EP2683839B1 - Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci - Google Patents
Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci Download PDFInfo
- Publication number
- EP2683839B1 EP2683839B1 EP12708008.3A EP12708008A EP2683839B1 EP 2683839 B1 EP2683839 B1 EP 2683839B1 EP 12708008 A EP12708008 A EP 12708008A EP 2683839 B1 EP2683839 B1 EP 2683839B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- strip
- martensite
- temperature
- austenite
- carbon
- 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.)
- Revoked
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- 229910000831 Steel Inorganic materials 0.000 title claims description 58
- 239000010959 steel Substances 0.000 title claims description 58
- 238000000034 method Methods 0.000 title claims description 28
- 230000008569 process Effects 0.000 title claims description 13
- 229910000734 martensite Inorganic materials 0.000 claims description 55
- 229910052799 carbon Inorganic materials 0.000 claims description 53
- 229910001566 austenite Inorganic materials 0.000 claims description 50
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 39
- 238000010791 quenching Methods 0.000 claims description 33
- 230000015572 biosynthetic process Effects 0.000 claims description 28
- 238000001816 cooling Methods 0.000 claims description 25
- 238000000137 annealing Methods 0.000 claims description 23
- 229910052748 manganese Inorganic materials 0.000 claims description 13
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- 229910001563 bainite Inorganic materials 0.000 claims description 12
- 150000001247 metal acetylides Chemical class 0.000 claims description 10
- 229910000859 α-Fe Inorganic materials 0.000 claims description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 229910052710 silicon Inorganic materials 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 238000005246 galvanizing Methods 0.000 claims description 5
- 230000000717 retained effect Effects 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 229910052757 nitrogen Inorganic materials 0.000 claims description 4
- 229910052787 antimony Inorganic materials 0.000 claims description 3
- 229910052796 boron Inorganic materials 0.000 claims description 3
- 229910052791 calcium Inorganic materials 0.000 claims description 3
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910001562 pearlite Inorganic materials 0.000 claims description 3
- 229910052698 phosphorus Inorganic materials 0.000 claims description 3
- 238000003303 reheating Methods 0.000 claims description 3
- 229910001567 cementite Inorganic materials 0.000 claims description 2
- 229910052717 sulfur Inorganic materials 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims 1
- 238000000638 solvent extraction Methods 0.000 description 31
- 238000007792 addition Methods 0.000 description 26
- 230000009466 transformation Effects 0.000 description 25
- 239000011572 manganese Substances 0.000 description 24
- 239000000203 mixture Substances 0.000 description 19
- 230000006641 stabilisation Effects 0.000 description 17
- 238000012545 processing Methods 0.000 description 11
- 238000005728 strengthening Methods 0.000 description 9
- 229910045601 alloy Inorganic materials 0.000 description 8
- 239000000956 alloy Substances 0.000 description 8
- 238000005266 casting Methods 0.000 description 8
- 230000001965 increasing effect Effects 0.000 description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 7
- 239000004411 aluminium Substances 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 230000001737 promoting effect Effects 0.000 description 7
- 239000011651 chromium Substances 0.000 description 6
- 239000010960 cold rolled steel Substances 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 230000000171 quenching effect Effects 0.000 description 5
- 238000005496 tempering Methods 0.000 description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 4
- 238000005097 cold rolling Methods 0.000 description 4
- 239000002131 composite material Substances 0.000 description 4
- 238000007571 dilatometry Methods 0.000 description 4
- 238000005098 hot rolling Methods 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 239000011701 zinc Substances 0.000 description 4
- 229910052725 zinc Inorganic materials 0.000 description 4
- QFGIVKNKFPCKAW-UHFFFAOYSA-N [Mn].[C] Chemical compound [Mn].[C] QFGIVKNKFPCKAW-UHFFFAOYSA-N 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000011575 calcium Substances 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000013067 intermediate product Substances 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 239000010955 niobium Substances 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 230000000979 retarding effect Effects 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000002939 deleterious effect Effects 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 230000010339 dilation Effects 0.000 description 2
- 230000001747 exhibiting effect Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000012467 final product Substances 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 229910001035 Soft ferrite Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910000797 Ultra-high-strength steel Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- -1 iron carbides Chemical class 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 210000001331 nose Anatomy 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 231100000572 poisoning Toxicity 0.000 description 1
- 230000000607 poisoning effect Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000000844 transformation Methods 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
-
- 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
- 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
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
- C23C2/0224—Two or more thermal pretreatments
-
- 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
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0278—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
Definitions
- WO2010/029983 discloses a method for manufacturing a high-strength steel sheet, comprising hot-rolling and then cold-rolling a billet to be formed into a steel sheet having the composition on a mass percent basis: 0.17%-0.73% C; 3.0% or less Si; 0.5%-3.0% Mn; 0.1% or less P; 0.07% or less S; 3.0% or less Al; 0.010% or less N, balance Fe and incidental impurities to form a cold-rolled steel sheet, annealing the cold-rolled steel sheet in an austenite single-phase region for 15 seconds to 600 seconds, cooling the cold-rolled steel sheet to a first temperature range of 50 °C to 300 °C at an average cooling rate of 8 °C/s or more, heating the cold-rolled steel sheet to a second temperature range of 350 °C to 490 °C, and maintaining the cold-rolled steel sheet at the second temperature range for 5 seconds to 1000 seconds.
- austenite is simply chemically stabilised by large additions of Mn. Although clearly differentiated strength-ductility combinations can be achieved in this way, processing has proven to be difficult since hard, brittle martensitic phases are developed in intermediate product. This renders further processing, such as cold rolling, difficult at dimensions relevant to commercial processing. Furthermore, alloy costs are high due to the high manganese content.
- the steel is then subjected to a thermal treatment to partition carbon from the martensite into the austenite.
- the carbon enrichment of the austenite fraction is achieved by partitioning from martensite or low temperature bainitic transformation or preferably a combination of both. By this partitioning, the formation of carbides is suppressed and the austenite is stabilised rather than decomposed.
- Combined stabilisation with partitioning and bainitic transformation enables the amount of austenite and the microstructure in which it is embedded to be optimised.
- the bainitic transformation also leads to carbon enrichment of the remaining austenite because the formation of carbides is suppressed. All compositions are given in weight percentages, unless otherwise indicated.
- the final microstructure of the steel comprises martensite, bainite and carbon-enriched austenite and, if T 1 ⁇ Ac 3 , equiaxed ferrite.
- the stabilisation of austenite results in the steel exhibiting improved ductility relative to traditional high strength steels.
- V Vanadium
- C Vanadium
- N Vanadium
- V addition up to 0.4wt% is effective. Higher additions are undesirable for reasons of cost and because excessive levels of precipitation tie up high amounts of C. Since free C is required for austenite stabilisation too high V requires increased C addition.
- V is below 0.1%.
- the equilibrium transformation temperature Ae 3 is only determined by the composition, the value of the corresponding Ac 3 temperature is not a constant value as its value depends among others on the heating rate during which Ac 3 is measured and the starting microstructure of the steel. Usually Ac 3 is determined using dilatometry. When the heating rate used during dilatometry and the microstructure of the test specimen are those used in the process according to the invention, the value of Ac 3 is easy to determine.
- the correct balance of isothermal holding temperature and isothermal holding time must be chosen for each composition. These can be determined by means of dilatometry as described hereinbelow.
- the partitioning temperature and time are chosen such as to optimise the enrichment of carbon in the austenite but without creation of deleterious microstructures during the isothermal hold.
- the strip is cooled to ambient temperature.
- the strip may also be coated with zinc or other such metallic layers using a suitable method of deposition either in-line or in a following process step.
- Si is preferred to that of Al such that a minimum silicon content of 1wt% and a max maximum aluminium content of 0.5 wt% is defined.
- Si provides substantial strengthening allowing the achievement of ultra high strength, more effectively suppresses carbide formation enabling longer isothermal holds without formation of large volumes of coarse iron carbides, and because it does not accelerate bainite formation to the same extent as Al thus preventing excessive formation of bainite and enabling higher strengths to be achieved.
- the metal or metal alloy coating is zinc, aluminium, magnesium or alloys thereof.
- the steel is afforded sacrificial corrosion protection since the zinc and aluminium will oxidise in preference to iron in the steel.
- the metallic coating is provided by hot-dip galvanising or by electro-galvanising.
- the partitioning step for 20s at 330°C shows no dilation of the sample, which means that no bainite is formed, carbon is partitioned and the martensite is only marginally tempered.
- the transformation to martensite re-starts at temperatures lower than the quench temperature of 280°C, namely at 250°C, which indicates that the austenite has been stabilized due to carbon partitioning.
- Increased partition times at 330°C show that the transformation to martensite re-starts at lower temperatures than 250°C.
- the dilation observed during annealing of the sample for 20s at 440°C means that bainite is formed.
- carbon is partitioned and the martensite is tempered. The consequence of this high partitioning temperature is that the martensite is severely tempered.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Claims (14)
- Procédé de production d'un acier trempé et partitionné en utilisant une bande d'acier laminée à froid et recuite contenant (en % en poids) :• 0,18 - 0,4 % C• 1,5 - 4,0 % Mn• 0,5 - 2,0 % Si• 0 - 1,5 % Al• 0 - 0,5 % Mo• 0 - 0,5% Ti• 0 - 0,1 % V• 0 - 0,010 % Nb• 0 - 0,005 % B• 0 - 0,015 % N• 0 - 0,08 % P• 0-0,01 %S• 0 - 0,06 % Sb• 0 - 0,05 % Ca• 0 - 0,5 % Cr• 0-1,0% Ni• le reste étant du fer et des impuretés inévitablesdans lequel le procédé de recuit comprend les étapes suivantes :(i) réchauffer la bande laminée à froid à une température de recuit T1 comprise entre Ac3-40 et Ac3+80 ;(ii) maintenir la bande à T1 pendant un temps de recuit t1 compris entre 10 et 200 secondes ;(iii) refroidir la bande recuite à la vitesse de refroidissement critique CR1 pour éviter la formation de ferrite et de perlite à une température de trempe T2 pour produire une microstructure dans la bande comprenant une fraction de martensite et une fraction d'austénite résiduelle ;(iv) recuire pour repartitionnement la bande refroidie à une température T3 pour enrichir l'austénite en carbone en repartitionnant le carbone à partir de la martensite à la fraction d'austénite pendant un temps de repartitionnement t2 compris entre 20 et 500 secondes, dans lequel la fraction de martensite est comprise entre 60 et 90 % de la microstructure au début du recuit de repartitionnement dans lequel (Ms-70) < T3 ≤ (Ms+50) ;(v) refroidir la bande à une vitesse de refroidissement CR2 à température ambiante.
- Procédé selon la revendication 1, dans lequel CR1 est d'au moins 30 °C/s.
- Procédé selon la revendication 1 ou 2, dans lequel la fraction de martensite est au maximum de 85 % de la microstructure au début du recuit de partitionnement.
- Procédé selon l'une quelconque des revendications précédentes, dans lequel T1 est supérieure à Ac3.
- Procédé selon l'une quelconque des revendications précédentes, dans lequel la bande laminée à froid contient au maximum 0,5 % d'Al.
- Procédé selon l'une quelconque des revendications précédentes, dans lequel la bande laminée à froid contient au moins 0,25 % de C et au moins 0,01 % d'Al.
- Procédé selon l'une quelconque des revendications précédentes, dans lequel T2 est égale à T3.
- Procédé selon l'une quelconque des revendications 1 à 7 dans lequel T2 est inférieure à T3.
- Procédé selon l'une quelconque des revendications précédentes, dans lequel la bande laminée à froid et recuite est revêtue d'une ou plusieurs couche(s) métallique(s), de préférence dans lequel l'étape de fourniture de revêtement métallique est par galvanisation à chaud ou électro-galvanisation.
- Bande d'acier produite par l'une quelconque des revendications 1 à 10, dans laquelle l'acier a une microstructure contenant au moins 5 % d'austénite, dans laquelle la microstructure contient de 60 à 90 % (en volume) de martensite traitée thermiquement et dans laquelle un e-rapport est d'au moins 1,8 et une résistance à la traction (UTS) d'au moins 900 MPa, dans laquelle l'e-rapport est défini comme emeasured/ecalculated et dans laquelle ecalculated est calculé selon :
et dans laquelle emeasured est l'allongement mesuré à partir d'un échantillon de longueur de calibre de 80 mm à 1 mm d'épaisseur, ou dans laquelle emeasured est l'allongement mesuré à une autre géométrie et converti en un allongement équivalent sur un calibre de 80 mm à 1 mm d'épaisseur à l'aide de : - Bande d'acier selon la revendication 11, dans laquelle la microstructure contient en outre un ou plusieurs parmi la bainite, la martensite, la martensite trempée, la ferrite, les carbures fins.
- Bande d'acier selon la revendication 11 ou 12, dans laquelle la microstructure ne contient pas de ferrite et/ou de cémentite grossière.
- Bande d'acier selon l'une quelconque des revendications 11 à 13, dans laquelle le rapport limite d'élasticité/résistance à la traction est d'au moins 0,6.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12708008.3A EP2683839B1 (fr) | 2011-03-07 | 2012-03-07 | Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11157239 | 2011-03-07 | ||
EP12708008.3A EP2683839B1 (fr) | 2011-03-07 | 2012-03-07 | Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci |
PCT/EP2012/053856 WO2012120020A1 (fr) | 2011-03-07 | 2012-03-07 | Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci |
Publications (2)
Publication Number | Publication Date |
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EP2683839A1 EP2683839A1 (fr) | 2014-01-15 |
EP2683839B1 true EP2683839B1 (fr) | 2015-04-01 |
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EP12708008.3A Revoked EP2683839B1 (fr) | 2011-03-07 | 2012-03-07 | Procédé pour produire un acier formable à haute résistance et acier formable à haute résistance produit par celui-ci |
Country Status (3)
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EP (1) | EP2683839B1 (fr) |
ES (1) | ES2535420T3 (fr) |
WO (1) | WO2012120020A1 (fr) |
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- 2012-03-07 ES ES12708008.3T patent/ES2535420T3/es active Active
- 2012-03-07 EP EP12708008.3A patent/EP2683839B1/fr not_active Revoked
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US11136656B2 (en) | 2015-05-21 | 2021-10-05 | Cleveland-Cliffs Steel Properties Inc. | High manganese 3rd generation advanced high strength steels |
CN106244924A (zh) * | 2016-08-31 | 2016-12-21 | 东北大学 | 一种冷轧淬火延性钢及制备方法 |
CN106244924B (zh) * | 2016-08-31 | 2017-12-29 | 东北大学 | 一种冷轧淬火延性钢及制备方法 |
EP3899067B1 (fr) * | 2018-12-18 | 2023-09-13 | ArcelorMittal | Tôle d'acier laminée à froid traitée thermiquement et son procédé de fabrication |
WO2023170245A1 (fr) * | 2022-03-10 | 2023-09-14 | Tata Steel Nederland Technology B.V. | Tôle d'acier à haute résistance présentant une excellente extensibilité de trou et son procédé de production |
Also Published As
Publication number | Publication date |
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WO2012120020A1 (fr) | 2012-09-13 |
EP2683839A1 (fr) | 2014-01-15 |
ES2535420T3 (es) | 2015-05-11 |
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