WO2010085983A1 - Fabrication process of coated stamped parts and parts prepared from the same - Google Patents

Fabrication process of coated stamped parts and parts prepared from the same Download PDF

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Publication number
WO2010085983A1
WO2010085983A1 PCT/EP2009/000670 EP2009000670W WO2010085983A1 WO 2010085983 A1 WO2010085983 A1 WO 2010085983A1 EP 2009000670 W EP2009000670 W EP 2009000670W WO 2010085983 A1 WO2010085983 A1 WO 2010085983A1
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WO
WIPO (PCT)
Prior art keywords
heating
temperature
precoating
comprised
layer
Prior art date
Application number
PCT/EP2009/000670
Other languages
French (fr)
Inventor
Isabelle Thirion
Thomas Vietoris
Raisa Grigorieva
Pascal Drillet
Ludwig Schaller
Karl Michael Bader
Uwe Paar
Michael Alsmann
Original Assignee
Arcelormittal Investigacion Y Desarrollo S.L.
Audi Ag
Volkswagen Ag
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.)
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Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=41059877&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2010085983(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Arcelormittal Investigacion Y Desarrollo S.L., Audi Ag, Volkswagen Ag filed Critical Arcelormittal Investigacion Y Desarrollo S.L.
Priority to PCT/EP2009/000670 priority Critical patent/WO2010085983A1/en
Priority to CA2751062A priority patent/CA2751062C/en
Priority to MA34139A priority patent/MA33095B1/en
Priority to PL10702612T priority patent/PL2391508T3/en
Priority to CN201080006436.1A priority patent/CN102300707B/en
Priority to MX2011008114A priority patent/MX351661B/en
Priority to HUE10702612A priority patent/HUE050213T2/en
Priority to PCT/EP2010/000586 priority patent/WO2010086186A1/en
Priority to JP2011546717A priority patent/JP5551184B2/en
Priority to RU2011136436/05A priority patent/RU2490133C2/en
Priority to US13/147,178 priority patent/US10131117B2/en
Priority to BRPI1007895A priority patent/BRPI1007895B1/en
Priority to KR1020117020574A priority patent/KR101658685B1/en
Priority to UAA201110594A priority patent/UA97934C2/en
Priority to EP10702612.2A priority patent/EP2391508B1/en
Priority to ES10702612T priority patent/ES2796928T3/en
Publication of WO2010085983A1 publication Critical patent/WO2010085983A1/en
Priority to ZA2011/05023A priority patent/ZA201105023B/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/012Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of aluminium or an aluminium alloy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/34Methods of heating
    • C21D1/40Direct resistance heating
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/34Methods of heating
    • C21D1/42Induction heating
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/62Quenching devices
    • C21D1/673Quenching devices for die quenching
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/68Temporary coatings or embedding materials applied before or during heat treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/68Temporary coatings or embedding materials applied before or during heat treatment
    • C21D1/70Temporary coatings or embedding materials applied before or during heat treatment while heating or quenching
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D7/00Modifying the physical properties of iron or steel by deformation
    • C21D7/13Modifying the physical properties of iron or steel by deformation by hot working
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/32Ferrous alloys, e.g. steel alloys containing chromium with boron
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/06Surface hardening
    • C21D1/08Surface hardening with flames
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/06Surface hardening
    • C21D1/09Surface hardening by direct application of electrical or wave energy; by particle radiation
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/002Bainite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the present invention pertains to a method for fabricating hot stamped parts prepared from steel sheet precoated with aluminium or an aluminium alloy, and to hot stamped coated products obtained by this method.
  • the use of a hot-stamping process of precoated sheets for the manufacturing of parts has become widespread especially in the automotive industry since it allows to produce parts with high mechanical resistance and good resistance to shocks.
  • the metallic precoating avoids oxidizing and decarburizing of the steel substrate during furnace heating before hot stamping. By interdiffusion between the precoating and the steel substrate, an intermetallic alloy with high melting temperature is formed in the coating. Heating temperature is chosen so as to austenitize the steel, thus further hardening of the steel substrate by quenching in the forming tools is also obtained.
  • European Patent Specification EP0971044 discloses a hot stamping process with steel sheets precoated with a coating on the basis of aluminium or aluminium alloy: the parts obtained after hot stamping offer high resistance to corrosion, to wear and fatigue, and are suitable for ulterior painting.
  • International Publication WO2008053273 discloses a hot stamping process wherein the heating and austenitizing steps in the furnace are chosen so as to obtain a succession of four distinctive layers in the coating of the stamped part: the heating rate for a temperature rise between 20 and 700 0 C is comprised between 4 and 12°C/s. This makes it possible to obtain improved spot weldability with this particular configuration of layers.
  • the pre-coated steel blanks are travelling on rollers in furnaces during heating before the hot stamping step.
  • the heating conditions of Al-precoated blanks are also chosen so as to avoid melting in the coating, which could lead to fouling of the rollers in the furnaces. As a consequence of fouling, the production line has sometimes to be temporarily stopped for maintenance, which reduces productivity.
  • the duration for heating and soaking of the blanks can be in the order of a few minutes.
  • the length of the furnaces where blanks are travelling can be quite important, which is a concern from an industrial point of view.
  • an object of this invention is a manufacturing process of a hot stamped coated part comprising the following successive steps, in this order :
  • a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, the precoating containing more than 50% of free aluminium and having a thickness comprised between 15 and 50 micrometers, then - cutting the steel sheet to obtain a precoated steel blank, then
  • V comprised between 3O 0 CVs and 90°C/s, V being the heating rate between the temperature Ti and the temperature T m , in order to obtain a coated heated blank, then
  • the heating rate V between the temperatures T 1 and T m is comprised between 50 and 8O 0 CVs.
  • the precoating comprises, by weight, 5- 11% Si, 2-4% Fe, optionally between 15 and 30ppm Ca, the remainder being aluminium and impurities inherent in processing, the temperature Tj is comprised between 567 and 577°C and the temperature T m is comprised between 855 and 950 0 C.
  • Another object of the invention is a manufacturing process of a hot stamped coated part, comprising the following successive steps, in this order : - providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, said precoating containing more than 50% of free aluminium and having a thickness comprised between 15 and 50 micrometers, then - cutting the steel sheet to obtain a precoated steel blank, then
  • the heating is performed at least partly by induction heating.
  • the heating is performed at least partly by resistance heating.
  • the heating is performed at least partly by infrared heating.
  • the heating is performed at least partly by gas burners.
  • the heating is performed by any combination of the heating processes above.
  • the total thickness of the coating is comprised between 20 and 22
  • the object of the invention is also a hot stamped coated part comprising a steel substrate having a microstructure comprising at least one constituent chosen among bainite or martensite, and a coating on each one of the two sides of said substrate, the coating being composed of the following layers, starting from the layer contiguous to said steel substrate : - a Fe 3 AI layer
  • the FeAI 3 layer containing a discontinuous minor phase of FeAI, atop of the FeAI layer.
  • FeAI layer atop of the Fe 3 AI layer has less than 13%Si in solid solution
  • FeAI 3 in the external layer has less than 6%Si in solid solution
  • the discontinuous minor phase of FeAI has less than 13%Si in solid solution.
  • the sum of thicknesses of the Fe 3 AI layer and the FeAI layer is less than one third of the total thickness of the coating.
  • the thickness of the coating on each one of said sides in comprised between 20 and 60 micrometers.
  • Figure 1 shows a cross section view of a structure of the coating of a hot stamped part according to the invention.
  • Figure 2 shows a cross section view of a layered structure of the coating of a hot stamped part obtained by a process non corresponding to the invention.
  • Figure 3 shows a top view of a surface of a coating manufactured according to the invention
  • Figure 4 and 5 illustrate top views of surfaces of coatings manufactured in conditions not corresponding to the invention
  • Figure 6 shows the nature of the coating and the liquid surfacic proportion at the end of the soaking period, as a function of heating rate.
  • the invention is implemented with precoated steel strips which comprise a strip, or substrate, of base steel and a precoating of aluminium or an aluminium alloy on both sides of the strip of the base steel.
  • precoating refers to the layer of aluminium or aluminium alloy deposited on the substrate which has not been heated, just before the step of hot stamping.
  • the heating cycle of Al-precoated sheet before hot forming and further soaking at high temperature cause a change in the nature and the morphology of the precoating, resulting from phase transformations and interdiffusion with the steel substrate.
  • Precoatings on the basis of aluminium or aluminium alloy may be obtained by continuous hot dip aluminizing through immersion of the steel sheet in a liquid bath of :
  • Al-Si Type I Aluminium, or Al-Si, containing, by weight, 5-11 % Si, 2-4% Fe, the remainder being aluminium, possibly between 15 and 30ppm Ca, and impurities inherent in processing. Silicon prevents the formation of a thick iron-metallic intermetallic layer which reduces adherence and formability.
  • Typical precoatings comprise, starting from the steel substrate, a very thin (usually less than 1 micrometer) interfacial layer with FeAI3 and Fe2AI5, atop a layer of ⁇ 5 phase (hexagonal phase of the type Fe 3 Si 2 AI 12 with mass concentrations of 29-36%Fe, 6-12%Si), usually 2-7 micrometers, and atop an Al-Si matrix including islands of eutectic Al-Fe-Si (Al dendrites, Si and ⁇ 6 (monoclinic phase of the type Fe 2 Si 2 AI 9 with 26-29%Fe and 13-16%Si in mass))
  • the invention is not limited to these compositions, however.
  • the thickness of Al precoating is comprised between 15 and 50 micrometers on each side. This range is chosen so as to obtain an optimal alloying of the precoating with the steel substrate according to the particular heating kinetics of the invention which will be presented below.
  • the precoating according to the invention contains more than 50% of free aluminium, as related to the total aluminium in the precoating. If such a condition is not fulfilled, a high quantity of aluminium is bound as a component with high melting point in the precoating, and there is no possibility to obtain sufficient melting under the heating conditions of the invention.
  • a sufficient proportion of mainly unalloyed Al, i.e. Al not bound with Fe or Si must be present.
  • An intermediate alloying thermal treatment after hot dip aluminizing and before heating and hot stamping prevents the possibility of implementing the invention, because this treatment would cause the formation of intermetallics with high melting point. Thus, a further heating before hot stamping would not cause a sufficient amount of melting in the coating for implementing the invention.
  • a further intermediate treatment might cause the formation of martensite in the substrate.
  • martensite has to be avoided in the steel substrate to minimise wear of the cutting tools.
  • damage may be induced around the cut edges due to the different intrinsic properties of these constituents.
  • the steel substrate composition is not critical as long as it displays good wettability when the sheet is hot dipped in the aluminium or aluminium alloy bath.
  • the steel substrate has a composition enabling the hot stamped part to obtain a high strength, for example ranging from 500 to 1600 MPa, depending on the requirements and usage conditions.
  • a steel composition comprising, by weight: 0.15% ⁇ C ⁇ 0.5%, 0.5% ⁇ Mn ⁇ 3%, 0.1 % ⁇ silicon ⁇ 0.5%, 0.01 % ⁇ Cr ⁇ 1%, Ni ⁇ 0.1%, C ⁇ O.1 %, Ti ⁇ 0.2%, AK0.1 %, PO.1 %, S ⁇ 0.05%, 0.0005% ⁇ B ⁇ 0.08%, and further containing iron and impurities inherent in processing, is preferred.
  • An example of a preferred commercially available steel for use in the strip of base steel is 22MnB5.
  • a steel composition comprising 0.040% ⁇ C ⁇ 0.100%, 0.80% ⁇ Mn ⁇ 2.00%, Si ⁇ 0.30%, S ⁇ 0.005%, P ⁇ 0.030%, 0.010% ⁇ Al ⁇ 0.070%, 0.015% ⁇ Nb ⁇ 0.100%, 0.030% ⁇ Ti ⁇ 0.080%, N ⁇ 0.009%, Cu ⁇ 0.100%, Ni ⁇ 0.100%, Cr ⁇ 0.100%, Mo ⁇ 0.100%, Ca ⁇ 0.006%, and further containing iron and impurities inherent in processing, is preferred.
  • the steel strip can be fabricated from a hot-rolling mill, and optionally may be cold-rolled again depending on the final thickness desired. Thicknesses may vary, for example, in the range between 0.7 to 3 mm.
  • Precoated strips are thereafter cut into precoated blanks in view of the subsequent hot stamping step.
  • the inventors have discovered that particular heating and soaking conditions give rise to particular coating microstructure and properties. These conditions are the following :
  • the blanks have to be heated under a non protective atmosphere up to an intermediate temperature Tj comprised between T e -
  • T e designates the solidus temperature of the precoating or, if this precoating solidifies with an eutectic mode, the eutectic temperature.
  • heating is performed up to a temperature just slightly inferior to the melting temperature of the precoating.
  • the eutectic temperature T e of the precoating is around 577°C.
  • This first heating step is not too critical since it occurs in a low temperature range where alloying kinetics is slow, and a wide range of heating rates and heating processes may be used in this first step.
  • This first heating step may be either performed with the same heating means than the following one, or by using separate heating means or devices.
  • the second step, following immediately the first one, is specially important for controlling the nature of the sequence of transformations in the precoating.
  • the heating rate V between Tj and an austenitizing temperature T m must be particularly controlled.
  • temperature T m has to be higher than 840 0 C for enabling the full transformation of austenite of the steel substrate. This temperature of 840° C makes it also possible for the pehtectic transformation to occur and causes the disappearance of the ⁇ 5 phase in the precoating. In the case of an Al-Si precoating (5-11 % Si, 2-4% Fe), the temperature T m has to be higher than 855 0 C.
  • T m has to be limited below 95O 0 C in order to prevent excessive aluminium oxide formation at the surface of the precoating, and/or unacceptable melting of the precoating.
  • T m must be comprised between 840 and 95O 0 C or 855 and 950 0 C for an Al-Si precoating.
  • the heating rate V must be higher or equal to 30°C/s: if the heating rate is too slow, a too high proportion of liquid is formed at the surface of the precoating at the end of the heating step and before the ulterior soaking. Thus, drops of precoating are susceptible to flow and to foul the rollers in the furnace with this high proportion of molten precoating. Furthermore, a slow heating rate favours the formation of a final coating composed of 4 or 5 layers. This layer disposition is less favourable than the coating of the invention from the point of view of resistance to deformation since the increase of the interfaces between the different phases and the increase in hardness gradients lowers the resistance to spalling.
  • the coating of the invention has not more than 3 layers. While not bound by a particular theory, it is believed that the reduction in the number of layers with different intrinsic properties lowers the formation of residual stresses, and thus the resistance to deformation.
  • the surface of the precoating is molten to a large extent when the temperature T m is reached.
  • the composition is locally enriched in Si, and further transformation occurs in the form of a ternary eutectic (Al-Si-Fe) with low melting point so that the surface of the precoating remains mainly liquid during the soaking at temperature T m .
  • the surface of the coating formed at the end of this soaking, resulting from the transformation of the precoating is mainly smooth and has a poor aptitude for ulterior painting.
  • the precoating is molten to an adequate extent on its surface and the kinetics of transformation are accelerated to such a high extent as to enable the transformation of the liquid phase into Fe and Al based intermetallic.
  • This high transformation kinetics also hampers the formation of a 4 or 5 layers structure in the coating.
  • a more compact coating is produced with less stratified layers. This brings an advantage because less interfaces are produced, which would induce in turn a higher mechanical resistance due to increased homogeneity.
  • the coating thus obtained is mainly composed of FeAI 3 .
  • the heating rate is comprised between 50 and 80 0 CVs 1 this character of compactness is more specially developed and the FeAI3 layer is for the most part present.
  • Figure 6 indicates that the specific range of heating rate of the invention makes it possible to obtain simultaneously a proportion of liquid at the surface lower than 30% at the end of the soaking, and a coating having not more than three layers.
  • Soaking is performed at temperature T m during a period of time tm comprised between 20 and 90s.
  • This soaking period enables the transformation of a fraction or the totality of the liquid phase at the surface of the precoating, into a coating having a majority of FeAI 3 intermetallics at its surface.
  • This soaking period enables also the full transformation of the steel substrate into austenite and the homogenisation of the austenite grain. This in turn makes it possible to obtain mechanical homogeneity on the final part.
  • This soaking period is shorter than for usual treatments, which in turn increases productivity.
  • Hot stamping is thus performed to obtain a stamped part. Cooling may be performed either in the hot stamping tooling itself, or partly after hot stamping and transfer of the part in a special cooling device.
  • the part is cooled with a cooling rate chosen, according to steel composition, so as to obtain martensite or bainite, or a combination of these constituents, which makes it possible to obtain parts with high mechanical resistance.
  • the heating rate between T 1 and T m is chosen so as to obtain between 10 and 60% of liquid phase at the surface of the precoating at temperature T m , before the beginning of soaking : if the surface proportion of liquid phase is higher than 60%, the risk of fouling of the rollers to occur in the furnaces becomes important.
  • the precoating does not melt completely in its thickness and, due to surface tension of the precoating, the drops of liquid aluminium are less susceptible to flow on the rollers, or susceptible to flow on a limited number of rollers because of much less liquid ratio to transform.
  • soaking time at T m is chosen so as to transform isothermally this liquid phase for obtaining a heated blank with a coating having less than 30% of liquid phase on its surface at the end of said soaking period, and comprising by weight between 20 and 50% Fe on its surface.
  • the proportion of liquid on the surface is limited to 30% so as to obtain a rough surface on the final part.
  • An iron content less than 20% on the surface of the coating indicates an insufficient number of intermetallic crystals at the surface of the coating. When the Fe content is higher than 50%, the resistance to corrosion of the stamped part tends to be reduced.
  • the coating obtained on the hot stamped part according to the conditions of the invention is composed of (starting from the steel substrate):
  • This intermetallic phase contains less than 6% Si in solid solution.
  • This FeAI 3 layer which constitutes the majority of the coating, contains a minor phase under the form of discontinuous islands of FeAI.
  • This last phase contains less than 13%Si in solid solution.
  • this external layer is the large main constituent of the coating, i.e. when the sum of the thicknesses of the Fe 3 AI layer and the FeAI layer is less than one third of the total coating thickness.
  • the total coating thickness on the stamped part ranges from 20 to 60 micrometers.
  • an unalloyed layer 21 micrometers thick, with a matrix of Al-Si with composition above. Its structure is composed of Al dendrites including Si and Fe in solid solution and islands of Al-Si eutectic. This unalloyed layer occupies about 80% of the precoating thickness.
  • the eutectic melting temperature T e of this precoating is 577 0 C.
  • the thickness of the precoating was 15 micrometers.
  • the sheets were cut into blanks which were heated, hot stamped and rapidly cooled so as to obtain parts with a steel substrate fully composed of martensite.
  • Heating was performed under a non protective (usual) atmosphere using different techniques:
  • SEM Scanning Electron Microscope
  • the liquid phase proportion after soaking was determined on the hot stamped and cooled part with similar SEM observations of the coating surfaces, and quantification: the coatings may present a variable surfacic fraction of liquid at the end of the soaking step, the remaining fraction is constituted of crystallised intermetallic phases.
  • a high percentage of crystals emerging at the surface indicates good adhesion of further painting treatments (cataphoresis) This is also characterized by the criterion of smooth or uneven surface (low or high aptitude to painting).
  • the iron content was measured on the surface of the coating of the hot stamped and cooled part, using the technique of X-ray diffraction with low incidence angle.
  • the iron content of the liquid phase on the surface of the coating at the end of the soaking step is identical to the iron content of the coating, after the ulterior hot stamping and cooling steps.
  • Figure 1 illustrates an example of coating according to test condition H, corresponding to the invention: starting from the steel substrate (indicated by
  • the coating is composed of a 5 micrometers Fe 3 AI layer
  • This external layer is composed of 80% of FeAI 3 and 20% of FeAI. These percentages refer to the surfacic proportion which can be measured from image analysis on a cross-section microstructure of the coating, lntermetallic FeAI 3 contains 3% by weight Si in solid solution. FeAI (indicated by 5), in the form of discontinuous islands, contains 9%Si in solid solution. Similar microstructures are also observed in the other tests corresponding to the conditions of invention.
  • test B has been performed with a too low heating rate and soaking time ta, on a precoating of insufficient thickness.
  • Test F has been performed with a too high temperature T m and a too short soaking time : thus, the percentage of liquid before and after soaking is excessive.
  • Figure 4 illustrates the surface obtained in test L : Even if crystals are more present than in this case, adherence for painting is still insufficient.
  • the particular conditions of the invention lead to a favourable combination of layer disposition and a low surfacic proportion of liquid at the end of the soaking period, as indicated in figure 6. This in turn leads to good resistance to corrosion and wear, high mechanical resistance and weldability.
  • the productivity of the manufacturing process is significantly increased, since both the heating phases and the soaking times are reduced, which allows to design more compact hot stamping lines. Taking advantage of their characteristics, the hot stamped parts manufactured according to the invention will be used with profit in the automobile industry.

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Abstract

A manufacturing process of a hot stamped coated part comprising the following successive steps, in this order: providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, the precoating containing more than 50% of free aluminium and having a thickness comprised between 15 and 50 micrometers, then cutting the steel sheet to obtain a precoated steel blank, then heating the blank under non protective atmosphere up to a temperature Ti comprised between Te- 10°C and Te, Te being the eutectic or solidus temperature of the precoating, then heating the blank from the temperature Ti up to a temperature Tm comprised between 840 and 950°C under non protective atmosphere with a heating rate V comprised between 30°C/s and 90°C/s, V being the heating rate between the temperature Ti and the temperature Tm, in order to obtain a coated heated blank, then soaking the coated heated blank at said temperature Tm for a time tm comprised between 20s and 90s, then hot stamping the blank in order to obtain a hot stamped coated part, then cooling said stamped part at a cooling rate in order to form a microstructure in the steel substrate comprising at least one constituent chosen among martensite or bainite.

Description

FABRICATION PROCESS OF COATED STAMPED PARTS AND PARTS
PREPARED FROM THE SAME
The present invention pertains to a method for fabricating hot stamped parts prepared from steel sheet precoated with aluminium or an aluminium alloy, and to hot stamped coated products obtained by this method. The use of a hot-stamping process of precoated sheets for the manufacturing of parts has become widespread especially in the automotive industry since it allows to produce parts with high mechanical resistance and good resistance to shocks. The metallic precoating avoids oxidizing and decarburizing of the steel substrate during furnace heating before hot stamping. By interdiffusion between the precoating and the steel substrate, an intermetallic alloy with high melting temperature is formed in the coating. Heating temperature is chosen so as to austenitize the steel, thus further hardening of the steel substrate by quenching in the forming tools is also obtained. European Patent Specification EP0971044 discloses a hot stamping process with steel sheets precoated with a coating on the basis of aluminium or aluminium alloy: the parts obtained after hot stamping offer high resistance to corrosion, to wear and fatigue, and are suitable for ulterior painting.
International Publication WO2008053273 discloses a hot stamping process wherein the heating and austenitizing steps in the furnace are chosen so as to obtain a succession of four distinctive layers in the coating of the stamped part: the heating rate for a temperature rise between 20 and 7000C is comprised between 4 and 12°C/s. This makes it possible to obtain improved spot weldability with this particular configuration of layers. The pre-coated steel blanks are travelling on rollers in furnaces during heating before the hot stamping step. According to International Publication WO2008053273, the heating conditions of Al-precoated blanks are also chosen so as to avoid melting in the coating, which could lead to fouling of the rollers in the furnaces. As a consequence of fouling, the production line has sometimes to be temporarily stopped for maintenance, which reduces productivity.
Furthermore, the duration for heating and soaking of the blanks can be in the order of a few minutes. As a consequence, the length of the furnaces where blanks are travelling can be quite important, which is a concern from an industrial point of view. Thus, there is an important need to shorten the length of the heating lines.
Attempts have been performed to increase the productivity of the process by shortening the soaking duration at the austenitizing temperature: however, this approach has found its limits since a sufficient time is necessary for the interdiffusion of steel substrate elements, in particular iron, with the aluminium based coating. Furthermore, reduction of the heating time is also a problem since melting of the coating is experienced for the very rapid heating rates, thus leading to a smooth surface of the coating and poor adhesion of painting on the stamped part.
Thus, starting from Al based precoated steel sheets, there remains a need for a manufacturing process making it possible to prepare stamped parts or products with high mechanical resistance, and which offers superior ability to ulterior painting. There remains also a need for a process which makes it possible to obtain parts whose coating is very adherent to the substrate at fabrication or service temperatures, and offers superior resistance to spalling and corrosion. There remains also a need for a process with enhanced productivity, which makes it possible to avoid rollers fouling. It is an object of the present invention to solve the above mentioned problems and to provide a novel process for producing hot stamped parts prepared from an aluminium based or aluminium alloy pre-coated steel sheet. It is another object of the present invention to provide a process for fabrication of hot stamped parts which can be used in a motor vehicle. It is another object of the present invention to provide novel methods of making stamped parts whose coatings combine high adherence to the steel substrate, ability for painting and resistance to spalling. It is another object of the invention to provide a part with a novel coating after hot stamping, which combines high ability for painting and resistance to spalling and corrosion.
Thus, an object of this invention is a manufacturing process of a hot stamped coated part comprising the following successive steps, in this order :
- providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, the precoating containing more than 50% of free aluminium and having a thickness comprised between 15 and 50 micrometers, then - cutting the steel sheet to obtain a precoated steel blank, then
- heating the blank under a non protective atmosphere up to a temperature Tj comprised between Te-10°C and Te, Te being the eutectic or solidus temperature of the precoating, then
- heating the blank from the temperature T1 up to a temperature Tm comprised between 840 and 9500C under a non protective atmosphere at a heating rate
V comprised between 3O0CVs and 90°C/s, V being the heating rate between the temperature Ti and the temperature Tm, in order to obtain a coated heated blank, then
- soaking the coated heated blank at said temperature Tm for a time U comprised between 20s and 90s, then
- hot stamping the blank in order to obtain a hot stamped coated part, then
- cooling said stamped part at a cooling rate in order to form a microstructure in the steel substrate comprising at least one constituent chosen among martensite or bainite. According to a preferred embodiment, the heating rate V between the temperatures T1 and Tm is comprised between 50 and 8O0CVs. According to a preferred embodiment, the precoating comprises, by weight, 5- 11% Si, 2-4% Fe, optionally between 15 and 30ppm Ca, the remainder being aluminium and impurities inherent in processing, the temperature Tj is comprised between 567 and 577°C and the temperature Tm is comprised between 855 and 9500C.
Another object of the invention is a manufacturing process of a hot stamped coated part, comprising the following successive steps, in this order : - providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, said precoating containing more than 50% of free aluminium and having a thickness comprised between 15 and 50 micrometers, then - cutting the steel sheet to obtain a precoated steel blank, then
- heating the steel blank under non-protective atmosphere at a heating rate V up to a temperature Tm, in order to fully transform the steel substrate microstructure into austenite and to obtain, immediately after heating and prior to ulterior soaking, between 10 and 60% of liquid phase on the surface of the precoating, then,
- transforming the liquid phase of precoating at the temperature Tm during a soaking period U in order to obtain a coated heated blank with coating having less than 30% of liquid phase on its surface at the end of said soaking period, and comprising by weight between 20 and 50% Fe on its surface, then - hot stamping the blank in order to obtain a hot stamped part, then
- cooling the stamped part in order to form a microstructure in said steel substrate comprising at least one constituent chosen among martensite or bainite.
Preferentially, the heating is performed at least partly by induction heating. According to a preferential mode, the heating is performed at least partly by resistance heating.
Preferentially, the heating is performed at least partly by infrared heating.
According to a preferential mode, the heating is performed at least partly by gas burners. In a particular mode, the heating is performed by any combination of the heating processes above.
Preferentially, the total thickness of the coating is comprised between 20 and
60 micrometers.
The object of the invention is also a hot stamped coated part comprising a steel substrate having a microstructure comprising at least one constituent chosen among bainite or martensite, and a coating on each one of the two sides of said substrate, the coating being composed of the following layers, starting from the layer contiguous to said steel substrate : - a Fe3AI layer
- a FeAI layer atop of the Fe3AI layer
- an external layer composed of more than 70% of FeAI3, the FeAI3 layer containing a discontinuous minor phase of FeAI, atop of the FeAI layer. Preferentially, FeAI layer atop of the Fe3AI layer has less than 13%Si in solid solution, FeAI3 in the external layer has less than 6%Si in solid solution, and the discontinuous minor phase of FeAI has less than 13%Si in solid solution. Preferentially, the sum of thicknesses of the Fe3AI layer and the FeAI layer is less than one third of the total thickness of the coating. In a preferential mode, the thickness of the coating on each one of said sides in comprised between 20 and 60 micrometers.
Preferentially, 70% the surface of the external layer is composed of crystals. Other advantages and characteristics will appear in the description and exemplary embodiments below, in reference to the joint figures : Figure 1 shows a cross section view of a structure of the coating of a hot stamped part according to the invention.
Figure 2 shows a cross section view of a layered structure of the coating of a hot stamped part obtained by a process non corresponding to the invention. Figure 3 shows a top view of a surface of a coating manufactured according to the invention
Figure 4 and 5 illustrate top views of surfaces of coatings manufactured in conditions not corresponding to the invention
Figure 6 shows the nature of the coating and the liquid surfacic proportion at the end of the soaking period, as a function of heating rate. The invention is implemented with precoated steel strips which comprise a strip, or substrate, of base steel and a precoating of aluminium or an aluminium alloy on both sides of the strip of the base steel. The term "precoating" refers to the layer of aluminium or aluminium alloy deposited on the substrate which has not been heated, just before the step of hot stamping. As will be explained below, the heating cycle of Al-precoated sheet before hot forming and further soaking at high temperature cause a change in the nature and the morphology of the precoating, resulting from phase transformations and interdiffusion with the steel substrate. These transformations and intend iffusion mechanisms give rise to the formation of an optimum coating on the surface of the hot stamped parts. Precoatings on the basis of aluminium or aluminium alloy may be obtained by continuous hot dip aluminizing through immersion of the steel sheet in a liquid bath of :
- Type I Aluminium, or Al-Si, containing, by weight, 5-11 % Si, 2-4% Fe, the remainder being aluminium, possibly between 15 and 30ppm Ca, and impurities inherent in processing. Silicon prevents the formation of a thick iron-metallic intermetallic layer which reduces adherence and formability. Typical precoatings comprise, starting from the steel substrate, a very thin (usually less than 1 micrometer) interfacial layer with FeAI3 and Fe2AI5, atop a layer of τ5 phase (hexagonal phase of the type Fe3Si2AI12 with mass concentrations of 29-36%Fe, 6-12%Si), usually 2-7 micrometers, and atop an Al-Si matrix including islands of eutectic Al-Fe-Si (Al dendrites, Si and τ6 (monoclinic phase of the type Fe2Si2AI9 with 26-29%Fe and 13-16%Si in mass))
- Type Il Aluminium, containing 2-4% iron without Si.
The invention is not limited to these compositions, however.
The thickness of Al precoating is comprised between 15 and 50 micrometers on each side. This range is chosen so as to obtain an optimal alloying of the precoating with the steel substrate according to the particular heating kinetics of the invention which will be presented below.
The precoating according to the invention contains more than 50% of free aluminium, as related to the total aluminium in the precoating. If such a condition is not fulfilled, a high quantity of aluminium is bound as a component with high melting point in the precoating, and there is no possibility to obtain sufficient melting under the heating conditions of the invention. In other words, after hot dip aluminizing, a sufficient proportion of mainly unalloyed Al, i.e. Al not bound with Fe or Si, must be present. An intermediate alloying thermal treatment after hot dip aluminizing and before heating and hot stamping prevents the possibility of implementing the invention, because this treatment would cause the formation of intermetallics with high melting point. Thus, a further heating before hot stamping would not cause a sufficient amount of melting in the coating for implementing the invention.
Additionally, a further intermediate treatment might cause the formation of martensite in the substrate. As cutting or punching of the sheets into the blanks must be performed, martensite has to be avoided in the steel substrate to minimise wear of the cutting tools. Furthermore, when martensite-ferrite interfaces are present in the substrate microstructure, damage may be induced around the cut edges due to the different intrinsic properties of these constituents. The steel substrate composition is not critical as long as it displays good wettability when the sheet is hot dipped in the aluminium or aluminium alloy bath. However, for certain applications requiring high mechanical strength, such as structural parts in cars, it is preferred that the steel substrate has a composition enabling the hot stamped part to obtain a high strength, for example ranging from 500 to 1600 MPa, depending on the requirements and usage conditions. When higher levels of resistance are aimed at, a steel composition comprising, by weight: 0.15%<C<0.5%, 0.5%<Mn<3%, 0.1 %<silicon<0.5%, 0.01 %<Cr<1%, Ni<0.1%, CικO.1 %, Ti<0.2%, AK0.1 %, PO.1 %, S<0.05%, 0.0005%<B<0.08%, and further containing iron and impurities inherent in processing, is preferred. An example of a preferred commercially available steel for use in the strip of base steel is 22MnB5. When a level of strength in the range of 500MPa is desired, a steel composition comprising 0.040% < C < 0.100%, 0.80% < Mn < 2.00%, Si < 0.30%, S < 0.005%, P< 0.030%, 0.010% < Al < 0.070%, 0.015% < Nb < 0.100%, 0.030% < Ti< 0.080%, N < 0.009%, Cu < 0.100%, Ni < 0.100%, Cr < 0.100%, Mo < 0.100%, Ca < 0.006%, and further containing iron and impurities inherent in processing, is preferred
The steel strip can be fabricated from a hot-rolling mill, and optionally may be cold-rolled again depending on the final thickness desired. Thicknesses may vary, for example, in the range between 0.7 to 3 mm.
Precoated strips are thereafter cut into precoated blanks in view of the subsequent hot stamping step. The inventors have discovered that particular heating and soaking conditions give rise to particular coating microstructure and properties. These conditions are the following :
- As a first step, the blanks have to be heated under a non protective atmosphere up to an intermediate temperature Tj comprised between Te-
100C and Te. Te designates the solidus temperature of the precoating or, if this precoating solidifies with an eutectic mode, the eutectic temperature. Thus, heating is performed up to a temperature just slightly inferior to the melting temperature of the precoating. For example, in the case of an Al-Si precoating comprising 5-11 % Si and 2-4% iron, the eutectic temperature Te of the precoating is around 577°C. This first heating step is not too critical since it occurs in a low temperature range where alloying kinetics is slow, and a wide range of heating rates and heating processes may be used in this first step. This first heating step may be either performed with the same heating means than the following one, or by using separate heating means or devices.
- the second step, following immediately the first one, is specially important for controlling the nature of the sequence of transformations in the precoating. In particular, the heating rate V between Tj and an austenitizing temperature Tm, must be particularly controlled.
- First, temperature Tm has to be higher than 8400C for enabling the full transformation of austenite of the steel substrate. This temperature of 840° C makes it also possible for the pehtectic transformation to occur and causes the disappearance of the τ5 phase in the precoating. In the case of an Al-Si precoating (5-11 % Si, 2-4% Fe), the temperature Tm has to be higher than 8550C.
But the temperature Tm has to be limited below 95O0C in order to prevent excessive aluminium oxide formation at the surface of the precoating, and/or unacceptable melting of the precoating. Thus, Tm must be comprised between 840 and 95O0C or 855 and 9500C for an Al-Si precoating.
- Then, the heating rate V must be higher or equal to 30°C/s: if the heating rate is too slow, a too high proportion of liquid is formed at the surface of the precoating at the end of the heating step and before the ulterior soaking. Thus, drops of precoating are susceptible to flow and to foul the rollers in the furnace with this high proportion of molten precoating. Furthermore, a slow heating rate favours the formation of a final coating composed of 4 or 5 layers. This layer disposition is less favourable than the coating of the invention from the point of view of resistance to deformation since the increase of the interfaces between the different phases and the increase in hardness gradients lowers the resistance to spalling. The coating of the invention has not more than 3 layers. While not bound by a particular theory, it is believed that the reduction in the number of layers with different intrinsic properties lowers the formation of residual stresses, and thus the resistance to deformation.
If the heating rate V is higher than 900CVs1 the surface of the precoating is molten to a large extent when the temperature Tm is reached. The composition is locally enriched in Si, and further transformation occurs in the form of a ternary eutectic (Al-Si-Fe) with low melting point so that the surface of the precoating remains mainly liquid during the soaking at temperature Tm. Thus, the surface of the coating formed at the end of this soaking, resulting from the transformation of the precoating, is mainly smooth and has a poor aptitude for ulterior painting. When the heating rate V is comprised between 30 and 90°C/s, the precoating is molten to an adequate extent on its surface and the kinetics of transformation are accelerated to such a high extent as to enable the transformation of the liquid phase into Fe and Al based intermetallic. This high transformation kinetics also hampers the formation of a 4 or 5 layers structure in the coating. A more compact coating is produced with less stratified layers. This brings an advantage because less interfaces are produced, which would induce in turn a higher mechanical resistance due to increased homogeneity. In particular, the coating thus obtained is mainly composed of FeAI3. When the heating rate is comprised between 50 and 800CVs1 this character of compactness is more specially developed and the FeAI3 layer is for the most part present.
Figure 6 indicates that the specific range of heating rate of the invention makes it possible to obtain simultaneously a proportion of liquid at the surface lower than 30% at the end of the soaking, and a coating having not more than three layers.
Soaking is performed at temperature Tm during a period of time tm comprised between 20 and 90s. This soaking period enables the transformation of a fraction or the totality of the liquid phase at the surface of the precoating, into a coating having a majority of FeAI3 intermetallics at its surface. This soaking period enables also the full transformation of the steel substrate into austenite and the homogenisation of the austenite grain. This in turn makes it possible to obtain mechanical homogeneity on the final part. This soaking period is shorter than for usual treatments, which in turn increases productivity.
After the soaking period, the heated blank is transferred from the furnace to a hot stamping device. Hot stamping is thus performed to obtain a stamped part. Cooling may be performed either in the hot stamping tooling itself, or partly after hot stamping and transfer of the part in a special cooling device. The part is cooled with a cooling rate chosen, according to steel composition, so as to obtain martensite or bainite, or a combination of these constituents, which makes it possible to obtain parts with high mechanical resistance.
According to one form of the invention, the heating rate between T1 and Tm is chosen so as to obtain between 10 and 60% of liquid phase at the surface of the precoating at temperature Tm, before the beginning of soaking : if the surface proportion of liquid phase is higher than 60%, the risk of fouling of the rollers to occur in the furnaces becomes important. A minimal proportion of
10% is desired for being adapted to the lower thickness (15 micrometers) of the precoating in the invention. While not bound by a particular theory, it is believed that, under these particular conditions, the precoating does not melt completely in its thickness and, due to surface tension of the precoating, the drops of liquid aluminium are less susceptible to flow on the rollers, or susceptible to flow on a limited number of rollers because of much less liquid ratio to transform.
Then, soaking time at Tm is chosen so as to transform isothermally this liquid phase for obtaining a heated blank with a coating having less than 30% of liquid phase on its surface at the end of said soaking period, and comprising by weight between 20 and 50% Fe on its surface. The proportion of liquid on the surface is limited to 30% so as to obtain a rough surface on the final part. An iron content less than 20% on the surface of the coating indicates an insufficient number of intermetallic crystals at the surface of the coating. When the Fe content is higher than 50%, the resistance to corrosion of the stamped part tends to be reduced.
The coating obtained on the hot stamped part according to the conditions of the invention is composed of (starting from the steel substrate):
- a thin Fβ3AI layer - a very thin FeAI layer with less than 13% Si in solid solution, atop of the said Fe3AI layer
- an external layer composed of more than 70% of FeAI3 . This intermetallic phase contains less than 6% Si in solid solution. This FeAI3 layer, which constitutes the majority of the coating, contains a minor phase under the form of discontinuous islands of FeAI. This last phase contains less than 13%Si in solid solution.
Particularly good adhesion properties are observed when this external layer is the large main constituent of the coating, i.e. when the sum of the thicknesses of the Fe3AI layer and the FeAI layer is less than one third of the total coating thickness. The total coating thickness on the stamped part ranges from 20 to 60 micrometers.
Similarly, excellent paint adhesion is obtained when the coating displays, on its surface, more than 70% of intermetallic crystals, this percentage being expressed in surfacic proportion.
Examples:
Cold rolled steel sheets with thickness of 1 and 2mm, with steel composition comprising, in weight, 0.22%C, 1.2%Mn, 0.2%Si, 0.2%Cr, 0.040%AI, 0.003%B, 0.030%Ti, 0.0002%S, 0.020%P, the remainder being iron and impurities inherent in processing, were supplied. The microstructure is composed of ferrite-pearlite. At this stage, the absence of martensite enables easy further cutting, drilling or punching of the sheets. These steel sheets have been precoated by continuous immersion of the sheet in an Al-Si liquid bath. A precoating, 27 micrometers thick, comprising by weight 9%Si, 3%Fe, the remainder being aluminium and impurities inherent in processing, is thus obtained. This precoating is composed of : - A thin layer (less than 1 micrometer) of FeAI3 and Fe2AI5, directly in contact with the steel substrate.
- Atop of this layer, a layer of intermetallic τ5 with hexagonal structure, 5 micrometers thick
- Atop of this layer, an unalloyed layer, 21 micrometers thick, with a matrix of Al-Si with composition above. Its structure is composed of Al dendrites including Si and Fe in solid solution and islands of Al-Si eutectic. This unalloyed layer occupies about 80% of the precoating thickness.
Thus, Al is mostly free in this precoating, which indicates the possibility of sufficient ulterior melting in the heat treatment. The eutectic melting temperature Te of this precoating is 5770C.
In one testing condition referenced as "B" in table 1 below, the thickness of the precoating was 15 micrometers.
The sheets were cut into blanks which were heated, hot stamped and rapidly cooled so as to obtain parts with a steel substrate fully composed of martensite.
Heating was performed under a non protective (usual) atmosphere using different techniques:
- Heating by radiation in a resistance furnace - Heating in a furnace with gas burners
- Heating within an infrared furnace
- Induction heating
- Resistance heating, where sheets were maintained within conductive jaws and heated by Joule effect. Heating was performed up to a temperature Tj of 575°C (i.e. Te - 2°C), then up to a temperature Tm where soaking was eventually performed. The heating rate V from temperature T1 up to temperature Tm was controlled. Table 1 presents the different parameters of the tests and the results obtained.
The liquid phase percentage on the precoating surface after heating at Tm, and before the soaking step, was determined by examinations with a Scanning Electron Microscope (SEM) at 500X magnification, of the surfaces of specimens after interrupted quench at the temperature Tm before the soaking step: areas with liquid phase which existed at temperature Tm are characterized by a smooth surface and may be distinguished from crystallized phases which have a rough appearance (emerging single crystals).
The liquid phase proportion after soaking was determined on the hot stamped and cooled part with similar SEM observations of the coating surfaces, and quantification: the coatings may present a variable surfacic fraction of liquid at the end of the soaking step, the remaining fraction is constituted of crystallised intermetallic phases. A high percentage of crystals emerging at the surface indicates good adhesion of further painting treatments (cataphoresis) This is also characterized by the criterion of smooth or uneven surface (low or high aptitude to painting). The iron content was measured on the surface of the coating of the hot stamped and cooled part, using the technique of X-ray diffraction with low incidence angle. The iron content of the liquid phase on the surface of the coating at the end of the soaking step is identical to the iron content of the coating, after the ulterior hot stamping and cooling steps.
Figure imgf000015_0001
Table 1 Testing conditions and results obtained. Underlined values indicate conditions outside of the invention, n.d: not determined.
[1] Nature : I= corresponding to the invention R= Reference.
[2] Heating process for heating from Tj (575°C) to Tn, . FB= Furnace with burners heating. IF= Infrared heating. IN= Induction heating. R= Resistance heating (Joule effect) RF: Furnace heated by resistance.
[3] Liquid phase proportion on the surface of the precoating after heating at Tm, and before the soaking step.
[4] Liquid phase proportion on the surface of the coating after soaking at Tm.
[5] Iron content (% by weight) on the surface of the coating.
[6] Characterizes a coating having a three-layer structure with FeAI3 crystals on its surface. Tests C to E and G to I correspond to the conditions of the invention.
Figure 1 illustrates an example of coating according to test condition H, corresponding to the invention: starting from the steel substrate (indicated by
1 on the figure 1 ), the coating is composed of a 5 micrometers Fe3AI layer
(indicated as 2), a very thin (less than 1 micrometer) FeAI layer (indicated by
3) with 7% Si by weight in solid solution, and an external layer of 25 micrometers (indicated by 4) constituting more than 80% of the total thickness of the coating. This external layer is composed of 80% of FeAI3 and 20% of FeAI. These percentages refer to the surfacic proportion which can be measured from image analysis on a cross-section microstructure of the coating, lntermetallic FeAI3 contains 3% by weight Si in solid solution. FeAI (indicated by 5), in the form of discontinuous islands, contains 9%Si in solid solution. Similar microstructures are also observed in the other tests corresponding to the conditions of invention.
SEM observations (fig. 3) indicate a surface fully covered by crystals, mainly FeAI3. For a heating rate of 30CVs (test A) or 15°C/s (test B) the coating structure is composed of 5 layers, as illustrated in figure 2: starting from the substrate (indicated by 6) the coating is composed of Fe3AI layer (indicated by 7), FeAI (8), FeAI3 (9), FeAI (10) and FeAI3 (11 ) layers. Even if this layer disposition offers good weldability, its compactness is inferior to the one of the invention. It is also to mention that the main constituent of the external layer (i.e. FeAI3) is similar in figure 1 and figure 2, which indicates also the stability of the welding range in the conditions of invention. However, the conditions of the invention make it possible to obtain a compact layer, specially marked for test conditions D1E, G, H, I. Under the conditions of the invention, more than 70% of crystals are present on the surface of the coating, together with an iron content comprised between 20 and 50% on the surface of the external layer. This indicates a good aptitude for ulterior painting. Test B has been performed with a too low heating rate and soaking time ta, on a precoating of insufficient thickness. As a consequence, the liquid phase proportion at the end of the heating step is insufficient and the nature of the final coating is not corresponding to the invention. Test F has been performed with a too high temperature Tm and a too short soaking time : thus, the percentage of liquid before and after soaking is excessive. Furthermore, aluminium oxide has formed due to too high temperature. Its presence at the surface of the coating lowers weldability. Tests J to N have been heated at too high heating rates, from 100 to 180°C/s. Figure 5 illustrates the surface obtained in the test N, where the coating is fully covered of liquid after soaking at Tm. This coating displays very low adherence for ulterior cataphoresis.
Figure 4 illustrates the surface obtained in test L : Even if crystals are more present than in this case, adherence for painting is still insufficient. Thus, the particular conditions of the invention lead to a favourable combination of layer disposition and a low surfacic proportion of liquid at the end of the soaking period, as indicated in figure 6. This in turn leads to good resistance to corrosion and wear, high mechanical resistance and weldability. Furthermore, the productivity of the manufacturing process is significantly increased, since both the heating phases and the soaking times are reduced, which allows to design more compact hot stamping lines. Taking advantage of their characteristics, the hot stamped parts manufactured according to the invention will be used with profit in the automobile industry.

Claims

1. A manufacturing process of a hot stamped coated part comprising the following successive steps, in this order :
- providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, said precoating containing more than 50% of free aluminium and having a thickness selected to enable alloying with said steel substrate, said thickness being preferably comprised between 15 and 50 micrometers, then
- cutting said steel sheet to obtain a precoated steel blank, then
- heating said blank under a non protective atmosphere up to a temperature Tj near the melting temperature of said precoating, said temperature Ti being preferably comprised between Te-10°C and Te, where Te is the eutectic or solidus temperature of said precoating, then
- heating said blank from said temperature Ti up to an austenitization temperature Tm of said steel substrate, said temperature Tm being preferably comprised between 840 and 9500C, under a non-protective atmosphere at a heating rate V comprised between 30°C/s and 90°C/s, V being the heating rate between said temperature T1 and said temperature Tm, in order to obtain a coated heated blank, then
- soaking said coated heated blank at said temperature Tm for a time tm comprised between 20s and 90s, then
- hot stamping said blank in order to obtain a hot stamped coated part, then - cooling said stamped part at a cooling rate in order to form a microstructure in said steel substrate comprising at least one constituent chosen among martensite or bainite.
2. A manufacturing process according to claim 1 wherein said heating rate V between said temperatures Tj and Tm is comprised between 50 and 80°C/s.
3. A manufacturing process according to any of the claims 1 or 2 wherein said precoating is comprising, by weight, 5-11 % Si, 2-4% Fe, optionally between 15 and 30ppm Ca, the remainder being aluminium and impurities inherent in processing, said temperature Tj is comprised between 567and 577°C, and said temperature Tm is comprised between 855 and 9500C.
4. A manufacturing process of a hot stamped coated part, comprising the following successive steps, in this order :
- providing a hot rolled or cold rolled steel sheet comprising a steel substrate and an aluminium or aluminium-alloy precoating, said precoating containing more than 50% of free aluminium and having a thickness selected to enable alloying with said steel substrate, said thickness being preferably comprised between 15 and 50 micrometers, then
- cutting said steel sheet to obtain a precoated steel blank, then
- heating said steel blank under a non-protective atmosphere at a heating rate V up to a temperature Tm, in order to transform, preferably fully transform, the steel substrate microstructure into austenite and to obtain, immediately after heating and prior to ulterior soaking, a limited proportion of liquid phase on the surface of said precoating, said proportion being preferably comprised between 10 and 60%, then,
- transforming said liquid phase of the precoating at the temperature Tm during a soaking period U in order to obtain a coated heated blank with a coating having less than 30% of liquid phase on its surface at the end of said soaking period, and comprising by weight between 20 and 50% Fe on said surface, then
- hot stamping said blank in order to obtain a hot stamped part, then - cooling said stamped part in order to form a microstructure in said steel substrate comprising at least one constituent chosen among martensite or bainite.
5. A process according to any of the claims 1 to 4 wherein said heating is performed at least partly by induction heating.
6. A process according to any of the claims 1 to 4 wherein said heating is performed at least partly by resistance heating.
7. A process according to any of the claims 1 to 4 wherein said heating is performed at least partly by infrared heating.
8. A process according to any of the claims 1 to 4 wherein said heating is performed at least partly by gas burners.
9. A process according to any of the claims 1 to 4 wherein said heating is performed by any combination of the heating processes according to claims 5 to 8.
10. A process according to any of the claims 1 to 9 wherein the total thickness of said coating is comprised between 20 and 60 micrometers.
11. A hot stamped coated part comprising a steel substrate having a microstructure comprising at least one constituent chosen among bainite or martensite, and a coating on each one of the two sides of said substrate, said coating being composed of the following layers, starting from the layer contiguous to said steel substrate: - a Fe3AI layer
- a FeAI layer atop of the said Fe3AI layer
-an external layer composed of more than 70% of FeAI3, said FeAI3 layer containing a discontinuous minor phase of FeAI, atop of said FeAI layer
12. A hot stamped part according to claim 11 , wherein said FeAI layer atop of said Fe3AI layer has less than 13%Si in solid solution, wherein said FeAI3 in said external layer has less than 6%Si in solid solution, and wherein said discontinuous minor phase of FeAI has less than 13%Si in solid solution.
13. A hot stamped coated part according to any of claims 11 and 12, wherein the sum of thicknesses of said layer Fe3AI and said layer FeAI is less than one third of the total thickness of said coating.
14. A hot stamped coated part according to any of the claims 11 to 13 wherein the thickness of said coating on each one of said sides is comprised between 20 and 60 micrometers.
15. A hot stamped part according to any of claims 11 to 14 wherein more than 70% the surface of said external layer is composed of crystals.
PCT/EP2009/000670 2009-02-02 2009-02-02 Fabrication process of coated stamped parts and parts prepared from the same WO2010085983A1 (en)

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PCT/EP2009/000670 WO2010085983A1 (en) 2009-02-02 2009-02-02 Fabrication process of coated stamped parts and parts prepared from the same
ES10702612T ES2796928T3 (en) 2009-02-02 2010-02-01 Manufacturing process of coated stamped parts and parts prepared from it
JP2011546717A JP5551184B2 (en) 2009-02-02 2010-02-01 Coated stamping part manufacturing method and part made therefrom
US13/147,178 US10131117B2 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts
PL10702612T PL2391508T3 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
CN201080006436.1A CN102300707B (en) 2009-02-02 2010-02-01 Method for producing coated stamped parts and parts produced thereby
MX2011008114A MX351661B (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same.
HUE10702612A HUE050213T2 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
PCT/EP2010/000586 WO2010086186A1 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
CA2751062A CA2751062C (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
RU2011136436/05A RU2490133C2 (en) 2009-02-02 2010-02-01 Method of forming parts with coating and parts thus produced
MA34139A MA33095B1 (en) 2009-02-02 2010-02-01 PROCESS FOR MANUFACTURING COATED STAMPED PARTS AND PARTS PREPARED THEREFROM
BRPI1007895A BRPI1007895B1 (en) 2009-02-02 2010-02-01 manufacturing process of coated stamped parts and parts prepared from the same
KR1020117020574A KR101658685B1 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
UAA201110594A UA97934C2 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts (embodiments) and parts prepared from the same
EP10702612.2A EP2391508B1 (en) 2009-02-02 2010-02-01 Fabrication process of coated stamped parts and parts prepared from the same
ZA2011/05023A ZA201105023B (en) 2009-02-02 2011-07-07 Fabrication process of coated stamped parts and parts prepared from the same

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BRPI1007895B1 (en) 2020-04-07
CA2751062A1 (en) 2010-08-05

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