US20240254610A1 - Hot-Formed Steel Part and Manufacturing Method - Google Patents
Hot-Formed Steel Part and Manufacturing Method Download PDFInfo
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- US20240254610A1 US20240254610A1 US18/565,931 US202218565931A US2024254610A1 US 20240254610 A1 US20240254610 A1 US 20240254610A1 US 202218565931 A US202218565931 A US 202218565931A US 2024254610 A1 US2024254610 A1 US 2024254610A1
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 61
- 239000010959 steel Substances 0.000 title claims abstract description 61
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 239000000203 mixture Substances 0.000 claims abstract description 55
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 39
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 27
- 229910001562 pearlite Inorganic materials 0.000 claims abstract description 24
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 9
- 150000001247 metal acetylides Chemical class 0.000 claims abstract description 9
- 229910001563 bainite Inorganic materials 0.000 claims description 45
- 238000001816 cooling Methods 0.000 claims description 42
- 239000011572 manganese Substances 0.000 claims description 35
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 30
- 229910052750 molybdenum Inorganic materials 0.000 claims description 22
- 239000010936 titanium Substances 0.000 claims description 18
- 229910052720 vanadium Inorganic materials 0.000 claims description 17
- 239000011265 semifinished product Substances 0.000 claims description 16
- 229910052799 carbon Inorganic materials 0.000 claims description 15
- 229910052748 manganese Inorganic materials 0.000 claims description 15
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 14
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 12
- 239000011733 molybdenum Substances 0.000 claims description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 11
- 239000010949 copper Substances 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 10
- 229910052759 nickel Inorganic materials 0.000 claims description 9
- 238000003754 machining Methods 0.000 claims description 8
- 238000004381 surface treatment Methods 0.000 claims description 8
- 239000000047 product Substances 0.000 claims description 7
- 230000006698 induction Effects 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 238000005496 tempering Methods 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010703 silicon Substances 0.000 claims description 3
- 238000005482 strain hardening Methods 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 2
- 238000007792 addition Methods 0.000 description 26
- 230000015572 biosynthetic process Effects 0.000 description 16
- 238000010438 heat treatment Methods 0.000 description 14
- 229910052804 chromium Inorganic materials 0.000 description 13
- 230000000694 effects Effects 0.000 description 12
- 230000009466 transformation Effects 0.000 description 12
- 239000000243 solution Substances 0.000 description 8
- 229910052796 boron Inorganic materials 0.000 description 7
- 229910001021 Ferroalloy Inorganic materials 0.000 description 6
- 238000011161 development Methods 0.000 description 6
- 239000010955 niobium Substances 0.000 description 6
- 229910052757 nitrogen Inorganic materials 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 5
- 230000007613 environmental effect Effects 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000005242 forging Methods 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 230000001965 increasing effect Effects 0.000 description 3
- 229910001338 liquidmetal Inorganic materials 0.000 description 3
- 239000002244 precipitate Substances 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 230000000717 retained effect Effects 0.000 description 3
- 229910000628 Ferrovanadium Inorganic materials 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000009931 harmful effect Effects 0.000 description 2
- 230000016507 interphase Effects 0.000 description 2
- PNXOJQQRXBVKEX-UHFFFAOYSA-N iron vanadium Chemical compound [V].[Fe] PNXOJQQRXBVKEX-UHFFFAOYSA-N 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910052716 thallium Inorganic materials 0.000 description 2
- 229910001309 Ferromolybdenum Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 238000000844 transformation Methods 0.000 description 1
- 238000009489 vacuum treatment Methods 0.000 description 1
Classifications
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- 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
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- 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
- C21D1/06—Surface hardening
- C21D1/09—Surface hardening by direct application of electrical or wave energy; by particle radiation
- C21D1/10—Surface hardening by direct application of electrical or wave energy; by particle radiation by electric induction
-
- 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
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
- C21D1/20—Isothermal quenching, e.g. bainitic hardening
-
- 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
- C21D1/26—Methods of annealing
- C21D1/30—Stress-relieving
-
- 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
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
- C21D7/04—Modifying the physical properties of iron or steel by deformation by cold working of the surface
- C21D7/08—Modifying the physical properties of iron or steel by deformation by cold working of the surface by burnishing or the like
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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
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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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
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
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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
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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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
- C22C38/002—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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- 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
- C22C38/00—Ferrous alloys, e.g. steel alloys
- 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
- 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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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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
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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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
- C21D2211/001—Austenite
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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
- 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
- C21D2211/005—Ferrite
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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
- C21D2211/008—Martensite
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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
- C21D2211/009—Pearlite
Definitions
- the present invention relates to the use of a steel of determined composition for the manufacture of a mechanical part the mechanical features of which are obtained by natural cooling after a hot forming step (rolling, forging, etc.)
- Some mechanical parts such as crankshafts, wishbones, etc. require mechanical strengths on the order of 850-1000 MPa.
- Such requirements explain the use of micro-alloyed ferritic-pearlitic grades such as 38MnVS6.
- Such grades which are described by the standard DIN EN 10267, use the phenomenon of interphase precipitation in vanadium in order to obtain mechanical features superior to the mechanical features of conventional ferritic-pearlitic steels.
- Such grades are used for obtaining, without any heat treatment after hot forming, the mechanical strengths mentioned hereinabove.
- the grades are relatively easy to implement (the mechanical properties are obtained without any subsequent heat treatment), said grades have become widely established since the 1990's.
- the document SEW 605-Ed1 presents a representative overview of the development of bainitic grades in the field of long products. As shown upon reading said document, most of the detailed grades claim mechanical properties which are significantly higher than 950 MPa or even 1050 MPa. For this purpose, such grades use not only relatively high Mn and Cr concentrations, but also significant additions of Mo, Si and V, for all of the grades.
- EP 1 780 293 A2 presents a hot-formed bainitic-martensitic steel, and which is used for obtaining high mechanical features without any heat treatment (examples of mechanical strength at 1180 MPa are given).
- WO 2005/100618 presents a steel with an acicular ferrite structure (i.e., in theory, bainite formed intragranularly) used for obtaining, without any heat treatment, a mechanical strength of about 1150 MPa according to the examples.
- WO 2009/138586 A2 relates to a steel with a bainitic structure making it possible to obtain a mechanical strength of at least 1100 MPa without any heat treatment.
- WO 2016/151345 A1 is similar to the preceding example in that same describes a grade having a predominantly bainitic microstructure (70 to 100%) and having a mechanical strength higher than 1100 MPa in all the examples. The same applies to the WO 2019/180563 A1.
- Document EP 3061838A1 concerns a grade with a predominantly bainitic structure (minimum 60% bainite) having a mechanical strength higher than 1150 MPa.
- SEW 605-Ed1 suggests that, from the point of view of mechanical features, some of the proposed solutions might nevertheless be suitable. Such is the case for grades called 27MnCr6-3, and to a lesser extent 37Mn7 and 37MnCr4-3. Indeed, all such grades are likely to have mechanical strengths on the level of the mechanical strength of the 38MnVS6 (taken herein because the most used grade amongst the grades of NF EN 10267). However, the detail of the chemical compositions shows that for all said grades, the additions of V are needed. Such solutions are thus also not likely to answer the existing problems of a grade having a mechanical strength between 850 and 1000 MPa without any heat treatment and without a significant use of vanadium (or other critical ferroalloys).
- vanadium just like molybdenum (which has the same disadvantages in terms of cost), has the particularity of greatly slowing down the formation of ferrite-pearlite without, however, influencing the kinetics of bainite formation. It is thus understandable that same are used for bainitic grades, especially when it is sought to limit the additions of Mn and Cr as is imposed by the present problems.
- the invention can now be described in detail, the goal of which is namely to propose a new grade of steel making little or no use of ferroalloys the costs of which are fluctuating (V, Mo, NB, Ti), and to be used for obtaining a predominantly bainitic microstructure for parts with typical dimensions (thickness or diameter) of 20-100 mm, by natural cooling after rolling or hot forging, said parts having to have a mechanical strength comprised between 850 and 1000 MPa.
- bainite or bainite ferrite sometimes referred to as acicular ferrite or intragranular bainite are not considered distinct from the microstructure claimed for the steels of the invention, and that bainite should be understood in general, thus to the exclusion of ferrite-pearlite, Widmanstaetten ferrite, or martensite.
- the subject matter of the invention is a hot-formed steel part, characterized in that the composition of the steel, in percentages by weight, consists of:
- the mixture of bainite ferrite and carbides or residual austenite forms bainite, bainite including the morphologies of bainite or bainite ferrite called acicular ferrite or intragranular bainite.
- the residual austenite fraction is less than or equal to 5%.
- the steel part according to the invention preferentially has one or a plurality of the following features, taken alone or in combination:
- a further subject matter of the invention is a manufacturing method for a steel part, characterized in that:
- the method according to the invention can comprise one or a plurality of the following features, taken individually or in combination:
- the part concerned could be, but is not limited to, a crankshaft or an injection rail.
- composition ranges for the various elements of the invention will now be justified. As already mentioned, all concentrations are given in weight percentages.
- the concentration of carbon is comprised between 0.22 and 0.35%.
- Low carbon concentrations can be favorable to the rapid formation of bainite, and this point has been the subject matter of a specific patent (WO2011124851-A2); however, low carbon concentrations also facilitate the formation of pro-eutectoid ferrite. In the absence of vanadium in particular, such ferrite has a particularly low hardness and can be a preferred initiation site for fatigue failures.
- the low carbon concentrations also lead to the need for large quantities of ferroalloys, in order to maintain the mechanical properties. A low limit of 0.22% was thus retained, significantly more than many so-called bainitic grades, which favor concentrations on the order of 0.16-0.20%.
- the concentration of carbon is strictly higher than 0.25% and better higher than 0.26%.
- too high carbon concentrations lead to a significant slowdown of bainitic transformation while enhancing the formation of pearlite (which is not sought).
- alloying elements such as molybdenum or vanadium, which strongly slow down the transformation into ferrite-pearlite without affecting the kinetics of the bainitic transformation.
- An upper limit of 0.35% was thus retained, so as not to have to resort, in return, to the use of such elements.
- the choice of the preferred range makes it possible to avoid more definitely the absence of ferrite (for the low limit) and martensite (for the high limit).
- the carbon concentration is less than or equal to 0.30%.
- the concentration of Mn is comprised between 0.50 and 1.7%, preferentially greater than or equal to 1.10% and/or less than or equal to 1.70%.
- Mn is used, together with Cr, for controlling the parameter Bs, an indicator of the temperature at which bainite formation begins during continuous cooling.
- an addition of Mn lowers the parameter Bs. If the effect on Bs can be obtained for relatively low concentrations (0.50%), it is also preferable to avoid too high concentrations (>1.70%) which lead to problems of excessive segregation and to a too great lowering of the parameter Bs.
- the concentration of Cr is comprised [between] 0.50 and 1.70%.
- Cr is used in the same way as Mn for the purpose of controlling the parameter Bs. Same can be used as such for substituting a variably significant part of the manganese.
- a minimum concentration of 0.50% is required so as to guarantee that the microstructure of the invention is obtained, and a maximum concentration of 1.70% is imposed for limiting segregation phenomena and the cost of the grade.
- the concentration of Mo is comprised between traces and 0.15% and preferentially between traces and 0.10%.
- the well-established role of Mo has already been mentioned as slowing down the ferritic-pearlitic transformation, a particularly favorable role for obtaining a bainitic microstructure.
- the additions of Mo are, in the present invention, limited to 0.15% or even to 0.10%. This latter concentration can be reached by the mere presence of residues in the scrap that is possibly used so that such concentration is not necessarily a deliberate addition.
- the concentration of Mo is strictly less than 0.10%.
- the concentration of Si is comprised between traces and 0.40%, preferentially between traces and 0.35%.
- the concentration of Si is less than or equal to 0.25%, preferentially less than or equal to 0.15%.
- TRIP Transformation Induced Plasticity
- Such effect is generally observed for additions on the order of 1.2 to 1.5% for isothermal transformations.
- document EP 0787 812 B1 specifically mentions that silicon has no stabilizing effect on residual austenite below 0.8%.
- the aforementioned TRIP effect is not desirable, since TRIP implies a mechanical strength in excess of the target (850-1000 MPa); it is thus a question of guaranteeing the absence thereof or of greatly limiting the TRIP effect.
- the inventors were able to show that the views on the role of Si were erroneous, and that, within the range of claimed compositions and on components of typical dimensions of automotive parts, Si could contribute to the presence of residual austenite starting from 0.40% and even, in some cases, starting at 0.35%.
- the Si concentration has thus been deliberately limited to such values, the preferential concentration guaranteeing the result with greater certainty.
- Ni is comprised between traces and 0.50%, preferentially between traces and 0.35%.
- Nickel may be present only by being fed into the raw materials as a residual element, in which case Ni concentration will naturally be limited to 0.35%. The latter could be increased to 0.50% but additions in excess of said limit are prohibited for the same reasons as the additions of Mo and V (cost and fluctuation of the costs of ferroalloys, environmental impact).
- the concentration of Cu is comprised between traces and 0.50%, preferentially between traces and 0.30%. Just like Ni and a small amount of Mo, Cu can be present exclusively by being fed into the raw materials, as a residual element. Additions are thus not required, but the concentration thereof is limited to 0.50%, better to 0.30% in order to avoid any difficulties of hot forming.
- the concentration of V is comprised between traces and 0.08%, and preferentially between traces and 0.05%.
- vanadium can be oxidized during the elaboration from scrap, so that a concentration of less than 0.015% is always conceivable.
- modest additions can be made for improving the hardenability and the strength to tempering, without however exceeding 0.08%, and preferentially 0.05%, in order to minimize the consequences on the cost and the variability of the cost of the grade.
- Al is comprised between traces and 0.10% and preferentially between traces and 0.05%. Al is optionally added to deoxidize the steel. Additions are capped at 0.10% in order to limit the risk of formation of re-oxidation inclusions by contact of the liquid metal with air. Such limitation will be all the more effective if the preference interval is satisfied.
- B is comprised between 0.001 and 0.010% and preferentially between 0.001 and 0.006%.
- Boron is a powerful retarder of the formation of pro-eutectoid ferrite that is indispensable to the invention. It is well known to a person skilled in the art that the addition of boron in very small quantities leads to obtaining a pronounced effect, but a reproducible effect requires a minimum concentration of 0.001% (10 ppm). Moreover, in order to prevent the formation of boron precipitates and the harmful effects thereof, the additions are limited to 0.010%. The absence of the precipitates will be guaranteed with greater certainty by limiting to additions of less than 0.006%.
- Ti is comprised between 0.01 and 0.06%. Titanium is indispensable for fixing the nitrogen that is inevitably present during the elaboration and thereby allowing the boron to remain in solid solution.
- the inventors have established that, under the conditions of implementation of the invention, a concentration on the order of 0.01% could be sufficient. On the other hand, a concentration of more than 0.06% is not necessary from the point of view of the sought for effect and can also lead to the formation of precipitates harmful to the lifetime under fatigue. Additions beyond said limit are also not desirable for cost reasons.
- a minimum of Ti is imposed with respect to the N concentration (Ti % ⁇ 2.5 N %), in order to guarantee the effectiveness of the protection of B.
- Nb is comprised between traces and 0.05%.
- niobium can be added for improving the hardenability and/or for refining the austenitic grain at high temperature.
- the additions are limited to 0.05% for reasons similar to the reasons mentioned for Ti.
- the concentration will be limited to 0.02%.
- S is comprised between traces and 0.15%.
- sulfur can be added for improving the machinability of the grade, concentrations between 0.05 and 0.15% are then imparted thereto.
- the composition can comprise additions of Ca up to 0.010%, and/or Te up to 0.030%, and/or Se up to 0.050% and/or Bi up to 0.050% and/or Pb up to 0.100%.
- P is comprised between traces and 0.100%.
- the presence of P will be limited to 0.030% if it is sought to limit the consequences of the embrittling effect thereof.
- concentrations greater than or equal to 0.030% either because ductility is not a sought for property, or even because brittleness is wanted (case of breakable connecting rods).
- concentration will remain limited to 0.100%, beyond which the elaboration and rolling difficulties are significant.
- N is comprised between traces and 0.013%, preferentially between traces and 0.010%. Although inevitably present, nitrogen should be limited in order to maintain the effectiveness of boron additions. To this end, a maximum concentration of 0.013% is imposed, noting that a limit of 0.010% will improve the guarantee of obtaining the result.
- the other elements present in the steel of the invention are iron, and impurities resulting from the elaboration, present in usual concentrations taking into account the raw materials used and the mode of elaboration of the liquid steel (use of a converter or an electric arc furnace for obtaining the liquid metal, vacuum or non-vacuum treatment of liquid metal, etc.).
- the parameter Bs estimating the temperature at which bainite begins to form during cooling, should also be comprised between 540 and 600° C.
- the parameter or “bainitic transformation start temperature” Bs is defined by the following formula:
- C %, Mn %, Cr %, Mo % and Ni % denote the concentrations of C, Mn, Cr, Mo and Ni, respectively, in the steel composition, expressed as percentages by weight.
- the inventors go against the stream of the approach which chooses said parameter to be mainly bounded by a higher value, and as low as possible.
- the parameter Bs according to the invention makes it possible to form bainite at high temperature during cooling, so that a coarse bainite structure is obtained.
- bainite has a lower mechanical strength than in the steels according to the prior art mentioned hereinabove.
- a minimum value of 540° C. is needed for preventing a too high mechanical strength.
- concentrations of C, Mn and Cr corresponding to values greater than 600° C. are not compatible with obtaining the sought for microstructure.
- the parameter Bs is greater than 560° C., better still greater than 570° C.
- microstructure of the steel consists of, in surface fractions:
- bainite is in the form of a matrix of bainite ferrite strips or plates, between which carbides and/or austenite are present.
- bainite in particular bainite ferrite, is formed during cooling, as soon as the temperature becomes lower than the start temperature Bs for bainite transformation.
- bainite due to the high value of BS, bainite is formed at relatively high temperature.
- bainite has a coarse structure, making it possible to limit the mechanical strength to at most 1000 MPa.
- the residual austenite fraction has to be less than or equal to 10%, preferentially less than or equal to 5%. Indeed, as described hereinabove, the presence of residual austenite in the microstructure leads in particular to a higher mechanical strength. A residual austenite fraction greater than 10% would lead to a mechanical strength in excess of the target (850-1000 MPa). A high residual austenite fraction is thus detrimental to achieving the goal of the present invention. A residual austenite fraction less than or equal to 5% is thus preferred.
- the structure can include martensite, pro-eutectoid ferrite and/or pearlite, but the sum of the fractions of the constituents has to remain at most 30% and the sum of the fractions of pro-eutectoid ferrite and pearlite at most 10% in order to achieve the sought for mechanical features.
- the part is produced by a hot-forming, in austenitic phase, of a steel semi-finished product with the composition described hereinabove.
- the semi-finished product is e.g. a billet or a bar.
- the semi-finished product before hot-forming, is subjected to initial forming by machining or cold forming.
- the hot-forming is e.g. a hot forging or a hot rolling.
- Hot-forming is carried out in the austenitic phase (typically between 1100 and 1250° C.).
- Cooling is carried out, e.g. with still air, forced air, under a hood or in a container, depending on the sought for cooling rate.
- the sought for mechanical features are obtained without the use of any heat treatments after the hot-forming, nor any very restrictive particular control of the rate of cooling which can be carried out naturally in still air.
- the cooling rate between 750° C. and 550° C. is preferentially greater than or equal to 0.15° C./s, in order to prevent or limit the formation of ferrite and pearlite, which are likely to form in said temperature range.
- the cooling rate between 550° C. and 250° C. is comprised between 0.1 and 0.5° C./s. Indeed, given the parameter Bs according to the invention, bainitic ferrite is formed in said temperature range. The cooling rate should not be too high, in order to maximize bainite formation in said temperature range.
- the phase transformation is generally completed, so that the cooling rate is between 0.1° C./s and 100° C./s.
- an adaptation of the cooling can be used in certain cases, in particular due to the diameter of the parts.
- parts of large dimensions in particular with an equivalent diameter greater than or equal to 120 mm (i.e. such that the natural cooling rate of the parts is less than or equal to the cooling rate of a bar with a diameter of 120 mm)
- still air cooling could lead to too slow cooling, especially at the core of the parts, and lead to the occurrence of ferrite and/or pearlite in too large quantities.
- forced air cooling can be used in order to obtain a sufficient cooling rate.
- cooling can be implemented under a hood or in a container, in order to reduce the cooling rate.
- a shaping is carried out by cold machining or cold deformation, in order to obtain the part, in particular in order to obtain the precise dimensions and surface features of the final part.
- a surface treatment of the surface of the part is carried out by high-frequency induction in order to impart to same the benefits of such technique (increase in hardness, residual compression stresses, etc.).
- the surface treatment is generally carried out on a specific portion of the part.
- tempering can be carried out for adjusting the hardness of the treated zones of the part.
- a portion of the part is mechanically reinforced by a method such as roller burnishing, autofretting, or other methods aimed at obtaining local work hardening as well as residual compressive stresses in the part to be reinforced.
- the part is subjected to a deposition of a coating, e.g. by electrogalvanization or a deposition of paint, as well as, if appropriate, to heat treatments required by such a deposition.
- a deposition of a coating e.g. by electrogalvanization or a deposition of paint, as well as, if appropriate, to heat treatments required by such a deposition.
- Alt1 steel has a microstructure and tensile strength in accordance as expected, but with carbon and molybdenum concentrations not according to the invention.
- the use of molybdenum in significant quantities is prohibited, in order to limit the use of the corresponding ferroalloys.
- the comparison with Alt2 illustrates well the reason for the limitations on the concentration of carbon. Indeed, Alt2, for which the Mo concentration has been reduced compared to Alt1, has a microstructure which is not as per the requirements of the invention, with in particular ⁇ 25% pearlite. Such result clearly illustrates the difficulty of preventing the formation of said constituent without the use of molybdenum in excess of 0.2%.
- Alt3 steel has a non-conforming parameter Bs, with conforming microstructure and Si concentration.
- Bs non-conforming parameter
- the Alt4 and Alt5 steels have compositions very close to the compositions of the invention, with the exception of the Si concentration which is in excess of the maximum imposed by the invention.
- a mechanical strength significantly greater than the targeted mechanical strength (850-1000 MPa) results therefrom.
- Alt6 steel conforms at many points with the exception of the addition of Ti and B.
- Alt7 steel is also close to the steels of the invention but has a parameter Bs significantly lower than the parameter required, resulting in a mechanical strength much higher than the target.
- Inv1 up to Inv 4 steels all have a structure consisting of at least 70% of a mixture of bainitic ferrite and carbides or residual austenite in surface fractions, the residual austenite fraction being less than or equal to 5%, at most 30% of martensite and/or pro-eutectoid ferrite and/or pearlite, the pro-eutectoid ferrite and/or pearlite fraction being less than or equal to 10%.
- the molybdenum concentrations correspond to the concentrations which can be obtained by the mere presence of molybdenum as a residual element in the scrap used for the production.
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Application Number | Priority Date | Filing Date | Title |
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FR2105812A FR3123659A1 (fr) | 2021-06-02 | 2021-06-02 | Pièce en acier mise en forme à chaud et procédé de fabrication |
FRFR2105812 | 2021-06-02 | ||
PCT/EP2022/064945 WO2022253912A1 (fr) | 2021-06-02 | 2022-06-01 | Pièce en acier mise en forme à chaud et procédé de fabrication |
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US20240254610A1 true US20240254610A1 (en) | 2024-08-01 |
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US18/565,931 Pending US20240254610A1 (en) | 2021-06-02 | 2022-06-01 | Hot-Formed Steel Part and Manufacturing Method |
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US (1) | US20240254610A1 (fr) |
EP (1) | EP4347903A1 (fr) |
KR (1) | KR20240018573A (fr) |
BR (1) | BR112023025290A2 (fr) |
FR (1) | FR3123659A1 (fr) |
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Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
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FR2744733B1 (fr) * | 1996-02-08 | 1998-04-24 | Ascometal Sa | Acier pour la fabrication de piece forgee et procede de fabrication d'une piece forgee |
JPH11350074A (ja) * | 1998-04-07 | 1999-12-21 | Nippon Steel Corp | ガス圧接性に優れたベイナイト系レール |
FR2867785B3 (fr) | 2004-03-18 | 2006-02-17 | Ispat Unimetal | Piece mecanique de taille moyenne ou petite issue de la forge ou de la frappe |
DE102005052069B4 (de) | 2005-10-28 | 2015-07-09 | Saarstahl Ag | Verfahren zum Herstellen von Vormaterial aus Stahl durch Warmverformen |
FR2931166B1 (fr) | 2008-05-15 | 2010-12-31 | Arcelormittal Gandrange | Acier pour forge a chaud a hautes caracteristiques mecaniques des pieces produites |
FR2958660B1 (fr) | 2010-04-07 | 2013-07-19 | Ascometal Sa | Acier pour pieces mecaniques a hautes caracteristiques et son procede de fabrication. |
EP3061837A1 (fr) | 2015-02-27 | 2016-08-31 | Swiss Steel AG | Produit longitudinal bainitique nu et son procédé de fabrication |
WO2016151345A1 (fr) | 2015-03-23 | 2016-09-29 | Arcelormittal | Pieces a structure bainitique a hautes proprietes de resistance et procede de fabrication |
FR3064282B1 (fr) * | 2017-03-23 | 2021-12-31 | Asco Ind | Acier, procede pour la fabrication de pieces mecaniques en cet acier, et pieces ainsi fabriquees |
WO2019180492A1 (fr) | 2018-03-23 | 2019-09-26 | Arcelormittal | Pièce forgée en acier bainitique et son procédé de fabrication |
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- 2022-06-01 EP EP22731603.1A patent/EP4347903A1/fr active Pending
- 2022-06-01 US US18/565,931 patent/US20240254610A1/en active Pending
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EP4347903A1 (fr) | 2024-04-10 |
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