EP0747496B1 - Tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité renfermant du titane, et ses procédés de fabrication - Google Patents
Tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité renfermant du titane, et ses procédés de fabrication Download PDFInfo
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- EP0747496B1 EP0747496B1 EP96401006A EP96401006A EP0747496B1 EP 0747496 B1 EP0747496 B1 EP 0747496B1 EP 96401006 A EP96401006 A EP 96401006A EP 96401006 A EP96401006 A EP 96401006A EP 0747496 B1 EP0747496 B1 EP 0747496B1
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 59
- 239000010959 steel Substances 0.000 title claims abstract description 59
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims abstract description 13
- 239000010936 titanium Substances 0.000 title claims description 47
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims description 26
- 238000004519 manufacturing process Methods 0.000 title claims description 10
- 238000001816 cooling Methods 0.000 claims abstract description 24
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 19
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 14
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 12
- 229910001563 bainite Inorganic materials 0.000 claims abstract description 8
- 238000005098 hot rolling Methods 0.000 claims abstract description 8
- 150000004767 nitrides Chemical class 0.000 claims abstract description 8
- 150000003568 thioethers Chemical class 0.000 claims abstract description 8
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 6
- 150000001247 metal acetylides Chemical class 0.000 claims abstract description 6
- 239000000203 mixture Substances 0.000 claims description 12
- 238000005096 rolling process Methods 0.000 claims description 7
- 238000010583 slow cooling Methods 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 2
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 abstract description 9
- 229910052799 carbon Inorganic materials 0.000 abstract description 7
- 238000001556 precipitation Methods 0.000 abstract description 6
- 229910052717 sulfur Inorganic materials 0.000 abstract description 5
- 229910052782 aluminium Inorganic materials 0.000 abstract description 4
- 229910052804 chromium Inorganic materials 0.000 abstract description 4
- 229910052748 manganese Inorganic materials 0.000 abstract description 4
- 229910052698 phosphorus Inorganic materials 0.000 abstract description 4
- 239000010955 niobium Substances 0.000 description 23
- 230000009466 transformation Effects 0.000 description 16
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 12
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 8
- 239000011572 manganese Substances 0.000 description 8
- 239000010703 silicon Substances 0.000 description 8
- 239000011651 chromium Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 235000001508 sulfur Nutrition 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 239000002244 precipitate Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 239000011593 sulfur Substances 0.000 description 3
- -1 titanium carbides Chemical class 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000001000 micrograph Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- 241000282376 Panthera tigris Species 0.000 description 1
- 229910004283 SiO 4 Inorganic materials 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 101150087698 alpha gene Proteins 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- SOQBVABWOPYFQZ-UHFFFAOYSA-N oxygen(2-);titanium(4+) Chemical class [O-2].[O-2].[Ti+4] SOQBVABWOPYFQZ-UHFFFAOYSA-N 0.000 description 1
- 235000008373 pickled product Nutrition 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0426—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0447—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
- C21D8/0463—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment following hot rolling
Definitions
- the invention relates to the steel industry. More specifically, it concerns the field hot-rolled steel sheets which should have high strength properties and drawability, especially for the automotive industry to form parts of vehicle structures.
- HLE steels are steels microalloyed with niobium, titanium or vanadium. They have a high elastic limit, the minimum according to the grade can range from approximately 300 MPa to approximately 700 MPa, obtained thanks to a refinement of the ferritic grain and a fine hardening precipitation. However, their formability is limited, especially for the highest grades. They have a high elastic limit / tensile strength (R e / R m ) ratio.
- the so-called “double phase” or “dual phase” steels have a microstructure composed of ferrite and martensite. Ferritic transformation is favored by rapid cooling of the sheet, from the end of the hot rolling, to a temperature below Ar 3 , followed by slow cooling in air. The martensitic transformation is then obtained by rapid cooling to a temperature below M s . For a given resistance level, these steels have excellent formability, but this degrades for resistances greater than 650 MPa, due to the large proportion of martensite that they contain.
- TRIP transformation Induced Plasticity steels have a microstructure composed of ferrite, bainite and residual austenite. They allow reach very high resistances, but their weldability is very low due to their high carbon content.
- hot-rolled sheet steels whose structure essentially contains ferrite hardened by precipitates of titanium carbide and / or niobium and martensite, or even residual austenite. These steels have the composition, expressed in weight percentages: C ⁇ 0.18%; 0.5 ⁇ If ⁇ 2.5%; 0.5 ⁇ Mn ⁇ 2.5%; P ⁇ 0.05%; S ⁇ 0.02%; 0.01 ⁇ A1 ⁇ 0.1%; 0.0 2 ⁇ Ti ⁇ 0.5% and / or 0.03 ⁇ Nb ⁇ 1%, with C% ⁇ 0.05 + Ti / 4 + Nb / 8.
- the object of the invention is to provide users of rolled steel sheets with hot products with a very good compromise between resistance levels good formability and good weldability, as well as a flawless surface.
- the invention also relates to methods of manufacturing such sheets.
- the sheets according to the invention are distinguished from those known hitherto for the same uses firstly by their substantially lower content in silicon, their ranges of titanium and niobium contents significantly narrowed, and stricter requirements on the distribution of the different phases of the structure. And obtaining the structure, therefore the desired properties for the sheet, involves special conditions during the heat treatment immediately following hot rolling.
- Their composition and manufacturing method mean that these steels represent, in several respects, a combination of HLE steels and double steels phase.
- a steel comprising (all percentages are percentages by weight) a lower carbon content or equal to 0.12%, a manganese content of between 0.5 and 1.5%, a content of silicon less than or equal to 0.3%, a phosphorus content less than or equal to 0.1%, sulfur content less than or equal to 0.05%, aluminum content between 0.01 and 0.1%, a chromium content of less than 1%, a content of effective titanium (we will explain below what this term means) between 0.03 and 0.15% and a niobium content of between 0 and 0.05%.
- the slab is then hot rolled on a strip train to form a sheet a few mm thick.
- the sheet undergoes a heat treatment which gives it a microstructure composed at least 75% ferrite and at least 10% martensite.
- the ferrite is hardened by a precipitation of titanium carbides or carbonitrides, and also of carbides or niobium carbonitrides if this element is present significantly.
- the microstructure may optionally also include bainite and austenite residual.
- Silicon is an alpha-element, which therefore promotes ferritic transformation. It is also hardening in solid solution.
- the invention is based, among other things, on a very significant drop in the silicon content of the steel compared to the prior art illustrated by document EP 0 548 950.
- the advantage of a significant drop in the content of silicon is that the surface appearance problems encountered on steels of the prior art arise, in fact, from an appearance on the surface of the slab, in the reheating furnace, of oxide Fe 2 SiO 4 which forms with FeO oxide a low melting eutectic. This eutectic penetrates into the grain boundaries and promotes the anchoring of the scale, which can therefore only be imperfectly removed during pickling.
- Another advantage of this lowering of the silicon content is the improvement in the weldability of the steel.
- the steels of the invention provided that the other specifications on their composition and method of manufacture are respected, tolerate having only low, or even very low, silicon contents.
- phosphorus is alphagene and hardens. But its content should be limited to 0.1%, and may be as low as possible. Indeed, it would likely, at high content, to form a mid-thickness segregation which could cause delamination. Furthermore, it can segregate at grain boundaries, which increases fragility.
- chromium Although not strictly speaking necessary, an addition of chromium (limited at 1%) is recommended because it promotes the formation of martensite and the ferritic transformation.
- Titanium is a micro-alloying element which forms precipitates of carbide and carbonitride hardening ferrite. Its addition is intended to obtain, thanks to this hardening, a high level of resistance. However, this effect is only obtained if titanium has the possibility of combining with carbon.
- account must therefore be taken of the possibilities of titanium oxides, nitrides and sulfides. The significant formation of oxides can be easily avoided by adding aluminum during the deoxidation of the liquid steel. As for the quantities of nitrides and sulphides formed, they depend on the nitrogen and sulfur contents of the liquid steel.
- titanium it is not possible, during preparation and casting, to drastically limit these nitrogen and sulfur contents, a sufficient amount of titanium must be added to the metal bath so that in the solidified metal, after precipitation nitrides and sulfides, the titanium content not in the form of nitrides, sulfides or oxides (and therefore available to form carbides and carbonitrides) is between 0.03 and 0.15%. It is this content which is called “effective titanium content” and which is shortened to "Ti eff %".
- Ti eff % Ti total % - 3.4 x N% - 1.5 x S%.
- This addition of titanium can advantageously be supplemented by an addition niobium to achieve even higher resistance levels.
- niobium makes the sheet more difficult to laminate.
- adding titanium and niobium beyond the prescribed amounts is unnecessary, because we would then see a saturation of the hardening effect.
- the sheet can be wound, either immediately, or after a stay in the air.
- the sheet metal can then be wound, again with or without a previous stay in the air.
- niobium nitrides and carbonitrides slows down ferritic transformation. It is therefore desirable that the duration of the slow cooling step during which the ferritic transformation is sufficient to ensure the smooth running of this transformation. For procedure No. 1 which was previously described, we therefore recommend that step 1 last at least 8 s. For procedure No. 2, a minimum duration of stage 2 of 5 s is recommended.
- the micrograph in Figure 1 shows the structure of a steel corresponding to grade B with 0.030% titanium.
- the cooling of the sheet after hot rolling has was carried out according to procedure No. 2.
- the clear areas are equiaxed ferrite and represent 88% of the structure.
- the dark beaches are martensite, and represent almost the entire remainder of the structure.
- Figure 2 shows the structure of a steel corresponding to the grade C with 0.060% titanium.
- the cooling of the sheet after hot rolling has was carried out according to procedure No. 2
- the equiaxed ferrite represents 86% of the structure.
- the steels according to the invention can be used in particular to constitute parts of motor vehicle structures, such as chassis elements, wheel sails, suspension arms, as well as all stamped parts in front have a high resistance to mechanical stress.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
Description
C ≤ 0,18 %; 0,5 ≤ Si ≤ 2,5 %; 0,5 ≤ Mn ≤2,5 %; P ≤ 0,05 %; S ≤ 0,02 %; 0,01 ≤ A1 ≤ 0,1%;0,0 2≤ Ti ≤ 0,5% et/ou 0,03 ≤ Nb ≤ 1%, avec C% ≥ 0,05+Ti/4 + Nb/8.
- C ≤ 0,12 %;
- 0,5 ≤ Mn ≤ 1,5 %;
- 0 ≤ Si ≤ 0,3 %;
- 0 ≤ P ≤ 0,1%;
- 0 ≤ S ≤ 0,05 %;
- 0,01 ≤ Al ≤ 0,1 %;
- 0 ≤ Cr ≤ 1 %;
- 0,03 ≤ Tieff ≤ 0,15 %, Tieff étant la teneur en titane non sous forme de nitrures, de sulfures ou d'oxydes;
- 0 ≤ Nb ≤ 0,05 %;
- reste fer et impuretés inévitables;
- il se place en solution solide;
- en abaissant le point Ar3, il permet d'abaisser la température de fin de laminage et d'obtenir un grain ferritique fin;
- c'est un élément trempant.
- C ≤ 0,12 %;
- 0,5 ≤ Mn ≤ 1,5 %;
- 0 ≤ Si ≤ 0,3 %;
- 0 ≤ P ≤ 0,1%;
- 0 ≤ S ≤ 0,05 %;
- 0,01 ≤ Al ≤ 0,1 %;
- 0 ≤ Cr ≤ %;
- 0,03 ≤ Tieff ≤ 0,15 %, Tieff étant la teneur en titane non sous forme de nitrures, de sulfures ou d'oxydes;
- 0 ≤ Nb ≤ 0,05 %;
- étape 1: refroidissement lent, à l'air, à une vitesse de 2 à 15 °C/s, effectué enttre TFL et une température dite "température de début de trempe" (TDT) située entre 730 °C et le point Ar1 de la nuance coulée; c'est au cours de ce refroidissement qu'a lieu la transformation ferritique; il ne doit pas durer plus de 40 s pour ne pas aboutir à des précipités de trop forte taille qui détérioreraient la résistance à la traction de la tôle;
- étape 2: refroidissement rapide, effectué par exemple par aspersion à l'eau, à une vitesse de 20 à 150 °C/s entre TDT et une température dite "température de fin de refroidissement" (TFR) qui est inférieure ou égale à 300 °C.
- étape 1: refroidissement rapide, à l'eau, à une vitesse de 20 à 150°C/s, commençant moins de 10 s après la fin du laminage à chaud, entre TFL et une température intermédiaire (Tinter) inférieure au point Ar3 de la nuance; pendant cette opération, l'acier reste dans le domaine austénitique;
- étape 2: refroidissement lent, à l'air, à une vitesse de 2 à 15 °C/s, d'une durée inférieure à 40 s, entre Tinter et TDT, qui est comprise entre le point Ar1 de la nuance et 730 °C; la transformation ferritique a lieu au cours de cette étape;
- étape 3: refroidissement rapide, à l'eau, à une vitesse de 20 à 150 °C/s, entre TDT et TFR, cette dernière température étant inférieure ou égale à 300 °C.
- une transformation plus rapide, donc plus complète pour une durée donnée du refroidissement à l'air, qui elle-même peut être limitée par la longueur de la table de refroidissement;
- une taille de grain ferritique plus faible;
- une précipitation de carbures et de carbonitrures de titane et niobium plus fine et plus durcissante.
Nuances d'acier testées | |||||||||
Nuance | C % | Mn % | P % | Si % | Cr % | N % | S % | Tieff % | Nb % |
A (référence) | 0,072 | 0,982 | 0,040 | 0,190 | 0,750 | 0,0059 | 0,0021 | - | - |
B | 0,075 | 0,965 | 0,040 | 0,190 | 0,760 | 0,0046 | 0,0025 | 0,030 | - |
C | 0,072 | 0,955 | 0,040 | 0,180 | 0,760 | 0,0046 | 0,0018 | 0,060 | - |
D | 0,077 | 0,862 | 0,043 | 0,180 | 0,770 | 0,0057 | 0,0025 | 0,110 | - |
E | 0,080 | 1,200 | 0,040 | 0,220 | 0,750 | 0,0052 | 0,0022 | 0,0120 | 0,040 |
Résultats expérimentaux | ||||||
Nuance | Mode de refroidissement | TDT (°C) | Rp0,2 (MPa) | Rm (MPa) | Rp0,2/Rm | n |
A (référence) | N°2 | 720 | 319 | 590 | 0,54 | 0,20 |
A (référence) | N°2 | 650 | 308 | 570 | 0,54 | 0,20 |
B | N°1 | 730 | 425 | 685 | 0,62 | 0,16 |
B | N°1 | 660 | 501 | 748 | 0,67 | 0,15 |
B | N°2 | 730 | 511 | 774 | 0,66 | 0,16 |
B | N°2 | 660 | 492 | 745 | 0,66 | 0,14 |
C | N°1 | 720 | 475 | 730 | 0,65 | 0,15 |
C | N°1 | 650 | 535 | 764 | 0,70 | 0,15 |
C | N°2 | 720 | 549 | 820 | 0,67 | 0,13 |
C | N°2 | 650 | 528 | 800 | 0,66 | 0,13 |
D | N°1 | 710 | 615 | 848 | 0,72 | 0,12 |
D | N°1 | 620 | 648 | 865 | 0,75 | 0,12 |
E | N°2 | 710 | 595 | 860 | 0,69 | 0,12 |
Claims (6)
- Tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité, caractérisée en ce que sa composition, exprimée en pourcentages pondéraux, est:C ≤ 0,12 %;0,5 ≤ Mn ≤ 1,5 %;0 ≤ Si ≤ 0,3 %;0 ≤ P ≤ 0,1 %;0 ≤ S ≤ 0,05 %;0,01 ≤ Al ≤ 0,1 %;0 ≤ Cr ≤ 1 %;0,03 ≤ Tieff ≤ 0,15 %, Tieff étant la teneur en titane non sous forme de nitrures, de sulfures ou d'oxydes;0 ≤ Nb ≤ 0,05 %;reste fer et impuretés inévitables;
- Tôle d'acier selon la revendication 1, caractérisée en ce que sa teneur en Nb est comprise entre 0,02 et 0,05 %.
- Procédé de fabrication d'une tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité, caractérisé en ce que:on élabore et on coule sous forme de brame un acier dont la composition est conforme à celle de la tôle selon la revendication 1;puis on lamine à chaud ladite brame sous forme de tôle en achevant le laminage à une température comprise entre le point Ar3 et 950 °C;puis on applique à ladite tôle un refroidissement lent à une vitesse de 2 à 15 °C/s pendant une durée inférieure à 40 s, jusqu'à une température comprise entre le point Ar1 et 730 °C;puis on applique à ladite tôle un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure ou égale à 300 °C.
- Procédé de fabrication d'une tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité, caractérisé en ce que:on élabore et on coule sous forme de brame un acier dont la composition est conforme à celle de la tôle selon la revendication 1;puis on lamine à chaud ladite brame sous forme de tôle en achevant le laminage à une température comprise entre le point Ar3 et 950 °C;puis on applique à ladite tôle, moins de 10 s après la fin du laminage à chaud, un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure au point Ar3;puis on applique à ladite tôle un refroidissement lent à une vitesse de 2 à 15 °C/s pendant une durée inférieure à 40 s, jusqu'à une température comprise entre le point Ar1 et 730 °C;puis on applique à ladite tôle un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure ou égale à 300 °C.
- Procédé de fabrication d'une tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité, caractérisé en ce que:on élabore et on coule sous forme de brame un acier dont la composition est conforme à celle de la tôle selon la revendication 2;puis on lamine à chaud ladite brame sous forme de tôle en achevant le laminage à une température comprise entre le point Ar3 et 950 °C;puis on applique à ladite tôle un refroidissement lent à une vitesse de 2 à 15 °C/s pendant une durée comprise entre 8 et 40 s, jusqu'à une température comprise entre le point Ar1 et 730 °C;puis on applique à ladite tôle un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure ou égale à 300 °C.
- Procédé de fabrication d'une tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité, caractérisé en ce que:on élabore et on coule sous forme de brame un acier dont la composition est conforme à celle de la tôle selon la revendication 2;puis on lamine à chaud ladite brame sous forme de tôle en achevant le laminage à une température comprise entre le point Ar3 et 950 °C;puis on applique à ladite tôle, moins de 10 s après la fin du laminage à chaud, un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure au point Ar3;puis on applique à ladite tôle un refroidissement lent à une vitesse de 2 à 15 °C/s pendant une durée comprise entre 5 et 40 s, jusqu'à une température comprise entre le point Ar1 et 730 °C;puis on applique à ladite tôle un refroidissement rapide à une vitesse de 20 à 150 °C/s jusqu'à une température inférieure ou égale à 300 °C.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9506745 | 1995-06-08 | ||
FR9506745A FR2735147B1 (fr) | 1995-06-08 | 1995-06-08 | Tole d'acier laminee a chaud a haute resistance et haute emboutissabilite renfermant du titane, et ses procedes de fabrication. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0747496A1 EP0747496A1 (fr) | 1996-12-11 |
EP0747496B1 true EP0747496B1 (fr) | 2000-01-19 |
Family
ID=9479729
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96401006A Revoked EP0747496B1 (fr) | 1995-06-08 | 1996-05-10 | Tôle d'acier laminée à chaud à haute résistance et haute emboutissabilité renfermant du titane, et ses procédés de fabrication |
Country Status (8)
Country | Link |
---|---|
US (1) | US5759297A (fr) |
EP (1) | EP0747496B1 (fr) |
JP (1) | JPH08337840A (fr) |
AT (1) | ATE189008T1 (fr) |
CA (1) | CA2178305A1 (fr) |
DE (1) | DE69606227T2 (fr) |
ES (1) | ES2143725T3 (fr) |
FR (1) | FR2735147B1 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2757877B1 (fr) * | 1996-12-31 | 1999-02-05 | Ascometal Sa | Acier et procede pour la fabrication d'une piece en acier mise en forme par deformation plastique a froid |
BE1013359A3 (fr) * | 2000-03-22 | 2001-12-04 | Centre Rech Metallurgique | Procede pour la fabrication d'une bande en acier multiphase laminee a chaud. |
US6669789B1 (en) | 2001-08-31 | 2003-12-30 | Nucor Corporation | Method for producing titanium-bearing microalloyed high-strength low-alloy steel |
US6837235B2 (en) * | 2002-03-14 | 2005-01-04 | Ssw Holdings Company, Inc. | Porcelain oven rack |
JP4470701B2 (ja) * | 2004-01-29 | 2010-06-02 | Jfeスチール株式会社 | 加工性および表面性状に優れた高強度薄鋼板およびその製造方法 |
US20070272231A1 (en) * | 2006-05-25 | 2007-11-29 | Ssw Holding Company, Inc. | Oven rack having an integral lubricious, dry porcelain surface |
US10053757B2 (en) | 2012-08-03 | 2018-08-21 | Tata Steel Ijmuiden Bv | Process for producing hot-rolled steel strip |
PL2896715T3 (pl) * | 2012-09-26 | 2017-12-29 | Nippon Steel & Sumitomo Metal Corporation | Dwufazowa blacha stalowa cienka i sposób jej wytwarzania |
CN103334057A (zh) * | 2013-06-18 | 2013-10-02 | 首钢总公司 | 一种热轧马氏体钢及其生产方法 |
US10301697B2 (en) * | 2015-11-19 | 2019-05-28 | Nippon Steel & Sumitomo Metal Corporation | High strength hot rolled steel sheet and manufacturing method thereof |
DE102016121905A1 (de) * | 2016-11-15 | 2018-05-17 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung von Radschüsseln aus Dualphasenstahl mit verbesserter Kaltumformbarkeit |
KR101917469B1 (ko) * | 2016-12-23 | 2018-11-09 | 주식회사 포스코 | 재질편차가 적고 표면품질이 우수한 고강도 열연강판 및 그 제조방법 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3897280A (en) * | 1972-12-23 | 1975-07-29 | Nippon Steel Corp | Method for manufacturing a steel sheet and product obtained thereby |
US4033789A (en) * | 1976-03-19 | 1977-07-05 | Jones & Laughlin Steel Corporation | Method of producing a high strength steel having uniform elongation |
US4141761A (en) * | 1976-09-27 | 1979-02-27 | Republic Steel Corporation | High strength low alloy steel containing columbium and titanium |
US4398970A (en) * | 1981-10-05 | 1983-08-16 | Bethlehem Steel Corporation | Titanium and vanadium dual-phase steel and method of manufacture |
JPS6126756A (ja) * | 1984-07-17 | 1986-02-06 | Kawasaki Steel Corp | 良化成処理性を有する極低炭素鋼板 |
JPS63118012A (ja) * | 1986-11-07 | 1988-05-23 | Sumitomo Metal Ind Ltd | 低降伏比高張力厚鋼板の製造法 |
JPH0745687B2 (ja) * | 1987-12-18 | 1995-05-17 | 株式会社神戸製鋼所 | 伸びフランジ性の優れた高強度熱延薄鋼板の製造方法 |
-
1995
- 1995-06-08 FR FR9506745A patent/FR2735147B1/fr not_active Expired - Fee Related
-
1996
- 1996-05-10 EP EP96401006A patent/EP0747496B1/fr not_active Revoked
- 1996-05-10 DE DE69606227T patent/DE69606227T2/de not_active Revoked
- 1996-05-10 ES ES96401006T patent/ES2143725T3/es not_active Expired - Lifetime
- 1996-05-10 AT AT96401006T patent/ATE189008T1/de not_active IP Right Cessation
- 1996-05-15 US US08/648,447 patent/US5759297A/en not_active Expired - Fee Related
- 1996-06-05 CA CA002178305A patent/CA2178305A1/fr not_active Abandoned
- 1996-06-10 JP JP8170671A patent/JPH08337840A/ja not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
FR2735147A1 (fr) | 1996-12-13 |
ATE189008T1 (de) | 2000-02-15 |
DE69606227D1 (de) | 2000-02-24 |
CA2178305A1 (fr) | 1996-12-09 |
JPH08337840A (ja) | 1996-12-24 |
DE69606227T2 (de) | 2000-09-07 |
FR2735147B1 (fr) | 1997-07-11 |
EP0747496A1 (fr) | 1996-12-11 |
US5759297A (en) | 1998-06-02 |
ES2143725T3 (es) | 2000-05-16 |
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