WO2000062960A1 - Materiau de moulage a base de poudre metallique et corps moule par recompression, corps fritte obtenu a partir dudit corps moule par recompression, et procedes de production y relatifs - Google Patents
Materiau de moulage a base de poudre metallique et corps moule par recompression, corps fritte obtenu a partir dudit corps moule par recompression, et procedes de production y relatifs Download PDFInfo
- Publication number
- WO2000062960A1 WO2000062960A1 PCT/JP2000/001615 JP0001615W WO0062960A1 WO 2000062960 A1 WO2000062960 A1 WO 2000062960A1 JP 0001615 W JP0001615 W JP 0001615W WO 0062960 A1 WO0062960 A1 WO 0062960A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- metal powder
- molding
- graphite
- molding material
- sintered body
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/02—Compacting only
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
Definitions
- the present invention relates to a metal powder compact, a recompressed compact thereof, a sintered body obtained from the recompressed compact, and a method for producing the same.
- the present invention relates to a metal powder compact, a recompressed compact thereof, a sintered compact obtained from the recompressed compact, and a method for producing the same, which are suitable for obtaining various structural mechanical parts made of a sintered metal.
- Background art
- the basic process of obtaining sintered metal is mixing of raw material powder, compacting, sintering and post-treatment (heat treatment, etc.).
- a product can be obtained only by the above steps, but in many cases, between or after each step, additional processing or various treatments are performed according to the purpose.
- Japanese Patent Application Laid-Open No. 1-123005 discloses that in order to obtain a mechanical component having high mechanical strength by using a sintered metal, a mixed powder is compacted to form a preform, A production method is disclosed in which after the preliminary spherical body is pre-sintered to form a molding material, the molding material is recompressed (cold forged) and sintered (main sintering).
- the re-compression molding (cold forging) process of the molding material comprises a temporary compression molding process and a main compression molding process, and a liquid lubricant is applied to the surface of the molding material to perform the temporary compression molding. Thereafter, a negative pressure is applied to the molding material to remove the lubricant by suction, and then the compression molding of the molding material is performed.
- the amount of carbon in the product that is, the amount of graphite added to the metal powder.
- the value is increased, the elongation of the molding material is reduced and the hardness is increased. Therefore, the deformability of the molding material when it is recompressed is reduced, which causes a problem that the recompression molding becomes difficult.
- the preformed body is pre-sintered to form a forming material.
- the molding material plays an important factor in determining the ease of recompression molding and the mechanical properties of the obtained mechanical part. In order to achieve this, it was necessary to obtain a molding material that contained a certain amount of graphite, had high elongation, had low hardness, and had excellent deformability. Was.
- the properties of the molding material containing the predetermined amount of graphite, particularly the elongation and hardness, which are important properties for the ease of recompression molding of the molding material are as follows. It has been found that the density is determined by the density of the preformed body before the formation, the structure of the forming material obtained by temporarily sintering the preformed body, and in particular, the form of carbon contained in the forming material. Disclosure of the invention
- the present invention has been devised in view of the conventional circumstances described above, and is a method for recompressing a metal powder molding material having excellent deformability, which is suitable for obtaining a mechanical part having high mechanical strength by a sintered metal. It is an object of the present invention to provide a molded body, a sintered body obtained from the recompression molded body, and a method for producing the same.
- the invention of claim 1 is directed to a preliminary powder having a density of 7.3 g / cm 3 or more obtained by compacting a metal powder obtained by mixing graphite with a metal powder containing iron as a main component.
- the compact was pre-sintered at a temperature of 700 to 100 ° C. to obtain a metal powder compact having a structure in which graphite remains at the grain boundaries of the metal powder.
- the invention according to claim 2 is characterized in that the amount of graphite mixed with the metal powder is 0.3% by weight or more.
- the invention according to claim 3 is characterized in that the metal powder molding material according to claim 1 or 2 is recompressed to form a recompressed body.
- the invention according to claim 4 is a method for producing a recompression-molded article, comprising: pressing a metal powder obtained by mixing graphite with a metal powder containing iron as a main component; A preforming step of obtaining a preformed body of 7.3 g Z cm 3 or more,
- the preformed body obtained in this preforming step is calcined at a temperature of 700 to 100 ° C. to form a metal having a structure in which graphite remains at the grain boundaries of the metal powder.
- a preliminary sintering process for obtaining a powdered material is calcined at a temperature of 700 to 100 ° C. to form a metal having a structure in which graphite remains at the grain boundaries of the metal powder.
- It is characterized in that it comprises a recompression step of recompressing the metal powder molding material obtained in the preliminary sintering step.
- the molding space of the molding die includes a large-diameter portion into which an upper punch is inserted, a small-diameter portion into which a lower punch is inserted, and a taper portion connecting the large-diameter portion and the small-diameter portion.
- One or both of the lower punches is characterized in that a notch is provided at the outer peripheral end of the end face facing the molding space of the molding die to increase the volume of the molding space.
- the amount of graphite mixed with the metal powder is set to 0.3% by weight or more. It is special.
- metallic powder obtained by mixing graphite in a metal powder containing iron as a main component was obtained by compacting, density 7. 3 g Z cm 3 or more preforming
- the body is pre-sintered at a temperature of 700 to 100000 to form a metal powder molding material having a structure in which graphite remains at the grain boundaries of the metal powder,
- the re-compression molded body is re-sintered at a predetermined temperature
- the sintered body has a structure in which graphite is diffused and remains at a predetermined ratio in the metal powder and its grain boundaries.
- the invention according to claim 8 is characterized in that the amount of graphite mixed with the metal powder of the sintered body according to claim 7 is 0.3% by weight or more.
- the invention according to claim 9 is a method for producing a sintered body, comprising: pressing a metal powder obtained by mixing graphite with a metal powder containing iron as a main component; . a preforming step of obtaining a 3 g / cm 3 or more preforms,
- the pre-formed body obtained in this pre-forming step is calcined at a temperature of 700 to 100 ° C. to obtain a metal having a structure in which graphite remains at the grain boundaries of the metal powder.
- a temporary sintering process to obtain a powdered material A recompression step of recompressing the metal powder molding material obtained in the preliminary sintering step to obtain a recompression molded body;
- the metal powder filled in the forming space of the forming die is formed by an upper punch and a lower punch. Formed by pressing,
- the molding space of the molding die includes a large-diameter portion into which an upper punch is inserted, a small-diameter portion into which a lower punch is inserted, and a taper portion connecting the large-diameter portion and the small-diameter portion.
- One or both of the punch and the lower punch is characterized in that a notch for increasing the volume of the molding space is provided at the outer peripheral end of the end face facing the molding space of the molding die.
- the invention according to claim 11 is the method for manufacturing a sintered body according to claim 9 or 10, wherein the amount of graphite mixed with the metal powder is set to 0.3% by weight or more. It features.
- the invention according to claim 12 is characterized in that a density of 7.3 g Z cm 3 or more obtained by compacting a metal powder obtained by mixing graphite with a metal powder containing iron as a main component.
- the preform is pre-sintered at a temperature of 700 to 100 ° C. to form a metal powder molding material having a structure in which graphite remains at the grain boundaries of the metal powder.
- the re-compression molded body is re-sintered at a predetermined temperature
- the amount of graphite mixed with the metal powder is set to 0.3% by weight or more.
- a metal powder obtained by mixing graphite with a metal powder containing iron as a main component is compacted to have a density of 7.3 gZcm 3 or more.
- the pre-formed body obtained in this pre-forming step is pre-sintered at 70.0 to 10000 ° C. to obtain a metal powder molding material having a structure in which graphite remains at grain boundaries of the metal powder. Sintering process,
- It is characterized in that it comprises a heat treatment step of heat treating the sintered body obtained in the resintering step.
- the preforming step comprises: forming a metal powder filled in a forming space of a forming die into an upper punch and a lower punch. And formed by pressing
- the molding space of the molding die includes a large-diameter portion into which an upper punch is inserted, a small-diameter portion into which a lower punch is inserted, and a taper portion connecting the large-diameter portion and the small-diameter portion.
- One or both of the lower punches is characterized in that a notch is provided at the outer peripheral end of the end face facing the molding space of the molding die to increase the volume of the molding space.
- the invention according to claim 16 is the method for producing a sintered body according to claim 14 or 15, wherein the amount of graphite mixed with the metal powder is 0.3% by weight or more.
- the invention according to claim 17 relates to the metal powder of the metal powder molding material according to claim 1, wherein the metal powder is molybdenum (Mo), nickel (N i), manganese (i ⁇ in ), Copper (Cu), chromium (Cr), tungsten (W), vanadium (V), Kovar (Co) to improve strength, hardenability, and other mechanical properties by forming a solid solution with the base material, or to form precipitates such as carbides to improve strength, hardness, and other mechanical characteristics.
- Mo molybdenum
- Ni nickel
- manganese i ⁇ in
- Copper Copper
- Cr chromium
- W tungsten
- V vanadium
- Kovar Co
- Alloy steel powder containing iron as a main component that contains at least one alloying element that improves the sinterability is such that graphite remains at the grain boundaries of the metal powder, and carbides of iron and alloying elements It is characterized by a structure with almost no precipitates such as.
- the invention according to claim 18 relates to the metal powder of the metal powder molding material according to claim 1, wherein the metal powder is composed of: molybdenum (Mo), nickel (Ni), and manganese (Mn). , Copper (Cu), chromium (Cr), tungsten (W), vanadium (V), cobalt (Co), etc., form a solid solution to improve strength, hardenability, and other mechanical properties Alternatively, a powder mainly composed of an alloying element that improves the strength, hardness and other mechanical properties by generating precipitates such as carbides is diffused and adhered to a metal powder mainly composed of iron. It is characterized in that the structure after the preliminary sintering is a structure in which graphite remains at the grain boundaries of the metal powder and almost no precipitates such as carbides of iron and alloy elements are generated.
- the invention according to claim 19 relates to the metal powder of the metal powder molding material according to claim 1, wherein the metal powder is molybdenum (Mo), nickel (Ni), manganese (Mn). , Copper (Cu), chromium (Cr), tungsten (W), vanadium (V :), cobalt (Co), etc., form a solid solution in the base material to improve strength, hardenability, and other mechanical properties.
- a powder mainly composed of an alloying element that improves the strength, hardness, and other mechanical properties by generating precipitates such as carbides is mixed with a metal powder mainly composed of iron. It is characterized in that the structure after pre-sintering is a structure in which graphite remains at the grain boundaries of the metal powder and hardly produces precipitates such as iron and carbides of alloying elements.
- the amount of graphite mixed with the metal powder of the metal powder molding material according to any one of the seventeenth to nineteenth aspects is set to 0.1% by weight or more. It is characterized by:
- An invention according to claim 21 is a recompressed molded body having a densified structure having almost no voids, by recompressing the metallic powder molded material according to any one of claims 17 to 19. It is characterized by having.
- the invention according to claim 22 is characterized in that the amount of graphite mixed with the metal powder of the recompressed molded product according to claim 21 is set to 0.1% by weight or more.
- the invention according to claim 23 relates to a method for producing a recompressed molded body, obtained by compacting each of the metal powders according to claims 17 to 19, and having a density of 7.3 gZcm 3. A preforming step of obtaining the above preformed body,
- the preformed body obtained in this preforming step is calcined at a temperature of 700 to 1000 to obtain a metal powder compact having a structure in which graphite remains at grain boundaries of the metal powder.
- a preliminary sintering process
- It is characterized in that it comprises a recompression step of recompressing the metal powder molding material obtained in the preliminary sintering step.
- the invention according to claim 24 is characterized in that the recompressed molded body according to claim 21 or 22 is resintered at a predetermined temperature, and the structure in which graphite is diffused and the structure in which graphite remains are subjected to the resintering temperature. Characterized in that the sintered body has a predetermined ratio in accordance with
- the invention according to claim 25 relates to a method for producing a sintered body, obtained by compacting each of the metal powders according to claims 17 to 19, and having a density of 7.3 gZcm 3 or more.
- the preformed body obtained in this preforming step is calcined at a temperature of 700 to 1 000 ° C to form a metal powder compact having a structure in which graphite remains at the grain boundaries of the metal powder.
- a preliminary sintering process for obtaining a material is calcined at a temperature of 700 to 1 000 ° C to form a metal powder compact having a structure in which graphite remains at the grain boundaries of the metal powder.
- the invention according to claim 26 is characterized in that the sintered body according to claim 24 is heat-treated to obtain a sintered body having a hardened tissue.
- the invention according to claim 27 relates to a method for producing a sintered body, wherein each of the metal powders according to claims 17 to 19 is compacted to have a density of 7.3 g Z cm 3.
- the preformed body obtained in this preforming step is pre-sintered at 700 to 100000 to form a metal powder molding material having a structure in which graphite remains at the grain boundaries of the metal powder.
- a preliminary sintering step
- It is characterized by comprising a heat treatment step of heat-treating the sintered body obtained in the re-sintering step.
- the invention according to claim 28 is characterized in that the amount of graphite mixed with the metal powder is 0.1% by weight or more as a sintered body.
- the invention according to claim 29 includes a forming die having a forming space filled with the metal powder, an upper punch and a lower punch inserted into the forming die to process the metal powder, and A large-diameter portion into which the upper punch is inserted, a small-diameter portion into which the lower punch is inserted, and a taper portion connecting the large-diameter portion and the small-diameter portion are formed in the die forming space.
- a preform is formed by a device in which a notch for increasing the volume of the molding space is formed at one or both end faces of the punch and the lower punch facing the molding space, and the preform formed by this is formed.
- the invention according to claim 30 relates to a method for producing a recompression molded body, comprising: a molding die having a molding space filled with a metal powder; an upper punch inserted into the molding die to process the metal powder; A lower punch is provided, and a large-diameter portion into which the upper punch is inserted, a small-diameter portion into which the lower punch is inserted, and a tape connecting the large-diameter portion and the small-diameter portion are formed in the molding space of the molding die.
- a preformed body is formed by a device in which a notch for increasing the volume of the molding space is formed on one or both of the upper punch and the lower punch at an end face facing the molding space, and
- the preformed body formed by the above is pre-sintered at a temperature of 700 to 100000 to form a metal powder molding material according to any one of claims 17 to 19,
- This metal powder compact was recompressed to form a recompressed body. It is characterized by the following.
- the invention according to claim 31 is the recompression-molded product according to claim 29, wherein the amount of graphite mixed with the metal powder is set to 0.1% by weight or more. I do.
- the invention according to claim 32 includes a molding die having a molding space filled with the metal powder, an upper punch and a lower punch inserted into the molding die to process the metal powder, and A large-diameter portion into which the upper punch is inserted, a small-diameter portion into which the lower punch is inserted, and a taper portion connecting the large-diameter portion and the small-diameter portion are formed in the molding space of the die.
- a preform is formed by a device in which a notch for increasing the volume of the molding space is formed at one or both end faces of the punch and the lower punch facing the molding space, and the preform formed by this is formed.
- the invention according to claim 33 relates to a method for manufacturing a sintered body, comprising: a forming die having a forming space filled with a metal powder; an upper punch inserted into the forming die to process the metal powder; A large-diameter portion into which the upper punch is inserted; a small-diameter portion into which the lower punch is inserted; and a large-diameter portion into which the lower punch is inserted. And a taper portion extending over the small diameter portion, and a notch for increasing the volume of the molding space is formed on one or both of the upper punch and the lower punch at the end face facing the molding space. To form a preform, and the preform thus formed is
- the metal powder molding material according to any one of claims 1 to 19 is pre-sintered at a temperature of 700 to 100000 to form a metal powder molding material according to any one of claims 1 to 19, and the metal powder molding material is recompressed. And re-sintering the re-compressed body to form the re-compressed body.
- the invention according to claim 34 is the sintered body according to claim 32, characterized in that the amount of graphite mixed with the metal powder is 0.1% by weight or more. .
- the invention according to claim 35 is characterized in that the resintering temperature of the sintered body according to claims 7, 12 and 24 is set to 700 to 130.
- the recompressed molded article of the present invention is obtained by recompressing a metal powder molding material (hereinafter, simply referred to as a molding material). It is obtained by pre-sintering the preformed body obtained by powder molding at a temperature of 700 to 100000.
- a metal powder molding material hereinafter, simply referred to as a molding material.
- the density of the preform is 7.3 g Z cm 3 or more.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 g Z cm 3 or more is a structure in which graphite remains at the grain boundaries of the metal powder. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is deposited near graphite. . For this reason, the molding material has properties of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous and is in an isolated state.
- Growth A molding material having a large value can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside the furnace is also reduced. Although it diffuses to the surroundings and promotes carburization, the isolated voids are advantageously prevented, resulting in greater elongation. This means that the elongation of the molding material
- a recompressed compact of a metal powder compact having excellent deformability which is suitable for obtaining a mechanical component having high mechanical strength by a sintered metal, can be obtained.
- the metal powder is formed by mixing a metal powder containing iron as a main component with 0.3% by weight or more of graphite.
- a metal powder capable of producing high carbon steel can be obtained.
- the recompressed molded article of the present invention can increase the mechanical strength of the metallic powder molded material obtained by recompressing the metallic powder molded material.
- the mechanical strength is increased to the same degree as that of a forged material. be able to.
- the pre-formed body is obtained by a pre-forming step
- the forming material is obtained by temporarily sintering the pre-formed body in a pre-sintering step. Is obtained by recompressing a molding material in a recompressing step.
- the density of the preformed body formed in the preforming step is 7.3 g / cm 3 or more.
- the preformed The molding material obtained by sintering in the sintering step can have a large elongation and a low hardness.
- the structure of the forming material obtained by pre-sintering the pre-formed body having the density of 7.3 gZ cm 3 or more in the pre-sintering step has a structure in which graphite remains at grain boundaries of the metal powder. Is done. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is deposited near graphite.
- the molding material has properties of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state.
- a molding material having a large elongation after temporary sintering can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside Although the diffusion of carbon into the surroundings promotes carburization, the voids are isolated, and this is advantageously prevented, resulting in a large elongation.
- the temporary sintering in the temporary sintering step causes sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder over a wide range, thereby increasing the Is obtained.
- the pre-sintering temperature in the pre-sintering step is selected from 700 to 100 in the invention according to claim 4. Accordingly, the metal powder has a structure in which graphite remains at the grain boundaries, has an elongation of 10% or more, and has a hardness of HRB60 or less, and has excellent deformability. The material is obtained.
- the preforming step of the preformed body is performed by pressing a metal powder filled in a forming space of a forming die with an upper punch and a lower punch.
- the preform as a whole 7. 3 g Z cm 3 becomes more dense, but friction between the preform and the forming die increases, provided on one or both of the upper punch and the lower punch In the notched portion, the density of the preform becomes locally low and the friction decreases. Accordingly, the preform, I act coupled with the tapered portion formed in the molding space of the molding die roll is readily released from the forming die, density 7. 3 g / cm 3 or more preliminary A molded article is obtained.
- the recompression step is preferably performed in a normal temperature state. In this case, since the molding material has excellent deformability, it is easily recompressed.
- the recompressed compact has a structure in which the metal particles of the molding material are deformed significantly by the recompression molding and flattened.
- the structure of the molding material is such that graphite is present at the grain boundaries of the metal powder. Is left in the state, so that it has excellent machinability and lubricity.
- a method for producing a recompressed compact of a metal powder compact having excellent deformability which is suitable for obtaining a mechanical component having high mechanical strength by a sintered metal. can get.
- the metal powder compacted in the preforming step according to claims 4 and 5 is the invention according to claim 6, wherein graphite is mixed with the metal powder containing iron as a main component. It is formed.
- the amount of graphite added to the metal powder is 0.3% by weight or more.
- the sintered body is obtained by resintering the recompressed molded body at a predetermined temperature.
- This recompressed compact is obtained by recompressing a metal powder compact, and the metal powder compact is a pre-compacted compact obtained by compacting a metal powder. Obtained by temporary sintering at a temperature of 00 ° C.
- the density of the preform 7. 3 g Z cm 3 are as above, Yotsute thereto, child this pre ⁇ form presintered to increase the elongation of the molding material obtained, and the hardness lower Can be.
- the structure of the molding material obtained by temporarily sintering the preform having a density of 7.3 g Z cm 3 or more is a structure in which graphite remains at the grain boundaries of the metal powder. . This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is precipitated near graphite. For this reason, the molding material has properties of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous and is in an isolated state.
- a molding material with large elongation can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside the furnace is also reduced. Although it diffuses into the surroundings and promotes carburization, the isolated cavities can be advantageously prevented to provide significant elongation.
- the re-compression molding of the molding material obtained by temporarily sintering the preformed body is performed, preferably in a normal temperature state.
- the molding material since the molding material has excellent deformability, it can be easily recompressed, and a recompressed body having a small molding load and high dimensional accuracy can be obtained.
- a sintered body is obtained by resintering the recompressed molded body.
- graphite present at the grain boundaries of the metal powder diffuses into the ferrite ground (solid solution or carbide is formed).
- the structure is such that graphite is diffused and remains at a predetermined ratio in the ferrite or pearlite structure of the metal powder.
- the predetermined ratio includes the case where the residual amount of black bell is zero.
- the residual ratio of the graphite varies depending on the resintering temperature. The higher the resintering temperature, the lower the residual ratio of the graphite. Thereby, the mechanical properties such as predetermined strength can be selected for the sintered body.
- the metal powder is formed by mixing 0.3% by weight or more of graphite with metal powder containing iron as a main component.
- the mechanical strength of the sintered body obtained by recompressing and resintering the molding material is the same as that of the forged material. It can be raised to a degree.
- the preformed body is obtained by a preforming step
- the forming material is obtained by temporarily sintering the preformed body in a presintering step
- the recompression forming body is a forming element.
- the material is obtained by recompression molding in the recompression step
- the sintered body is obtained by resintering the recompression molded body.
- the density of the preformed body formed in the preforming step is 7.3 gZ cm 3 or more.
- the density of 7. 3 g / cm 3 or more preforms the preliminary sintering step in preliminary sintering and the molded material obtained we are the tissue is a tissue graphite grain boundary of the metal powder remaining You. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is deposited near graphite. For this reason, the molding material has a property of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state.
- a molding material having a large elongation after sintering can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside Although the diffusion of carbon into the surroundings promotes carburization, the voids are isolated, and this is advantageously prevented, resulting in a large elongation.
- the temporary sintering in the preliminary sintering step causes sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder, resulting in a large elongation. Is obtained.
- the sintering temperature in the sintering step is selected from 700 to 100 ° C.
- the recompression step is preferably performed in a normal temperature state. In this case, since the molding material has excellent deformability, it is easily recompressed.
- a sintered body is obtained by resintering the recompressed compact in the resintering step.
- the graphite present at the grain boundaries of the metal powder is diffused (solid solution or A structure in which graphite is diffused and remains in the ferrite or pearlite structure of the metal powder at a predetermined ratio in a state in which carbide is formed).
- the prescribed ratio includes the case where the residual amount of graphite is zero.
- the residual ratio of graphite in the sintered body changes depending on the resintering temperature, and the higher the resintering temperature, the lower the residual ratio of graphite. Thereby, the mechanical properties such as the predetermined strength can be selected for the sintered body.
- the preforming step of the preformed body is performed by pressing a metal powder filled in a forming space of a forming die with an upper punch and a lower punch.
- the preformed body has a high density of 7.3 g Z cm 3 or more as a whole, and friction between the preformed body and the forming die is increased, but one of the upper punch and the lower punch is used.
- the density of the preform becomes locally low and the friction decreases. For this reason, the preformed body is easily separated from the forming die together with the function of the tapered portion formed in the forming space of the forming die.
- a preform having a density of at least 7.3 gZcm 3 is obtained.
- the metal powder is formed by mixing 0.3% by weight or more of graphite with a metal powder containing iron as a main component.
- the mechanical strength of the sintered body obtained by recompressing and resintering the molding material is substantially the same as that of forged material It can be raised to a higher level.
- the sintered body is obtained by subjecting a sintered body obtained by resintering the recompressed molded body at a predetermined temperature to a heat treatment.
- the recompression molding is obtained by recompressing a metal powder molding material, and the metal powder molding material is obtained by firing a preform obtained by compacting a metal powder at a predetermined temperature. It is obtained by tying.
- the density of the preform is 7.3 g / cm 3 or more.
- the density of the preform is 7.3 gZcm 3 or more.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 gZ cm 3 or more is a structure in which graphite remains at the grain boundaries of the metal powder. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which graphite is deposited in the vicinity of graphite. For this reason, the molding material has properties of large elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state.
- a molding material with large elongation can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside the furnace is also reduced. Although it diffuses to the surroundings and promotes carburization, the isolated cavities are advantageously prevented, Large elongation will be obtained. This means that the elongation of the molding material
- the recompression molding of the molding material obtained by temporarily sintering the preformed body is preferably performed at room temperature. In this case, since the molding material has excellent deformability, it can be easily recompressed.
- a sintered body is obtained by resintering the recompressed molded body.
- graphite present at the grain boundaries of the metal powder diffuses into the ferrite ground (solid solution or carbide is formed).
- the predetermined ratio includes the case where the residual amount of graphite is zero.
- the residual ratio of graphite in the sintered body changes depending on the resintering temperature, and the higher the resintering temperature, the lower the residual ratio of graphite. Thereby, the mechanical properties such as the predetermined strength can be selected for the sintered body.
- a heat treatment is applied to a sintered body obtained by resintering the recompressed molded body at a predetermined temperature.
- the heat treatment is performed by various treatments such as induction hardening, carburizing and quenching, and nitriding, and a combination thereof.
- the sintered body obtained by resintering the recompressed body at a predetermined temperature has a high density with no voids due to the recompression molding, so that the diffusion of carbon due to the heat treatment decreases as going from the surface to the inside. . For this reason, the sintered body subjected to the heat treatment has increased hardness near the surface and has toughness inside, and has excellent mechanical properties as a whole.
- the re-compressed compact of the metal powder molding material having excellent deformability which is suitable for obtaining a mechanical part having high mechanical strength by a sintered metal, is re-fired.
- the sintered body obtained by subjecting the sintered body to heat treatment is obtained.
- the metal powder is formed by mixing 0.3% by weight or more of graphite with a metal powder containing iron as a main component.
- the mechanical strength of the sintered body obtained by recompressing and resintering the molding material is the same as that of the forged material. It can be raised to a degree.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 g Z cm 3 or more in the sintering step is a structure in which graphite remains at the grain boundaries of the metal powder. You. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is precipitated near graphite. For this reason, the molding material has properties of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state.
- a molded material having a large elongation after preliminary sintering can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside Although the diffusion of carbon into the surroundings promotes carburization, the voids are isolated, and this is advantageously prevented, resulting in a large elongation.
- the molding material The elongation is hardly affected by the amount of graphite because the density is 7.3 g Z cm 3 or more, so that carbon diffusion hardly occurs when the preform is pre-sintered. In addition, it shows that almost no diffusion of carbon occurs, so that the hardness of the molding material obtained by sintering can be kept low.
- the sintering in the sintering step sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder occurs over a wide range, so that a large elongation can be obtained.
- the temporary sintering temperature in the temporary sintering step is selected from 700 to 100 ° C., thereby having a structure in which graphite remains at the grain boundaries of the metal powder.
- a molding material having an excellent deformability with an elongation of 10% or more and a hardness of HRB 60 or less can be obtained.
- the recompression step is preferably performed in a normal temperature state. In this case, since the molding material has excellent deformability, it is easily recompressed.
- a sintered body is obtained by resintering the recompressed molded body in the resintering step.
- black solids present at the grain boundaries of the metal powder diffuse into the ferrite ground (solid solution )
- a metal powder is formed into a structure in which graphite is diffused and remains in a ferrite or pearlite structure at a predetermined ratio.
- the predetermined ratio includes the case where the residual amount of graphite is zero.
- the residual ratio of graphite in the sintered body changes depending on the resintering temperature, and the higher the resintering temperature, the lower the residual ratio of graphite. Thereby, the mechanical properties such as the predetermined strength can be selected for the sintered body.
- a heat treatment is applied to a sintered body obtained by resintering the recompressed molded body at a predetermined temperature.
- the heat treatment is performed by various treatments such as induction quenching, carburizing and quenching, and a combination thereof.
- the sintered body obtained by resintering the recompressed body at a predetermined temperature has a high-density structure without voids due to the recompression molding. Diffusion decreases from the surface to the inside. For this reason, the sintered body subjected to the heat treatment has increased hardness near the surface and has toughness inside, and thus has excellent mechanical properties as a whole.
- the metal powder filled in the molding space of the molding die is pressed by the upper punch and the lower punch.
- the preformed body has a high density of 7.3 gZcm 3 or more as a whole, and the friction between the preformed body and the forming die is increased, but the cutting provided on one or both of the upper punch and the lower punch is performed.
- the density of the preform becomes locally low and the friction is reduced.
- the preformed body is easily released from the forming die together with the function of the tapered portion formed in the forming space of the forming die, and has a density of 7.3 g / cm 3 or more. Is obtained.
- the metal powder to be compacted in the preforming step according to claim 14 or 15 is the invention according to claim 16, wherein the metal powder contains at least 0.3% by weight of the metal powder containing iron as a main component. It is formed by mixing graphite. By setting the amount of graphite to be added to the metal powder to 0.3% by weight or more, the mechanical strength of the sintered body obtained by recompressing and resintering the molding material is substantially the same as that of a forged material. Can be increased.
- the density of the preform obtained by compacting is 7.3 gZcm 3 or more
- the molding material that obtained the preform was provisionally sintered
- the graphite remains reliably at the grain boundaries of the metal powder, resulting in low hardness, high elongation, high lubricity at the grain boundaries of the metal powder, and an overall increase in moldability. That is, in the preformed body formed at a high density of 7.3 gZcm 3 or more, the gaps between the particles of the metal powder are not continuous and are in an isolated state.
- Atmospheric gases are unlikely to enter the inside of the preform, and the gas generated from the graphite inside is unlikely to diffuse to the surroundings, which greatly contributes to the suppression of carbon diffusion (residual graphite).
- the structure of the obtained molding material is such that graphite remains at the grain boundaries of the gold powder, and almost no precipitates such as iron and carbides of alloy elements are generated. ing.
- the structure is such that ferrite, austenite, or pearlite or veneite is slightly precipitated near graphite.
- the microstructure is slightly precipitated from gauze or bainite. Therefore, the molding material before recompression molding is hardly affected by the diffusion of carbon, and as a result, the hardness is low, the elongation is large, and the residual graphite lubricates the grain boundaries of the metal powder. By doing so, moldability is further enhanced.
- the molding material can also obtain a large elongation from this point.
- the gap of the molding material is reduced in a state where graphite remains at the grain boundaries of the metal powder. It is crushed and has a dense structure with almost no voids.
- the molding material used here hardly diffuses carbon, it can be easily recompressed into a predetermined shape with a small molding load (deformation resistance).
- a molding material in which a large amount of carbon diffuses into the molding material conventional molding material
- re-compression is extremely difficult because of its high hardness, low elongation, and low slippage between metal particles.
- the diffusion of carbon Since there is almost no hardness, the hardness is low and the elongation is large, and the graphite remaining at the grain boundaries secures the slip between the metal particles. As a result, recompression molding can be easily performed. Since the recompression molding can be performed at room temperature, the dimensional accuracy of the recompression molding does not decrease due to the occurrence of scale or transformation, and the recompression molding after the application is extremely accurate. It will be.
- the alloy component added to the metal powder enhances the degree of work hardening in the recompression molding, so that the plastically processed body can obtain a higher hardness than when no alloying element is added. Since graphite lubricates the metal grain boundaries, recompression molding can be performed with low deformation resistance. In particular, in the case of the metal powder molding material according to claims 18 and 19, the diffusion of the alloy element appears near the surface of the metal powder, and it is difficult to proceed inside the metal powder, so that the work hardened due to lower deformation resistance. A plastically processed body can be obtained.
- this plastic workpiece can be applied to sliding parts requiring high strength and high precision.
- the metal powder compacted in the preforming step according to any one of claims 17 to 19 is a metal powder containing iron as a main component in an amount of 0.1. It is formed by mixing graphite by weight or more. By setting the amount of graphite added to the metal powder to 0.1% by weight or more, the mechanical strength of a sintered body obtained by recompressing and resintering the molding material can be increased.
- the metal powder used here is a mixture of alloy steel powder and 0.1% by weight or more of graphite, the preformed body is not sintered or the obtained metal powder molding material is further added later.
- resintering virtually no carbon is decarburized. Therefore, the mechanical strength of the member obtained by re-compression molding, re-sintering, or the like of the molding material can be sufficiently increased to the same degree as that of the forged material.
- the preformed body formed in the preforming step is 7.3 g / cm 3 or more, the preformed body is temporarily sintered in the presintering step. The elongation of the molding material obtained by this can be increased and the hardness can be lowered.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 g Z cm 3 or more in the sintering step is a structure in which graphite remains at the grain boundaries of the metal powder. It is said. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which perlite is precipitated in the vicinity of graphite.
- the molding material has properties of high elongation and low hardness, and has excellent deformability.
- the sintering in the sintering step sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder occurs over a wide range, so that a large elongation can be obtained.
- the metal powder has a structure in which graphite remains at grain boundaries of the metal powder, An extrudable metal material with excellent deformability with an elongation of 10% or more and a hardness of HRB 60 or less is obtained.
- the recompression-molded product is recompressed by cold forging or the like, and the voids of the molding material are crushed in a state where graphite remains at the grain boundaries of the metal powder, resulting in a dense structure with almost no voids.
- the graphite present at the grain boundaries of the metal powder is simultaneously formed on the ferrite ground by the re-sintering and simultaneously with the surface diffusion or sintering at the contact surface of the metal powder. Diffusion (forms solid solution or carbide).
- the metal powder has a structure in which one or more of non-diffused alloy components such as ferrite, perlite, austenite, and nickel (Ni) are mixed. If graphite remains, the metal powder is used. It becomes a structure in which graphite is scattered inside.
- the alloying elements that form a solid solution with the base material dissolve more uniformly into the base material, and the alloying elements that form precipitates such as carbides form the precipitates.
- the effect of the improvement of the characteristic is reflected in the macro organization.
- the strength of the sintered body is higher than that of the recompressed body, and a mechanical strength equal to or higher than that of a forged material that does not particularly require a hardened layer can be obtained.
- this sintered body was re-sintered after re-compression molding, it had a recrystallized structure with a crystal grain size of about 20 im or less, which not only increased strength but also increased elongation. And the impact value increase, and the fatigue strength also increases.
- the density of the pre-formed body formed in the pre-forming step is 7.3 g / cm 3 or more, so that the pre-formed body is calcined in the pre-sintering step.
- the elongation of the molding material obtained by sintering can be increased and the hardness can be reduced.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 g Z cm 3 or more in the sintering step is a structure in which graphite remains at the grain boundaries of the metal powder. You. this Indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which pearlite is deposited near graphite. For this reason, the molding material has a property of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state.
- a molded material having a large elongation after preliminary sintering can be obtained. That is, when the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside Although the diffusion of carbon into the surroundings promotes carburization, the voids are isolated, and this is advantageously prevented, resulting in a large elongation.
- the sintering in the sintering step causes sintering due to surface diffusion or melting on the contact surface between the particles of the metal powder over a wide range, so that a large elongation can be obtained.
- the sintering temperature in the sintering step is selected from 700 to 100 ° C.
- the recompression step is preferably performed in a normal temperature state. In this case, since the molding material has excellent deformability, it is easily recompressed.
- a molding load of the recompression molding is small and a recompression molded body having high dimensional accuracy can be obtained.
- a sintered body is obtained by resintering the recompressed compact in the resintering step.
- the graphite present at the grain boundaries of the metal powder diffuses into the ferrite ground (solid solution or solid solution).
- the prescribed ratio includes the case where the residual amount of graphite is zero.
- the residual ratio of graphite in the sintered body changes depending on the resintering temperature, and the higher the resintering temperature, the lower the residual ratio of graphite. Thereby, the mechanical properties such as the predetermined strength can be selected for the sintered body.
- a re-compression molded body of a metal powder molding material having excellent deformability suitable for obtaining a mechanical part having high mechanical strength by a sintered metal is re-formed.
- a method for manufacturing a sintered body obtained by sintering is obtained.
- the sintered body that has been heat-treated by quenching or the like hardens by dissolving graphite in a supersaturated manner, or by depositing fine carbides, or by depositing nitrides. Form a layer. For this reason, in this sintered body, the diffusion of carbon due to the heat treatment becomes smaller toward the inside, and the hardness is increased by heat treatment only in the vicinity of the surface while maintaining the toughness inside.
- the density of the preformed body formed in the preforming step is set to 7.3 g Z cm 3 or more, so that the preformed body is temporarily set in the preliminary sintering step.
- the molding material obtained by sintering can have large elongation and low hardness.
- the structure of the forming material obtained by temporarily sintering the preformed body having the density of 7.3 g Z cm 3 or more in the sintering step is a structure in which graphite remains at the grain boundaries of the metal powder. You. This indicates that carbon is hardly diffused into the crystal of the metal powder, and at least graphite is not completely diffused into the crystal grains to form a solid solution or form a carbide.
- the structure of the metal powder has a ferrite structure as a whole or a structure in which powder is deposited near graphite.
- the molding material has a property of high elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder is not continuous, and is in an isolated state. A molded material having a large elongation after preliminary sintering can be obtained.
- the voids between the particles of the metal powder are continuous, in addition to the atmosphere gas in the furnace penetrating into the preform during the preliminary sintering, the gas generated from the graphite inside Although the diffusion of carbon into the surroundings promotes carburization, the voids are isolated, and this is advantageously prevented, resulting in a large elongation.
- the elongation of the molding material is set to a density of 7.3 g Z cm 3 or more, so that carbon diffusion hardly occurs when the preformed body is temporarily sintered.
- the graph shows that it is hardly affected by the amount of ⁇ , and that almost no diffusion of carbon occurs, so that the hardness of the molding material obtained by pre-sintering can be kept low.
- the sintering in the sintering step sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder occurs over a wide range, so that a large elongation can be obtained.
- the temporary sintering temperature in the temporary sintering step is selected from 700 to 100 ° C., thereby having a structure in which graphite remains at the grain boundaries of the metal powder.
- a molding material having an excellent deformability with an elongation of 10% or more and a hardness of HRB 60 or less can be obtained.
- the recompression step is preferably performed in a normal temperature state. In this case, since the molding material has excellent deformability, it is easily recompressed.
- a sintered body is obtained by resintering the recompressed compact in the resintering step.
- graphite present at the grain boundaries of the metal powder diffuses into the ferrite ground (solid solution or solid solution).
- the carbon powder is formed), and the metal powder has a structure in which graphite is diffused and remains at a predetermined ratio in the ferrite or pearlite structure.
- the predetermined ratio includes the case where the residual amount of graphite is zero.
- the residual ratio of graphite in the sintered body changes depending on the resintering temperature, and the higher the resintering temperature, the lower the residual ratio of graphite. Thereby, the mechanical properties such as the predetermined strength can be selected for the sintered body.
- a heat treatment is applied to a sintered body obtained by resintering the recompressed molded body at a predetermined temperature.
- the heat treatment is performed by various treatments such as induction hardening, carburizing and quenching, and nitriding, and a combination thereof.
- the sintered body obtained by resintering the recompressed body at a predetermined temperature has a high-density structure without voids due to the recompression molding. Less. For this reason, the sintered body subjected to the heat treatment has increased hardness near the surface and has toughness inside, and thus has excellent mechanical properties as a whole.
- the metal powder molding material can be obtained by recompression molding and resintering.
- the mechanical strength of the resulting sintered body can be increased to the same extent as forged material.
- preform for molding material since the overall 7. It is necessary to 3 g Z cm 3 or more dense, the release of the preform Sometimes it is considered that the friction for removal increases, but the equipment used here is a notch provided in one or both of the upper and lower punches to locally reduce the density of the preformed body. It is possible to reduce the friction of the mold release by lowering the density.
- the pre-formed body is easily released from the forming die together with the function of the tapered portion formed in the forming space of the forming die, and the pre-formed body has a density of 7.3 g / cm 3 or more .
- a molded article is easily obtained.
- the metal powder molding material obtained by temporarily sintering the pre-formed body has a high density of the pre-formed body. And the subsequent recompression molding can be easily performed. Therefore, the recompressed molded article has a dense structure with almost no voids, and is easy to recompress at room temperature. Molded with high precision.
- the present invention relates to a method for producing a recompressed molded article according to claim 29, wherein the recompression molding having a unique action and effect described in claim 29 by such a production method.
- a molded body is easily obtained.
- the amount of graphite added to the metal powder is set to 0.1% by weight or more, whereby metal The mechanical strength of the sintered body obtained by re-compressing and re-sintering the powder molding material can be increased to the same extent as (1) forged material.
- the device used here is a notch provided in one or both of the upper and lower punches, and locally reduces the density of the preform. Density can be reduced to reduce the friction of mold release. For this reason, the pre-formed body is easily released from the forming die together with the function of the tapered portion formed in the forming space of the forming die, and the pre-formed body having a density of 7.3 g / cm 3 or more is formed. A molded article is easily obtained.
- the metal powder molding material obtained by temporarily sintering the preformed body contains a sufficient amount of graphite remaining at the grain boundaries of the metal powder. And the subsequent re-compression molding is facilitated. Accordingly, the recompressed molded article obtained by the recompression molding has a dense structure with almost no voids, and is easily formed at a normal temperature because of being easily recompressed.
- a sintered body is obtained by re-sintering the recompressed molded body.
- graphite present at the grain boundaries of the metal powder diffuses into the ferrite ground (solid solution or carbide is formed).
- the structure in which graphite is diffused and remains in the ferrite or pearlite structure of the metal powder at a predetermined ratio is set.
- the case includes the case where the residual amount of graphite is zero.
- the residual ratio of the graphite varies depending on the resintering temperature.
- the mechanical properties such as predetermined strength can be selected for the sintered body. Therefore, a sintered body obtained by re-sintering a re-compressed compact of a metal powder compact having excellent deformability, which is suitable for obtaining a mechanical component having high mechanical strength by a sintered metal, is obtained. .
- the present invention relates to a method for producing the sintered body described in claim 32, wherein the production method has a unique function and effect described in claim 32.
- a compression molded body can be easily obtained.
- the metal powder molding material can be obtained by recompression molding and resintering.
- the mechanical strength of the resulting sintered body can be increased to the same extent as (1) forged material.
- the resintering temperature in the resintering step according to each of claims 7, 12, and 24 is selected from 700 to 130 ° C. .
- a sintered body is obtained in which the diffusion of graphite is small and the residual ratio of graphite is large in the low temperature range of the resintering temperature.
- a sintered body having a minimum strength and a small strength of crystal regrowth is obtained.
- FIG. 1 is an explanatory view of a recompression molding of a metal powder molding material and a manufacturing process of a sintered body obtained from the recompression molding in the embodiment of the present invention.
- Figure 2 shows the manufacturing process of the preformed body, in which the metal powder is filled in the molding space of the molding die (a), the metal powder is pressed by the upper and lower punches (b), It is an explanatory view showing a state in which the forming die is started to be lowered to take out the preform after completion (c), and a state in which the preform is taken out (cl).
- FIG. 3 shows a preform formed from a metal powder mixed with 0.5% by weight of graphite.
- FIG. 4 is a drawing showing the relationship between the density and the elongation of the molding material obtained by temporarily sintering at 0, using data (a :) and graph (b).
- Figure 4 is a drawing showing the structure of the molding material.
- Fig. 5 shows the change in elongation of the molding material with a density of 7.3 gZcm 3 when the amount of graphite and the sintering temperature were changed, as shown in data (a) and graph (b).
- Fig. 3 is a drawing showing data (a) and graph (b) showing changes in elongation when the amount of graphite and the sintering temperature were changed for a molding material having a density of 7.5 gZcm 3 .
- Fig. 7 shows the change in hardness when the amount of graphite and the sintering temperature are changed for a molding material with a density of 7.3 gZcm 3 , using graphs (a;) and graph (b). It is a drawing.
- Fig. 8 shows the change in hardness when the amount of graphite and the sintering temperature are changed for a molding material with a density of 7.5 gZcm 3 , as shown in (a) and (b). It is.
- Figure 9 is a particle size formed from a 20 graphite 0.5 wt% mixed metallic powders, for molding materials having a density of 7. S gZcm 3 and 7. 5 gZc m 3, the provisional sintering temperature and the yield stress Is a drawing showing data (a) and a graph (b).
- Fig. 10 shows the sintering temperature and yield of 7.3 gZcm 3 and 7.5 gZcm 3 of a molding material formed from a metal powder mixed with 0.5% by weight of graphite having a particle size of 5 im. It is a drawing showing the relationship with stress by data (a) and graph (b).
- Fig. 11 is a drawing showing the structure of the recompression-molded body when the recompression molding is mild (a) and further when the recompression molding is performed (b).
- Fig. 12 is a drawing showing the structure of the sintered body
- Fig. 13 is a drawing showing the change in the graphite residual ratio when the resintering temperature is changed, using data (a) and graph (b). .
- FIG. 14 is a drawing showing the change in tensile strength when the resintering temperature was changed, using data (a) and graph (b).
- FIG. 15 is a drawing showing the change in hardness when the resintering temperature is changed by data (a;) and graph (b).
- Figure 16 shows the relationship between the refastening temperature and the tensile strength when the sintered body obtained by changing the resintering temperature was heat-treated under the specified conditions by data (a),. And graph (b). It is a drawing.
- FIG. 17 is a drawing showing data (a) and a graph (b) showing the relationship between the distance from the surface of the heat-treated body subjected to heat treatment under predetermined conditions and hardness.
- FIG. 18 is a drawing showing a structure of a forming material formed by temporarily sintering a preform corresponding to Example 1 or 2 in the embodiment of the present invention.
- FIG. 19 is a drawing showing, with data and a graph, changes in elongation when the sintering temperature and the amount of graphite were changed for the molding material corresponding to Example 1.
- FIG. 20 is a drawing showing, with data and a graph, changes in elongation when the sintering temperature and the amount of graphite were changed for the molding material corresponding to Example 2.
- FIG. 21 is a drawing showing, with data and a graph, a change in hardness of the forming material corresponding to Example 1 when the sintering temperature and the amount of graphite were changed.
- FIG. 22 is a drawing showing, with data and a graph, a change in hardness of the forming material corresponding to Example 2 when the sintering temperature and the amount of graphite were changed.
- FIG. 23 is a drawing showing the forming load (deformation resistance) per unit time as data and a graph when the forming material corresponding to Example 1 was recompressed (cold forged).
- FIG. 24 is a drawing showing the forming load (deformation resistance) per unit time by data and a graph when the forming material corresponding to Example 2 was recompressed (cold forged).
- FIG. 25 is a drawing showing, with data and a graph, a change in tensile strength when the sintering temperature and the amount of graphite were changed for the plastically processed body corresponding to Example 1.
- FIG. 26 is a drawing showing, in a graph and a graph, changes in tensile strength when the sintering temperature and the amount of graphite were changed for the plastically processed body corresponding to Example 2.
- Figure 27 shows changes in the anti-sintering temperature and the amount of graphite for the plastic workpiece corresponding to Example 1. It is a drawing which shows the change of the hardness at the time of making it by data and a graph.
- FIG. 28 is a drawing showing, with data and a graph, a change in hardness when the sintering temperature and the amount of graphite are changed for the plastically processed body corresponding to Example 2.
- FIG. 29 is a drawing showing the structure of a composition processed body obtained by recompressing (cold forging) the molding material corresponding to Example 1 or 2 with a relatively small cross-sectional reduction rate (deformation amount).
- FIG. 30 is a drawing showing the structure of a composition processed body obtained by recompressing (cold forging) the molding material corresponding to Example 1 or 2 with a relatively large cross-sectional reduction rate.
- FIG. 31 is a drawing showing the structure of a re-sintered product corresponding to Example 1 or 2.
- FIG. 32 is a diagram showing, with data and a graph, a change in the residual graphite ratio when the resintering temperature and the resintering time were changed for the resintered body corresponding to Example 1.
- FIG. 33 is a drawing showing, with data and a graph, changes in tensile strength when the resintering temperature was changed for the resintered body corresponding to Example 1.
- FIG. 34 is a drawing showing, with data and a graph, a change in tensile strength when the resintering temperature was changed for the resintered body corresponding to Example 2.
- FIG. 35 is a drawing showing, with data and a graph, a change in hardness of the resintered body corresponding to Example 1 when the resintering temperature was changed.
- FIG. 36 is a drawing showing, with data and a graph, a change in hardness when the resintering temperature was changed for the resintered body corresponding to Example 2.
- FIG. 37 is a drawing showing, with data and a graph, changes in tensile strength when the resintering temperature was changed for the heat-treated body corresponding to Example 1.
- FIG. 38 is a drawing showing, with data and a graph, a change in tensile strength when the resintering temperature was changed for the heat-treated body corresponding to Example 2.
- FIG. 3 9 is an internal hardness distribution of the heat treatment processed body corresponding to Example 2, the same metallic powder density 7. 0 g Z cm 3 in the same conditions as in Example 2 subsequent to temporary compression molding
- Fig. 3 is a drawing showing the internal hardness distribution of a heat-treated processed body (conventional method) obtained by performing the processing, and data and graphs.
- 1 is a preforming step
- 2 is a sintering step
- 3 is a recompression step
- 4 is a resintering step
- 5 is a heat treatment step.
- the metal powder 7 is compacted to obtain a pre-formed body 8, and in the pre-sintering step 2, the pre-formed body 8 is pre-sintered to obtain a forming material 9.
- the molding material 9 is recompressed and molded to obtain a recompressed body 10.
- the resintering step 4 the recompressed molded body 10 is resintered to obtain a sintered body 11, and in the heat treatment step 5, the sintered body 11 is subjected to a heat treatment.
- the preforming step 1 is a step of obtaining a preformed body 8 by compacting the metal powder 7, and in this embodiment, as shown in FIGS. 2 (a) to 2 (d),
- the powder 7 is filled into the molding space 15 of the molding die 14 and is pressed by the upper punch 16 and the lower punch 17, whereby the preform 8 is obtained.
- the metal powder 7 and the molding die 14 are in a normal temperature state.
- the metal powder 7 is formed by mixing 0.3% by weight or more of graphite 7b with a metal powder 7a containing iron as a main component.
- the recompressed compact 10 obtained by recompressing the molding material 9 and the recompressed compact 1 , 0 can be re-sintered to increase the mechanical strength of the sintered body 11 to about the same level as the forged material.
- the molding space 15 of the molding die 14 filled with the metal powder 7 includes a large-diameter portion 19 into which the upper punch 16 is inserted, and a small-diameter portion 20 into which the lower punch 17 is inserted. A tapered portion 21 connecting the large diameter portion 19 and the small diameter portion 20 is provided.
- the upper punch 16 and the lower punch 17 inserted into the molding space 15 of the molding die 14 and in this embodiment, the upper punch 16 has a molding space of the molding die 14. Increase the volume of molding space 15 at the outer peripheral end of end face 22 facing 15 Notches 23 to be formed are formed.
- the notch 23 is formed in an annular shape with a hook-shaped cross section.
- Reference numeral 24 denotes a core inserted into the molding space 15 of the molding die 14, and the preformed body 8 formed in the molding space 15 is formed into an elliptical cylindrical shape by the core 24. Become.
- a metal powder 7a obtained by mixing 0.3% by weight or more of graphite 7b with a metal powder 7a containing iron as a main component in a forming space 15 of a forming die 14 is used. (See Fig. 2 (a)).
- the upper punch 16 and the lower punch 17 are inserted into the molding space 15 of the molding die 14 to press the metal powder 7. Specifically, the upper punch 16 is inserted into the large diameter portion 19 of the molding space 15, and the lower punch 17 is inserted into the small diameter portion 20 of the molding space 15 and pressed. At this time, the upper punch 16 in which the notch 23 is formed is stopped in the large diameter portion 19 (see FIG. 2B).
- the upper punch 16 is retracted (elevated), and the forming die 14 is lowered (see FIG. 2 (c)).
- the preformed body 8 is removed from the forming space 15 (see FIG. 2 (d)).
- the taper portion 21 has a so-called draft angle, and the preform 8 formed by compacting is taken out. Can be easily performed.
- a notch 23 for increasing the volume of the molding space 15 is formed at the outer peripheral end of the end face 22 facing the molding space 15 of the molding die 14, The notch 23 locally reduces the density of the preform 8 locally. Therefore, the friction between the preform 8 and the forming die 14 and the springback of the preform 8 are suppressed to be low, and the preform 8 can be easily taken out.
- the preform 8 having the density of 7.3 gZcm 3 or more can be easily obtained.
- the forming material 9 obtained by temporarily sintering the preformed body 8 in the preliminary sintering step 2 (described later in detail) ) Can be increased. That is, as shown in FIG. 3, the elongation of the molding material 9 can be made 10% or more by setting the density of the preformed body 8 to 7.3 g / cm 3 or more.
- the pre-formed body 8 obtained in the forming step 1 is pre-sintered in the pre-sintering step 2.
- a molding material 9 having a structure in which graphite 7b remains at the grain boundaries of the metal powder 7a is obtained.
- the entire structure of the metal powder 7a is a ferrite (F) structure, and a part of the graphite 7b remains.
- the structure of the metal powder 7a exhibits a structure in which pearlite (P) is deposited near the graphite 7b on the ferrite ground.
- the graphite 7b does not have a structure in which all of the graphite 7b diffuses into the crystal grains to form a solid solution or forms a carbide.
- the molding material 9 has a property of large elongation and low hardness, and has excellent deformability.
- the gap between the particles of the metal powder 7a is not continuous, and is in an isolated state. Later, a molding material 9 with large elongation is obtained. That is, when the voids between the particles of the metal powder 7a are continuous, in addition to the fact that the atmospheric gas in the furnace penetrates deeply into the preform 8 through the voids during the preliminary sintering, However, the gas generated from the graphite inside diffuses into the surroundings to promote carburization, but since the voids are isolated, this can be advantageously prevented to obtain large elongation.
- sintering due to surface diffusion or melting at the contact surface between the particles of the metal powder 7a occurs over a wide range, so that a large elongation, preferably an elongation of 10% or more, is obtained. Is obtained.
- a temperature of 800 to 100 is preferably selected.
- the molding material 9 obtained through the pre-sintering step 2 is recompressed and recompressed.
- excellent deformability is imparted to the molding material 9 in order to reduce the deformation resistance in the recompression molding and facilitate the molding process.
- a forming material 9 having an elongation of 10% or more can be obtained.
- a molding material 9 having a hardness of HRB 60 or less can be obtained.
- the hardness of the molding material 9 is less than HRB 60 or less than the hardness obtained by annealing low carbon steel having a carbon content of about 0.2%.
- the yield stress of the molding material 9 is 800 to 100 000 in the preliminary sintering temperature. In the range of C, it becomes 202 to 272 MPa, which is smaller than the yield stress of low carbon steel having a carbon content of about 0.2%.
- the molding material 9 obtained in the preliminary sintering step 2 is recompressed in a recompression step 3 to obtain a recompression molded body 10.
- the recompression molding of the molding material 9 is preferably performed in a normal temperature state. In this case, since the molding material 9 has excellent deformability, it is easily recompressed, and no scale is generated.
- the recompressed body 10 has a structure in which graphite 7b remains at the grain boundaries of the metal powder 7a, and as shown in FIG. 11, depending on the degree of recompression molding, The 7a particles have a flattened shape.
- mild recompression molding has a structure in which the particles with a metal content of 7a are slightly flattened and many voids between the particles have been eliminated (see Fig. 11 (a)).
- the particles of the metal powder 7a are greatly flattened and have a structure in which voids between the particles are almost eliminated (see Fig. 11 (b)).
- the recompressed compact 10 has a structure in which the particles of the molding material 9 g metal powder 7 a are greatly deformed and flattened, and the structure of the molding material 9 is the grain of the metal powder 7 a. Since graphite 7b remains in the boundary, it has excellent machinability and lubricity.
- the pre-sintering temperature in the pre-sintering step 2 is set to 800 to 100 ° C.
- a structure in which graphite 7 b remains at the grain boundary of the metal powder 7 a is obtained.
- the elongation is 10% or more and the hardness becomes HRB 60 or less, a molding material 9 having more excellent deformability can be obtained.
- the sintered body 11 has a structure in which graphite 7 b present at the grain boundaries of the metal powder 7 a is diffused (formed into solid solution or carbide) in the ferrite ground,
- the structure is such that graphite 7b is diffused and remains at a predetermined ratio in the ferrite or pearlite structure of the metal powder 7a.
- the residual amount of graphite 7b may be zero.
- the residual ratio of graphite 7b in the sintered body 11 changes depending on the resintering temperature, and the higher the resintering temperature, the smaller the residual ratio of graphite 7b (see FIG. 13). Thereby, the sintered body 11 can be selected from mechanical properties such as predetermined strength.
- the resintering temperature in the resintering step 4 is preferably selected from 700 to 130 ° C.
- a sintered body 11 in which the diffusion of graphite 7b is small and the residual ratio of graphite 7b is large is obtained, and in the high-temperature region of the resintering temperature. A large amount of graphite 7b is diffused, the residual rate is small, the regrowth of the crystal is small, and the sintered body 11 having the highest strength is obtained.
- the resintering temperature When the resintering temperature is relatively high, ie, 1000 to 130 ° C., the residual ratio of graphite 7b decreases, and graphite 7b diffuses into the ferrite ground (solidified). (Dissolve or form carbides), further increasing strength and hardness.
- the resintering temperature exceeds 110 ° C., the tendency for the total carbon content to decrease with an increase in the decarburization amount and the strength and hardness to decrease due to the regrowth of crystal grains begins to appear. If the temperature exceeds 130 ° C., a coarse structure is generated due to the excessive growth of crystal grains, so that both the strength and the hardness are greatly reduced.
- the re-bonding temperature be in the range of 700 to 130 ° C., and to obtain a stable tissue, the range is 900 to 1,200 ° C. Is the most preferred thing to do.
- the recompressed molded product 10 of the metal powder molding material 9 having excellent deformability which is suitable for obtaining a mechanical part having high mechanical strength by a sintered metal, is re-sintered.
- a sintered body 11 and a method for producing the same are obtained.
- the resintering temperature in the resintering step is set to 700 to 130 or :, by selecting this resintering temperature, the diffusion of graphite 7b is small and the graphite 7b remains.
- a sintered body 11 having a high abundance and a sintered body 11 having a maximum strength are obtained by diffusing a large amount of graphite 7b and having a low residual rate, a small regrowth of crystals.
- the sintered body 11 is subjected to a heat treatment.
- the heat treatment in the heat treatment step 5 is performed by various treatments such as induction hardening, carburizing and quenching, and nitriding, and a combination thereof.
- the heat-treated sintered body 11 has a solid solution of graphite 7b in supersaturation, or a fine carbide or nitride precipitates to form a hardened layer, thereby imparting excellent mechanical properties.
- the heat-treated sintered body 11 has a higher tensile strength than the re-sintered sintered body 11 due to the formation of a hardened layer.
- the sintered body 11 obtained by resintering the recompressed molded body 10 at a predetermined temperature has a high-density structure without voids due to the recompression molding in the recompression step 3. Diffusion decreases from the surface to the inside. For this reason, as shown in FIG. 17, the sintered body 11 subjected to the heat treatment has increased hardness near the surface and has toughness inside, and has excellent mechanical properties as a whole. become.
- heat treatment is applied to a sintered body obtained by re-sintering a recompressed compact of a gold white powder molding material having excellent deformability, which is suitable for obtaining mechanical parts with high mechanical strength made of sintered metal.
- the resulting sintered body and the method for producing the same are obtained.
- the manufacturing steps of the metal powder molding material, the recompression molded body, and the sintered body of the embodiment in each invention are the same as those shown in FIG. 1, and the manufacturing steps of the preformed body are also shown in FIG.
- a metal powder 7 to be described later is formed into a forming die 14 as shown in FIGS.
- Filling into molding space 15 of upper punch 16 and lower punch Pressing at 17 gives a preform 8 with a density of 7.3 g Z cm 3 or more.
- the metal powder 7 and the molding die 14 are in a normal temperature state.
- the molding space 15 of the molding die 14 has a large diameter portion 19 into which the upper punch 16 is inserted, a small diameter portion 20 into which the lower punch 17 is inserted, and a large diameter portion 19 and a small diameter portion 2. And a taper portion 21 connecting the first and second portions.
- the upper punch 16 has a molding space 15 of the molding die 14.
- a notch 23 for increasing the volume of the molding space 15 is formed at the outer peripheral end of the end face 22 facing the side.
- the notch 23 is formed in a ring shape with a cross section in a cross section.
- Reference numeral 24 denotes a core inserted into the molding space 15 of the molding die 14, and the preformed body 8 molded in the molding space 15 is formed into a substantially cylindrical shape by the core 24. Become.
- the metal powder 7 is filled in the forming space 15 of the forming die 14.
- the metal powder 7 to be filled here a mixture of the following metal powder and 0.1% by weight or more of graphite is used.
- the metal powders used here are molybdenum (Mo), nickel (Ni), manganese (Mn), copper (Cu), chromium (Cr), tungsten (W), and vanadium (V). Containing one or more alloying elements such as cobalt (Co) or the like, with the balance being iron and a small amount of unavoidable impurities (metal powder corresponding to claim 17), or the alloy
- the powder (metal powder corresponding to claim 18) or the mixture (metal powder corresponding to claim 19) obtained by diffusing and adhering the powder containing the element as the main component to the metal powder containing iron as the main component is used. Used.
- the upper punch 16 and the lower punch 17 are inserted into the molding space 15 of the molding die 14 to press the metal powder 7. Specifically, the upper punch 16 is inserted into the large diameter portion 19 of the molding space 15, and the lower punch 17 is inserted into the small diameter portion 20 of the molding space 15. And pressurized. At this time, the upper punch 16 in which the notch 23 is formed is stopped in the large diameter portion 19 (see FIG. 2B).
- the upper punch 16 is retracted (elevated), and the forming die 14 is lowered (see FIG. 2. (c)).
- the preformed body 8 is removed from the forming space 15 (see FIG. 2 (d)).
- the tapered portion 21 has a so-called draft angle, and the pre-molded body 8 that has been compacted is taken out. Can be easily performed.
- the upper punch 16 has a notch 23 for increasing the volume of the molding space 15 at the outer peripheral end of the end face 22 facing the molding space 15 of the molding die 14, The notch 23 locally reduces the density of the preform 8 locally, and reduces the friction between the preform 8 and the forming die 14 and the springback of the preform 8. As a result, the preform 8 can be easily taken out.
- the preform 8 having the density of 7.3 g Z cm 3 or more can be easily obtained.
- the preformed body 8 obtained in the preforming step 1 is pre-sintered in the pre-sintering step 2.
- a molding material having a structure in which graphite 3b remains at the grain boundaries of the metal powder 3a and hardly produces precipitates such as carbides of iron and alloying elements is obtained.
- the structure of the metal powder 3a is composed entirely of ferrite (F) or austenite (A). If part of the graphite 3b is diffused, the structure of the metal powder 3a is a structure in which pearlite (P) or bainite (B) is slightly precipitated near the graphite 3b.
- the metal powder 3a corresponding to claim 18 or 19 when the metal powder 3a corresponding to claim 18 or 19 is used, when all of the graphite 3b remains at the grain boundaries of the metal powder 3a, the whole is ferrite (F), and Becomes a structure of austenite (A) or a structure having an undiffused alloy component such as nickel (Ni). When part of the graphite 3b is diffused, a pearlite (a) is formed near the graphite 3b. A structure in which P) or bainite (B) is slightly precipitated. That is, at least the entire metal powder 3a does not have a perlite (P) or bainite (B) structure. For this reason, the molding material has properties of low hardness and high elongation, and has excellent deformability.
- the density of the preform 8 is 7.3 g Z cm 3 or more, the gap between the particles of the metal powder 3a is not continuous, and the preform 8 is in an isolated state.
- a molding material having low hardness and high elongation after preliminary sintering can be obtained. That is, when the voids between the particles of the metal powder 3a are continuous, the atmosphere gas in the furnace during pre-sintering and the gas generated from graphite penetrate deeply into the preform 8 through the voids. Although the carburization is promoted, since the voids are isolated, these are advantageously prevented, the hardness is kept low, and a large elongation is obtained. Therefore, the hardness and elongation of the molding material are hardly affected by the amount of graphite 3b.
- provisional sintering step 2 provides a greater elongation because sintering occurs over a wide range on the contact surface between the particles of the metal powder 3a due to melting or melting.
- the sintering temperature in the preliminary sintering step 2 is lower than 700 ° C, the bonding of the metal powder by sintering does not proceed, and if it exceeds 100, graphite 3b is excessively diffused. Since the hardness becomes too high, the range of 700 to 100 ° C. is selected.
- a temperature of 800 to 100 ° C. is usually selected, but carbides such as chromium (Cr) are contained. When alloy elements that are easily formed are included, if the temperature exceeds 800 ° C, precipitates such as carbides of the alloy elements are formed and the hardness increases, so the temperature range of 700 to 800 ° C is limited. Selected.
- FIG. 19 is test data and a graph obtained by examining the relationship between the pre-sintering temperature and the elongation of the molding material in Example 1 described later.
- FIG. 20 is the graph in Example 2 described later. It is the test data and graph similar to FIG.
- FIG. 21 shows test data and a graph obtained by examining the relationship between the sintering temperature and the hardness of the molding material in the case of Example 1.
- FIG. 22 shows the relationship between FIG. 21 and FIG. 21 in the case of Example 2. Similar data and graphs.
- the sintering temperature is selected in the range of 700 to 100000, at least the elongation of the forming material is at least 5% and the hardness is around HRB60. Can be maintained.
- the value of HRB 60 is almost the same as the hardness when annealed to a high-strength cold-forged steel material, but this molding material according to the present invention does not require annealing. Values around HR b 60 can be obtained.
- the molding material obtained in the preliminary sintering step 2 is subjected to recompression molding (cold forging, etc.) in the next recompression step 3.
- the plastically worked body obtained here has a structure with almost no voids, because the voids in the structure are crushed and densified with respect to the molding material in which graphite 3b remains at the grain boundaries of the metal powder 3a. .
- FIGS. 23 and 24 show the forming load ( (Deformation resistance) can be made very small.
- the molding material has little carbon diffusion, it has low hardness and high elongation characteristics, and furthermore, the graphite present at the metal powder grain boundary promotes the slip between the metal powders. Therefore, the forming load at the time of recompression molding is reduced, and the plastically formed body is easily formed into a predetermined shape.
- FIG. 23 shows the case of the first embodiment
- FIG. 24 shows the case of the second embodiment.
- the plastic worked body secures a sufficient tensile strength as shown in FIGS. 25 and 26. As shown in FIGS. 27 and 28, sufficient hardness can be ensured.
- FIGS. 25 and 27 are for the case of the first embodiment, and FIGS. 26 and 28 are for the case of the second embodiment. Therefore, the plastic worked body has a tensile strength and hardness comparable to that of the ⁇ material, and the mechanical strength is sufficiently high.
- Fig. 29 and Fig. 30 show the structures of the plastically formed body when it is formed by recompression molding with relatively small deformation and when it is formed by recompression molding with large deformation. is there.
- graphite 3b remains at the grain boundaries of the metal powder 3a
- the structure of the metal powder 3a may be ferrite (F), austenite ( A) or a structure in which pearlite (P) or bainite (B) is slightly precipitated in the vicinity of graphite 3b, and if it corresponds to claims 18 and 19, ferrite (F) ), Austenite (A), or a structure in which one or more of the undiffused alloy components such as nickel (N i) are mixed, or a pearlite (P) or a base in the vicinity of graphite 3b
- the structure in which inite (B) is slightly precipitated is shown in FIG. 29, there are almost no voids, and the metal powder 3a has a slightly deformed shape. As shown, the voids were
- the plastically processed body thus obtained can be applied to sliding parts requiring high strength and high precision.
- the plastically processed body is re-sintered in the next re-sintering step 4.
- the obtained re-sintered body diffuses the graphite 3b present at the grain boundaries of the metal powder 3a into the ferrite ground simultaneously with the surface diffusion of the metal powder on the contact surface or sintering by melting.
- the metal powder 3 a may be a ferrite (F), a pearlite (P), or a bayite as shown in FIG.
- the residual ratio of the added graphite 3b (the ratio of the amount of undiffused graphite to the total carbon) is re-established.
- the higher the sintering temperature the smaller the structure, and the structure in which the graphite 3b is diffused and the structure in which the graphite 3b remains are formed at a predetermined ratio according to the resintering temperature.
- the resintering temperature is high, the residual ratio of graphite becomes 0 as shown in the figure, and the structure in which the graphite 3b remains does not exist.
- alloying elements that form a solid solution with the base material during resintering are added more uniformly by forming a precipitate with the alloying elements that form a solid solution with the base material and form precipitates such as carbides.
- the effect of the improvement of the mechanical properties by the alloy element is reflected on the macroscopic structure, and the mechanical properties of the entire re-sintered body are improved.
- the strength becomes sufficiently higher than that of the plastic work body, and by changing the diffusion amount of graphite 3b, a re-sintered work body that meets the strength, lubricity, and other required mechanical properties can be obtained. Will be able to gain. And re-sintered at a certain temperature
- the re-sintered product has high tensile strength and high hardness, and does not particularly require a hardened layer. It can provide mechanical strength equal to or higher than that of a forged material.
- the re-sintered product has a crystal grain size of approximately
- a recrystallized structure of about 20 m or less is obtained, and the crystal grain size becomes finer than the conventional sintered body having a crystal grain size of 40 to 50 m. This results in higher strength, high elongation, high fatigue strength, high impact value, and excellent mechanical properties.
- the resintering temperature is desirably in the temperature range of 900 to 130 ° C.
- the resintered body is subjected to heat treatment such as induction hardening, carburizing, nitriding and other combinations.
- heat treatment such as induction hardening, carburizing, nitriding and other combinations.
- graphite 3b forms a solid solution in supersaturation, or fine carbides are precipitated, and a hardened layer is formed.
- Fig. 37 and Fig. 38 the formation of the hardened layer resulted in a higher tensile strength than that of the re-sintered product, and as can be seen from the relationship between the distance from the surface and the hardness shown in Fig.
- the diffusion of carbon due to the heat treatment is as small as the inside, so that only the vicinity of the surface becomes hard by the heat treatment while maintaining the toughness inside. Therefore, it has excellent mechanical properties as a whole.
- the diffusion of carbon progresses to the inside, and the entire body has a high hardness.
- it since it has voids, it is brittle and has low toughness and rigidity.
- the heat-treated body according to the present invention is higher than a general sintered article. In addition to high strength and high toughness, it has high rigidity. ⁇ As with forged materials, heat treatment can be performed according to the required mechanical properties. In addition, when an alloy element that improves the heat treatment properties such as quenchability by being dissolved in the base material is added, a material having more excellent mechanical properties can be obtained.
- the heat-treated body obtained in this manner is used for driving parts such as camshafts, lorry parts, etc., vehicle engine parts, propeller shaft joint parts, drive shaft parts, clutch parts, mission parts, etc., power steering gear parts, Inexpensive when applied to mechanical parts that require high strength, high toughness and slidability, such as steering parts such as anti-lock brake parts, suspension parts, other various bearings and pump components, etc. be able to.
- driving parts such as camshafts, lorry parts, etc., vehicle engine parts, propeller shaft joint parts, drive shaft parts, clutch parts, mission parts, etc.
- power steering gear parts Inexpensive when applied to mechanical parts that require high strength, high toughness and slidability, such as steering parts such as anti-lock brake parts, suspension parts, other various bearings and pump components, etc. be able to.
- the preform 8 may be formed by heating a metal powder 7 and a molding die to a predetermined temperature to form a metal powder. It may be formed by so-called warm forming performed in a state where the yield point of 7 is lowered.
- the notch 23 may be provided in the lower punch 17. Also, it may be provided on both the upper punch 16 and the lower punch 17.
- Molybdenum (Mo) contains 0.2% by weight of the component. The balance is iron (Fe) and a small amount of alloy steel powder, which is an inevitable impurity, mixed with 0.3% by weight of graphite to form metal powder. and. the metallic powder was compacted, density to form a preform of 7.4 gZ cm 3, the preform was 60 minutes provisionally sintered at 800 ⁇ in a furnace of a nitrogen gas atmosphere Made a molding material. The elongation of this molded material was 11.2% and the hardness was HRB 53.3 (see Figs. 19 and 21).
- the molding material was re-compressed into a cup shape (cold forging) by backward extrusion at a cross-sectional reduction rate (amount of deformation) of 60% to obtain a plastically processed body.
- the forming load (deformation resistance) at the time of obtaining the plastic work body was 2078 MPa (see FIG. 23), and the tensile strength (converted from the radial crushing strength) of the plastic work body was 692 MPa.
- the hardness was HRB 75 (see Figs. 25 and 27).
- the density of the plastically worked body was 7.71 gZcm 3 .
- the plastically worked body was re-sintered at 110 ° C. in a furnace in a mixed atmosphere of nitrogen gas and hydrogen gas to obtain a re-sintered body.
- the resintered product had a tensile strength (converted from the radial crushing strength) of 676 MPa and a hardness of HRB 71 (see Figs. 33 and 35).
- the density of the re-sintered product was 7.71 gZcm 3 .
- the re-sintered body was carburized at a maximum of 860 ° C in a furnace having an atmosphere of carbon potential of 1.0%, oil-quenched at 90 ° C, tempered at 150 ° C, and heat-treated.
- the tensile strength (converted from the radial crushing strength) of the heat-treated body was 1185 MPa (see Fig. 37), the surface hardness was HRC59, and the internal (2 mm from the surface) It was HRC 33 (HV 330).
- the forming load (deformation resistance) at the time of obtaining the plastic work body was 2428 MPa (see FIG. 24), the tensile strength (converted value from the radial crushing strength) of the plastic work body was 706 MPa, and the hardness was HRB was 96 (see Figures 26 and 28).
- the density of the plastic body was 7.70 gZcm 3 .
- the plastic workpiece was re-sintered at 110 ° C. in a furnace in a mixed atmosphere of nitrogen gas and hydrogen gas.
- the tensile strength (converted from the radial crushing strength) of the re-sintered product was 784 MPa
- the hardness was HRB 100 (see Fig. 34 and Fig. 36)
- the density was 7.70 g / cm. Was 3 .
- the re-sintered body was carburized at a maximum of 860 ° C in a furnace having an atmosphere of carbon potential of 1.0%, oil-quenched at 90 ° C, tempered at 150 ° C, and heat-treated. I got As a result, the tensile strength (converted from radial crushing strength) of the heat-treated product was 1 678 MPa, the surface hardness was HRC 62, and the hardness of the inside (2 mm from the surface) was HRC 41 ( HV 400) (see Figures 38 and 39).
- Example 3 Example 3:
- a mixture of 2.0% by weight of copper (Cu) and 0.3% by weight of graphite is formed on the surface of iron (Fe) and iron powder, which is a small amount of inevitable impurities, to form a metallic powder.
- powder and powder formed shape, density and form a preform of 7. 4 g / cm '3, the preform was 60 McCulley sintered at 800 ° C in a furnace of a nitrogen gas atmosphere Made a molding material. The elongation of this molding material was 12.0%, and the hardness was HRB 47.
- this molding material was re-extruded in a cup shape by extruding backward at a cross-sectional reduction rate of 60% Compression molding (cold forging) was performed to obtain a plastically worked product.
- the forming load (deformation resistance) at the time of obtaining the plastic work body was 196 OMPa
- the tensile strength (converted value from the radial crushing strength) of the plastic work body was 510 MPa
- the hardness was HRB 7 It was five.
- the density of the plastic worked body was 7.70 gZcm 3 .
- the plastic workpiece was re-sintered at 110 ° C. in a furnace in a mixed atmosphere of nitrogen gas and hydrogen gas.
- the tensile strength (converted from the radial crushing strength) of the re-sintered product was 735 MPa
- the hardness was HRB 80
- the density was 7.75 g / cm 3 .
- the re-sintered body was carburized at a maximum of 860 ° C in a furnace having an atmosphere of carbon potential of 1.0%, oil-quenched at 90, and tempered at 150 ° C to obtain a heat-treated body.
- the tensile strength (converted from the radial crushing strength) of the heat-treated body was 98 OMPa
- the hardness of the surface was HRC 42
- the hardness of the inside (2 mm from the surface) was HRB 91. there were.
- Examples 4 to 7 will be described. These Examples differ from Example 1 only in the configuration of the alloy steel powder, and the amount of graphite mixed with the alloy steel powder (0.3 Weight%), density of the preformed body (7.4 g / cm 3 ), pre-sintering conditions (800 C C for 60 minutes in a nitrogen gas furnace), re-compression molding conditions (cross-section Reduction rate 60%), resintering conditions (in a furnace with a mixed atmosphere of nitrogen gas and hydrogen gas at 1150 ° C), heat treatment conditions (in a furnace with an atmosphere of carbon potential 1.0%) Carburizing at a maximum of 860 ° C, oil quenching at 90 ° C, and tempering at 150 ° C). Therefore, in the following examples, only the composition of the alloy and the test results shall be described.
- the alloy steel powder contains 1.0% by weight of nickel (Ni), 0.3% by weight of molybdenum ( ⁇ ) and 0.3% by weight of copper (Cu), with the balance being iron (Fe). From unavoidable impurities Configuration.
- the alloy steel powder contains chromium (Cr) 1.% by weight, manganese (Mn) 0.7% by weight, molybdenum (Mo) 0.3% by weight, and the remainder is inevitable with iron (Fe).
- Cr chromium
- Mo manganese
- Mo molybdenum
- Fe iron
- the alloy steel powder contains 1.0% by weight of chromium (Cr), 0.3% by weight of molybdenum (Mo), and 0.3% by weight of vanadium (V), with the balance being inevitable with iron (Fe).
- the structure was made of impurities.
- the alloy steel powder contains 65% by weight of cobalt (Co), 8.0% by weight of chromium (Cr), 2.0% by weight of tungsten (W), and 0.5% by weight of molybdenum (Mo). The balance was made up of iron (Fe) and unavoidable impurities.
- the metal powder molding material according to the present invention contains a predetermined amount of graphite suitable for obtaining a member having high mechanical strength, and has a hardness advantageous for recompression molding. It has low elongation properties (deformability).
- the recompressed molded article according to the present invention can surely increase hardness, fatigue strength, and other mechanical properties, and can also improve dimensional accuracy.
- the present invention is not limited to the configuration of the above embodiment, and can be modified without departing from the gist of the invention.
- the pre-formed body 8 is formed by so-called warm forming, in which the metal powder 7 and the molding die are heated to a predetermined temperature and the yield point of the metal powder 7 is lowered. You may do so.
- the notch 23 for increasing the volume of the forming space 15 is formed in the upper punch 16 has been described, but the notch 23 is formed in the lower punch 17. It may be provided on both the upper punch 17 and the lower punch 17.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020007014215A KR20010052876A (ko) | 1999-04-16 | 2000-03-17 | 금속질 가루 성형 소재와 그 재압축 성형체 및 이 재압축성형체로부터 얻어지는 소결체 및 그들의 제조 방법 |
DE60030063T DE60030063T2 (de) | 1999-04-16 | 2000-03-17 | Pulvermetallurgisches verfahren |
EP00909684A EP1097770B1 (en) | 1999-04-16 | 2000-03-17 | Powder metallurgy process |
CA002334753A CA2334753A1 (en) | 1999-04-16 | 2000-03-17 | Metallic powder molding material and its re-compression molded body and sintered body obtained from the re-compression molded body and production methods thereof |
US09/647,862 US6503443B1 (en) | 1999-04-16 | 2000-03-17 | Metallic powder molding material and its re-compression molded body and sintered body obtained from the re-compression molded body and production methods thereof |
US10/180,133 US6905530B2 (en) | 1999-04-16 | 2002-06-27 | Metallic powder-molded body, re-compacted body of the molded body, sintered body produced from the re-compacted body, and processes for production thereof |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11/109056 | 1999-04-16 | ||
JP10905699 | 1999-04-16 | ||
JP11007399A JP3871825B2 (ja) | 1999-04-16 | 1999-04-16 | 金属質粉成形素材の再圧縮成形体及びその再圧縮成形体から得られる焼結体並びにそれらの製造方法 |
JP11/110073 | 1999-04-16 |
Related Child Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/647,862 A-371-Of-International US6503443B1 (en) | 1999-04-16 | 2000-03-17 | Metallic powder molding material and its re-compression molded body and sintered body obtained from the re-compression molded body and production methods thereof |
US10/180,133 Division US6905530B2 (en) | 1999-04-16 | 2002-06-27 | Metallic powder-molded body, re-compacted body of the molded body, sintered body produced from the re-compacted body, and processes for production thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2000062960A1 true WO2000062960A1 (fr) | 2000-10-26 |
Family
ID=26448846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2000/001615 WO2000062960A1 (fr) | 1999-04-16 | 2000-03-17 | Materiau de moulage a base de poudre metallique et corps moule par recompression, corps fritte obtenu a partir dudit corps moule par recompression, et procedes de production y relatifs |
Country Status (8)
Country | Link |
---|---|
US (2) | US6503443B1 (ja) |
EP (1) | EP1097770B1 (ja) |
KR (1) | KR20010052876A (ja) |
CN (1) | CN1297389A (ja) |
CA (1) | CA2334753A1 (ja) |
DE (1) | DE60030063T2 (ja) |
TW (1) | TW436345B (ja) |
WO (1) | WO2000062960A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1201338A3 (en) * | 2000-10-30 | 2005-06-08 | Hitachi, Ltd. | Method of sintering and forging raw material |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6503443B1 (en) * | 1999-04-16 | 2003-01-07 | Unisia Jecs Corporation | Metallic powder molding material and its re-compression molded body and sintered body obtained from the re-compression molded body and production methods thereof |
JP3698409B2 (ja) * | 2000-10-25 | 2005-09-21 | 本田技研工業株式会社 | 焼結スプロケット |
US6837915B2 (en) * | 2002-09-20 | 2005-01-04 | Scm Metal Products, Inc. | High density, metal-based materials having low coefficients of friction and wear rates |
JP2004124244A (ja) * | 2002-09-30 | 2004-04-22 | Nippon Piston Ring Co Ltd | 高精度焼結カムロブ材 |
SE0401041D0 (sv) * | 2004-04-21 | 2004-04-21 | Hoeganaes Ab | Sintered metal parts and method for the manufacturing thereof |
EP2265437A1 (en) * | 2008-03-19 | 2010-12-29 | Höganäs Ab (publ) | Stator compacted in one piece |
AT507913B1 (de) * | 2009-03-02 | 2013-08-15 | Miba Sinter Austria Gmbh | Vorrichtung zum verdichten eines sinterbauteils |
DE102010021470A1 (de) * | 2010-05-25 | 2011-12-01 | Siemens Aktiengesellschaft | Käfigläufer für eine Asynchronmaschine und Verfahren zur Herstellung des Käfigläufers |
CN101920720B (zh) * | 2010-09-09 | 2013-07-10 | 烟台东一粉末冶金制造有限公司 | 柱塞体和其制造方法 |
EP2511031A1 (en) | 2011-04-12 | 2012-10-17 | Höganäs Ab (publ) | A powder metallurgical composition and sintered component |
CN102434853B (zh) * | 2011-10-25 | 2016-03-16 | 深圳市光峰光电技术有限公司 | 光波长转换片、其制备方法及使用该光波长转换片的光源 |
CN102433510B (zh) * | 2011-12-08 | 2013-09-18 | 东南大学 | 高强高韧铁基粉末冶金合金及其制备方法 |
JP6309215B2 (ja) | 2013-07-02 | 2018-04-11 | Ntn株式会社 | 焼結機械部品の製造方法及びこれに用いる混合粉末 |
KR101684858B1 (ko) * | 2016-04-12 | 2016-12-12 | (주)하나테크 | 밀폐형 슬리브의 제조방법 |
CN106270527A (zh) * | 2016-08-05 | 2017-01-04 | 海安县鹰球粉末冶金有限公司 | 镍合金汽车启动电机行星齿轮及其制造方法 |
US12098449B2 (en) | 2018-03-26 | 2024-09-24 | Jfe Steel Corporation | Alloyed steel powder for powder metallurgy and iron-based mixed powder for powder metallurgy |
CN111902556B (zh) * | 2018-03-26 | 2021-11-19 | 杰富意钢铁株式会社 | 粉末冶金用合金钢粉及粉末冶金用铁基混合粉末 |
CN112743079A (zh) * | 2019-10-30 | 2021-05-04 | 江苏智造新材有限公司 | 一种双离合变速箱机械油泵定子及其制备方法 |
JP7147963B2 (ja) * | 2019-11-18 | 2022-10-05 | Jfeスチール株式会社 | 粉末冶金用合金鋼粉、粉末冶金用鉄基混合粉及び焼結体 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07173504A (ja) * | 1993-10-27 | 1995-07-11 | Unisia Jecs Corp | 圧粉成形用金型装置 |
JPH08144027A (ja) * | 1994-11-24 | 1996-06-04 | Mitsubishi Materials Corp | 高強度および高靭性を有する遊離黒鉛析出鉄系焼結材料 |
JPH08144026A (ja) * | 1994-11-24 | 1996-06-04 | Mitsubishi Materials Corp | 高強度および高靭性を有する遊離黒鉛析出鉄系焼結体 |
JPH0949062A (ja) * | 1995-08-07 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結合金軸受 |
JPH0949047A (ja) * | 1995-08-04 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結合金軸受 |
JPH0949064A (ja) * | 1995-08-07 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性Fe基焼結合金軸受 |
JPH0949061A (ja) * | 1995-08-04 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結含油軸受 |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE508993A (ja) | ||||
CH352352A (de) | 1955-12-31 | 1961-02-28 | Cosid Werke Veb | Verfahren zur Herstellung eines Eisen-Graphit-Verbundwerkstoffes |
US3992158A (en) * | 1973-08-16 | 1976-11-16 | Eastman Kodak Company | Integral analytical element |
GB1402660A (en) | 1973-08-17 | 1975-08-13 | Toyo Kohan Co Ltd | Alloy steels |
JPH01123005A (ja) | 1987-11-09 | 1989-05-16 | Mazda Motor Corp | 焼結冷間鍛造方法 |
JPH01165702A (ja) | 1987-12-23 | 1989-06-29 | Kawasaki Steel Corp | 高密度および高強度の合金鋼焼結体の製造方法 |
US5620845A (en) * | 1988-06-06 | 1997-04-15 | Ampcor, Inc. | Immunoassay diagnostic kit |
US5340731A (en) * | 1988-07-08 | 1994-08-23 | University Of British Columbia | Method of preparing a B-1,4 glycan matrix containing a bound fusion protein |
GB8921260D0 (en) | 1989-09-20 | 1989-11-08 | Brico Engineering Company | Sintered materials |
US5108493A (en) | 1991-05-03 | 1992-04-28 | Hoeganaes Corporation | Steel powder admixture having distinct prealloyed powder of iron alloys |
US5225328A (en) * | 1991-05-30 | 1993-07-06 | Quidel Corporation | Stable alkaline phosphatase compositions with color enhancement and their use in assays |
US5866344A (en) * | 1991-11-15 | 1999-02-02 | Board Of Regents, The University Of Texas System | Antibody selection methods using cell surface expressed libraries |
US5154881A (en) | 1992-02-14 | 1992-10-13 | Hoeganaes Corporation | Method of making a sintered metal component |
US5368630A (en) | 1993-04-13 | 1994-11-29 | Hoeganaes Corporation | Metal powder compositions containing binding agents for elevated temperature compaction |
US5496934A (en) * | 1993-04-14 | 1996-03-05 | Yissum Research Development Company Of The Hebrew University Of Jerusalem | Nucleic acids encoding a cellulose binding domain |
US5571305A (en) | 1993-09-01 | 1996-11-05 | Kawasaki Steel Corporation | Atomized steel powder excellent machinability and sintered steel manufactured therefrom |
US5552109A (en) | 1995-06-29 | 1996-09-03 | Shivanath; Rohith | Hi-density sintered alloy and spheroidization method for pre-alloyed powders |
US6203753B1 (en) | 1996-05-13 | 2001-03-20 | The Presmet Corporation | Method for preparing high performance ferrous materials |
US5872322A (en) | 1997-02-03 | 1999-02-16 | Ford Global Technologies, Inc. | Liquid phase sintered powder metal articles |
JP3871781B2 (ja) * | 1997-10-14 | 2007-01-24 | 株式会社日立製作所 | 金属質粉成形素材及びその製造方法 |
US6503443B1 (en) * | 1999-04-16 | 2003-01-07 | Unisia Jecs Corporation | Metallic powder molding material and its re-compression molded body and sintered body obtained from the re-compression molded body and production methods thereof |
US6514307B2 (en) * | 2000-08-31 | 2003-02-04 | Kawasaki Steel Corporation | Iron-based sintered powder metal body, manufacturing method thereof and manufacturing method of iron-based sintered component with high strength and high density |
-
2000
- 2000-03-17 US US09/647,862 patent/US6503443B1/en not_active Expired - Lifetime
- 2000-03-17 WO PCT/JP2000/001615 patent/WO2000062960A1/ja active IP Right Grant
- 2000-03-17 DE DE60030063T patent/DE60030063T2/de not_active Expired - Lifetime
- 2000-03-17 CA CA002334753A patent/CA2334753A1/en not_active Abandoned
- 2000-03-17 CN CN00800456A patent/CN1297389A/zh active Pending
- 2000-03-17 KR KR1020007014215A patent/KR20010052876A/ko not_active Application Discontinuation
- 2000-03-17 EP EP00909684A patent/EP1097770B1/en not_active Expired - Lifetime
- 2000-04-06 TW TW089106336A patent/TW436345B/zh not_active IP Right Cessation
-
2002
- 2002-06-27 US US10/180,133 patent/US6905530B2/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07173504A (ja) * | 1993-10-27 | 1995-07-11 | Unisia Jecs Corp | 圧粉成形用金型装置 |
JPH08144027A (ja) * | 1994-11-24 | 1996-06-04 | Mitsubishi Materials Corp | 高強度および高靭性を有する遊離黒鉛析出鉄系焼結材料 |
JPH08144026A (ja) * | 1994-11-24 | 1996-06-04 | Mitsubishi Materials Corp | 高強度および高靭性を有する遊離黒鉛析出鉄系焼結体 |
JPH0949047A (ja) * | 1995-08-04 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結合金軸受 |
JPH0949061A (ja) * | 1995-08-04 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結含油軸受 |
JPH0949062A (ja) * | 1995-08-07 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性焼結合金軸受 |
JPH0949064A (ja) * | 1995-08-07 | 1997-02-18 | Mitsubishi Materials Corp | 相手攻撃性の低い耐摩耗性Fe基焼結合金軸受 |
Non-Patent Citations (1)
Title |
---|
See also references of EP1097770A4 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1201338A3 (en) * | 2000-10-30 | 2005-06-08 | Hitachi, Ltd. | Method of sintering and forging raw material |
Also Published As
Publication number | Publication date |
---|---|
TW436345B (en) | 2001-05-28 |
US6503443B1 (en) | 2003-01-07 |
US20020159908A1 (en) | 2002-10-31 |
KR20010052876A (ko) | 2001-06-25 |
DE60030063T2 (de) | 2007-01-04 |
CA2334753A1 (en) | 2000-10-26 |
EP1097770A1 (en) | 2001-05-09 |
EP1097770B1 (en) | 2006-08-16 |
US6905530B2 (en) | 2005-06-14 |
CN1297389A (zh) | 2001-05-30 |
DE60030063D1 (de) | 2006-09-28 |
EP1097770A4 (en) | 2004-01-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2000062960A1 (fr) | Materiau de moulage a base de poudre metallique et corps moule par recompression, corps fritte obtenu a partir dudit corps moule par recompression, et procedes de production y relatifs | |
JP5671526B2 (ja) | 高強度低合金焼結鋼 | |
KR100793128B1 (ko) | 철계 금속 분말 소결체, 이의 제조 방법 및 고강도와고밀도를 갖는 철계 소결체의 제조 방법 | |
JP6688287B2 (ja) | プレアロイ鉄基粉末、プレアロイ鉄基粉末を含有する鉄基粉末混合物、及び鉄基粉末混合物からプレス成形および焼結した部品を製造する方法 | |
CN104428085B (zh) | 烧结部件及起动器用小齿轮、以及它们的制造方法 | |
WO2005103315A1 (ja) | 鉄基焼結合金、鉄基焼結合金部材およびそれらの製造方法 | |
JP2007262536A (ja) | 焼結歯車およびその製造方法 | |
JP2003253372A (ja) | 高密度鉄基鍛造部品の製造方法 | |
US5881354A (en) | Sintered hi-density process with forming | |
JP3869620B2 (ja) | 合金鋼粉成形素材と合金鋼粉加工体及び合金鋼粉成形素材の製造方法 | |
JP3774625B2 (ja) | 焼結部材の鍛造方法 | |
CN111344429B (zh) | 铁基烧结合金材料及其制造方法 | |
US20100196188A1 (en) | Method of producing a steel moulding | |
JP2005042812A (ja) | サイレントチェーン用焼結スプロケットおよびその製造方法 | |
JP6819624B2 (ja) | 粉末冶金用鉄基混合粉末およびその製造方法ならびに引張強さと耐衝撃性に優れた焼結体 | |
JP2001523763A (ja) | 粉末ブレンドによる高密度成形方法 | |
JPH11117002A (ja) | 金属質粉成形素材及びその製造方法 | |
KR20050012161A (ko) | 사일런트 체인용 소결 스프로켓 및 그 제조방법 | |
WO2009030291A1 (en) | Method of producing a sinter-hardenable powder metal part | |
JP4060092B2 (ja) | 粉末冶金用合金鋼粉およびその焼結体 | |
JP6743720B2 (ja) | 粉末冶金用鉄基混合粉末およびその製造方法ならびに引張強さと耐衝撃性に優れた焼結体 | |
JP3871825B2 (ja) | 金属質粉成形素材の再圧縮成形体及びその再圧縮成形体から得られる焼結体並びにそれらの製造方法 | |
JP2003113402A (ja) | 傘歯車の製造方法、傘歯車のギアブランクの製造方法、傘歯車のギアブランクおよび傘歯車のギアブランク製造用の金型本体 | |
JP3475545B2 (ja) | 粉末冶金用混合鋼粉及びそれを含む焼結用材料 | |
JP2002294388A (ja) | 鉄基粉末成形用素材、その製造方法および高強度高密度鉄基焼結体の製造方法 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 00800456.0 Country of ref document: CN |
|
WWE | Wipo information: entry into national phase |
Ref document number: 09647862 Country of ref document: US |
|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): CA CN KR US |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE |
|
ENP | Entry into the national phase |
Ref document number: 2334753 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1020007014215 Country of ref document: KR |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2000909684 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 2000909684 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 1020007014215 Country of ref document: KR |
|
ENP | Entry into the national phase |
Ref document number: 2002 180133 Country of ref document: US Date of ref document: 20020627 Kind code of ref document: A |
|
WWR | Wipo information: refused in national office |
Ref document number: 1020007014215 Country of ref document: KR |
|
WWG | Wipo information: grant in national office |
Ref document number: 2000909684 Country of ref document: EP |