volume of titanium carbide or 12.5% to 87% by weight) and preferably about 20% to 58% by weight of titanium (about 40% to 80% by volume of titanium carbide or 25% to 75% by weight), substantially the balance being formed of a carbon-containing steel matrix.
  • Another tool steel of the foregoing type is one containing at least one refractory carbide selected from the group consisting of VC, CbC and TaC, with the balance formed substantially of carbon-containing steel matrix, for example a steel matrix constituting about 25% to 75%, or preferably 30% to 60% by weight of the total composition.
  • a sintered product is first fabricated which is annealed by furnace cooling from about 1300 C. to room temperature, the microstructure of the matrix metal generally comprising pearlite.
  • the annealed product is then machined into the desired shape by turning and/or grinding, and then subjected to a hardening heat treatment by austenitizing the annealed tool steel at a temperature of about 950 C. for about one-quarter of an hour followed by quenching in oil or water. Hardnesses of up to about 70 Rockwell C are obtained for such titanium carbide tool steels. This class of materials has found commercial acceptance as specialty steels.
  • a still further problem is the additional finish grinding which is sometimes required when the matrix of a heat treated titanium carbide steel has decarburized during heat treatment. While the decarburized matrix is generally softer, the presence of primary grains of refactory carbide makes grinding difficult. Moreover, the hardness of the decarburized matrix is adversely affected. To avoid this, strict precautions must be taken via atmosphere control to prevent decarburization.
  • Another object is to provide a new and improved refractory carbide tool steel capable of being hardened without quenching in oil, water or other liquid media.
  • a further object is to provide as an article of manufacture a tool steel bar stock containing substantially large amounts of titanium carbide distributed as primary carbide grains through a nickel-containing steel matrix having an age hardenable martensitic microstructure.
  • titanium carbide as a primary carbide.
  • primary carbide the titanium carbide which is added to the composition as such and which is substantially insoluble in the matrix, whereby it is still recognizable under the microscope after the composition is subjected to fabrication and to normal steel heat treating practice.
  • the nickel-containing carbidic tool steel comprises by volume about 20% to of primary carbide grains based on a carbide comprising essentially TiC distributed through a nickel-containing steel matrix making up substantially the balance, the matrix containing by weight of steel matrix about 10% to 30% nickel, about 0.2% to 9% titanium and up to about aluminum, the sum of the titanium and aluminum content not exceeding about 9%, up to about 25% cobalt, up to about molybdenum, with substantially the balance of the matrix by weight being at least 50% iron.
  • the elements making up the matrix composition are proportioned such that when the nickel content ranges fr'om about 10% to 22% and the sum of titanium and aluminum is less than about 1.5% or less than about 1.3%, the cobalt and molybdenum contents are each at least about 2% by weight; and such that when the nickel content ranges from about 18% to 30% and the molybdenum content is less than about 2%, the sum of titanium and aluminum in the matrix exceeds about 1.5%
  • a composition range which is particularly advantageous for our purpose is one comprising about 20% to 80% or 30% to 70% by volume of primary carbide grains based on a carbide comprising essentially TiC distributed through a matrix making up the balance containing by weight of the matrix about 18% to 30% nickel, about 1.5% to 9% of titanium, up to about 5% aluminum, the sum of titanium and aluminum not exceeding about 9%, substantially the balance of the matrix alloy being at least about 50% iron by weight.
  • Other metals which may advantageously be present include up to about 20% cobalt, up to about 2% molybdenum and chromium total with substantially the balance of the matrix being at least 50% iron.
  • a composition which is advantageous for our purpose comprises 24% to 30% nickel, 1.5% to 9% titanium and/ or aluminum, the total titanium and aluminum not exceeding 9%, and low carbon in the matrix, for example below 0.15 carbon and more advantageously below 0.1 carbon.
  • the titanium and/or aluminum content may range from about 5% to 9% by weight total.
  • composition range which is advantageous for our purpose is one comprising about 20% to 80% or 30% to 70% by volume of said primary carbide grains distributed through a nickel alloy steel matrix constituting the balance, the matrix containing by weight about 18% to 24% nickel, about 1.5% to 3% of a metal from the group titanium and aluminum, low carbon, e.g., not exceeding 0.1% C, and the balance of the matrix su bstantially iron.
  • a still further composition range which is advantageous for our purpose is one comprising about 20% to 80% or 30% to 70% by volume of said primary carbide grains distributed through a low carbon nickel alloy steel matrix containing by weight of the matrix about 10% to 22% nickel, about 0.2% to 1.5% of titanium, up to about 1.5% aluminum, with the sum of titanium and aluminum content less than 1.5%, about 2% to 10% cobalt, about 2% to 8% molybdenum and the balance of the matrix substantially iron of at least about 50% by weight, the carbon content being maintained below 0.15% and more advantageously not exceeding 0.1%.
  • a matrix composition which is particularly advantageous when employed with the primary carbide over the foregoing ranges is one comprising about 16% to 22% nickel, about 6% to 10% cobalt and about 2% to 6% of molybdenum, about 0.2% to 1% titanium, up to about 0.4% aluminum and the balance of the matrix substantially iron of at least about 50% by weight.
  • the foregoing compositions may contain up to 10% in the aggregate of up to about 5% Cr, up to about 7% W, up to about 3% Ch and/or Ta, up to about 6% Cu, up to about 0.5% Mn, up to about 1% Be, etc.
  • the resulting carbidic composition can be solution treated at an elevated temperature and air cooled to form a soft martensitic matrix having attributes that enable the resulting product to be easily machined and/ or ground to substantially precise dimensions prior to hardening.
  • the hardening treatment employed after the solution treatment is unlike the high temperature a-ustenitizing quenching treatment in that relatively low temperatures are employed while the matrix is in the martensitic condition, followed by air cooling.
  • the heat treatment is in nature of an age-hardening treatment due to the presence of age hardening elements, which heat treatment is carried out at a temperature in the range of about 265 C. to 655 C. (about 500 F. to 1200 B).
  • the matrix had the following composition by weight:
  • the balance iron includes smal amounts of other ingredients which do not adversely affect the novel characteristics of the alloy.
  • TiC powder of average particle size about 5 to 7 microns is mixed with 1,000 grams of powdered steelforming ingredients corresponding to the aforementioned matrix metal composition.
  • the TiC powder employed has a total carbon content of about 19.45% by weight which corresponds to a total of about 6.48% carbon by weight in 1,500 grams of powder mixture. It is desirable for optimum results that the carbon content of the matrix metal be maintained below 0.15% by weight of matrix.
  • a strong carbide former other than Mo and Cr, and which is substantially insoluble in the matrix as the carbide such as excess metallic titanium is added to the mixture to combine with the excess free carbon to form a secondary carbide of titanium by reaction. This is achieved by adding the titanium in the form of TiH which yields active titanium for combining with free carbon.
  • Another strong carbide former which may be added is zirconium in the form of zirconium hydride. The amount of titanium added is calculated to be at least 4 times the amount of free carbon to be combined as TiC plus excess titanium to provide about 0.2% to 0.4% free titanium to enter the matrix metal. Examples of other strong carbide formers which form substantially insoluble carbides are V, Cb, Ta, etc.
  • the dry powder is then pressed into compacts or slugs at tons per square inch.
  • the compacts thus produced are subjected to liquid phase sintering by heating them to about 1425 C. in vacuum in 2 /2 hours and holding at temperature for three-quarters of an hour, followed by cooling to 1300 C. in 30 minutes and then furnace cooling from 1300 C. to room temperature.
  • the sintering is advantageously carried out on a ceramic plate of previously fired Magnorite (a commercial MgO refractory).
  • the hardness after sintering is 50 R and the compact has a density of over 99% of true density.
  • the sintered alloy is solution annealed by heating to a temperature at which austenite prevails, for example, from about 760 C. (1400 F.) to 1165 C. (2150 F.) followed by air cooling. After heating the alloy at 815 C. (15 00 F.) for thirty minutes and air cooling to ambient temperature, it had a Rockwell C hardness of about 48, the microstructure of the matrix being soft martensite. In this condition, the alloy machines and/ or grinds easily to a precisely dimensioned shape. By cooling the alloy to ambient temperature in air from the solution temperature, transformation to soft martensite is effected. Thus, any growth that has occurred due to transformation to martensite presents no problems since the carbidic alloy can be easily machined and then hardened without any further growth taking place.
  • the alloy is hardened by aging it at a temperature in the range of about 260 C. (500 F.) to 650 C. (1200 F.) for about three hours followed by air cooling.
  • the alloy solution treated at 815 C. exhibited a hardness after aging at 483 C. (900 F.) for three hours and cooling in air of about 60 R
  • the same alloy solution treated at 1150 C. (2100 F.) and aged at 483 C. (900 F.) exhibited a higher hardness of about 63 R
  • the advantage of the hardening heat treatment at the lower temperature is that substantially close dimensional tolerance can be maintained with intricate shapes and cracking greatly inhibited.
  • the amount of carbon in the nickelcontaining steel matrix be maintained as low as possible, for example, below 0.15% by weight of the matrix.
  • Til-I was omitted from the mixture as a result of which the assintered hardness was 57.8 R and the solution hardness after cooling from 1500 C. was 61.5 R Because the free carbon was not combined with titanium, the solution hardness rose substantially above 50 R and was as high as 61.5 R
  • EXAMPLE 2 Primary carbide, about 30 vol. percent of TiC, Matrix steel, about 70 vol. percent nickel-containing steel.
  • the nominal composition of the matrix by weight is as follows:
  • the amount of TiC present includes with it the excess titanium added to combine with the free carbon and prevent it from entering the matrix metal.
  • EXAMPLE 3 Primary carbide, about 65 vol. percent TiC, Matrix steel, about 35 vol. percent nickel-containing steel.
  • the matrix has the following nominal composition by weight:
  • sufiicient TiH was added to the mixture to combine with the free carbon during sintering to convert it to a secondary carbide of titanium.
  • EXAMPLE 4 Primary carbide, about 25 vol. percent TiC, Matrix steel, about 75 vol. percent nickel-containing steel.
  • the nominal composition of the matrix steel by weight Sufiicient excess of TiH is added to the mix to insure combining with free carbon prior to sintering and convert it to a secondary carbide of titanium.
  • EXAMPLE 5 Primary carbide, about 40 vol. percent TiC, Matrix steel, about 60 vol. percent of nickel-containing steel.
  • the nominal composition of the matrix by weight is as follows:
  • the amount of free carbon resulting from the use of TrC is compensated for by adding sufficient TiH to the mixture prior to sintering.
  • EXAMPLE 6 Primary carbide, about 75 vol. percent TiC, Matrix steel, about 25 vol. percent nickel-containing steel.
  • Free carbon in the system was compensated for by the addition of TiH to the powder mixture prior to sintering.
  • EXAMPLE 7 Primary carbide, about 50 vol. percent TiC, Matrix steel, about 50 vol. percent nickel-containing steel.
  • Free carbon in the system is combined with titanium by adding Til-I to the powder mixture prior to sintering.
  • the iron given as the balance in the foregoing examples does not include the presence of amounts of other ingradients which do not adversely affect the novel characteristics of the carbide steel and small amounts of such other ingredients such as calcium, boron, zirconium, manganese, silicon and the like.
  • the powder metallurgy method of mixing the powdered ingredients and then compacting the mixture into a desired shape followed by liquid phase or solid state sintering at an elevated temperature to achieve full densification comprises mixing the appropriate amount of steelforming ingredients with the appropriate amount of the primary carbide, using a small amount of wax to give sufiicient green strength to the resulting pressed compact, for example one gram of wax for each 100 grams of mixture.
  • the mixture may be shaped a variety of ways. We find it advantageous to press the mixture to a density at least 50% of true density by pressing over the range of about t.s.i. to 75 t.s.i., preferably t.s.i.
  • the product is allowed to furnace cool to ambient temperature. If necessary, the as-sintered product is subjected to any mechanical cleaning and then solution treated over the range of about 760 C. (14-00" F.) to 1165 C. (2150 F.) followed by air cooling. Vl/C have found the range of 760 C. (1400 F.) to 982 C. (1800 F.) to be particularly advantageous.
  • the solution treatment may be carried out at a temperature for one-quarter hour or longer, for example, one hour.
  • ingredients which may be present in the matrix metal besides the main constituents include up to about 1% Mn, up to about 0.5% Si, up to about 0.1% Ca, up to about 0.1% B, up to about 0.1% Zr, etc.
  • Other alloying ingredients which may be present in the matrix steel in amounts which do not adversely affect the novel characteristics of the carbidic tool steel are Cr, Cu, W, V and Cb, among others.
  • carbides may be present in amounts which do not adversely affect the tool steel, such as up to about 25% zirconium carbide and the like, provided they are substantially insoluble in the matrix.
  • the invention provides a carbidic tool steel comprising about 20% to 80% or 30% to 70% by volume of primary carbide grains comprising essentially titanium carbide distributed through a relatively low carbon alloy steel matrix making up substantially the balance, the matrix being characterized on slow cooling from its austenitizing temperature by a microstructure comprising substantially martensite in the relatively soft condition containing at least one age hardening element.
  • the foregoing composition despite the presence of substantial amounts of primary carbide, is advantageous in that after it is sintered, it can be solution treated by air cooling from a high temperature (i.e., the austenitizing temperature) to form a matrix of relatively soft martensite.
  • an article of this composition may then be precision machined to any shape, however intricate, and then hardened at a relatively low temperature without any substantial amount of warping, cracking, or volumetric change occurring.
  • a carbidic tool steel having a quench-hardenable steel matrix generally requires re-finishing after hardening due to volumetric growth, warping, etc.
  • Another advantage of the composition of the invention is that decarburization is not a problem since the matrix does not rely on the presence of carbon to achieve the requisite hardening. Thus, the usual precaution of strict atmosphere control during heat treatment is not necessary.
  • the invention provides a carbidic heat treatable ferrous alloy which in the form of bar stock, rounds, squares, blocks, ingots and other shapes can be utilized in the fabrication of cutting tools, blanking dies, forming dies, drawing dies, rolls, hot extrusion dies, forging dies, upsetting dies, broaching tools, and in general all types of wear and/ or heat resisting elements, tools or machine parts.
  • a hardenable refractory carbide tool steel comprising about 20% to by volume of primary carbide grains comprising essentially titanium carbide distributed through a low carbon alloy steel matrix making up substantially the balance, the matrix being characterized in the solution annealed state by a mocrostructure of soft martensite containing at least one age hardening element.
  • a heat treatable carbidic tool steel comprising about 20% to 80% by volume of primary carbide grains comprising essentially titanium carbide distributed through a matrix of a high nickel alloy steel constituting the balance; said matrix nickel alloy steel containing by weight of matrix about 10 to 30% nickel, about 0.2 to 9% of titanium and up to about 5% aluminum, the sum of titanium and aluminum not exceeding about 9%, up to about 25% cobalt, up to about 10% molybdenum, substantially the balance of the matrix being at least 50% iron; the metals making up the matrix composition being proportion such that when the nickel content ranges from about 10% to 22% and the sum of aluminum and titanium is less than about 1.5%, the cobalt and molybdenum contents are each at least about 2% by weight; and such that when the nickel content ranges from about 18% to 30% and the molybdenum content is less than 2%, the sum of aluminum and titanium exceeds 1.5%, said matrix being also characterized in the solution treated condition by microstructure of soft martensite.
  • a heat treatable carbidic tool steel comprising about 30% to 70% by volume of primary carbide grains comprising essentially titanium carbide distributed through a matrix of a high nickel alloy steel constituting the balance; said matrix nickel alloy steel containing by weight of matrix about 10 to 30% nickel, about 0.2 to 9% of titanium and up to about 5% aluminum, the sum of ti tanium and aluminum not exceeding about 9%, up to about 25% cobalt, up to about 10% molybdenum, substantially the balance of the matrix being at least 50% iron, an efiective amount of a strong carbide former at least sufiicient to combine with carbon in excess of the carbon combined as primary carbide selected from the group consisting of vanadium, columbium, tantalum, zirconium and titanium, the titanium of said group being that amount in addition to the titanium employed in producing the nickel alloy steel matrix; the metals making up the matrix composition being proportioned such that when the nickel content ranges from about 10% to 22% and the sum of aluminum and titanium is less than about 1.5%, the cobal
  • a heat treatable carbidic tool steel comprising about 30% to 70% by volume of primary carbide grains comprising essentially titanium carbide distributed through a matrix of a high nickel alloy steel constituting the balance; said matrix nickel alloy steel containing by weight of matrix about 16% to 22% nickel, about 0.2% to 1% titanium, up to about 0.4% aluminum, about 6% to 10% cobalt, about 2% to 6% molybdenum, the amount of titanium present being at least suflicient to combine with carbon in excess of the carbon combined as primary carbide and provide age hardening, substantially the balance of the matrix being at least 50% iron, said matrix being also characterized in the solution treated condition by a microstructure of soft martensite.
  • a heat treatable high carbon high titanium tool steel comprising about 20% to 80% by volume of primary carbide grains comprising essentially titanium carbide distributed through a matrix of a high nickel alloy steel constituting the balance; said matrix nickel alloy steel containing by weight of matrix about 18 to 30% nickel, about 1.5 to 9% of a metal selected from the group consisting of titanium and aluminum, up to about 20% cobalt, less than about 2% total of a metal selected from the group consisting of molybdenum and chromium, and an effective amount of a strong carbide former at least sufiicient to combine with carbon present in excess of the carbon combined as primary titanium carbide selected from the group consisting of vanadium, columbium, tantalum, zirconium and titanium, the titanium of said group being that amount in addition to the titanium employed in producing the nickel alloy steel matrix, substantially the balance of the matrix being at least 50% iron, said matrix being also characterized in the solution treated condition by a microstructure of soft martensite.
  • a heat treatable high carbon tool steel comprising about 20% to 80% by volume of primary carbide grains comprising essentially of titanium carbide distributed through a matrix of a high nickel alloy steel constituting the balance; said matrix nickel alloy steel containing by weight of matrix about 18 to 24% nickel, about 1.5% to 3% of a metal selected from the group consisting of titanium and aluminum, and an effective amount of a strong carbide former at least sufficient to combine with carbon in excess of the carbon combined as primary carbide selected from the group consisting of vanadium, columbium, tantalum, zirconium and titanium, the titanium of said group being that amount in addition to the titanium employed in producing the nickel alloy steel matrix, substantially the balance of the matrix being at least 50% iron.
  • a method of producing a machinable refractory carbide tool steel which comprises providing a compact produced by compressing a powder mixture containing about 20% to 80% by volume of primary carbide grains comprising essentially titanium carbide dispersed through a matrix powder of nickel-containing steel-forming ingredients constituting the balance, said matrix powder containing by weight of matrix about 10 to 30% nickel, about 0.2 to 9% of titanium and up to about 5% aluminum, the sum of the titanium and aluminum not exceeding 9%, up to about 25% cobalt, up to about 10% molybdenum, a strong carbide former in an amount at least sufficient to combine with any carbon in excess of the carbon combined as primary carbide selected from the group consisting of vanadium, columbium, tantalum, zirconium and titanium, the titanium of said group being that amount in addition to the titanium employed in producing the nickel alloy steel matrix, substantially the balance of the matrix being at last 50% iron; the metals making up the matrix composition being proportioned such that when the nickel content ranges from about 10% to 22% and the sum of aluminum and

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US481386A 1965-08-20 1965-08-20 Heat-treatable nickel-containing refractory carbide tool steel Expired - Lifetime US3369891A (en)

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Application Number Priority Date Filing Date Title
US481386A US3369891A (en) 1965-08-20 1965-08-20 Heat-treatable nickel-containing refractory carbide tool steel
US481416A US3369892A (en) 1965-08-20 1965-08-20 Heat-treatable nickel-containing refractory carbide tool steel
GB31392/66A GB1094829A (en) 1965-08-20 1966-07-13 Improvements in or relating to tool steel
DEC39812A DE1298293B (de) 1965-08-20 1966-08-04 Hochverschleissfeste, bearbeitbare und haertbare Sinterstahllegierung und Verfahren zu deren Herstellung
CH1136966A CH465242A (fr) 1965-08-20 1966-08-08 Acier à outil au carbure réfractaire et procédé de préparation d'un tel acier
FR72922A FR1489454A (fr) 1965-08-20 1966-08-12 Acier à outil à carbure réfractaire durcissable et procédé de préparation d'un tel acier
SE6611130A SE370959B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1965-08-20 1966-08-17

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US481416A US3369892A (en) 1965-08-20 1965-08-20 Heat-treatable nickel-containing refractory carbide tool steel

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3450511A (en) * 1967-11-10 1969-06-17 Deutsche Edelstahlwerke Ag Sintered carbide hard alloy
US3492101A (en) * 1967-05-10 1970-01-27 Chromalloy American Corp Work-hardenable refractory carbide tool steels
US3713788A (en) * 1970-10-21 1973-01-30 Chromalloy American Corp Powder metallurgy sintered corrosion and heat-resistant, age hardenable nickel-chromium refractory carbide alloy
US3715792A (en) * 1970-10-21 1973-02-13 Chromalloy American Corp Powder metallurgy sintered corrosion and wear resistant high chromium refractory carbide alloy
DE2208070A1 (de) * 1971-11-17 1973-05-24 Chromalloy American Corp Plasma-flammgespritzte titancarbidwerkzeugstahl-ueberzuege auf metallsubstraten, die so gebildeten verbundwerkstoffe und verfahren zu deren herstellung
US3771975A (en) * 1970-07-16 1973-11-13 Deutsche Edelstahlwerke Ag Sinter metal alloy
DE2411017A1 (de) * 1973-11-06 1975-05-07 Chromalloy American Corp Stahl-gebundene titancarbid-massen und deren herstellung sowie daraus gefertigte, gehaertete, verschleissfeste elemente
US3914113A (en) * 1970-09-11 1975-10-21 Quebec Iron & Titanium Corp Titanium carbide preparation
US3966423A (en) * 1973-11-06 1976-06-29 Mal M Kumar Grain refinement of titanium carbide tool steel
US4023739A (en) * 1975-04-09 1977-05-17 Uddeholms Aktiebolag Lining element for pulp refiners
US4180401A (en) * 1976-07-06 1979-12-25 Thyssen Edelstahlwerke Aktiengesellschaft Sintered steel alloy
US4194910A (en) * 1978-06-23 1980-03-25 Chromalloy American Corporation Sintered P/M products containing pre-alloyed titanium carbide additives
US4556424A (en) * 1983-10-13 1985-12-03 Reed Rock Bit Company Cermets having transformation-toughening properties and method of heat-treating to improve such properties
US5358545A (en) * 1990-09-18 1994-10-25 Carmet Company Corrosion resistant composition for wear products
US20150093286A1 (en) * 2013-09-30 2015-04-02 Advanced International Multitech Co., Ltd. Stainless steel alloy for golf club head
CN109196129A (zh) * 2016-05-19 2019-01-11 株式会社日本制钢所 铁基烧结合金及其制造方法
WO2020132085A1 (en) * 2018-12-19 2020-06-25 Oerlikon Metco (Us) Inc. High-temperature low-friction cobalt-free coating system for gate valves, ball valves, stems, and seats
EP3988229A1 (de) * 2020-10-26 2022-04-27 Deutsche Edelstahlwerke Specialty Steel GmbH & Co. KG Pulver für die verwendung in einem pulvermetallurgischen oder additiven verfahren, stahlwerkstoff und verfahren zur herstellung eines bauteils

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3472709A (en) * 1966-03-25 1969-10-14 Nasa Method of producing refractory composites containing tantalum carbide,hafnium carbide,and hafnium boride
US3496036A (en) * 1967-05-25 1970-02-17 Penn Nuclear Corp Process of making titanium alloy articles
US3450528A (en) * 1968-07-25 1969-06-17 Crucible Steel Corp Method for producing dispersioned hardenable steel
US3859085A (en) * 1971-05-12 1975-01-07 Toyoda Chuo Kenkyusho Kk Method for producing iron-base sintered alloys with high density
JPS57181367A (en) * 1981-04-08 1982-11-08 Furukawa Electric Co Ltd:The Sintered high-v high-speed steel and its production
JP5122068B2 (ja) * 2004-04-22 2013-01-16 株式会社小松製作所 Fe系耐摩耗摺動材料
US8246767B1 (en) * 2005-09-15 2012-08-21 The United States Of America, As Represented By The United States Department Of Energy Heat treated 9 Cr-1 Mo steel material for high temperature application
CN115029643B (zh) * 2022-05-16 2024-02-20 湖南英捷高科技有限责任公司 一种优异抗热震性能汽车零件及其制备方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2828202A (en) * 1954-10-08 1958-03-25 Sintercast Corp America Titanium tool steel
US3053706A (en) * 1959-04-27 1962-09-11 134 Woodworth Corp Heat treatable tool steel of high carbide content
US3093519A (en) * 1961-01-03 1963-06-11 Int Nickel Co Age-hardenable, martensitic iron-base alloys
US3093518A (en) * 1959-09-11 1963-06-11 Int Nickel Co Nickel alloy
US3132937A (en) * 1962-06-11 1964-05-12 Int Nickel Co Cast steel
US3303066A (en) * 1966-04-22 1967-02-07 Burgess Norton Mfg Co Powder metallurgy age hardenable alloys

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3183127A (en) * 1959-04-27 1965-05-11 Chromalloy Corp Heat treatable tool steel of high carbide content

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2828202A (en) * 1954-10-08 1958-03-25 Sintercast Corp America Titanium tool steel
US3053706A (en) * 1959-04-27 1962-09-11 134 Woodworth Corp Heat treatable tool steel of high carbide content
US3093518A (en) * 1959-09-11 1963-06-11 Int Nickel Co Nickel alloy
US3093519A (en) * 1961-01-03 1963-06-11 Int Nickel Co Age-hardenable, martensitic iron-base alloys
US3132937A (en) * 1962-06-11 1964-05-12 Int Nickel Co Cast steel
US3303066A (en) * 1966-04-22 1967-02-07 Burgess Norton Mfg Co Powder metallurgy age hardenable alloys

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3492101A (en) * 1967-05-10 1970-01-27 Chromalloy American Corp Work-hardenable refractory carbide tool steels
US3450511A (en) * 1967-11-10 1969-06-17 Deutsche Edelstahlwerke Ag Sintered carbide hard alloy
US3771975A (en) * 1970-07-16 1973-11-13 Deutsche Edelstahlwerke Ag Sinter metal alloy
US3914113A (en) * 1970-09-11 1975-10-21 Quebec Iron & Titanium Corp Titanium carbide preparation
US3713788A (en) * 1970-10-21 1973-01-30 Chromalloy American Corp Powder metallurgy sintered corrosion and heat-resistant, age hardenable nickel-chromium refractory carbide alloy
US3715792A (en) * 1970-10-21 1973-02-13 Chromalloy American Corp Powder metallurgy sintered corrosion and wear resistant high chromium refractory carbide alloy
DE2208070A1 (de) * 1971-11-17 1973-05-24 Chromalloy American Corp Plasma-flammgespritzte titancarbidwerkzeugstahl-ueberzuege auf metallsubstraten, die so gebildeten verbundwerkstoffe und verfahren zu deren herstellung
DE2411017A1 (de) * 1973-11-06 1975-05-07 Chromalloy American Corp Stahl-gebundene titancarbid-massen und deren herstellung sowie daraus gefertigte, gehaertete, verschleissfeste elemente
US3966423A (en) * 1973-11-06 1976-06-29 Mal M Kumar Grain refinement of titanium carbide tool steel
US4023739A (en) * 1975-04-09 1977-05-17 Uddeholms Aktiebolag Lining element for pulp refiners
US4180401A (en) * 1976-07-06 1979-12-25 Thyssen Edelstahlwerke Aktiengesellschaft Sintered steel alloy
US4194910A (en) * 1978-06-23 1980-03-25 Chromalloy American Corporation Sintered P/M products containing pre-alloyed titanium carbide additives
US4556424A (en) * 1983-10-13 1985-12-03 Reed Rock Bit Company Cermets having transformation-toughening properties and method of heat-treating to improve such properties
US5358545A (en) * 1990-09-18 1994-10-25 Carmet Company Corrosion resistant composition for wear products
US20150093286A1 (en) * 2013-09-30 2015-04-02 Advanced International Multitech Co., Ltd. Stainless steel alloy for golf club head
US10907240B2 (en) 2016-05-19 2021-02-02 The Japan Steel Works, Ltd. Iron-based sintered alloy and method for producing same
CN109196129A (zh) * 2016-05-19 2019-01-11 株式会社日本制钢所 铁基烧结合金及其制造方法
KR20190008863A (ko) * 2016-05-19 2019-01-25 가부시끼가이샤 니혼 세이꼬쇼 철계 소결 합금 및 그 제조 방법
US20190153573A1 (en) * 2016-05-19 2019-05-23 The Japan Steel Works, Ltd. Iron-based sintered alloy and method for producing same
EP3460083A4 (en) * 2016-05-19 2019-10-30 The Japan Steel Works, Ltd. IRON-BASED SINTERED ALLOY AND METHOD FOR THE PRODUCTION THEREOF
WO2020132085A1 (en) * 2018-12-19 2020-06-25 Oerlikon Metco (Us) Inc. High-temperature low-friction cobalt-free coating system for gate valves, ball valves, stems, and seats
CN113365766A (zh) * 2018-12-19 2021-09-07 欧瑞康美科(美国)公司 用于闸阀、球阀、阀杆和阀座的高温低摩擦无钴涂覆系统
US11644106B2 (en) 2018-12-19 2023-05-09 Oerlikon Metco (Us) Inc. High-temperature low-friction cobalt-free coating system for gate valves, ball valves, stems, and seats
CN113365766B (zh) * 2018-12-19 2024-04-05 欧瑞康美科(美国)公司 用于闸阀、球阀、阀杆和阀座的高温低摩擦无钴涂覆系统
EP3988229A1 (de) * 2020-10-26 2022-04-27 Deutsche Edelstahlwerke Specialty Steel GmbH & Co. KG Pulver für die verwendung in einem pulvermetallurgischen oder additiven verfahren, stahlwerkstoff und verfahren zur herstellung eines bauteils
WO2022090054A1 (de) 2020-10-26 2022-05-05 Deutsche Edelstahlwerke Specialty Steel Gmbh & Co. Kg Pulver für die verwendung in einem pulvermetallurgischen oder additiven verfahren, stahlwerkstoff und verfahren zur herstellung eines bauteils

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US3369892A (en) 1968-02-20
DE1298293B (de) 1969-06-26
CH465242A (fr) 1968-11-15
SE370959B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1974-11-04
GB1094829A (en) 1967-12-13

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