US20150217372A1 - Machine part and process for producing same - Google Patents
Machine part and process for producing same Download PDFInfo
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- US20150217372A1 US20150217372A1 US14/422,892 US201314422892A US2015217372A1 US 20150217372 A1 US20150217372 A1 US 20150217372A1 US 201314422892 A US201314422892 A US 201314422892A US 2015217372 A1 US2015217372 A1 US 2015217372A1
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- machine part
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- 238000000034 method Methods 0.000 title claims description 14
- 239000000843 powder Substances 0.000 claims abstract description 123
- 239000002994 raw material Substances 0.000 claims abstract description 79
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 65
- 238000010438 heat treatment Methods 0.000 claims abstract description 39
- 229910052742 iron Inorganic materials 0.000 claims abstract description 32
- 238000005245 sintering Methods 0.000 claims abstract description 29
- 239000000956 alloy Substances 0.000 claims abstract description 26
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 26
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 18
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 17
- 239000011733 molybdenum Substances 0.000 claims abstract description 17
- 239000000314 lubricant Substances 0.000 claims description 33
- 239000007787 solid Substances 0.000 claims description 26
- 238000000748 compression moulding Methods 0.000 claims description 21
- 238000004519 manufacturing process Methods 0.000 claims description 20
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 18
- 238000005096 rolling process Methods 0.000 claims description 11
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- 238000000465 moulding Methods 0.000 claims description 7
- 239000000463 material Substances 0.000 description 27
- 238000010276 construction Methods 0.000 description 19
- 229910052751 metal Inorganic materials 0.000 description 17
- 239000002184 metal Substances 0.000 description 17
- 238000005299 abrasion Methods 0.000 description 14
- 238000010791 quenching Methods 0.000 description 13
- 230000000171 quenching effect Effects 0.000 description 13
- 229910052799 carbon Inorganic materials 0.000 description 7
- 238000007906 compression Methods 0.000 description 7
- 230000006835 compression Effects 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 6
- 238000002156 mixing Methods 0.000 description 6
- 239000011651 chromium Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000005255 carburizing Methods 0.000 description 4
- 238000005469 granulation Methods 0.000 description 4
- 230000003179 granulation Effects 0.000 description 4
- 239000012535 impurity Substances 0.000 description 4
- 238000002347 injection Methods 0.000 description 4
- 239000007924 injection Substances 0.000 description 4
- 238000005496 tempering Methods 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- CADICXFYUNYKGD-UHFFFAOYSA-N sulfanylidenemanganese Chemical compound [Mn]=S CADICXFYUNYKGD-UHFFFAOYSA-N 0.000 description 3
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 3
- 238000011049 filling Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000003672 processing method Methods 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- 108010038629 Molybdoferredoxin Proteins 0.000 description 1
- HBELESVMOSDEOV-UHFFFAOYSA-N [Fe].[Mo] Chemical compound [Fe].[Mo] HBELESVMOSDEOV-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- VAWNDNOTGRTLLU-UHFFFAOYSA-N iron molybdenum nickel Chemical compound [Fe].[Ni].[Mo] VAWNDNOTGRTLLU-UHFFFAOYSA-N 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 229910052982 molybdenum disulfide Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Images
Classifications
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- 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
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
-
- 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
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
-
- B22F1/0003—
-
- 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
- B22F3/12—Both compacting and sintering
-
- 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
- B22F3/12—Both compacting and sintering
- B22F3/16—Both compacting and sintering in successive or repeated steps
- B22F3/162—Machining, working after consolidation
-
- 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
- B22F3/24—After-treatment of workpieces or articles
-
- 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
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/08—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of toothed articles, e.g. gear wheels; of cam discs
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- 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
- B22F3/24—After-treatment of workpieces or articles
- B22F2003/248—Thermal after-treatment
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H55/00—Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
- F16H55/02—Toothed members; Worms
- F16H55/06—Use of materials; Use of treatments of toothed members or worms to affect their intrinsic material properties
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
Definitions
- the present invention relates to a machine part and a manufacturing method therefor, and more particularly, to a machine part formed of a sintered metal and a manufacturing method therefor.
- a machine part to be used for a power transmission application or a machine part to be used in a part subjected to pressure in a pump or the like (pressure receiving part) is required to have particularly high mechanical strength, abrasion resistance, fatigue strength, and the like. Therefore, a machine part of this kind is generally formed of an ingot material.
- a number of processing steps are required. Further, a great material loss is caused in such steps. Therefore, a machine part obtained by processing an ingot material is generally liable to have high cost. In such circumstances, various attempts have recently been made to produce the machine part as described above by using a sintered metal (sintered material).
- Patent Literature 1 the applicant of the present application has proposed a machine part (power transmission part), which is formed of a sintered material obtained by molding granulated powder of fine powders each containing iron as a main component into a green compact, followed by sintering, and which is obtained by subjecting the sintered material to heat treatment (quenching and tempering treatment).
- the sintered material to be used as a base material for the machine part in Patent Literature 1 has a high density (a true density ratio of 85% or more) as compared to a general sintered material because of, for example, the following reasons: (1) the sintered material is produced by using as a main raw material the granulated powder obtained through granulation of the fine powders so as to have an appropriate grain size, and hence exhibits improved flowability in a mold, and by extension, improved moldability even though the fine powders are used; and (2) the granulated powder obtained through granulation of the fine powders has a large surface area, and hence sintering property between adjacent granulated powders is improved.
- the machine part formed of such sintered material has improved mechanical strength, abrasion resistance, and the like as compared to a machine part formed of the general sintered material.
- the sintered material proposed in Patent Literature 1 can be manufactured through similar steps to those in the case of the general sintered material except that raw material powder containing as a main raw material the granulated powder is used.
- a construction of Patent Literature 1 it is considered that a machine part having improved demand characteristics including mechanical strength and abrasion resistance can be produced with high accuracy at relatively low cost.
- Patent Literature 1 JP 2011-94789 A
- Patent Literature 1 the machine part formed of a sintered material proposed in Patent Literature 1 is still far inferior in mechanical strength, abrasion resistance, and the like to a machine part formed of an ingot material owing to its true density ratio being set to 85% or more. Therefore, its application is inevitably limited.
- it is essential to produce (prepare) the granulated powder of high quality in order to enable stable manufacturing (mass-production) of a desired machine part, but a lot of labor and cost are required for stably obtaining such granulated powder of high quality. Therefore, the construction of Patent Literature 1 cannot achieve a cost reduction effect as much as expected, and the cost of the machine part may be increased instead.
- an object of the present invention is to provide a machine part formed of a sintered metal, which can be mass-produced at low cost and is excellent in mechanical strength, abrasion resistance, and the like.
- a machine part comprising a sintered compact obtained by sintering a green compact of raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, the machine part including at least a hardened layer formed through heat treatment, and having a true density ratio of 97% or more and less than 100%.
- the “true density” in the equation means a theoretical density of a material having no pores in its interior portion, such as an ingot material.
- the “density of entire machine part formed of sintered compact” in the equation is measured by, for example, a method specified in JIS Z2501.
- a method of manufacturing a machine part comprising a sintered compact having a true density ratio of 97% or more and less than 100% comprising: a compression molding step of compression molding raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, in a mold to obtain a green compact; a sintering step of heating the green compact at a temperature equal to or higher than a sintering temperature of the iron-based alloy powder to obtain a sintered compact; and a heat treatment step of subjecting the sintered compact to heat treatment to form a hardened layer.
- the machine part formed of a sintered metal according to one embodiment of the present invention has a true density ratio of 97% or more and less than 100% (roughly corresponding to 7.6 g/cm 3 or more and less than 7.8 g/cm 3 , when converted into a density), and is highly densified to the extent approximate to that in the case of an ingot material. Therefore, the machine part exhibits excellent characteristics in mechanical strength, abrasion resistance, fatigue strength, and the like.
- Such machine part formed of a sintered metal having a high density and high strength can be obtained by adopting using the sintered compact (sintered material) including a hardened layer formed through heat treatment after the sintering, and further adopting the following constructions (1) and (2) in a material aspect: (1) selectively using as main powder constituting the raw material powder the iron-based alloy powder containing molybdenum; and (2) setting the blending ratio of the carbon powder in the raw material powder to 0.1 to 0.8 mass %, which is lower than that in a general sintered metal.
- the adoption of the above-mentioned construction (1) improves compression moldability and sintering property.
- the adoption of the above-mentioned construction (2) further improves the compression moldability along with a reduction in the blending amount of carbon having a low specific gravity, while securing lubricity between powders and heat treatment property (heat treatment property after the sintering). Thus, a high density is achieved.
- the use of the raw material powder containing the iron-based alloy powder as a main raw material and having an appropriate amount of carbon powder blended therein, as the raw material powder for obtaining the machine part according to one embodiment of the present invention eliminates the need for troublesome treatment such as granulation treatment proposed in Patent Literature 1 in the process of preparing and producing the raw material powder. Therefore, the manufacturing cost can be significantly reduced as compared to the construction of Patent Literature 1. As described above, according to one embodiment of the present invention, it is possible to obtain the machine part formed of a sintered metal, which can be mass-produced at low cost and is excellent in mechanical strength, abrasion resistance, and the like.
- the addition amount of the solid lubricant is preferably as low as possible from the viewpoint of highly densifying the green compact.
- the addition amount of the solid lubricant is preferably 0.1 mass % or less, more preferably 0.05 mass % or less in terms of outer percentage, given that the mass of the raw material powder is defined as 100%.
- At least a part of the hardened layer may comprise a dense layer in which a porous structure is more densified than in another area. With this, the machine part can achieve a higher density and higher strength.
- such machine part may be obtained by performing a plastic processing step of subjecting the sintered compact to plastic processing between the sintering step and the heat treatment step.
- plastic processing in the plastic processing step for example, rolling can be adopted.
- the processing method to be adopted is appropriately selected depending on, for example, the shape of the machine part. Whatever processing method is adopted, cold plastic processing can efficiently improve the accuracy and density (strength) of a portion to be processed as compared to warm or hot plastic processing.
- the hardness of the machine part having the above-mentioned construction may gradually reduce from a surface to a core portion (a center portion in the thickness direction). This can provide the machine part with toughness, and hence prolong the durability lifetime of the machine part.
- the present invention described above can be preferably applied to the production of a machine part such as a gear or a cam by using a sintered metal.
- a machine part such as a gear or a cam by using a sintered metal.
- the present invention is not only applied to a gear, a cam, or the like and can also be preferably applied to the production of any other machine part (for example, a bearing) by using a sintered metal.
- FIG. 1 is a perspective view of a gear as a machine part according to one embodiment of the present invention.
- FIG. 3 is a block diagram illustrating a manufacturing procedure of the gear illustrated in FIG. 1 .
- FIG. 4 is a schematic sectional view illustrating an initial stage of a compression molding step.
- FIG. 5 is a schematic sectional view illustrating a middle stage of the compression molding step.
- FIG. 6 is an enlarged view of a main portion illustrating one embodiment of a plastic processing step.
- FIG. 7 is a view schematically illustrating a state in which the shape of a sintered compact changes along with plastic processing.
- FIG. 8 is a graph showing actually measured results of the hardness of the sintered compact before and after the plastic processing.
- FIG. 1 is a perspective view of a machine part according to one embodiment of the present invention
- FIG. 2 is an enlarged sectional view (enlarged sectional view in the plane surface perpendicular to the axis) of a portion X illustrated in FIG. 1
- the machine part illustrated in FIG. 1 is, for example, a gear (gear for a transmission) 1 to be used by being incorporated into a transmission of an automobile.
- the gear 1 includes a large-diameter annular portion 3 having a tooth surface 2 along its outer circumference, a small-diameter annular portion 4 having a mounting hole for mounting the gear 1 to a rotation shaft (not shown), and a plurality of connecting portions 5 for connecting the large-diameter annular portion 3 and the small-diameter annular portion 4 , in an integrated manner.
- the gear 1 is formed of a sintered metal and has a true density ratio of 97% or more and less than 100%.
- a hardened layer (surface hardened layer) 8 is formed in the entire area of the gear 1 through heat treatment after sintering (by subjecting a sintered compact to heat treatment).
- a dense layer 7 in which a porous structure is more densified than in another area is formed in the area in which the tooth surface 2 is formed (outer circumference of the large-diameter annular portion 3 ) in the gear 1 .
- the dense layer 7 is formed by subjecting the outer circumference of a sintered compact to plastic processing
- the hardened layer 8 is formed by subjecting the sintered compact after the plastic processing (after the formation of the dense layer 7 ) to heat treatment, while the methods of forming the dense layer 7 and the hardened layer 8 are described in detail later. That is, the hardened layer 8 is formed so as to include the dense layer 7 .
- the dense layer 7 has a higher hardness than the hardened layer 8 .
- the hardness is the highest in the surface and gradually reduces toward the core portion (center portion in the thickness direction). Therefore, the tooth surface 2 has the highest mechanical strength, the highest abrasion resistance, and the like of the portions constituting the gear 1 .
- the gear 1 as the machine part having the above-mentioned construction is manufactured by a raw material powder preparation step S 1 , a compression molding step S 2 , a sintering step S 3 , a plastic processing step S 4 , and a heat treatment step S 5 in the stated order, as illustrated in FIG. 3 .
- the steps are hereinafter described in that order.
- raw material powder 10 (see FIG. 5 ) as a material for forming the gear 1 is prepared and produced.
- the raw material powder 10 there is used raw material powder that contains as a main raw material (main powder) iron-based alloy powder containing molybdenum (Mo) and nickel (Ni) and has an appropriate amount of carbon (C) powder blended therein.
- main powder iron-based alloy powder containing molybdenum (Mo) and nickel (Ni) and has an appropriate amount of carbon (C) powder blended therein.
- iron-based alloy powder described above partially alloyed powder or completely alloyed powder of molybdenum, nickel, and iron (Fe) is used.
- the ratios of the elements in the raw material powder 10 are as follows: 0.2 to 0.8 mass % of molybdenum, 0.2 to 0.8 mass % of nickel, and 0.1 to 0.8 mass % of carbon, with the balance being iron (and inevitable impurities), given that the mass of the raw material powder 10 is defined as 100.
- raw material powder in which the blending ratios of molybdenum, nickel, and carbon are each 0.5 mass %, with the balance being iron (and inevitable impurities) is used.
- the iron-based alloy powder one having an average grain size of from 40 to 150 ⁇ m is used in consideration of cost and compression moldability. Specifically, small-size iron-based alloy powder having an average grain size of less than 40 ⁇ m is expensive, and reduces the compression moldability owing to its poor flowability. In contrast, when large-size iron-based alloy powder having an average grain size exceeding 150 ⁇ m is used, it is difficult to obtain a green compact having a high density because large pores are liable to be formed between the powders.
- the raw material powder 10 is subjected to compression molding by using a molding device 11 as illustrated in FIGS. 4 and 5 , to provide a green compact having a shape close to that of the gear 1 illustrated in FIG. 1 (substantially finished product shape).
- the molding device 11 includes, as main constituents, a mold 12 having a core 13 , upper and lower punches 14 , 15 , and a die 16 , which are disposed coaxially, a heater 17 for heating the die 15 (mold 12 ), and a lubricant injection nozzle 18 for injecting a solid lubricant 19 into a cavity 12 a of the mold 12 .
- the solid lubricant 19 is injected from the lubricant injection nozzle 18 arranged between the core 13 and the upper punch 14 into the cavity 12 a as illustrated in FIG. 4 .
- the solid lubricant 19 is allowed to adhere to the surfaces defining the cavity 12 a (a radially outer surface 13 a of the core 13 , an upper edge surface 15 a of the lower punch 15 , and a radially inner surface 16 a of the die 16 ) (see the enlarged view in FIG. 5 ).
- the solid lubricant 19 there may be used any lubricant of the same kind as or different kind from the solid lubricant added to the raw material powder 10 .
- solid lubricant 19 there may be used not only one kind, but a mixture of two or more kinds
- a solid lubricant of the same kind as the solid lubricant added to the raw material powder 10 that is, zinc stearate is used as the solid lubricant 19 .
- the heater 17 is activated to heat the die 16 (mold 12 ) at least a time period from the filling of the raw material powder 10 into the cavity 12 a to the completion of the formation of the green compact.
- the green compact is obtained by subjecting the raw material powder 10 filled into the cavity 12 a to compression molding in the state in which the mold 12 is heated.
- the heating of the die 16 by the heater 17 is performed so that the temperature of the die 16 is 70° C. or more, more preferably a temperature equal to or higher than the melting point of the solid lubricant 19 and 120° C. or less.
- a lubricant component of the solid lubricant 19 adhering to the surfaces defining the cavity 12 a can diffuse and penetrate efficiently between the raw material powder 10 (green compact) and the cavity 12 a , further between the powders constituting the raw material powder 10 . Therefore, the moldability and mold releasability of the green compact are improved even when the amount of the solid lubricant 19 to adhere to the surfaces defining the die 12 a or the amount of the solid lubricant to be added to the raw material powder 10 is reduced. Accordingly, this provides an advantage in obtaining the green compact having a high density and high accuracy, and by extension, the gear 1 having high strength.
- the heating of the die 16 by the heater 17 may be performed so as to keep the die 16 in the above-mentioned temperature range at all times.
- this embodiment adopts a so-called internal heating method of heating the die 16 (mold 12 ) by the heater 17 disposed inside the die 16
- an external heating method of heating the mold 12 by the heater or the like disposed outside the mold 12 may be adopted.
- the raw material powder 10 preliminarily heated may be filled into the cavity 12 a of the mold 12 .
- the green compact thus obtained is transferred to the sintering step S 3 .
- the green compact is heated at a temperature equal to or higher than the sintering temperature of the iron-based alloy powder constituting the green compact, to bind by sintering the powders adjacent to each other.
- a sintered compact 1 ′ is obtained (see FIG. 6 ).
- Sintering in an active gas atmosphere such as oxygen may cause oxidation of the powder constituting the green compact and adversely affect the mechanical strength and the like of the sintered compact 1 ′, and by extension, of the gear 1 , because the green compact is obtained through compression molding of the raw material powder 10 containing as a main raw material the iron-based alloy powder.
- the green compact is placed in an inert gas atmosphere (for example, nitrogen gas atmosphere) and heated at 1,200° C. or more and 1,300° C. or less (for example, 1,250° C.) for a predetermined time period, to provide the sintered compact 1 ′.
- an inert gas atmosphere for example, nitrogen gas atmosphere
- 1,200° C. or more and 1,300° C. or less for example, 1,250° C.
- 1,250° C. for example, 1,250° C.
- the sintered compact 1 ′ thus obtained is transferred to the plastic processing step S 4 .
- the sintered compact 1 ′ is subjected to plastic processing to form the tooth surface 2 in a finished shape on the outer circumference of the sintered compact 1 ′.
- the formation of the tooth surface 2 is performed by, for example, using a rolling machine 20 as schematically illustrated in FIG. 6 .
- the rolling machine 20 includes a support shaft 23 for supporting the sintered compact 1 ′ in a rotatable manner, two roller dies 21 , 22 each arranged at the radially outer side of the support shaft 23 and having a forming portion for forming the tooth surface 2 on its outer circumference.
- the two roller dies 21 , 22 are arranged so as to face each other across the support shaft 23 (sintered compact 1 ′).
- the roller dies 21 , 22 are rotated while being pressed against the outer circumference of the sintered compact 1 ′ supported by the support shaft 23 in a rotatable manner (rotated in a counterclockwise direction in the example illustrated in FIG. 6 ).
- the tooth surface 2 in a finished shape is formed on the entire circumference of the the sintered compact 1 ′.
- the rolling processing described above is performed on, for example, the sintered compact 1 ′ including a tooth surface 2 ′ constructed by consecutively providing tooth portions each having an involute shape (see the two-dot chain line in FIG. 7 ).
- the tooth portions constituting the tooth surface 2 ′ are each subjected to compression deformation in the circumferential direction and elongation deformation in the radial direction along with the rolling processing, to be formed into a tooth portion in a finished shape illustrated by the solid line in FIG. 7 .
- the porous structure on the outer circumference of the sintered compact 1 ′ is densified to form the dense layer 7 (see FIG. 2 ).
- the porous structure is densified to form the dense layer 7 as described above, pores in which stress is to be concentrated are reduced, and thus, the tooth surface 2 excellent in mechanical strength, particularly in fatigue strength, is obtained.
- FIG. 8 shows measured results of the hardness of the sintered compact 1 ′ on its outer circumference before and after the plastic processing.
- the hardness of the sintered compact 1 ′ on its outer circumference is significantly increased after the rolling processing as compared to before the rolling processing.
- the hardness significantly increases particularly around the surface of the sintered compact 1 ′, gradually reduces therefrom to the core portion (inner portion) of the sintered compact 1 ′, and becomes almost constant beyond a predetermined depth.
- the sintered compact 1 ′ having the tooth surface 2 in a finished shape formed therein is transferred to the heat treatment step S 5 .
- the sintered compact 1 ′ is subjected to heat treatment, to form the hardened layer 8 on the entire surface area of the sintered compact 1 ′ associated with quenching (see FIG. 2 ).
- the mechanical strength and abrasion resistance of the sintered compact 1 ′ are entirely increased.
- the mechanical strength and abrasion resistance of the area in which the dense layer 7 is formed are further increased in the sintered compact 1 ′.
- the method for the heat treatment is not particularly limited, and any known method such as carburizing quenching, immersion quenching, or high-frequency quenching can be appropriately adopted.
- carburizing quenching is adopted. Tempering is performed after the quenching in order to provide the sintered compact 1 ′ (gear 1 ) with high toughness as well as high mechanical strength and the like.
- finishing processing such as grinding processing, polishing processing, lapping processing, or super finishing processing may be performed, as required.
- the gear 1 formed of a sintered metal according to the present invention has a true density ratio of 97% or more and less than 100% (roughly corresponding to 7.6 g/cm 3 or more and less than 7.8 g/cm 3 when converted into a density) and is highly densified to the extent approximate to that in the case of an ingot material. Therefore, the gear 1 exhibits excellent characteristics in mechanical strength, abrasion resistance, fatigue strength, and the like.
- the inventors of the invention of the present application have realized the sintered compact 1 ′ having a high density and high strength by adopting the following constructions (1) and (2) particularly in a material aspect: (1) selectively using as a main raw material constituting the raw material powder 10 the iron-based alloy powder containing molybdenum; and (2) setting the blending ratio of the carbon powder in the raw material powder 10 to from 0.1 to 0.8 mass %, which is lower than that in a general sintered metal.
- the adoption of the above-mentioned construction (1) improves the compression moldability and the sintering property.
- the gear 1 according to the present invention includes the hardened layer 8 formed through the heat treatment after the sintering, and hence achieves high strength.
- the sintered compact 1 ′ is subjected to carburizing, quenching, and tempering as the heat treatment, and hence the hardness of the gear 1 gradually reduces from the surface to the core portion. Therefore, the gear 1 has high toughness as well, and hence is excellent in durability lifetime and impact resistance.
- the use of the raw material powder containing the iron-based alloy powder as a main raw material and having an appropriate amount of the carbon powder blended therein, as the raw material powder 10 for obtaining the gear 1 eliminates the need for troublesome treatment such as granulation treatment disclosed in Patent Literature 1 in the process of preparing and producing the raw material powder 10 . Therefore, manufacturing cost can be significantly reduced as compared to the construction of Patent Literature 1.
- the gear 1 formed of a sintered metal and the manufacturing method therefor according to embodiments of the present invention have been described above, but the composition of the raw material powder 10 suitable for manufacturing of the gear 1 is not limited to the one described above.
- the raw material powder 10 that contains as a main raw material iron based alloy powder containing molybdenum (partially alloyed powder of molybdenum-iron) and has carbon powder and chromium (Cr) powder blended therein may be used.
- a construction in which the powders are blended so that the contents of molybdenum, carbon, and chromium may be from 0.2 to 0.8 mass %, from 0.1 to 0.8 mass %, and from 0.5 to 2.0 mass %, respectively, and the balance may be iron (and an unavoidable impurity), given that the mass of the raw material powder 10 is defined as 100.
- the raw material powder 10 that contains as a main raw material iron based alloy powder containing molybdenum and nickel (partially alloyed powder of molybdenum-nickel-iron) and has carbon powder and manganese sulfide (MnS) powder blended therein may also be used.
- the powders are blended so that the contents of molybdenum, nickel, carbon, and manganese sulfide may be from 0.2 to 0.8 mass %, from 0.2 to 0.8 mass %, from 0.1 to 0.8 mass %, and from 0.5 to 2.0 mass %, respectively, with the balance being iron (and inevitable impurities), given that the mass of the raw material powder 10 is defined as 100.
- the plastic processing step S 4 may be omitted while, in the embodiment described above, the plastic processing step S 4 is performed between the sintering step S 3 and the heat treatment step S 5 , and in the plastic processing step S 4 , the sintered compact 1 ′ is formed into a finished shape and the dense layer 7 in which a porous structure is more densified than in another area is formed.
- the plastic processing step S 4 can be omitted when the green compact in a finished shape can be formed through the compression molding step S 2 and the sintered compact 1 ′ having a true density ratio of 97% or more and less than 100% can be obtained only by forming the hardened layer 8 through the heat treatment step S 5 .
- the present invention can also be applied to any other machine part such as a gear or a cam to be used by being incorporated into various mechanical devices (for example, a cam for a vane pump).
- the machine part according to the present invention is formed of a sintered compact highly densified to the extent approximate to that of an ingot material and can be mass-produced at low cost while securing high mechanical strength and high abrasion resistance, and hence is extremely advantageous because the machine part can be applied to such application in which replacement from a machine part formed of an ingot material has hitherto been difficult and thus contribute to reduction in cost of various mechanical devices.
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Abstract
Provided is a gear (1) (machine part), including a sintered compact obtained by sintering a green compact of raw material powder (10) that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, the gear (1) (machine part) including a hardened layer (8) formed through heat treatment after the sintering, and having a true density ratio of 97% or more and less than 100%.
Description
- The present invention relates to a machine part and a manufacturing method therefor, and more particularly, to a machine part formed of a sintered metal and a manufacturing method therefor.
- For example, a machine part to be used for a power transmission application (power transmission part) or a machine part to be used in a part subjected to pressure in a pump or the like (pressure receiving part) is required to have particularly high mechanical strength, abrasion resistance, fatigue strength, and the like. Therefore, a machine part of this kind is generally formed of an ingot material. However, in order to obtain a machine part formed of an ingot material satisfying the above-mentioned demand characteristics with high accuracy, a number of processing steps are required. Further, a great material loss is caused in such steps. Therefore, a machine part obtained by processing an ingot material is generally liable to have high cost. In such circumstances, various attempts have recently been made to produce the machine part as described above by using a sintered metal (sintered material).
- For example, in
Patent Literature 1, the applicant of the present application has proposed a machine part (power transmission part), which is formed of a sintered material obtained by molding granulated powder of fine powders each containing iron as a main component into a green compact, followed by sintering, and which is obtained by subjecting the sintered material to heat treatment (quenching and tempering treatment). The sintered material to be used as a base material for the machine part inPatent Literature 1 has a high density (a true density ratio of 85% or more) as compared to a general sintered material because of, for example, the following reasons: (1) the sintered material is produced by using as a main raw material the granulated powder obtained through granulation of the fine powders so as to have an appropriate grain size, and hence exhibits improved flowability in a mold, and by extension, improved moldability even though the fine powders are used; and (2) the granulated powder obtained through granulation of the fine powders has a large surface area, and hence sintering property between adjacent granulated powders is improved. Therefore, the machine part formed of such sintered material has improved mechanical strength, abrasion resistance, and the like as compared to a machine part formed of the general sintered material. In addition, the sintered material proposed inPatent Literature 1 can be manufactured through similar steps to those in the case of the general sintered material except that raw material powder containing as a main raw material the granulated powder is used. In view of the foregoing, when a construction ofPatent Literature 1 is adopted, it is considered that a machine part having improved demand characteristics including mechanical strength and abrasion resistance can be produced with high accuracy at relatively low cost. - Patent Literature 1: JP 2011-94789 A
- However, the machine part formed of a sintered material proposed in
Patent Literature 1 is still far inferior in mechanical strength, abrasion resistance, and the like to a machine part formed of an ingot material owing to its true density ratio being set to 85% or more. Therefore, its application is inevitably limited. In addition, in the construction ofPatent Literature 1, it is essential to produce (prepare) the granulated powder of high quality in order to enable stable manufacturing (mass-production) of a desired machine part, but a lot of labor and cost are required for stably obtaining such granulated powder of high quality. Therefore, the construction ofPatent Literature 1 cannot achieve a cost reduction effect as much as expected, and the cost of the machine part may be increased instead. - In view of such circumstances, an object of the present invention is to provide a machine part formed of a sintered metal, which can be mass-produced at low cost and is excellent in mechanical strength, abrasion resistance, and the like.
- According to one embodiment of the present invention, which has been made to achieve the above-mentioned object, there is provided a machine part, comprising a sintered compact obtained by sintering a green compact of raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, the machine part including at least a hardened layer formed through heat treatment, and having a true density ratio of 97% or more and less than 100%.
- The true density ratio as used herein is represented by the calculation equation described below.
-
True density ratio=(density of entire machine part formed of sintered compact/true density)×100 [%] - It should be noted that the “true density” in the equation means a theoretical density of a material having no pores in its interior portion, such as an ingot material. In addition, the “density of entire machine part formed of sintered compact” in the equation is measured by, for example, a method specified in JIS Z2501.
- In addition, according to one embodiment of the present invention, which has been made to achieve the above-mentioned object, there is provided a method of manufacturing a machine part comprising a sintered compact having a true density ratio of 97% or more and less than 100%, the method comprising: a compression molding step of compression molding raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, in a mold to obtain a green compact; a sintering step of heating the green compact at a temperature equal to or higher than a sintering temperature of the iron-based alloy powder to obtain a sintered compact; and a heat treatment step of subjecting the sintered compact to heat treatment to form a hardened layer.
- As described above, the machine part formed of a sintered metal according to one embodiment of the present invention has a true density ratio of 97% or more and less than 100% (roughly corresponding to 7.6 g/cm3 or more and less than 7.8 g/cm3, when converted into a density), and is highly densified to the extent approximate to that in the case of an ingot material. Therefore, the machine part exhibits excellent characteristics in mechanical strength, abrasion resistance, fatigue strength, and the like.
- As a result of diligent studies, the inventors of the invention of the present application have found that such machine part formed of a sintered metal having a high density and high strength can be obtained by adopting using the sintered compact (sintered material) including a hardened layer formed through heat treatment after the sintering, and further adopting the following constructions (1) and (2) in a material aspect: (1) selectively using as main powder constituting the raw material powder the iron-based alloy powder containing molybdenum; and (2) setting the blending ratio of the carbon powder in the raw material powder to 0.1 to 0.8 mass %, which is lower than that in a general sintered metal. Specifically, the adoption of the above-mentioned construction (1) improves compression moldability and sintering property. The adoption of the above-mentioned construction (2) further improves the compression moldability along with a reduction in the blending amount of carbon having a low specific gravity, while securing lubricity between powders and heat treatment property (heat treatment property after the sintering). Thus, a high density is achieved.
- On the other hand, the use of the raw material powder containing the iron-based alloy powder as a main raw material and having an appropriate amount of carbon powder blended therein, as the raw material powder for obtaining the machine part according to one embodiment of the present invention eliminates the need for troublesome treatment such as granulation treatment proposed in
Patent Literature 1 in the process of preparing and producing the raw material powder. Therefore, the manufacturing cost can be significantly reduced as compared to the construction ofPatent Literature 1. As described above, according to one embodiment of the present invention, it is possible to obtain the machine part formed of a sintered metal, which can be mass-produced at low cost and is excellent in mechanical strength, abrasion resistance, and the like. - Herein, a method for the above-mentioned heat treatment is not particularly limited, and any known quenching method such as carburizing quenching, immersion quenching, or high-frequency quenching can be appropriately selected. It should be noted that tempering is preferably performed in combination after the quenching in order to provide the machine part with high toughness as well.
- In the above-mentioned manufacturing method according to one embodiment of the present invention, the compression molding step may comprise compression molding the raw material powder in a state in which a solid lubricant adheres to a molding surface of the mold. Further, in addition to or instead of the foregoing, the raw material powder to be used may have a solid lubricant added thereto. This improves the lubricity between the raw material powder and the mold or the lubricity between the powders, and hence provides an advantage in obtaining the green compact having a high density, and by extension, the machine part formed of a sintered metal having high strength. It should be noted that, when the raw material powder to be used has a solid lubricant added thereto, the addition amount of the solid lubricant is preferably as low as possible from the viewpoint of highly densifying the green compact. Specifically, the addition amount of the solid lubricant is preferably 0.1 mass % or less, more preferably 0.05 mass % or less in terms of outer percentage, given that the mass of the raw material powder is defined as 100%.
- When the compression molding of the raw material powder is performed in a state in which a solid lubricant adheres to a molding surface of the mold and/or the raw material powder to be used has a solid lubricant added thereto, the compression molding of the raw material powder is preferably performed in a state in which the mold is heated (preferably heated to a temperature equal to or higher than the melting point of the solid lubricant). This allows a lubricant component to diffuse and penetrate with high efficiency. Therefore, the addition amount (blending amount) of the solid lubricant can be reduced. Thus, the green compact having a high density, and by extension, the machine part having high strength can be easily obtained at low cost.
- In the machine part having the above-mentioned construction, at least a part of the hardened layer may comprise a dense layer in which a porous structure is more densified than in another area. With this, the machine part can achieve a higher density and higher strength.
- It should be noted that such machine part may be obtained by performing a plastic processing step of subjecting the sintered compact to plastic processing between the sintering step and the heat treatment step. As the plastic processing in the plastic processing step, for example, rolling can be adopted. However, the processing method to be adopted is appropriately selected depending on, for example, the shape of the machine part. Whatever processing method is adopted, cold plastic processing can efficiently improve the accuracy and density (strength) of a portion to be processed as compared to warm or hot plastic processing.
- The hardness of the machine part having the above-mentioned construction may gradually reduce from a surface to a core portion (a center portion in the thickness direction). This can provide the machine part with toughness, and hence prolong the durability lifetime of the machine part.
- In the machine part having the above-mentioned construction, as the iron-based alloy powder constituting the raw material powder, there may be used iron-based alloy powder containing 0.2 to 0.8 mass % of molybdenum, given that the mass of the raw material powder is defined as 100. In addition, as the iron-based alloy powder, there may be used iron-based alloy powder further containing 0.2 to 0.8 mass % of nickel (Ni), given that the mass of the raw material powder is defined as 100. In addition, the raw material powder may further contain chromium (Cr) powder, manganese sulfide (MnS) powder, or the like.
- The present invention described above can be preferably applied to the production of a machine part such as a gear or a cam by using a sintered metal. Needless to say, the present invention is not only applied to a gear, a cam, or the like and can also be preferably applied to the production of any other machine part (for example, a bearing) by using a sintered metal.
- As described above, according to one embodiment of the present invention, it is possible to mass-produce the machine part formed of a sintered metal exhibiting excellent characteristics in mechanical strength, abrasion resistance, and the like at low cost.
-
FIG. 1 is a perspective view of a gear as a machine part according to one embodiment of the present invention. -
FIG. 2 is an enlarged sectional view of a portion X illustrated inFIG. 1 . -
FIG. 3 is a block diagram illustrating a manufacturing procedure of the gear illustrated inFIG. 1 . -
FIG. 4 is a schematic sectional view illustrating an initial stage of a compression molding step. -
FIG. 5 is a schematic sectional view illustrating a middle stage of the compression molding step. -
FIG. 6 is an enlarged view of a main portion illustrating one embodiment of a plastic processing step. -
FIG. 7 is a view schematically illustrating a state in which the shape of a sintered compact changes along with plastic processing. -
FIG. 8 is a graph showing actually measured results of the hardness of the sintered compact before and after the plastic processing. - Embodiments of the present invention are hereinafter described with reference to the drawings.
-
FIG. 1 is a perspective view of a machine part according to one embodiment of the present invention, andFIG. 2 is an enlarged sectional view (enlarged sectional view in the plane surface perpendicular to the axis) of a portion X illustrated inFIG. 1 . The machine part illustrated inFIG. 1 is, for example, a gear (gear for a transmission) 1 to be used by being incorporated into a transmission of an automobile. Thegear 1 includes a large-diameterannular portion 3 having atooth surface 2 along its outer circumference, a small-diameter annular portion 4 having a mounting hole for mounting thegear 1 to a rotation shaft (not shown), and a plurality of connectingportions 5 for connecting the large-diameterannular portion 3 and the small-diameter annular portion 4, in an integrated manner. - The
gear 1 is formed of a sintered metal and has a true density ratio of 97% or more and less than 100%. A hardened layer (surface hardened layer) 8 is formed in the entire area of thegear 1 through heat treatment after sintering (by subjecting a sintered compact to heat treatment). In addition, as illustrated inFIG. 2 , adense layer 7 in which a porous structure is more densified than in another area is formed in the area in which thetooth surface 2 is formed (outer circumference of the large-diameter annular portion 3) in thegear 1. Thedense layer 7 is formed by subjecting the outer circumference of a sintered compact to plastic processing, and thehardened layer 8 is formed by subjecting the sintered compact after the plastic processing (after the formation of the dense layer 7) to heat treatment, while the methods of forming thedense layer 7 and thehardened layer 8 are described in detail later. That is, thehardened layer 8 is formed so as to include thedense layer 7. For such construction, thedense layer 7 has a higher hardness than thehardened layer 8. In addition, in each of theportions 3 to 5 of thegear 1, the hardness is the highest in the surface and gradually reduces toward the core portion (center portion in the thickness direction). Therefore, thetooth surface 2 has the highest mechanical strength, the highest abrasion resistance, and the like of the portions constituting thegear 1. - The
gear 1 as the machine part having the above-mentioned construction is manufactured by a raw material powder preparation step S1, a compression molding step S2, a sintering step S3, a plastic processing step S4, and a heat treatment step S5 in the stated order, as illustrated inFIG. 3 . The steps are hereinafter described in that order. - In the raw material powder preparation step S1, raw material powder 10 (see
FIG. 5 ) as a material for forming thegear 1 is prepared and produced. Herein, as theraw material powder 10, there is used raw material powder that contains as a main raw material (main powder) iron-based alloy powder containing molybdenum (Mo) and nickel (Ni) and has an appropriate amount of carbon (C) powder blended therein. As the iron-based alloy powder described above, partially alloyed powder or completely alloyed powder of molybdenum, nickel, and iron (Fe) is used. The ratios of the elements in theraw material powder 10 are as follows: 0.2 to 0.8 mass % of molybdenum, 0.2 to 0.8 mass % of nickel, and 0.1 to 0.8 mass % of carbon, with the balance being iron (and inevitable impurities), given that the mass of theraw material powder 10 is defined as 100. Herein, raw material powder in which the blending ratios of molybdenum, nickel, and carbon are each 0.5 mass %, with the balance being iron (and inevitable impurities) is used. - As the iron-based alloy powder, one having an average grain size of from 40 to 150 μm is used in consideration of cost and compression moldability. Specifically, small-size iron-based alloy powder having an average grain size of less than 40 μm is expensive, and reduces the compression moldability owing to its poor flowability. In contrast, when large-size iron-based alloy powder having an average grain size exceeding 150 μm is used, it is difficult to obtain a green compact having a high density because large pores are liable to be formed between the powders.
- One kind or two or more kinds of solid lubricants, such as zinc stearate and molybdenum disulfide, may be added (blended in terms of outer percentage) to the
raw material powder 10. In this embodiment, less than 0.05 mass % of zinc stearate is added to theraw material powder 10, given that the mass of theraw material powder 10 is defined as 100. - Next, in the compression molding step S2, the
raw material powder 10 is subjected to compression molding by using amolding device 11 as illustrated inFIGS. 4 and 5 , to provide a green compact having a shape close to that of thegear 1 illustrated inFIG. 1 (substantially finished product shape). Themolding device 11 includes, as main constituents, amold 12 having a core 13, upper andlower punches die 16, which are disposed coaxially, aheater 17 for heating the die 15 (mold 12), and alubricant injection nozzle 18 for injecting asolid lubricant 19 into acavity 12 a of themold 12. Themold 12 is set in, for example, a CNC press machine using as a drive source a servomotor (not shown). In addition, themold 12 may be equipped with a vibration imparting device for imparting vibration in order to enhance filling property of theraw material powder 10, while the illustration is omitted. - In the
molding device 11 having the above-mentioned construction, first, thesolid lubricant 19 is injected from thelubricant injection nozzle 18 arranged between the core 13 and theupper punch 14 into thecavity 12 a as illustrated inFIG. 4 . Thus, thesolid lubricant 19 is allowed to adhere to the surfaces defining thecavity 12 a (a radiallyouter surface 13 a of the core 13, an upper edge surface 15 a of thelower punch 15, and a radiallyinner surface 16 a of the die 16) (see the enlarged view inFIG. 5 ). As thesolid lubricant 19, there may be used any lubricant of the same kind as or different kind from the solid lubricant added to theraw material powder 10. In addition, there may be used not only one kind, but a mixture of two or more kinds Herein, a solid lubricant of the same kind as the solid lubricant added to theraw material powder 10, that is, zinc stearate is used as thesolid lubricant 19. - After the
solid lubricant 19 is allowed to adhere to the surfaces defining thecavity 12 a as described above, thelubricant injection nozzle 18 is moved backward and theraw material powder 10 is loaded and filled into thecavity 12 a. Next, theupper punch 14 is relatively moved so as to be close to thelower punch 15, to pressurize theraw material powder 10 filled into thecavity 12 at a pressure of, for example, from 800 to 1,100 MPa. Thus, the green compact is formed. Then, theupper punch 14 is moved upward, and concurrently thelower punch 15 is moved upward, to discharge the green compact out of thecavity 12 a (to release the green compact from the mold). - Herein, in the process for forming the green compact described above, the
heater 17 is activated to heat the die 16 (mold 12) at least a time period from the filling of theraw material powder 10 into thecavity 12 a to the completion of the formation of the green compact. Specifically, the green compact is obtained by subjecting theraw material powder 10 filled into thecavity 12 a to compression molding in the state in which themold 12 is heated. The heating of the die 16 by theheater 17 is performed so that the temperature of the die 16 is 70° C. or more, more preferably a temperature equal to or higher than the melting point of thesolid lubricant 19 and 120° C. or less. With this, a lubricant component of thesolid lubricant 19 adhering to the surfaces defining thecavity 12 a can diffuse and penetrate efficiently between the raw material powder 10 (green compact) and thecavity 12 a, further between the powders constituting theraw material powder 10. Therefore, the moldability and mold releasability of the green compact are improved even when the amount of thesolid lubricant 19 to adhere to the surfaces defining the die 12 a or the amount of the solid lubricant to be added to theraw material powder 10 is reduced. Accordingly, this provides an advantage in obtaining the green compact having a high density and high accuracy, and by extension, thegear 1 having high strength. - It should be noted that the heating of the die 16 by the
heater 17 may be performed so as to keep the die 16 in the above-mentioned temperature range at all times. In addition, while this embodiment adopts a so-called internal heating method of heating the die 16 (mold 12) by theheater 17 disposed inside thedie 16, an external heating method of heating themold 12 by the heater or the like disposed outside themold 12 may be adopted. In addition, theraw material powder 10 preliminarily heated may be filled into thecavity 12 a of themold 12. - The green compact thus obtained is transferred to the sintering step S3. In the sintering step S3, the green compact is heated at a temperature equal to or higher than the sintering temperature of the iron-based alloy powder constituting the green compact, to bind by sintering the powders adjacent to each other. Thus, a sintered compact 1′ is obtained (see
FIG. 6 ). Sintering in an active gas atmosphere such as oxygen may cause oxidation of the powder constituting the green compact and adversely affect the mechanical strength and the like of the sintered compact 1′, and by extension, of thegear 1, because the green compact is obtained through compression molding of theraw material powder 10 containing as a main raw material the iron-based alloy powder. Therefore, in the sintering step S3, the green compact is placed in an inert gas atmosphere (for example, nitrogen gas atmosphere) and heated at 1,200° C. or more and 1,300° C. or less (for example, 1,250° C.) for a predetermined time period, to provide the sintered compact 1′. The reason why the lower limit of the heating temperature is set to 1,200° C. is that, when the green compact is heated at a lower temperature (for example, 1,120° C., which is a temperature for forming a sintered compact of a general iron-based metal), the powders fail to be bound to each other with sufficient binding strength. In addition, the reason why the upper limit of the heating temperature is set to 1,300° C. is that a strength improving effect is saturated. It should be noted that the green compact may be sintered in vacuum, not in the inert gas atmosphere as described above. - The sintered compact 1′ thus obtained is transferred to the plastic processing step S4. In the plastic processing step S4, the sintered compact 1′ is subjected to plastic processing to form the
tooth surface 2 in a finished shape on the outer circumference of the sintered compact 1′. The formation of thetooth surface 2 is performed by, for example, using a rollingmachine 20 as schematically illustrated inFIG. 6 . The rollingmachine 20 includes asupport shaft 23 for supporting the sintered compact 1′ in a rotatable manner, two roller dies 21, 22 each arranged at the radially outer side of thesupport shaft 23 and having a forming portion for forming thetooth surface 2 on its outer circumference. The two roller dies 21, 22 are arranged so as to face each other across the support shaft 23 (sintered compact 1′). In such rollingmachine 20, the roller dies 21, 22 are rotated while being pressed against the outer circumference of the sintered compact 1′ supported by thesupport shaft 23 in a rotatable manner (rotated in a counterclockwise direction in the example illustrated inFIG. 6 ). With this, thetooth surface 2 in a finished shape is formed on the entire circumference of the the sintered compact 1′. It should be noted that the rolling processing described above is performed on, for example, the sintered compact 1′ including atooth surface 2′ constructed by consecutively providing tooth portions each having an involute shape (see the two-dot chain line inFIG. 7 ). In this case, the tooth portions constituting thetooth surface 2′ are each subjected to compression deformation in the circumferential direction and elongation deformation in the radial direction along with the rolling processing, to be formed into a tooth portion in a finished shape illustrated by the solid line inFIG. 7 . - In addition, along with this, the porous structure on the outer circumference of the sintered compact 1′ is densified to form the dense layer 7 (see
FIG. 2 ). When the porous structure is densified to form thedense layer 7 as described above, pores in which stress is to be concentrated are reduced, and thus, thetooth surface 2 excellent in mechanical strength, particularly in fatigue strength, is obtained. - The rolling processing (plastic processing step S4) described above may be performed in any temperature range for cold processing, warm processing, or hot processing. It should be noted that cold rolling processing is preferred from the viewpoints of improving the formation accuracy of the
tooth surface 2 and prolonging the durability lifetime of the roller dies 21, 22. - Now,
FIG. 8 shows measured results of the hardness of the sintered compact 1′ on its outer circumference before and after the plastic processing. As apparent fromFIG. 8 , the hardness of the sintered compact 1′ on its outer circumference is significantly increased after the rolling processing as compared to before the rolling processing. The hardness significantly increases particularly around the surface of the sintered compact 1′, gradually reduces therefrom to the core portion (inner portion) of the sintered compact 1′, and becomes almost constant beyond a predetermined depth. - Through the steps described above, the sintered compact 1′ having a true density ratio of 97% or more and less than 100%, herein having a true density ratio of 97% (roughly corresponding to 7.6 g/cm3 when converted into a density) is formed.
- Finally, the sintered compact 1′ having the
tooth surface 2 in a finished shape formed therein is transferred to the heat treatment step S5. In the heat treatment step S5, the sintered compact 1′ is subjected to heat treatment, to form thehardened layer 8 on the entire surface area of the sintered compact 1′ associated with quenching (seeFIG. 2 ). With this, the mechanical strength and abrasion resistance of the sintered compact 1′ are entirely increased. In particular, the mechanical strength and abrasion resistance of the area in which thedense layer 7 is formed are further increased in the sintered compact 1′. The method for the heat treatment is not particularly limited, and any known method such as carburizing quenching, immersion quenching, or high-frequency quenching can be appropriately adopted. Herein, carburizing quenching is adopted. Tempering is performed after the quenching in order to provide the sintered compact 1′ (gear 1) with high toughness as well as high mechanical strength and the like. - Through the steps described above, the
gear 1 as the machine part as illustrated inFIGS. 1 and 2 is completed. After the heat treatment step S5, with a view to further improving the accuracy of the portions of the sintered compact 1′ (gear 1), finishing processing such as grinding processing, polishing processing, lapping processing, or super finishing processing may be performed, as required. - As described above, the
gear 1 formed of a sintered metal according to the present invention has a true density ratio of 97% or more and less than 100% (roughly corresponding to 7.6 g/cm3 or more and less than 7.8 g/cm3 when converted into a density) and is highly densified to the extent approximate to that in the case of an ingot material. Therefore, thegear 1 exhibits excellent characteristics in mechanical strength, abrasion resistance, fatigue strength, and the like. - As a result of diligent studies, the inventors of the invention of the present application have realized the sintered compact 1′ having a high density and high strength by adopting the following constructions (1) and (2) particularly in a material aspect: (1) selectively using as a main raw material constituting the
raw material powder 10 the iron-based alloy powder containing molybdenum; and (2) setting the blending ratio of the carbon powder in theraw material powder 10 to from 0.1 to 0.8 mass %, which is lower than that in a general sintered metal. Specifically, the adoption of the above-mentioned construction (1) improves the compression moldability and the sintering property. The adoption of the above-mentioned construction (2) further improves the compression moldability along with a reduction in the blending amount of carbon having a low specific gravity, while securing lubricity between the powders and hardenability after sintering. Thus, a high density is achieved. - In addition, the
gear 1 according to the present invention includes thehardened layer 8 formed through the heat treatment after the sintering, and hence achieves high strength. Particularly in this embodiment, the sintered compact 1′ is subjected to carburizing, quenching, and tempering as the heat treatment, and hence the hardness of thegear 1 gradually reduces from the surface to the core portion. Therefore, thegear 1 has high toughness as well, and hence is excellent in durability lifetime and impact resistance. - On the other hand, the use of the raw material powder containing the iron-based alloy powder as a main raw material and having an appropriate amount of the carbon powder blended therein, as the
raw material powder 10 for obtaining thegear 1 eliminates the need for troublesome treatment such as granulation treatment disclosed inPatent Literature 1 in the process of preparing and producing theraw material powder 10. Therefore, manufacturing cost can be significantly reduced as compared to the construction ofPatent Literature 1. As described above, according to the present invention, it is possible to mass-produce thegear 1 formed of a sintered metal that is excellent in mechanical strength, abrasion resistance, fatigue strength, and the like and has high toughness at low cost. - The
gear 1 formed of a sintered metal and the manufacturing method therefor according to embodiments of the present invention have been described above, but the composition of theraw material powder 10 suitable for manufacturing of thegear 1 is not limited to the one described above. - For example, the
raw material powder 10 that contains as a main raw material iron based alloy powder containing molybdenum (partially alloyed powder of molybdenum-iron) and has carbon powder and chromium (Cr) powder blended therein may be used. In this case, there may be given, for example, a construction in which the powders are blended so that the contents of molybdenum, carbon, and chromium may be from 0.2 to 0.8 mass %, from 0.1 to 0.8 mass %, and from 0.5 to 2.0 mass %, respectively, and the balance may be iron (and an unavoidable impurity), given that the mass of theraw material powder 10 is defined as 100. In addition, for example, theraw material powder 10 that contains as a main raw material iron based alloy powder containing molybdenum and nickel (partially alloyed powder of molybdenum-nickel-iron) and has carbon powder and manganese sulfide (MnS) powder blended therein may also be used. In this case, there may be given, for example, a construction in which the powders are blended so that the contents of molybdenum, nickel, carbon, and manganese sulfide may be from 0.2 to 0.8 mass %, from 0.2 to 0.8 mass %, from 0.1 to 0.8 mass %, and from 0.5 to 2.0 mass %, respectively, with the balance being iron (and inevitable impurities), given that the mass of theraw material powder 10 is defined as 100. - In addition, the plastic processing step S4 may be omitted while, in the embodiment described above, the plastic processing step S4 is performed between the sintering step S3 and the heat treatment step S5, and in the plastic processing step S4, the sintered compact 1′ is formed into a finished shape and the
dense layer 7 in which a porous structure is more densified than in another area is formed. Specifically, the plastic processing step S4 can be omitted when the green compact in a finished shape can be formed through the compression molding step S2 and the sintered compact 1′ having a true density ratio of 97% or more and less than 100% can be obtained only by forming thehardened layer 8 through the heat treatment step S5. - In addition, although the case in which the present invention is applied to a gear for a transmission of an automobile has been described above, the present invention can also be applied to any other machine part such as a gear or a cam to be used by being incorporated into various mechanical devices (for example, a cam for a vane pump). In particular, the machine part according to the present invention is formed of a sintered compact highly densified to the extent approximate to that of an ingot material and can be mass-produced at low cost while securing high mechanical strength and high abrasion resistance, and hence is extremely advantageous because the machine part can be applied to such application in which replacement from a machine part formed of an ingot material has hitherto been difficult and thus contribute to reduction in cost of various mechanical devices.
-
-
- 1 gear (machine part)
- 1′ sintered compact
- 2 tooth surface
- 7 dense layer
- 8 hardened layer
- 10 raw material powder
- 12 mold
- 12 a cavity
- 17 heater
- 18 lubricant injection nozzle
- 19 solid lubricant
- 20 rolling machine
- S1 raw material powder preparation step
- S2 compression molding step
- S3 sintering step
- S4 plastic processing step
- S5 heat treatment step
Claims (12)
1. A machine part, comprising a sintered compact obtained by sintering a green compact of raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein,
the machine part including a hardened layer formed through heat treatment after the sintering, and having a true density ratio of 97% or more and less than 100%.
2. The machine part according to claim 1 , wherein at least a part of the hardened layer comprises a dense layer in which a porous structure is more densified than in another area.
3. The machine part according to claim 1 , wherein a hardness of the machine part gradually reduces from a surface to a core portion.
4. The machine part according to claim 1 , wherein the iron-based alloy powder contains 0.2 to 0.8 mass % of molybdenum, given that a mass of the raw material powder is defined as 100.
5. The machine part according to claim 1 , wherein the iron-based alloy powder further contains 0.2 to 0.8 mass % of nickel, given that a mass of the raw material powder is defined as 100.
6. A method of manufacturing a machine part comprising a sintered compact having a true density ratio of 97% or more and less than 100%, the method comprising:
a compression molding step of compression molding raw material powder that contains as a main raw material iron-based alloy powder containing molybdenum and has 0.1 to 0.8 mass % of carbon powder blended therein, in a mold to obtain a green compact;
a sintering step of heating the green compact at a temperature equal to or higher than a sintering temperature of the iron-based alloy powder to obtain a sintered compact; and
a heat treatment step of subjecting the sintered compact to heat treatment to form a hardened layer.
7. The method of manufacturing a machine part according to claim 6 , wherein the compression molding step comprises compression molding the raw material powder in a state in which a solid lubricant adheres to a molding surface of the mold.
8. The method of manufacturing a machine part according to claim 6 , wherein the raw material powder to be used has a solid lubricant added thereto.
9. The method of manufacturing a machine part according to claim 7 , wherein the compression molding of the raw material powder is performed in a state in which the mold is heated.
10. The method of manufacturing a machine part according to claim 6 , further comprising a plastic processing step of subjecting the sintered compact to plastic processing between the sintering step and the heat treatment step.
11. The method of manufacturing a machine part according to claim 10 , wherein the plastic processing comprises rolling processing.
12. The method of manufacturing a machine part according to claim 8 , wherein the compression molding of the raw material powder is performed in a state in which the mold is heated.
Applications Claiming Priority (3)
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JP2012-184184 | 2012-08-23 | ||
JP2012184184A JP5936954B2 (en) | 2012-08-23 | 2012-08-23 | Manufacturing method of machine parts |
PCT/JP2013/069857 WO2014030480A1 (en) | 2012-08-23 | 2013-07-23 | Machine part and process for producing same |
Related Parent Applications (1)
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PCT/JP2013/069857 A-371-Of-International WO2014030480A1 (en) | 2012-08-23 | 2013-07-23 | Machine part and process for producing same |
Related Child Applications (1)
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US14/878,135 Division US20160023274A1 (en) | 2012-08-23 | 2015-10-08 | Machine part and process for producing same |
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US20150217372A1 true US20150217372A1 (en) | 2015-08-06 |
Family
ID=50149792
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US14/422,892 Abandoned US20150217372A1 (en) | 2012-08-23 | 2013-07-23 | Machine part and process for producing same |
US14/878,135 Abandoned US20160023274A1 (en) | 2012-08-23 | 2015-10-08 | Machine part and process for producing same |
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US14/878,135 Abandoned US20160023274A1 (en) | 2012-08-23 | 2015-10-08 | Machine part and process for producing same |
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US (2) | US20150217372A1 (en) |
EP (1) | EP2889388B1 (en) |
JP (1) | JP5936954B2 (en) |
CN (1) | CN104540973B (en) |
WO (1) | WO2014030480A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107921535A (en) * | 2016-04-07 | 2018-04-17 | 住友电气工业株式会社 | Make the method and sintered body of sintered body |
CN112893845A (en) * | 2021-01-19 | 2021-06-04 | 上海大学 | Powder metallurgy high-precision helical gear manufacturing method |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6271310B2 (en) * | 2014-03-21 | 2018-01-31 | 株式会社豊田中央研究所 | Iron-based sintered material and method for producing the same |
DE112019007673T5 (en) * | 2019-08-30 | 2022-06-15 | Sumitomo Electric Industries, Ltd. | sintered gear |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5427600A (en) * | 1992-11-30 | 1995-06-27 | Sumitomo Electric Industries, Ltd. | Low alloy sintered steel and method of preparing the same |
US20090129964A1 (en) * | 2005-01-05 | 2009-05-21 | Stackpole Limited | Method of forming powder metal components having surface densification |
US7722803B2 (en) * | 2006-07-27 | 2010-05-25 | Pmg Indiana Corp. | High carbon surface densified sintered steel products and method of production therefor |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3362059A (en) * | 1965-12-28 | 1968-01-09 | Ford Motor Co | Gear rolling dies and method for manufacturing external tooth gears |
DE3942091C1 (en) * | 1989-12-20 | 1991-08-14 | Etablissement Supervis, Vaduz, Li | |
JPH06212368A (en) * | 1992-11-30 | 1994-08-02 | Sumitomo Electric Ind Ltd | Low alloy sintered steel excellent in fatigue strength and its production |
CA2287783C (en) * | 1998-11-05 | 2005-09-20 | Kabushiki Kaisha Kobe Seiko Sho | Method for the compaction of powders for powder metallurgy |
US6338747B1 (en) * | 2000-08-09 | 2002-01-15 | Keystone Investment Corporation | Method for producing powder metal materials |
JP3741654B2 (en) * | 2002-02-28 | 2006-02-01 | Jfeスチール株式会社 | Manufacturing method of high density iron-based forged parts |
SE0401041D0 (en) * | 2004-04-21 | 2004-04-21 | Hoeganaes Ab | Sintered metal parts and method of manufacturing thereof |
DE112005000921B4 (en) * | 2004-04-23 | 2013-08-01 | Kabushiki Kaisha Toyota Chuo Kenkyusho | A process for producing an iron-based sintered alloy and an iron-based sintered alloy element |
JP2007262536A (en) * | 2006-03-29 | 2007-10-11 | Hitachi Powdered Metals Co Ltd | Sintered gear and its production method |
US7905018B2 (en) * | 2006-03-29 | 2011-03-15 | Hitachi Powdered Metals Co., Ltd. | Production method for sintered gear |
JP2009120918A (en) * | 2007-11-16 | 2009-06-04 | Sumitomo Denko Shoketsu Gokin Kk | Method for producing sintered component |
JP5113555B2 (en) * | 2008-02-28 | 2013-01-09 | 株式会社豊田中央研究所 | Iron-based sintered alloy and method for producing the same |
JP5363081B2 (en) * | 2008-11-28 | 2013-12-11 | 住友電気工業株式会社 | Metallurgical powder, dust core, metallurgical powder manufacturing method and dust core manufacturing method |
JP5955498B2 (en) | 2009-09-29 | 2016-07-20 | Ntn株式会社 | Manufacturing method of power transmission parts |
JP6087042B2 (en) * | 2010-09-30 | 2017-03-01 | 日立化成株式会社 | Method for manufacturing sintered member |
-
2012
- 2012-08-23 JP JP2012184184A patent/JP5936954B2/en not_active Expired - Fee Related
-
2013
- 2013-07-23 CN CN201380041680.5A patent/CN104540973B/en not_active Expired - Fee Related
- 2013-07-23 WO PCT/JP2013/069857 patent/WO2014030480A1/en active Application Filing
- 2013-07-23 US US14/422,892 patent/US20150217372A1/en not_active Abandoned
- 2013-07-23 EP EP13830532.1A patent/EP2889388B1/en not_active Not-in-force
-
2015
- 2015-10-08 US US14/878,135 patent/US20160023274A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5427600A (en) * | 1992-11-30 | 1995-06-27 | Sumitomo Electric Industries, Ltd. | Low alloy sintered steel and method of preparing the same |
US20090129964A1 (en) * | 2005-01-05 | 2009-05-21 | Stackpole Limited | Method of forming powder metal components having surface densification |
US7722803B2 (en) * | 2006-07-27 | 2010-05-25 | Pmg Indiana Corp. | High carbon surface densified sintered steel products and method of production therefor |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107921535A (en) * | 2016-04-07 | 2018-04-17 | 住友电气工业株式会社 | Make the method and sintered body of sintered body |
CN112893845A (en) * | 2021-01-19 | 2021-06-04 | 上海大学 | Powder metallurgy high-precision helical gear manufacturing method |
Also Published As
Publication number | Publication date |
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WO2014030480A1 (en) | 2014-02-27 |
EP2889388B1 (en) | 2019-04-03 |
EP2889388A4 (en) | 2016-07-13 |
JP5936954B2 (en) | 2016-06-22 |
CN104540973A (en) | 2015-04-22 |
JP2014040646A (en) | 2014-03-06 |
CN104540973B (en) | 2018-01-12 |
EP2889388A1 (en) | 2015-07-01 |
US20160023274A1 (en) | 2016-01-28 |
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