[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

WO2022263887A1 - Method for producing a steel part and steel part - Google Patents

Method for producing a steel part and steel part Download PDF

Info

Publication number
WO2022263887A1
WO2022263887A1 PCT/IB2021/055331 IB2021055331W WO2022263887A1 WO 2022263887 A1 WO2022263887 A1 WO 2022263887A1 IB 2021055331 W IB2021055331 W IB 2021055331W WO 2022263887 A1 WO2022263887 A1 WO 2022263887A1
Authority
WO
WIPO (PCT)
Prior art keywords
steel
temperature
steel part
semi
cold
Prior art date
Application number
PCT/IB2021/055331
Other languages
French (fr)
Inventor
Marion FROTEY
Bernard Resiak
Original Assignee
Arcelormittal
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Arcelormittal filed Critical Arcelormittal
Priority to CN202180099057.XA priority Critical patent/CN117441033A/en
Priority to MX2023014918A priority patent/MX2023014918A/en
Priority to EP21734517.2A priority patent/EP4355920A1/en
Priority to PCT/IB2021/055331 priority patent/WO2022263887A1/en
Priority to KR1020237042447A priority patent/KR20240007218A/en
Priority to BR112023024874A priority patent/BR112023024874A2/en
Priority to JP2023577646A priority patent/JP2024524929A/en
Priority to US18/568,929 priority patent/US20240301528A1/en
Priority to CA3220321A priority patent/CA3220321A1/en
Publication of WO2022263887A1 publication Critical patent/WO2022263887A1/en

Links

Classifications

    • 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
    • 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
    • C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • C21D9/525—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length for wire, for rods
    • 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
    • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • 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
    • 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
    • C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
    • 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
    • C21D6/005—Heat treatment of ferrous alloys containing Mn
    • 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
    • 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
    • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
    • 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
    • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0273—Final recrystallisation annealing
    • 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
    • C21D8/06—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires
    • 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
    • C21D8/06—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires
    • C21D8/065—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires of ferrous alloys
    • 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
    • C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • 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
    • 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
    • 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
    • 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
    • C22C38/04—Ferrous alloys, e.g. steel alloys containing 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
    • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
    • 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
    • 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
    • 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
    • C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
    • 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
    • C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/05—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
    • C23C22/06—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6
    • C23C22/07—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 containing phosphates
    • 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
    • C21D2211/00—Microstructure comprising significant phases
    • C21D2211/001—Austenite
    • 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
    • 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
    • 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
    • C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
    • C21D8/0436—Cold rolling
    • 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
    • C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • C21D8/0463—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment following hot rolling
    • 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
    • C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • C21D8/0473—Final recrystallisation annealing

Definitions

  • the present invention relates to a method for manufacturing through cold forming, in particular via cold heading, assembly parts, such as screws, bolts, etc., that the automotive industry commonly uses for chassis or wheel hub components of vehicles.
  • WO201 6/158470 is Age hardening steel excellent in machinability before aging treatment and excellent in fatigue characteristics, toughness, and low cycle fatigue characteristics after aging treatment, that is, age hardening steel containing predetermined amounts of C, Si, Mn, S, Cr, Al, V, Nb, Ca, and REM, limiting contents of P, Ti, and N to predetermined amounts or less, having a balance of Fe and impurities, having an area ratio of bainite structures of 70% or more. But the steel of WO2016/158470 lacks hydrogen embrittlement.
  • WO201 1/124851 is a mechanical steel part in steel with high characteristics, characterized in that its composition, comprising in weight percentages, is wherein the contents of C, Mn and Cr are such that (830-270C %-90 Mn %-70Cr %) the remainder of the steel part being iron and impurities resulting from processing, and wherein the in that its structure of the steel is bainitic and contains no more than a total of 20% of martensite and/or pro-eutectoid ferrite and/or pearlite. But the steel of WO2011/124851 is not demonstrate hydrogen embrittlement as well as reduction area of 58% or more.
  • an aim of the invention is to provide a steel part which may be used as an assembly part for a motor vehicle, and which has improved resistance to hydrogen embrittlement while simultaneously having :
  • the steel part shows a hardness from 360Hv to 405Hv.
  • the steel part according to the invention has a composition comprising, by weight: 0.05% ⁇ C ⁇ 0.15%
  • Carbon is present in the steel of present invention from 0.05% to 0.15%. Carbon imparts strength to the steel by solid solution strengthening and carbon is gammagenous hence delays the formation of Ferrite. Carbon is the element that impacts the formation of Cementite-free Lath-Like Bainite. A minimum of 0.05% of carbon is required to reach a tensile strength of 1100 MPa but if carbon is present above 0.15%, carbon deteriorates ductility as well as machinability of the final product due to the formation of cementite.
  • the carbon content is advantageously in the range 0.08% to 0.14% to obtain simultaneously high strength and high ductility and more preferably from 0.09% to 0.14%.
  • Silicon is present in the steel of present invention from 0.01% to 1%. Silicon imparts the steel of present invention with strength through solid solution strengthening. In particular, at the above-mentioned contents, the silicon has the effect of hardening the bainite microstructure through solid solution hardening. Silicon reduces the formation of cementite nucleation as silicon hinders precipitation and diffusion-controlled growth of carbides by forming a Si-enriched layer around precipitate nuclei. Therefore, resulting the cementite-free lath-like bainite. Silicon also acts as a deoxidizer. A minimum of 0.01% of silicon is required to impart strength to the steel of present invention.
  • An amount of more than 1 % raises the activity of carbon in austenite promoting its transformation into pro- eutectoid ferrite, which can deteriorate the strength, and also resulting retardation for formation of bainite under continuous cooling thereby too much retained austenite at the end of cooling.
  • the preferred limit for Silicon from 0.01 to 0.9% and more preferably from 0.01% to 0.5%
  • Manganese is added in the present steel from 1.2% to 2%.
  • Manganese provides hardenability to the steel. It allows to decrease the critical cooling rate for which a bainitic transformation can be obtained in continuous cooling without any prior transformation and the manganese lowers the bainite start temperature of the steel, and therefore results in a refinement of the bainitic structure to form lath bainite and thus increases the mechanical properties of the part.
  • a minimum content of 1.2% by weight is necessary to obtain the desired bainitic microstructure.
  • manganese has a negative effect on the steel of present invention as retained austenite can transform into MA islands or fresh martensite and these phases are detrimental for the properties.
  • manganese forms sulphides such as MnS.
  • the preferred limit of manganese is from 1.3% to 1.9 % and more preferably from 1.4% to 1 .9%.
  • Chromium is present from 0.1% to 2% in the steel of present invention. Chromium is an indispensable element in order to produce bainitic structure, especially lath bainite and impart Elongation and ductility to the steel of present invention. Addition of Chromium promotes homogeneous and finer bainitic microstructure during the temperature range between Bs and room temperature. A minimum content of 0.1% of Chromium is required to produce the targeted bainitic microstructure and chromium also slows down the softening during the tempering treatment, allowing higher holding temperatures which favors degassing but also the formation of carbides that trap hydrogen. But the presence of Chromium content of 2% or more excessively increases the hardness of the steel, it makes it difficult to form it by cold forming, and in particular cold heading. It is advantageous to have Chromium from 0.2% to 1 .6% and more preferably from 0.3% to 1 .4%.
  • the steel aluminum is at a content from 0.001% to 0.1 wt%.
  • Aluminum is a deoxidizer of the steel in the liquid state. It then contributes, in the form of nitrides, to controlling austenitic grain coarsening during hot rolling. On the other hand, present in too large an amount, it may lead to a coarsening of aluminate type inclusions in the steel which may prove damaging to the properties of the steel, especially its toughness.
  • the aluminum content may be comprised at a content from 0.001 to 0.09 wt%.
  • the nitrogen content is comprised from 0% to 0.01 wt%. Nitrogen traps boron via the formation of boron nitrides, which makes the role of this element in the hardenability of the steel ineffective. Therefore, in the steel according to the invention, the nitrogen content is limited to 0.01 wt%. Nevertheless, added in small amounts, it makes it possible, via the formation in particular of titanium nitrides (TiN) and aluminum nitrides (AIN), to avoid excessive austenitic grain coarsening during heat treatments undergone by the steel. Similarly, it also allows, in this case, the formation of carbonitride precipitates that will contribute toward the trapping of hydrogen. Therefore, in the steel according to the invention, the nitrogen content is greater than or equal to 0.003 wt%.
  • the steel according to the invention comprises at most 0.015 wt% of phosphorus and at most 0.015 wt% of sulfur.
  • the effect of phosphorus and sulfur are particularly harmful in the steels according to the invention, for several reasons. Indeed, since these elements are poisons for hydrogen recombination, they contribute to a higher concentration of atomic hydrogen capable of penetrating into the material, therefore to an increased risk of delayed fracture of the part in use. Moreover, by segregating at the grain boundaries, the phosphorus and the sulfur reduce the cohesion thereof. Their content must therefore be kept very low. For this purpose, measures must be taken to ensure that the steel is dephosphorized and desulfurized during its melting in the liquid state.
  • the steel may optionally contains from 0.01 to 1wt% of nickel. This element provides an increase in the strength of the steel and has beneficial effects on the resistance to brittle fracture. It also improves, in a known manner, the corrosion resistance of the steel.
  • Boron is an optional element and can be present in the alloy at contents from 0.0003 to 0.01 wt%.
  • boron By segregating at the prior austenitic grain boundaries, boron, even at very low contents, strengthens the grains boundaries, and makes it possible to increase the resistance to hydrogen-induced delayed fracture.
  • the boron increases the cohesion of the grain boundary via its intrinsic effect, but also by making phosphorus segregation more difficult at these grain boundaries.
  • the boron further strongly increases the hardenability of the steel and thus makes it possible to limit the carbon content needed to obtain the desired bainitic microstructure.
  • boron acts in synergy with molybdenum and niobium, thus increasing the effectiveness of these elements and their own influence that their respective contents permit. An excess of boron (above 0.01 wt%) would however lead to the formation of brittle iron boro-carbides.
  • the molybdenum is an optional element and is comprised from 0.003 to 1 wt%. Molybdenum interacts strongly with phosphorus and limits the damaging effect of the phosphorus by limiting its segregation at the prior austenite grain boundaries. Furthermore, it displays a marked carbide-forming behavior. For given mechanical properties, it allows higher holding tempering temperature, which, as a result, favor the development of carbides that will be hydrogen traps. It is therefore an element that increases the resistance to delayed fracture.
  • Titanium is an optional element and present in the alloy at contents comprised from 0.01 to 0.04 wt%. Titanium is added to the liquid steel in order to increase the hardness of the material. Flere, within the ranges indicated, it also increases the delayed fracture resistance in several ways. It contributes to austenitic grain refinement and forms precipitates that trap hydrogen. Finally, the hardening effect of the titanium makes it possible to carry out tempering operations at higher holding temperatures. The maximum titanium content is set here in order to avoid obtaining precipitates of too large a size which would then degrade the resistance of the steel to delayed fracture.
  • the steel of present invention can optionally contain niobium at contents comprised from 0.01 to 0.1 wt%.
  • Niobium improves the hydrogen resistance, as it can on the one hand limit the formation of borocarbides Fe 3 (C,B) ; Fe 23 (C,B) 26 which consume, and therefore, lower the “free” boron content available for segregation at the grain boundaries, and, on the other hand, limits the austenitic grain growth by forming carbonitrides.
  • the refinement of grains results in a higher total length of grain boundaries, and therefore in a better distribution of harmful elements, such as phosphorous and sulfur, in lower concentration.
  • a decrease in austenitic grain size results in an acceleration of the kinetics of the bainitic transformation.
  • niobium content is set in order to avoid obtaining precipitates of too large size which would then degrade the resistance of the steel to delayed fracture. Furthermore, when it is added in too large amount, niobium leads to an increased risk of “crack” defects at the surface of the billets and blooms as continually cast. These defects, if they cannot be completely eliminated, may prove very damaging in respect of the integrity of the properties of the final part, especially as regards fatigue strength and hydrogen resistance. This is why the niobium content is kept below 0.1 wt%.
  • the steel may comprise vanadium at a content lower than or equal to 0.5 wt%.
  • vanadium makes it possible to carry out tempering operations at higher temperatures.
  • the maximum vanadium content is set to avoid obtaining precipitates of too large size which might degrade the resistance of the steel to delayed hydrogen fracture.
  • the vanadium content may be comprised at a content from 0.05 to 0.5 wt%.
  • the rest of the composition is iron and unavoidable impurities, in particular resulting from the elaboration.
  • composition of the steel part consists of the above-mentioned elements.
  • the steel part according to the invention is more particularly a cold formed steel part, and more particularly a cold headed steel part.
  • the steel part has a microstructure comprising, in surface fractions or area%, of at least 80% bainite, and a cumulative presence of Residual Austenite and martensite from 1 % to 25%.
  • Bainite is present in the steel according to the invention as a matrix phase and imparts strength to such steel. Bainite is present in the steel at least 80% by area fraction and preferably from 80% to 95% by area fraction and more preferably from 85% to 95%. Bainite is formed during quenching.
  • Such bainite may include Cementite-Free Lath-Like Bainite and Lower bainite.
  • the cementite- free Lath-Like bainite is consisting of bainite in the form of laths and including, between these laths, carbides such that the number N of inter-lath carbides larger than 0.1 micrometers per unit of surface area is less than or equal to 50000/mm 2 .
  • This cementite-free lath-like bainite structure confers to the steel of present invention a good resistance against hydrogen.
  • the lower bainite is consisting of bainite in the form of laths and including, fine iron carbides sticks which are precipitated inside the laths.
  • the lower bainite structure provide the steel of present invention with elongation and tensile strength.
  • the lath structure of both Lower bainite and cementite free lath like bainite allow for a better distribution of the hydrogen which tends to segregate such an improved distribution of the hydrogen that may be present in the bainite areas of the microstructure therefore increases the resistance to hydrogen.
  • Residual Austenite and Martensite are cumulatively present from 1% to 25% by area fraction in fhe steel according to the invention.
  • Martensite is formed during cooling after the soaking from the unstable austenite formed during annealing.
  • Martensite is composed of fine laths elongated in one direction inside each grain issued from a primary austenite grain, in which fine iron carbides sticks which are 50 to 200 nm long are precipitated between the laths following the ⁇ 111> direction. Martensite imparts ductility and strength to the Steel of present invention.
  • the steel parts according to the invention may advantageously be used as parts for chassis, wheel hub applications .
  • these steel parts may be used as bolts and screws for such applications, and for example chassis bolts, hub to bearing bolts, rim to hub bolts .
  • the diameter of the steel part is for example lower than or equal to 22 mm, and more particularly lower than or equal to 20 mm, and even more particularly lower than or equal to 16 mm. More particularly, the diameter of the steel part is for example greater than or equal to 5.5 mm.
  • the steel part described above may, for example, be obtained using a method comprising:
  • the heat treatment comprising:
  • the semi-finished product provided during the provision step has the following composition, by weight:
  • This composition corresponds to the composition previously described for the steel part.
  • the semi-finished product is in particular a wire, having, for example, a diameter comprised from 5 mm to 25 mm.
  • the annealing step is performed at an annealing temperature strictly lower than the Ac1 temperature of the steel.
  • the Ac1 temperature is the temperature at which austenite begins to form during heating.
  • the annealing step is intended for temporarily decreasing the tensile strength of the steel so as to prepare it for cold forming.
  • the steel has a tensile strength lower than or equal to 600 MPa.
  • Such an annealing is called globulization or spherodization annealing.
  • the semi-finished product is heated to an annealing temperature greater than or equal to Ac1-20°C.
  • the semi-finished product is preferably held at the annealing temperature for a time which is chosen, as a function of the annealing temperature, such that the tensile strength of the steel after annealing is lower than or equal to 600 MPa.
  • the holding time at the annealing temperature is comprised from 5 to 9 hours.
  • the annealing step is performed at an annealing temperature equal to 720°C, and the holding time at the annealing temperature is equal to 5 hours.
  • the annealing step is preferably carried out in a neutral atmosphere, for example in an atmosphere consisting of nitrogen gaz.
  • the semi-finished product After holding at the annealing temperature, the semi-finished product is cooled down to room temperature.
  • the cooling is preferably performed at a speed chosen so as to avoid the precipitation of pearlite and the formation of bainite, and thus so as to maintain a tensile strength smaller than or equal to 600MPa after cooling.
  • This cooling speed can be determined without difficulty using the CCT diagram of the steel.
  • the cooling from the annealing temperature is performed in three stages: a first cooling stage from the annealing temperature to about 670°C, where the steel is cooled at a cooling speed smaller than or equal to 25°C/h, a second cooling stage from about 670°C to about 150°C at a cooling speed smaller than or equal to 250°C/s and a third cooling stage, from about 150°C down to ambient temperature at a cooling speed corresponding to cooling in ambient or natural air.
  • This three-step cooling and the corresponding temperatures and speeds are given only by way of example, and different temperatures and speeds may be used depending in particular on the composition of the steel and on the final tensile strength desired.
  • the cold forming step is, for example, a cold heading step, such that a cold headed product is obtained at the end of the cold forming step, and a cold headed steel part is obtained at the end of the heat treatment.
  • the method optionally comprises, between the annealing and the cold heading step, a step of cold drawing the annealed semi-finished product so as to reduce a diameter thereof.
  • This cold drawing step is in particular a wire drawing step.
  • the cold drawing step is preceded by a surface preparation comprising cleaning the surface of the semi-finished part, followed by a step of forming a lubricating coating on the surface of the semi-finished part.
  • the cleaning step for example comprises a degreasing and/or a mechanical or chemical descaling or pickling, optionally followed by a neutralization.
  • neutralization is a cleaning process used to clean all the alien particles or substances from the surface of the steel in order to reduce the risk of corrosion.
  • the step of forming a lubricating coating for example comprises a phosphate treatment and a soaping.
  • the cold-formed steel part is subjected to a heat treatment comprising:
  • a holding temperature comprised from 100°C to 400°C for a time from 15 minutes to 2 hours.
  • This optional heat treatment is a tempering heat treatment.
  • the product is held at a holding temperature in a furnace.
  • the product can be held at the holding temperature by dipping in a molten salt bath
  • the products are allowed to cool down to the ambient temperature in ambient or natural air.
  • the heating step is carried out in such a manner that the steel part has an entirely austenitic microstructure at the end of the heating step.
  • the average size of the austenite grains formed during this heating step is lower than or equal to 20 pm, and in particular comprised from 8 to 15 pm. This size is, for example, measured with a magnification of 500:1.
  • This small grain size results from the presence of micro-alloying elements in the steel which form precipitates able to pin the grain boundaries in order to avoid grain growth during the austenitizing step.
  • This austenite grain size is the prior austenite grain size of the cold formed and quenched and tempered steel part according to the invention.
  • the heat treatment temperature is for example higher by a least 50°C than the full austenitisation temperature Ac3 of the steel.
  • the steel part is held at the heat treatment temperature for a time comprised from 5 minutes to 120 minutes.
  • the holding temperature during the holding step is comprised from 200 to 380°C.
  • the thus obtained steel part has the microstructure described above for the steel part.
  • R1 to R4 are reference steels composition which are not according to the present invention.
  • the remainder of the composition consists of iron and unavoidable impurities.
  • inventive steels and the reference steels are reheated at 1150°C and then are hot rolled with a finishing temperature above 800°C in the form of wire having a diameter of 16mm. Thereafter all the wire rods (semi-finished product) for both inventive as well as reference steels were subjected to annealing comprising holding the wire rods at a temperature of 720°C with a holding time of 5 hours, followed by cooling. Cooling was performed in three stages comprising cooling at a cooling speed of 25°C/h down to 670°C, followed by cooling at 250°C/h until 150°C, and finally natural or ambient air cooling down to room temperature.
  • Tensile tests were performed directly on wire rods. The tensile testing was performed according to standard NF EN ISO 6892-1 , i.e. with a cross head speed of 8 mm/min. Each value is the average of three measurements.
  • a hardness profile along the cross section of the samples was performed. Vickers hardness tests were carried out under a load of 30 kg for 15 seconds durations. The hardness was measured according to standard NF EN ISO 6507-1. Each value is the average of three measurements.
  • the microstructure of the obtained products was analyzed based on cross-sections of these products. More particularly, the structures present in the cross- sections were characterized by light optical microscopy (LOM) and by scanning electron microscopy (SEM). The LOM and SEM observations were performed after etching using a Nital containing solution.
  • LOM light optical microscopy
  • SEM scanning electron microscopy
  • TS refers to the tensile strength measured by tensile test in the longitudinal direction relative to the rolling direction
  • YS refers to the yield strength measured by tensile test in the longitudinal direction relative to the rolling direction
  • RA (%) refers to the percent reduction of area measured by tensile test in the longitudinal direction relative to the rolling direction
  • El (%) refers to the total elongation measured by tensile test in the longitudinal direction relative to the rolling direction
  • HV30 refers to the result of the hardness measurement
  • the hydrogen resistance of the corresponding samples was determined by comparison of the results of a slow strain rate tensile test conducted on the smooth test samples subjected to strain rate of 10 5 s 1 on an uncharged sample and then on a sample charged with hydrogen in accordance with NF A-05-304 standards.
  • the inventors determined the ductility (through the percent reduction of area Ra) on the charged and uncharged samples and compared the results through an embrittlement index.
  • the total H2 content inside samples before charging was equal to about 0.3 ppm.
  • embrittlement index I R3 relating to the percent reduction of area is calculated using the following formula:
  • embrittlement index close to 1 means that the grade is very sensitive to Flydrogen Embrittlement.
  • An embrittlement index I R3 lower than to 0.09 was considered satisfactory in view of the desired applications and embrittlement index I Ra lower than or equal to 0.08 is advantageous for the desired applications.
  • the inventors further observed the fracture surface mode in each case.
  • the steels having compositions 11 to I6 exhibit a higher hydrogen resistance than the reference grade R1 toR4 after quenching.
  • the samples according to the invention (l1 to I6) absorb less hydrogen under the same charging conditions than the comparative samples (R1 to R4).
  • the method according to the invention further has the advantage that it allows obtaining, after annealing, a sufficiently low tensile strength so as to enable the use of conventional cold forming tools, and reduce the wear thereof, while at the time resulting in final parts having a high tensile strength (greater than or equal to 1100 MPa).
  • Table 5 Microstructure
  • microstructures of the steels were characterized using Light Optical Microscopy (LOM) Scanning Electron Microscopy (SEM) after 2% Nital etching. Quantitative X-ray analysis has been done to determine the fraction of retained austenite. the underlined values are not according to the invention.
  • LOM Light Optical Microscopy
  • SEM Scanning Electron Microscopy

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Heat Treatment Of Steel (AREA)
  • Heat Treatment Of Strip Materials And Filament Materials (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

Method for producing a steel part comprising by weight: 0.05% ≤ C ≤ 0.15%, 0.01% ≤ Si ≤ 1%, 1.2% ≤ Mn ≤ 2%, 0.1% ≤ Cr ≤ 2%, 0.001 ≤ Al ≤ 0.1%, 0.003% ≤ N ≤ 0.01%, 0 ≤ S ≤ 0.015%, 0 ≤ P ≤ 0.015%,0% ≤ Ni ≤ 1%,0% ≤ B ≤ 0.01%, 0% ≤ Mo ≤ 1%, 0% ≤ Ti ≤ 0.04 %, 0% ≤ Nb ≤ 0.1%, 0 ≤ V ≤ 0.5% the remainder consisting of iron and unavoidable impurities, annealing this semi-finished product at an annealing temperature strictly lower than the Ac1 temperature of the steel; cooling it down to room temperature; cold forming the semi-finished product into a cold formed product; subjecting the cold formed product to a heat treatment comprising heating the cold formed product to a heat treatment temperature greater than or equal to the full austenitisation temperature Ac3 of the steel; and quenching to room temperature; optionally reheating the product at a holding temperature from 180°C to 400°C for a time from 15 minutes to 2 hours.

Description

Method for producing a steel part and steel part
The present invention relates to a method for manufacturing through cold forming, in particular via cold heading, assembly parts, such as screws, bolts, etc., that the automotive industry commonly uses for chassis or wheel hub components of vehicles.
As is known, the automotive industry continually aims to decrease the vehicle weight ; which can be done by modifying their safety assembly. The weight reduction requires an increasingly reduced size of the parts. These parts, however, remain subject to the same mechanical stresses, and must therefore have increasingly high mechanical properties, in particular tensile strength.
WO201 6/158470 is Age hardening steel excellent in machinability before aging treatment and excellent in fatigue characteristics, toughness, and low cycle fatigue characteristics after aging treatment, that is, age hardening steel containing predetermined amounts of C, Si, Mn, S, Cr, Al, V, Nb, Ca, and REM, limiting contents of P, Ti, and N to predetermined amounts or less, having a balance of Fe and impurities, having an area ratio of bainite structures of 70% or more. But the steel of WO2016/158470 lacks hydrogen embrittlement.
WO201 1/124851 is a mechanical steel part in steel with high characteristics, characterized in that its composition, comprising in weight percentages, is
Figure imgf000002_0001
wherein the contents of C, Mn and Cr are such that (830-270C %-90 Mn %-70Cr %)
Figure imgf000002_0002
Figure imgf000002_0003
Figure imgf000002_0004
the remainder of the steel part being iron and impurities resulting from processing, and wherein the in that its structure of the steel is bainitic and contains no more than a total of 20% of martensite and/or pro-eutectoid ferrite and/or pearlite. But the steel of WO2011/124851 is not demonstrate hydrogen embrittlement as well as reduction area of 58% or more.
However, it is desirable to further improve the resistance to hydrogen embrittlement of the parts.
Therefore, an aim of the invention is to provide a steel part which may be used as an assembly part for a motor vehicle, and which has improved resistance to hydrogen embrittlement while simultaneously having :
- an ultimate tensile strength greater than or equal to 1100 MPa and preferably above 1150 MPa, or even above 1180 MPa, - a yield strength greater than or above 880MPa and preferably above 900MPa
- a total elongation of 12% or more and preferably 13% or more.
- Hydrogen Embrittlement index of less than 0.09 and preferably less than or equal to 0.08
- a reduction in area of more than 58% and preferably above 60% or more and more preferably 62% or more.
In a preferred embodiment, the steel part shows a hardness from 360Hv to 405Hv.
The invention will be better understood upon reading the description that follows, given solely by way of example.
In the entire patent application, the contents are indicated in weight % (wt%).
The steel part according to the invention has a composition comprising, by weight: 0.05% ≤ C ≤ 0.15%
0.01% ≤ Si ≤ 1%
1.2% ≤ Mn ≤ 2%
0.1 % ≤ Cr ≤ 2%
0.001 ≤ Al ≤ 0.1%
0.003% ≤ N ≤ 0.01%
0 ≤ S ≤ 0.015%
0 ≤ P ≤ 0.015% optionally 0% ≤ Ni ≤ 1%
0% ≤ Mo ≤ 1.0%
0% ≤ Nb ≤ 0.1%
0% ≤ Ti ≤ 0.04 %
0 ≤ V ≤ 0.5%
0% ≤ B ≤ 0.01% the remainder consisting of iron and unavoidable impurities.
Carbon is present in the steel of present invention from 0.05% to 0.15%. Carbon imparts strength to the steel by solid solution strengthening and carbon is gammagenous hence delays the formation of Ferrite. Carbon is the element that impacts the formation of Cementite-free Lath-Like Bainite. A minimum of 0.05% of carbon is required to reach a tensile strength of 1100 MPa but if carbon is present above 0.15%, carbon deteriorates ductility as well as machinability of the final product due to the formation of cementite. The carbon content is advantageously in the range 0.08% to 0.14% to obtain simultaneously high strength and high ductility and more preferably from 0.09% to 0.14%.
Silicon is present in the steel of present invention from 0.01% to 1%. Silicon imparts the steel of present invention with strength through solid solution strengthening. In particular, at the above-mentioned contents, the silicon has the effect of hardening the bainite microstructure through solid solution hardening. Silicon reduces the formation of cementite nucleation as silicon hinders precipitation and diffusion-controlled growth of carbides by forming a Si-enriched layer around precipitate nuclei. Therefore, resulting the cementite-free lath-like bainite. Silicon also acts as a deoxidizer. A minimum of 0.01% of silicon is required to impart strength to the steel of present invention. An amount of more than 1 % raises the activity of carbon in austenite promoting its transformation into pro- eutectoid ferrite, which can deteriorate the strength, and also resulting retardation for formation of bainite under continuous cooling thereby too much retained austenite at the end of cooling. The preferred limit for Silicon from 0.01 to 0.9% and more preferably from 0.01% to 0.5%
Manganese is added in the present steel from 1.2% to 2%. Manganese provides hardenability to the steel. It allows to decrease the critical cooling rate for which a bainitic transformation can be obtained in continuous cooling without any prior transformation and the manganese lowers the bainite start temperature of the steel, and therefore results in a refinement of the bainitic structure to form lath bainite and thus increases the mechanical properties of the part. A minimum content of 1.2% by weight is necessary to obtain the desired bainitic microstructure. But above 2 %, manganese has a negative effect on the steel of present invention as retained austenite can transform into MA islands or fresh martensite and these phases are detrimental for the properties. In addition, manganese forms sulphides such as MnS. These sulphides can increase machinability if the shape and distribution are well controlled. If not, they might have a very detrimental effect on Elongation. The preferred limit of manganese is from 1.3% to 1.9 % and more preferably from 1.4% to 1 .9%.
Chromium is present from 0.1% to 2% in the steel of present invention. Chromium is an indispensable element in order to produce bainitic structure, especially lath bainite and impart Elongation and ductility to the steel of present invention. Addition of Chromium promotes homogeneous and finer bainitic microstructure during the temperature range between Bs and room temperature. A minimum content of 0.1% of Chromium is required to produce the targeted bainitic microstructure and chromium also slows down the softening during the tempering treatment, allowing higher holding temperatures which favors degassing but also the formation of carbides that trap hydrogen. But the presence of Chromium content of 2% or more excessively increases the hardness of the steel, it makes it difficult to form it by cold forming, and in particular cold heading. It is advantageous to have Chromium from 0.2% to 1 .6% and more preferably from 0.3% to 1 .4%.
The steel aluminum is at a content from 0.001% to 0.1 wt%. Aluminum is a deoxidizer of the steel in the liquid state. It then contributes, in the form of nitrides, to controlling austenitic grain coarsening during hot rolling. On the other hand, present in too large an amount, it may lead to a coarsening of aluminate type inclusions in the steel which may prove damaging to the properties of the steel, especially its toughness. In particular, the aluminum content may be comprised at a content from 0.001 to 0.09 wt%.
In the steel according to the invention, the nitrogen content is comprised from 0% to 0.01 wt%. Nitrogen traps boron via the formation of boron nitrides, which makes the role of this element in the hardenability of the steel ineffective. Therefore, in the steel according to the invention, the nitrogen content is limited to 0.01 wt%. Nevertheless, added in small amounts, it makes it possible, via the formation in particular of titanium nitrides (TiN) and aluminum nitrides (AIN), to avoid excessive austenitic grain coarsening during heat treatments undergone by the steel. Similarly, it also allows, in this case, the formation of carbonitride precipitates that will contribute toward the trapping of hydrogen. Therefore, in the steel according to the invention, the nitrogen content is greater than or equal to 0.003 wt%.
The steel according to the invention comprises at most 0.015 wt% of phosphorus and at most 0.015 wt% of sulfur. The effect of phosphorus and sulfur are particularly harmful in the steels according to the invention, for several reasons. Indeed, since these elements are poisons for hydrogen recombination, they contribute to a higher concentration of atomic hydrogen capable of penetrating into the material, therefore to an increased risk of delayed fracture of the part in use. Moreover, by segregating at the grain boundaries, the phosphorus and the sulfur reduce the cohesion thereof. Their content must therefore be kept very low. For this purpose, measures must be taken to ensure that the steel is dephosphorized and desulfurized during its melting in the liquid state. The steel may optionally contains from 0.01 to 1wt% of nickel. This element provides an increase in the strength of the steel and has beneficial effects on the resistance to brittle fracture. It also improves, in a known manner, the corrosion resistance of the steel.
Boron is an optional element and can be present in the alloy at contents from 0.0003 to 0.01 wt%. By segregating at the prior austenitic grain boundaries, boron, even at very low contents, strengthens the grains boundaries, and makes it possible to increase the resistance to hydrogen-induced delayed fracture. The boron increases the cohesion of the grain boundary via its intrinsic effect, but also by making phosphorus segregation more difficult at these grain boundaries. The boron further strongly increases the hardenability of the steel and thus makes it possible to limit the carbon content needed to obtain the desired bainitic microstructure. Finally, boron acts in synergy with molybdenum and niobium, thus increasing the effectiveness of these elements and their own influence that their respective contents permit. An excess of boron (above 0.01 wt%) would however lead to the formation of brittle iron boro-carbides.
The molybdenum is an optional element and is comprised from 0.003 to 1 wt%. Molybdenum interacts strongly with phosphorus and limits the damaging effect of the phosphorus by limiting its segregation at the prior austenite grain boundaries. Furthermore, it displays a marked carbide-forming behavior. For given mechanical properties, it allows higher holding tempering temperature, which, as a result, favor the development of carbides that will be hydrogen traps. It is therefore an element that increases the resistance to delayed fracture.
Titanium is an optional element and present in the alloy at contents comprised from 0.01 to 0.04 wt%. Titanium is added to the liquid steel in order to increase the hardness of the material. Flere, within the ranges indicated, it also increases the delayed fracture resistance in several ways. It contributes to austenitic grain refinement and forms precipitates that trap hydrogen. Finally, the hardening effect of the titanium makes it possible to carry out tempering operations at higher holding temperatures. The maximum titanium content is set here in order to avoid obtaining precipitates of too large a size which would then degrade the resistance of the steel to delayed fracture.
The steel of present invention can optionally contain niobium at contents comprised from 0.01 to 0.1 wt%. Niobium improves the hydrogen resistance, as it can on the one hand limit the formation of borocarbides Fe3(C,B) ; Fe23(C,B)26 which consume, and therefore, lower the “free” boron content available for segregation at the grain boundaries, and, on the other hand, limits the austenitic grain growth by forming carbonitrides. The refinement of grains results in a higher total length of grain boundaries, and therefore in a better distribution of harmful elements, such as phosphorous and sulfur, in lower concentration. Furthermore, a decrease in austenitic grain size results in an acceleration of the kinetics of the bainitic transformation. The maximum niobium content is set in order to avoid obtaining precipitates of too large size which would then degrade the resistance of the steel to delayed fracture. Furthermore, when it is added in too large amount, niobium leads to an increased risk of “crack” defects at the surface of the billets and blooms as continually cast. These defects, if they cannot be completely eliminated, may prove very damaging in respect of the integrity of the properties of the final part, especially as regards fatigue strength and hydrogen resistance. This is why the niobium content is kept below 0.1 wt%.
Further optionally, the steel may comprise vanadium at a content lower than or equal to 0.5 wt%. When it is present, thanks to its hardening effect, the vanadium makes it possible to carry out tempering operations at higher temperatures. The maximum vanadium content is set to avoid obtaining precipitates of too large size which might degrade the resistance of the steel to delayed hydrogen fracture. In particular, the vanadium content may be comprised at a content from 0.05 to 0.5 wt%.
The rest of the composition is iron and unavoidable impurities, in particular resulting from the elaboration.
More particularly, the composition of the steel part consists of the above-mentioned elements.
The steel part according to the invention is more particularly a cold formed steel part, and more particularly a cold headed steel part.
The steel part has a microstructure comprising, in surface fractions or area%, of at least 80% bainite, and a cumulative presence of Residual Austenite and martensite from 1 % to 25%.
Bainite is present in the steel according to the invention as a matrix phase and imparts strength to such steel. Bainite is present in the steel at least 80% by area fraction and preferably from 80% to 95% by area fraction and more preferably from 85% to 95%. Bainite is formed during quenching. Such bainite may include Cementite-Free Lath-Like Bainite and Lower bainite. The cementite- free Lath-Like bainite is consisting of bainite in the form of laths and including, between these laths, carbides such that the number N of inter-lath carbides larger than 0.1 micrometers per unit of surface area is less than or equal to 50000/mm2. This cementite-free lath-like bainite structure confers to the steel of present invention a good resistance against hydrogen. The lower bainite is consisting of bainite in the form of laths and including, fine iron carbides sticks which are precipitated inside the laths. The lower bainite structure provide the steel of present invention with elongation and tensile strength. The lath structure of both Lower bainite and cementite free lath like bainite allow for a better distribution of the hydrogen which tends to segregate such an improved distribution of the hydrogen that may be present in the bainite areas of the microstructure therefore increases the resistance to hydrogen.
Residual Austenite and Martensite are cumulatively present from 1% to 25% by area fraction in fhe steel according to the invention. Martensite is formed during cooling after the soaking from the unstable austenite formed during annealing. Martensite is composed of fine laths elongated in one direction inside each grain issued from a primary austenite grain, in which fine iron carbides sticks which are 50 to 200 nm long are precipitated between the laths following the <111> direction. Martensite imparts ductility and strength to the Steel of present invention. However, when martensite and Residual austenite cumulatively presence is above 25%, it imparts excess strength but diminishes the elongation beyond acceptable limit for the steel of present invention due to the reason that martensite has same amount of carbon content as of Residual Austenite hence the fresh martensite is brittle and hard. Preferred limit for the cumulative presence of Residual Austenite and martensite for the steel of present invention is from 4% to 22% and more preferably from 4% to 20%.
The steel parts according to the invention may advantageously be used as parts for chassis, wheel hub applications . In particular, these steel parts may be used as bolts and screws for such applications, and for example chassis bolts, hub to bearing bolts, rim to hub bolts .
The diameter of the steel part is for example lower than or equal to 22 mm, and more particularly lower than or equal to 20 mm, and even more particularly lower than or equal to 16 mm. More particularly, the diameter of the steel part is for example greater than or equal to 5.5 mm.
The steel part described above may, for example, be obtained using a method comprising:
- providing a semi-finished product made of steel; - annealing this semi-finished product at an annealing temperature strictly lower than the Ac1 temperature of the steel;
- cold forming the semi-finished product into a cold formed product;
- subjecting the cold formed product to a heat treatment so as to obtain a cold formed steel part, the heat treatment comprising:
- heating the cold formed product to a heat treatment temperature greater than or equal to the full austenitization temperature (Ac3) of the steel
- quenching to room temperature
- and then optionally,
- holding the product at a holding temperature comprised from 100°C to 400°C for a time from 15 minutes to 2 hours.
The semi-finished product provided during the provision step has the following composition, by weight:
0.05% ≤ C ≤ 0.15%
0.01% ≤ Si ≤ 1%
1.2% ≤ Mn ≤ 2%
0.1 % ≤ Cr ≤ 2%
0.001 ≤ Al ≤ 0.1%
0.003% ≤ N ≤ 0.01%
0 ≤ S ≤ 0.015%
0 ≤ P ≤ 0.015% optionally 0% ≤ Cu ≤ 1 %
0% ≤ Ni ≤ 1%
0% ≤ Mo ≤ 1.0%
0% ≤ Nb ≤ 0.1%
0% ≤ Ti ≤ 0.04 %
0 ≤ V ≤ 0.5%
0% ≤ B ≤ 0.01% the remainder consisting of iron and unavoidable impurities.
This composition corresponds to the composition previously described for the steel part.
The semi-finished product is in particular a wire, having, for example, a diameter comprised from 5 mm to 25 mm. As mentioned above, the annealing step is performed at an annealing temperature strictly lower than the Ac1 temperature of the steel. As is conventional, the Ac1 temperature is the temperature at which austenite begins to form during heating.
The annealing step is intended for temporarily decreasing the tensile strength of the steel so as to prepare it for cold forming. For example, at the end of the annealing step, the steel has a tensile strength lower than or equal to 600 MPa. Such an annealing is called globulization or spherodization annealing.
More particularly, during the annealing step, the semi-finished product is heated to an annealing temperature greater than or equal to Ac1-20°C.
During the annealing step, the semi-finished product is preferably held at the annealing temperature for a time which is chosen, as a function of the annealing temperature, such that the tensile strength of the steel after annealing is lower than or equal to 600 MPa. For example, the holding time at the annealing temperature is comprised from 5 to 9 hours.
According to a particular example, the annealing step is performed at an annealing temperature equal to 720°C, and the holding time at the annealing temperature is equal to 5 hours.
The annealing step is preferably carried out in a neutral atmosphere, for example in an atmosphere consisting of nitrogen gaz.
After holding at the annealing temperature, the semi-finished product is cooled down to room temperature.
The cooling is preferably performed at a speed chosen so as to avoid the precipitation of pearlite and the formation of bainite, and thus so as to maintain a tensile strength smaller than or equal to 600MPa after cooling. This cooling speed can be determined without difficulty using the CCT diagram of the steel.
According to a particular example, the cooling from the annealing temperature is performed in three stages: a first cooling stage from the annealing temperature to about 670°C, where the steel is cooled at a cooling speed smaller than or equal to 25°C/h, a second cooling stage from about 670°C to about 150°C at a cooling speed smaller than or equal to 250°C/s and a third cooling stage, from about 150°C down to ambient temperature at a cooling speed corresponding to cooling in ambient or natural air. This three-step cooling and the corresponding temperatures and speeds are given only by way of example, and different temperatures and speeds may be used depending in particular on the composition of the steel and on the final tensile strength desired. The cold forming step is, for example, a cold heading step, such that a cold headed product is obtained at the end of the cold forming step, and a cold headed steel part is obtained at the end of the heat treatment.
The method optionally comprises, between the annealing and the cold heading step, a step of cold drawing the annealed semi-finished product so as to reduce a diameter thereof. This cold drawing step is in particular a wire drawing step.
Preferably, the cold drawing step is preceded by a surface preparation comprising cleaning the surface of the semi-finished part, followed by a step of forming a lubricating coating on the surface of the semi-finished part.
The cleaning step for example comprises a degreasing and/or a mechanical or chemical descaling or pickling, optionally followed by a neutralization. In this context, neutralization is a cleaning process used to clean all the alien particles or substances from the surface of the steel in order to reduce the risk of corrosion.
The step of forming a lubricating coating for example comprises a phosphate treatment and a soaping.
After cold forming, the cold-formed steel part is subjected to a heat treatment comprising:
- heating the cold formed product to a heat treatment temperature greater than or equal to the full austenitization temperature Ac3 of the steel;
- quenching to room temperature
- and then, optionally, holding the product at a holding temperature comprised from 100°C to 400°C for a time from 15 minutes to 2 hours.
This optional heat treatment is a tempering heat treatment.
According to an example, during the holding step, the product is held at a holding temperature in a furnace. According to another example, the product can be held at the holding temperature by dipping in a molten salt bath
After the end of the holding step, the products are allowed to cool down to the ambient temperature in ambient or natural air.
The heating step is carried out in such a manner that the steel part has an entirely austenitic microstructure at the end of the heating step.
The average size of the austenite grains formed during this heating step is lower than or equal to 20 pm, and in particular comprised from 8 to 15 pm. This size is, for example, measured with a magnification of 500:1.
This small grain size results from the presence of micro-alloying elements in the steel which form precipitates able to pin the grain boundaries in order to avoid grain growth during the austenitizing step. This austenite grain size is the prior austenite grain size of the cold formed and quenched and tempered steel part according to the invention.
The heat treatment temperature is for example higher by a least 50°C than the full austenitisation temperature Ac3 of the steel.
5 More particularly, during the heating step, the steel part is held at the heat treatment temperature for a time comprised from 5 minutes to 120 minutes.
Preferably the holding temperature during the holding step is comprised from 200 to 380°C.
At the end of the holding step, a cold formed, and more particularly cold headed, and 10 quenched steel part is obtained.
The thus obtained steel part has the microstructure described above for the steel part.
Experiments
Laboratory tests were carried out on castings having the chemical compositions 11 to 15 16 which are according to the present invention. R1 to R4 are reference steels composition which are not according to the present invention.
Table 1 : Chemical compositions of the castings
Figure imgf000012_0001
20 In the above Table 1 , the compositions are indicated in wt% and the underlined values are not according to the invention.
In all of the above compositions, the remainder of the composition consists of iron and unavoidable impurities.
25 Table 2 - Process parameters
The inventive steels and the reference steels are reheated at 1150°C and then are hot rolled with a finishing temperature above 800°C in the form of wire having a diameter of 16mm. Thereafter all the wire rods (semi-finished product) for both inventive as well as reference steels were subjected to annealing comprising holding the wire rods at a temperature of 720°C with a holding time of 5 hours, followed by cooling. Cooling was performed in three stages comprising cooling at a cooling speed of 25°C/h down to 670°C, followed by cooling at 250°C/h until 150°C, and finally natural or ambient air cooling down to room temperature. These cooling speeds were obtained by adjusting the heating conditions in the annealing furnace accordingly, the heating being reduced or turned off depending on the needs, in a manner known to the skilled person. Ac1 and Ac3 for both Inventive Steels (11 to I6) and reference steel (R1 to R3) are calculated by a dilatometry study. Thereafter the cold formed steel part is subjected to a heating and quenching heat treatment according to the table 2.
Table 2 - Process parameters
Figure imgf000013_0001
The underlined values are not according to the invention in Table 2. Table 3 : Mechanical properties
Tensile tests were performed directly on wire rods. The tensile testing was performed according to standard NF EN ISO 6892-1 , i.e. with a cross head speed of 8 mm/min. Each value is the average of three measurements.
A hardness profile along the cross section of the samples was performed. Vickers hardness tests were carried out under a load of 30 kg for 15 seconds durations. The hardness was measured according to standard NF EN ISO 6507-1. Each value is the average of three measurements.
The results of these tests are summarized in Table 3 below.
Furthermore, the microstructure of the obtained products was analyzed based on cross-sections of these products. More particularly, the structures present in the cross- sections were characterized by light optical microscopy (LOM) and by scanning electron microscopy (SEM). The LOM and SEM observations were performed after etching using a Nital containing solution.
The results of these analyses are summarized in the following Table 4.
In Tables 3, the following abbreviations are used:
TS (MPa) refers to the tensile strength measured by tensile test in the longitudinal direction relative to the rolling direction,
YS (MPa) refers to the yield strength measured by tensile test in the longitudinal direction relative to the rolling direction,
RA (%) refers to the percent reduction of area measured by tensile test in the longitudinal direction relative to the rolling direction,
El (%) refers to the total elongation measured by tensile test in the longitudinal direction relative to the rolling direction,
HV30 refers to the result of the hardness measurement,
Table 3: Mechanical properties of the samples after quenching
Figure imgf000014_0001
Figure imgf000015_0001
the underlined values are not according to the invention.
Table 4 : Flydrogen Embrittlement Results
For each of the experiments 11 to I6 as well as R1 to R3, the hydrogen resistance of the corresponding samples was determined by comparison of the results of a slow strain rate tensile test conducted on the smooth test samples subjected to strain rate of 105 s 1 on an uncharged sample and then on a sample charged with hydrogen in accordance with NF A-05-304 standards.
More particularly, the inventors determined the ductility (through the percent reduction of area Ra) on the charged and uncharged samples and compared the results through an embrittlement index.
The total H2 content inside samples before charging was equal to about 0.3 ppm.
Flydrogen charging was performed through cathodic charging using an electrolytic solution composed of H2SO4 1N with the addition of an hydrogen promoter Thiourea 2.5 mg/L, with a current density I = 0.8 mA/cm2 for 5 hours.
For each pair of samples (charged and uncharged), the embrittlement index IR3 relating to the percent reduction of area is calculated using the following formula:
I Ra = 1 - [RA(H2)/ RA(H2=0)], where RA(H2) corresponds to the value of the percent reduction of area measured on the sample charged with hydrogen, and RA(H2=0) corresponds to the value of the percent reduction of area measured on the uncharged sample.
An embrittlement index close to 1 means that the grade is very sensitive to Flydrogen Embrittlement. An embrittlement index IR3 lower than to 0.09 was considered satisfactory in view of the desired applications and embrittlement index IRa lower than or equal to 0.08 is advantageous for the desired applications.
The inventors further observed the fracture surface mode in each case.
The results of these tests are summarized in Table 4.
Figure imgf000016_0001
As can be seen from the above Table 4, the ductility for the inventive steel is not significantly affected by hydrogen.
The steels having compositions 11 to I6 exhibit a higher hydrogen resistance than the reference grade R1 toR4 after quenching.
The comparison of the samples 11 to I6 having a bainite content greater than or equal to 80% as shown in table 5 with the sample having a martensitic microstructure that is R1 to R4 as shown in table 5 shows that the bainitic structure is less sensitive to hydrogen embrittlement than the martensitic structure.
It can finally be observed that the samples according to the invention (l1 to I6) absorb less hydrogen under the same charging conditions than the comparative samples (R1 to R4).
Therefore, these experiments show that the steel parts according to the invention are particularly well adapted for applications as mentioned above, they have very good mechanical properties, and in particular a good tensile strength, associated with an improved resistance to hydrogen embrittlement as compared to prior art steel parts.
The method according to the invention further has the advantage that it allows obtaining, after annealing, a sufficiently low tensile strength so as to enable the use of conventional cold forming tools, and reduce the wear thereof, while at the time resulting in final parts having a high tensile strength (greater than or equal to 1100 MPa). Table 5: Microstructure
The microstructures of the steels were characterized using Light Optical Microscopy (LOM) Scanning Electron Microscopy (SEM) after 2% Nital etching. Quantitative X-ray analysis has been done to determine the fraction of retained austenite.
Figure imgf000017_0001
the underlined values are not according to the invention.

Claims

1. Method for producing a steel part comprising:
- providing a semi-finished product made of a steel comprising, by weight: 0.05% ≤ C ≤ 0.15%
0.01% ≤ Si ≤ 1%
1.2% ≤ Mn ≤ 2%
0.1% ≤ Cr ≤ 2%
0.001 ≤ Al ≤ 0.1 %
0.003% ≤ N ≤ 0.01%
0 ≤ S ≤ 0.015%
0 ≤ P ≤ 0.015% optionally 0% ≤ Ni ≤ 1%
0% ≤ B ≤ 0.01%
0% ≤ Mo ≤ 1%
0% ≤ Ti ≤ 0.04 %
0% ≤ Nb ≤ 0.1%
0 ≤ V ≤ 0.5% the remainder consisting of iron and unavoidable impurities,
- annealing this semi-finished product at an annealing temperature strictly lower than the Ac1 temperature of the steel;
- cooling it down to room temperature;
- cold forming the semi-finished product into a cold formed product;
- subjecting the cold formed product to a heat treatment comprising:
- heating the cold formed product to a heat treatment temperature greater than or equal to the full austenitisation temperature Ac3 of the steel; and
- quenching to room temperature;
- optionally reheating the product at a holding temperature from 180°C to 400°C for a time from 15 minutes to 2 hours.
2.- Method according to claim 1 , wherein, during the heating step of the heat treatment, the cold formed product is heated to a heat treatment temperature which is at least 50°C greater than the full austenitisation temperature Ac3 of the steel.
3.- Method according to claim 1 or claim 2, wherein the annealing temperature is greater than or equal to Ac1 minus 20°C.
4.- Method according to any one of claims 1 to 3, wherein the semi-finished product is a wire having diameter from 5mm to 25mm.
5.- Method according to any one of claims 1 to 4, further comprising, before the cold forming step, a preparation of the surface of the semi-finished product, comprising cleaning the surface of the semi-finished product and forming a lubricating coating on the surface thereof.
6.- Method according to claim 5, wherein the step of forming a lubricating coating on the surface of the semi-finished product comprises performing a phosphate treatment and a soaping.
7.- Method according to any one of the preceding claims, wherein the carbon content of the steel is comprised from 0.08 to 0.14 wt%.
8.- Method according to any one of the preceding claims, wherein the manganese content of the steel is comprised from 1.3 to 1 .9 wt%.
9.- Method according to any one of the preceding claims, wherein the chromium content of the steel is comprised from 0.2 to 1 .6 wt%.
10.- Method according to any one of the preceding claims, wherein the cold forming step is a cold heading step.
11.- Method according to any one of the preceding claims, wherein, during the holding step, the product is held at the holding temperature by dipping in a molten salt bath.
12.- Steel part made of an alloy comprising, by weight: 0.05% ≤ C ≤ 0.15%
0.01% ≤ Si ≤ 1%
1.2% ≤ Mn ≤ 2%
0.1% ≤ Cr ≤ 2%
0.001 ≤ Al ≤ 0.1 %
0.003% ≤ N ≤ 0.01%
0 ≤ S ≤ 0.015%
0 ≤ P ≤ 0.015% optionally 0% ≤ Ni ≤ 1%
0% ≤ B ≤ 0.01%
0% ≤ Mo ≤ 1%
0% ≤ Ti ≤ 0.04 %
0% ≤ Nb ≤ 0.1%
0 ≤ V ≤ 0.5% the remainder consisting of iron and unavoidable impurities, wherein the steel part has a microstructure comprising, at least 80 area% of bainite and a cumulative presence of martensite and residual austenite from 1 area% to 25 area%, wherein the steel part has a tensile strength of 1100 MPa or more.
13.- Steel part according to claim 12, wherein the martensite of the steel has iron carbides in stick form with sticks being 50 to 200nm long.
14.- Steel part according to any one of claims 12 or 13, wherein the steel part has a hardness from 360HV to 405 HV.
15.- Steel part according to any one of claims 12 to 14, wherein the steel part has a hydrogen embrittlement index of less than 0.09.
16.- Steel part according to any one of claims 12 to 15, wherein the steel part has a reduction in area of more than 58%.
PCT/IB2021/055331 2021-06-16 2021-06-16 Method for producing a steel part and steel part WO2022263887A1 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
CN202180099057.XA CN117441033A (en) 2021-06-16 2021-06-16 Method for producing a steel component and steel component
MX2023014918A MX2023014918A (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part.
EP21734517.2A EP4355920A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part
PCT/IB2021/055331 WO2022263887A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part
KR1020237042447A KR20240007218A (en) 2021-06-16 2021-06-16 How to manufacture steel parts and steel parts
BR112023024874A BR112023024874A2 (en) 2021-06-16 2021-06-16 METHOD FOR PRODUCING A STEEL PART AND STEEL PART
JP2023577646A JP2024524929A (en) 2021-06-16 2021-06-16 Manufacturing method of steel parts and steel parts
US18/568,929 US20240301528A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part
CA3220321A CA3220321A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2021/055331 WO2022263887A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part

Publications (1)

Publication Number Publication Date
WO2022263887A1 true WO2022263887A1 (en) 2022-12-22

Family

ID=76601519

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2021/055331 WO2022263887A1 (en) 2021-06-16 2021-06-16 Method for producing a steel part and steel part

Country Status (9)

Country Link
US (1) US20240301528A1 (en)
EP (1) EP4355920A1 (en)
JP (1) JP2024524929A (en)
KR (1) KR20240007218A (en)
CN (1) CN117441033A (en)
BR (1) BR112023024874A2 (en)
CA (1) CA3220321A1 (en)
MX (1) MX2023014918A (en)
WO (1) WO2022263887A1 (en)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011124851A2 (en) 2010-04-07 2011-10-13 Ascometal Mechanical part made of steel having high properties and process for manufacturing same
EP2995698A1 (en) * 2013-05-08 2016-03-16 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) HOT-DIP ZINC-COATED STEEL SHEET OR ALLOYED HOT-DIP ZINC-COATED STEEL SHEET HAVING SUPERIOR STRENGTH-BENDABILITY BALANCE WITH TENSILE STRENGTH OF 1180 MPa OR MORE
WO2016158470A1 (en) 2015-03-31 2016-10-06 新日鐵住金株式会社 Age-hardening steel and method of manufacturing parts using age-hardening steel
WO2020058829A1 (en) * 2018-09-20 2020-03-26 Arcelormittal Cold rolled and coated steel sheet and a method of manufacturing thereof
EP3631021A1 (en) * 2017-05-22 2020-04-08 Arcelormittal Method for producing a steel part and corresponding steel part
EP3640357A1 (en) * 2017-06-15 2020-04-22 Nippon Steel Corporation Rolled wire for spring steel
WO2020229877A1 (en) * 2019-05-15 2020-11-19 Arcelormittal A cold rolled martensitic steel and a method for it's manufacture
WO2021009543A1 (en) * 2019-07-16 2021-01-21 Arcelormittal Method for producing a steel part and steel part
WO2021089851A1 (en) * 2019-11-08 2021-05-14 Ssab Technology Ab Medium manganese steel product and method of manufacturing the same

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011124851A2 (en) 2010-04-07 2011-10-13 Ascometal Mechanical part made of steel having high properties and process for manufacturing same
EP2995698A1 (en) * 2013-05-08 2016-03-16 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) HOT-DIP ZINC-COATED STEEL SHEET OR ALLOYED HOT-DIP ZINC-COATED STEEL SHEET HAVING SUPERIOR STRENGTH-BENDABILITY BALANCE WITH TENSILE STRENGTH OF 1180 MPa OR MORE
WO2016158470A1 (en) 2015-03-31 2016-10-06 新日鐵住金株式会社 Age-hardening steel and method of manufacturing parts using age-hardening steel
EP3631021A1 (en) * 2017-05-22 2020-04-08 Arcelormittal Method for producing a steel part and corresponding steel part
EP3640357A1 (en) * 2017-06-15 2020-04-22 Nippon Steel Corporation Rolled wire for spring steel
WO2020058829A1 (en) * 2018-09-20 2020-03-26 Arcelormittal Cold rolled and coated steel sheet and a method of manufacturing thereof
WO2020229877A1 (en) * 2019-05-15 2020-11-19 Arcelormittal A cold rolled martensitic steel and a method for it's manufacture
WO2021009543A1 (en) * 2019-07-16 2021-01-21 Arcelormittal Method for producing a steel part and steel part
WO2021089851A1 (en) * 2019-11-08 2021-05-14 Ssab Technology Ab Medium manganese steel product and method of manufacturing the same

Also Published As

Publication number Publication date
CN117441033A (en) 2024-01-23
JP2024524929A (en) 2024-07-09
MX2023014918A (en) 2024-02-14
EP4355920A1 (en) 2024-04-24
KR20240007218A (en) 2024-01-16
US20240301528A1 (en) 2024-09-12
BR112023024874A2 (en) 2024-02-15
CA3220321A1 (en) 2022-12-22

Similar Documents

Publication Publication Date Title
US8845825B2 (en) High strength spring-use heat treated steel
KR101768785B1 (en) High-strength spring steel wire with excellent hydrogen embrittlement resistance, manufacturing process therefor, and high-strength spring
EP1693476A1 (en) Steel product for structural member of automobile and method for production thereof
EP3631021B1 (en) Method for producing a steel part and corresponding steel part
KR20150002848A (en) Steel wire for high-strength spring having exceptional coiling performance and hydrogen embrittlement resistance, and method for manufacturing same
CN110079743B (en) 1500 MPa-grade low-hydrogen delayed cracking sensitive hot forming steel and production method thereof
EP3999667B1 (en) Method for producing a steel part and steel part
KR20190075378A (en) High-strength wire rod and steel with excellent hydrogen retardation resistance and manufacturing the same
KR102647462B1 (en) Cold rolled and coated steel sheet and method of manufacturing the same
KR20200062926A (en) Cold-rolled steel sheet having high resistance for hydrogen embrittlement and manufacturing method thereof
CN112840058B (en) Wire rod and steel wire for spring having enhanced toughness and corrosion fatigue properties, and methods for manufacturing same
KR101867709B1 (en) Wire rod and steel wire for spring having excellent corrosion fatigue resistance and method for manufacturing the same
CN115210398B (en) Steel sheet, member, and method for producing same
WO2022263887A1 (en) Method for producing a steel part and steel part
RU2822646C2 (en) Method of making steel element and steel part
CN116724131A (en) High-strength wire rod for cold heading having excellent heat treatment characteristics and hydrogen-induced delayed fracture resistance, heat-treated component, and method for producing same
KR101886171B1 (en) Process for making a high strength steel plate with high yield ratio
RU2788982C1 (en) Steel part and method for its production
WO2024003593A1 (en) Forged part of steel and a method of manufacturing thereof
JP2024013082A (en) Case-hardening steel

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 21734517

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 3220321

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 202317078015

Country of ref document: IN

REG Reference to national code

Ref country code: BR

Ref legal event code: B01A

Ref document number: 112023024874

Country of ref document: BR

WWE Wipo information: entry into national phase

Ref document number: 202180099057.X

Country of ref document: CN

WWE Wipo information: entry into national phase

Ref document number: 2301007974

Country of ref document: TH

ENP Entry into the national phase

Ref document number: 20237042447

Country of ref document: KR

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 1020237042447

Country of ref document: KR

WWE Wipo information: entry into national phase

Ref document number: MX/A/2023/014918

Country of ref document: MX

WWE Wipo information: entry into national phase

Ref document number: 140250140003006401

Country of ref document: IR

ENP Entry into the national phase

Ref document number: 2023577646

Country of ref document: JP

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 2021734517

Country of ref document: EP

Ref document number: 2024100842

Country of ref document: RU

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2021734517

Country of ref document: EP

Effective date: 20240116

ENP Entry into the national phase

Ref document number: 112023024874

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20231128