EP4402294A1 - Pièce en acier trempé à la presse à haute résistance et son procédé de fabrication - Google Patents

Pièce en acier trempé à la presse à haute résistance et son procédé de fabrication

Info

Publication number
EP4402294A1
EP4402294A1 EP22768480.0A EP22768480A EP4402294A1 EP 4402294 A1 EP4402294 A1 EP 4402294A1 EP 22768480 A EP22768480 A EP 22768480A EP 4402294 A1 EP4402294 A1 EP 4402294A1
Authority
EP
European Patent Office
Prior art keywords
steel sheet
temperature
steel
comprised
steel part
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
EP22768480.0A
Other languages
German (de)
English (en)
Inventor
Sebastian Cobo
Alice DUMONT
Pascal DIETSCH
Stéphanie MICHAUT
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ArcelorMittal SA
Original Assignee
ArcelorMittal SA
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 SA filed Critical ArcelorMittal SA
Publication of EP4402294A1 publication Critical patent/EP4402294A1/fr
Pending legal-status Critical Current

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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
    • 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
    • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/26—Methods of annealing
    • C21D1/28—Normalising
    • 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
    • C21D1/62—Quenching devices
    • C21D1/673—Quenching devices for die quenching
    • 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226—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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys 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
    • C21D8/00—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247—Modifying the physical properties of ferrous metals or ferrous alloys 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
    • 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
    • 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
    • C22C38/26—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
    • C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
    • C23C2/06—Zinc or cadmium or alloys based thereon
    • 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
    • C23C2/12—Aluminium or alloys based thereon
    • 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
    • C21D2211/005—Ferrite
    • 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

Definitions

  • the present invention relates to high strength press hardened steel parts having good bendability and weldability properties.
  • High strength press-hardened parts can be used as structural elements in automotive vehicles for anti-intrusion or energy absorption functions.
  • This weight reduction can be achieved in particular thanks to the use of steel parts with a tempered martensitic or bainitic/martensitic microstructure.
  • Such types of parts can be welded, and the motor vehicle manufacturers prescribe that the weld joint should not constitute the weakest zone of the welded steel part. Indeed, the presence of spot welds on structural components in the car body can result in failure during crash, due to the localisation of the strain in the softened heat affected zone (HAZ).
  • HAZ softened heat affected zone
  • the purpose of the invention therefore is to solve the above-mentioned problem and to provide a press hardened steel part having a combination of high mechanical properties with tensile strength TS above or equal to 1000 MPa, a uniform elongation loss AUEI in spot welded areas below or equal to 25% and a bending angle above or equal to 55 °.
  • the press hardened steel part according to the invention has a fracture strain above or equal to 0.50.
  • the press hardened steel part according to the invention has a yield strength YS above or equal to 980 MPa.
  • the object of the present invention is achieved by providing a steel part according to claim 1 .
  • the steel part can also comprise characteristics of anyone of claims 2 to 4.
  • An other object is achieved by providing the method according to claim 5.
  • An other object is achieved by providing the method according to any one of claims 6 to 8.
  • composition of the steel according to the invention will now be described, the content being expressed in weight percent.
  • the carbon content is from 0.2% to 0.34% to ensure a satisfactory strength. Above 0.34% of carbon, fracture strain and bending angle of the steel sheet do not achieved the targeted values. Moreover, the weldability of the steel sheet may be reduced. If the carbon content is lower than 0.2%, the tensile and yield strengths will not reach the targeted value.
  • the manganese content is from 0.50% to 1 .24 %. Above 1 .24% of addition, the risk of central segregation increases to the detriment of the bendability, and the fracture strain may be reduced. Below 0.50% the hardenability of the steel sheet is reduced, and the tensile and yield strengths will not reach the targeted value.
  • the silicon content is from 0.5% to 2%.
  • Silicon is an element participating in the hardening in solid solution. Silicon is added to limit carbides formation and to ensure high level of tensile strength. Above 2%, silicon oxides form at the surface, which impairs the coatability of the steel. Moreover, the weldability of the steel sheet may be reduced.
  • the silicon content is from 0.5% to 1.8%. More preferably the silicon content is from 0.6% to 1 .8%, more preferably from 0.6% to 1 .6%.
  • the aluminium content can optionally be added up to 0.2% as it is a very effective element for deoxidizing the steel in the liquid phase during elaboration.
  • the aluminium content is below or equal to 0.1 %. More preferably, the aluminium content is below or equal to 0.06%.
  • the chromium content can be added up to 0.8% to improve hardening in solid solution.
  • the chromium content is below or equal to 0.8% to limit processability issues and cost.
  • the chromium content is below or equal to 0.6%.
  • Niobium content can optionally be added up to 0.06% for prior austenitic grain size refinement and to improve ductility of the steel. Above 0.06% of addition, the risk of formation of NbC or Nb(C,N) carbides increases to the detriment of the bendability.
  • the titanium content can optionally be added up to 0.06% in order to protect boron from formation of BN.
  • the titanium content is higher than 0.01 %.
  • the boron content can optionally be added up to 0.005%. Boron improves the hardenability of the steel.
  • the boron content is not higher than 0.005% to avoid a risk of breaking the slab during continuous casting.
  • Molybdenum can optionally be added up to 0.35%. As boron, molybdenum improves the hardenability of the steel. Molybdenum is not higher than 0.35% to limit cost.
  • the remainder of the composition of the steel is iron and impurities resulting from the smelting.
  • P, S and N at least are considered as residual elements which are unavoidable impurities.
  • the press hardened steel part has a microstructure comprising, in surface fraction, 95% or more of tempered martensite.
  • This tempered martensite is formed during the heating of the steel part to a temperature Ttemp comprised from 390°C to 510°C, for a holding time ttemp comprised from 1 s to 1000s.
  • Some bainite, ferrite and austenite can optionally be present, the sum of which being, in surface fraction, of 5% or less.
  • microstructure of the press hardened steel part is 100% made of tempered martensite.
  • the press hardened steel part according to the invention can be produced by any appropriate manufacturing method and the man skilled in the art can define one. It is however preferred to use the method according to the invention comprising the following steps: A steel sheet having a composition according to the invention is provided and cut to a predetermined shape, so as to obtain a steel blank.
  • the steel blank is heated to a temperature THF comprised from 810°C to 960°C, preferably from 850°C to 950°C and more preferably from 880°C to 950°C, and is maintained at said THF temperature for a holding time tHF comprised from 5 s to 1200s, to obtain a heated steel blank with a fully austenitic microstructure.
  • THF a temperature comprised from 810°C to 960°C, preferably from 850°C to 950°C and more preferably from 880°C to 950°C
  • the steel part is then die-quenched until reaching a temperature below or equal to 200°C.
  • the steel part is reheated to a temperature Ttemp comprised from 390°C to 510°C, and maintained at said temperature Ttemp for a holding time ttemp comprised from 1 s to 1000s, to obtain a tempered steel part, in order to ensure temperature homogeneity on all the steel part.
  • the tensile strength of the steel part is reduced.
  • the uniform elongation loss AUEI in spot welded areas is above 25%. The tempered steel part is then cooled to room temperature.
  • the HAZ sensitivity is assessed through the uniform elongation loss of JIS tensile specimen with weld compared to a reference without weld.
  • the uniform elongation loss AUEI is calculated as follows:
  • the uniform elongation UEI of the steel is measured according to standard JIS Z2241 on a tensile test specimen. A welded spot is done on a tensile test specimen, centred on the deformation area of the specimen. The uniform elongation UElw of this welded tensile test specimen is measured according to standard JIS Z2241. The uniform elongation loss AUEI is determined by the formula :
  • AUEI [(UEI-UEIw)/UEI]*100
  • the steel sheet provided to manufacture the steel part is produced by the following successive steps:
  • a steel slab having a composition described above is cast and reheated to a temperature Treheat comprised from 1 100°C to 1300°C before to be hot rolled at a finish hot rolling temperature comprised from 800°C to 950°C to obtain a hot rolled steel sheet.
  • the hot rolled steel sheet is then coiled to a temperature Tcoii lower than 670°C.
  • the hot rolled steel sheet can optionally be pickled to remove oxidation.
  • the hot rolled steel sheet can optionally be heated to a temperature THBA comprised from 500°C to 750°C, and maintained at said THBA temperature for a holding time tHBA comprised from 300s to 50h.
  • the steel sheet is then cold rolled to obtain a cold rolled steel sheet.
  • the cold-rolling reduction ratio is preferably comprised from 20% to 80%. Below 20%, the recrystallization during subsequent heat-treatment is not favored, which may impair the ductility of the steel sheet. Above 80%, there is a risk of edge cracking during cold rolling.
  • the cold rolled steel sheet is optionally annealed to an annealing temperature TA comprised from 650°C to 900°C and maintained at said temperature TAfor a holding time tA comprised from 10s to 1200s, to obtain an annealed steel sheet, in order to reduce the tensile strength to facilitate the cut of the steel.
  • the steel sheet is finally cooled to room temperature.
  • the said annealed steel sheet is coated with aluminium or aluminium alloy coating or with zinc or zinc alloy coating before being cooled to room temperature.
  • the steel sheet provided to manufacture the steel part is produced by the following successive step:
  • a steel slab having a composition according to the invention is cast and reheated to a temperature Treheat comprised from 1 100°C to 1300°C before being hot rolled at a finish hot rolling temperature comprised from 800°C to 950°C to obtain a hot rolled steel sheet.
  • the hot rolled steel sheet is then coiled to a temperature Tcoii lower than 670°C.
  • the hot rolled steel sheet can optionally be pickled to remove oxidation.
  • the hot rolled steel sheet can optionally be heated to a temperature THBA from 500°C to 750°C, and maintained at said THBA temperature for a holding time tHBA from 300s to 50h.
  • the steel sheet is then cold rolled to obtain a cold rolled steel sheet.
  • the cold-rolling reduction ratio is preferably from 20% to 80%. Below 20%, the recrystallization during subsequent heat-treatment is not favored, which may impair the ductility of the steel sheet. Above 80%, there is a risk of edge cracking during cold rolling.
  • the cold rolled steel sheet is optionally annealed to an annealing temperature TA comprised from 500°C to 750°C and maintained at said temperature TAfor a holding time tA comprised from 300s to 50h, to obtain an annealed steel sheet, in order to reduce the tensile strength to facilitate the cut of the steel.
  • the steel sheet is finally cooled to room temperature.
  • the press hardened steel part according to the invention has a tensile strength TS above or equal to 1000 MPa, a uniform elongation loss AllEI in spot welded areas below or equal to 25%, and a bending angle above or equal to 55 °.
  • the press hardened steel part has a yield strength YS above or equal to 980MPa.
  • the press hardened steel part according to the invention has a fracture strain above or equal to 0.50.
  • the tested compositions are gathered in the following table wherein the element contents are expressed in weight percent.
  • Steel semi-products, as cast, were reheated at 1250°C, hot rolled with a finish hot rolling temperature comprised from 800 to 950°C, coiled at 580°C and cold rolled with a reduction rate of 58%. Steel sheets are then heated to a temperature TA of 790°C and maintained at said temperature TA for a holding time tA of 180s.
  • the steel sheets were cut to a predetermined shape, so as to obtain a steel blank.
  • the steel blanks were then heated to a temperature THF for a holding time IHF of 120s, before being transferred to a forming press.
  • the heated blanks were hot- formed in the forming press to obtain a steel part, before being die-quenched until reaching a temperature of 80°C.
  • the surface fractions are determined through the following method: a specimen is cut from the press hardened steel part, polished and etched with a reagent known per se, for example Nital reagent, to reveal the microstructure. The section is afterwards examined through optical or scanning electron microscope, for example with a Scanning Electron Microscope with a Field Emission Gun (“FEG- SEM”) at a magnification greater than 5000x, coupled to an Electron Backscatter Diffraction (EBSD) device.
  • FEG- SEM Field Emission Gun
  • EBSD Electron Backscatter Diffraction
  • Tempered martensite can be distinguished from martensite thanks to its low dislocation density compared to martensite.
  • TS and YS are measured according to ISO standard ISO 6892-1 .
  • the bending angle has been determined on press hardened parts according to the method VDA238-100 bending Standard (with normalizing to a thickness of 1 .5 mm).
  • fracture strain refers to the fracture strain criterion defined by Pascal Dietsch et al. in “Methodology to assess fracture during crash simulation: fracture strain criteria and their calibration”, in Metallurgical Research Technology Volume 1 14, Number 6, 2017.
  • the fracture strain is the equivalent strain within the material at the deformation point when the critical bending angle has been reached.
  • the fracture strain values have been determined in plane strain conditions, which is the most severe condition in view of vehicle collision, and are obtained thank to finite elements analysis.
  • Table 5 Spot welding properties of the press hardened steel part A welded spot is done on the tensile test specimen, centred on the deformation area of the specimen. The corresponding uniform elongation loss AUEI of the resistance spot weld are gathered in table 5.
  • examples 1 -7 are the only one to show combination of high mechanical properties, with TS higher than 10OOMPa, a bending angle above or equal to 55°, and an uniform elongation loss lower than 25%. Moreover examples 1 -7 have a fracture strain higher than 0.50.
  • the tempering temperature applied on steel part of trials 8 and 9 is too low to limit the detrimental impact of HAZ softening on the uniform elongation, as shown by the uniform elongation loss higher than 25%. Moreover, in comparison to trial 2 with the same steel composition, the low temperature of tempering of trial 8 leads to a higher uniform elongation loss and lower fracture strain value than trial 2.

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

Abstract

L'invention concerne une pièce en acier trempé à la presse ayant une composition comprenant, en pourcentage en poids les constituants suivants : C dans la plage allant de 0,2 à 0,34 %, Mn dans la plage allant de 0,50 à 1,24 %, Si dans la plage allant de 0,5 à 2 %, P ≤ 0,020 %, S ≤ 0,010 %, N ≤ 0,010 %, et comprenant éventuellement un ou plusieurs des éléments suivants : Al : ≤ 0,2 %, Cr ≤ 0,8 %, Nb ≤ 0,06 %, Ti ≤ 0,06 %, B ≤ 0,005 %, Mo ≤ 0,35 %, le reste de la composition étant constitué de fer et d'impuretés inévitables résultant de la fusion. La pièce en acier trempé à la presse a une microstructure comprenant, en fraction de surface, 95 % ou plus de martensite revenue et 5 % ou moins de bainite, d'austénite ou de ferrite.
EP22768480.0A 2021-09-14 2022-08-26 Pièce en acier trempé à la presse à haute résistance et son procédé de fabrication Pending EP4402294A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/IB2021/058358 WO2023041953A1 (fr) 2021-09-14 2021-09-14 Pièce en acier durci sous presse à haute résistance et son procédé de fabrication
PCT/IB2022/058005 WO2023042018A1 (fr) 2021-09-14 2022-08-26 Pièce en acier trempé à la presse à haute résistance et son procédé de fabrication

Publications (1)

Publication Number Publication Date
EP4402294A1 true EP4402294A1 (fr) 2024-07-24

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EP4689212A1 (fr) * 2023-04-05 2026-02-11 ArcelorMittal Tôle d'acier laminée à froid et traitée thermiquement et son procédé de fabrication
WO2025003736A1 (fr) * 2023-06-30 2025-01-02 Arcelormittal Tôle d'acier et pièce d'acier emboutie à chaud à haute résistance ayant une excellente anisotropie de flexion et son procédé de fabrication
WO2025003735A1 (fr) 2023-06-30 2025-01-02 Arcelormittal Tôle d'acier et pièce d'acier emboutie à chaud à haute résistance ayant une excellente flexion et son procédé de fabrication
WO2025125855A1 (fr) * 2023-12-11 2025-06-19 Arcelormittal Pièce en acier durcie sous presse et son procédé de fabrication
WO2026022517A1 (fr) * 2024-07-26 2026-01-29 Arcelormittal Pièce en acier à haute résistance et procédé d'estampage à chaud associé

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JP4735211B2 (ja) 2004-11-30 2011-07-27 Ｊｆｅスチール株式会社 自動車用部材およびその製造方法
EP2465962B1 (fr) * 2006-07-14 2013-12-04 Kabushiki Kaisha Kobe Seiko Sho Feuilles d'acier très résistantes et leurs procédés de production
JP5257062B2 (ja) 2008-12-25 2013-08-07 新日鐵住金株式会社 靭性及び耐水素脆化特性に優れた高強度ホットスタンピング成形品及びその製造方法
JP5327106B2 (ja) 2010-03-09 2013-10-30 Ｊｆｅスチール株式会社 プレス部材およびその製造方法
RU2648104C2 (ru) * 2013-09-18 2018-03-22 Ниппон Стил Энд Сумитомо Метал Корпорейшн Горячештампованная деталь и способ ее изготовления
TWI609087B (zh) * 2014-03-31 2017-12-21 新日鐵住金股份有限公司 熱壓印鋼材
KR101665819B1 (ko) * 2014-12-24 2016-10-13 주식회사 포스코 열처리 강재, 내구특성이 우수한 초고강도 성형품 및 그 제조방법
WO2017006144A1 (fr) 2015-07-09 2017-01-12 Arcelormittal Acier pour trempe à la presse et pièce trempée à la presse fabriquée à partir d'un tel acier
KR101797316B1 (ko) 2015-12-21 2017-11-14 주식회사 포스코 고강도 및 우수한 내구성을 가지는 자동차용 부품 및 그 제조방법
WO2019003445A1 (fr) 2017-06-30 2019-01-03 Ｊｆｅスチール株式会社 Élément pressé à chaud et son procédé de production, et tôle d'acier laminée à froid pour pressage à chaud
JP7088140B2 (ja) * 2019-08-06 2022-06-21 Ｊｆｅスチール株式会社 高強度薄鋼板およびその製造方法
KR102237488B1 (ko) * 2019-12-16 2021-04-08 주식회사 포스코 펀칭 성형성이 우수한 고경도 강판 및 그 제조방법

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CN117980509A (zh) 2024-05-03
WO2023041953A1 (fr) 2023-03-23
WO2023042018A1 (fr) 2023-03-23
MX2024003168A (es) 2024-04-15
US20240401162A1 (en) 2024-12-05
JP2024532941A (ja) 2024-09-10
JP2026048789A (ja) 2026-03-17
JP7791312B2 (ja) 2025-12-23
ZA202401756B (en) 2025-03-26
CA3232414A1 (fr) 2023-03-23
KR20240063932A (ko) 2024-05-10

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