WO2023109106A1 - 一种短流程贝氏体热作模具及其制备方法 - Google Patents
一种短流程贝氏体热作模具及其制备方法 Download PDFInfo
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- WO2023109106A1 WO2023109106A1 PCT/CN2022/105085 CN2022105085W WO2023109106A1 WO 2023109106 A1 WO2023109106 A1 WO 2023109106A1 CN 2022105085 W CN2022105085 W CN 2022105085W WO 2023109106 A1 WO2023109106 A1 WO 2023109106A1
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- mold
- bainite
- nitriding
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- 229910001563 bainite Inorganic materials 0.000 title claims abstract description 70
- 238000000034 method Methods 0.000 title claims abstract description 57
- 238000002360 preparation method Methods 0.000 title claims abstract description 28
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 57
- 239000010959 steel Substances 0.000 claims abstract description 57
- 239000000463 material Substances 0.000 claims abstract description 47
- 238000011282 treatment Methods 0.000 claims abstract description 34
- 238000005496 tempering Methods 0.000 claims abstract description 32
- 238000003754 machining Methods 0.000 claims abstract description 29
- 238000005242 forging Methods 0.000 claims abstract description 28
- 238000001816 cooling Methods 0.000 claims abstract description 21
- 238000000137 annealing Methods 0.000 claims abstract description 16
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 9
- 239000012535 impurity Substances 0.000 claims abstract description 8
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 4
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 4
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 3
- 238000005121 nitriding Methods 0.000 claims description 66
- 239000000203 mixture Substances 0.000 claims description 17
- 238000005728 strengthening Methods 0.000 claims description 15
- 230000000694 effects Effects 0.000 claims description 10
- 229910045601 alloy Inorganic materials 0.000 claims description 8
- 239000000956 alloy Substances 0.000 claims description 8
- 238000010002 mechanical finishing Methods 0.000 claims description 8
- 238000010274 multidirectional forging Methods 0.000 claims description 7
- 238000005266 casting Methods 0.000 claims description 6
- 239000002994 raw material Substances 0.000 claims description 6
- 238000003723 Smelting Methods 0.000 claims description 5
- 238000013461 design Methods 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 16
- 238000010791 quenching Methods 0.000 abstract description 8
- 230000000171 quenching effect Effects 0.000 abstract description 7
- 238000005265 energy consumption Methods 0.000 abstract description 4
- 230000002708 enhancing effect Effects 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 description 19
- 239000010410 layer Substances 0.000 description 18
- 150000001875 compounds Chemical class 0.000 description 8
- 230000000052 comparative effect Effects 0.000 description 6
- 229910052717 sulfur Inorganic materials 0.000 description 5
- 239000011162 core material Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- VZSRBBMJRBPUNF-UHFFFAOYSA-N 2-(2,3-dihydro-1H-inden-2-ylamino)-N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]pyrimidine-5-carboxamide Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C(=O)NCCC(N1CC2=C(CC1)NN=N2)=O VZSRBBMJRBPUNF-UHFFFAOYSA-N 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 238000003917 TEM image Methods 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000007788 roughening Methods 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/24—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass dies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/84—Controlled slow cooling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D11/00—Process control or regulation for heat treatments
- C21D11/005—Process control or regulation for heat treatments for cooling
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/007—Heat treatment of ferrous alloys containing Co
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/04—Making ferrous alloys by melting
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- C—CHEMISTRY; METALLURGY
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- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- 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
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C—CHEMISTRY; METALLURGY
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- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
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- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
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- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/02—Pretreatment of the material to be coated
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/36—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases using ionised gases, e.g. ionitriding
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/36—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases using ionised gases, e.g. ionitriding
- C23C8/38—Treatment of ferrous surfaces
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/80—After-treatment
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F17/00—Multi-step processes for surface treatment of metallic material involving at least one process provided for in class C23 and at least one process covered by subclass C21D or C22F or class C25
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/24—Nitriding
- C23C8/26—Nitriding of ferrous surfaces
Definitions
- the present invention provides a short-flow bainite hot-working mold and its preparation method, which solves the problems of long manufacturing cycle of the current hot-working mold, many heat treatment processes, serious time-consuming and energy-consuming problems, etc. technical problem.
- the preparation steps of the hot work mold are as follows:
- the cooling rate of the material after forging is controlled between 0.5-3°C/s to obtain a mold material with a bainite structure, and its hardness is 390- 450HV30 hardness range; at the same time, due to the characteristics of material composition, it has the ability of secondary strengthening of bainite tempering.
- the surface nitriding treatment is to nitriding the mold insert with precise dimensions at 520-600°C, the thickness of the nitriding layer is 110-150 ⁇ m, and the thickness of the white layer is 3- 8 ⁇ m. At this point, the hardness of the mold insert surface increases to 820-920HV 0.3 .
- the mold insert is mechanically finished after the first tempering to obtain a mold insert with accurate dimensions, the second tempering is omitted, and the second tempering heat treatment is combined with the nitriding heat treatment, by This omits an energy-consuming heat treatment process.
- the method for preparing the bainite hot-working mold of the present invention is as follows:
- the forging conditions are as follows: heat the die steel billet to 1050-1150°C for 6-10h, carry out multi-directional forging, control the final forging temperature ⁇ 980°C, and control the cooling at a cooling rate of 0.5-3°C/s after forging to obtain Bainian Body tissue mold blank.
- the hardness of the mold blank with bainite structure is 390-450HV30, and it can be directly used for mechanical rough machining without special annealing and softening treatment.
- due to the characteristics of material composition it has the ability of secondary strengthening of bainite tempering.
- the short-flow bainite hot working die of this embodiment is composed of the following elements by mass percentage: C: 0.55%; Si: 0.22%; Mn: 1.30%; W: 2.50%; Mo: 4.50%; V: 0.80% ; Co: 0.90%; RE: 0.05%, P: 0.01%, S: 0.01%, and the rest are Fe and unavoidable impurities.
- Comparing Example 1 with Comparative Example 1 it can be seen that the technical solution of the present invention, after omitting one-step forging and annealing and softening, one-step high-temperature quenching and hardening, and one-step secondary tempering treatment, the performance of the mold insert material and the effect of long-process processing Quite, in terms of heart hardness, it is even slightly better. After omitting the above-mentioned process, the preparation cycle of the hot work mold can be significantly reduced, energy consumption can be reduced, and production cost can be reduced.
- Example 1 Comparing Example 1 with Comparative Example 2, it can be seen that after changing the alloy composition of the mold steel, if the mold insert is still prepared according to the mold preparation process of Example 1 of the present invention, the technical effect of Example 1 cannot be obtained (Example 1 1.
- the core hardness is 50.5HRC
- the impact toughness value Ak is 106J
- the surface hardness is increased to 910HV 0.3 ). This shows that the unique die steel alloy composition of the present invention provides a precondition for omitting process steps.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Heat Treatment Of Articles (AREA)
- Forging (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
Abstract
一种短流程贝氏体热作模具的制备方法,包括:设计模具钢成分为:C:0.50-0.60%,Si:0.20-0.25%,Mn:1.00-1.50%,W:2.10-3.00%,Mo:3.50-5.00%,V:0.50-1.00%,Co:0.60-1.10%,P≤0.02%,RE:0.01-0.10%,[RE]/[S]>3.0,[RE]×[S]<0.004%,余量为Fe和不可避免的杂质。通过对模具钢成分设计和调整,锻造和控冷后的贝氏体组织模具钢材料硬度较低,可直接机粗加工,而锻造及机粗加工后经一次回火处理,使模具钢材料贝氏体发生二次强化效应,此时的模具钢兼具优良的硬度、耐磨性和韧性,具有极佳的综合力学性能。短流程贝氏体热作模具的制备方法省略了现有技术中机械粗加工之间的退火软化和机械粗加工后的淬火硬化工序,缩短热作模具的生产周期,降低了能耗和生产成本。还提供了一种短流程贝氏体热作模具。
Description
本发明涉及模具制造技术领域,尤其涉及一种短流程贝氏体热作模具及其制备方法。
模具工业作为制造业的基石,在现代工业发展过程中起着非常重要的作用。模具钢,特别是热作模具钢,在工业制造领域中具有非常广泛的应用,如热锻模具、压铸模具和热作模具等。
传统的热作模具从模具材料制造到成品模具往往需要十几道的生产流程。如:模具材料冶炼-铸造-退火处理-锻造-锻造退火-模具机加工(粗加工)-模具热处理-模具精加工-模具渗氮处理等。
在模具的制造过程中,模具要经过多次的加热及冷却热处理进行材料组织调控,以满足机加工和生产过程中对于材料性能的要求,如材料硬度等。在模具材料何模具的制备过程中,材料需要进行多次热处理,包括锻后软化退火、淬火硬化、软化回火、表面强化热处理工艺等。具体地,如模具材料锻造后进行长时间的球化退火处理降低硬度以便进行机加工(硬度太大无法机加工)。机加工后还需要进行淬火硬化和回火处理,以得到良好的综合力学性能。在进行多次回火并进过精加工后还需进行表面强化热处理工艺等。由此可见,目前的热作模具制造周期长,热处理工序多,耗时耗能严重。
发明内容
(一)要解决的技术问题
鉴于现有技术的上述缺点、不足,本发明提供一种短流程贝氏体热作模具及其制备方法,其解决了目前热作模具制造周期长,热处理工序 多,耗时和耗能严重等技术问题。
(二)技术方案
为了达到上述目的,本发明采用的主要技术方案包括:
第一方面,本发明提供一种短流程贝氏体热作模具的制备方法,其包括:
设计模具钢成分为(按质量百分比计):C:0.50-0.60%,Si:0.20-0.25%,Mn:1.00-1.50%,W:2.10-3.00%,Mo:3.50-5.00%,V:0.50-1.00%,Co:0.60-1.10%,P≤0.02%,RE:0.01-0.10%,[RE]/[S]>3.0,[RE]×[S]<0.004%,余量为Fe和不可避免的杂质;
所述热作模具的制备步骤如下:
S1、按照模具钢成分称量合金原料,经冶炼、铸造、退火,得到模具钢坯料;
S2、将模具钢坯料锻造,得到贝氏体组织模具钢材料;
S3、机械粗加工,制成模具镶块;
S4、回火处理,通过贝氏体二次强化作用得到硬化后的贝氏体模具镶块;
S5、机械精加工,得到尺寸精确的模具镶块;
S6、表面渗氮处理;
S7、组装模具镶块,制得成品模具。
根据本发明的较佳实施例,其中,S2中,将所述模具钢坯料加热到1050-1150℃保温6-10h,进行多向锻造,控制终锻温度≥980℃,锻造后以0.5-3℃/s的冷速控制冷却,得到贝氏体组织模具坯料。此时,贝氏体组织模具坯料的硬度小于450HV30,无需进行专门的退火软化处理,即可直接用于机械粗加工,在粗加工时保留加工尺寸余量。
其中,通过模具材料多向锻造后并控制终锻温度≥980℃,控制锻后材料的冷却速度在0.5-3℃/s之间,得到具有贝氏体组织的模具材料,其硬度在390-450HV30硬度区间;同时,由于材料成分特点而具备贝氏体 回火二次强化的能力。
根据本发明的较佳实施例,S4中,回火处理温度控制在540-680℃,回火2-3次,每次回火时间2.0-6.0小时,优选回火2次、每次2.5小时,使贝氏体组织模具镶块材料产生强烈的二次强化效应,得到兼具高硬度、韧性以及耐磨性好的贝氏体模具镶块,此时,模具镶块的硬度提高至49-51HRC硬度范围,满足冲压模具的硬度要求。
根据本发明的较佳实施例,S6中,所述表面渗氮处理是将尺寸精确的模具镶块在520-600℃下渗氮,渗氮层厚度为110-150μm,白亮层厚度为3-8μm。此时,模具镶块表面的硬度提高至820-920HV
0.3。
根据本发明的较佳实施例,S6中,所述表面渗氮处理是采用表面等离子渗氮工艺。
根据本发明的较佳实施例,S6中,所述表面等离子渗氮工艺的条件为:电压:910-980V;气氛比值:NH
3:Ar=1:7;炉压:200-280Pa;渗氮温度:520℃-600℃;渗氮时间:5h-9h。
第二方面,本发明提供一种短流程贝氏体热作模具,其采用上述任一实施例的制备方法制得。
(三)有益效果
(1)通过本发明设计的模具钢成分,在经过锻造后控冷可得到贝氏体组织,该贝氏体组织的模具钢材料无需经过“锻后退火降低硬度”的处理,直接适于机械粗加工。因此可省略掉在机械粗加工之前的“退火软化”处理。
(2)本发明设计的模具钢成分,具有贝氏体回火二次硬化效应,能够在S4的回火温度下产生强烈的二次强化效应,达到提升材料硬度和耐磨性的作用。也就是说,机械粗加工后的高温淬火硬化热处理的目标可在S4的中低温回火处理过程中一并实现。因此,本发明在机械粗加工后S4的回火处理步骤之前,省略掉专门的“高温淬火硬化热处理”的工序。
(3)、本发明在一次回火后便对模具镶块进行机械精加工处理,以 得到尺寸精确的模具镶块,省略第二次回火,将第二次回火热处理与渗氮热处理合并,由此省略一步耗能的热处理工序。
尽管本发明相对现有热作模具的制备流程省略至少三步工序(一次锻后退火降低硬度工序、一次高温淬火硬化工序、第二次回火处理工序),但本发明制备的热作模具仍然具有优异的性能:硬度为49-51HRC,冲击韧性值Ak为106J以上,渗氮后表面维氏硬度达到820HV
0.3以上,尤其适合作为热冲压成型的模具。本发明的一种短流程贝氏体热作模具的制备方法,相比传统的长流程奥氏体模具制作流程,本发明制作的热作模具有热传导性能好,耐磨性能高,抗高温黏着性能好等特点,同时模具材料制造周期短,工序短,耗能少、成本低的等优点。
此外,本发明制备的热作模具能有效的防止模具表面的拉毛,经表面等离子渗氮后更能大大延长模具的使用寿命。模具磨损后,经修模和再此等离子渗氮即可重新投入使用,从而大大地提高热作模具的总使用寿命。
图1为本发明中短流程贝氏体热作模具的制备方法流程图。
图2为本发明实施例1中锻造后的贝氏体组织模具钢材料的SEM图。
图3为本发明实施例1中锻造后的贝氏体组织模具钢材料的CCT曲线。
图4为本发明实施例1中经机械粗加工后,回火二次强化后得到的贝氏体模具钢的TEM图。
图5为本发明实施例1中经表面等离子渗氮工艺处理后的材料组织金相图。
图6为现有技术中长流程奥氏体热作模具的制备方法流程图。
为了更好的解释本发明,以便于理解,下面结合附图,通过具体实 施方式,对本发明作详细描述。
本发明的短流程贝氏体热作模具,钢成分为:C:0.50-0.60%,Si:0.20-0.25%,Mn:1.00-1.50%,W:2.10-3.00%,Mo:3.50-5.00%,V:0.50-1.00%,Co:0.60-1.10%,P≤0.02%,RE:0.01-0.10%,[RE]/[S]>3.0,[RE]×[S]<0.004%,余量为Fe和不可避免的杂质。
制备流程参见图1所示,依次为:模具材料冶炼→铸造成坯→铸造后退火→锻造→模具机械粗加工→第一次回火处理→机械精加工→表面渗氮处理→组装成品模具。与图6比较可知,图6中虚线框所表示的工序为本发明相对现有技术的省略工序。
具体地,按照上述模具钢的成分设计,制备本发明的贝氏体热作模具的方法如下:
(1)、按照模具钢成分称量合金原料,经冶炼、铸造、退火,得到模具钢坯料。这一步处理按常规操作进行。
(2)、将模具钢坯料锻造,得到贝氏体组织模具钢材料。锻造条件为:将模具钢坯料加热到1050-1150℃保温6-10h,进行多向锻造,控制终锻温度≥980℃,锻造后以0.5-3℃/s的冷速控制冷却,得到贝氏体组织模具坯料。此时,贝氏体组织模具坯料的硬度为390-450HV30,无需进行专门的退火软化处理,即可直接用于机械粗加工。同时,由于材料成分特点而具备贝氏体回火二次强化的能力。
(3)、机械粗加工,制成模具镶块。在粗加工时保留加工尺寸余量。
(4)、回火处理,通过贝氏体二次强化作用得到硬化后的贝氏体模具镶块。在回火过程中,温度控制在540-680℃,回火2-3次,每次回火时间2.0-6.0小时,使贝氏体组织模具镶块材料产生强烈的二次强化效应,得到兼具高硬度、韧性以及耐磨性好的贝氏体模具镶块,此时,模具镶块的硬度提高至49-51HRC硬度范围,满足冲压模具的硬度要求。
(5)、机械精加工,得到尺寸精确的模具镶块。
(6)、表面渗氮处理。采用表面等离子渗氮工艺,在520-600℃下 渗氮,渗氮层厚度为110-150μm,白亮层厚度为3-8μm。渗氮条件为:电压:910-980V;气氛比值:NH
3:Ar=1:7;炉压:200-280Pa;渗氮温度:520℃-600℃;渗氮时间:5h-9h。
渗氮工艺处理后,模具镶块表面的硬度提高至820-920HV
0.3。
(7)组装模具镶块,制得成品模具。
相对于现有技术,本发明提供的贝氏体模具钢,通过以上化学元素成份的配比设计和调整,尤其是碳和合金元素的配比量,获得了锻造后控冷可产生二次强化效应的贝氏体模具钢,经锻造和机粗加工后,进行一次回火,即使模具钢材料贝氏体发生二次强化效应,此时的模具钢兼具优良的硬度、耐磨性和韧性,具有极佳的综合力学性能。利用这一特性,省略了现有技术中机械粗加工之间的退火软化处理和机械粗加工后的淬火硬化处理。
在上述技术方案的基础上,进一步地,将机械精加工前的第二回火处理工序和精加工后的表面渗氮工序合并到一个处理工序中,在该处理工序中,同时实现回火以提高模具镶块材料韧性和渗氮提高材料表面硬度两个目的,从而减少工序,缩短现有热作模具的制备流程,降低生产周期和能耗。
以下结合本发明的具体实施例,说明本发明的方案及技术效果。
实施例1
本实施例的短流程贝氏体热作模具,由以下质量百分比的元素组成:C:0.50%;Si:0.20%;Mn:1.00%;W:2.10%;Mo:3.50%;V:0.50%;Co:0.60%;RE:0.01%,P:0.01%,S:0.003%,其余为Fe和不可避免杂质。所述贝氏体热作模具制备步骤如下:
(1)、按照模具钢成分称量合金原料,经1400℃电炉熔炼后浇筑成钢锭,再经电渣重熔后在700℃保温8小时进行退火,得到模具钢坯料。
(2)、将模具钢坯料加热到1150℃保温8小时后,进行多向锻造,控制终锻温度为990℃,并将锻造后的材料在热处理炉中控冷以1℃/s的 冷速控制冷却到室温,得到贝氏体组织模具钢材料,硬度为405HV30。
(3)、机械粗加工,制成贝氏体组织模具镶块。对此时具有全贝氏体组织的模具钢镶块的扫描电镜图如图2所示:此时材料组织为回火贝氏体组织,其中贝氏体碳化物以颗粒状为主。贝氏体模具钢的CCT曲线如图3所示,为新型模具材料的连续冷却转变曲线,在冷速为0.5-10℃/s冷却时,得到贝氏体为主要组织的模具材料。
(4)、将贝氏体组织模具镶块在620℃保温2h回火处理,得到二次强化后的贝氏体模具镶块,硬度为49.5HRC,冲击韧性值Ak为118J,满足冲压模具的硬度要求。经过二次强化后的贝氏体模具钢的透射电镜如图4所示,回火后的材料组织为由高密度位错和细小的碳化物组成,使材料具备良好的性能,如硬度和耐磨性。
(5)、机械精加工,得到尺寸精确的模具镶块。
(6)、表面渗氮处理。采用表面等离子渗氮工艺,在600℃下渗氮,渗氮条件为:电压:920V;气氛比值:NH
3:Ar=1:7;炉压:240Pa,渗氮时间:5h。渗氮层厚度为118μm,模具表面化合物白亮层厚度为5μm。渗氮工艺处理后,模具镶块表面的硬度提高至890HV
0.3。图5所示,为本实施例的模具镶块经表面等离子渗氮工艺处理后的材料组织金相图。由图中可以看出,经渗氮处理后材料表层被一层连续且厚度均匀的化合物层所覆盖,此化合物层硬度可达900HV
0.3左右,能够有效抵抗高温黏着磨损的发生,亚表层是深度为120μm扩散层组织,其由Fe
3N和Fe
4N等化合物及回火贝氏体组织组成,其硬度由亚表层向内呈递减趋势,可以为表层组织提供有效的支撑作用,提高耐高温的性能。
(7)拼装模具镶块,得到热作模具,该模具尤适于用于热冲压模具。
实施例2
本实施例的短流程贝氏体热作模具,由以下质量百分比的元素组成:C:0.55%;Si:0.22%;Mn:1.30%;W:2.50%;Mo:4.50%;V:0.80%;Co:0.90%;RE:0.05%,P:0.01%,S:0.01%,其余为Fe和不可避免杂 质。
所述贝氏体热作模具制备步骤如下:
(1)、按照模具钢成分称量合金原料,经1400℃电炉熔炼后浇筑成钢锭,再经电渣重熔后在700℃保温8小时进行退火,得到模具钢坯料。
(2)、将模具钢坯料加热到1150℃保温8小时后,进行多向锻造,控制终锻温度为1010℃,并将锻造后的材料在热处理炉中控冷以2℃/s的冷速控制冷却到室温,得到贝氏体组织模具钢材料,硬度为425HV30。
(3)、机械粗加工,制成贝氏体组织模具镶块。
(4)、将贝氏体组织模具镶块在580℃保温2h(回火处理),得到二次强化后的贝氏体模具镶块,硬度为50.5HRC,冲击韧性值Ak为106J,满足冲压模具的硬度要求。
(5)、机械精加工,得到尺寸精确的模具镶块。
(6)、表面渗氮处理。采用表面等离子渗氮工艺,在560℃下渗氮,渗氮条件为:电压:950V;气氛比值:NH
3:Ar=1:7;炉压:260Pa,渗氮时间:6h。渗氮层厚度为136μm,模具表面化合物白亮层厚度为4.85μm。渗氮工艺处理后,模具镶块表面的硬度提高至910HV
0.3。
(7)拼装模具镶块,得到热冲压模具。
实施例3
本实施例的短流程贝氏体热作模具,由以下质量百分比的元素组成:C:0.60%;Si:0.20%;Mn:1.50%;W:3.00%;Mo:5.0%;V:1.00%;Co:1.10%;RE:0.07%,P:0.01%,S:0.02%,其余为Fe和不可避免杂质。
所述贝氏体热作模具制备步骤如下:
(1)、按照模具钢成分称量合金原料,经1400℃电炉熔炼后浇筑成钢锭,再经电渣重熔后在700℃保温8小时进行退火,得到模具钢坯料。
(2)、将模具钢坯料加热到1050℃保温8小时后,进行多向锻造,控制终锻温度为1000℃,并将锻造后的材料在热处理炉中控冷以2.5℃/s 的冷速控制冷却到室温,得到贝氏体组织模具钢材料,硬度为436HV30。
(3)、机械粗加工,制成贝氏体组织模具镶块。
(4)、将贝氏体组织模具镶块在540℃保温3.5h(回火处理),得到二次强化后的贝氏体模具镶块,硬度为51HRC,冲击韧性值Ak为123J,满足冲压模具的硬度要求。
(5)、机械精加工,得到尺寸精确的模具镶块。
(6)、表面渗氮处理。采用表面等离子渗氮工艺,在520℃下渗氮,渗氮条件为:电压:980V;气氛比值:NH
3:Ar=1:7;炉压:280Pa,渗氮时间:7h。渗氮层厚度为133μm,模具表面化合物白亮层厚度为5.2μm。渗氮工艺处理后,模具镶块表面的硬度提高至928HV
0.3。
(7)拼装模具镶块,得到热冲压模具。
对比例1
本对比例的短流程贝氏体热作模具,由以下质量百分比的元素组成:C:0.50%;Si:0.20%;Mn:1.00%;W:2.10%;Mo:3.50%;V:0.50%;Co:0.60%;RE:0.01%,P:0.01%,S:0.003%,其余为Fe和不可避免杂质。所述热作模具的制备方法按照图6所示的长流程处理,并按照实施例1相同的表面渗氮条件进行渗氮。渗氮结束后,模具镶块性能为:心部材料硬度为49.3HRC,冲击韧性值Ak为115J,渗氮层厚度为118μm,模具表面化合物白亮层厚度为5μm。渗氮工艺处理后,模具镶块表面的硬度提高至870HV
0.3。
将实施例1与对比例1相比可知,本发明的技术方案,在省略一步锻造后退火软化,一步高温淬火硬化、一步二次回火处理后,模具镶块材料的性能与长流程处理的效果相当,心部硬度方面,甚至略显更优。而省略前述工序后,可明显减少热作模具的制备周期、减少能耗和降低生产成本。
对比例2
本对比例的短流程贝氏体热作模具,改变模具钢的成分为:C:0.40%; Si:0.90%;Mn:0.50%;Cr:4.60%;Mo:1.20%;V:0.80%;RE:0.01%,P:0.01%,S:0.003%。按照实施例1的贝氏体热作模具制备步骤进行制备,渗氮结束后得到的模具镶块性能为:心部材料硬度为45.2HRC,冲击韧性值Ak为105J,渗氮层厚度为118μm,模具表面化合物白亮层厚度为3μm。渗氮工艺处理后,模具镶块表面的硬度提高至790HV
0.3。
将实施例1与对比例2相比可知,在改变模具钢的合金组成后,若仍按照本发明实施例1的模具制备流程制备模具镶块,并不能获得实施例1的技术效果(实施例1,心部硬度为50.5HRC、冲击韧性值Ak为106J、表面的硬度提高至910HV
0.3)。这说明,本发明独特的模具钢合金组成,为省略工艺步骤提供了前提条件。
此外,将本发明实施例1-3制备的热作模具,与现有的奥氏体热冲压模具的性能相比较可知,本发明制作的模具与现有奥氏体热冲压模具具备相当的综合力学性能。由此可见,本发明的新型贝氏体模具材料在短流程制备工艺处理后,可以得到与传统制备流程工艺相似的综合性能,但在制备时间和制造成本上具有明显的优势。
最后应说明的是:以上各实施例仅用以说明本发明的技术方案,而非对其限制;尽管参照前述各实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分或者全部技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的范围。
Claims (7)
- 一种短流程贝氏体热作模具的制备方法,其特征在于,其包括:设计模具钢成分为:C:0.50-0.60%,Si:0.20-0.25%,Mn:1.00-1.50%,W:2.10-3.00%,Mo:3.50-5.00%,V:0.50-1.00%,Co:0.60-1.10%,P≤0.02%,RE:0.01-0.10%,[RE]/[S]>3.0,[RE]×[S]<0.004%,余量为Fe和不可避免的杂质;所述热作模具的制备步骤如下:S1、按照模具钢成分称量合金原料,经冶炼、铸造、退火,得到模具钢坯料;S2、将模具钢坯料锻造,得到贝氏体组织模具钢材料;S3、机械粗加工,制成模具镶块;S4、回火处理,通过贝氏体二次强化作用得到硬化后的贝氏体模具镶块;S5、机械精加工,得到尺寸精确的模具镶块;S6、表面渗氮处理;S7、组装模具镶块,制得成品模具。
- 根据权利要求1所述的制备方法,其特征在于,S2中,将所述模具钢坯料加热到1050-1150℃保温6-10h,进行多向锻造,控制终锻温度≥980℃,锻造后以0.5-3℃/s的冷速控制冷却,得到贝氏体组织模具坯料。
- 根据权利要求1所述的制备方法,其特征在于,S4中,回火处理温度控制在540-680℃,回火2-3次,每次回火时间2.0-6.0小时,使贝氏体组织模具镶块材料产生强烈的二次强化效应。
- 根据权利要求1所述的制备方法,其特征在于,S6中,所述表面渗氮处理是将尺寸精确的模具镶块在520-600℃下渗氮,渗氮层厚度为110-150μm,白亮层厚度为3-8μm。
- 根据权利要求1所述的制备方法,其特征在于,S6中,所述表面渗氮处理是采用表面等离子渗氮工艺。
- 根据权利要求5所述的制备方法,其特征在于,S6中,所述表面 等离子渗氮工艺的条件为:电压:910-980V;气氛比值:NH 3:Ar=1:7;炉压:200-280Pa;渗氮温度:520℃-600℃;渗氮时间:5h-9h。
- 一种短流程贝氏体热作模具,其特征在于,是采用上权利要求1-6任一项所述的制备方法制得。
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