US3720504A - Sintered steel-bonded hard metal alloy and a method of preparing the same - Google Patents

Sintered steel-bonded hard metal alloy and a method of preparing the same Download PDF

Info

Publication number
US3720504A
US3720504A US00081497A US3720504DA US3720504A US 3720504 A US3720504 A US 3720504A US 00081497 A US00081497 A US 00081497A US 3720504D A US3720504D A US 3720504DA US 3720504 A US3720504 A US 3720504A
Authority
US
United States
Prior art keywords
hard metal
steel
alloys
weight
graphite
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00081497A
Inventor
F Frehn
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsche Edelstahlwerke AG
Original Assignee
Deutsche Edelstahlwerke AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Deutsche Edelstahlwerke AG filed Critical Deutsche Edelstahlwerke AG
Application granted granted Critical
Publication of US3720504A publication Critical patent/US3720504A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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 sintered alloy of the type comprising a steel matrix and one or more metal carbides and which has high abrasion resistance, is characterized by the presence of free graphite in the steel matrix.
  • Such sintered alloys are obtained by a method of sintering in which the sintered alloys are maintained for an extended period of time at sintering temperatures followed by controlled cooling.
  • This invention relates to sintered steel-bonded hard metal alloys, and particularly relates to such alloys containing primarily metal carbide e.g. titanium carbide, and to a method of producing such alloys.
  • metal carbide e.g. titanium carbide
  • Hard metal alloys in which one of the components is a hard metal, namely a metal carbide, boride, nitride or silicide, and the other component is steel, are well known. Due to the high content of hard metal amounting to between 10 and 75% by weight of the alloy, such hard metal alloys are extremely abrasion-resistant and are used for instance for making plastics-forming tools, such as draw plates.
  • Such materials may be porous sintered bearing materials, consisting for instance of iron, bronze, copper, German silver, plastics, carbon and other materials. Their lubricating properties derive from the fact that their pores are filled with oil, or materials such as copper, phosphor bronze and similar materials may have an inherent lubricity.
  • Other materials that have self-lubricating properties are cast irons in which the presence of flaky or spheroidal graphite together with phosphides and sulphides is responsible for a self-lubricating effect.
  • Other cast iron types contain minor proportions of chromium carbides and molybdenum carbides and possess a somewhat improved abrasion resistance. However, the wear-resistance of these materials likewise falls short of requirements.
  • the present invention provides a highly abrasion resistant hard alloy which has self-lubricating properties, and which is suitable for the fabrication of parts that in use will be exposed to considerable rubbing wear.
  • the invention provides a sintered steel-bonded hard metal alloy consisting essentially of 10 to 75% by weight of hard metal consisting substantially of one or more metal td States atent 3,720,504 Patented Mar. 13, 1973 carbides, and from to 90% by weight of a steel matrix containing free graphite.
  • the graphite content of alloys according to the invention is preferably between 0.8% and 3.9% by Weight based on the total weight of the alloy.
  • Preferred hard metal alloys according to the invention consist essentially of all percentages being by weight.
  • 7 metal alloys is preferably from 15 to 35%.
  • titanium carbide in the said preferred alloys may be replaced by one or more other metal carbides.
  • the resultant structure resembles that of cast iron and has the self-lubricating properties of the latter.
  • Tests have confirmed that the life of steel-bonded hard metal alloys that are known to be extremely abrasionresistant is substantially prolonged by the addition of the graphite in the steel matrix whenever alloys according to the invention are subjected to rubbing wear.
  • the wearresistance to rubbing friction was also found to exist in situations when only one of the two frictionally co-operating parts consisted of the steel-bonded hard metal alloy according to the invention, and the other of another material.
  • solubilities during sintering differ from those obtaining when a melt freezes, during which freezing carbon is primarily precipitated only from hypereutectic alloys (above 4.3% by weight of C), and continuing solidification causing graphite to attach itself to the carbon.
  • freezing carbon is primarily precipitated only from hypereutectic alloys (above 4.3% by weight of C)
  • graphite to attach itself to the carbon.
  • the formation of cementite must be prevented and the solution of the carbon in the iron assured. Consequently the manner in which the overall sintering treatment of hard metal alloys according to the invention is conducted is of primary importance.
  • a method according to the invention of sintering the said hard metal alloys is provided by forming a pressing of powdered starting materials (namely the elements forming the hard metal component and the steel matrix), and heating the pressing at the rate of from 80 to 100 C. per hour to a sintering temperature of from 1000 to 1200 C., maintaining the thus-heated pressing at the sintering temperature for at least 4, and preferably from 4 to 6 hours, cooling the sintered pressing at the rate of from 30 to 50 C. per hour to a temperature between 750 and 850C, and then further coolingthe pressing to room temperature at the rate of from 100 to 200 C. per hour.
  • powdered starting materials namely the elements forming the hard metal component and the steel matrix
  • the successful sintering of the process depends on the chemical composition, since during sintering the reaction proceeds and a hard brittle material resembling white iron is produced having properties that are the exact reverse of those of the required material.
  • the randomly-orientated graphite improves the resistance to temperature shock and the thermal conductivity of the material.
  • the deliberately non-orientated, but finely and evenly distributed graphite flakes lead to a very low coefficient of friction and a high resistance to heat cracking which may occur when high and rapid surface friction arises, as when parts are inexpertly ground and the temperature is allowed to fluctuate by rapid heating and cooling.
  • a hard metal alloy according to the invention was prepared containing 20% by weight of titanium carbide, 2.5% by weight of carbon, 2.0% by weight of silicon, 1.5% by Weight of nickel, balance iron.
  • the steel matrix was purely ferritic and the graphite was present in spheroidal and flaky form.
  • the titanium carbide was evenly distributed in grain sizes between 1 and 3 m.
  • the hardness of the said alloy was 33 to 36 HRC, corresponding to 321 to 35.3 H8.
  • the proportion by volume of the graphite was in the range 35 to 40%, and provided the alloy with the desired self-lubricating property in addition to resistance to abrasive wear.
  • This ferritic structure containing flaky graphite lamellae and having a titanium carbide content provides outstanding damping properties which improve even further with greater carbon contents, i.e. a pearlitic structure.
  • An increase of the nickel content to 36.0% by weight leads to the production of an austenitic matrix having embedded therein titanium carbides and graphite, the content of carbon controlling the quantity of graphite present.
  • Such austenitic alloys are corrosion resistant, nonmagnetic, non-scaling, very tough and also satisfactorily machinable.
  • the coefficient of thermal expansion of austenitic alloys is nearly twice that of ferritic or pearlitic alloys containing titanium carbide and graphite.
  • Manganese contents encourage the formation of austenite and may be as high as 7.0% by weight.
  • Aluminium in quantities up to 7.0% by weight increases the volume of the liquid phase, which is desirable when the hard metal contents are high.
  • Copper up to 8.0% by weight has an aging effect and also improves the lubricity of the alloy.
  • Boron up to 0.1% by weight has a deoxidant effect in the interior of the alloy and causes existing oxygen to be bound by forming B 0 in the alloy, which easily volatilises at relatively low temperatures in a vacuum.
  • the elements, chromium, molybdenum, vanadium and titanium are not often required in hard metal alloys according to the invention, because they are strong carbide-formers that would at once react with the graphite. However, they may be incorporated in total quantities not exceeding 2.0% by weight, for hardening the alloy.
  • the production of hard metal alloys according to the invention utilizes the main constituents, namely hard metal, and the individual components of the steel matrix.
  • the individual elements forming the hard metal component and the steel matrix, or key alloys containing the same such as carbonyl iron, graphite, silicon, for instance in the form of ferrosilicon, may be dry mixed, wet ground to a grain size of 1 to 3 ,um., vacuum dried, pressed and sintered in a vacuum of 2 '10 torr at about 1100 C.
  • Sintering proceeds in the manner hereinbefore described by slow heating, soaking for several hours at sintering temperature and gradual cooling in stages after sintering has taken place.
  • a heat treatment of the sintered hard metal alloy may subsequently be carried out. This may comprise annealing to relieve internal stress without affecting the structure at a temperature between 550 and 650 C.
  • a heat treatment may be performed between 650 and 800 C.
  • For pearlitic basic structures hardening in oil at 870 to 900 C. followed by drawing between 200 and 240 C. may be performed.
  • Steel-bonded hard metal alloys according to the invention are particularly suitable for providing parts that are subject to rubbing friction and that should therefore have self-lubricating properties to prevent the co-operating part from being excessively worn. Thus they may be used for a variety of specific applications, for instance for bearings which may work at temperatures rising up to 900 C. if the matrix is austenitic, for brake drums, brake shoes, brake blocks, clutch presser plates, valve tappets, liners, sealing rings, gaskets, piston rings, parts of machinery and pump parts.
  • the cost of production thereof may be reduced.
  • a sintered steel-bonded hard metal alloy consisting essentially of 10 to 75% by weight of hard metal consisting substantially of one or more metal carbides and from 25% to by weight of a steel matrix containing free graphite.
  • a hard metal alloy according to claim 1 having a composition (by weight):
  • a hard metal alloy according to claim 4 containing from to of titanium carbide.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

A SINTERED ALLOY OF THE TYPE COMPRISING A STEEL MATRIX AND ONE OR MORE METAL CARBIDES AND WHICH HAS HIGH ABRASION RESISTANCE, IS CHARACTERIZED BY THE PRESENCE OF FREE GRAPHITE IN THE STEEL MATRIX. SUCH SINTERED ALLOYS ARE OBTAINED BY A METHOD OF SINTERING IN WHICH THE SINTERED ALLOYS ARE MAINTAINED FOR AN EXTENDED PERIOD OF TIME AT SINTERING TEMPERATURES FOLLOWED BY CONTROLLED COOLING.

Description

SINTERED STEEL-BONDED HARD METAL ALLOY AND A METHOD OF PREPARING THE SAME Fritz Frehn, Krefeld, Germany, assignor to Deutsche Edelstahlwerke Aktiengesellschaft, Krefeld, Germany No Drawing. Filed Oct. 16, 1970, Ser. No. 81,497 Claims priority, application Germany, Oct. 24, 1969,
P 19 53 481.7 Int. Cl. B22f 1/00 US. Cl. 29182.7 7 Claims ABSTRACT OF THE DISCLOSURE A sintered alloy of the type comprising a steel matrix and one or more metal carbides and which has high abrasion resistance, is characterized by the presence of free graphite in the steel matrix. Such sintered alloys are obtained by a method of sintering in which the sintered alloys are maintained for an extended period of time at sintering temperatures followed by controlled cooling.
This invention relates to sintered steel-bonded hard metal alloys, and particularly relates to such alloys containing primarily metal carbide e.g. titanium carbide, and to a method of producing such alloys.
Hard metal alloys in which one of the components is a hard metal, namely a metal carbide, boride, nitride or silicide, and the other component is steel, are well known. Due to the high content of hard metal amounting to between 10 and 75% by weight of the alloy, such hard metal alloys are extremely abrasion-resistant and are used for instance for making plastics-forming tools, such as draw plates.
For parts that are subject to abrasive wear conventional steel-bonded hard metal alloys have not hitherto proved entirely satisfactory. When two parts consisting of conventional hard metal alloys are in sliding contact, even slight surface roughness causes high rubbing friction immediately on failure of the lubricant film between the two surfaces, or its absence. In circumstances when one sliding part consists of a steel-bonded hard metal alloy and the other consists of another material, which for structural reasons frequently obtains, for instance when a steel shaft runs in steel-bonded hard metal alloy bearing bushes, then the part which does not consist of a steel-bonded hard metal alloy experiences very high abrasive wear by the rubbing action of the steel-bonded hard metal alloy part.
Materials that have so-called emergency running properties are also known, but these have little if any resistance to abrasive wear. Such materials may be porous sintered bearing materials, consisting for instance of iron, bronze, copper, German silver, plastics, carbon and other materials. Their lubricating properties derive from the fact that their pores are filled with oil, or materials such as copper, phosphor bronze and similar materials may have an inherent lubricity. Other materials that have self-lubricating properties are cast irons in which the presence of flaky or spheroidal graphite together with phosphides and sulphides is responsible for a self-lubricating effect. Other cast iron types contain minor proportions of chromium carbides and molybdenum carbides and possess a somewhat improved abrasion resistance. However, the wear-resistance of these materials likewise falls short of requirements.
The present invention provides a highly abrasion resistant hard alloy which has self-lubricating properties, and which is suitable for the fabrication of parts that in use will be exposed to considerable rubbing wear.
The invention provides a sintered steel-bonded hard metal alloy consisting essentially of 10 to 75% by weight of hard metal consisting substantially of one or more metal td States atent 3,720,504 Patented Mar. 13, 1973 carbides, and from to 90% by weight of a steel matrix containing free graphite.
The graphite content of alloys according to the invention is preferably between 0.8% and 3.9% by Weight based on the total weight of the alloy.
Preferred hard metal alloys according to the invention consist essentially of all percentages being by weight.
7 metal alloys is preferably from 15 to 35%.
Up to 50% by weight of the titanium carbide in the said preferred alloys may be replaced by one or more other metal carbides.
Due to the presence of the graphite present in the steel matrix of the steel-bonded hard metal alloy according to the invention, the resultant structure resembles that of cast iron and has the self-lubricating properties of the latter. Tests have confirmed that the life of steel-bonded hard metal alloys that are known to be extremely abrasionresistant is substantially prolonged by the addition of the graphite in the steel matrix whenever alloys according to the invention are subjected to rubbing wear. The wearresistance to rubbing friction was also found to exist in situations when only one of the two frictionally co-operating parts consisted of the steel-bonded hard metal alloy according to the invention, and the other of another material.
Due to the relatively high content of hard metal in the alloys according to the invention, such alloys can be produced only by conventional powder metallurgical techniques. A particular difficulty is the introduction of the free graphite into the steel matrix. The unusually high carbon content of the steel matrix in the alloys and the resultant low-melting eutectic in the stable system of the iron-carbon phase diagram (4.3% by weight C and 1153 C.) are responsble for major difiiculties met in sintering, particularly since the proportion of this phase exceeds 50% by volume, and more particularly since completely dense, i.e. completely non-porous sinter bodies, are required. The solution of the carbon during sintering and its precipitation in the form of free graphite when cooling from sintering temperature give rise to complicated shrinkage conditions. The low density of the graphite compared with iron is a decisive factor in providing such difiiculties.
The solubilities during sintering differ from those obtaining when a melt freezes, during which freezing carbon is primarily precipitated only from hypereutectic alloys (above 4.3% by weight of C), and continuing solidification causing graphite to attach itself to the carbon. By contrast, during sintering the formation of cementite must be prevented and the solution of the carbon in the iron assured. Consequently the manner in which the overall sintering treatment of hard metal alloys according to the invention is conducted is of primary importance.
A method according to the invention of sintering the said hard metal alloys is provided by forming a pressing of powdered starting materials (namely the elements forming the hard metal component and the steel matrix), and heating the pressing at the rate of from 80 to 100 C. per hour to a sintering temperature of from 1000 to 1200 C., maintaining the thus-heated pressing at the sintering temperature for at least 4, and preferably from 4 to 6 hours, cooling the sintered pressing at the rate of from 30 to 50 C. per hour to a temperature between 750 and 850C, and then further coolingthe pressing to room temperature at the rate of from 100 to 200 C. per hour.
The successful sintering of the process depends on the chemical composition, since during sintering the reaction proceeds and a hard brittle material resembling white iron is produced having properties that are the exact reverse of those of the required material.
The addition of preferably at least 1% by weight of silicon, usually in the form of ferrosilicon, substantially inhibits the formation of cementite and promotes the formation of graphite. Aluminium and titanium have a similar effect. A particularly important step however is the method of sintering, i.e. a soaking time of at least 4, preferably 4 to 6 hours at sintering temperature and a cooling step that lasts for several hours as hereinbefore described to establish equilibrium between the alloy components, in order to precipitate the graphite in even distribution and to produce it in a desirable fiaky form to provide the lubrication of the thus-produced material. The randomly-orientated graphite improves the resistance to temperature shock and the thermal conductivity of the material. The deliberately non-orientated, but finely and evenly distributed graphite flakes lead to a very low coefficient of friction and a high resistance to heat cracking which may occur when high and rapid surface friction arises, as when parts are inexpertly ground and the temperature is allowed to fluctuate by rapid heating and cooling.
A hard metal alloy according to the invention was prepared containing 20% by weight of titanium carbide, 2.5% by weight of carbon, 2.0% by weight of silicon, 1.5% by Weight of nickel, balance iron. The steel matrix was purely ferritic and the graphite was present in spheroidal and flaky form. The titanium carbide was evenly distributed in grain sizes between 1 and 3 m. The hardness of the said alloy was 33 to 36 HRC, corresponding to 321 to 35.3 H8. The proportion by volume of the graphite was in the range 35 to 40%, and provided the alloy with the desired self-lubricating property in addition to resistance to abrasive wear. This ferritic structure containing flaky graphite lamellae and having a titanium carbide content provides outstanding damping properties which improve even further with greater carbon contents, i.e. a pearlitic structure.
Additions of silicon in a quantity of from 0.5% to 6.0% by weight that are necessary for graphitisation improve the corrosion resistance.
An increase of the nickel content to 36.0% by weight leads to the production of an austenitic matrix having embedded therein titanium carbides and graphite, the content of carbon controlling the quantity of graphite present. Such austenitic alloys are corrosion resistant, nonmagnetic, non-scaling, very tough and also satisfactorily machinable. The coefficient of thermal expansion of austenitic alloys is nearly twice that of ferritic or pearlitic alloys containing titanium carbide and graphite.
Manganese contents encourage the formation of austenite and may be as high as 7.0% by weight.
Aluminium in quantities up to 7.0% by weight increases the volume of the liquid phase, which is desirable when the hard metal contents are high.
Copper up to 8.0% by weight has an aging effect and also improves the lubricity of the alloy.
Additions of magnesium and/ or cerium cause the graphite to appear in the spheroidal form, as in the case of cast iron.
Boron up to 0.1% by weight has a deoxidant effect in the interior of the alloy and causes existing oxygen to be bound by forming B 0 in the alloy, which easily volatilises at relatively low temperatures in a vacuum.
The elements, chromium, molybdenum, vanadium and titanium are not often required in hard metal alloys according to the invention, because they are strong carbide-formers that would at once react with the graphite. However, they may be incorporated in total quantities not exceeding 2.0% by weight, for hardening the alloy.
The production of hard metal alloys according to the invention utilizes the main constituents, namely hard metal, and the individual components of the steel matrix. The individual elements forming the hard metal component and the steel matrix, or key alloys containing the same such as carbonyl iron, graphite, silicon, for instance in the form of ferrosilicon, may be dry mixed, wet ground to a grain size of 1 to 3 ,um., vacuum dried, pressed and sintered in a vacuum of 2 '10 torr at about 1100 C.
Sintering proceeds in the manner hereinbefore described by slow heating, soaking for several hours at sintering temperature and gradual cooling in stages after sintering has taken place. A heat treatment of the sintered hard metal alloy may subsequently be carried out. This may comprise annealing to relieve internal stress without affecting the structure at a temperature between 550 and 650 C. For changing the streaky pearlite into a grainy pearlite a heat treatment may be performed between 650 and 800 C. For forming a ferritic matrix soft annealing between 800 and 925 C. is desirable. This causes the Fe C to decompose completely with an accompanying increase in volume. For pearlitic basic structures hardening in oil at 870 to 900 C. followed by drawing between 200 and 240 C. may be performed.
Steel-bonded hard metal alloys according to the invention are particularly suitable for providing parts that are subject to rubbing friction and that should therefore have self-lubricating properties to prevent the co-operating part from being excessively worn. Thus they may be used for a variety of specific applications, for instance for bearings which may work at temperatures rising up to 900 C. if the matrix is austenitic, for brake drums, brake shoes, brake blocks, clutch presser plates, valve tappets, liners, sealing rings, gaskets, piston rings, parts of machinery and pump parts. By associating parts made of the alloys according to the invention with steel or cast iron backing elements to which the alloy elements are soldered, welded or bolted, the cost of production thereof may be reduced.
What is claimed is:
1. A sintered steel-bonded hard metal alloy consisting essentially of 10 to 75% by weight of hard metal consisting substantially of one or more metal carbides and from 25% to by weight of a steel matrix containing free graphite.
2. A hard metal alloy according to claim 1, wherein the said steel matrix contains from 0.8% to 3.9% by wcleight of free graphite based on the overall weight of the al oy.
3. A hard metal alloy according to claim 1, wherein the said metal-carbide is titanium carbide.
4. A hard metal alloy according to claim 1, having a composition (by weight):
Aluminium 0-7,0
Percent Manganese 0-7.0 Nickel 0-360 Copper 0-8.0 Magnesium 0-0.1 Cerium 0-0.1 Boron 0-0.1 Total of chromium, molybdenum, vanadium, titanium 0-2.0 Iron with a content of combined carbon necessary for the hardening of the alloy Balance 5. A hard metal alloy according to claim 4, containing from to of titanium carbide.
6. A hard metal alloy according to claim 4, in which up to of the titanium carbide is replaced by one or more other metal carbides.
7. A method of producing a hard metal alloy consisting essentially of 10% to by weight of hard metal consisting essentially of at least one metal carbide and from 25% to by weight of a steel matrix containing free graphite, said method comprising:
mixing the at least one metal carbide and the components of the steel matrix together, forming pressings thereof, and
heating the pressings at the rate of 80 to C. per
hour to a sintering temperature of from 1000 to 1200 C., maintaining the thus-heated pressings at References Cited UNITED STATES PATENTS Gregory et al. 29-1827 Geotzel et al 75--203 Holtz, Jr 29-182.7 Prill et al 29-1827 Frehn 29-182.7 Ellis et al 29--182.7 Tarkan et a1 29182.8
OTHER REFERENCES Roberts et al., Tool Steels, 3rd ed., ASM (1962), p.
CARL D. QUARFORTH, Primary Examiner B. HUNT, Assistant Examiner US. Cl. X.R.
US00081497A 1969-10-24 1970-10-16 Sintered steel-bonded hard metal alloy and a method of preparing the same Expired - Lifetime US3720504A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1953481A DE1953481C2 (en) 1969-10-24 1969-10-24 Sintered steel-bonded carbide hard alloy and process for their manufacture

Publications (1)

Publication Number Publication Date
US3720504A true US3720504A (en) 1973-03-13

Family

ID=5749027

Family Applications (1)

Application Number Title Priority Date Filing Date
US00081497A Expired - Lifetime US3720504A (en) 1969-10-24 1970-10-16 Sintered steel-bonded hard metal alloy and a method of preparing the same

Country Status (7)

Country Link
US (1) US3720504A (en)
JP (1) JPS5031848B1 (en)
CH (1) CH557882A (en)
DE (1) DE1953481C2 (en)
FR (1) FR2066359A5 (en)
GB (1) GB1316298A (en)
SE (1) SE362444B (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3918924A (en) * 1972-06-13 1975-11-11 Chugai Electric Ind Co Ltd Method for producing wear-resistant ferrous sintered metal containing high amounts of titanium carbide grains and carbon particles
US3966423A (en) * 1973-11-06 1976-06-29 Mal M Kumar Grain refinement of titanium carbide tool steel
US3967935A (en) * 1972-09-11 1976-07-06 Deutsche Edelstahlwerke Gesellschaft Mit Beschrankter Haftung Corrosion and wear resistant steel sinter alloy
US3977837A (en) * 1973-11-06 1976-08-31 Chromalloy American Corporation Titanium carbide tool steel having improved properties
US3981062A (en) * 1973-10-01 1976-09-21 Ford Motor Company Apex seal composition for rotary engines
US4156606A (en) * 1976-11-18 1979-05-29 Thyssen Edelstahlwerke Ag Hard-material alloy for use in tool parts and parts subject to wear
US4287643A (en) * 1977-09-13 1981-09-08 Trutzschler Gmbh & Co. Carding element
DE19743745A1 (en) * 1997-10-02 1999-04-08 Schlafhorst & Co W Roller saw tooth fitting
US20050217764A1 (en) * 2004-04-05 2005-10-06 Takemori Takayama Ferrous abrasion resistant sliding materials and sliding members
US20060046867A1 (en) * 2004-09-01 2006-03-02 Murphy James M Golf club shaft having a steel and graphite composition
US20060237412A1 (en) * 2005-04-22 2006-10-26 Wallin Jack G Welding compositions for improved mechanical properties in the welding of cast iron
US20180154449A1 (en) * 2016-12-06 2018-06-07 Miba Sinter Austria Gmbh Method for producing a swashplate

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE399911C (en) * 1976-02-05 1980-02-18 Sandvik Ab Wear detail with high durability and good toughness, composed of solid metal and cast iron
EP0062311B1 (en) * 1981-04-06 1985-07-17 Mitsubishi Materials Corporation Tungsten carbide-base hard alloy for hot-working apparatus members
DE3128236C2 (en) * 1981-04-09 1983-12-22 Thyssen Edelstahlwerke AG, 4000 Düsseldorf Self-lubricating hard alloy
DE102017203076A1 (en) * 2017-02-24 2018-08-30 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Composite materials with very high wear resistance

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3918924A (en) * 1972-06-13 1975-11-11 Chugai Electric Ind Co Ltd Method for producing wear-resistant ferrous sintered metal containing high amounts of titanium carbide grains and carbon particles
US3967935A (en) * 1972-09-11 1976-07-06 Deutsche Edelstahlwerke Gesellschaft Mit Beschrankter Haftung Corrosion and wear resistant steel sinter alloy
US3981062A (en) * 1973-10-01 1976-09-21 Ford Motor Company Apex seal composition for rotary engines
US3966423A (en) * 1973-11-06 1976-06-29 Mal M Kumar Grain refinement of titanium carbide tool steel
US3977837A (en) * 1973-11-06 1976-08-31 Chromalloy American Corporation Titanium carbide tool steel having improved properties
US4156606A (en) * 1976-11-18 1979-05-29 Thyssen Edelstahlwerke Ag Hard-material alloy for use in tool parts and parts subject to wear
US4287643A (en) * 1977-09-13 1981-09-08 Trutzschler Gmbh & Co. Carding element
DE19743745A1 (en) * 1997-10-02 1999-04-08 Schlafhorst & Co W Roller saw tooth fitting
US6101805A (en) * 1997-10-02 2000-08-15 W. Schlafhorst Ag & Co. Opening roller for an open-end spinning device
US8480820B2 (en) * 2004-04-05 2013-07-09 Komatsu Ltd. Ferrous abrasion resistant sliding materials and sliding members
US20050217764A1 (en) * 2004-04-05 2005-10-06 Takemori Takayama Ferrous abrasion resistant sliding materials and sliding members
US20060046867A1 (en) * 2004-09-01 2006-03-02 Murphy James M Golf club shaft having a steel and graphite composition
US20060237412A1 (en) * 2005-04-22 2006-10-26 Wallin Jack G Welding compositions for improved mechanical properties in the welding of cast iron
US20130294820A1 (en) * 2005-04-22 2013-11-07 Stoody Company Welding compositions for improved mechanical properties in the welding of cast iron
US9403241B2 (en) * 2005-04-22 2016-08-02 Stoody Company Welding compositions for improved mechanical properties in the welding of cast iron
US9409259B2 (en) * 2005-04-22 2016-08-09 Stoody Company Welding compositions for improved mechanical properties in the welding of cast iron
US20180154449A1 (en) * 2016-12-06 2018-06-07 Miba Sinter Austria Gmbh Method for producing a swashplate
CN108150379A (en) * 2016-12-06 2018-06-12 米巴烧结奥地利有限公司 For manufacturing the method for swash plate
US10792733B2 (en) * 2016-12-06 2020-10-06 Miba Sinter Austria Gmbh Method for producing a swashplate
CN108150379B (en) * 2016-12-06 2021-04-23 米巴烧结奥地利有限公司 Method for producing a swash plate

Also Published As

Publication number Publication date
FR2066359A5 (en) 1971-08-06
DE1953481C2 (en) 1973-11-15
JPS5031848B1 (en) 1975-10-15
SE362444B (en) 1973-12-10
CH557882A (en) 1975-01-15
GB1316298A (en) 1973-05-09
DE1953481A1 (en) 1972-02-10
DE1953481B2 (en) 1972-07-06

Similar Documents

Publication Publication Date Title
US3720504A (en) Sintered steel-bonded hard metal alloy and a method of preparing the same
US4970049A (en) Sintered materials
Glaeser Materials for tribology
JP4799004B2 (en) Fe-based seal sliding member and manufacturing method thereof
US2828202A (en) Titanium tool steel
US3053706A (en) Heat treatable tool steel of high carbide content
US4271239A (en) Sintered metal articles and process for their manufacture
US3782930A (en) Graphite-containing ferrous-titanium carbide composition
CN1278563A (en) Solid self-lubricating wear-resisting alloy cast material
US6039785A (en) Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear
JPH0610103A (en) Vane material excellent in wear resistance and sliding property
Igharo et al. Effects of consolidation parameters on properties of sintered high speed steels
JPS6389642A (en) Abrasion resistant iron sintered article
US4420539A (en) Process for producing antifriction materials
US2494238A (en) Method of making gray cast iron
JPH08501832A (en) Method of producing sintered alloy steel components
US4909843A (en) Highly wear-resistant iron-nickel-copper-molybdenum sintered alloy with addition of phosphorous
JPH06322470A (en) Cast iron powder for powder metallurgy and wear resistant ferrous sintered alloy
JPS62164850A (en) Wear resistant ferrous sintered alloy and its production
JP2564528B2 (en) High corrosion and wear resistant tools, materials for parts
JPS5934223B2 (en) Self-lubricating sintered member and its manufacturing method
Novytskyi et al. Effect of copper on tribological characteristics and subsurface structure of cast Fe-Cr-C alloys in sliding friction
SU449970A1 (en) Cermet antifriction material
US2035392A (en) Copper steel alloys
JP2600245B2 (en) Vane lumber